JP2005113683A - Various full rotor blade steam gas turbine combined engine - Google Patents

Various full rotor blade steam gas turbine combined engine Download PDF

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JP2005113683A
JP2005113683A JP2003073042A JP2003073042A JP2005113683A JP 2005113683 A JP2005113683 A JP 2005113683A JP 2003073042 A JP2003073042 A JP 2003073042A JP 2003073042 A JP2003073042 A JP 2003073042A JP 2005113683 A JP2005113683 A JP 2005113683A
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temperature water
heat
vaporization
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supercritical
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Hiroyasu Tanigawa
浩保 谷川
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    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

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Abstract

<P>PROBLEM TO BE SOLVED: To prevent global warming as an internal combustion engine discharging almost no emission of CO2 or the like by cooling tap water by low-temperature combustion gas by setting combustion gas exhaust temperature to be close to -273°C under consideration of preventing of global warming, so that great cold heat is supplied to a user at no manufacturing cost. <P>SOLUTION: In this full rotor blade steam gas turbine combined engine, high pressure combustion heat is exchanged to the utmost in a combustor-heat exchanger. The combustion gas exhaust temperature is set to be close to -273°C, so that roughly full heat quantity of compression air is added to provide almost twice heat recovery quantity of existing boiler. Combustion gas heat quantity power generation quantity is added to combustion gas quantity power generation quantity to provide 270-540 times as much as hypothetical power generation of an existing gas turbine. Electricity cost is thus reduced to 1/10, and tap water heat of 100°C or less to the whole heat quantity is supplied to the user at no manufacturing cost by using a full rotor blade steam turbine provided with a vaporization latent heat recovering device. By a full rotor blade steam gas turbine cold heat recovering device, low temperature combustion gas is wholly converted into tap water cold heat, so that it is supplied to the user at tap water cold heat of 5°C or around, with no emission of CO2. <P>COPYRIGHT: (C)2005,JPO&NCIPI

Description

【０００１】
【発明の属する技術分野】
本発明は既存内燃機関技術が、熱量を殆ど利用しない容積利用で、燃料電池や風力発電と競合する理由を、明快に説明するため、アイディアを仮説数字で説明するが、正解は実験数値とし、アイディア仮説数字に限定しない。例えば最先端再熱蒸気タービンは、熱量を全く利用しない容積利用ため、断熱膨張真空部では１００００倍以上に膨張し、重力仕事率が水の１／１００００以下に低減して、同一出力では１００００倍の動翼面積を必要とし、超臨界圧力等に落差を増大しても速度利用が不可能なため、動翼の１０〜２０倍前後も速度エネルギを消費し、回転仕事をしない静翼を１／２も設け、ボイラで加熱した熱量全部で海水温度を上昇して、仮説発電量を１／５００等に低減しております。そこで高温水と気化爆発力を利用して熱回収再利用再再利用することで、供給熱量を最少の気化熱に近付け、圧縮空気熱量等供給熱量全部の温熱を副産物として需要家に供給し、膨大な冷熱も副産物で供給して、地球温暖化防止する技術に関する。
【０００２】
再熱は逆転して全動翼蒸気ガスタービン合体機関（略称合体機関で説明）燃焼器兼熱交換器４により、限り無く高圧燃焼熱交換燃焼ガス温度を最低にし、熱回収して得た超臨界圧力温度等の高温水回収熱量を最大の、既存ボイラの２倍前後回収熱量にし、加熱高温手段１０１で加熱高温とし、霧吹きの原理９１ｅを利用して超臨界温度等複数温度の高温水５ｂを噴射する、高温水噴射ノズル５９ｂにより、超臨界温度等複数温度の高温水との間に気化膜を設けて、摩擦損失最少で超臨界温度等複数温度の高温水を噴射し、気化爆発エネルギによりノズル内では機関銃の弾丸のように高温水を加速して、気化爆発容積速度利用等により高温水を吹雪等のように加速し、ノズル外では高温水を散弾ロケットや吹雪等のように加速して、気化潜熱を最適利用して熱回収再再再利用し、重力仕事率を最大にして消費熱量を最少にする技術に関する。
【０００３】
大気圧重力仕事率を最先端再熱蒸気タービンの１７００倍高温水出力として、重力仕事率（以下単位容積質量×速度同じとする）を１７００倍に近付け、超臨界圧力から大気圧まで使用して気化熱を回収し、飽和温度１００℃凝縮水を再再再使用することで、回収熱量及び供給熱量を気化熱の最少に近付け、回収熱量全部を温熱として需要家に供給し、同一燃料量既存ガスタービンの５００倍仮説発電量等に上昇します。動翼面積の一部乃至大部分を既存再熱蒸気タービンの１／１７００に縮小して、重力仕事率を考慮することで合理的な動翼面積の設計を可能にし、高温水を略直線蛇行的に噴射して、機械効率を１０〜２０倍に上昇して出力を発生する、全動翼蒸気タービンや全動翼蒸気ガスタービン等とし、静翼で堰き止める無茶苦茶を全廃して、電気料金の１／１０等を狙う技術に関する。
【０００４】
再熱蒸気タービンの復水器真空まで断熱膨張や再熱を逆転して、超臨界圧力から大気圧まで落差も充分とし、気化潜熱回収器６６ａを設けた全動翼蒸気タービンとして、１００℃以下の気化熱全部を回収熱量の温熱として需要家に供給し、凝縮水全部を燃焼器兼熱交換器４に繰り返し再再再供給して、超臨界温度等複数温度の高温水５ｂとし、燃料燃焼熱量の供給を気化熱のみに近付け、単位熱量の重力仕事率を極限まで増大します。燃料燃焼熱量の低減と凝縮水の繰り返し循環使用が可能な、全動翼蒸気タービンにして、加えた燃料燃焼熱量の略全部の膨大な温熱を、副産物の水道水として貯蔵し、製造原価略０で需要家に供給して、既存技術の使用熱量全部で海水温度を上昇する、を皆無にする技術に関する。
【０００５】
既存最先端ガスタービンも容積利用のため、タービン耐熱限界温度により落差の上昇が不可能です。更に動翼の１０〜２０倍前後も速度エネルギを消費して、回転仕事をしない静翼を１／２も設けて、断熱膨張５００℃前後で高温排気し、発電量を１／５００等に低減して、地球温暖化を加速しています。そこで合体機関燃焼器兼熱交換器４により、限り無く高圧燃焼熱交換冷却燃焼して、熱回収量を既存ボイラの２倍前後に増大し、燃焼ガスタービン入口温度を最低にして、燃焼ガス温度と容積の障害を最低にし、燃焼ガスの熱量と質量を有効利用して、同一燃料量既存ガスタービンの５００倍仮説発電量等にする技術に関する。
【０００６】
通常燃料使用の場合、燃焼ガス温度と容積の障害を最低として２倍以上の落差とし、合体機関の全動翼ガスタービンにより略直線蛇行的に噴射して、機械効率を１０〜２０倍に上昇し、燃焼ガス質量出力を発生排気の過程で、燃焼ガス排気温度を−２７３℃に近付（−温度全部を含める）け、冷熱回収器１０２の低温燃焼ガスにより水道水を冷却して、復水器真空（−圧力全部を含める）まで膨張させ、製造原価略０で使用燃焼ガス全部を、膨大な副産物の冷熱水道水に変換して需要家に供給します。用途により燃焼器兼熱交換器４の圧縮空気圧力を、全動翼により極限まで上昇して、ドライアイスや液体窒素等の製造回収を可能にし、燃焼ガス質量仮説発電量を、既存ガスタービンの２０〜４０倍以上等に上昇する技術に関する。
【０００７】
そこで最先端ガスタービンを逆転して、燃焼ガスタービン入口温度を最低にするため、ガスタービン燃焼器を全動翼ガスタービン燃焼器兼熱交換器４とし、全動翼により限り無く高圧圧縮熱交換冷却燃焼して、熱回収量を既存ボイラの２倍前後にすることで、燃焼ガスタービン入口温度を最低とし、該排気温度を−２７３℃に近付け、圧縮した空気の保有熱量略全部を含めて、既存ボイラの２倍前後の回収熱量の燃焼ガス熱量出力とします。そして燃焼ガス熱量出力を、超臨界温度等複数温度の高温水５ｂとして各種用途に利用し、燃焼ガス熱量発電量乃至出力を（既存ガスタービンの５倍落差×２倍熱量×５０倍質量重力仕事率×１０〜２０倍機械効率×１／２０減少率）＝（既存ガスタービンの２５０〜５００倍燃焼ガス熱量仮説発電量乃至出力）等にする技術に関する。
【０００８】
微粉炭燃料燃焼の場合、発電量及び冷熱の回収量を最大にするため、超臨界温度等の最少最適量の高温水５ｂを、全動翼蒸気ガスタービンの最上流に供給し、加熱高温手段１０１により加熱高温として、高温水との間に気化膜を設けて摩擦損失を最少とした、高温水噴射ノズル５９ｂより高温水５ｂを、霧吹きの原理９１ｅを利用して噴射し、気化爆発エネルギや気化爆発容積速度により、ノズル内やノズル外では、高温水を機関銃の弾丸や散弾ロケットや吹雪等のように加速して、全動翼蒸気ガスタービンを駆動し、中流最適段に低温燃焼ガス全部を供給して、出力発生の過程で断熱膨張した低温燃焼ガス灰分を核に水分を凝集して、復水器真空まで膨張を可能にし、最適最少量高温水の使用で冷熱回収量と発電量を最大にして、ＣＯ２等の排気を０等として地球温暖化防止し、燃焼ガス全部を膨大な冷熱に変換して、製造原価略０で需要家に供給する技術に関する。
【０００９】
再熱蒸気タービンを逆転した全動翼蒸気タービンを駆動の過程では、既存ボイラの２倍前後の回収熱量を、超臨界温度等複数温度の高温水供給とし、出力発生の過程では、夫々の高温水加減弁７ａより高温水管６ａを介して、高温水５ｂを夫々の高温水溜３２ａに供給し、夫々加熱高温手段１０１により加熱高温となった高温水噴射ノズル５９ｂより、高温水との間に気化膜を設けて摩擦損失最少で、霧吹きの原理９１ｅを利用して噴射し、気化爆発エネルギや気化爆発容積速度により、ノズル内では機関銃の弾丸や吹雪等のように高温水を加速し、ノズル外では高温水５ｂを散弾ロケットや吹雪等のように加速して、重力仕事率が最先端再熱蒸気タービンの、大気圧部１７００倍重力仕事率の高温水噴射質量を、既存ガスタービンの５０倍等とする技術に関する。
【００１０】
全動翼蒸気ガスタービンでは超臨界温度等複数温度の高温水５ｂを、合体機関の最上流に霧吹きの原理９１ｅを利用して噴射する、高温水噴射ノズル５９ｂより高温水を噴射して駆動の過程で、全動翼により略直線蛇行的に噴射して、機械効率を１０〜２０倍に上昇し、中流最適段に燃料熱量０以下の燃焼ガス質量を供給して、全動翼ガスタービン燃焼ガス質量出力＝（既存ガスタービンの２倍落差×１倍質量×１０〜２０倍機械効率）＝（既存ガスタービンの２０〜４０倍燃焼ガス質量仮説出力）とし、合体機関出力＝（燃焼ガス質量出力＋燃焼ガス熱量出力）＝（既存ガスタービンの２０〜４０倍出力＋２５０〜５００倍出力）＝（既存ガスタービンの２７０〜５４０倍仮説出力）に増大する技術に関する。
【００１１】
供給熱量の略全部を高温水５ｂの気化爆発エネルギに変換して、高温水の重力仕事率を既存ガスタービン燃焼ガスの５０倍質量等に増大し、最適速度の高温水５ｂで出力を発生します。燃焼ガス熱量出力を発生の過程では、夫々加熱高温とした、高温水噴射ノズル５９ｂや、電磁加熱タービン動翼８１の全動翼蒸気タービン等として、高温水との間に気化膜を設けて摩擦損失を最小とし、略直線蛇行的に噴射して機械効率を１０〜２０倍に上昇します。そして既存ボイラの２倍回収熱量の（同一燃料量高温水熱量質量出力）＝（５０倍質量重力仕事率×５倍落差×２倍回収熱量×１０〜２０倍機械効率×１／２０減少率）＝（既存ガスタービンの２５０〜５００倍燃焼ガス熱量仮説出力）等に上昇する技術に関する。
【００１２】
全動翼タービン動翼を電磁誘導加熱高温とするため、電磁調理器と同様にコイル９８を設けて通電し、比透磁率の大きい鉄を含む材料の中に磁力線９９を集めて、うず電流による電気抵抗によってジュール熱を発生し、加熱高温各種の電磁加熱タービン動翼８１を構成します。そして電磁加熱タービン動翼８１と高温水との間に気化膜を設けて、全動翼により略直線蛇行的に噴射して、摩擦損失最小・重力仕事率最大で大気圧まで出力を発生して、構造や容積が１／１０等の大幅に小型簡単な、例えば回転出力輸送機器用としての、全動翼蒸気ガスタービン合体機関の、燃焼ガス熱量出力＋質量出力を（同一燃料量既存ガスタービンの２５０〜５００倍出力＋２０〜４０倍出力）＝（既存ガスタービンの２７０〜５４０倍仮説出力）等の、回転出力輸送機器にする技術に関する。
【００１３】
全動翼ガスタービン圧縮機翼を、撥水性金属・撥水性物質の被覆・撥水性セラミックス・撥水性加工の、何れか１以上で構成の撥水性水冷却翼８７にして、水冷却した低温の全動翼圧縮機翼により、略直線蛇行的に最も効率良く空気を圧縮して空気冷却し、摩擦損失最小で空気を圧縮し、全動翼圧縮機翼を冷却した水を噴射して、直接圧縮空気を冷却の過程で、撥水性水冷却翼８７と水等との間の摩擦損失を低減して熱回収し、圧縮空気圧力を全動翼により極限まで上昇して出力を発生し、ドライアイスや液体窒素等を製造可能にすると共に、燃焼器兼熱交換器４に最も効率良く低温空気を供給する、各種合体機関の技術に関する。
【００１４】
各種合体機関の燃焼器兼熱交換器４により限りなく高圧燃焼熱交換し、圧縮空気保有熱量を含め、燃料発熱量全部＋圧縮空気保有熱量を熱回収し、既存ボイラの２倍前後の熱回収量の超臨界温度等複数温度の高温水５ｂとして、各種合体機関を駆動します。そして起動時には高温水が皆無のため、起動時のみ（燃焼ガス質量×２倍落差×１０〜２０倍機械効率）＝（既存ガスタービンと同一燃焼ガス質量２０〜４０倍仮説出力）により、各種全動翼ガスタービンとして駆動し、燃料の消費熱量を０以下として、該熱効率を無限上昇とします。そして出力発生の過程で高温水温度を上昇し、大気圧や復水器真空まで膨張させる、各種全動翼蒸気ガスタービン合体機関に移行する技術に関する。
【００１５】
合体機関の燃焼器兼熱交換器４により限りなく高圧燃焼熱交換して得た、最低温度の燃焼ガス質量出力＋既存ボイラの２倍前後の回収熱量の超臨界温度等複数温度の高温水５ｂ出力を、夫々大気圧まで使用し（既存ガスタービンと同一質量２倍落差×１０〜２０倍機械効率＋２５０〜５００倍出力）＝（既存ガスタービンの２７０〜５４０倍仮説出力）とします。排気飽和温度１００℃の気化熱を気化潜熱回収器６６ａで回収して、燃焼器兼熱交換器４に給水３として利用の他方で、ＣＯ２等の燃焼ガスを５０倍質量等の凝縮水に溶解して回収し、膨大な窒素やＣＯ２等の回収により肥料等の製造を可能にして、大気圧まで回転出力として使用の合体機関で駆動する、自動車等の回転出力駆動機器の技術に関する。
【００１６】
回転出力輸送機器の自動車等の出力発生は、超臨界温度等複数温度の高温水５ｂ全部を、複数の高温水加減弁７ａより高温水管６ａを介して、全動翼蒸気ガスタービン合体機関の夫々の高温水溜３２ａに供給し、夫々の加熱高温手段１０１により加熱高温とした、夫々の高温水噴射ノズル５９ｂより複数温度の高温水５ｂを、複数の高温水溜３２ａより夫々の霧吹きの原理９１ｅに供給して噴射の過程で、最高温度の高温水５ｂを中核に複数温度の高温水５ｂで構成した、霧吹きの原理９１ｅより、ノズルと高温水との間に気化膜を設けて摩擦損失を最少とし、気化爆発エネルギや気化爆発容積速度等により、ノズル内では高温水を機関銃の弾丸や吹雪のように加速して、気化爆発エネルギを最も効率良く利用する技術に関する。
【００１７】
ノズル外では高温水を散弾ロケットや吹雪等のように加速して、電磁加熱高温とした全動翼タービン動翼８１により、高温水５ｂと動翼との間に気化膜を設けて、摩擦損失最少で略直線蛇行的に加速噴射して全動翼を高温水駆動し、機械効率を１０〜２０倍に上昇します。最適中流段に低温燃焼ガス質量を供給して、燃焼ガスを高温水で冷却しながら出力を発生させ、出力発生断熱膨張の過程で燃焼ガス排気温度を−２７３℃に近付け、飽和温度１００℃の水蒸気より気化潜熱回収器６６ａの給水３で熱回収して、給水３と低温燃焼ガスにより水蒸気を冷却して凝縮水とし、回転出力輸送機器でＣＯ２等の燃焼ガスを５０倍質量等の凝縮水に溶解して排水し、ＣＯ２等の燃焼ガス排気を０に近付ける技術に関する。
【００１８】
回転出力輸送機器用等は、低温燃焼ガス溶解用の凝縮水を最大として、ＣＯ２等燃焼ガス排気を０とするため、全出力を合体機関回転出力とし、既存ガスタービンの２７０〜５４０倍仮説出力とします。用途により高温水噴射用の水に化学物質等を混入し、ＣＯ２等の燃焼ガスを合成溶解容易とし、輸送用機器等からのＣＯ２等公害ガス排気を無害化し、燃焼ガス排気温度を−２７３℃に近付け、気化潜熱回収器６６ａの給水３と低温ＣＯ２等燃焼ガスにより、飽和水蒸気を冷却して５０倍質量等の凝縮水に溶解し、ＣＯ２等燃焼ガス排気を０にする過程で、動力を伝達しながら、多段に昇圧して超高圧少量送水する、送水ポンプ兼磁気摩擦動力伝達装置１００ａや、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａを、全ての全動翼蒸気ガスタービン合体機関の中核技術とする技術に関する。
【００１９】
噴射推進出力発生の輸送機器用等としては、ＣＯ２等の燃焼ガス排気を０として、２７０〜５４０倍仮説出力等とするため、燃焼器兼熱交換器４により、限り無く高圧燃焼熱交換して最大の熱回収量とし、熱回収した超臨界温度等複数温度の高温水５ｂの一部で、用途により全動翼圧縮機を含む全動翼蒸気タービンを駆動します。残りの高温水５ｂの大部分及び燃焼ガス全部を、夫々の霧吹きの原理９１ｅ・９１ｂを利用してバイパス噴射推進し、残りの高温水を燃焼器兼熱交換器４等に適宜に貯蔵して最適利用し、火災や非常時に安全な１０倍速度等の超音速飛行機等として使用し、排気の過程では低温燃焼ガスにより水蒸気容積を１／１７００に冷却凝集して、排気騒音を１／１０等に低減する、各種輸送機器用等の全動翼蒸気ガスタービン合体機関技術に関する。
【００２０】
燃焼ガス１０全部や高温水５ｂの大部分をバイパス噴射推進する船舶等では、既存ガスタービンの２７０〜５４０倍仮説出力に増大することで、その噴射推進速度を１０倍の時速５００ｋｍ等に上昇します。噴射推進の過程では断熱膨張低温燃焼ガスにより直接海水を冷却して、ＣＯ２等の燃焼ガス全部を海底に供給する過程で、用途により酸素等の空気を吸引して供給し、膨大な海水域に僅少な窒素や酸素やＣＯ２を供給して海域を活性化し、微生物や藻類や魚介類等の食料増産を図ります。そして回転出力や噴射推進出力を利用する、各種発電設備や熱と電気と冷熱の併給設備や、熱と電気の併給設備や各種汎用機関や、各種車両や各種機械用や、各種航空機や各種飛行物体や、各種船舶や各種飛行船舶や、各種飛行車両等あらゆる用途に対応可能にする技術に関する。
【００２１】
【従来の技術】
既存ガスタービンは偶々出力を発生したものの改良で、基礎研究皆無の熱量を全く利用しない容積利用のため、タービンの耐熱限界温度に制約されて、燃焼ガス落差×質量＝重力仕事率の増大が不可能乃至困難に加えて、熱量を利用しないで断熱膨張５００℃前後に、単位容積の重力仕事率を大幅に低減して高温排気し、断熱膨張して熱回収が困難な排気後に熱回収する等、無茶苦茶設計です。更に動翼の１０倍〜２０倍前後も速度エネルギを消費して、回転仕事を全くしない静翼を１／２も設けているため、全熱出力が１／２７０や１／５４０等に低減して、燃料電池の出力に近付き大損失です。
【００２２】
既存蒸気タービンも偶々出力を発生したものの改良で、基礎研究皆無の熱量を全く利用しない容積利用のため、超臨界圧力過熱蒸気を再三再熱して、復水器真空では１００００倍以上に断熱膨張し、単位重力仕事率を１／１００００に低減して、同一出力に１００００倍の動翼面積が必要です。膨大過ぎる蒸気速度も全く利用不可のため、動翼の１０〜２０倍前後も速度エネルギを消費して、回転仕事を全くしない静翼を半分も設けて、蒸気速度を堰き止めて減速する等、無茶苦茶過ぎるのです。蒸気容積のみ利用のサイクルでは、合理的な設計が不可能なため、無茶苦茶な設計となり、全熱出力が１／２５０や１／５００等に低減して、風力発電や燃料電池の発電量に近付け、膨大な熱需要があるのに、ボイラで加熱した全熱量で海水温度等を上昇して大損失し、ＣＯ２等をボイラから排気して地球温暖化を加速する、無茶苦茶をしております。
【００２３】
先の出願としてガスタービン燃焼器を熱交換器と兼用した、特願２０００−０２４５５２号、特願２０００−０３２５３９号、特願２０００−０４３７０６号、特願２０００−０５８０７９号、特願２０００−１０７４４６号、特願２０００−３９２４０１号、特願２００１−０１１３９９号、特願２００１−０１５２３４号、特願２００１−０２０９６３号、特願２００１−１７１１２８号、特願２００１−３１２３３８号、特願２００１−３３６１３９号、特願２００２−１２５７２号、特願２００２−１１８９３３号、特願２００２−１４２２７０号、特願２００２−３４９５４４号、特願２００３−３１２５号があります。
【００２４】
以上先の出願に基づく優先権主張出願は概略的に、全動翼を含む及び／ガスタービンの全複数の燃焼器を、熱交換器としても兼用して、限りなく高圧燃焼熱交換して、燃焼ガス入り口温度を最低に近付けて該排気温度を-２７３℃に近付け、燃焼ガス熱量と燃焼ガス質量を、別々に使用可能とし、過熱蒸気や高温水や燃焼ガスを水噴射冷却して、大気圧重力仕事率１７００倍の水質量を最適最大として、発電用では供給熱量を気化熱のみの気化爆発エネルギに近付けて、重力仕事率を最大にすると共に、供給熱量略全部を１００℃以下で需要家に供給することで、水道水や低温燃焼ガスにより水蒸気を冷却凝集し、ＣＯ２等の燃焼ガス排気を〇等として地球温暖化防止して、用途に合わせて無駄の最少を狙うものです。
【００２５】
【発明が解決しようとする課題】
既存最先端再熱蒸気タービンは、熱量を全く利用しない容積利用のため、再三再熱して容積を増大し、最終段復水器真空では蒸気容積が１００００倍以上に増大し、重力仕事率が１／１００００等に低減するため、動翼面積を１００００倍に増大しないと、同一落差では同一出力が得られません。即ち、合理的な設計が不可能な動翼面積や大蒸気速度のため、動翼の１０〜２０倍も速度エネルギを消費して、回転仕事をしない膨大な量の静翼を設けて、多段に堰き止めて風向きを反転させ、実用過熱蒸気速度に減速する、無茶苦茶過ぎる設計のため、無茶苦茶設計の既存ガスタービンと比較説明します。そこで合理的な設計が可能な全動翼蒸気タービンや全動翼蒸気ガスタービン等の全動翼蒸気ガスタービン合体機関を提供することを目的とします。
【００２６】
更に問題なのは膨大な温熱や冷熱の需要が有るのに、ボイラで発生回収した熱量を全く利用しないで、断熱膨張させて使用した熱量全部で海水温度を上昇し、膨大なＣＯ２等の燃焼ガスをボイラから排気して地球温暖化を加速し、発電量を１／２７０〜１／５４０に低減しております。そこで供給熱量略全部を１００℃以下の温熱として需要家に供給し、海水温度の上昇を皆無として、ＣＯ２等燃焼ガス排気温度を−２７３℃に近付け、燃焼ガス略全部を冷熱に変換して需要家に供給し、ＣＯ２等の排気を０として、燃焼ガス熱量発電量＋燃焼ガス質量発電量を、２７０〜５４０倍仮説発電量に増大して、電気料金を１／１０等に低減し、地球温暖化防止することを目的とする。
【００２７】
そこで既存ガスタービン燃焼器を合体機関燃焼器兼熱交換器４として、限り無く高圧燃焼熱交換冷却燃焼して、燃焼ガスタービン入口温度を最低として、燃焼ガス排気温度を−２７３℃に近付け、熱交換して得た燃焼ガス熱量出力の、超臨界圧力等の高温水回収熱量を既存ボイラの２倍前後の最大とし、超臨界温度等複数温度の高温水気化爆発エネルギにより、ノズル内では機関銃の弾丸や吹雪のように高温水を加速し、ノズル外では散弾ロケットや吹雪のように高温水を加速して、大気圧単位容積の重力仕事率を、燃焼ガスの１０００倍に増大して出力を発生させ、燃焼ガス熱量出力を（既存ガスタービンの５倍落差×２倍熱量×５０倍重力仕事率×１０〜２０倍機械効率×１／２０減少率）＝（既存ガスタービンの２５０〜５００倍仮説発電量乃至出力）に増大することを目的にます。
【００２８】
用途により出力発生の過程で更に水噴射して水蒸気を冷却し、その容積を縮小して重力仕事率を増大し、減速した出力発生として、排気の過程では気化潜熱回収器６６ａを復水器と略同様に設けて、空気抽出器により用途に合わせた飽和温度にし、冷却水も用途に合わせて給水３や水道水７０を使用し、通常は１００℃以下の飽和温度として水道水７０や給水３で気化熱回収し、温熱水道水は貯蔵して給水３は補給水とし、燃焼器兼熱交換器４には凝縮水を繰り返し再再供給して、同一熱量を繰り返し使用します。貯蔵した供給熱量略全部の膨大な温熱を、製造原価略０で需要家に供給し、可能な限り発電の副産物の温熱有効利用を拡大し、海水温度の上昇を皆無にすることを目的とします。
【００２９】
気化潜熱回収器６６ａにより同一熱量を繰返し熱回収して、凝縮水を燃焼器兼熱交換器４に供給し、燃料燃焼熱量を気化熱に近付けて大幅に低減し、熱回収して得た超臨界温度等複数温度の高温水５ｂを、全動翼蒸気タービンの最上流複数の高温水溜３２ａに供給し、加熱高温手段１０１により加熱高温とした複数の高温水噴射ノズル５９ｂより、複数温度の高温水５ｂとの間に気化膜を設けて摩擦損失を最少とし、超臨界温度等高温水５ｂの気化爆発力や容積速度を利用して、ノズル内では機関銃の弾丸や吹雪のように高温水を加速し、ノズル外では散弾ロケットや吹雪のように高温水を加速して、落差や重力仕事率を最大に近付けた出力発生とし、電磁加熱高温とした、電磁加熱タービン動翼８１と高温水との間に気化膜を設けて、摩擦損失最少として全動翼により略直線蛇行的に噴射して、機械効率を１０〜２０倍に上昇させることを目的とします。
【００３０】
発電量と冷熱供給量を最大にする場合は、微粉炭燃焼と高温水５ｂ出力とし、最終段復水器真空での動翼面積の一部乃至大部分を、重力仕事率の増大で１／１００００に近付けて、合理的動翼面積の設計を可能にし、燃焼ガス排気温度を−２７３℃に近付けます。そして電磁加熱高温の電磁加熱タービン動翼８１を具備した、全動翼蒸気ガスタービンの最上流に最適最少量の高温水５ｂを供給し、全動翼電磁加熱タービン動翼８１により、略直線蛇行的に高温水５ｂを噴射して、電磁加熱タービン動翼８１と高温水５ｂとの間に気化膜を設けて、摩擦損失最少で出力を発生し、中流最適段に熱交換して得た低温燃焼ガス質量を供給して、燃焼ガス質量発電量を（既存ガスタービンの２倍落差×灰分等２倍質量×１０〜２０倍機械効率）＝（既存ガスタービンの４０〜８０倍仮説発電量）の最大にし、燃焼ガス全部の冷熱最大量を需要家に供給することを目的とする。
【００３１】
既存最先端ガスタービンも、熱量を全く利用しない容積利用のため、タービン耐熱限界温度の上昇により、落差の増大が不可能になり、排気温度が５００℃前後と非常に高く、動翼の１０〜２０倍も速度エネルギを消費して仕事をしない、静翼を１／２も設けて実用燃焼ガス速度に減速する、無茶苦茶設計です。そこで冷熱回収量を最大にする場合は、通常燃料全動翼ガスタービン燃焼器兼熱交換器４とし、全動翼により極限まで高圧燃焼熱交換冷却燃焼して、燃焼ガス質量出力を２０〜４０倍仮説出力とし、燃焼ガス排気温度を−２７３℃に近付け、冷熱回収器１０２により極低温燃焼ガス全部より、ドライアイスや液体窒素の製造を可能にし、又は最大量の冷熱水道水として需要家に供給し、全動翼送風機１０３の吐出側を昇圧して、ＣＯ２等の燃焼ガスを水中に移動し、ＣＯ２等の排気を０乃至０に近付けることを目的とします。
【００３２】
燃焼器兼熱交換器４で熱交換して得た燃焼ガス熱量出力を、圧縮空気保有熱量−２７３℃以上略全部も含めて、既存ボイラの２倍前後の熱回収量の、超臨界温度等複数温度の高温水５ｂ熱回収量とし、熱交換して得た燃焼ガス質量出力を含めて、全動翼蒸気タービン乃至全動翼ガスタービン乃至全動翼蒸気ガスタービンを駆動し、更に霧吹きの原理９１ｂ・９１ｄ・９１ｅ・９１ｆを利用して、特殊装置９２ｂ・９２ｅ乃至水噴射装置９３ｄ・９３ｆを駆動し、既存ガスタービンの２７０〜５４０倍仮説発電量乃至出力の、発電機器や輸送機器等にし、地球温暖化防止することを目的とする。
【００３３】
【課題を解決するための手段】
実験数値が正解ですが、前段階のアイディアを明快に説明するため、すべて仮説数字で説明しておりますが、アイディア仮説数字に限定はしません。既存最先端再熱蒸気タービンのように再熱して、熱量を全く利用しない容積利用では、超臨界圧力から真空部まで蒸気速度が膨大過ぎて、有効利用困難ないし不可能に加えて、蒸気容積も１００００倍等に膨張し、単位容積重力仕事率が１／１００００に減少して、同一落差同一出力に１００００倍の動翼面積が必要になり、合理的な設計は不可能になり、動翼の１０〜２０倍も蒸気速度を堰き止めて回転仕事をしない、静翼を１／２も設けて実用蒸気速度に減速する等、無茶苦茶過ぎるのです。そこで合理的設計が可能な各種全動翼合体機関を提供します。
【００３４】
即ち実現不可能な動翼面積のため、再熱を逆転した全動翼蒸気タービンを使用して、超臨界温度等複数温度の高温水を霧吹きの原理等適宜に混合して噴射し、落差及び気化爆発エネルギにより、高温水を加速して出力を発生し、発電用等では供給熱量を気化熱に近付けて最少にします。そして加熱高温手段１０１により加熱高温として高温水との間に気化膜を設けて、摩擦損失を最少として砲身状や末広砲身状とした、高温水噴射ノズル５９ｂより超臨界温度等複数温度の高温水を、霧吹きの原理等適宜に混合して噴射して、ノズル内では機関銃の弾丸や吹雪のように高温水を加速し、ノズル外では散弾ロケットや吹雪のように高温水を加速して、燃焼ガス熱量出力を（既存ガスタービンの５倍落差×２倍回収熱量質量×５０倍重力仕事率×１０〜２０倍機械効率×１／２０減少率）＝（既存ガスタービンの２５０〜５００倍燃焼ガス熱量仮説発電量乃至出力）に増大します。
【００３５】
大気圧部重力仕事率が、水蒸気の１７００倍の高温水質量を最適最大として、動翼面積の一部乃至大部分を、既存再熱蒸気タービンの１／１７００等に縮小し、合理的な設計を可能にます。超臨界温度等複数温度の高温水落差や気化爆発力を利用することで、容積の増大を僅少として合理的な全動翼の設計を可能にし、重力仕事率が全燃焼ガスの５０倍等の高温水と、加熱高温の電磁加熱外側タービン動翼群１９や、電磁加熱内側タービン動翼群２０との間に気化膜を設けて、摩擦損失最少で略直線蛇行的に噴射して、機械効率を１０〜２０倍に上昇して回転出力を発生し、高温水の気化爆発力や気化爆発容積により、噴射速度を合理的な設計が可能に減速して、重力仕事率を極限まで増大し、燃焼ガス熱量出力を、既存ガスタービンの２５０〜５００倍仮説発電量乃至出力等に上昇します。
【００３６】
既存最先端ガスタービンも熱量を全く利用しない容積利用のため、出力が小さく排気温度も５００℃前後と高温で、ＣＯ２等の排出で地球温暖化を加速するため、前述のように全熱量を回収して５００倍燃焼ガス熱量出力等とし、燃焼ガス質量出力も既存ガスタービンの４０倍等に上昇します。そこで先ず既存ガスタービン燃焼器を燃焼器兼熱交換器４として、燃焼ガス温度と容積の障害を最低にし、限りなく高圧燃焼熱交換冷却燃焼して、燃焼ガスタービン入口温度を最低にし、燃焼ガス排気温度を−２７３℃に近付け、圧縮した空気の保有熱量−２７３℃以上略全部も含めて、既存ボイラの２倍前後の熱回収量の、超臨界温度等各種温度の高温水として、熱回収量を用途に合わせて最大にし、低温燃焼ガス全部を冷熱回収器１０２により、用途に合わせてドライアイスや液体窒素等として回収利用し、又は水道水冷熱に変換して需要家に供給します。
【００３７】
発電設備の冷熱回収用に限定した全動翼ガスタービンでは、燃焼ガス排気温度を−２７３℃に近付け、従来復水器と略同様に冷熱回収器１０２を設けて、従来冷却水に換えて水道水により冷熱を回収して、需要家に供給します。ドライアイスや液体窒素等を回収する用途の場合は、全動翼圧縮機の圧縮空気圧力を上昇して遠心力を利用し、冷熱回収器前でドライアイスや液体窒素を分離回収利用します。圧縮圧力を既存ガスタービンの２〜４倍の１０〜２０ＭＰａ等として、理論空燃比まで燃料燃焼質量も、同一圧縮空気量既存ガスタービンの略４倍にし、同一圧縮空気量出力を（既存ガスタービンの２倍落差×４倍質量×１０〜２０倍機械効率）＝（既存ガスタービンの８０〜１６０倍仮説発電量）に増大します。そして燃焼ガス質量出力を（既存ガスタービンの２倍落差質量×１０〜２０倍機械効率）＝（既存ガスタービンの２０〜４０倍仮説発電量）に増大します。
【００３８】
燃焼ガス熱量の高温水により摩擦損失最少で出力を発生させるため、全動翼蒸気タービン電磁加熱タービン動翼８１の、外側軸装置及び内側軸装置にコイル９８を設け、公知技術により回転接点を設けて通電し、電磁誘導加熱調理器と略同様に、環状の電磁加熱噴口８３を含む、電磁加熱外側タービン動翼群１９及び電磁加熱内側タービン動翼群２０を、鉄系の比透磁率の大きい材料で構成して、磁力線９９の渦電流により加熱高温にし、電磁加熱タービン動翼８１と高温水との間に気化膜を設け、摩擦損失を最小の重力仕事率を最大として、最適高温水速度に減速して合理的な回転出力を発生し、全動翼により略直線蛇行的に噴射して機械効率を１０〜２０倍に上昇し、既存ガスタービンの５００倍仮説発電量乃至出力等に増大します。
【００３９】
全動翼蒸気タービン電磁加熱タービン動翼８１により、略直線蛇行的に噴射して、気化爆発エネルギを最適利用して既存技術静翼を全廃し、機械効率を１０〜２０倍に上昇し、排気の過程では復水器と略同様に設けた、気化潜熱回収器６６ａの空気抽出器により、用途に合わせて飽和温度を１００℃・８０℃以下等とし、冷却水も給水３や水道水７０を用途に合わせて使用して、既存技術海水温度の上昇を全廃し、気化潜熱回収器６６ａにより熱回収した凝縮水を、燃焼器兼熱交換器４に供給することで、同一熱量を限り無く繰り返し再再再使用して、供給熱量の燃料燃焼質量を略気化熱の最低に低減すると共に、供給熱量略全部の膨大な温熱を、製造原価略０の副産物として、１００℃以下の水道水温熱として需要家に供給し、電気料金も１／１０等とします。
【００４０】
発電量と冷熱回収量を最大にして、ＣＯ２等の燃焼ガス排気を０等にする場合は、起動時のみ全動翼ガスタービンとして使用する、安価微粉炭燃料燃焼の全動翼蒸気ガスタービンの最上流に、最適最少量の超臨界圧力高温水を供給し、電磁加熱タービン動翼８１により略直線蛇行的に噴射して出力発生の過程で、中流最適段に冷却された灰分を含む燃焼ガスを供給して、出力発生の過程で用途により低温水噴射し、灰分を含めて重力仕事率を増大して最適減速し、その気化爆発水蒸気や燃焼ガスを冷却して、最大量の電力を供給すると共に、断熱膨張低温燃焼ガス灰を核に全水分を凝集することで、ＣＯ２等の燃焼ガスに被覆を設けて、撥水性タービン動翼８７ａ又は電磁加熱タービン動翼８１を選択して、摩擦損失最少で出力を発生し、冷熱回収器１０２で水分を含む低温燃焼ガスより、最大量の冷熱を水道水で回収して貯蔵し、水道水冷熱として需要家に供給します。
【００４１】
最大量の冷熱を５℃前後の水道水冷熱で貯蔵しておき、冷熱水道水管を配管して需要家に供給し、既存の業務用家庭用冷蔵設備やクーラーに変えて、脱フロンの安価な水道水冷熱利用の、業務用家庭用の冷凍設備や冷蔵設備やクーラーを提供し、膨大過ぎる冷熱は散水して都市部を丸ごと冷却する等とし、冷房や冷凍設備や冷蔵設備の運用費を１／１０等に低減します。膨大になり過ぎる冷熱水で海水を冷却する過程では、低温ＣＯ２や窒素等を大量の海水に溶解して冷熱水とし、酸素等の空気を吸引して海底に最適量を希薄供給し、微生物や海草や魚介類を繁殖させる工夫をして海域の活性化を図ります。又は水道水等を冷却した冷熱のＣＯ２や窒素等の溶解水は、生ゴミや泥土や植物片に固定して膨大安価な肥料等とし、深海固定等の常識を逆転して発電による海水温度の上昇も逆転します。
【００４２】
空気圧縮の過程では、全動翼圧縮機を撥水性水冷却翼８７で構成し、撥水性金属・撥水性物質の被覆・撥水性セラミックス・撥水性加工の、何れか１以上で構成の撥水性全動翼圧縮機翼を水冷却翼にすることで、圧縮空気を略直線蛇行的に圧縮して水冷却し、更にその水を水噴射手段５６から水噴射して直接空気冷却し、低温圧縮空気にする過程で、撥水性水冷却翼８７と水等との間の摩擦損失を最小に近付けて、最低温度の圧縮空気を燃焼器兼熱交換器４に供給し、限りなく高圧燃焼熱交換冷却燃焼して、燃焼ガスのタービン入口温度を、用途に合わせた最低温度に低下させます。
【００４３】
全動翼蒸気ガスタービン合体機関の燃焼器兼熱交換器４により、限り無く高圧燃焼熱交換冷却燃焼して、燃焼ガスのタービン入口温度を最低にすることで、燃焼ガス排気温度を−２７３℃に近付けます。そして出力発生の過程では用途に合わせて、電磁加熱タービン動翼８１又は撥水性タービン動翼８７ａを選択し、全動翼により略直線蛇行的に高温水５ｂや燃焼ガスを噴射して、摩擦損失最少で出力を発生します。用途により水噴射手段５６ａにより低温水を噴射して、気化爆発水蒸気や燃焼ガスを冷却し、単位容積を縮小して重力仕事率を増大し、高温水の気化爆発水蒸気速度や燃焼ガス速度を、水質量の速度重力仕事率にエネルギ変換し、最適速度に減速します。
【００４４】
用途により気化爆発エネルギ水蒸気や燃焼ガスを低温水噴射冷却して、水の重力仕事率にエネルギ変換して最適速度に減速し、２７０〜５４０倍仮説発電量に増大する過程で、膨張低温燃焼ガスによる水蒸気の冷却を僅少にして、燃焼ガス排気温度を−２７３℃に近付ける過程で、低温燃焼ガス灰分を核に水分を凝集して、自然現象と同様に雹や水滴の被覆を設けて真空まで膨張させ、冷熱回収器１０２による回収冷熱を最大にします。冷熱として回収した燃焼ガス全部の膨大な冷熱で、水道水等を熱交換冷却して貯蔵する過程で、燃焼ガスの窒素やＣＯ２等を膨大な水に溶解して、非常に安価で膨大な肥料等の製造を可能にし、世界の火力発電所から排出されるＣＯ２等の燃焼ガス排気を０等にし、冷熱の回収利用を最大にして地球温暖化防止します。
【００４５】
有限の燃料資源を子孫にも残すためには、発電用は安価微粉炭燃料の燃焼とし、燃焼灰の重力仕事率により全重力仕事率を更に増大して、燃焼ガス質量発電量を増大し、有限の燃料資源を最も合理的に配分使用します。燃焼器兼熱交換器４で限りなく高圧燃焼熱交換冷却燃焼して、全動翼蒸気ガスタービン燃焼ガス入口温度を最低にする過程を、安価微粉炭燃料の燃焼にし、燃焼ガス排気温度を−２７３℃に近付けて、圧縮空気保有熱量−２７３℃以上略全部を含め、既存ボイラの２倍前後の回収熱量を、超臨界温度等複数温度の高温水に変換した、全動翼蒸気タービン出力を含む燃焼ガス熱量出力は、前記同様に、既存ガスタービンの２５０〜５００倍仮設発電量にします。
【００４６】
そして同一燃料量燃焼ガス質量発電量を（既存ガスタービンの２倍落差×１０〜２０倍機械効率×燃焼灰を含め２倍質量）＝（既存ガスタービンの４０〜８０倍燃焼ガス質量発電量）に増大します。出力発生の過程では前述のように、全動翼蒸気ガスタービンの最上流に供給した最少最適量の高温水出力とし、中流最適段に供給した燃焼ガス質量出力の、燃焼灰を含む低温燃焼ガスを核に低温水分を凝集し、真空を可能にして冷熱回収量と発電量を最大にします。そして（燃焼ガス質量発電量）＋（燃焼ガス熱量発電量）＝（既存ガスタービンの４０〜８０倍燃焼ガス質量発電量）＋（既存ガスタービンの２５０〜５００倍燃焼ガス熱量発電量）＝（既存ガスタービンの２９０〜５８０倍仮説発電量）に増大します。
【００４７】
燃焼ガス熱量出力＋燃焼ガス質量出力全部を、回転出力として燃焼ガス排気を０等とする、輸送機器の自動車等で使用する場合は、全動翼蒸気ガスタービンの最上流複数の高温水溜３２ａに、燃焼器兼熱交換器４で熱交換して得た超臨界温度等複数温度の高温水全部を、夫々の高温水加減弁７ａより燃焼ガス熱量出力として供給し、加熱高温手段１０１で加熱高温とした、砲身状乃至末広砲身状の高温水噴射ノズル５９ｂより噴射して、ノズルと高温水との間に気化膜を設けて、摩擦損失最少で気化爆発力や気化容積速度を最適利用し、ノズル内やノズル外では、機関銃の弾丸や散弾ロケットや吹雪のように高温水を加速して、加熱高温とした電磁加熱タービン動翼８１と高温水との間にも気化膜を設けて、摩擦損失最少の重力仕事率最大の高温水速度最適で、略直線蛇行的に噴射し、機械効率を１０〜２０倍に上昇します。
【００４８】
大気圧重力仕事率が既存蒸気タービンの１７００倍の、高温水５ｂの質量を用途に合わせて最大にし、中流最適段に最低温度の燃焼ガスを供給し、一瞬高温水５ｂで燃焼ガス１０を冷却し、出力発生の過程で逆転して、低温燃焼ガスにより高温水を冷却して、気化潜熱回収器６６ａにより給水３により熱回収して、燃焼器兼熱交換器４に供給使用し、ＣＯ２等の燃焼ガスを５０倍質量等の凝縮水に溶解して排水し、ＣＯ２等の燃焼ガス排気を０等にすると共に、大気圧部重力仕事率を既存技術の１７００倍の高温水出力にして、タービン動翼面積の一部乃至大部分を１／１７００の、合理的な動翼面積にします。即ち回収熱量を高温水の気化爆発力として使用することで、タービンの動翼面積も１／１００動翼面積等に縮小し、合理的な設計や回転数を可能にすると共に、構造を１／１０等に小型簡単にします。
【００４９】
自動車等の回転出力輸送用機器の場合は、飽和温度が１００℃前後に限定され、気化潜熱回収器６６ａは重量が大きい空冷となり、凝縮水を燃焼器兼熱交換器４に限り無く再再供給使用が通常のため、燃焼ガス溶解水の用途が無い場合は、燃焼ガスの全部又は一部により、全動翼ガスタービンを駆動して発電等で利用して、その排気を冷房用等の別用途に使用し、又はドライアイスや液体窒素等として回収利用する、全動翼蒸気ガスタービンとします。凝縮水を再再使用して超臨界温度等複数温度の高温水にしますが、構造が簡単となり、燃焼ガス熱量出力が（同一燃料量既存ガスタービンの５０倍質量重力仕事率×５倍落差×２倍回収熱量×１０〜２０倍機械効率×１／２０減少率）＝（２５０〜５００倍仮説出力）等となり、燃焼ガス質量出力を０等とした、各種輸送機器用の、全動翼蒸気ガスタービン合体機関として使用します。
【００５０】
回転出力＋噴射推進力利用の場合、回転出力用の超臨界温度等複数温度の高温水温度は、排気噴射速度等も推進力として利用するため過熱蒸気に近付き、霧吹きの原理を利用した、空気吸引噴射乃至水吸引噴射する、噴射推進出力発生用の超臨界圧力等の高温水温度も、非常に大きな速度を利用可能なため、過熱蒸気温度に近付きます。従って全動翼蒸気ガスタービン合体機関の空気圧縮機を駆動するため、高温水の気化爆発エネルギを回転出力にエネルギ変換する部分を除き、霧吹きの原理を利用した構造が非常に簡単になるため、廃熱回収が不可能を相殺した出力となり、既存ガスタービンの２７０〜５４０倍仮設出力等の、全動翼蒸気ガスタービン合体機関として、超音速旅客機や宇宙往還親飛行機や噴射推進船舶等として使用し、その速度を１０倍前後に増大します。
【００５１】
例えば図６の、全動翼蒸気タービン合体機関乃至全動翼蒸気ガスタービン合体機関は、通常の起動装置により全動翼蒸気タービンを含む全動翼圧縮機を駆動し、前方の空気を吸入して、燃焼器兼熱交換器４により限り無く高圧燃焼熱交換冷却燃焼して、起動時のみ全動翼蒸気タービンを全動翼ガスタービンで使用し、公知技術により図に無いバルブ制御して、熱交換して得た燃焼ガス熱量出力の、高温水を超臨界圧力等として貯蔵しながら、熱交換して得た燃焼ガス質量出力の低温燃焼ガスを、全動翼蒸気タービンの最上流に供給し、その回転出力で全動翼圧縮機を駆動し、超臨界温度等複数温度の高温水温度を上昇しながら、排気速度質量を噴射推進力として、起動準備運転を継続します。
【００５２】
起動準備運転で熱交換して得た超臨界温度等の高温水温度上昇時には、図に無いバルブ制御により、燃焼ガス質量の低温燃焼ガス１０全部を、霧吹きの原理９１ｂよりバイパス噴射して、前方の空気を吸引して噴射し、その吸引力と噴射速度質量を噴射推進力とし、熱交換して得た燃焼ガス熱量の超臨界温度等複数温度の高温水の一部を、全動翼蒸気タービンの最上流複数の高温水溜り３２ａに供給して、夫々の高温水噴射ノズル５９ｂにより適宜に混合して噴射し、電磁加熱タービン動翼８１により摩擦損失最少で回転出力を発生して、その回転出力により全動翼空気圧縮機を駆動し、その空気吸引力と排気噴射速度×質量を噴射推進力とし、残りの高温水全部を適宜に貯蔵してバイパス噴射して、既存超音速ジェット機の１０倍前後の速度で高速飛行します。
【００５３】
即ち公知技術による図に無いバルブ制御により、熱交換して得た燃焼ガス全部と残りの高温水は、夫々の霧吹きの原理９１ｂと９１ｅを利用してバイパス噴射し、断熱膨張ラムジエツトを遥かに越える大落差で燃焼ガスをバイパス噴射し、ラムジェットの５倍落差前後５０倍仮説質量等で高温水をバイパス噴射して、前方の空気を吸引して噴射推進し、空気吸引力と噴射速度×質量により、既存ジェット機の１０倍前後の超音速飛行を含めて、超音速ジエツト機や宇宙往還親飛行機や、飛行船舶や飛行物体等を最も効率良く噴射推進し、噴射推進の過程で低温燃焼ガスにより、水蒸気容積を１/１７００容積等に冷却縮小して、溶解水を海上等に希薄供給して海域の活性化を図り、排気騒音を１／１０等に低減して、騒音公害を皆無に近付けます。
【００５４】
【発明の実施の形態】
発明の実施の形態や実施例を、図面を参照して説明するが、既説明の実施形態や実施例と、その構成が略同じ部分には、同一の名称又は符号を付して、重複説明は省略し、特徴的な部分や説明不足部分は、順次追加重複説明する。又、発明の意図する所及び予想を具体的に明快に説明するため、アイディアを仮説数字で説明しておりますが、前記仮説倍率を含めて数字に限定しません。
【００５５】
この発明により最も簡単に効率良く空気を冷却圧縮し、熱回収して低温空気として使用する燃焼器兼熱交換器４は、既に特許出願済の燃焼器兼熱交換器を、用途に合わせて選択使用します。又、極低温燃焼ガスや高温水５ｂ等で、最も効率良く出力を発生させるため、加熱高温の電磁加熱タービン動翼８１を使用しますが、用途によりその一部又は全部を、撥水性タービン動翼８７ａに置換します。また燃焼ガス排気温度を−２７３℃に近付けて、極低温燃焼ガスとしますが、前記説明を含めて、−２７３℃に近付けるは、実用的な最低温度として使用し、−１００℃前後や−２０℃前後等−温度全部に拡大して使用します。
【００５６】
図１の全動翼蒸気タービンの第１実施例には、図３等の燃焼器兼熱交換器４により熱交換して得た、同一燃料量既存ボイラの２倍前後の回収熱量の全部又は大部分を、超臨界温度等複数温度の高温水５ｂとして高温水管６ａにより、高温水加減弁７ａを介して、全動翼蒸気タービンの最上流複数の高温水溜３２ａに、夫々複数温度の高温水を別々に供給し、断熱材４８ａを介して設けて、直接の電気抵抗や電磁加熱等公知技術により加熱高温とする、加熱高温手段１０１により加熱高温とした、砲身状乃至末広砲身状の高温水噴射ノズル５９ｂにより、高温水５ｂとの間に気化膜を設けて、摩擦損失最少で大落差容積利用や気化爆発エネルギ利用により、高温水５ｂを重力仕事率最大の消費熱量最少で加速して、最も効率良く回転出力を発生します。
【００５７】
従って高温水噴射ノズル５９ｂ内では超臨界温度等複数温度の高温水を、機関銃の弾丸や吹雪のように加速し、ノズル外では散弾ロケットや吹雪のように高温水５ｂを加速して、電磁誘導加熱高温の電磁加熱タービン動翼８１との間に気化膜を設け、摩擦損失最少で略直線蛇行的に噴射して、機械効率を既存蒸気タービンの１０〜２０倍に上昇し、例えば燃焼ガス熱量出力を（既存ガスタービンの５倍落差×２倍回収熱量×５０倍質量重力仕事率×１０〜２０倍機械効率×１／２０減少率）＝（既存ガスタービンの２５０〜５００倍仮説出力）等に増大し、出力発生の過程でも用途により水噴射して、高温水気化爆発や容積利用による水蒸気５を冷却して、水蒸気容積を大気圧部１／１７００等に縮小し、蒸気速度の大部分は高温水質量の速度重力仕事率にエネルギ変換し、最適速度に減速して、合理的な設計が可能な回転数にし、構造を１／１０等に小型簡単にします。
【００５８】
落差は超臨界圧力より大気圧まで使用で充分等とし、大気圧部単位容積重力仕事率が、最先端蒸気タービンの１７００倍の高温水落差×質量を、既存ガスタービン燃焼ガスの５倍落差超臨界圧力×５０倍質量等とし、重力仕事率最大×最適速度に減速し、電磁加熱タービン動翼８１の動翼面積の一部乃至大部分を、１／１７００に縮小して、合理的な設計が可能な動翼面積に縮小し、大気圧部単位動翼面積の最大出力を１７００倍に増大します。電磁加熱タービン動翼８１の大幅な動翼面積の縮小及び、全重力仕事率の大幅な増大及び、高温水速度の最適速度に減速により、全動翼蒸気タービンの合理的設計を可能にし、低速回転の可能や１／１０等の小型簡単化や、５００倍等の仮説出力に増大します。
【００５９】
合理的設計や低速大出力回転可能や小型簡単大出力にすることで、全動翼翼形として略直線蛇行的に噴射を可能にすると共に、電磁加熱外側タービン動翼群１９及び、電磁加熱内側タービン動翼群２０を、段落毎環状に一体鋳造８４及び全自動加工も可能にします。そして鋳造時のタービン翼等に、用途により断熱して設けた図に無い適宜の冷却手段５５の水を噴射する、断熱して設けた水噴射手段５６ａの鋳込みを可能にし、外径組立環状部８５や内径組立環状部８６の接続部付近に、水噴射手段５６ａを設けて、電磁加熱外側タービン動翼群１９及び、電磁加熱内側タービン動翼群２０の電磁加熱タービン動翼８１とし、略直線蛇行的に噴射して、機械効率を既存蒸気タービンの１０〜２０倍に上昇します。
【００６０】
翼間隔を拡大した全動翼翼形や全動翼翼幅や全動翼翼角度を、重力仕事率大気圧部１７００倍等の増大に合わせた形状にします。そして鋳造時の電磁加熱タービン動翼８１を、磁力線を通し易い鉄を主成分とした材料で構成し、磁力線を集めて渦電流により、電磁調理器と略同様に電磁誘導加熱高温にします。外側軸装置及び内側軸装置にコイル９８を設け、公知技術による回転接点により通電して、電磁加熱外側タービン動翼群１９及び、電磁加熱内側タービン動翼群２０に、磁力線を集めて渦電流による電気抵抗により電磁誘導加熱高温にし、出力発生の過程では高温水との間に気化膜を設けて、摩擦損失最少として略直線蛇行的に高温水５ｂを噴射して、重力仕事率最大の最適噴射速度で、機械効率を既存蒸気タービンの１０〜２０倍に上昇します。
【００６１】
排気の過程では、既存復水器と略同様に設けた気化潜熱回収器６６ａの空気抽出器により、飽和温度１００℃以下等を可能とし、冷却水の海水に換えて水道水７０で熱回収することで、１００℃等の回収凝縮水を限り無く繰り返し燃焼器兼熱交換器４に供給して再再再使用し、供給燃料燃焼質量を気化熱の最低に節減すると共に、供給燃料燃焼熱量全部を飽和温度１００℃以下の水道水温熱として、気化潜熱回収器６６ａにより熱回収して貯蔵しておき、供給熱量略全部の膨大な水道水温熱を発電の副産物として、製造原価略０で需要家に供給して需要の拡大を図り、燃料燃焼使用熱量全部による、既存蒸気タービンの海水温度の上昇を皆無として、電気料金を１／１０等とします。
【００６２】
図２の超臨界温度等複数温度の高温水５ｂを、霧吹きの原理等により適宜に混合して噴射する、各種高温水噴射ノズル５９ｂを説明する。既存蒸気タービンのように、堰き止めて蒸気速度を実用速度に減速する無茶苦茶や、１７００倍容積に増大して合理的な設計を不可能にする無茶苦茶を全廃して、超臨界温度等複数温度の高温水５ｂの内、最高温度の高温水５ｂを中心に配置して、１以上複数温度の高温水と９０°前後で交差・合流混合して噴射する、又は１以上複数温度の高温水と霧吹きの原理で合流混合して噴射する、何れかの高温水噴射ノズル５９ｂとして、合理的に電磁加熱タービン動翼８１を、最も効率良く高温水５ｂを加速して駆動するものが、各種高温水噴射ノズル５９ｂです。
【００６３】
そこで超臨界温度等最高温度温度の高温水５ｂを中心として、複数温度の高温水５ｂを霧吹きの原理等により適宜に混合して噴射し、超臨界温度等最高温度の高温水容積利用により、水蒸気速度を確保しながら複数温度の高温水質量により、重力仕事率を増大して最適減速する過程で、複数温度の高温水気化爆発力を最適利用して、供給熱量最少の発電量乃至出力最大を狙うものです。従って最高温度の高温水５ｂを通水する高温水噴射ノズル５９ｂを中心として、複数温度の高温水５ｂを通水する高温水噴射ノズル５９ａを合流して、超臨界温度等複数温度の高温水を霧吹きの原理等で適宜に混合して噴射する、高温水噴射ノズル５９ｂを構成します。
【００６４】
図２では紙面の都合で砲身状又は末広砲身状の部分が不明ですが、図に無い延長部分が中核部分の砲身状又は末広砲身状のノズル部分で、このノズル内では高温水５ｂを機関銃の弾丸や吹雪のように加速します。電気抵抗等の公知技術で加熱する加熱高温手段１０１により加熱高温として、高温水管６ａより高温水溜３２ａ経由で供給された、高温水５ｂとの間に気化膜を設けて、摩擦損失最少で高温水を加速します。加熱高温手段１０１の外側には断熱材４８ａを設けて、全動翼蒸気タービンや全動翼蒸気ガスタービンの最上流及び、霧吹きの原理９１ｅ・９１ｆの最上流に具備して、全動翼蒸気タービンや全動翼蒸気ガスタービン及び、特殊装置９２ｅや水噴射装置９３ｆを構成し、最も効率良く回転出力及び噴射推進出力を発生します。
【００６５】
図３の全動翼ガスタービンの第一実施例は、全動翼圧縮機の主要部分の、外側圧縮機動翼群１６及び内側圧縮機動翼群１７の、撥水性金属・撥水性物質の被覆・撥水性セラミックス・撥水性加工の、何れか１以上で構成の撥水性水冷却翼８７等を、図にない冷却手段５５により通水して水冷却し、その水を水噴射手段５６より水噴射して圧縮空気を直接接触冷却し、その熱を給水３で熱回収して空気容積を縮小します。撥水性水冷却翼８７で成る全動翼とすることで、翼間隔を増大した全動翼翼形として、圧縮空気を略直線蛇行的に効率よく圧縮し、水との摩擦損失最小で圧縮する、撥水性の外側圧縮機動翼群１６及び内側圧縮機動翼群１７を、段落毎圧縮機翼群を環状に一体鋳造８４とし、全自動加工仕上げを可能にします。
【００６６】
全自動加工が可能な環状に一体鋳造８４の組立構造とし、環状鋳造組立接続部で冷却手段５５の水路を連結して、該組立接続部付近に水噴射手段５６を設けます。冷却手段５５の水路を、１以上複数又は段落全部又は段落半分の撥水性水冷却翼８７を冷却後に、水噴射手段５６より水噴射して直接空気冷却し、最も効率良く水冷却した低温空気を、用途に合わせて全動翼により限り無く高圧圧縮します。熱回収した高温給水と低温圧縮空気により、燃焼器兼熱交換器４で限りなく高圧燃焼熱交換冷却燃焼して熱回収し、全動翼ガスタービン燃焼ガス入口温度を最低に低下させ、熱回収量を既存ボイラの２倍前後に増大して、低温燃焼ガス排気温度を−２７３℃に近付けます。
【００６７】
燃焼器兼熱交換器４で限りなく高圧燃焼熱交換冷却燃焼熱回収して、燃焼ガスの温度と容積の障害を最低にし、圧縮圧力を既存ガスタービンの２倍以上の１０ＭＰa以上とし、燃料燃焼質量も理論空燃比まで、同一圧縮空気量既存ガスタービンの略４倍燃焼とし、燃料燃焼熱量の消費を０以下とした、燃焼ガス質量出力を（同一圧縮空気量最低温度の燃焼ガス質量出力）＝（既存ガスタービンの２倍落差×４倍燃料質量×１０〜２０倍機械効率）＝（同一圧縮空気量既存ガスタービンの８０〜１６０倍仮説発電量）とし、（同一燃料量既存ガスタービンの２０〜４０倍仮説発電量）とします。
【００６８】
熱交換して得た最低温度の燃焼ガス１０質量を、全動翼ガスタービンの最上流の環状の燃焼ガス溜９より、外側軸装置の環状の受け口２３を介して、全動翼ガスタービンの最上流に供給して出力を発生させ、全動翼圧縮機を駆動しながら燃焼器兼熱交換器４内で、超臨界温度等複数温度の高温水温度を上昇して保存貯金増大し、その高温水５ｂの温度上昇時に、夫々の高温水加減弁７ａを開放制御して、高温水５ｂを図１の全動翼蒸気タービンの、夫々複数の高温水溜３２ａに別々に供給して、断熱して設けて加熱高温とした加熱高温手段１０１により、加熱高温とした砲身状乃至末広砲身状の高温水噴射ノズル５９ｂより、高温水５ｂとの間に気化膜を設けて、摩擦損失最少で容積利用及び気化爆発エネルギにより高温水を加速して、既存ガスタービンの５００倍仮説発電量や出力等を発生し、電気料金を１／１０等に低減します。
【００６９】
出力発生の過程では、撥水性タービン動翼と燃焼ガスとの間の摩擦損失を最少として、略直線蛇行的に噴射して機械効率を１０〜２０倍に上昇し、用途により水噴射して燃焼ガス温度を低下させて最適速度に低減し、又は全動翼圧縮機により限り無く高圧圧縮して、排気の過程では冷熱回収器１０２により極低温燃焼ガス全部を、ドライアイスや液体窒素等として遠心力により分別回収して利用し、又は熱交換２〜５℃の水道水冷熱に変換して需要家に供給します。同時にドライアイスや液体窒素や水道水冷熱により圧縮空気を冷却する、業務用や家庭用の冷凍設備機器や冷蔵設備機器や空冷設備機器を提供して、脱フロンによる地球温暖化防止すると共に、ＣＯ２等の燃焼ガスを水に溶解可能にして、ＣＯ２等燃焼ガス排気０を可能とします。
【００７０】
図４の全動翼蒸気ガスタービン乃至、全動翼ガスタービン乃至、全動翼蒸気ガスタービン合体機関の第一実施例は、第１実施例を含めてすべて熱量を利用するため、従来型のガスタービンが無くなります。そして起動時には超臨界温度等の高温水５ａが皆無のため、燃焼ガス１０のみにより超臨界温度等複数温度の高温水を発生させる、全動翼ガスタービンとして使用し、高温水加減弁７ａを閉止して、内側軸装置の最適中間段に燃焼ガスを供給する、全動翼ガスタービンとして使用し、燃焼器兼熱交換器４により限り無く高圧燃焼熱交換冷却燃焼して、燃焼ガスタービン入口温度を用途に合わせて最低温度とし、熱交換して得た、超臨界温度等複数温度にする高温水５ｂの温度を上昇させて、起動準備をします。
【００７１】
全動翼圧縮機及び燃焼器兼熱交換器４を、全動翼ガスタービンと同様に設けて、限りなく高圧燃焼熱交換冷却燃焼して熱回収し、全動翼蒸気ガスタービン燃焼ガス入口温度を最低に低下させ、熱回収量を既存ボイラの２倍前後に増大し、低温燃焼ガス排気温度を−２７３℃に近付けます。燃焼ガスの温度と容積の障害を最低にして、圧縮圧力を既存ガスタービンの２倍以上の１０ＭＰa以上とし、燃料燃焼質量も理論空燃比まで、同一圧縮空気量既存ガスタービンの略４倍燃焼を可能とします。
【００７２】
公害低減・地球温暖化防止が急務であり、例えば有限の燃料資源を子孫にも残すため、公知のゴミガス化燃料やゴミ微細化燃料や、燃えるもの全部を燃焼して熱回収補助使用して、超臨界温度等複数温度の高温水として高温水加減弁７ａを介して、夫々複数の高温水溜３２ａに別々に供給して電力に変換します。そして該燃焼ガス空気も全動翼圧縮機で圧縮して、水噴射手段５６により直接低温空気に冷却し、燃焼器兼熱交換器４により再燃焼させて再熱回収して、通常使用乃至通常使用に合流して補助使用し、熱回収量を増大します。
【００７３】
発電用には安価豊富な微粉炭燃料の燃焼として、全動翼蒸気ガスタービン燃焼器兼熱交換器４により、限り無く高圧燃焼熱交換冷却燃焼して、燃焼ガス排気温度を−２７３℃に近付け、気化潜熱回収器６６ａにより給水３により、気化潜熱を回収して燃焼器兼熱交換器４に供給し、熱交換して得た既存ボイラの２倍前後の燃焼ガス熱量の、超臨界温度等複数温度の高温水５ｂ全部を、全動翼蒸気ガスタービンの最上流に供給し、中流最適段に低温燃焼ガス質量を供給して出力を発生し、気化潜熱回収器６６ａで給水３により気化熱を回収して、５０倍質量等の凝縮水にＣＯ２等燃焼ガス排気を溶解して排水し、ＣＯ２等の燃焼ガス排気を０等にします。
【００７４】
全回転出力の全動翼蒸気ガスタービン合体機関の起動時には、公知の起動装置により全動翼圧縮機を含めて駆動し、燃焼器兼熱交換器４により限り無く高圧燃焼熱交換冷却燃焼して、最低温度の燃焼ガス１０を環状の燃焼ガス溜９より、外側軸装置の環状の通路を介して内側軸装置の内側より、中流最適段に供給して出力を発生させ、全動翼圧縮機を駆動しながら燃焼器兼熱交換器４内で、超臨界温度等複数温度の高温水温度を上昇して保存貯金増大し、その高温水５ｂの温度上昇時に、夫々の高温水加減弁７ａを開放制御して、高温水全部を夫々複数の高温水溜３２ａに別々に供給して、断熱して設けて加熱高温とした加熱高温手段１０１により、加熱高温とした砲身状乃至末広砲身状の高温水噴射ノズル５９ｂより、高温水５ｂとの間に気化膜を設けて、摩擦損失最少で容積利用及び気化爆発エネルギにより高温水を加速して、既存ガスタービンの５４０倍仮説発電量や出力等を発生し、電気料金を１／１０等に低減します。
【００７５】
出力発生の過程では、高温水噴射ノズル５９ｂと高温水５ｂとの間に気化膜を設けて、摩擦損失最少として気化爆発力や容積利用により、高温水噴射ノズル５９ｂ内では高温水を機関銃の弾丸や吹雪のように加速し、ノズル外では散弾ロケットや吹雪のように高温水５ｂを加速して、加熱高温の電磁加熱タービン動翼８１との間でも気化膜を設け、摩擦損失最少で全動翼により略直線蛇行的に噴射して、機械効率を既存蒸気タービンの１０〜２０倍に上昇し、用途により水噴射して気化爆発水蒸気を冷却し、蒸気速度の一部乃至大部分を、水質量の速度重力仕事率にエネルギ変換して最適速度に低減します。そして排気前には低温燃焼ガス灰分等を核に水分を凝集して、水滴等の被覆を生成させて５０倍質量等の凝縮水に溶解することで、ＣＯ２等の燃焼ガス排気０等を可能とします。
【００７６】
発電量と冷熱の回収量を最大にする場合は、全動翼蒸気タービン＋全動翼蒸気ガスタービンとして使用し、大部分の高温水５ｂは全動翼蒸気タービンで使用し、最適少量の高温水５ｂを全動翼蒸気ガスタービンの最上流に供給し、中流最適段に冷却した最低温度の燃焼ガス１０を供給して、最初は高温水で更に燃焼ガスを冷却し、出力発生の過程で逆転し、全量の低温燃焼ガス灰分等を核に水分を凝集することで、燃焼ガス全部に被覆を設けて真空を可能にし、燃焼ガス全部を−２７３℃に近付けて、発電量及び冷熱の回収量を最大に増大します。
【００７７】
燃焼ガス全部を冷熱として分別回収した膨大な水滴は、その一部乃至全部で水道水を冷却して冷熱として貯蔵しておき、電気料金を１／１０等に低減した電力の副産物として、製造原価が略０の安価な水道水冷熱を需要家に供給し、その安価な冷熱利用の冷蔵庫やクーラーや業務用冷蔵設備を提供し、販路を爆発させることで、既存の家庭用や業務用の冷蔵庫やクーラーや業務用冷蔵設備等を全廃して、脱フロンとした地球温暖化防止すると共に冷熱水道管を満杯し、膨大過ぎる水道水冷熱は散水して都市部等を丸ごと冷却します。
【００７８】
又は膨大な残りのＣＯ２や燃焼灰等を含む冷熱は、含有する窒素やＣＯ２等を植物が要求しており、有効利用するため生ゴミや植物片や泥土等に合成固定して、膨大な肥料を生成して食料の増産を図ります。残りの冷熱は別途海水を冷却して、海底にＣＯ２や窒素等の希釈した冷熱を供給する過程で、酸素等の必要物質を吸引して海中に供給し、海の生物の生態を微生物まで徹底的に研究して、最適濃度で供給します。魚介類や海藻類を繁殖させる、最適微生物や動植物を先ず繁殖させ、微生物や魚介類や海草類や海藻類を繁殖させて、ＣＯ２や窒素等の燃焼ガスにより食料の増産を図り、地球温暖化防止します。
【００７９】
そして燃焼器兼熱交換器４により限り無く高圧燃焼熱交換冷却燃焼して、熱交換して得た最低温度の燃焼ガス質量発電量を（既存ガスタービンの２倍落差×石炭灰等２倍質量×１０〜２０倍機械効率）＝（既存ガスタービンの４０〜８０倍燃焼ガス質量発電量）に増大して、資源の有効利用にします。そして（燃焼ガス質量発電量＋燃焼ガス熱量発電量）＝（４０〜８０倍＋２５０〜５００倍）＝（既存ガスタービンの２９０〜５８０倍全動翼蒸気ガスタービン＋全動翼蒸気タービン仮説発電量）に増大し、同一燃料量の発電量を増大して地球温暖化防止します。
【００８０】
大気圧付近で排気する、全動翼蒸気ガスタービン合体機関第１実施例の別形態として、全出力を回転力で利用する自動車等の各種陸上輸送機器や、陸海空の各種輸送機器の用途では、ＣＯ２等の燃焼ガスを凝縮水に溶解して回収しても、有効利用が困難なため凝縮水を繰返し燃焼器兼熱交換器４に再再供給して、限りなく高圧燃焼熱交換冷却燃焼熱回収が必要です。そこで熱交換して得た既存ボイラの２倍前後の燃焼ガス熱量出力を、超臨界温度等複数温度の高温水５ｂ全部として、図１・６の全動翼蒸気タービンの最上流に供給し、略直線蛇行的に噴射して出力を発生し、空冷式気化潜熱回収器６６ｂにより熱回収した空気は、暖房用等として使用して凝縮水を繰返し燃焼器兼熱交換器４に再再供給し、限りなく高圧燃焼熱交換冷却燃焼熱回収して、既存ガスタービンの２５０〜５００倍仮説出力にします。
【００８１】
低温燃焼ガス１０全部は図６の燃焼ガス取出口８８より、全動翼圧縮機や燃焼器兼熱交換器の無い、図３の小型簡単大出力の全動翼ガスタービンに供給し、出力発生の過程で用途により、低温水噴射して燃焼ガス１０を冷却し、容積を縮小して全重力仕事率を増大し、既存ガスタービンの２０〜４０倍仮説発電量等の別用途使用として、電気モーターによる駆動を可能にし、燃焼ガス排気温度を−２７３℃に近付けて、冷熱回収器１０２により用途に合わせて、ドライアイスや液体窒素等として回収可能とし、又は冷房用等として使用する、各種自動車等の輸送用機器として使用し、地球温暖化防止します。
【００８２】
全出力で回転力発生の全動翼蒸気ガスタービン合体機関は、排気水蒸気５の飽和温度が１００℃と高温のため、出力発生の過程で最低温度の燃焼ガス１０を圧力に合わせて、最適中間段に供給して出力を発生し、用途により低温水噴射により水蒸気５や燃焼ガスを冷却して、水蒸気容積や燃焼ガス容積を縮小し、最低温度の高温水質量を増大します。排気前には蒸気速度の大部分を、高温水質量の大気圧１７００倍重力仕事率にエネルギ変換して最適減速し、全重力仕事率や回転出力を、既存ガスタービンの２７０〜５４０倍仮説出力等に大幅に増大し、構造を１／１０等に大幅に小型簡単大出力にします。
【００８３】
全重力仕事率の大幅増大により、電磁加熱タービン動翼８１面積の大幅縮小及び、全動翼蒸気ガスタービン合体機関を小型簡単大出力・設計容易にし、水蒸気５や高温水５ｂや燃焼ガス１０等を、略直線蛇行的に噴射して出力を発生する、全動翼翼形にすると共に、翼間隔を拡大して翼幅や翼形や翼角度も、重力仕事率増大に合わせた形状にします。そして電磁加熱外側タービン動翼群１９及び、電磁加熱内側タービン動翼群２０を、電磁調理器と略同様に、外側軸装置及び内側軸装置にコイル９８を設けて通電し、夫々のコイル９８の磁力線を、夫々の電磁加熱タービン動翼８１に集めて、磁力線の渦電流の電気抵抗により電磁誘導加熱高温とした、全動翼電磁加熱タービン動翼８１と、高温水５ｂとの間に気化膜を設けて、摩擦損失を最小にし、略直線蛇行的に噴射して出力を発生し、機械効率を既存蒸気タービンの１０〜２０倍に上昇します。
【００８４】
図５の空気を吸引して噴射推進する、全動翼蒸気ガスタービン合体機関の第２実施例は、通常の起動装置により起動して、全動翼ガスタービンとして駆動の過程で、全動翼圧縮機により限り無く高圧圧縮して、燃焼器兼熱交換器４により高圧燃焼熱交換冷却燃焼熱回収して、燃焼ガス質量の低温燃焼ガス１０を、内側軸装置の内側から最適中流段に供給して出力を発生させる、全動翼ガスタービンとして使用し、燃焼ガス熱量の超臨界温度等複数温度の高温水温度を上昇します。全動翼とすることで翼間隔を増大した全動翼翼形として、圧縮空気を略直線蛇行的に圧縮する、撥水性水冷却翼８７で成る、外側圧縮機動翼群１６及び内側圧縮機動翼群１７を、段落毎圧縮機翼を環状に一体鋳造８４とします。全自動加工が可能な環状に一体鋳造８４の組立構造とし、環状鋳造組立接続部で冷却手段５５の水路を連結して、該組立環状接続部付近に水噴射手段５６を設けます。
【００８５】
全動翼圧縮機の主要部分の、外側圧縮機動翼群１６及び内側圧縮機動翼群１７の撥水性水冷却翼８７等を、図にない冷却手段５５により給水３で水冷却し、その給水を水噴射手段５６より噴射して圧縮空気を直接冷却し、低温圧縮空気として容積を縮小し、最も効率良く水冷却した低温圧縮空気にします。熱回収した給水３と低温圧縮空気により、燃焼器兼熱交換器４で限りなく高圧燃焼熱交換冷却燃焼熱回収して、全動翼蒸気ガスタービン燃焼ガス入口温度を最低に低下させ、同一燃料量の回収燃焼ガス熱量を、既存ボイラの２倍前後の熱回収量の、超臨界温度等複数温度の高温水５ｂとして燃焼ガス熱量出力とし、熱交換して得た低温燃焼ガスを燃焼ガス質量出力にします。
【００８６】
燃焼器兼熱交換器４で限りなく高圧燃焼熱交換冷却燃焼して熱回収し、既存ガスタービンの５００倍仮説出力等を発生して、燃焼ガス排気温度を−２７３℃に近付ける過程を、温度と容積の障害を最低にし、圧縮空気圧力を既存ガスタービンの２倍以上の、１０ＭＰａ以上を可能にして理論空燃比まで、同一圧縮空気量既存ガスタービンの４倍前後の燃料を燃焼可能にします。該熱交換して得た従来４倍燃料全発熱量＋圧縮した空気の−２７３℃以上略全熱量を（同一圧縮空気量既存ガスタービンの５倍落差×４倍回収熱量×５０倍超臨界圧力高温水重力仕事率×１０〜２０倍機械効率×１／２０減少率）＝（同一圧縮空気量既存ガスタービンの５００〜１０００倍仮説出力）等に増大します。
【００８７】
ＣＯ２等の燃焼ガス排気を０に近付けるため、超臨界温度等複数温度の高温水５ｂの貯蔵温度上昇時に、高温水加減弁７ａを開放制御して通常の出力を発生します。例えば超臨界温度等複数温度の高温水５ｂの一部を、全動翼蒸気ガスタービンの最上流に供給し、前述同様に中流最適段に最低温度の燃焼ガス１０全部を供給し、全動翼圧縮機を含む全動翼蒸気ガスタービンを駆動して、用途により出力を発生の過程で低温水噴射して、気化爆発水蒸気や燃焼ガスを冷却し、最低温度最少容積の単位容積重力仕事率を最大で、高温水や燃焼ガスや水蒸気を噴射して、空気吸引力と噴射質量最適速度により噴射推進出力を発生します。
【００８８】
高温水質量の速度重力仕事率にエネルギ変換して最適減速し、最大の噴射推進力を発生して、内側軸装置の中空部や外側軸装置の外周部の空気を吸引し、噴射推進する過程で、霧吹きの原理９１ｅの噴射高温水を含めて、低温燃焼ガスを５０倍質量等の水分に凝集溶解して、ＣＯ２等の燃焼ガス排気や水蒸気の容積を、１／１０００や１／１７００の水滴に縮小して、排気騒音を１/１０等とし、ＣＯ２等の燃焼ガス排気を０に近付け、海上等を噴射推進して、ＣＯ２や窒素や酸素等を希薄供給します。
【００８９】
大部分の超臨界温度等複数温度の高温水５ｂを、既存ガスタービンの５倍落差等により、複数の高温水加減弁７ａより、夫々複数の高温水溜３２ａに供給し、公知技術を含む複数の霧吹きの原理９１ｅを利用して、加熱高温手段１０１により適宜に加熱高温として、高温水５ｂとの間に気化膜を設けて摩擦損失を最少とした、砲身状乃至末広砲身状の高温水噴射ノズル５９ｂより、超臨界温度等複数温度の高温水５ｂを、霧吹きの原理等で適宜に混合して噴射し、超臨界圧力等の容積利用と気化爆発エネルギ利用により、重力仕事率を合理的な最大に上昇して出力を発生します。
【００９０】
出力発生の過程では高温水５ｂの気化爆発力や容積速度利用により、ノズル内では高温水５ｂを機関銃の弾丸や吹雪のように加速し、ノズル外では高温水を散弾ロケットや吹雪のように加速して、夫々霧吹きの原理９１ｅを利用して、前方の空気を多段に吸引して最適速度で噴射し、空気吸引力を含めて噴射質量速度により噴射推進する、夫々の特殊装置９２ｅよりバイパス噴射して、既存ガスタービンの２７０〜５４０倍仮説出力とし、ジェット旅客機等の速度を１０倍前後に増大して、排気騒音は１／１０等に低減して噴射推進します。
【００９１】
ジェット機や飛行船舶や飛行物体等を噴射推進させる過程を、霧吹きの原理を利用して、直接空気質量の速度エネルギに変換し、ラムジエツトを遥かに越える高速度で、最も効率良く空気を吸引して噴射推進し、１０倍前後の速度のマッハ１０以上に上昇して噴射推進します。超臨界温度等複数温度の高温水５ｂの貯蔵温度上昇により、非常に安全な噴射推進にすると共に、燃料の積載量を１／１０等に低減して使用量を１／１００等に低減し、火災の発生を１／１００等に低減して、火災発生時も高温水５ｂを噴射して消火容易にし、非常に安全なジェット機や飛行船舶や飛行物体や超高速船舶等にします。
【００９２】
超臨界温度等複数温度の高温水５ｂの一部と燃焼ガス１０全部により、全動翼蒸気ガスタービンを駆動して全動翼圧縮機を駆動して、前方の空気を吸引して噴射推進し、大部分の高温水５ｂを、公知技術を含む複数の霧吹きの原理９１ｅを利用して、夫々の特殊装置９２ｅにより高温水５ｂを、ラムジェットを遥かに越える大落差でバイパス噴射し、夫々前方の空気を多段に吸引して噴射し、超臨界温度等複数温度の高温水５ｂの、容積利用及び気化爆発エネルギ利用による質量速度を、直接空気質量の速度エネルギに変換して最適減速し、最適噴射速度で最も効率良く大質量噴射して、夫々の空気吸引力を加えて最適の噴射質量速度で噴射推進させるものです。
【００９３】
図６の全動翼蒸気ガスタービン合体機関の第３実施例も、起動時は図に無い弁を開閉制御して、燃焼器兼熱交換器４により限り無く高圧燃焼熱交換冷却燃焼して、熱交換して得た低温燃焼ガス１０を、高温水溜３２ａに供給して全動翼蒸気タービンを駆動する、全動翼ガスタービンとして使用します。燃焼器兼熱交換器４の超臨界温度等複数温度の高温水５ｂの温度上昇時に、燃焼ガス１０から高温水５ｂに切り替える、弁開弁閉弁制御して、高温水加減弁７ａを開放制御し、超臨界温度等複数温度の高温水５ｂの一部により、全動翼圧縮機を含む全動翼蒸気タービンを駆動して、高温水や気化爆発水蒸気を排気して、全動翼圧縮機や内側軸装置の中空部や外側軸装置の外周部から空気を吸引して、空気吸入出力と噴射質量速度により噴射推進出力を発生します。
【００９４】
燃焼ガス熱量を取り除いた、燃焼ガス質量出力の低温燃焼ガス１０全部や、残り大部分の高温水５ｂは夫々の霧吹きの原理を利用して、構造を簡単にすることでエネルギ変換効率を最高とし、ラムジエツトの５倍落差×５０倍質量重力仕事率等の噴射質量速度で噴射推進し、既存ガスタービンの２７０〜５４０倍仮説出力の、ジェット旅客機や飛行船舶や宇宙往還親飛行機等とし、その速度を１０倍前後に増大します。燃焼ガス１０や高温水５ｂは、夫々複数の霧吹きの原理９１ｂや９１ｅを利用して、夫々の特殊装置９２ｂや９２ｅによりバイパス噴射し、夫々前方の空気を多段に吸引して噴射推進力にする過程で、低温燃焼ガスにより水蒸気を冷却凝集して、水蒸気容積を１／１７００等に縮小し、排気騒音を１／１０等に低減します。
【００９５】
全動翼圧縮機の主要部分の、外側圧縮機動翼群１６及び内側圧縮機動翼群１７の撥水性水冷却翼８７等を、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより、昇圧した給水３を冷却手段５５により通水して水冷却し、その給水を水噴射手段５６より水噴射して圧縮空気を直接冷却し、その熱を回収した給水として空気容積を縮小します。全動翼とすることで翼間隔を増大した全動翼翼形として、圧縮空気を略直線蛇行的に圧縮して、最も効率良く低温空気を圧縮する撥水性水冷却翼８７で成る、外側圧縮機動翼群１６及び内側圧縮機動翼群１７を、段落毎に環状に一体鋳造８４とします。
【００９６】
全自動加工が可能な環状に一体鋳造８４の組立構造とし、環状鋳造組立接続部で冷却手段５５の水路を連結して、該組立環状接続部付近に水噴射手段５６を設けます。冷却手段５５の水路は撥水性水冷却翼８７を冷却後に、水噴射手段５６より水噴射直接接触空気冷却し、最も効率良く給水３で空気冷却して、低温空気を全動翼圧縮機で用途により限り無く高圧圧縮します。熱回収した給水３と低温圧縮空気により、燃焼器兼熱交換器４で限りなく高圧燃焼熱交換冷却燃焼して、既存ボイラの２倍前後の熱回収し、全動翼蒸気タービンの環状の燃焼ガス溜９の、燃焼ガス温度を用途に合わせて最低に低下させます。
【００９７】
全動翼蒸気タービン等、動圧や反動で駆動する回転出力機関は、超臨界温度等複数温度の高温水５ｂは、超臨界圧力から大気圧までで充分大きな落差で、燃焼ガスの５０倍質量など大きな重力仕事率のため、構造を１/１０等の小型簡単合理的な設計を可能にします。既存蒸気タービンのように落差を増大した容積利用にしても、重力仕事率を極限まで低減すると、膨大な静翼を設けて蒸気速度を堰き止めて実用速度に減速する等、無茶苦茶設計になるため、動圧出力を増大する単位容積重力仕事率の増大を最重要とし、大気圧単位容積重力仕事率の最大を１７００倍に増大して、該動翼面積の一部乃至大部分を１／１７００に縮小し、合理的な全動翼の設計や１／１０等の小型簡単大出力を可能にます。
【００９８】
燃焼器兼熱交換器４で限りなく高圧燃焼熱交換して熱回収し、燃焼ガス取出口８８の燃焼ガス温度を最低に低下させて、既存ボイラの２倍前後の回収熱量を、超臨界温度等複数温度の高温水５ｂの回収熱量として最大に増大し、大部分の出力を構造が最も簡単な霧吹きの原理を利用することで、エネルギ変換効率を最高として、熱交換して得た（燃焼ガス熱量出力既存ガスタービンの２５０〜５００倍出力）＋（燃焼ガス質量出力既存ガスタービンの２０〜４０倍出力）＝（同一燃料量既存ガスタービンの２７０〜５４０倍仮説出力）にします。
【００９９】
超臨界温度等複数温度の高温水５ｂとしてその一部を、全動翼蒸気タービンの最上流に供給し、出力発生の過程で用途により水噴射して、気化爆発水蒸気や容積利用水蒸気を冷却し、水蒸気容積速度の一部分を、大気圧１７００倍単位容積重力仕事率の水に変換して、最適容積速度に縮小減速し、最も効率良く回転出力を発生させます。そして夫々の霧吹きの原理９１ｅ・９１ｂを利用して、残りの高温水５ｂと燃焼ガス１０を、夫々既存ガスタービンの５倍落差や２倍落差でバイパス噴射し、既存ガスタービンの２７０〜５４０倍仮説出力にする過程で、低温燃焼ガスにより水蒸気を冷却して１／１７００容積に縮小し、排気騒音を１／１０等に低減して、ＣＯ２等燃焼ガス排気を０に近付けて水滴で排出し、地球温暖化防止します。
【０１００】
図７の全動翼蒸気ガスタービン合体機関の第４実施例は、全動翼翼形として外側圧縮機動翼群１６及び内側圧縮機動翼群１７を、段落毎に環状に一体鋳造８４し、全自動加工が可能な組立構造とし、環状鋳造組立接続部で冷却手段５５の水路を連結して、該組立環状接続部付近に水噴射手段５６を設けます。そして全動翼圧縮機の撥水性水冷却翼８７の、段落半分又は段落全部又は段落複数を、冷却手段５５により通水して水冷却し、その水を水噴射手段５６より噴射して、圧縮空気を直接接触水冷却し、その熱を給水３で最も効率良く熱回収して、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａ等により、燃焼器兼熱交換器４に供給し、低温空気を限り無く高圧圧縮して燃焼器兼熱交換器４に供給します。
【０１０１】
熱回収した給水３と低温圧縮空気により、燃焼器兼熱交換器４で限りなく高圧燃焼熱交換冷却燃焼熱回収して、燃焼ガス取出口８８の温度を用途に合わせて最低に低下させ、同一燃料量既存ボイラの２倍前後の回収熱量の燃焼ガス熱量出力を、超臨界温度等複数温度の高温水５ｂ等として、その一部を単位重力仕事率が重要な、全動翼蒸気タービンの最上流に供給し、出力発生の過程で用途により給水３を噴射して、容積利用水蒸気や気化爆発水蒸気を冷却し、水蒸気容積速度の一部分を、大気圧１７００倍単位容積重力仕事率の水に変換して、最適容積に縮小して最適減速し、最も効率良く回転出力を発生させ、回転出力により全動翼圧縮機を駆動し、排気噴射出力は船舶等の浮上推進出力とします。
【０１０２】
燃焼ガス１０全部及び残り大部分の超臨界温度等複数温度の高温水５ｂを、夫々の霧吹きの原理９１ｄ・９１ｆを利用して、前方の水を多段に吸引して噴射し、夫々の速度を直接水の速度質量にエネルギ変換して最適減速し、最も効率良く大量の水を吸引して噴射する、夫々１以上複数の水噴射装置９３ｄ・９３ｆにより出力を発生し、大部分の出力を構造が最も簡単な霧吹きの原理を利用することで、エネルギ変換効率を最高として、既存ガスタービンの２７０〜５４０倍仮説出力の、各種高速船舶や各種高速水上移動機器を、同一燃料量既存技術の１０倍前後等適宜の速度で噴射推進させ、地球温暖化防止します。
【０１０３】
燃焼ガス１０全部を夫々の霧吹きの原理９１ｄを利用して噴射し、前方の水を多段に吸引して噴射して、直接水の速度質量にエネルギ変換する過程では、燃焼ガス１０が断熱膨張大気圧−２７３℃に近付くため、海水等を冷却してＣＯ２や窒素等の燃焼ガスを大量の海水に溶解し、海底などに冷熱として供給する過程でも、霧吹きの原理を適宜に利用して、空気や酸素等を吸引して海中に希薄供給し、海の生物の生態を微生物まで徹底的に研究し、微生物や魚介類や海草類や海藻類を繁殖させて、食料の増産を図り、ＣＯ２等の燃焼ガス排気を０等にし、地球温暖化防止します。
【０１０４】
図８・図９・図１０・図１１を参照して、送水ポンプ兼磁気摩擦動力伝達装置１００ａ及び、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａを説明する。通常の変速や逆転を含む各種動力伝達装置は、主として歯車装置を使用している。このため、歯面に大きな荷重を含む、滑り歯面を必須とするため、潤滑油を必要とするのに加えて、摩擦熱損失も非常に大きく、高速回転を含む大動力の伝達装置には、使用不可という問題がある。
【０１０５】
全動翼蒸気ガスタービン合体機関を実用化するには、ころがり接触による、超高速大動力伝達装置が必須です。超高速大動力伝達装置を可能にすると共に、潤滑油も不用にするためには、歯車装置の滑り歯面を皆無に近づけた転がり接触の、水冷却した摩擦熱を回収して燃焼器兼熱交換器４に供給する、多段多数で超高圧少量送水して、既存技術の２〜１０倍回転数を狙う宇宙往還親飛行機等の、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、送水ポンプ兼磁気摩擦動力伝達装置１００ａとして使用し、互いに反対方向に回転する外側軸装置と内側軸装置を結合して、超高圧少量送水ポンプや各種動力伝達装置としても使用し、給水３により熱回収して超高圧少量送水します。
【０１０６】
歯車のかみ合い高さを限りなく縮小した低凹凸４０として、転がり接触の送水ポンプ兼磁気摩擦動力伝達装置１００ａとし、回転方向３５上流側及び下流側、又は上流側又は下流側に、棒磁石３３又は電磁石３４を設けます。そして磁石の強い吸引力を利用して、各種着磁摩擦車装置５１や、図にない各種磁着摩擦車装置９０や、各種内着磁摩擦車装置４９や、図にない各種内磁着摩擦車装置８９等の、すべての噛み合わせ使用を可能にし、既存技術の２〜１０倍回転数を狙います。
【０１０７】
超高圧少量送水の各種送水ポンプ兼各種二重反転磁気摩擦動力伝達装置１４ａとし、外箱９４に吸水路９５や送水路９６を設け、各種送水ポンプ９７兼用として、公知技術を含めて全面的に使用します。即ち、転がり接触に近付けて、摩擦熱損失を大幅に低減し、更に超高圧少量送水する送水ポンプ９７と兼用として、自己発熱を回収する、超高速で大動力を伝達する、送水ポンプ兼磁気摩擦動力伝達装置１００ａや、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、潤滑油に換えて無公害の水冷却とし、熱回収した給水３を、燃焼器兼熱交換器４側に供給して使用する、送水ポンプ９７兼用の二重反転磁気摩擦動力伝達装置１４とするものです。
【０１０８】
超高速大動力を伝達する、二重反転磁気摩擦動力伝達装置１４や、磁気摩擦動力伝達装置１００とするために、転がり接触に近付けても、摩擦熱の発生を避けられません。一方全動翼蒸気ガスタービン合体機関は、超高圧少量の水や大量の熱を利用して、内側軸装置と外側軸装置を二重反転させて、出力を発生させるため、超高速大動力を伝達すると共に、熱回収して超高圧少量送水する送水ポンプ９７が必要なため、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、送水ポンプ兼磁気摩擦動力伝達装置１００ａとして使用します。
【０１０９】
そこで各種歯車に換えて、各種着磁摩擦車３７や各種内着磁摩擦車３８や、各種磁着摩擦車３９や図にない各種内磁着摩擦車４４等を使用し、二重反転磁気摩擦動力伝達装置１４として使用の過程で、回転方向上流側及び下流側又は上流側又は下流側に、棒磁石３３乃至電磁石３４を設けることで、着磁摩擦車や磁着摩擦車や内着磁摩擦車や内磁着摩擦車の、すべての組み合わせを、磁石の強い吸引力により、互いに互換して使用を可能にし、既存技術の２〜１０倍回転数を狙う、各種送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、各種送水ポンプ兼磁気摩擦動力伝達装置１００ａとして使用します。
【０１１０】
着磁摩擦車３７や磁着摩擦車３９や内着磁摩擦車３８や内磁着摩擦車４４の、動力伝達面３１には低凹凸４０を設けます。低凹凸４０は噛み合い高さを限りなく低下させて、転がり接触として歯車以外の形状を可能にし、図に無いすべての噛み合う形状全部とします。歯車形低凹凸４０として具体的には、平歯車に換えて平凹凸４１車とし、ハスバ歯車に換えてハスバ凹凸４２車とし、ヤマバ歯車に換えてヤマバ凹凸４３車を設けて、超高圧少量送水や大動力高速伝達を可能にします。
【０１１１】
又は図に無い平内歯車に換えて平内凹凸４１ａ車とし、ハスバ内歯車に換えてハスバ内凹凸４２ａ車とし、ヤマバ内歯車に換えてヤマバ内凹凸４３ａ車を設ける。そして公知の各種歯車ポンプと同様に、外箱９４や吸水路９５や送水路９６を設けて、摩擦熱を回収して超高圧少量送水する送水ポンプ９７兼用として、超高速大動力を伝達する、既存技術の２〜１０倍回転数を狙う、各種送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、各種送水ポンプ兼磁気摩擦動力伝達装置１００ａとして使用します。
【０１１２】
図８ａ・図８ｂの着磁摩擦車３７ａの実施例は、環筒状の強磁性材料の径方向左右に、磁極のＮ極及びＳ極を着磁して、その両側を環板状のヨーク４７で挟んで、外径方向動力伝達面３１に延長して固着します。該動力伝達面３１の外周面に低凹凸４０の平凹凸４１やハスバ凹凸４２等を設けて、夫々着磁摩擦車３７ａ・３７ａ等として、各要素を互いに互換して、着磁摩擦車３７ａ・磁着摩擦車３９や、転がり接触の着磁摩擦車装置５１とし、図９の着磁摩擦車装置５１ｃ＋９７や図１１の９７＋１４と同様に外箱９４や吸水路９５や送水路９６等を設けて、各種送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、各種送水ポンプ兼磁気摩擦動力伝達装置１００ａとして使用します。
【０１１３】
図８ｃの着磁摩擦車３７ｂの実施例は、環筒状の強磁性材料の内径側と外径側に磁極のＮ極及びＳ極を着磁して、ヨーク４７を磁石の内周側から左右外径動力伝達面３１に延長します。該動力伝達面近傍のヨークと磁石の間に、摩擦増大手段４５を環状に設けて固着し、その外周面に低凹凸４０のヤマバ凹凸４３を設けて、夫々着磁摩擦車３７ｂ・３７ｂとして、各要素を互いに互換して磁着摩擦車３９・着磁摩擦車３７ｂや、図１０の着磁摩擦車装置５１ｄ＋９７や図１１の９７＋１４と同様に外箱９４や吸水路９５や送水路９６等を設けて、各種送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、各種送水ポンプ兼磁気摩擦動力伝達装置１００ａとして使用します。
【０１１４】
図８ｄ・図８ｅ・図８ｆの磁着摩擦車３９の実施例は、環筒状の強磁性材料の外径面の動力伝達面３１に、摩擦増大手段４５を設けます。又は動力伝達面３１のまま、その外周面に低凹凸４０の平凹凸４１又はハスバ凹凸４２又はヤマバ凹凸４３を設けて、夫々各種磁着摩擦車３９・３９等とします。図９・図１０図１１のように、回転方向上流側及び下流側に棒磁石３３又は電磁石３４を設けることで、夫々各要素を互いに互換して、図番の無い転がり接触の各種磁着摩擦車装置９０や、各種磁気摩擦動力伝達装置１００とします。
【０１１５】
又は図にない環筒状の強磁性材料の内径面の動力伝達面３１に、摩擦増大手段４５を設けます。又は動力伝達面３１のまま、その内周面に低凹凸４０の平凹凸４１又はハスバ凹凸４２又はヤマバ凹凸４３を設けて、夫々各種内磁着摩擦車４４・４４等とします。夫々各要素を互いに互換して、転がり接触の各種内磁着摩擦車装置８９等とし、図９や図１０や図１１の、磁気摩擦動力伝達装置１００や二重反転磁気摩擦動力伝達装置１４と略同様に、外箱９４や多数の吸水路９５や多数の送水路９６等を設けて、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、送水ポンプ兼磁気摩擦動力伝達装置１００ａ等として使用します。
【０１１６】
例えば図９・図１０の各種送水ポンプ兼磁気摩擦動力伝達装置１００ａの、第１実施例及び第２実施例は、着磁摩擦車装置５１ｃ・５１ｄに、既存歯車ポンプと同様に外箱９４を設け、夫々に吸水路９５及び送水路９６を設けて、各種送水ポンプ９７を構成使用します。そして吸水路９５より給水３を供給して、各種磁気摩擦動力伝達装置１００で発生する熱を回収して、送水路９６より燃焼器兼熱交換器４側に送水します。
【０１１７】
しかし着磁摩擦車装置５１ｃ・５１ｄ等、多種多数の各種送水ポンプ兼磁気摩擦動力伝達装置１００ａにより、送水ポンプ兼用となるのと動力伝達が主力のため、回転数も変化します。そこで公知の制御装置により、１以上多数の送水路９６や吸水路９５を最適制御して、１以上多段に昇圧の過程で水噴射手段５６・５６ａに供給し、燃焼器兼熱交換器４で超臨界温度等複数温度の高温水５ｂとします。即ち１以上多数の送水ポンプ９７により、摩擦熱を回収して自己水冷却し、超高速大動力を伝達しながら超高圧少量送水する、各種送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａや、各種送水ポンプ兼磁気摩擦動力伝達装置１００ａとして使用します。
【０１１８】
例えば、図１１の超高速大動力を伝達して、超高圧少量送水を可能にする、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａは、外箱９４に多数の吸水路９５及び多数の送水路９６及び多数の着磁摩擦車３７ａ及び内着磁摩擦車３８ａ等で、多数の送水ポンプ９７が構成されるため、外箱９４も非常に複雑になります。しかし着磁摩擦車３７ａの周速度は２種類のため、同じ周速度のものを合流して、この場合は２段や多段に昇圧して圧力制御し、用途に合わせて他の送水ポンプとも組み合わせて、燃焼器兼熱交換器４側に給水します。多数の送水ポンプ９７により摩擦熱を回収して自己水冷却し、超高速大動力を伝達する、送水ポンプ９７兼用の各種二重反転磁気摩擦動力伝達装置１４として使用します。
【０１１９】
図１１（ａ）（ｂ）（ｃ）を参照して説明する。（ｂ）（ｃ）は夫々（ａ）のｃ−ｃ及びｄ−ｄ視図であり、互いに反対方向に回転する全動翼蒸気ガスタービン合体機関の、内側軸装置と外側軸装置の回転動力を結合する、二重反転磁気摩擦動力伝達装置１４は、多数の送水ポンプ９７により摩擦熱を多段に回収して自己水冷却し、互いに反対方向に回転する２軸の超高速大動力を、最適回転比で二重反転伝達する、二重反転磁気摩擦動力伝達装置１４として使用します。
【０１２０】
全動翼蒸気ガスタービン合体機関の外側軸装置に固着された、磁石部４６及びヨーク４７を含む、第一主動内着磁摩擦車３８ａの回転により、機関本体に固定された外箱９４に軸支された、支軸５０の左端に固着された複数の第一従動着磁摩擦車３７ａが回転し、その回転により支軸５０の右端に固着した、複数の第二主動着磁摩擦車３７ａが回転し、その回転により内側軸装置に固着された、第二従動着磁摩擦車３７ａが回転し、互いに反対方向に回転する外側軸装置の回転力と、内側軸装置の回転力を結合して、内側軸装置又は外側軸装置より全回転出力を取り出し可能にし、又は両方より夫々回転出力を取り出し可能とします。
【０１２１】
図１１（ｂ）（ｃ）は、超高速大動力の伝達と超高圧少量送水する、送水ポンプ９７兼用の二重反転磁気摩擦動力伝達装置１４として使用の過程で、回転方向上流側及び下流側又は上流側又は下流側に、棒磁石３３乃至電磁石３４を設けることで、着磁摩擦車３７や磁着摩擦車３９や内着磁摩擦車３８や内磁着摩擦車４４の、すべての組み合わせを、磁石の強い吸引力により、互いに互換して使用を可能にします。外側軸装置に固着の内着磁摩擦車３８ａや、内側軸装置に固着の着磁摩擦車３７ａや、夫々に噛み合う夫々複数の着磁摩擦車３７ａを含めて、既存歯車ポンプと略同様に外箱９４を設けます。
【０１２２】
そして内着磁摩擦車３８ａに噛み合う複数の着磁摩擦車３７ａの、回転方向棒磁石３３又は電磁石３４を含む上流側に送水路９６を設け、回転方向棒磁石３３又は電磁石３４を含む下流側に吸水路９５を設け、内側軸装置に固着の着磁摩擦車３７ａに噛み合う複数の着磁摩擦車３７ａの、回転方向電磁石３４又は棒磁石３３を含む上流側に送水路９６を設け、回転方向電磁石３４又は棒磁石３３を含む下流側に吸水路９５を設けて、送水ポンプ９７兼超高速大動力を伝達する送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａを構成します。
【０１２３】
図１２により本発明による地球温暖化防止を説明する。世界の火力発電所や原子力発電所では、ボイラや原子力等で加熱した超臨界圧力過熱蒸気は、蒸気タービンにより断熱膨張させて、容積のみ利用して熱量を全く利用しないで、ボイラや原子力等で加熱した熱量全部で海水温度を上昇するため、膨大な熱量の損失と環境破壊になります。更に超臨界圧力過熱蒸気から復水器真空まで再熱等で断熱膨張させると、容積は１００００倍を超えて重力仕事率が１／１００００以下となり、同一条件の出力に１００００倍以上の動翼面積が必要で、膨大な蒸気速度も利用困難となり、動翼の１０〜２０倍も蒸気速度を消費して、回転仕事をしない静翼を１／２も設けて、蒸気速度を堰き止めて実用速度に減速する等、無茶苦茶設計による地球温暖化加速を避けられません。
【０１２４】
最も甚大な無茶苦茶は、動翼の１０〜２０倍も速度エネルギを消費して、全く回転仕事をしない静翼を１／２も設けて、過熱蒸気速度を堰き止めて減速していることです。そこで熱量を有効利用するため、ガスタービン燃焼器を熱交換器と兼用して、全動翼蒸気ガスタービン燃焼器兼熱交換器４により、限り無く高圧燃焼熱交換冷却燃焼して、燃焼ガス排気温度を−２７３℃に近付け、膨大な冷熱や温熱を発電の副産物として製造原価略０で供給し、ＣＯ２等燃焼ガス排気により水蒸気を冷却して、凝縮水等にＣＯ２等の燃焼ガスを溶解して、ＣＯ２等の排気を０等として地球温暖化防止します。そして同一燃料量既存ボイラの２倍前後に回収熱量を増大し、超臨界温度等複数温度の高温水５ｂ等として回収して（燃焼ガス熱量出力＋燃焼ガス質量出力）＝（既存ガスタービンの２７０〜５４０倍仮説出力）に増大し、地球温暖化防止します。
【０１２５】
既存ボイラの２倍前後の超臨界温度等複数温度の高温水５ｂの熱量を、全動翼蒸気タービンの最上流に供給し、大気圧既存再熱蒸気タービンの１７００倍重力仕事率の超臨界圧力高温水５ｂを、加熱高温として高温水との間に気化膜を設けて、摩擦損失を最少とした高温水噴射ノズル５９ｂ内やノズル外では、気化爆発力や容積速度利用により、高温水５ｂを機関銃の弾丸や散弾ロケットや吹雪のように加速して、大気圧単位容積重力仕事率を既存蒸気タービンの１７００倍に近付け、燃焼ガス熱量出力＋燃焼ガス質量出力を、同一燃料量既存ガスタービンの２７０〜５４０倍仮説出力に上昇し、地球温暖化防止します。
【０１２６】
全動翼蒸気タービンでは加えた熱全部を回収利用するため、気化潜熱回収器６６ａを既存復水器と略同様に設けて、例えば飽和温度１００℃の気化熱を海水に換えて水道水で冷却し、熱回収して得た膨大な気化熱全部を、発電の副産物として製造原価略０の水道水温熱として、１００℃以下で貯蔵しておき、１/１０等の安価な電気料金と共に水道水温熱として需要家に供給し、需要の爆発的拡大を図ります。そして凝縮水全部は、燃焼器兼熱交換器４に限り無く繰り返し循環供給することで、燃焼器兼熱交換器４では高温水の気化爆発エネルギの供給のみとし、燃料燃焼質量を最少に低減して、気化熱全部＋αで海水温度を上昇していた、既存技術蒸気タービンの無茶苦茶を全廃します。
【０１２７】
全動翼ガスタービン発電の副産物を簡略説明する、全動翼ガスタービン燃焼器兼熱交換器４により、限り無く高圧燃焼熱交換冷却燃焼して、燃焼ガス排気温度を−２７３℃に近付け、冷熱回収器１０２により、低温燃焼ガス全部の膨大な冷熱を水道水で回収し、発電の副産物の製造原価略０の水道水冷熱として、２〜５℃等で貯蔵しておき、１/１０等の安価な電気料金と共に、水道水冷熱として需要家に供給し、業務用や家庭用の冷蔵設備やクーラーや冷凍設備を全廃して、水道水冷熱利用の冷蔵設備やクーラーや冷凍設備を供給し、膨大過ぎる水道水冷熱は散水して都市部を丸ごと冷却する等、ＣＯ２等の燃焼ガス排気０や脱フロンにより、地球温暖化防止します。
【０１２８】
図１３の全動翼ガスタービン及び全動翼蒸気タービンの回転力で駆動する、各種装置を説明する。燃焼器兼熱交換器４により限り無く高圧燃焼熱交換冷却燃焼して、既存ボイラの２倍前後の熱回収量として、燃焼ガス排気温度を−２７３℃に近付け、全動翼ガスタービン及び全動翼蒸気タービンにより、電気料金を１／１０等に低減して、気化潜熱回収器６６ａにより供給熱量全部を、発電の副産物として１００℃以下の水道水温熱として需要家に供給し、冷熱回収器１０２により燃焼ガス全部を発電の副産物の、膨大な水道水冷熱として需要家に供給する、各種熱と電気と冷熱の供給設備を駆動します。
【０１２９】
回転出力発生用の全動翼蒸気タービンの、燃焼器兼熱交換器４により限り無く高圧燃焼熱交換冷却燃焼し、燃焼ガス排気温度を−２７３℃に近付けて、全動翼ガスタービンを駆動して、発電や冷房等の別用途に使用します。熱交換して得た既存ボイラの２倍前後の熱回収量の高温水５ｂとして、大気圧まで出力を発生させて、既存ガスタービンの２５０〜５００倍仮説出力とし、空冷式気化潜熱回収器６６ｂにより凝縮水を回収して、燃焼器兼熱交換器４に限り無く供給し、凝縮水を限り無く循環使用する、各種全動翼蒸気ガスタービン合体機関により、各種自動車・各種車両・各種機械・各種汎用機関・各種戦車等を駆動します。
【０１３０】
高温水５ｂの一部で回転出力発生の全動翼蒸気タービンの、燃焼器兼熱交換器４により限り無く高圧燃焼熱交換冷却燃焼し、燃焼ガス排気温度を−２７３℃に近付けます。大部分の高温水５ｂや燃焼ガス全部を、霧吹きの原理を利用してバイパス噴射し、前方の空気又は水を吸引して噴射し、既存ガスタービンの２７０〜５４０倍仮説出力として、既存技術の１０倍速度や排気騒音の１／１０等を狙う、各種全動翼蒸気ガスタービン合体機関により、各種超高速船舶・各種垂直昇降飛行機・各種超高速艦船・各種超高速戦闘機・各種宇宙往還親飛行機・各種超高速音速機・各種超高速飛行機器等を駆動します。
【０１３１】
【発明の効果】
超臨界温度等複数温度の高温水５ｂを、高温水噴射ノズル５９ｂより噴射するため、最も効率良く大気圧単位容積重力仕事率を、既存蒸気タービンの１７００倍に近付けて、同一燃料量既存ガスタービンの５００倍仮説出力等に増大する効果がある。
【０１３２】
超臨界温度等複数温度の高温水５ｂを、高温水噴射ノズル５９ｂより噴射するため、最も効率良く大気圧単位容積重力仕事率を、既存蒸気タービンの１７００倍に近付け、動翼面積の一部乃至大部分を１／１７００に縮小して、合理的な動翼面積を設計可能にし、構造を１／１０等の小型簡単大出力にする効果がある。
【０１３３】
超臨界温度等複数温度の高温水５ｂを使用するため、加熱高温手段により加熱高温とした高温水噴射ノズル５９ｂにより、高温水との間に気化膜を設けて、摩擦損失最少で高温水の気化爆発力や容積速度利用により、高温水噴射ノズル５９ｂ内では高温水を機関銃の弾丸や吹雪のように加速し、ノズル外では散弾ロケットや吹雪のように高温水を加速して、同一燃料量既存ガスタービンの５００倍仮説出力等にする効果がある。
【０１３４】
全動翼電磁加熱タービン動翼８１及び電磁加熱噴口８３を、電磁加熱高温として高温水との間に気化膜を設けて、摩擦損失を僅少として全動翼により略直線蛇行的に噴射するため、最も効率良く出力を発生する効果があります。
【０１３５】
電磁加熱外側タービン動翼群１９及び、電磁加熱内側タービン動翼群２０を段落毎環状に一体鋳造として、容易確実に電磁加熱高温にする効果があります。
【０１３６】
断熱して設けた水噴射手段５６ａの鋳込みにより、水噴射して燃焼ガスや気化爆発水蒸気を冷却し、単位容積質量や全質量を増大して温度低下し、ＣＯ２等の燃焼ガス排気を０に近付けることを、確実容易にする効果があります。
【０１３７】
燃焼ガス排気温度を−２７３℃に近付けて、大きな単位容積重力仕事率や全重力仕事率にしても、全動翼電磁加熱タービン動翼８１により、高温水等との間に気化膜を設けて摩擦損失最小で、大きな出力を発生させる効果があります。
【０１３８】
低温高圧空気を燃焼器兼熱交換器で、限りなく高圧燃焼熱交換することで、理論空燃比まで燃料燃焼質量を、既存ガスタービンの４倍前後に増大し、全動翼蒸気ガスタービン合体機関の燃焼ガス入口温度や、燃焼器兼熱交換器の燃焼ガス出口温度を最低としたため、圧縮圧力を２倍以上の１０ＭＰａ以上に上昇し、燃焼ガス質量出力を、既存ガスタービンの２０〜４０倍仮説出力に上昇する効果があります。
【０１３９】
熱交換して得た燃焼ガス熱量に、圧縮空気−２７３℃以上略全部を加えて、同一燃料量既存ボイラの２倍前後の燃焼ガス熱量を、超臨界温度等複数温度の高温水５ｂに変換して回収し、燃焼ガス熱量出力を、既存ガスタービンの２５０〜５００倍仮説出力に上昇する効果がある。
【０１４０】
超臨界温度等複数温度の高温水５ｂとして、全動翼蒸気ガスタービンや、全動翼蒸気タービンや、特殊装置９２ｅ・９２ｂを駆動して、最も効率良く空気を吸引して噴射推進し、燃焼ガス質量出力＋燃焼ガス熱量出力を、既存ガスタービンの２７０〜５４０倍仮説出力に増大する効果があります。
【０１４１】
超臨界温度等複数温度の高温水として、全動翼蒸気ガスタービンや、全動翼蒸気タービンや、水噴射装置９３ｄ・９３ｆを駆動して、最も効率良く水を吸引して噴射推進し、燃焼ガス質量出力＋燃焼ガス熱量出力を、既存ガスタービンの２７０〜５４０倍仮説出力に増大する効果があります。
【０１４２】
燃焼ガス排気温度を−２７３℃に近付けて、全動翼ガスタービンの燃焼ガス熱量消費０以下の、同一燃料量燃焼ガス質量出力を、既存ガスタービンの２０〜４０倍仮説出力に上昇する効果があります。
【０１４３】
低温水噴射して気化爆発水蒸気や燃焼ガスを冷却し、重力仕事率が１０００倍や１７００倍の水質量の速度パワーに、エネルギ変換して最適減速するため、全動翼蒸気ガスタービン合体機関の構造を、１／１０前後等に小型簡単大出力に設計できる効果があります。
【０１４４】
燃焼器兼熱交換器で限りなく高圧燃焼熱交換して、既存ボイラの２倍前後の熱回収量とし、電気料金を１／１０等に低下させて、発電所等から排出されるＣＯ２等の地球温暖化燃焼ガスを、最も効率良く回収利用する効果もあります。
【０１４５】
既存の業務用や家庭用の冷蔵設備や冷凍設備や冷房設備を全廃し、水道水冷熱利用の業務用や家庭用の冷蔵設備や冷凍設備や冷房設備を提供し、脱フロンやＣＯ２排気０等による地球温暖化防止の効果もあります。
【０１４６】
発電量を増大する程極低温燃焼ガスの増産になるため、海水を冷却すると海底にＣＯ２や窒素や酸素を希薄供給して、餌となる微生物や海藻や魚類等を繁殖させて、海域等を活性化する効果があり、濃度さえ適正なら有効利用可能で、海底固定等の誤りを逆転して、人類のために貢献する手法を皆で考える効果がある。
【０１４７】
各種全動翼蒸気ガスタービン合体機関の燃焼器兼熱交換器で、限りなく高圧燃焼熱交換することで、理論空燃比まで同一圧縮空気量の燃料燃焼質量を、既存ガスタービンの４倍前後とし、燃焼ガス入口温度を最低としたため、圧縮圧力を２倍以上の１０ＭＰａ以上を可能にし、同一燃料量既存ガスタービンの５００倍仮説出力等に増大する効果があります。
【０１４８】
熱交換して得た低温燃焼ガスや高温水５ｂの水蒸気を水冷却し、単位容積重力仕事率が既存蒸気タービンの大気圧１７００倍の水質量を、最大最適に増大して重力仕事率を５０倍前後に増大可能する効果があります。
【０１４９】
既存蒸気タービン過熱蒸気の大気圧部１７００倍重力仕事率の、大きな動圧により出力を発生出来る大きな効果があります。
【０１５０】
重力仕事率を大気圧部既存蒸気タービンの１７００倍に増大することで、タービン動翼面積の一部乃至大部分を、１／１７００に縮小して、構造を１／１０等の大幅に小型簡単に出来る効果があります。
【０１５１】
既存再熱蒸気タービンの再熱や静翼を全廃して、構造を全動翼小型簡単大出力に出来る大きな効果があります。
【０１５２】
全動翼蒸気ガスタービンや、全動翼蒸気ガスタービン合体機関で出力を発生の過程で、水噴射して水蒸気や燃焼ガスを冷却して、低温水質量を増大するため、断熱膨張低温燃焼ガスにより水分を冷却凝集して、自然現象と同様に水滴等として、５０倍質量等の水にＣＯ２等の燃焼ガスを合成溶解混合する過程で、化学物質等を加えて無害で排出可能にする効果もあります。
【０１５３】
各種自動車や各種船舶や各種飛行機や、各種機械装置等から排出される、ＣＯ２等の公害燃焼ガス排気を水滴として排出して、ＣＯ２等の排気を大幅に低減する効果があります。
【０１５４】
全動翼蒸気ガスタービン合体機関としたため、全動翼ガスタービンの全動翼圧縮機や燃焼器兼熱交換器４を除去して、非常に小型簡単な全動翼ガスタービンに出来る効果があります。
【０１５５】
空冷式気化潜熱回収器６６ｂを含めたため、各種自動車等の輸送用機器では、凝縮水を燃焼器兼熱交換器４に限り無く繰返し供給して、凝縮水を循環使用出来る効果があります。
【図面の簡単な説明】
【図１】全動翼蒸気タービンの第１実施例を示す一部断面図。
【図２】高温水噴射ノズル５９ｂの実施例を示す断面説明図。
【図３】全動翼ガスタービンの第１実施例を示す一部断面図。
【図４】全動翼蒸気ガスタービン合体機関の第１実施例を示す一部断面図。
【図５】全動翼蒸気ガスタービン合体機関の第２実施例を示す一部断面図。
【図６】全動翼蒸気ガスタービン合体機関の第3実施例を示す一部断面図。
【図７】全動翼蒸気ガスタービン合体機関の第４実施例を示す一部断面図。
【図８】着磁摩擦車及び磁着摩擦車の実施例を示す一部断面図。
【図９】送水ポンプ兼磁気摩擦動力伝達装置の第１実施例の一部断面図。
【図１０】送水ポンプ兼磁気摩擦動力伝達装置の第２実施例の一部断面図。
【図１１】送水ポンプ兼二重反転磁気摩擦動力伝達装置の実施例の一部断面図。
【図１２】全動翼蒸気ガスタービン合体機関で地球温暖化防止する説明図。
【図１３】全動翼蒸気ガスタービン合体機関で駆動する装置を示す説明図。
【符号の説明】
１：導水管 ２：給水ポンプ ３：給水 ４：燃焼器兼熱交換器 ５：水蒸気 ５ａ：高温水 ５ｂ：高温水（霧吹きの原理等で適宜に混合して噴射する超臨界温度等複数温度の高温水） ６：蒸気管 ６ａ：高温水管 ７：蒸気加減弁 ７ａ：高温水加減弁 ８：環状の圧縮空気溜 ９：環状の燃焼ガス溜 １０：燃焼ガス １１：燃料 １２：出力軸 １３：止め弁 １４：二重反転磁気摩擦動力伝達装置 １４ａ：送水ポンプ兼二重反転磁気摩擦動力伝達装置 １５：圧縮空気 １６：外側圧縮機動翼群 １７：内側圧縮機動翼群 １９：電磁加熱外側タービン動翼群 ２０：電磁加熱内側タービン動翼群 ２１：環状の出口 ２２：環状の受け口 ２３：環状の受け口 ２４：環状の電磁加熱噴口群 ２５：燃焼器外箱部 ２６：水冷外壁 ２７：燃料蒸気供給手段 ２８：バイパス ３１：動力伝達面 ３２：過熱蒸気溜 ３２ａ：高温水溜 ３３：棒磁石 ３４：電磁石 ３５：回転方向 ３６：磁極 ３７：着磁摩擦車 ３８：内着磁摩擦車 ３９：磁着摩擦車 ４０：低凹凸 ４１：平凹凸 ４２：ハスバ凹凸 ４３：ヤマバ凹凸 ４４：内磁着摩擦車 ４５：摩擦増大耐久手段 ４６：磁石部 ４７：ヨーク（着磁摩擦車用） ４８：絶縁材料 ４８ａ：断熱材 ４９ａ：内着磁摩擦車装置 ４９ｂ：内着磁摩擦車装置 ５０：支軸 ５１ａ：着磁摩擦車装置 ５１ｂ：着磁摩擦車装置 ５１ｃ：着磁摩擦車装置 ５１ｄ：着磁摩擦車装置 ５２：水冷外壁単位 ５３：鍔 ５４：水冷内壁 ５５：冷却手段 ５６：水噴射手段 ５６ａ：水噴射手段 ５７：毛細管放出手段 ５８：排気熱交換器 ５９：過熱蒸気筒口 ５９ａ：高温水噴射ノズル ５９ｂ：高温水噴射ノズル（超臨界温度等複数温度の高温水を霧吹きの原理等適宜に混合して噴射） ６０：燃料噴口 ６１：針弁 ６２：燃料小穴 ６３：燃料穴開閉器 ６４：空気穴開閉器 ６５：空気穴 ６６：凝縮水熱交換器 ６６ａ：気化潜熱回収器 ６６ｂ：空冷式気化潜熱回収器 ６７：復水器 ６８：凝縮水 ６９：排気 ７０：水道水 ７１：温熱 ７２：冷熱 ７３：冷却水 ７４：推力 ８０：ヨーク ８１：電磁加熱タービン動翼 ８３：電磁加熱噴口 ８４：環状に一体鋳造 ８５：外径組立環状部 ８６：内径組立環状部 ８７：撥水性水冷却翼 ８７ａ：撥水性タービン動翼 ８８：燃焼ガス取出口 ８９：内磁着摩擦車装置 ９０：磁着摩擦車装置 ９１ａ：霧吹きの原理（高温水噴射で空気を吸引噴射） ９１ｂ：霧吹きの原理（燃焼ガス噴射で空気を吸引噴射） ９１ｃ：霧吹きの原理（高温水噴射で水を吸引噴射） ９１ｄ：霧吹きの原理（燃焼ガス多段噴射で水を吸引噴射） ９１ｅ：霧吹きの原理（複数温度高温水噴射で空気を吸引噴射） ９１ｆ：霧吹きの原理（複数温度高温水噴射で水を吸引噴射） ９２ａ：特殊装置（高温水噴射で空気を吸引噴射） ９２ｂ：特殊装置（燃焼ガス噴射で空気吸引噴射）９２ｅ：特殊装置（複数温度高温水噴射で空気を吸引噴射） ９３ａ：水噴射装置（高温水複数段噴射で水を吸引噴射） ９３ｂ：水噴射装置（燃焼ガス噴射で水を吸引噴射） ９３ｄ：水噴射装置（燃焼ガス複数段噴射で水を吸引噴射） ９３ｆ：水噴射装置（複数温度高温水複数段噴射で水を吸引噴射）９４：外箱 ９５：吸水路 ９６：送水路 ９７：送水ポンプ ９８：コイル ９９：磁力線 １００：磁気摩擦動力伝達装置 １００ａ：送水ポンプ兼磁気摩擦動力伝達装置 １０１：加熱高温手段 １０２：冷熱回収器 １０３：全動翼送風機[0001]
BACKGROUND OF THE INVENTION
In the present invention, in order to explain clearly why the existing internal combustion engine technology competes with fuel cells and wind power generation by volume utilization that hardly uses heat, the idea is explained with hypothetical numbers, but the correct answer is an experimental value, It is not limited to idea hypothesis numbers. For example, the state-of-the-art reheat steam turbine uses a volume that does not use heat at all, so it expands more than 10,000 times in the adiabatic expansion vacuum part, reduces the gravitational power to 1 / 10,000 or less of water, and 10000 times at the same output Therefore, even if the head is increased to a supercritical pressure or the like, the speed cannot be used. / 2 is also provided, and the seawater temperature is increased by the total amount of heat heated by the boiler, reducing hypothetical power generation to 1/500. Therefore, by using high-temperature water and vaporization explosive force, heat recovery, reuse, and reuse, the supply heat quantity is brought close to the minimum vaporization heat, and the heat of all supply heat quantity such as compressed air heat quantity is supplied to customers as a by-product, It relates to technology that prevents global warming by supplying enormous amounts of cold heat as a by-product.
[0002]
The reheat is reversed, and the full-blade steam gas turbine combined engine (explained in the abbreviated combined engine) combustor / heat exchanger 4 is used to minimize the high-pressure combustion heat exchange combustion gas temperature and recover the heat. High-temperature water recovery heat quantity such as critical pressure temperature is set to about twice the maximum recovery heat quantity of existing boilers, is heated to high temperature by the heating high-temperature means 101, and high-temperature water 5b having multiple temperatures such as supercritical temperature using the spraying principle 91e. A high temperature water injection nozzle 59b is used to provide a vaporization film between high temperature water such as supercritical temperature and the like, and to inject high temperature water such as supercritical temperature with minimum friction loss, and vaporization explosion energy By accelerating the hot water inside the nozzle like a bullet of a machine gun, accelerating the hot water like a snowstorm by using the vaporization explosion volume velocity, etc., and hot water outside the nozzle like a shot rocket or snowstorm Accelerate the latent heat of vaporization And suitable use by utilizing the heat recovery re retrocession, to a technique for the heat consumption in the maximum to minimize the gravity work rate.
[0003]
Atmospheric pressure gravitational power is 1700 times higher than that of the most advanced reheat steam turbine, and the gravitational power (hereinafter referred to as unit volume mass x speed is the same) is approached 1700 times and used from supercritical pressure to atmospheric pressure. By recovering the heat of vaporization and re-reusing the condensed water at a saturation temperature of 100 ° C, the amount of recovered heat and the amount of heat supplied are brought to the minimum of the heat of vaporization, and the entire amount of recovered heat is supplied to the customer as heat, and the same amount of fuel already exists. It increases to 500 times hypothetical power generation etc. of gas turbine. Part or most of the rotor blade area is reduced to 1/1700 of the existing reheat steam turbine, allowing the design of a rational rotor blade area by taking into account the gravitational power, and hot water is made to meander in a straight line , The mechanical efficiency is increased by 10 to 20 times and the output is generated, and the entire moving blade steam turbine or all moving blade steam gas turbine is used. The present invention relates to a technology aiming at 1/10 of the electricity bill.
[0004]
Reversing the adiabatic expansion and reheating up to the condenser vacuum of the reheat steam turbine, the drop from the supercritical pressure to the atmospheric pressure is sufficient, and the whole blade steam turbine provided with the vaporization latent heat recovery unit 66a is 100 ° C. or less. All the heat of vaporization is supplied to the customer as the heat of recovered heat, and all the condensed water is repeatedly re-supplied to the combustor / heat exchanger 4 to obtain high-temperature water 5b having multiple temperatures such as supercritical temperature, and fuel combustion. The supply of heat is made close to the heat of vaporization, and the gravitational power of unit heat is increased to the limit. An all-blade steam turbine capable of reducing fuel combustion heat and recirculating condensate water, and storing the enormous amount of heat from the added fuel combustion heat as by-product tap water. It is related to a technology that eliminates the supply of heat to customers and the rise of seawater temperature with the total amount of heat used by existing technology.
[0005]
The existing state-of-the-art gas turbine also uses volume, so it is impossible to increase the head due to the turbine heat limit temperature. Furthermore, about 10 to 20 times as much as the moving blades, speed energy is consumed, and 1/2 of the stationary blades that do not perform rotation work are provided, and high-temperature exhaust is performed at about 500 ° C. for adiabatic expansion, reducing the power generation amount to 1/500 or the like. And accelerating global warming. Therefore, the combined engine combustor and heat exchanger 4 performs unlimited high-pressure combustion heat exchange cooling combustion, increases the heat recovery amount to about twice that of the existing boiler, minimizes the combustion gas turbine inlet temperature, and reduces the combustion gas temperature. In addition, the present invention relates to a technology that minimizes the volume hindrance and effectively uses the heat amount and mass of the combustion gas to make the same fuel amount 500 times the hypothetical power generation amount of the existing gas turbine.
[0006]
In the case of normal fuel use, the drop in the combustion gas temperature and volume is minimized to a minimum of 2 times or more, and the entire rotor blade gas turbine of the combined engine is injected in a substantially linear meandering to increase the mechanical efficiency by 10 to 20 times. In the process of generating exhaust gas, the combustion gas exhaust temperature is brought close to −273 ° C. (including the entire −temperature), and the tap water is cooled by the low-temperature combustion gas in the cold heat recovery unit 102 to recover the combustion gas. It expands to a water tank vacuum (including all pressures), converts all of the combustion gas used at a manufacturing cost of nearly 0 to a huge amount of by-product cold and hot tap water, and supplies it to customers. Depending on the application, the compressed air pressure of the combustor and heat exchanger 4 can be raised to the limit by all the moving blades, enabling production and recovery of dry ice, liquid nitrogen, etc. The present invention relates to a technology that increases 20 to 40 times or more.
[0007]
Therefore, in order to reverse the state-of-the-art gas turbine and minimize the combustion gas turbine inlet temperature, the gas turbine combustor is the full blade gas turbine combustor / heat exchanger 4 and the high pressure compression heat exchange is unlimited with all the blades. By cooling and combusting, the heat recovery amount is about twice that of the existing boiler, the combustion gas turbine inlet temperature is minimized, the exhaust temperature is brought close to -273 ° C, and almost all of the retained heat amount of compressed air is included. , Combustion gas calorific power output is about twice the amount of recovered heat of existing boilers. The combustion gas calorie output is used for various applications as high-temperature water 5b having a plurality of temperatures such as supercritical temperature, and the combustion gas calorific power generation amount or output (5 times drop of existing gas turbine × 2 times calorie × 50 times mass gravity work) (Rate x 10 to 20 times mechanical efficiency x 1/20 reduction rate) = (250 to 500 times that of the existing gas turbine, hypothetical power generation or output of combustion gas).
[0008]
In the case of pulverized coal fuel combustion, in order to maximize the amount of power generation and the recovery of cold heat, the minimum optimum amount of high-temperature water 5b such as supercritical temperature is supplied to the uppermost stream of all blade steam gas turbines, and heating high temperature means The high-temperature water 5b is jetted using the spraying principle 91e from the high-temperature water jet nozzle 59b, which is heated to a high temperature by 101 and provided with a vaporized film between the high-temperature water and the friction loss is minimized, Due to the vaporization explosion volume velocity, inside the nozzle and outside the nozzle, hot water is accelerated like machine gun bullets, shot rockets, snowstorms, etc., driving all blade steam gas turbines, and low-temperature combustion gas at the middle stage optimum stage Supplying all of them, agglomerating the water using the low-temperature combustion gas ash that is adiabatically expanded in the process of generating power, allowing it to expand to the condenser vacuum, and using the optimal minimum amount of high-temperature water to recover the amount of cold and generate electricity Maximize the amount, CO2 etc. An exhaust to prevent global warming as 0 like, to convert the whole combustion gas in the vast thermal technology relating supplied to customers in manufacturing cost substantially zero.
[0009]
In the process of driving all blade steam turbines with reheat steam turbines reversed, the recovered heat quantity about twice that of existing boilers is supplied with high-temperature water at multiple temperatures such as supercritical temperature. High-temperature water 5b is supplied from the water control valve 7a to the respective high-temperature water reservoirs 32a via the high-temperature water pipe 6a, and is vaporized between the high-temperature water from the high-temperature water injection nozzle 59b heated to high temperature by the heating high-temperature means 101. A film is provided to minimize friction loss and spray using the spraying principle 91e, and high-temperature water is accelerated in the nozzle like a bullet of a machine gun or a blizzard by the vaporization explosion energy or vaporization volume velocity. Outside, the hot water 5b is accelerated like a shot rocket or a snowstorm, and the high-temperature water injection mass with the gravitational power of 1700 times the gravitational power of the atmospheric pressure part of the state-of-the-art reheat steam turbine is 50% of that of the existing gas turbine. Double On the art.
[0010]
In a full-blade steam gas turbine, high-temperature water 5b having a plurality of temperatures such as supercritical temperatures is injected into the uppermost stream of the combined engine by using a spraying principle 91e, and high-temperature water is injected from a high-temperature water injection nozzle 59b. In the process, injection is performed in a substantially linear meander by all the moving blades, the mechanical efficiency is increased by 10 to 20 times, and the combustion gas mass with a fuel calorie of 0 or less is supplied to the optimum middle flow stage, and the combustion of all the moving blade gas turbines Gas mass output = (double drop of existing gas turbine × 1 times mass × 10-20 times mechanical efficiency) = (20-40 times combustion gas mass hypothesis output of existing gas turbine), combined engine output = (combustion gas mass) This is related to a technique of increasing output + combustion gas calorie output) = (20 to 40 times output of existing gas turbine + 250 to 500 times output) = (270 to 540 times hypothesis output of existing gas turbine).
[0011]
Convert almost all of the supplied heat into vaporization explosion energy of high temperature water 5b, increase the gravitational power of high temperature water to 50 times the mass of existing gas turbine combustion gas, etc., and generate output with high temperature water 5b at the optimum speed The In the process of generating the calorific value of the combustion gas, a vaporized film is provided between the high-temperature water and friction as a high-temperature water injection nozzle 59b, an electromagnetically heated turbine rotor blade 81, etc. Minimizing loss and jetting almost linearly meandering to increase machine efficiency 10 to 20 times. And the double recovery heat amount of the existing boiler (same fuel amount high temperature water heat mass output) = (50 times mass gravity power x 5 times drop x 2 times recovery heat x 10-20 times machine efficiency x 1/20 reduction rate) = (Related to the technology of rising to 250 to 500 times the combustion gas calorific value hypothesis output of the existing gas turbine).
[0012]
In order to make all the turbine blades have high electromagnetic induction heating temperature, the coil 98 is provided and energized in the same manner as the electromagnetic cooker, and the magnetic field lines 99 are collected in the material containing iron having a large relative permeability, and the eddy current is applied. Joule heat is generated by electrical resistance, and various high-temperature electromagnetically heated turbine blades 81 are constructed. A vaporization film is provided between the electromagnetically heated turbine rotor blade 81 and the high-temperature water, and the entire rotor blade is injected in a substantially linear meandering manner to generate an output up to atmospheric pressure with a minimum friction loss and a maximum gravitational power. The combustion gas heat output + mass output of the combined moving-blade steam gas turbine combined engine (for example, for rotary output transportation equipment) with a structure and volume of 1/10, etc. (250 to 500 times output + 20 to 40 times output) = (270 to 540 times hypothesis output of existing gas turbine).
[0013]
All the rotor blade gas turbine compressor blades are made into a water-repellent water cooling blade 87 composed of one or more of water-repellent metal, water-repellent substance coating, water-repellent ceramics, and water-repellent finish, The compressor blades are used to compress air in the most efficient manner in a substantially linear meandering manner to cool the air, compress the air with the minimum friction loss, and inject the cooled water directly into the compressor blades. In the process of cooling the compressed air, heat is recovered by reducing friction loss between the water-repellent water cooling blade 87 and water, etc., and the compressed air pressure is raised to the limit by all the moving blades to generate output and dry. The present invention relates to the technology of various coalescence engines that can manufacture ice, liquid nitrogen, and the like and supply cold air to the combustor and heat exchanger 4 most efficiently.
[0014]
Excessive high-pressure combustion heat exchange is performed by the combustor and heat exchanger 4 of various coalescence engines, and all the heat generated from the fuel, including the amount of heat stored in the compressed air, plus the amount of heat stored in the compressed air is recovered. Various coalescence engines are driven as high-temperature water 5b with multiple temperatures such as supercritical temperature. And since there is no high-temperature water at the time of start-up, only at start-up (combustion gas mass x double drop x 10 to 20 times mechanical efficiency) = (the same combustion gas mass as the existing gas turbine 20 to 40 times hypothesis output) Driven as a rotor blade gas turbine, the heat consumption of fuel is reduced to 0 or less, and the thermal efficiency is increased infinitely. In addition, the present invention relates to a technology for increasing the temperature of high-temperature water in the process of generating power and expanding it to atmospheric pressure or condenser vacuum, and shifting to various all-blade steam gas turbine combined engines.
[0015]
High-temperature water 5b at multiple temperatures, such as the combustion gas mass output at the lowest temperature + the supercritical temperature of the recovered heat quantity about twice that of the existing boiler, obtained by endlessly high-pressure combustion heat exchange with the combustor / heat exchanger 4 of the combined engine Use each output up to atmospheric pressure (same mass double drop as existing gas turbine x 10 to 20 times mechanical efficiency + 250 to 500 times output) = (270 to 540 times hypothetical output of existing gas turbine). The heat of vaporization at an exhaust saturation temperature of 100 ° C. is recovered by the vaporization latent heat recovery unit 66a and used as the feed water 3 for the combustor and heat exchanger 4, while the combustion gas such as CO2 is dissolved in 50 times the mass of condensed water. The present invention relates to a technique for a rotational output drive device such as an automobile, which can be recovered by collecting fertilizer and the like by collecting a large amount of nitrogen, CO2, and the like, and is driven by a combined engine used as a rotational output up to atmospheric pressure.
[0016]
The output of the rotary output transportation equipment such as an automobile is generated by using all the high-temperature water steam gas turbine combined engines of all the high-temperature water 5b having a plurality of temperatures such as the supercritical temperature via the high-temperature water pipes 6a from the plurality of high-temperature water control valves 7a. The hot water 5b having a plurality of temperatures is supplied from each of the high temperature water jet nozzles 59b and supplied to each of the spraying principles 91e from the plurality of high temperature water reservoirs 32a. Then, in the process of injection, the vaporizing film is provided between the nozzle and the high-temperature water to minimize the friction loss from the spraying principle 91e, which is composed of the high-temperature water 5b having the highest temperature as the core and the high-temperature water 5b having the highest temperature. Further, the present invention relates to a technique for accelerating high-temperature water in a nozzle like a bullet of a machine gun or a snowstorm by using a vaporization explosion energy, a vaporization explosion volume velocity, or the like to use vaporization explosion energy most efficiently.
[0017]
Outside the nozzle, high temperature water is accelerated like a shot rocket, snowstorm, etc., and an electromagnetically heated high temperature turbine blade 81 is used to provide a vaporized film between the high temperature water 5b and the rotor blade, resulting in friction loss. Accelerates jets in a minimum and substantially linear meander to drive all blades with high-temperature water, increasing mechanical efficiency by 10 to 20 times. The mass of the low temperature combustion gas is supplied to the optimum middle stage, the output is generated while cooling the combustion gas with the high temperature water, the combustion gas exhaust temperature is brought close to −273 ° C. in the process of the output adiabatic expansion, and the saturation temperature is 100 ° C. Heat is recovered from the water vapor by the feed water 3 of the vaporization latent heat recovery unit 66a, and the water vapor is cooled by the feed water 3 and the low-temperature combustion gas to form condensed water. It is related with the technique which melt | dissolves and drains, and makes combustion gas exhaust gas, such as CO2, approach 0.
[0018]
For rotary output transportation equipment, etc., condensate for dissolving low-temperature combustion gas is maximized and combustion gas exhaust such as CO2 is set to 0, so that all output is combined engine rotation output, and 270 to 540 times hypothetical output of existing gas turbine will do. Depending on the application, chemical substances etc. are mixed in the water for high temperature water injection, combustion gas such as CO2 can be easily synthesized and dissolved, pollution gas exhaust such as CO2 from transportation equipment etc. is made harmless, and the combustion gas exhaust temperature is -273 ° C In the process where the saturated water vapor is cooled by the feed water 3 of the vaporization latent heat recovery unit 66a and the combustion gas such as low-temperature CO2 and dissolved in condensed water of 50 times mass or the like, and the exhaust gas of CO2 or the like is exhausted to zero, The all-blade steam gas turbine combined engine includes a water pump / magnetic friction power transmission device 100a and a water reversing pump / counter-reversal magnetic friction power transmission device 14a that increase the pressure in multiple stages and supply a small amount of water while transmitting. Related to the core technology.
[0019]
For transportation equipment that generates injection propulsion output, the combustion gas exhaust such as CO2 is set to 0 and the hypothetical output is 270 to 540 times. Therefore, high-pressure combustion heat exchange is performed by the combustor / heat exchanger 4 as much as possible. A part of high temperature water 5b with multiple temperatures such as supercritical temperature that recovers heat is used to drive all blade turbines including all blade compressors depending on the application. Most of the remaining high-temperature water 5b and all combustion gas are propelled by bypass injection using the respective spraying principles 91e and 91b, and the remaining high-temperature water is appropriately stored in the combustor / heat exchanger 4 or the like. It is optimally used and used as a supersonic airplane such as a 10x speed that is safe in the event of a fire or emergency. In the exhaust process, the water vapor volume is cooled and aggregated to 1/1700 by low-temperature combustion gas, and the exhaust noise is reduced to 1/10, etc. The present invention relates to an all-blade steam gas turbine combined engine technology for various transportation equipment.
[0020]
In a ship that bypasses and propells the entire combustion gas 10 and most of the high-temperature water 5b, the injection propulsion speed increases to 10 times the speed of 500 km, etc. by increasing to 270 to 540 times the hypothetical output of the existing gas turbine. The In the process of injection propulsion, the seawater is directly cooled by adiabatic expansion low-temperature combustion gas, and all the combustion gas such as CO2 is supplied to the seabed. We supply a small amount of nitrogen, oxygen and CO2 to activate the sea area and increase food production such as microorganisms, algae and seafood. And various power generation facilities, heat / electricity / cold heat supply facilities, heat / electricity power supply facilities, various general-purpose engines, various vehicles, various machines, various aircraft, various flights, which use rotational output and jet propulsion output The present invention relates to a technology that makes it possible to deal with various uses such as objects, various ships, various flying ships, and various flying vehicles.
[0021]
[Prior art]
Although the existing gas turbines generated an accidental output, they were improved, and because they use a volume that does not use the heat of basic research at all, they are constrained by the heat-resistant limit temperature of the turbine, and there is no increase in the combustion gas drop x mass = gravity power. In addition to being possible or difficult, without using heat, adiabatic expansion around 500 ° C without using heat, drastically reducing the gravitational power of unit volume and exhausting at high temperature, adiabatic expansion and heat recovery after exhausting where heat recovery is difficult It's an unreasonable design. Furthermore, about 1/2 to 20 times that of the moving blades, speed energy is consumed, and 1/2 of the stationary blades that do not perform any rotation work are provided, so that the total heat output is reduced to 1/270 or 1/540. It approaches the output of the fuel cell and is a large loss.
[0022]
Although the existing steam turbine also generated an accidental power, it was improved and the supercritical pressure superheated steam was reheated again and again in order to utilize the volume without any basic research, and the condenser vacuum adiabatically expanded more than 10,000 times. The unit gravity power is reduced to 1/10000, and the rotor area is 10,000 times the same output. Too much steam speed is not available at all, so speed energy is consumed 10 to 20 times that of the moving blade, half the stationary blade that does not do any rotation work is provided, the steam speed is dammed and decelerated, etc. It ’s too bad. Since a rational design is impossible in a cycle using only the steam volume, the design is unreasonable, and the total heat output is reduced to 1/250 or 1/500. Although there is a huge demand for heat, the total amount of heat heated by the boiler raises the seawater temperature, etc., causing a large loss and exhausting CO2 etc. from the boiler to accelerate global warming. We are.
[0023]
As prior applications, Japanese Patent Application No. 2000-024552, Japanese Patent Application No. 2000-032539, Japanese Patent Application No. 2000-043706, Japanese Patent Application No. 2000-058079, Japanese Patent Application No. 2000-107446, which also used a gas turbine combustor as a heat exchanger. Japanese Patent Application No. 2000-392401, Japanese Patent Application No. 2001-011399, Japanese Patent Application No. 2001-015234, Japanese Patent Application No. 2001-020963, Japanese Patent Application No. 2001-171128, Japanese Patent Application No. 2001-31338, Japanese Patent Application No. 2001-336139, There are Japanese Patent Application Nos. 2002-12572, 2002-118933, 2002-142270, 2002-349544, and 2003-3125.
[0024]
The priority application based on the above-mentioned application generally includes all rotor blades and / or all the plurality of combustors of the gas turbine also serve as heat exchangers, and performs high-pressure combustion heat exchange as much as possible. The exhaust gas temperature is brought close to -273 ° C by approaching the combustion gas inlet temperature to the minimum, and the combustion gas calorific value and the combustion gas mass can be used separately. The water mass with 1700 times the atmospheric pressure gravitational power is set to the optimum maximum, and for power generation, the supply heat amount is brought close to the vaporization energy of vaporization heat only, the gravitational work rate is maximized, and almost all supply heat amount is demanded at 100 ° C or less. By supplying it to the house, water vapor is cooled and aggregated with tap water and low-temperature combustion gas, and CO2 and other combustion gas exhausts are set to 〇 etc. to prevent global warming and aim to minimize waste according to the application.
[0025]
[Problems to be solved by the invention]
The existing state-of-the-art reheat steam turbine uses a volume that does not use heat at all, so it is reheated repeatedly to increase the volume. In the final stage condenser vacuum, the steam volume increases more than 10,000 times, and the gravitational power is reduced to 1/10000. Therefore, the same output cannot be obtained with the same head unless the rotor blade area is increased 10,000 times. In other words, because of the blade area and large steam velocity that cannot be rationally designed, it consumes speed energy 10 to 20 times that of the blade, and provides a huge amount of stationary blades that do not perform rotational work. This is a design that is too unreasonable because it reverses the wind direction, reverses the wind direction, and decelerates to a practical superheated steam speed. Therefore, the purpose is to provide all-blade steam gas turbine combined engines such as all-blade steam turbine and all-blade steam gas turbine that can be rationally designed.
[0026]
What is more problematic is that there is a huge demand for heat and cold, but the heat generated and recovered in the boiler is not used at all. By exhausting from the boiler, the global warming is accelerated and the power generation is reduced to 1/270 ~ 1/540. Therefore, almost all of the supplied heat is supplied to the customer as hot heat of 100 ° C. or less, the seawater temperature does not rise at all, and the exhaust gas exhaust temperature such as CO 2 is brought close to −273 ° C. Supply to home, set CO2 and other exhaust to 0, increase combustion gas calorific power generation amount + combustion gas mass power generation amount to 270-540 times hypothetical power generation amount, reduce electricity bill to 1/10 etc., The purpose is to prevent global warming.
[0027]
Therefore, the existing gas turbine combustor is used as the combined engine combustor / heat exchanger 4 and the high-pressure combustion heat exchange cooling combustion is performed as much as possible, the combustion gas turbine inlet temperature is minimized, the combustion gas exhaust temperature is brought close to −273 ° C., and the heat The combustion gas calorie output obtained by replacing the maximum heat recovery heat energy such as supercritical pressure is about twice that of the existing boiler, and due to the high temperature water vapor explosion energy of multiple temperatures such as supercritical temperature, the machine gun in the nozzle Accelerate hot water like a bullet or snowstorm, and accelerate hot water like a shot rocket or snowstorm outside the nozzle to increase the gravitational power per unit of atmospheric pressure 1000 times the combustion gas and output And the combustion gas calorific power output (5 times drop of existing gas turbine × 2 times calorific value × 50 times gravitational power × 10-20 times mechanical efficiency × 1/20 reduction rate) = (250-500 of existing gas turbine) Double hypothesis Two aims to increase the amount or output).
[0028]
Depending on the application, water is jetted in the process of generating power to cool the water vapor, the volume is reduced to increase the gravitational power, and the output of vaporization is reduced. In the process of exhaust, the vaporization latent heat recovery unit 66a is used as a condenser. Provided in substantially the same manner, the saturation temperature is adjusted according to the application by the air extractor, and the cooling water is also supplied with the water supply 3 or tap water 70 according to the application. Usually, the tap water 70 or the supply water 3 is set at a saturation temperature of 100 ° C. or less. Vaporized heat is recovered, hot tap water is stored, feed water 3 is made up, and condensate is repeatedly re-supplied to the combustor / heat exchanger 4 to repeatedly use the same amount of heat. The purpose is to supply customers with a huge amount of stored heat, with almost no manufacturing cost, to expand the effective use of heat generated by-products as much as possible, and to eliminate the rise in seawater temperature as much as possible. .
[0029]
The same amount of heat is repeatedly recovered by the vaporization latent heat recovery unit 66a, the condensed water is supplied to the combustor / heat exchanger 4, and the fuel combustion heat amount is brought close to the heat of vaporization to greatly reduce the heat recovery. A plurality of high-temperature water 5b having a plurality of temperatures such as critical temperatures is supplied to a plurality of high-temperature water reservoirs 32a in the uppermost stream of the whole rotor blade steam turbine, and a plurality of high-temperature water injection nozzles 59b heated to a high temperature by the heating high-temperature means 101 A vaporization film is provided between the water 5b and the friction loss is minimized, and the high temperature water such as a bullet of a machine gun or a snowstorm is used in the nozzle by utilizing the vaporization explosive force and volume velocity of the high temperature water 5b such as supercritical temperature. Electromagnetically heated turbine blades 81 and high-temperature water are generated by accelerating high-temperature water outside the nozzle, generating high-pressure water and accelerating high-temperature water like a shot rocket and blowing snow, and generating a head and gravity power close to the maximum. A vaporization film is provided between the The total rotor blade as loss minimum by substantially linear serpentine manner injection, it aims to increase mechanical efficiency of 10 to 20 times.
[0030]
When maximizing the amount of power generation and the supply of cold heat, pulverized coal combustion and high-temperature water 5b output are used, and part or most of the blade area in the final stage condenser vacuum is reduced to 1/10000 by increasing the gravitational power. It will be possible to design a rational blade area, and the combustion gas exhaust temperature will approach -273 ° C. Then, the optimum minimum amount of high-temperature water 5b is supplied to the uppermost stream of the all-blade steam gas turbine equipped with the electromagnetically heated high-temperature electromagnetically heated turbine rotor blade 81. Low temperature obtained by injecting high-temperature water 5b, providing a vaporized film between the electromagnetically heated turbine blade 81 and the high-temperature water 5b, generating an output with a minimum friction loss, and exchanging heat in the middle-stream optimum stage Combustion gas mass is supplied, and combustion gas mass power generation amount is (double drop of existing gas turbine x double mass of ash, etc. x 10 to 20 times mechanical efficiency) = (40 to 80 times hypothetical power generation of existing gas turbine) The purpose is to supply the consumer with the maximum amount of cooling energy for all combustion gases.
[0031]
The existing state-of-the-art gas turbine also uses a volume that does not use heat at all, so the rise of the turbine heat limit temperature makes it impossible to increase the head, and the exhaust temperature is very high at around 500 ° C. It is an unreasonable design that consumes 20 times the speed energy and does not work, and reduces the speed to a practical combustion gas speed by providing half the vanes. Therefore, in order to maximize the amount of cold recovery, the normal fuel all-blade gas turbine combustor / heat exchanger 4 is used, and all the blades perform high-pressure combustion heat exchange cooling combustion to the limit, and the combustion gas mass output is 20 to 40. Double hypothesis output, the combustion gas exhaust temperature is brought close to -273 ° C, and the cold heat recovery device 102 enables the production of dry ice and liquid nitrogen from all the cryogenic combustion gas, or the maximum amount of cold hot water for customers. The purpose is to increase the discharge side of all blade rotor 103 and move the combustion gas such as CO2 into the water and bring the exhaust such as CO2 close to 0 or 0.
[0032]
Combustion gas heat output obtained by exchanging heat with the combustor / heat exchanger 4 includes the heat recovery amount about twice that of the existing boiler, including almost all of the compressed air holding heat amount of −273 ° C., supercritical temperature, etc. The heat recovery amount of high-temperature water 5b at a plurality of temperatures, including the combustion gas mass output obtained through heat exchange, drives the full blade turbine, the full blade gas turbine, or the full blade steam gas turbine. Using the principles 91b, 91d, 91e, and 91f, the special equipment 92b and 92e through the water injection devices 93d and 93f are driven, and the power generation equipment and transportation equipment that generate 270 to 540 times the hypothetical power generation or output of the existing gas turbine. To prevent global warming.
[0033]
[Means for Solving the Problems]
Although the experimental values are correct, all hypothetical numbers are used to explain the ideas in the previous stage clearly, but the hypothetical numbers are not limited. In the case of volume utilization that reheats and does not use the amount of heat at all, such as existing state-of-the-art reheat steam turbines, the steam velocity is too large from the supercritical pressure to the vacuum part, making it difficult or impossible to use effectively, as well as the volume of steam. 10000 times expansion, unit volume gravity power is reduced to 1/10000, and the same head and output are required 10,000 times larger blade area, making rational design impossible, It is too unreasonable, such as blocking the steam speed by 10 to 20 times and not rotating work, and reducing the steam speed to a practical steam speed by installing 1/2 vane. Therefore, we offer all types of all-wing blade combined engines that can be rationally designed.
[0034]
In other words, due to the impossibility of impeller blade area, using a full rotor blade steam turbine with reversed reheat, high temperature water such as supercritical temperature is appropriately mixed and sprayed, such as the principle of spraying, By vaporizing explosion energy, high-temperature water is accelerated to generate output, and for power generation, etc., the amount of heat supplied approaches the vaporized heat and is minimized. Then, a vaporized film is provided between the high temperature water and the high temperature water as the high temperature by the high temperature heating means 101 to form a barrel shape or a divergent barrel shape with a minimum friction loss, and high temperature water having a plurality of temperatures such as a supercritical temperature from the high temperature water injection nozzle 59b. Are sprayed by mixing them as appropriate, such as the principle of spraying, accelerating the hot water inside the nozzle like a machine gun bullet or snowstorm, and accelerating the hot water like a shot rocket or snowstorm outside the nozzle, Combustion gas calorific power output (5 times drop of existing gas turbine x 2 times recovered heat mass x 50 times gravity power x 10 to 20 times mechanical efficiency x 1/20 reduction rate) = (250 to 500 times combustion of existing gas turbine) Gas calorific value hypothetical power generation or output).
[0035]
Atmospheric pressure gravitational power is optimally designed with a maximum hot water mass of 1700 times that of water vapor, and part or most of the blade surface area is reduced to 1/1700 of existing reheat steam turbines. Makes it possible. Utilizing high temperature water drop at multiple temperatures such as supercritical temperature and vaporization explosive force, it is possible to design a rational rotor blade with a small increase in volume, and the gravitational power is 50 times that of all combustion gases. A vaporization film is provided between the high-temperature water and the heated high-temperature electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine blade group 20 to inject substantially linearly and meanderingly with minimal friction loss. To 10-20 times to generate rotational output, the vaporization explosive power of high-temperature water and the vaporization explosion volume reduce the injection speed to a reasonable design, and increase the gravitational power to the limit, Increases combustion gas calorific power output to hypothetical power generation or output 250 to 500 times that of existing gas turbines.
[0036]
Since the existing state-of-the-art gas turbine uses a volume that does not use heat at all, the output is small and the exhaust temperature is as high as around 500 ° C. In order to accelerate global warming by discharging CO2 etc., the total heat is recovered as described above. As a result, the combustion gas heat output is increased 500 times, and the combustion gas mass output is increased 40 times that of the existing gas turbine. Therefore, the existing gas turbine combustor is first used as the combustor / heat exchanger 4 to minimize the combustion gas temperature and volume obstacle, to perform the high-pressure combustion heat exchange cooling combustion as much as possible, to minimize the combustion gas turbine inlet temperature, and the combustion gas Heat recovery as high-temperature water at various temperatures such as supercritical temperature, with the heat recovery amount approaching −273 ° C. The amount is maximized according to the application, and all the low-temperature combustion gas is recovered and used as dry ice or liquid nitrogen according to the application by the cold energy recovery device 102, or converted to tap water cold energy and supplied to customers.
[0037]
In the all-blade gas turbine limited to recovering the cold energy of the power generation equipment, the combustion gas exhaust temperature is brought close to −273 ° C., and the cold heat recovery device 102 is provided in the same manner as the conventional condenser, and the water supply is replaced with the conventional cooling water. Cold water is recovered with water and supplied to customers. For applications that collect dry ice or liquid nitrogen, etc., the compressed air pressure of all rotor blade compressors is increased to use centrifugal force, and dry ice and liquid nitrogen are separated and recovered before the cold heat recovery unit. The compression pressure is set to 2 to 4 times that of the existing gas turbine, such as 10 to 20 MPa, etc., and the fuel combustion mass to the theoretical air-fuel ratio is also almost 4 times that of the existing gas turbine with the same compressed air amount. 2 times drop x 4 times mass x 10-20 times mechanical efficiency) = (80-160 times the hypothetical power generation of existing gas turbines). And the combustion gas mass output is increased to (2 times drop mass of existing gas turbine x 10 to 20 times mechanical efficiency) = (20 to 40 times hypothetical power generation of existing gas turbine).
[0038]
In order to generate an output with minimum friction loss by high temperature water of combustion gas calorific value, a coil 98 is provided on the outer shaft device and the inner shaft device of the all blade steam turbine electromagnetic heating turbine blade 81, and a rotating contact is provided by a known technique. The electromagnetically heated outer turbine rotor blade group 19 and the electromagnetically heated inner turbine rotor blade group 20 including the annular electromagnetic heating nozzle 83 are substantially similar to the electromagnetic induction heating cooker, and the iron-based relative permeability is large. Composed of materials, heated to high temperature by eddy current of magnetic field lines 99, provided with a vaporized film between the electromagnetically heated turbine rotor blade 81 and the high temperature water, the frictional loss is minimized and the maximum gravitational power is maximized, and the optimum high temperature water velocity To generate a reasonable rotational output, substantially linearly meandering with all the moving blades to increase the mechanical efficiency by 10 to 20 times, and increase to 500 times the hypothetical power generation amount or output of the existing gas turbine To do.
[0039]
Fully moving blade steam turbine Electromagnetically heated turbine moving blade 81 injects in a substantially linear meander, optimally utilizes vaporization explosion energy, abolishes existing technology stationary blades, increases mechanical efficiency 10 to 20 times, exhausts In the process, the air extractor of the vaporization latent heat recovery unit 66a provided in substantially the same manner as the condenser is used to set the saturation temperature to 100 ° C. or 80 ° C. or less according to the application, and the cooling water is supplied from the water supply 3 or the tap water 70. Use according to the application, completely abolish the temperature of the existing technology seawater, supply the condensed water recovered by the vaporization latent heat recovery unit 66a to the combustor and heat exchanger 4, and repeat the same amount of heat as much as possible Re-reuse to reduce the fuel combustion mass of the supply heat amount to about the minimum of vaporization heat, and the enormous amount of heat of supply heat amount as a by-product of manufacturing cost about 0 as tap water temperature below 100 ° C Supplied to consumers and electricity charges / You and 10, and the like.
[0040]
When maximizing the power generation amount and the amount of cold recovery and reducing the combustion gas exhaust gas such as CO2 to 0, etc., it is used as an all-blade gas turbine only at the time of start-up. Combustion gas containing ash that is cooled to the most suitable stage in the middle stream by supplying the optimum minimum amount of supercritical pressure high-temperature water to the most upstream stream and injecting in a substantially linear meandering manner by the electromagnetically heated turbine rotor blade 81 In the process of generating power, low-temperature water is jetted depending on the application, the gravity power including ash is increased and optimum deceleration is performed, the vaporized explosion steam and combustion gas are cooled, and the maximum amount of power is supplied. At the same time, by agglomerating all the water with the adiabatic expansion low-temperature combustion gas ash as the core, a coating is provided on the combustion gas such as CO2, and the water-repellent turbine blade 87a or the electromagnetically heated turbine blade 81 is selected for friction. Generates output with minimal loss and cools From low-temperature combustion gas containing moisture collector 102, the cold heat of the maximum amount stored is recovered with tap water, and then supplied to customers as a water cooled heat.
[0041]
Store the maximum amount of cold heat at about 5 ° C with tap water, supply cold water tap water pipes to consumers, and replace existing commercial refrigeration equipment and coolers for cheap de-Freon Providing commercial household refrigeration equipment, refrigeration equipment, and coolers that use cold water from tap water. Sprinkling too much cold water to cool the whole city, etc., and operating expenses for cooling, refrigeration equipment, and refrigeration equipment are 1 Reduces to / 10 etc. In the process of cooling seawater with too much cold water, low-temperature CO2 and nitrogen are dissolved in a large amount of seawater to form cold water, and oxygen, etc. is sucked in to supply an optimal amount to the seabed in a dilute manner. We will try to revitalize the sea area by breeding seaweed and seafood. Or cold water such as CO2 or nitrogen that has cooled tap water, etc., is fixed to raw garbage, mud, or plant pieces to make a huge amount of cheap fertilizer, etc. The rise is also reversed.
[0042]
In the process of air compression, the whole moving blade compressor is composed of a water-repellent water cooling blade 87, and is composed of one or more of water-repellent metal, water-repellent substance coating, water-repellent ceramics and water-repellent finish. The compressor blades are water-cooled blades by compressing the compressed air substantially linearly in a meandering manner to cool the water, and the water is jetted from the water jetting means 56 to directly cool the air, thereby compressing at a low temperature. In the process of turning to air, the friction loss between the water repellent water cooling blade 87 and water is brought to a minimum, compressed air at the lowest temperature is supplied to the combustor / heat exchanger 4, and high-pressure combustion heat exchange is possible. Cooling combustion is performed to reduce the turbine inlet temperature of the combustion gas to the lowest temperature suitable for the application.
[0043]
The combustion gas exhaust temperature is set to −273 ° C. by reducing the turbine inlet temperature of the combustion gas to the minimum by the high pressure combustion heat exchange cooling combustion without limit by the combustor and heat exchanger 4 of the all-blade steam gas turbine combined engine. Close to In the process of generating power, the electromagnetically heated turbine rotor blade 81 or the water-repellent turbine rotor blade 87a is selected in accordance with the application, and hot water 5b and combustion gas are injected in a substantially linear meandering manner by all the rotor blades, resulting in friction loss. Minimal output. Depending on the application, low temperature water is injected by the water injection means 56a, the vaporized explosion steam and combustion gas are cooled, the unit volume is reduced to increase the gravity power, the vaporization explosion steam speed and the combustion gas speed of high temperature water are increased, Converts energy into the gravity power of water mass and decelerates to the optimum speed.
[0044]
Depending on the application, vaporized explosive energy water vapor or combustion gas is cooled by low-temperature water injection, converted into the gravitational power of water, decelerated to the optimum speed, and expanded to 270 to 540 times hypothetical power generation. In the process of making the cooling of the steam by means of a little and bringing the combustion gas exhaust temperature close to -273 ° C, water is condensed with the low temperature combustion gas ash as the core, and the coating of soot and water droplets is provided as in the natural phenomenon until the vacuum Inflate and maximize the cold energy recovered by the cold energy collector 102. A huge amount of fertilizer that dissolves nitrogen and CO2 of combustion gas in a huge amount of water in the process of heat exchange cooling and storing tap water etc. with a huge amount of cold heat recovered as cold heat. , Etc., reducing CO2 and other combustion gas emissions from thermal power plants around the world to 0, etc., and maximizing the collection and use of cold energy to prevent global warming.
[0045]
In order to leave limited fuel resources for the offspring, the power generation is to burn cheap pulverized coal fuel, further increase the total gravitational power by the gravitational power of combustion ash, increase the combustion gas mass power generation, The most reasonable allocation of finite fuel resources is used. Combustion and heat exchanger 4 infinitely high-pressure combustion heat exchange cooling combustion, the process of minimizing the temperature of all rotor blade steam gas turbine combustion gas inlet to the combustion of cheap pulverized coal fuel, combustion gas exhaust temperature- The total moving blade steam turbine output, which is converted to high-temperature water at multiple temperatures such as supercritical temperature, is about 273 ° C, and the recovered heat amount of about twice that of the existing boiler, including almost all of the compressed air retained heat amount of -273 ° C or higher. The combustion gas calorie output including the temporary power generation is 250 to 500 times that of the existing gas turbine.
[0046]
And the same fuel amount combustion gas mass power generation amount (double drop of existing gas turbine × 10 to 20 times mechanical efficiency × double mass including combustion ash) = (40 to 80 times combustion gas mass power generation amount of existing gas turbine) Will increase. In the process of generating power, as described above, the lowest optimum amount of high-temperature water output supplied to the uppermost stream of all blade steam gas turbines is used, and the mass output of combustion gas supplied to the middle-stream optimum stage is low-temperature combustion gas including combustion ash. Integrates low-temperature moisture at the core, enabling vacuum and maximizing the amount of cold recovery and power generation. And (combustion gas mass power generation amount) + (combustion gas calorific power generation amount) = (combustion gas calorific power generation amount 40 to 80 times that of the existing gas turbine) + (250 to 500 times combustion gas calorific power generation amount of the existing gas turbine) = ( It increases to 290 to 580 times the hypothetical power generation) of existing gas turbines.
[0047]
When using the combustion gas calorie output + combustion gas mass output as the rotational output and the combustion gas exhaust as 0, etc., in the automobile of the transportation equipment, etc. , All the high-temperature water having a plurality of temperatures such as supercritical temperature obtained by heat exchange in the combustor / heat exchanger 4 is supplied as a combustion gas calorific value output from each high-temperature water control valve 7a, and heated by the heating high-temperature means 101 Injected from a high-temperature water injection nozzle 59b having a barrel shape or a wide-angle barrel shape, a vaporization film is provided between the nozzle and the high-temperature water, and the vaporization explosive force and the vaporization volume velocity are optimally utilized with minimum friction loss. Inside the nozzle and outside the nozzle, a high-temperature water is accelerated like a bullet of a machine gun, a shot rocket, or a snowstorm, and a vaporized film is provided between the high-temperature water and the electromagnetically heated turbine blade 81 heated to a high temperature, Friction loss minimum gravity power maximum With warm water rate optimal, almost linearly meandering to injection, to increase mechanical efficiency to 10 to 20 times.
[0048]
The atmospheric pressure gravity power is 1700 times that of the existing steam turbine, the mass of the high-temperature water 5b is maximized according to the application, the combustion gas at the lowest temperature is supplied to the optimum middle flow stage, and the combustion gas 10 is cooled with the high-temperature water 5b for a moment. Then, it reverses in the process of generating the output, cools the high-temperature water with the low-temperature combustion gas, recovers the heat with the feed water 3 by the vaporization latent heat recovery unit 66a, and supplies it to the combustor / heat exchanger 4 for use, such as CO2 The combustion gas is dissolved in condensed water of 50 times mass, etc. and drained, the combustion gas exhaust of CO2 etc. is reduced to 0 etc., and the atmospheric pressure gravitational power is set to 1700 times higher than that of the existing technology, A part or most of the turbine rotor blade area will be a reasonable rotor blade area of 1/1700. In other words, by using the recovered heat amount as the vaporization explosive force of high-temperature water, the rotor blade area of the turbine is reduced to 1/100 rotor blade area, etc., enabling rational design and rotation speed, and reducing the structure to 1 / Make it as small and easy as 10 mag.
[0049]
In the case of rotating output transportation equipment such as automobiles, the saturation temperature is limited to around 100 ° C., the vaporization latent heat recovery unit 66a is air-cooled with a large weight, and condensate is resupplied to the combustor / heat exchanger 4 without limitation. If the combustion gas dissolved water is not used because it is normally used, the combustion blade gas turbine is driven by all or part of the combustion gas and used for power generation. A full-blade steam gas turbine that is used for applications or recovered as dry ice or liquid nitrogen. Condensed water is reused to make high-temperature water with multiple temperatures such as supercritical temperature, but the structure becomes simple and the calorific power output of combustion gas is the same fuel amount (50 times mass gravity power of existing gas turbine × 5 times drop × 2 times recovered heat x 10 to 20 times mechanical efficiency x 1/20 reduction rate) = (250 to 500 times hypothesis output), etc., and all blade steam for various transportation equipment with combustion gas mass output set to 0 etc. Used as a gas turbine coalescence engine.
[0050]
In the case of using rotation output + injection propulsion force, the high-temperature water temperature of multiple temperatures such as supercritical temperature for rotation output is close to superheated steam because the exhaust injection speed etc. is also used as propulsion force, and the air that uses the principle of spraying High-temperature water temperature such as supercritical pressure for generating jet propulsion output, which uses suction injection or water suction injection, can approach the superheated steam temperature because a very large speed can be used. Therefore, in order to drive the air compressor of the all-blade steam gas turbine combined engine, the structure using the principle of spraying is very simple except for the part that converts the vaporization explosion energy of high-temperature water into rotational output, Waste heat recovery cancels out the impossibility, and is used as a supersonic passenger aircraft, space return parent airplane, jet propulsion ship, etc. as a combined moving blade steam gas turbine engine with a temporary output of 270-540 times that of an existing gas turbine And increase the speed around 10 times.
[0051]
For example, the full-blade steam turbine combined engine to the full-blade steam gas turbine combined engine shown in FIG. 6 drives a full-blade compressor including the full-blade steam turbine by a normal starting device and sucks forward air. The high pressure combustion heat exchange cooling combustion is performed by the combustor and heat exchanger 4 without limitation, and the full blade steam turbine is used in the full blade gas turbine only at the time of start-up. Supply low temperature combustion gas with mass output of combustion gas obtained by heat exchange to the uppermost stream of all rotor blade steam turbines while storing high temperature water with supercritical pressure etc. of combustion gas calorie output obtained by heat exchange Then, the rotor blade compressor is driven by the rotation output, and the startup preparation operation is continued using the exhaust velocity mass as the jet propulsion force while increasing the high-temperature water temperature such as the supercritical temperature.
[0052]
When the temperature of the high-temperature water such as supercritical temperature obtained by heat exchange in the start-up preparation operation is increased, the low-temperature combustion gas 10 of the combustion gas mass is bypass-injected by the spraying principle 91b by the valve control not shown in the figure, A part of high-temperature water at multiple temperatures, such as the supercritical temperature of the combustion gas calorific value obtained by heat exchange, is used for all blade blade steam. The turbine is supplied to a plurality of hot water pools 32a at the uppermost stream and appropriately mixed by each high temperature water injection nozzle 59b and injected, and the electromagnetic heating turbine rotor blade 81 generates a rotational output with a minimum friction loss. The full-blade air compressor is driven by the rotational output, and the air suction force and exhaust injection speed x mass are used as the injection propulsion force. 10 times faster And press to high-speed flight.
[0053]
That is, by the valve control not shown in the figure by the known technology, all the combustion gas obtained by heat exchange and the remaining high-temperature water are bypass-injected using the respective spraying principles 91b and 91e, far exceeding the adiabatic expansion ramjet. Bypass injection of combustion gas with a large drop, bypass injection of high-temperature water with hypothesis mass etc. around 5 times the drop of the ramjet, sucking forward air and propelling it, air suction force and injection speed × mass The most efficient jet propulsion, including supersonic jet aircraft, space return planes, flying ships and flying objects, including supersonic flight about 10 times that of existing jets, and low-temperature combustion gas in the course of jet propulsion , Reduce the water vapor volume to 1/1700 volume, etc., dilute supply of dissolved water to the sea, etc. to activate the sea area, reduce exhaust noise to 1/10 etc., and make noise pollution almost zero Ma .
[0054]
DETAILED DESCRIPTION OF THE INVENTION
Embodiments and examples of the present invention will be described with reference to the drawings. The same names or reference numerals are given to the same parts as those in the above-described embodiments and examples, and the description will be repeated. Is omitted, and the characteristic part and the lack of explanation will be explained in order. In addition, in order to explain the intention and expectation of the invention specifically and clearly, the ideas are explained with hypothetical figures, but not limited to the figures including the above-mentioned hypothesis magnification.
[0055]
According to the present invention, the combustor / heat exchanger 4 that cools and compresses air most simply and efficiently, recovers heat, and uses it as low-temperature air is selected according to the application as a combustor / heat exchanger that has already been applied for. Use In order to generate the most efficient output with cryogenic combustion gas or high-temperature water 5b, etc., the heated high-temperature electromagnetically heated turbine rotor blade 81 is used. Replace with wing 87a. In addition, the combustion gas exhaust temperature is brought to -273 ° C, and it is assumed to be a cryogenic combustion gas. However, including the above explanation, the approach to -273 ° C is used as a practical minimum temperature, and is around -100 ° C or -20 ° C. Use around the entire temperature, such as around ℃.
[0056]
In the first embodiment of the full blade steam turbine of FIG. 1, all of the recovered heat amount, which is about twice the same fuel amount as that of the existing boiler, obtained by heat exchange by the combustor and heat exchanger 4 of FIG. Most of the high-temperature water 5b having a plurality of temperatures, such as supercritical temperatures, is supplied to the plurality of high-temperature water reservoirs 32a of the entire rotor blade steam turbine by the high-temperature water pipe 6a through the high-temperature water control valve 7a. Is provided through a heat insulating material 48a, heated to a high temperature by a known technique such as direct electrical resistance or electromagnetic heating, and heated to a high temperature by the heating high-temperature means 101. The spray nozzle 59b provides a vaporized film between the high-temperature water 5b, accelerates the high-temperature water 5b with the least amount of heat consumed by the gravitational power, and minimizes friction loss, and uses the large drop volume and vaporization explosion energy. Generates most efficient rotation output You.
[0057]
Therefore, in the high temperature water injection nozzle 59b, high temperature water such as a supercritical temperature is accelerated like a bullet of a machine gun or a snowstorm, and outside the nozzle, the high temperature water 5b is accelerated like a shot rocket or a snowstorm. A vaporized film is provided between the induction-heated high-temperature electromagnetically heated turbine rotor blades 81 and injected in a substantially linear meandering manner with a minimum friction loss to increase the mechanical efficiency 10 to 20 times that of the existing steam turbine. Heat output (5 times drop of existing gas turbine x 2 times recovered heat x 50 times mass gravitational power x 10 to 20 times mechanical efficiency x 1/20 reduction rate) = (250 to 500 times hypothesis output of existing gas turbine) In the process of generating power, water is jetted depending on the application, and the steam 5 is cooled by high-temperature vaporization explosion or volume utilization, the steam volume is reduced to the atmospheric pressure part 1/1700, etc., and the steam speed is increased. The part is the speed of hot water mass And energy conversion in heavy lifting rate decelerates to the optimum speed, rational design and the rotational speed possible, compact simplified structure to 1/10 and the like.
[0058]
The drop should be sufficient from the supercritical pressure to atmospheric pressure, and the atmospheric pressure unit volumetric gravity power is 1700 times higher than the state-of-the-art steam turbine. The critical pressure x 50 times mass, etc., reduced to the maximum gravitational power x optimum speed, and partly or most of the blade area of the electromagnetically heated turbine rotor blade 81 is reduced to 1/1700 to make a rational design Can be reduced, and the maximum output of the unit blade area of the atmospheric pressure section is increased 1700 times. By reducing the blade area of the electromagnetically heated turbine blade 81, greatly increasing the total gravitational power, and decelerating to the optimum speed of the high-temperature water speed, it is possible to rationally design the all blade steam turbine. It increases the possibility of rotation, simplification of the size of 1/10, and hypothesis output of 500 times.
[0059]
By rational design, low-speed, high-output rotation and small, simple, high-output, it is possible to inject substantially linearly meandering as all blades, and the electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine The moving blade group 20 can be integrally cast 84 and fully automatic in the form of a ring for each stage. Then, it is possible to inject water of an appropriate cooling means 55 not shown in the drawing provided by heat insulation to a turbine blade or the like at the time of casting, and to allow the water injection means 56a provided by heat insulation to be cast. The water injection means 56a is provided in the vicinity of the connecting portion of the inner diameter 85 and the inner diameter assembly annular portion 86 to form the electromagnetic heating turbine blade group 19 of the electromagnetic heating outer turbine blade group 19 and the electromagnetic heating inner turbine blade group 20, and substantially straight. Serpentine injection increases mechanical efficiency 10-20 times that of existing steam turbines.
[0060]
Make the blade shape, blade width, and blade angle with the blade spacing widened to match the increase in gravitational power, atmospheric pressure, etc. 1700 times. The electromagnetically heated turbine rotor blade 81 at the time of casting is made of a material whose main component is iron, which allows easy passage of magnetic field lines, and the magnetic field lines are collected and eddy currents are used to raise the temperature to electromagnetic induction heating in a similar manner to an electromagnetic cooker. A coil 98 is provided on the outer shaft device and the inner shaft device, and energization is performed by a rotating contact according to a known technique. Magnetic field lines are collected in the electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine blade group 20 by eddy current. Electromagnetic induction heating is performed by electrical resistance, and a vaporization film is provided between the high-temperature water and the high-temperature water 5b is sprayed in a substantially linear meandering manner to minimize friction loss, and the optimum injection with the highest gravitational power is achieved. Speed increases mechanical efficiency 10-20 times that of existing steam turbines.
[0061]
In the process of exhaust, the air extractor of the vaporization latent heat recovery unit 66a provided in substantially the same manner as the existing condenser enables a saturation temperature of 100 ° C. or less, and heat is recovered with tap water 70 instead of cooling water. Thus, the recovered condensed water of 100 ° C. or the like is repeatedly supplied to the combustor / heat exchanger 4 and reused again to reduce the supply fuel combustion mass to the minimum of the vaporization heat, and to the entire supply fuel combustion heat quantity. As a tap water temperature with a saturation temperature of 100 ° C. or less, heat is recovered and stored by the vaporization latent heat recovery unit 66a, and a large amount of the tap water temperature with almost all of the supply heat is used as a by-product of power generation at a manufacturing cost of almost zero. The demand for electricity will be increased by reducing the seawater temperature of the existing steam turbine due to the total amount of heat used for fuel combustion, and the electricity price will be reduced to 1/10.
[0062]
Various high-temperature water injection nozzles 59b that mix and inject the high-temperature water 5b having a plurality of temperatures such as the supercritical temperature shown in FIG. Like the existing steam turbines, the supercritical temperature has been completely abolished by the unreasonable bitterness that dams up and reduces the steam speed to a practical speed, and the unreasonable bitterness that increases to 1700 times the volume and makes rational design impossible. Among the high temperature water 5b having the same temperature, the hot water 5b having the highest temperature is arranged at the center, and the water is injected by crossing and confluence mixing at about 90 ° with one or more high temperature waters, As one of the high-temperature water injection nozzles 59b that joins and mixes and injects the high-temperature water and the spraying principle, the electromagnetically heated turbine rotor blade 81 is driven by accelerating the high-temperature water 5b most efficiently. Various high temperature water jet nozzles 59b.
[0063]
Therefore, the high temperature water 5b having the highest temperature such as the supercritical temperature is mainly mixed and sprayed by appropriately mixing the high temperature water 5b having a plurality of temperatures according to the spraying principle and the like. In the process of increasing the gravitational power and optimally decelerating with high-temperature water mass at multiple temperatures while ensuring speed, optimally use the high-temperature water vaporization explosive force at multiple temperatures to minimize the amount of generated heat or the maximum output. This is what we aim for. Accordingly, the high-temperature water injection nozzle 59b that passes the high-temperature water 5b having the highest temperature is joined to the high-temperature water injection nozzle 59a that passes the high-temperature water 5b having the highest temperature. The high-temperature water injection nozzle 59b, which mixes and jets appropriately according to the spraying principle, etc., is constructed.
[0064]
In FIG. 2, the barrel-shaped or divergent barrel-shaped part is unknown due to space limitations, but the extension part not shown in the figure is the barrel-shaped or divergent-barreled nozzle part, in which hot water 5b is injected into the machine gun Accelerate like bullets and snowstorms. A vaporized film is provided between the high-temperature water 5b supplied from the high-temperature water pipe 6a via the high-temperature water reservoir 32a as a high temperature by the heating high-temperature means 101 that heats by a known technique such as electric resistance, and the high-temperature water with minimum friction loss. Accelerate A heat insulating material 48a is provided outside the heating and high temperature means 101, and is provided in the uppermost stream of all blade steam turbines or all blade steam gas turbines and the most upstream of the spraying principle 91e / 91f. The turbine, full blade steam gas turbine, special device 92e and water injection device 93f are configured to generate the most efficient rotation output and injection propulsion output.
[0065]
The first embodiment of the full blade gas turbine of FIG. 3 is a coating of a water repellent metal and a water repellent material on the outer compressor blade group 16 and the inner compressor blade group 17 in the main part of the whole blade compressor. A water-repellent water cooling blade 87 or the like composed of one or more of water-repellent ceramics and water-repellent finishes is cooled by passing water by a cooling means 55 (not shown), and the water is jetted from the water jet means 56. Then, the compressed air is directly contact cooled and the air volume is reduced by recovering the heat with water supply 3. By making the entire moving blade composed of the water-repellent water cooling blade 87, the compressed air is efficiently compressed in a substantially linear meandering manner and compressed with a minimum friction loss with water, as an entire moving blade airfoil with an increased blade interval. The water-repellent outer compressor blade group 16 and the inner compressor blade group 17 are made into a single-piece casting 84 in which the compressor blade group for each stage is formed into a ring, enabling fully automatic machining finishing.
[0066]
An assembly structure of an integral casting 84 is formed in an annular shape that can be fully automated, and the water channel of the cooling means 55 is connected at the annular casting assembly connection portion, and the water injection means 56 is provided in the vicinity of the assembly connection portion. After cooling one or more or all or half or half of the water-repellent water cooling blades 87 of the cooling means 55, water is jetted from the water jet means 56 to directly cool the air, and the most efficiently cooled low-temperature air is cooled. , High pressure compression is possible with all rotor blades according to the application. The recovered high-temperature water supply and the low-temperature compressed air are used in the combustor and heat exchanger 4 to recover heat by infinitely high-pressure combustion heat exchange cooling and combustion, reducing the temperature of all blade gas turbine combustion gas inlets to the minimum, and heat recovery Increase the volume to around twice that of the existing boiler, and bring the low-temperature combustion gas exhaust temperature closer to -273 ° C.
[0067]
Combustor and heat exchanger 4 recovers the heat of the high-pressure combustion heat exchange, cooling, and combustion as much as possible, minimizes the obstacles to the temperature and volume of the combustion gas, and sets the compression pressure to 10 MPa or more, which is more than twice that of the existing gas turbine. Combustion gas mass output (combustion gas mass output with the same compressed air amount minimum temperature) with the same compressed air amount combustion up to the theoretical air fuel ratio, approximately four times the combustion of existing gas turbines, and consumption of fuel combustion heat is 0 or less = (Double drop of existing gas turbine x 4 times fuel mass x 10 to 20 times mechanical efficiency) = (The same compressed air amount is 80 to 160 times the hypothetical power generation amount of existing gas turbine) 20-40 times hypothetical power generation).
[0068]
10 masses of the lowest temperature combustion gas obtained by heat exchange is transferred from the uppermost annular combustion gas reservoir 9 of the entire rotor blade gas turbine through the annular receiving port 23 of the outer shaft device. In the combustor and heat exchanger 4 while driving the whole blade compressor, increasing the high temperature water temperature such as supercritical temperature and increasing the storage savings. When the temperature of the high-temperature water 5b rises, each high-temperature water control valve 7a is controlled to open, and the high-temperature water 5b is separately supplied to each of the plurality of high-temperature water reservoirs 32a of the full blade steam turbine of FIG. The vaporizing film is provided between the high-temperature water spray nozzle 59b and the high-temperature water 5b from the high-temperature water spray nozzle 59b which is heated and heated by the high-temperature heating means 101 which is provided and heated to high temperature, and uses the volume with minimum friction loss. Accelerate high-temperature water by vaporization explosion energy and To generate a 500-fold hypothesis amount of power generation and output such as turbines, to reduce the electricity rate to 1/10 or the like.
[0069]
In the process of generating power, the friction loss between the water-repellent turbine blades and the combustion gas is minimized, and it is injected in a substantially linear meandering to increase the mechanical efficiency by 10 to 20 times. Reduce the gas temperature to the optimum speed, or compress as much as possible with the full blade compressor, and in the exhaust process, all the cryogenic combustion gas is centrifuged as dry ice, liquid nitrogen, etc. Separately collected by force and used, or converted to tap water cooling heat of 2 to 5 ° C for heat exchange and supplied to customers. At the same time, we provide commercial and household refrigeration equipment, refrigeration equipment, and air cooling equipment that cools compressed air using dry ice, liquid nitrogen, and tap water cooling heat to prevent global warming due to de-fluorocarbons, and CO2 Combustion gas such as CO2 can be dissolved in water, and CO2 and other combustion gas exhaust is possible.
[0070]
The first embodiment of the all-blade steam gas turbine to all-blade blade gas turbine to all-blade steam gas turbine combined engine of FIG. 4 uses the amount of heat, including the first embodiment. The gas turbine disappears. And since there is no high-temperature water 5a such as supercritical temperature at the time of start-up, it is used as an all-blade gas turbine that generates high-temperature water such as supercritical temperature only by the combustion gas 10 and closes the high-temperature water control valve 7a. Then, the combustion gas is supplied to the optimum intermediate stage of the inner shaft device, is used as a whole blade gas turbine, and is combusted by the combustor and heat exchanger 4 as much as possible with high-pressure combustion heat exchange cooling and combustion gas turbine inlet temperature Prepare the start-up by increasing the temperature of the high-temperature water 5b, which is obtained by heat exchange and made into multiple temperatures such as supercritical temperature.
[0071]
The full blade compressor and the combustor / heat exchanger 4 are provided in the same manner as the full blade gas turbine, and the high pressure combustion heat exchange cooling combustion is performed to recover the heat without limit, and the full blade steam gas turbine combustion gas inlet temperature The heat recovery is increased to about twice that of existing boilers, and the low-temperature combustion gas exhaust temperature approaches -273 ° C. Combustion gas temperature and volume are minimized, the compression pressure is set to 10 MPa or more, which is more than twice that of the existing gas turbine, and the fuel combustion mass is the same as the theoretical air-fuel ratio. Make it possible.
[0072]
There is an urgent need to reduce pollution and prevent global warming.For example, in order to leave finite fuel resources for descendants, well-known garbage gasification fuel, garbage refinement fuel, and all burning things are burned and heat recovery is used. As high-temperature water of multiple temperatures such as supercritical temperature, it is supplied separately to multiple high-temperature water reservoirs 32a via the high-temperature water control valve 7a and converted into electric power. The combustion gas air is also compressed by the full blade compressor, directly cooled to the low temperature air by the water injection means 56, recombusted by the combustor / heat exchanger 4 and reheated for recovery. Combined with use, supplementary use increases heat recovery.
[0073]
For power generation, as a combustion of abundant pulverized coal fuel, all-blade steam gas turbine combustor / heat exchanger 4 performs infinitely high-pressure combustion heat exchange cooling combustion to bring the combustion gas exhaust temperature close to -273 ° C. The latent heat of vaporization is recovered by the water supply 3 by the vaporization latent heat recovery device 66a, supplied to the combustor / heat exchanger 4, and the heat amount of the combustion gas about twice that of the existing boiler obtained by heat exchange, the supercritical temperature, etc. All the high-temperature water 5b having a plurality of temperatures is supplied to the uppermost stream of the all-blade steam gas turbine, the mass of the low-temperature combustion gas is supplied to the optimum stage in the middle stream, and an output is generated. The CO2 and other combustion gas exhaust is dissolved in 50% mass condensate and drained to reduce the CO2 and other combustion gas exhaust to zero.
[0074]
When starting up the full-rotation bladed steam gas turbine combined engine with full-rotation output, it is driven by a known starter including the full-blade compressor, and the combustor / heat exchanger 4 performs unlimited high-pressure combustion heat exchange cooling combustion. The lowest temperature combustion gas 10 is supplied from the annular combustion gas reservoir 9 through the annular passage of the outer shaft device from the inside of the inner shaft device to the middle flow optimum stage to generate an output, and the all blade compressor In the combustor and heat exchanger 4, the temperature of the high temperature water such as supercritical temperature is increased to increase the storage savings, and when the temperature of the high temperature water 5 b rises, each high temperature water control valve 7 a is Opening control is performed, and all the high-temperature water is separately supplied to each of the plurality of high-temperature water reservoirs 32a. Between the spray nozzle 59b and the hot water 5b By providing a vaporized film, high temperature water is accelerated by volume utilization and vaporization explosion energy with minimum friction loss, generating 540 times the hypothetical power generation amount and output of existing gas turbines, reducing electricity bills to 1/10 etc. The
[0075]
In the process of generating power, a vaporization film is provided between the high-temperature water injection nozzle 59b and the high-temperature water 5b. Accelerates like bullets and snowstorms, accelerates hot water 5b like shot rockets and snowstorms outside the nozzle, and provides a vaporized film between the heated high-temperature electromagnetically heated turbine rotor blades 81 and minimizes friction loss. Injected in a substantially linear meandering manner by moving blades, the mechanical efficiency is increased 10 to 20 times that of the existing steam turbine, water is injected depending on the application to cool the vaporized explosion steam, and part or most of the steam speed is Water mass velocity Converts energy into gravity power and reduces to optimum velocity. And before the exhaust, by condensing water with the low temperature combustion gas ash etc. as the core, forming a coating such as water droplets and dissolving it in condensed water of 50 times mass etc., it is possible to exhaust CO2 etc. combustion gas will do.
[0076]
When maximizing the amount of power generation and the recovery of cold heat, it is used as a full blade steam turbine + all blade steam gas turbine, and most of the high-temperature water 5b is used in all blade steam turbines. Water 5b is supplied to the uppermost stream of the all blade steam gas turbine, and the lowest temperature combustion gas 10 is supplied to the middle stage optimum stage, and the combustion gas is first cooled with high temperature water. By reversing and condensing moisture with the whole amount of low-temperature combustion gas ash as a core, all the combustion gas is coated to enable vacuum, and all the combustion gas is brought close to -273 ° C to recover the power generation amount and cold heat Increase the amount to the maximum.
[0077]
Enormous water droplets that are separated and recovered as all the combustion gas as cold heat are stored as cold heat by cooling some or all of the tap water, and as a by-product of electricity that reduces electricity costs to 1/10 etc., the manufacturing cost Supply low-cost tap water cooling to customers, provide refrigerators, coolers, and commercial refrigeration equipment that use low-cost cold heat, and explode sales channels to make existing household and commercial refrigerators In addition, we completely abolished cooling, commercial refrigeration equipment, etc. to prevent global warming by removing chlorofluorocarbons and filling up cold water pipes, sprinkling too much tap water cooling water to cool the whole urban area.
[0078]
Or, cold energy containing a large amount of remaining CO2 and combustion ash, etc., requires plants to contain nitrogen, CO2, etc., and in order to make effective use, it is synthesized and fixed in garbage, plant fragments, mud, etc. To increase food production. The remaining cold heat is the process of cooling the seawater separately and supplying the cold water diluted with CO2 and nitrogen to the seabed, sucking in necessary substances such as oxygen and supplying them into the sea, and thoroughly ecologically marine organisms to microorganisms Research and supply optimal concentration. Propagating seafood and seaweeds, first breeding optimal microorganisms and animals and plants, and then breeding microorganisms, seafood, seaweeds and seaweeds, and increasing food production with combustion gases such as CO2 and nitrogen to prevent global warming To do.
[0079]
And the high temperature combustion heat exchange cooling combustion without limit by the combustor and heat exchanger 4 and the combustion gas mass power generation amount of the lowest temperature obtained by heat exchange (double drop of existing gas turbine x double mass of coal ash etc. × 10 to 20 times the mechanical efficiency) = (40 to 80 times the combustion gas mass power generation amount of the existing gas turbine) to increase the effective use of resources. And (combustion gas mass power generation amount + combustion gas calorific power generation amount) = (40 to 80 times + 250 to 500 times) = (290 to 580 times that of the existing gas turbine) Full moving blade steam gas turbine + All moving blade steam turbine hypothetical power generation amount ) To prevent global warming by increasing power generation with the same amount of fuel.
[0080]
As another form of the first moving blade steam gas turbine combined engine first embodiment that exhausts near atmospheric pressure, various ground transportation equipment such as automobiles that use the full power with rotational force, and various transportation equipment in land, sea, and air, Even if the combustion gas such as CO2 is dissolved and recovered in the condensed water, it is difficult to effectively use it. Therefore, the condensed water is repeatedly re-supplied to the combustor / heat exchanger 4, and the high-pressure combustion heat exchange cooling combustion heat is unlimited. Recovery is required. Therefore, the combustion gas calorific power output about twice that of the existing boiler obtained by heat exchange is supplied to the uppermost stream of all the blade steam turbines of FIGS. The air generated in a substantially linear meandering manner to generate an output and the heat recovered by the air-cooled latent heat recovery unit 66b is used for heating or the like, and the condensed water is repeatedly supplied to the combustor / heat exchanger 4 again. Infinitely, high-pressure combustion heat exchange cooling combustion heat recovery, and 250-500 times the hypothetical output of the existing gas turbine.
[0081]
All the low-temperature combustion gas 10 is supplied from the combustion gas outlet 88 of FIG. 6 to the small and simple high-power all-blade gas turbine of FIG. 3 without a full blade compressor or combustor / heat exchanger to generate output. Depending on the application, low-temperature water injection is performed to cool the combustion gas 10 and the volume is reduced to increase the total gravitational power. Various motor vehicles that can be driven by a motor, can be recovered as dry ice, liquid nitrogen, etc., or can be used for cooling, etc., depending on the application by using a cold heat recovery device 102 with the combustion gas exhaust temperature approaching −273 ° C. It is used as a transport device for preventing global warming.
[0082]
The full-blade steam gas turbine combined engine that generates rotational force with full output has a saturation temperature of exhaust steam 5 at a high temperature of 100 ° C. The output is supplied to the stage, and the steam 5 and the combustion gas are cooled by low-temperature water injection depending on the application, the steam volume and the combustion gas volume are reduced, and the mass of hot water at the lowest temperature is increased. Before exhaust, most of the steam velocity is converted to energy at 1700 times the gravitational power of atmospheric pressure of high-temperature water and optimally decelerated, and the total gravitational power and rotational output are output 270 to 540 times that of the existing gas turbine. And the structure is greatly reduced to 1/10, etc.
[0083]
By greatly increasing the total gravitational power, the area of the electromagnetically heated turbine rotor blade 81 is greatly reduced, and the all rotor blade steam gas turbine combined engine is made small, simple, large output and easy to design, and the steam 5, hot water 5b, combustion gas 10, etc. Is made into an all-blade airfoil that generates power by jetting in a substantially linear meander, and the blade interval, blade shape, and blade angle are also adjusted to the gravitational power increase by expanding the blade spacing. Then, the electromagnetic heating outer turbine blade group 19 and the electromagnetic heating inner turbine blade group 20 are energized with the coils 98 provided to the outer shaft device and the inner shaft device in substantially the same manner as the electromagnetic cooker. A vaporized film is formed between the whole blade electromagnetic heating turbine blade 81 and the high-temperature water 5b, in which the magnetic lines of force are collected in each electromagnetic heating turbine blade 81 and are heated to electromagnetic induction heating by the electric resistance of the eddy current of the magnetic line of force. To minimize friction loss and generate power by almost linearly meandering, increasing mechanical efficiency 10-20 times that of existing steam turbines.
[0084]
The second embodiment of the all-blade steam gas turbine combined engine that sucks and propels the injection shown in FIG. 5 is activated by a normal starter and is driven as an all-blade gas turbine. Infinitely high pressure compressed by the compressor, high pressure combustion heat exchange cooled combustion heat recovery by the combustor and heat exchanger 4, and the low temperature combustion gas 10 of the combustion gas mass is supplied from the inside of the inner shaft device to the optimum middle stage It is used as an all-blade gas turbine that generates output and raises the temperature of multiple high-temperature water such as the supercritical temperature of the combustion gas calorific value. Outer compressor blade group 16 and inner compressor blade group consisting of water-repellent water cooling blades 87 that compress compressed air substantially linearly in a meandering manner as a whole blade shape with increased blade spacing by making all blades. 17 is an integral casting 84 in which the compressor blades of each paragraph are annular. An assembly structure of integral casting 84 is formed in an annular shape capable of fully automatic processing, and the water channel of cooling means 55 is connected at the annular casting assembly connection portion, and water injection means 56 is provided near the assembly annular connection portion.
[0085]
The water-repellent water cooling blades 87 and the like of the outer compressor blade group 16 and the inner compressor blade group 17 of the main part of the whole blade compressor are water-cooled with the water supply 3 by the cooling means 55 (not shown). Injected from the water injection means 56, the compressed air is directly cooled, the volume is reduced as low-temperature compressed air, and the water-cooled low-temperature compressed air is most efficiently cooled. The recovered heat supply water 3 and the low-temperature compressed air are used in the combustor and heat exchanger 4 to recover the high-pressure combustion heat exchange cooling combustion heat as much as possible to reduce the temperature of all the blade steam gas turbine combustion gas to the minimum, and the same fuel The amount of recovered combustion gas calorific value is about twice the heat recovery amount of existing boilers, and the combustion gas calorific value is output as high-temperature water 5b with multiple temperatures such as supercritical temperature. To output.
[0086]
In the combustor and heat exchanger 4, heat recovery is performed by infinitely high-pressure combustion heat exchange cooling, generating a 500 times hypothesis output of the existing gas turbine, and the process of bringing the combustion gas exhaust temperature close to −273 ° C. The volume of the compressed air pressure is more than twice that of the existing gas turbine, more than 10 MPa, and the theoretical air-fuel ratio can be increased to about 4 times that of the existing gas turbine. . The total heat generation amount of the conventional 4 times fuel obtained by the heat exchange + the total heat amount of −273 ° C. or more of the compressed air (the same compressed air amount 5 times the drop of the existing gas turbine × 4 times the recovered heat amount × 50 times the supercritical pressure) Hot water gravity work rate x 10-20 times mechanical efficiency x 1/20 reduction rate) = (same compressed air amount 500-1000 times hypothetical output of existing gas turbine) etc.
[0087]
In order to bring the combustion gas exhaust such as CO2 close to 0, when the storage temperature of the high temperature water 5b with multiple temperatures such as supercritical temperature rises, the high temperature water control valve 7a is controlled to open and normal output is generated. For example, a part of the high-temperature water 5b having a plurality of temperatures such as supercritical temperature is supplied to the uppermost stream of the all blade steam gas turbine, and the combustion gas 10 having the lowest temperature is supplied to the middle flow optimum stage as described above. Drives a full-blade steam gas turbine including a compressor, injects low-temperature water in the process of generating output depending on the application, cools vaporized explosion steam and combustion gas, and reduces the unit volume gravity power of minimum volume to the minimum temperature At maximum, high-temperature water, combustion gas, and water vapor are injected, and the propulsion output is generated by the air suction force and the optimal injection mass speed.
[0088]
Process of converting the energy into the gravity gravity power of high-temperature water mass, optimally decelerating, generating the maximum injection propulsion force, sucking the air in the hollow part of the inner shaft device and the outer peripheral part of the outer shaft device, and propelling the jet Then, the low-temperature combustion gas including the sprayed high-temperature water of the spraying principle 91e is agglomerated and dissolved in water such as 50 times the mass, and the volume of the combustion gas exhaust gas such as CO 2 and the water vapor volume is 1/1000 or 1/1700. Reduced to water droplets, exhaust noise is reduced to 1/10, etc., combustion gas exhaust such as CO2 is brought close to 0, the sea is injected and propelled, and CO2, nitrogen, oxygen, etc. are supplied in a lean manner.
[0089]
Most high-temperature water 5b having a plurality of temperatures such as supercritical temperatures is supplied to a plurality of high-temperature water reservoirs 32a from a plurality of high-temperature water control valves 7a by a five-fold drop or the like of an existing gas turbine. Using a spraying principle 91e, a high-temperature water injection nozzle having a barrel-shaped or wide-spread-barrel-shaped nozzle is provided with a vaporization film between the high-temperature water 5b and appropriately heated to a high temperature by the heating high-temperature means 101 to minimize friction loss. From 59b, high temperature water 5b with multiple temperatures such as supercritical temperature is appropriately mixed and sprayed according to the principle of spraying, etc., and the gravitational power is rationally maximized by utilizing volume such as supercritical pressure and vaporization explosion energy. Rises to generate output.
[0090]
In the process of generating power, the high-temperature water 5b is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by using the vaporization explosive force and volume velocity of the high-temperature water 5b, and the high-temperature water like a shot rocket or snowstorm outside the nozzle. By using the spraying principle 91e, the front air is sucked in multiple stages and injected at an optimum speed, and is bypassed from each special device 92e that propels the jet at a jet mass speed including the air suction force. By jetting, the 270 to 540 times hypothetical output of the existing gas turbine is increased, the speed of jet passenger aircraft etc. is increased by around 10 times, and the exhaust noise is reduced to 1/10 etc. and propulsion is promoted.
[0091]
The process of jetting propulsion jets, flying ships, flying objects, etc. is directly converted into velocity energy of air mass using the principle of spraying, and the air is sucked in most efficiently at a high speed far exceeding the ramjet. The propulsion is propelled and the propulsion is increased to 10 or more times the speed of Mach 10 or more. By increasing the storage temperature of high-temperature water 5b with multiple temperatures such as supercritical temperature, it will be very safe injection propulsion, reduce the fuel load to 1/10 etc., reduce the usage to 1/100 etc., Reduces the occurrence of fire to 1/100, etc., and injects high-temperature water 5b even in the event of a fire, making it easy to extinguish fire, making it a very safe jet, flying ship, flying object, ultra-high speed ship, etc.
[0092]
The whole blade steam gas turbine is driven by a part of the high-temperature water 5b having a plurality of temperatures such as the supercritical temperature and the entire combustion gas 10, the whole blade compressor is driven, and the air in front is sucked and propelled. By using a plurality of spraying principles 91e including known techniques, most of the high-temperature water 5b is bypass-injected by a special head 92e with a large drop far exceeding the ramjet. The mass velocity of the high-temperature water 5b with multiple temperatures such as supercritical temperature is directly converted into the velocity energy of the air mass and optimally decelerated, and optimized. The most efficient mass injection at the injection speed, and each air suction force is applied and propelled at the optimum injection mass speed.
[0093]
The third embodiment of the all blade steam gas turbine combined engine of FIG. 6 also controls opening and closing of a valve (not shown) at the time of start-up, and the high pressure combustion heat exchange cooling combustion is performed by the combustor / heat exchanger 4 without any limitation. The low-temperature combustion gas 10 obtained through heat exchange is supplied to the high-temperature water reservoir 32a and used as an all-blade gas turbine that drives all blade turbines. When the temperature of the high-temperature water 5b having a plurality of temperatures such as the supercritical temperature of the combustor / heat exchanger 4 is increased, the combustion gas 10 is switched to the high-temperature water 5b, and the valve opening / closing control is performed to open the high-temperature water control valve 7a. Then, the whole blade compressor is driven by a part of the high temperature water 5b having a plurality of temperatures such as a supercritical temperature, and the whole blade compressor including the whole blade compressor is exhausted to exhaust the high temperature water and vaporized explosion steam. Air is sucked from the hollow part of the inner shaft device and the outer periphery of the outer shaft device, and the jet propulsion output is generated by the air suction output and the injection mass velocity.
[0094]
All of the low-temperature combustion gas 10 with the combustion gas mass output and most of the remaining high-temperature water 5b after removing the calorific value of the combustion gas, using each spraying principle, makes the structure simple and maximizes the energy conversion efficiency. , Jet propulsion with a jet mass speed of ramjet, 5 times drop × 50 times mass gravity power, etc., and 270-540 times hypothetical output of existing gas turbines, etc. Is increased to around 10 times. The combustion gas 10 and the high temperature water 5b are bypass-injected by the special devices 92b and 92e, respectively, using a plurality of spraying principles 91b and 91e, respectively, and the front air is sucked in multiple stages to obtain an injection propulsion force. In the process, water vapor is cooled and aggregated with low-temperature combustion gas, the water vapor volume is reduced to 1/1700, etc., and the exhaust noise is reduced to 1/10, etc.
[0095]
Water supply whose water repellent water cooling blades 87 and the like of the outer compressor blade group 16 and the inner compressor blade group 17 of the main part of the whole blade compressor are pressurized by a water feed pump and counter-rotating magnetic friction power transmission device 14a. 3 is passed through the cooling means 55 to cool the water, the water supply is jetted from the water injection means 56, the compressed air is directly cooled, and the air volume is reduced as the recovered water. Outer compressor motion consisting of a water-repellent water cooling blade 87 that compresses compressed air almost linearly in a meandering manner and compresses low-temperature air most efficiently as an all-blade blade shape with increased blade spacing by making it a full blade The blade group 16 and the inner compressor rotor blade group 17 are formed into an integral casting 84 in an annular shape for each paragraph.
[0096]
An assembly structure of integral casting 84 is formed in an annular shape capable of fully automatic processing, and the water channel of cooling means 55 is connected at the annular casting assembly connection portion, and water injection means 56 is provided near the assembly annular connection portion. The water passage of the cooling means 55 cools the water-repellent water cooling blades 87, then cools the water jet directly by contact with the water jet means 56, cools the air efficiently with the water supply 3, and uses the low-temperature air in the full blade compressor High pressure compression as much as possible. The heat recovery water supply 3 and the low-temperature compressed air are used in the combustor and heat exchanger 4 for unlimited high-pressure combustion heat exchange cooling combustion, recovering heat about twice that of the existing boiler, and annular combustion of all rotor blade steam turbines The combustion gas temperature of the gas reservoir 9 is lowered to the minimum according to the application.
[0097]
For rotary power engines driven by dynamic pressure or reaction, such as full-blade steam turbines, high-temperature water 5b with multiple temperatures, such as supercritical temperature, has a sufficiently large drop from supercritical pressure to atmospheric pressure, 50 times the mass of combustion gas Because of its large gravitational power, etc., it enables a simple and rational design with a structure of 1/10. Even when using a volume with an increased head like the existing steam turbine, if the gravity power is reduced to the limit, a vast stationary blade is installed to stop the steam speed and reduce it to the practical speed, etc. Therefore, the increase in the unit volume gravity power that increases the dynamic pressure output is regarded as the most important, and the maximum of the atmospheric pressure unit volume gravity power is increased by 1700 times so that a part or most of the moving blade area is 1 Reduces to 1700, enabling rational all-blade design and small, simple, large output such as 1/10.
[0098]
Excessive high-pressure combustion heat exchange is performed in the combustor and heat exchanger 4 to recover heat, and the combustion gas temperature at the combustion gas outlet 88 is lowered to the minimum, so that the recovered heat amount about twice that of the existing boiler is reduced to the supercritical temperature. The maximum amount of heat recovered from the high-temperature water 5b at a plurality of temperatures is maximized, and most of the output is obtained through heat exchange with the highest energy conversion efficiency by using the principle of spraying with the simplest structure (combustion) Gas heat output 250 to 500 times output of existing gas turbine) + (combustion gas mass output 20 to 40 times output of existing gas turbine) = (270 to 540 times hypothesis output of existing gas turbine with the same fuel amount).
[0099]
A part of the high-temperature water 5b with multiple temperatures such as supercritical temperature is supplied to the uppermost stream of all blade steam turbines, water is injected depending on the application in the process of output generation, and vaporized explosion steam and volumetric steam are cooled. A part of the water vapor volume velocity is converted to water with an atmospheric pressure of 1,700 times unit volume gravity power, and reduced to the optimum volume velocity, and the rotation output is generated most efficiently. Then, using the respective spraying principles 91e and 91b, the remaining high-temperature water 5b and the combustion gas 10 are bypass-injected with a 5-fold or 2-fold drop of the existing gas turbine, respectively, and 270 to 540 times that of the existing gas turbine. In the process of hypothetical output, the steam is cooled by low-temperature combustion gas and reduced to 1/1700 volume, the exhaust noise is reduced to 1/10 etc., and the combustion gas exhaust such as CO2 is brought close to 0 and discharged as water droplets. Prevent global warming.
[0100]
In the fourth embodiment of the fully moving blade steam gas turbine combined engine of FIG. 7, the outer compressor blade group 16 and the inner compressor blade group 17 are integrally cast 84 in an annular form for each stage as a fully moving blade shape, and fully automatic. The assembly structure can be machined, and the water channel of the cooling means 55 is connected at the annular casting assembly connection part, and the water injection means 56 is provided near the assembly annular connection part. Then, the half or all of the water-repellent water cooling blades 87 of the whole moving blade compressor are cooled by passing water through the cooling means 55, and the water is injected from the water injection means 56 to be compressed. The air is directly cooled by contact water, and the heat is recovered most efficiently by the feed water 3 and supplied to the combustor / heat exchanger 4 by the water pump / counter-rotating magnetic friction power transmission device 14a, etc. Is supplied to the combustor and heat exchanger 4 with high pressure compression.
[0101]
The recovered heat supply water 3 and the low-temperature compressed air are used in the combustor and heat exchanger 4 as much as possible to recover the high-pressure combustion heat exchange cooling combustion heat, and the temperature of the combustion gas outlet 88 is lowered to the minimum according to the application. Fuel amount The combustion gas calorific power output, which is about twice that of the existing boiler, is output as high temperature water 5b with multiple temperatures such as supercritical temperature, etc. Supply upstream and inject the feed water 3 depending on the application in the process of generating power, cool the volume-utilized water vapor and vaporized explosion water vapor, and convert a part of the water vapor volume velocity to water with an atmospheric pressure of 1700 times unit volume gravity power Then, the volume is reduced to the optimum volume, the optimum deceleration is performed, the rotation output is generated most efficiently, and the entire blade compressor is driven by the rotation output, and the exhaust injection output is used as a floating propulsion output for ships and the like.
[0102]
The combustion water 10 and the remaining most of the high-temperature water 5b, such as the supercritical temperature, are jetted by injecting and jetting water in front of multiple stages using the respective spraying principles 91d and 91f. Directly convert the energy into the velocity mass of water, optimally decelerate, and generate the output by one or more water injection devices 93d and 93f, which suck and inject a large amount of water most efficiently, and most of the output is structured By using the simplest spraying principle, the energy conversion efficiency is maximized, and 270-540 times the hypothetical output of existing gas turbines, various high-speed ships and various high-speed waterborne mobile devices can be used with the same fuel amount of existing technology 10 Prevents global warming by propelling at an appropriate speed, such as around double.
[0103]
In the process of injecting all of the combustion gas 10 by using the respective spraying principle 91d and sucking and injecting the water in front in multiple stages and directly converting the energy into the velocity mass of the water, the combustion gas 10 has a large adiabatic expansion. Even in the process of cooling seawater and dissolving CO2 and nitrogen and other combustion gases in a large amount of seawater and supplying it as cold heat to the seabed, etc. , Sucking oxygen and oxygen into the sea, dilutively supplying them into the sea, thoroughly studying the ecology of marine organisms, including microorganisms, breeding microorganisms, seafood, seaweeds, and seaweeds to increase food production, such as CO2 Combustion gas exhaust is reduced to 0, preventing global warming.
[0104]
The water pump / magnetic friction power transmission device 100a and the water pump / counter-reverse magnetic friction power transmission device 14a will be described with reference to FIGS. Various power transmission devices including normal gear shifting and reverse rotation mainly use gear devices. For this reason, a sliding tooth surface that includes a large load on the tooth surface is essential, and in addition to the need for lubricating oil, the frictional heat loss is also very large, and a high-power transmission device that includes high-speed rotation There is a problem that it cannot be used.
[0105]
In order to put all-blade steam gas turbine combined engines into practical use, an ultra-high-speed, high-power transmission device using rolling contact is essential. In order to enable an ultra-high speed and large power transmission device and to eliminate the need for lubricating oil, the water-cooled frictional heat of the rolling contact with the sliding tooth surface of the gear unit approaching nothing is recovered and combined with the combustor heat. Water supply pump and counter-rotating magnetic frictional power transmission device 14a, such as a space-returning parent plane that aims at 2 to 10 times the number of revolutions of existing technology, and supplies water to the exchanger 4 with a large number of multi-stage water supplies. Used as a pump and magnetic friction power transmission device 100a, combined with an outer shaft device and an inner shaft device that rotate in opposite directions, and used as an ultra-high pressure small quantity water pump and various power transmission devices. Then, a small amount of ultra-high pressure is sent.
[0106]
As the low unevenness 40 in which the meshing height of the gears is reduced as much as possible, the rolling contact water pump and magnetic friction power transmission device 100a is formed, and the rotation direction 35 upstream and downstream, or upstream or downstream, the bar magnet 33 or An electromagnet 34 is provided. Then, by using the strong attractive force of the magnet, various magnetized friction wheel devices 51, various magnetized friction wheel devices 90 not shown, various inner magnetized friction wheel devices 49, and various inner magnetized friction devices not shown. It enables all meshing use of car devices 89, etc., aiming at 2 to 10 times the number of revolutions of existing technology.
[0107]
Various water pumps and various counter-rotating magnetic friction power transmission devices 14a for ultra-high pressure and small amount water supply are provided, and a water absorption passage 95 and a water supply passage 96 are provided in the outer box 94. Use In other words, it is close to rolling contact, greatly reduces frictional heat loss, and also serves as a water pump 97 that feeds ultra-high pressure and small amounts of water, collects self-heating, and transmits high power at ultra-high speed. The power transmission device 100a, the water pump and counter-rotating magnetic friction power transmission device 14a, or non-polluting water cooling instead of the lubricating oil, and the heat-recovered feed water 3 is supplied to the combustor and heat exchanger 4 side. The counter-rotating magnetic friction power transmission device 14 is also used as a water pump 97.
[0108]
Friction heat is unavoidable even when approaching rolling contact to make the counter-rotating magnetic friction power transmission device 14 or the magnetic friction power transmission device 100 that transmits ultra-high speed and large power. On the other hand, an all-blade steam gas turbine combined engine uses ultra-high pressure and a small amount of water and a large amount of heat to double-invert the inner shaft device and the outer shaft device to generate output, thereby generating ultra-high speed and large power. Since a water pump 97 that transfers heat and recovers heat and supplies a small amount of ultra-high pressure is required, it can be used as a water pump and counter-rotating magnetic friction power transmission device 14a or a water pump and magnetic friction power transmission device 100a.
[0109]
Therefore, instead of various gears, various magnetized friction wheels 37, various internally magnetized friction wheels 38, various magnetized friction wheels 39, various internally magnetized friction wheels 44 not shown in the figure, and the like are used. By providing the bar magnet 33 to the electromagnet 34 on the upstream side and the downstream side or the upstream side or the downstream side in the rotational direction in the process of use as the power transmission device 14, a magnetized friction wheel, a magnetized friction wheel, or an inner magnetized friction is provided. All combinations of cars and internal magnetized friction cars can be used interchangeably with the strong attraction of magnets. Various water pumps and counter rotating magnets aiming at 2 to 10 times the number of revolutions of existing technology It is used as the friction power transmission device 14a and various water pumps and magnetic friction power transmission devices 100a.
[0110]
Low unevenness 40 is provided on the power transmission surface 31 of the magnetized friction wheel 37, the magnetized friction wheel 39, the inner magnetized friction wheel 38, and the inner magnetized friction wheel 44. The low unevenness 40 reduces the meshing height as much as possible, enables a shape other than the gear as rolling contact, and makes all the meshing shapes not shown in the figure. Specifically, the gear-shaped low unevenness 40 is replaced with a spur gear and replaced with a 41 spur uneven surface, replaced with a Hasuba gear with a 42 sprocket uneven surface, and replaced with a Yamaha gear with 43 corrugated uneven surfaces and provided with a super high pressure small amount of water. And high power high speed transmission.
[0111]
Alternatively, a flat internal irregularity 41a car is provided instead of the flat internal gear not shown, a Hasuba internal irregularity 42a car is provided instead of the Hasuba internal gear, and a Yamaba internal irregularity 43a car is provided instead of the Yamaha internal gear. And as with various known gear pumps, an outer box 94, a water absorption path 95, and a water supply path 96 are provided, and the super high speed and large power is transmitted as a water pump 97 that collects frictional heat and supplies a small amount of ultra high pressure water. It is used as various water pumps and counter-rotating magnetic friction power transmission device 14a aiming at 2 to 10 times the speed of existing technology, and as various water pumps and magnetic friction power transmission device 100a.
[0112]
The embodiment of the magnetized friction wheel 37a shown in FIGS. 8a and 8b is such that the north and south poles of the magnetic pole are magnetized on the left and right in the radial direction of the annular cylindrical ferromagnetic material, and the annular plate-like yokes on both sides thereof. It is sandwiched between 47 and extended to the power transmission surface 31 in the outer diameter direction. The power transmission surface 31 is provided with a flat unevenness 41 of a low unevenness 40, a Hasuba unevenness 42, etc. on the outer peripheral surface of the power transmission surface 31 so that each element is mutually compatible as a magnetized friction wheel 37a, 37a, etc. The magnetized friction wheel 39 or the rolling contact magnetized friction wheel device 51 is provided with an outer box 94, a water absorption path 95, a water supply path 96, and the like in the same manner as the magnetized friction wheel apparatus 51c + 97 in FIG. 9 and 97 + 14 in FIG. It is used as various water pumps and counter rotating magnetic friction power transmission device 14a and various water pumps and magnetic friction power transmission device 100a.
[0113]
In the embodiment of the magnetized friction wheel 37b of FIG. 8c, the N pole and S pole of the magnetic pole are magnetized on the inner diameter side and the outer diameter side of the annular cylindrical ferromagnetic material, and the yoke 47 is moved from the inner peripheral side of the magnet. Extends to the left and right outer diameter power transmission surface 31. Between the yoke and the magnet in the vicinity of the power transmission surface, the friction increasing means 45 is provided and fixed in an annular shape, and the Yamaba unevenness 43 of the low unevenness 40 is provided on the outer peripheral surface thereof, as magnetized friction wheels 37b and 37b, respectively. Each element is interchanged so that the outer casing 94, the water absorption path 95, the water supply path 96, etc. are similar to the magnetized friction wheel 39, the magnetized friction wheel 37b, the magnetized friction wheel device 51d + 97 in FIG. 10, and 97 + 14 in FIG. Installed and used as various water pumps and counter rotating magnetic friction power transmission device 14a and various water pumps and magnetic friction power transmission device 100a.
[0114]
In the embodiment of the magnetized friction wheel 39 of FIGS. 8d, 8e, and 8f, the friction increasing means 45 is provided on the power transmission surface 31 of the outer diameter surface of the annular cylindrical ferromagnetic material. Alternatively, the power transmission surface 31 is provided with a flat asperity 41 of a low asperity 40, a Hasuba asperity 42, or a Yamaba asperity 43 on its outer peripheral surface, which are used as various magnetic friction wheels 39 and 39, respectively. As shown in FIGS. 9 and 10, by providing bar magnets 33 or electromagnets 34 on the upstream side and the downstream side in the rotation direction, the respective elements are compatible with each other, and various types of magnetic friction of rolling contact without a figure number. The vehicle device 90 and various magnetic friction power transmission devices 100 are used.
[0115]
Alternatively, friction increasing means 45 is provided on the power transmission surface 31 of the inner surface of the annular cylindrical ferromagnetic material not shown. Alternatively, the power transmission surface 31 is provided with a flat unevenness 41 of a low unevenness 40, a Hasuba unevenness 42 or a Yamaba unevenness 43 on the inner peripheral surface thereof, and various internal magnetized friction wheels 44 and 44, respectively. Each element is mutually interchangeable to form various types of inner-magnetized friction wheels 89 and the like that are in rolling contact with the magnetic friction power transmission device 100 and the counter-rotating magnetic friction power transmission device 14 shown in FIGS. 9, 10, and 11. In substantially the same manner, an outer box 94, a large number of water intake paths 95, a large number of water supply paths 96, and the like are provided and used as a water pump and counter-rotating magnetic friction power transmission device 14a, a water pump and magnetic friction power transmission device 100a, and the like. To do.
[0116]
For example, in the first and second embodiments of the water pump and magnetic friction power transmission device 100a shown in FIGS. 9 and 10, the outer casing 94 is provided in the magnetized friction wheel devices 51c and 51d in the same manner as the existing gear pump. Installed, water intake channel 95 and water supply channel 96 are provided for each, and various water pumps 97 are used. Then, the water supply 3 is supplied from the water intake path 95, the heat generated by the various magnetic friction power transmission devices 100 is recovered, and the water is supplied from the water supply path 96 to the combustor / heat exchanger 4 side.
[0117]
However, since the power transmission is the main force of the water friction pump and magnetic friction power transmission device 100a such as the magnetized friction wheel devices 51c and 51d, the rotational speed also changes. Therefore, one or more water supply passages 96 and water intake passages 95 are optimally controlled by a known control device, and supplied to the water injection means 56 and 56a in the process of pressure increase in one or more stages, and the combustor and heat exchanger 4 High temperature water 5b with multiple temperatures such as supercritical temperature. That is, by using one or more water pumps 97, friction heat is recovered and self-water cooling is performed. Used as various water pumps and magnetic friction power transmission device 100a.
[0118]
For example, the water pump and counter-rotating magnetic friction power transmission device 14a that transmits ultra-high speed and large power and enables ultra-high pressure and small-volume water feeding in FIG. Since the water channel 96, the many magnetized friction wheels 37a, the inner magnetized friction wheel 38a, and the like constitute a large number of water pumps 97, the outer box 94 is also very complicated. However, since the peripheral speed of the magnetized friction wheel 37a is two types, those with the same peripheral speed are merged. In this case, the pressure is controlled by increasing the pressure to two stages or multiple stages, and combined with other water pumps according to the application. Then, water is supplied to the combustor and heat exchanger 4 side. Friction heat is collected by a large number of water pumps 97, self-cooled by water, and used as various counter-rotating magnetic frictional power transmission devices 14 that also serve as a water pump 97 and transmit super-high power.
[0119]
This will be described with reference to FIGS. 11 (a), 11 (b), and 11 (c). (B) and (c) are cc and dd views of (a), respectively, and the rotational power of the inner shaft device and the outer shaft device of the all-blade steam gas turbine combined engine rotating in opposite directions to each other. The counter-rotating magnetic frictional power transmission device 14 that couples the two shafts recovers frictional heat in multiple stages by a large number of water pumps 97, self-water cools, and optimally uses two shafts of ultra-high speed and large power that rotate in opposite directions. Used as a counter rotating magnetic frictional power transmission device 14 that transmits counter rotating at the rotation ratio.
[0120]
A shaft is attached to an outer box 94 fixed to the engine body by the rotation of the first main driven inner magnetized friction wheel 38a including the magnet portion 46 and the yoke 47, which are fixed to the outer shaft device of the all-blade steam gas turbine combined engine. A plurality of first driven magnetized friction wheels 37a fixed to the left end of the support shaft 50 rotate, and a plurality of second main magnetization magnetized friction wheels 37a fixed to the right end of the support shaft 50 by rotation thereof. The second driven magnetized friction wheel 37a, which is rotated and fixed to the inner shaft device by the rotation, rotates and combines the rotational force of the outer shaft device rotating in the opposite direction and the rotational force of the inner shaft device. , The full rotation output can be taken out from the inner shaft device or the outer shaft device, or the rotation output can be taken out from both respectively.
[0121]
11 (b) and 11 (c) show the process of use as a counter rotating magnetic friction power transmission device 14 also serving as a water pump 97 for transmitting ultra high speed and large power and delivering ultra high pressure and small amount of water. Alternatively, all combinations of the magnetized friction wheel 37, the magnetized friction wheel 39, the inner magnetized friction wheel 38, and the inner magnetized friction wheel 44 are provided by providing the bar magnets 33 to the electromagnets 34 on the upstream side or the downstream side. The magnet's strong attractive force makes it compatible with each other. Including the inner magnetized friction wheel 38a fixed to the outer shaft device, the magnetized friction wheel 37a fixed to the inner shaft device, and the plurality of magnetized friction wheels 37a meshing with each other, the outer gear is substantially the same as the existing gear pump. A box 94 is provided.
[0122]
A water supply path 96 is provided upstream of the plurality of magnetized friction wheels 37 a meshing with the inner magnetized friction wheel 37 a including the rotational direction bar magnet 33 or the electromagnet 34, and downstream of the rotation direction bar magnet 33 or the electromagnet 34. A water supply passage 95 is provided, and a water supply passage 96 is provided on the upstream side including the rotation direction electromagnet 34 or the bar magnet 33 of the plurality of magnetization friction wheels 37a meshing with the magnetization friction wheel 37a fixed to the inner shaft device. A water absorption path 95 is provided on the downstream side including 34 or the bar magnet 33 to constitute a water pump 97 and a counter rotating magnetic friction power transmission device 14a that transmits super high speed and large power.
[0123]
FIG. 12 illustrates prevention of global warming according to the present invention. In the world's thermal power plants and nuclear power plants, supercritical pressure superheated steam heated by boilers, nuclear power, etc. is adiabatically expanded by a steam turbine, using only the volume and not using heat at all. Since the seawater temperature rises with all the heat that is heated, a huge amount of heat is lost and the environment is destroyed. Furthermore, when adiabatic expansion is performed from supercritical pressure superheated steam to condenser vacuum by reheating or the like, the volume exceeds 10,000 times and the gravitational power becomes 1 / 10,000 or less, and the rotor blade area is 10,000 times or more for the output under the same conditions. Is necessary, and enormous steam speed becomes difficult to use, consumes steam speed 10 to 20 times that of the moving blade, and also provides half of the stationary blades that do not perform rotation work. Acceleration of global warming due to unreasonable design such as slowing down is inevitable.
[0124]
The most unreasonable unpleasant is that it consumes 10 to 20 times the speed energy of the moving blades and has 1/2 stationary blades that do not rotate at all, slowing down the superheated steam velocity is. Therefore, in order to effectively use the amount of heat, the gas turbine combustor is also used as a heat exchanger, and the high-pressure combustion heat exchange cooling combustion is performed by the all blade steam gas turbine combustor / heat exchanger 4 as much as possible, and the combustion gas exhaust is performed. The temperature is brought close to −273 ° C., enormous amounts of cold and warm heat are supplied as a by-product of power generation at a manufacturing cost of approximately 0, water vapor is cooled by combustion gas exhaust such as CO2, and combustion gas such as CO2 is dissolved in condensed water. In order to prevent global warming, exhaust of CO2 etc. is set to zero. Then, the recovered heat amount is increased to about twice that of the existing boiler with the same fuel amount and recovered as high-temperature water 5b having a plurality of temperatures such as supercritical temperature (combustion gas heat output + combustion gas mass output) = (270 of existing gas turbine) Increase to ~ 540 times hypothesis output) and prevent global warming.
[0125]
The heat quantity of high-temperature water 5b at multiple temperatures, such as the supercritical temperature approximately twice that of the existing boiler, is supplied to the uppermost stream of the all blade steam turbine, and the supercritical pressure is 1700 times the gravity power of the existing reheat steam turbine. The high temperature water 5b is heated and heated, and a vaporized film is provided between the high temperature water and the high temperature water injection nozzle 59b in which the friction loss is minimized or outside the nozzle by using the vaporization explosive force or volume velocity. Accelerate like machine gun bullets, shot rockets and snowstorms, bring atmospheric pressure unit volumetric gravitational power closer to 1700 times that of existing steam turbines, and make combustion gas heat output + combustion gas mass output the same fuel amount 270 to 540 times the hypothesis output, preventing global warming.
[0126]
In order to recover and use all of the heat applied to the full blade steam turbine, a vaporization latent heat recovery unit 66a is provided in substantially the same manner as the existing condenser, and the vaporization heat at a saturation temperature of 100 ° C. is changed to seawater and cooled with tap water And all of the enormous heat of vaporization obtained by heat recovery is stored at 100 ° C or less as tap water temperature with a manufacturing cost of almost 0 as a by-product of power generation, and tap water together with an inexpensive electricity bill such as 1/10 We will supply it to customers as heat and explode the demand. All the condensed water is circulated and supplied to the combustor / heat exchanger 4 repeatedly as much as possible, and the combustor / heat exchanger 4 only supplies high-temperature water vaporization / explosion energy to minimize the fuel combustion mass. In addition, we will abolish the unreasonable technology of steam turbines that have increased the seawater temperature with all the heat of vaporization + α.
[0127]
By using the all-blade gas turbine combustor and heat exchanger 4 to briefly explain the by-products of all-blade gas turbine power generation, the high-pressure combustion heat exchange cooling combustion is performed as much as possible, and the combustion gas exhaust temperature is brought close to -273 ° C. The collector 102 collects a huge amount of cold heat from the low-temperature combustion gas with tap water, and stores it at 2 to 5 ° C. or the like as cold water for tap water with a production cost of power generation of about 0, and stores it at 1/10, etc. Along with cheap electricity charges, supply to customers as tap water cooling heat, completely eliminate commercial and household refrigeration equipment, coolers and refrigeration equipment, supply chilling equipment, cooler and refrigeration equipment using tap water cooling heat, Too much tap water cooling water sprinkles and cools the whole city area, and CO2 and other combustion gas exhausts 0 and defluorocarbons prevent global warming.
[0128]
Various devices that are driven by the rotational force of the full blade gas turbine and the full blade steam turbine of FIG. 13 will be described. High-pressure combustion heat exchange cooling combustion is performed by the combustor and heat exchanger 4 as much as possible, and the combustion gas exhaust temperature is brought close to −273 ° C. as a heat recovery amount about twice that of the existing boiler. The electricity cost is reduced to 1/10 or the like by the blade steam turbine, and the entire supply heat amount is supplied to the consumer as tap water temperature of 100 ° C. or less as a by-product of power generation by the vaporization latent heat recovery unit 66a. Drives various heat, electricity, and cold supply equipment that supplies all of the combustion gas to consumers as a by-product of power generation, and a large amount of cold water.
[0129]
The full-blade steam turbine for generating rotational output is subjected to high-pressure combustion heat exchange cooling combustion without limit by the combustor / heat exchanger 4 and the exhaust gas temperature is brought close to −273 ° C. to drive the full-blade gas turbine. And used for other purposes such as power generation and cooling. As high-temperature water 5b having a heat recovery amount of about twice that of the existing boiler obtained by heat exchange, an output is generated up to atmospheric pressure to obtain a hypothetical output of 250 to 500 times that of the existing gas turbine, and an air-cooled vaporization latent heat recovery unit 66b Condensate is collected by the above, and supplied to the combustor and heat exchanger 4 as much as possible, and all the moving blade steam gas turbine combined engines that circulate and use the condensate as much as possible are used in various automobiles, various vehicles, various machines, Drives various general-purpose engines and tanks.
[0130]
A high-pressure combustion heat exchange cooling combustion is performed infinitely by the combustor and heat exchanger 4 of the all rotor blade steam turbine that generates rotational output with a part of the high-temperature water 5b, and the combustion gas exhaust temperature approaches -273 ° C. Most of the high-temperature water 5b and all combustion gases are bypass-injected using the principle of spraying, and the air or water in front is sucked and injected. As a hypothetical output of 270-540 times that of the existing gas turbine, Various all-speed blade steam gas turbine combined engines aiming at 10 times speed and exhaust noise, etc., various super high speed vessels, various vertical lift aircraft, various ultra high speed ships, various ultra high speed fighters, various space return parents Drives airplanes, various ultra-high speed sound speed aircraft, various ultra-high-speed aircraft.
[0131]
【The invention's effect】
In order to inject the high-temperature water 5b having a plurality of temperatures such as supercritical temperature from the high-temperature water injection nozzle 59b, the atmospheric pressure unit volume gravity power is brought close to 1700 times that of the existing steam turbine, and the same fuel amount of the existing gas turbine Has an effect of increasing the hypothesis output to 500 times.
[0132]
In order to inject the high-temperature water 5b having a plurality of temperatures such as supercritical temperature from the high-temperature water injection nozzle 59b, the atmospheric pressure unit volume gravity power is brought close to 1700 times that of the existing steam turbine most efficiently, Most of them are reduced to 1/1700, which makes it possible to design a reasonable moving blade area and to make the structure small, simple, and large output such as 1/10.
[0133]
Since high-temperature water 5b having a plurality of temperatures such as supercritical temperature is used, a vaporized film is provided between the high-temperature water and the high-temperature water jet nozzle 59b heated to high temperature by means of heating high-temperature means, and vaporization of high-temperature water with minimum friction loss. By using explosive force and volume velocity, high temperature water is accelerated inside the high temperature water injection nozzle 59b like a bullet of a machine gun or snowstorm, and high temperature water is accelerated outside the nozzle like a shot rocket or snowstorm, and the same amount of fuel. It has the effect of making the hypothetical output 500 times that of existing gas turbines.
[0134]
In order to inject the entire moving blade electromagnetically heated turbine blade 81 and the electromagnetic heating nozzle 83 with a vaporized film between the high temperature water and the electromagnetic heating high temperature, and to inject substantially linearly meandering by all the moving blades with little friction loss, It has the effect of generating output most efficiently.
[0135]
The electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine blade group 20 are integrally cast in an annular shape for each stage, and have the effect of easily and reliably increasing the electromagnetic heating temperature.
[0136]
By water injection means 56a provided in a thermally insulated manner, water is injected to cool the combustion gas and vaporized explosion water vapor, the unit volume mass and the total mass are increased and the temperature is lowered, and the combustion gas exhaust gas such as CO2 is reduced to zero. It has the effect of making it easier to get closer.
[0137]
Even when the combustion gas exhaust temperature is brought close to −273 ° C. and a large unit volume gravity power or total gravity power is obtained, a vaporization film is provided between high temperature water and the like by the whole blade electromagnetic heating turbine blade 81. It has the effect of generating large output with minimal friction loss.
[0138]
By exchanging low-temperature and high-pressure air with a combustor and heat exchanger as much as possible, high-pressure combustion heat, the fuel combustion mass is increased to about four times that of the existing gas turbine to the stoichiometric air-fuel ratio. Since the combustion gas inlet temperature and the combustion gas outlet temperature of the combustor / heat exchanger are minimized, the compression pressure is increased to 10 MPa or more, which is twice or more, and the combustion gas mass output is 20 to 40 times that of the existing gas turbine. This has the effect of increasing the hypothesis output.
[0139]
Add almost all of the compressed air at 273 ° C or higher to the calorific value of the combustion gas obtained by heat exchange, and convert the calorific value of the combustion gas approximately twice that of existing boilers into high-temperature water 5b with multiple temperatures such as supercritical temperature. Thus, there is an effect that the combustion gas heat output is increased to a hypothetical output 250 to 500 times that of the existing gas turbine.
[0140]
As the high-temperature water 5b with multiple temperatures such as supercritical temperature, the full-blade steam gas turbine, full-blade steam turbine, and special devices 92e and 92b are driven, and the air is sucked and propelled most efficiently for combustion. It has the effect of increasing gas mass output + combustion gas calorie output to a hypothetical output of 270-540 times that of existing gas turbines.
[0141]
As high-temperature water with multiple temperatures such as supercritical temperature, drive all-blade steam gas turbines, all-blade steam turbines, and water injection devices 93d and 93f to aspirate and propel the water most efficiently. It has the effect of increasing gas mass output + combustion gas calorie output to a hypothetical output of 270-540 times that of existing gas turbines.
[0142]
Combustion gas exhaust temperature is brought close to −273 ° C., and the effect of increasing the same fuel amount combustion gas mass output, which is less than or equal to zero combustion gas heat consumption of all rotor blade gas turbines, to a hypothetical output 20 to 40 times that of existing gas turbines. There is.
[0143]
In order to cool the vaporized explosion steam and combustion gas by low-temperature water injection and convert the energy to the speed power of the water mass with 1000 times or 1700 times gravitational power, and optimally decelerate, There is an effect that the structure can be designed to be small, easy and large output around 1/10.
[0144]
Excessive high pressure combustion heat exchange with a combustor and heat exchanger, heat recovery amount about twice that of existing boilers, reducing electricity bills to 1/10, etc., CO2 etc. discharged from power plants etc. It also has the effect of recovering and using the global warming combustion gas most efficiently.
[0145]
Completely abolish existing commercial and household refrigeration equipment, refrigeration equipment, and cooling equipment, provide commercial and household refrigeration equipment, refrigeration equipment, and refrigeration equipment, and use refrigeration, CO2 exhaust, etc. Has the effect of preventing global warming.
[0146]
As the amount of power generation increases, the production of cryogenic combustion gas increases, so when the seawater is cooled, dilute supply of CO2, nitrogen and oxygen to the seabed, breeding food microbes, seaweeds and fish, etc. It has an effect of activating, and can be used effectively if the concentration is appropriate, and it has the effect of thinking about methods that contribute to humanity by reversing errors such as seabed fixation.
[0147]
Combustion and heat exchangers of various all-blade steam gas turbine combined engines, and by performing high-pressure combustion heat exchange as much as possible, the fuel combustion mass of the same amount of compressed air up to the theoretical air-fuel ratio is about four times that of existing gas turbines. Because the combustion gas inlet temperature is minimized, the compression pressure can be increased to 10MPa, more than twice, and the same fuel amount can be increased to 500 times the hypothetical output of existing gas turbines.
[0148]
The low-temperature combustion gas obtained by heat exchange and the water vapor of the high-temperature water 5b are water-cooled, and the unit mass gravity power is increased to a maximum of 1700 times the atmospheric pressure of the existing steam turbine, and the gravitational power is increased by 50%. It has the effect of increasing around twice.
[0149]
The existing steam turbine superheated steam has a great effect of generating output with a large dynamic pressure of 1700 times gravity power of the superheated steam.
[0150]
By increasing the gravitational power to 1700 times that of the existing steam turbine in the atmospheric pressure section, part or most of the turbine blade area is reduced to 1/1700, and the structure is greatly reduced in size to 1/10. There is an effect that can be done.
[0151]
It has the great effect of eliminating the reheating and stationary blades of the existing reheat steam turbine and making the structure of all the moving blades small and easy.
[0152]
Adiabatic expansion low-temperature combustion gas in order to increase the mass of low-temperature water by injecting water and cooling water vapor and combustion gas in the process of generating output in a full-blade steam gas turbine and all-blade steam gas turbine combined engine The effect of cooling and agglomerating water and adding chemical substances etc. to harmless discharge in the process of synthesizing and mixing combustion gas such as CO2 in 50 times mass water etc. as water drops etc. like natural phenomenon There is also.
[0153]
It emits pollution combustion gas exhaust such as CO2 discharged from various automobiles, various ships, various airplanes, and various mechanical devices as water droplets, and has the effect of greatly reducing CO2 exhaust.
[0154]
Because it is an all-blade steam gas turbine combined engine, it is possible to remove the all-blade compressor and combustor / heat exchanger 4 of the all-blade gas turbine, and to make a very small and simple all-blade gas turbine. .
[0155]
Since the air-cooled latent heat recovery unit 66b is included, in transportation equipment such as various automobiles, the condensed water can be repeatedly supplied to the combustor / heat exchanger 4 as many times as possible, and the condensed water can be circulated and used.
[Brief description of the drawings]
FIG. 1 is a partial sectional view showing a first embodiment of a full blade steam turbine.
FIG. 2 is an explanatory cross-sectional view showing an embodiment of a high-temperature water injection nozzle 59b.
FIG. 3 is a partial cross-sectional view showing a first embodiment of a full blade gas turbine.
FIG. 4 is a partial cross-sectional view showing a first embodiment of a full-blade steam gas turbine combined engine.
FIG. 5 is a partial cross-sectional view showing a second embodiment of the all blade steam gas turbine combined engine.
FIG. 6 is a partial cross-sectional view showing a third embodiment of the all blade steam gas turbine combined engine.
FIG. 7 is a partial cross-sectional view showing a fourth embodiment of the all blade steam gas turbine combined engine.
FIG. 8 is a partial cross-sectional view showing an embodiment of a magnetized friction wheel and a magnetized friction wheel.
FIG. 9 is a partial cross-sectional view of a first embodiment of a water pump / magnetic frictional power transmission device.
FIG. 10 is a partial cross-sectional view of a second embodiment of the water pump / magnetic frictional power transmission device.
FIG. 11 is a partial cross-sectional view of an embodiment of a water pump and counter-rotating magnetic frictional power transmission device.
FIG. 12 is an explanatory diagram for preventing global warming in an all-blade steam gas turbine combined engine.
FIG. 13 is an explanatory diagram showing an apparatus that is driven by an all-blade steam gas turbine combined engine.
[Explanation of symbols]
1: Water guide pipe 2: Water supply pump 3: Water supply 4: Combustor and heat exchanger 5: Steam 5a: High temperature water 5b: High temperature water (multiple temperature such as supercritical temperature to be mixed and injected as appropriate according to the principle of spraying) 6: Steam pipe 6a: High temperature water pipe 7: Steam control valve 7a: High temperature water control valve 8: Annular compressed air reservoir 9: Annular combustion gas reservoir 10: Combustion gas 11: Fuel 12: Output shaft 13: Stop Valve 14: Counter-rotating magnetic friction power transmission device 14a: Water pump and counter-rotating magnetic friction power transmission device 15: Compressed air 16: Outer compressor rotor blade group 17: Inner compressor rotor blade group 19: Electromagnetically heated outer turbine rotor blade Group 20: Electromagnetically heated inner turbine blade group 21: Annular outlet 22: Annular receptacle 23: Annular receptacle 24: Annular electromagnetic heating nozzle group 25: Combustor outer box part 26: Water-cooled outer wall 27: Fuel vapor supply means 28: Buy Path 31: Power transmission surface 32: Superheated steam reservoir 32a: High temperature water reservoir 33: Bar magnet 34: Electromagnet 35: Direction of rotation 36: Magnetic pole 37: Magnetized friction wheel 38: Inner magnetized friction wheel 39: Magnetized friction wheel 40: Low unevenness 41: Flat unevenness 42: Hasuba unevenness 43: Yamaba unevenness 44: Inner magnetized friction wheel 45: Friction increasing durability means 46: Magnet part 47: Yoke (for magnetized friction wheel) 48: Insulating material 48a: Insulating material 49a : Inner magnetized friction wheel device 49b: Inner magnetized friction wheel device 50: Support shaft 51a: Magnetized friction wheel device 51b: Magnetized friction wheel device 51c: Magnetized friction wheel device 51d: Magnetized friction wheel device 52: Water cooling Outer wall unit 53: 鍔 54: Water cooling inner wall 55: Cooling means 56: Water injection means 56a: Water injection means 57: Capillary discharge means 58: Exhaust heat exchanger 59: Superheated steam tube port 59a: High temperature water injection nozzle 59b: High temperature Injection nozzle (High temperature water such as supercritical temperature is mixed and injected as appropriate, including spraying principle) 60: Fuel injection port 61: Needle valve 62: Small fuel hole 63: Fuel hole switch 64: Air hole switch 65: Air hole 66: Condensate heat exchanger 66a: Evaporative latent heat recovery unit 66b: Air-cooled latent heat recovery unit 67: Condenser 68: Condensed water 69: Exhaust 70: Tap water 71: Heat 72: Cooling 73: Cooling water 74 : Thrust 80: Yoke 81: Electromagnetically heated turbine blade 83: Electromagnetically heated nozzle 84: Annular casting integrally 85: Outer diameter assembly annular portion 86: Inner diameter assembly annular portion 87: Water repellent water cooling blade 87a: Water repellent turbine blade 88: Combustion gas outlet 89: Inner magnetized friction wheel device 90: Magnetized friction wheel device 91a: Principle of spraying (suction injection of air by high-temperature water injection) 91b: Principle of spraying (suction injection of air by combustion gas injection) ) 91c: Principle of spraying (water is sucked and injected by high-temperature water injection) 91d: Principle of spraying (water is sucked and injected by multistage injection of combustion gas) 91e: Principle of spraying (air is sucked and injected by multi-temperature high-temperature water injection) 91f: Principle of spraying (water is sucked and jetted by multiple temperature high temperature water jet) 92a: Special device (air is sucked and jetted by high temperature water jet) 92b: Special device (air suction jet by combustion gas jet) 92e: Special device (multiple temperature high temperature) 93a: Water injection device (suction injection of water by high temperature water multi-stage injection) 93b: Water injection device (suction injection of water by combustion gas injection) 93d: Water injection device (combustion gas multiple stages) 93f: Water injection device (suction injection of water with multi-temperature high-temperature water multi-stage injection) 94: Outer box 95: Water absorption path 96: Water supply path 97: Water supply pump 98: Coil 99: Magnetic field line 100 : Magnetic frictional power transmission device 100a: Water pump and magnetic frictional power transmission device 101: High temperature heating means 102: Cold heat recovery device 103: Fully moving blade blower

Claims (2014)

燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized in that it is converted to high-temperature water at a plurality of temperatures such as a supercritical temperature by a combustor and heat exchanger (4) so that the amount of heat supplied to the high-temperature water approaches the minimum heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  All-blade steam gas turbine combined engine characterized by converting to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bringing the supercritical pressure hot water supply heat amount to the minimum heat of vaporization . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that it is converted into high-temperature water having a plurality of temperatures such as a supercritical temperature by a combustor and heat exchanger (4) so that the amount of heat supplied to the high-temperature water is close to that of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that it is converted to high-temperature water at multiple temperatures such as supercritical temperature by a combustor and heat exchanger (4) to bring the supercritical pressure high-temperature water supply heat close to vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Whole blade steam, characterized by converting to high temperature water with multiple temperatures such as supercritical temperature by a combustor and heat exchanger (4), and making use of vaporization explosive force by bringing the amount of heat supplied to the high temperature water close to the minimum vaporization heat Gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted to high-temperature water with multiple temperatures such as supercritical temperature by a combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is made close to the minimum vaporization heat and the vaporization explosive force is used. Rotor steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  A full rotor blade steam gas turbine characterized in that it is converted to high-temperature water at multiple temperatures such as supercritical temperature by using a combustor and heat exchanger (4) and the vaporization explosive force is utilized by bringing the amount of heat supplied to high-temperature water close to that of vaporization heat. Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  All rotor blades characterized in that they are converted to high-temperature water at multiple temperatures such as supercritical temperature by a combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is made close to the vaporization heat and the vaporization explosive force is used. Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water injection nozzle (59b) using the vaporization explosive force by converting the high temperature water supply heat amount to the minimum vaporization heat by converting it into high temperature water such as supercritical temperature by the combustor and heat exchanger (4) An all-rotor-blade steam gas turbine combined engine characterized by more injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water injection nozzle using the vaporization explosive force by converting to supercritical pressure high temperature water supply heat amount to the minimum vaporization heat by converting to high temperature water such as supercritical temperature by combustor and heat exchanger (4) (59b) An all-blade steam gas turbine combined engine characterized by injection from (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as supercritical temperature by the combustor and heat exchanger (4), and the high temperature water supply heat is made close to the heat of vaporization and injected from the high temperature water injection nozzle (59b) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water injection nozzle (59b) is converted into high temperature water having a plurality of temperatures such as a supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high temperature water supply heat amount is made close to the vaporization heat and the vaporization explosive force is used. ) All-rotor-blade steam gas turbine combined engine characterized by more injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  By using a combustor and heat exchanger (4), high temperature water such as a supercritical temperature is converted to high temperature water, and the high temperature water supply heat amount is made close to the minimum vaporization heat and the vaporization explosive force is used to heat the high temperature means (101). An all-rotor-blade steam gas turbine combined engine characterized by being injected from a high-temperature water injection nozzle (59b) that is heated to a high temperature. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), bring the supercritical pressure high temperature water supply heat close to the minimum vaporization heat and use vaporization explosive force to heat high temperature means ( 101) An all-rotor-blade steam gas turbine combined engine characterized by being injected from a high-temperature water injection nozzle (59b) heated to a high temperature by 101). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount is brought close to the heat of vaporization, and the high-temperature heat (101) is heated by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by being injected from the high-temperature water injection nozzle (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water heating means (101) using the combustor and heat exchanger (4) to convert it to high temperature water at multiple temperatures such as supercritical temperature, making the supercritical pressure high temperature water supply heat close to the heat of vaporization and utilizing the vaporization explosive force An all-rotor-blade steam gas turbine combined engine characterized by jetting from a high-temperature water jet nozzle (59b) heated to a high temperature. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  By using a combustor and heat exchanger (4), high temperature water such as a supercritical temperature is converted to high temperature water, and the high temperature water supply heat amount is made close to the minimum vaporization heat and the vaporization explosive force is used to heat the high temperature means (101). An all-rotor-blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) that are heated to high temperatures. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), bring the supercritical pressure high temperature water supply heat close to the minimum vaporization heat and use vaporization explosive force to heat high temperature means ( 101) A full moving blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by 101). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount is brought close to the heat of vaporization, and the high-temperature heat (101) is heated by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water heating means (101) using the combustor and heat exchanger (4) to convert it to high temperature water at multiple temperatures such as supercritical temperature, making the supercritical pressure high temperature water supply heat close to the heat of vaporization and utilizing the vaporization explosive force An all-rotor-blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water injection nozzle (59b) using the vaporization explosive force by converting the high temperature water supply heat amount to the minimum vaporization heat by converting it into high temperature water such as supercritical temperature by the combustor and heat exchanger (4) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water injection nozzle using the vaporization explosive force by converting to supercritical pressure high temperature water supply heat amount to the minimum vaporization heat by converting to high temperature water such as supercritical temperature by combustor and heat exchanger (4) (59b) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount is made close to the heat of vaporization and the vaporization explosive force is used to make all of the heat from the high-temperature water injection nozzle (59b) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a rotor blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water injection nozzle (59b) is converted into high temperature water having a plurality of temperatures such as a supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high temperature water supply heat amount is made close to the vaporization heat and the vaporization explosive force is used. ) A full-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a full-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  By using a combustor and heat exchanger (4), high temperature water such as a supercritical temperature is converted to high temperature water, and the high temperature water supply heat amount is made close to the minimum vaporization heat and the vaporization explosive force is used to heat the high temperature means (101). An all-rotor-steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59b), which is heated to a high temperature, is injected into the uppermost stream of all the rotor blade steam turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), bring the supercritical pressure high temperature water supply heat close to the minimum vaporization heat and use vaporization explosive force to heat high temperature means ( 101) An all-blade steam gas turbine combined engine characterized in that the hot-water injection nozzle (59b) heated to a high temperature by 101) is jetted to the uppermost stream of the entire bucket steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount is brought close to the heat of vaporization, and the high-temperature heat (101) is heated by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by being injected from the high-temperature water injection nozzle (59b) into the uppermost stream of the entire bucket steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water heating means (101) using the combustor and heat exchanger (4) to convert it to high temperature water at multiple temperatures such as supercritical temperature, making the supercritical pressure high temperature water supply heat close to the heat of vaporization and utilizing the vaporization explosive force A full-blade steam gas turbine combined engine, characterized in that it is jetted from the high-temperature water injection nozzle (59b) heated to high temperature by the uppermost stream of the full-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  By using a combustor and heat exchanger (4), high temperature water such as a supercritical temperature is converted to high temperature water, and the high temperature water supply heat amount is made close to the minimum vaporization heat and the vaporization explosive force is used to heat the high temperature means (101). An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of all the rotor blade steam turbines from a plurality of high-temperature water injection nozzles (59b) having high heating temperatures. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), bring the supercritical pressure high temperature water supply heat close to the minimum vaporization heat and use vaporization explosive force to heat high temperature means ( 101) An all-rotor-steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all the rotor blade steam turbines from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by 101). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount is brought close to the heat of vaporization, and the high-temperature heat (101) is heated by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized in that it is jetted from the plurality of high-temperature water injection nozzles (59b) to the uppermost stream of the entire bucket steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water heating means (101) using the combustor and heat exchanger (4) to convert it to high temperature water at multiple temperatures such as supercritical temperature, making the supercritical pressure high temperature water supply heat close to the heat of vaporization and utilizing the vaporization explosive force An all-rotor-blade steam gas turbine combined engine, characterized in that it is injected into the uppermost stream of all the rotor blade steam turbines from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water injection nozzle (59b) using the vaporization explosive force by converting the high temperature water supply heat amount to the minimum vaporization heat by converting it into high temperature water such as supercritical temperature by the combustor and heat exchanger (4) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water injection nozzle using the vaporization explosive force by converting to supercritical pressure high temperature water supply heat amount to the minimum vaporization heat by converting to high temperature water such as supercritical temperature by combustor and heat exchanger (4) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine from (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount is made close to the heat of vaporization and the vaporization explosive force is used to make all of the heat from the high-temperature water injection nozzle (59b) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of a bucket steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water injection nozzle (59b) is converted into high temperature water having a plurality of temperatures such as a supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high temperature water supply heat amount is made close to the vaporization heat and the vaporization explosive force is used. ) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  By using a combustor and heat exchanger (4), high temperature water such as a supercritical temperature is converted to high temperature water, and the high temperature water supply heat amount is made close to the minimum vaporization heat and the vaporization explosive force is used to heat the high temperature means (101). An all-rotor-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine from a high-temperature water injection nozzle (59b) that is heated to a high temperature. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), bring the supercritical pressure high temperature water supply heat close to the minimum vaporization heat and use vaporization explosive force to heat high temperature means ( 101) An all-rotor-steam gas turbine combined engine characterized in that it is jetted from the high-temperature water injection nozzle (59b) heated to a high temperature by 101) to the uppermost stream of all the rotor-blade steam gas turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount is brought close to the heat of vaporization, and the high-temperature heat (101) is heated by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine from the high-temperature water injection nozzle (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water heating means (101) using the combustor and heat exchanger (4) to convert it to high temperature water at multiple temperatures such as supercritical temperature, making the supercritical pressure high temperature water supply heat close to the heat of vaporization and utilizing the vaporization explosive force An all-blade steam gas turbine combined engine, characterized in that it is injected from the high-temperature water injection nozzle (59b) heated to a high temperature by the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  By using a combustor and heat exchanger (4), high temperature water such as a supercritical temperature is converted to high temperature water, and the high temperature water supply heat amount is made close to the minimum vaporization heat and the vaporization explosive force is used to heat the high temperature means (101). An all-rotor-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-rotor-blade steam gas turbine from a plurality of high-temperature water injection nozzles (59b) having high heating temperatures. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を最少の気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), bring the supercritical pressure high temperature water supply heat close to the minimum vaporization heat and use vaporization explosive force to heat high temperature means ( 101) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of all the blade steam gas turbines from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by 101). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount is brought close to the heat of vaporization, and the high-temperature heat (101) is heated by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized in that it is jetted from the plurality of high-temperature water spray nozzles (59b) to the uppermost stream of the entire bucket steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water heating means (101) using the combustor and heat exchanger (4) to convert it to high temperature water at multiple temperatures such as supercritical temperature, making the supercritical pressure high temperature water supply heat close to the heat of vaporization and utilizing the vaporization explosive force An all-blade steam gas turbine combined engine, characterized in that it is injected into the uppermost stream of the entire bucket steam gas turbine from a plurality of high-temperature water injection nozzles (59b) heated at a high temperature. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the amount of heat supplied to the high temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), to the minimum, the heat of vaporization This is an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-rotor-blade steam gas turbine combined engine characterized by being close to 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  It is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat amount including the recovered heat amount of the vaporization latent heat recovery device (66a) is brought close to the heat of vaporization. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring supercritical pressure high temperature water supply heat, including recovered heat of vaporization latent heat recovery unit (66a), closer to vaporization heat It is characterized by an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-rotor-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization. An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization This is a combined full-blade steam gas turbine engine characterized by injection into the uppermost stream of a full-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization. An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of a blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization This is a combined full-blade steam gas turbine engine characterized by being injected into the uppermost stream of the full-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-rotor steam gas turbine combined engine characterized by the use of vaporization explosive power. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-rotor-blade steam gas turbine combined engine characterized by utilizing vaporization explosive power close to 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and vaporization explosion. An all-blade steam gas turbine combined engine characterized by the use of power. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization This is an all-bladed steam gas turbine combined engine characterized by the use of vaporization explosive power. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-rotor-steam gas turbine combined engine characterized by utilizing the vaporization explosive force injected into the uppermost stream of the all-rotor-steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-blade steam gas turbine combined engine, which is characterized by utilizing the vaporization explosive force by being injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization. An all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force injected into the uppermost stream of the blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization This is an all-blade steam gas turbine combined engine that uses the vaporization explosive force by injecting into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force injected into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-blade steam gas turbine combined engine, which is characterized by utilizing the vaporization explosive force by being injected into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization. An all-blade steam gas turbine combined engine characterized by using the vaporization explosive force injected into the uppermost stream of the blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization All-blade steam gas turbine combined engine, which is characterized by utilizing the vaporization explosive force injected into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-blade steam gas turbine combined engine characterized by jetting from a high-temperature water jet nozzle (59b) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-rotor-blade steam gas turbine combined engine characterized by being injected from a high-temperature water injection nozzle (59b) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and vaporization explosion. An all-blade steam gas turbine combined engine characterized by jetting from a high-temperature water jet nozzle (59b) using force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization An all-rotor-blade steam gas turbine combined engine characterized by jetting from a high-temperature water jet nozzle (59b) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-blade steam gas turbine combined engine characterized by injecting into the uppermost stream of all the rotor blade steam turbines from the high-temperature water injection nozzle (59b) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all the rotor blade steam turbines from the high-temperature water injection nozzle (59b) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat from the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and explosion An all-rotor-steam gas turbine combined engine, characterized in that it is injected into the uppermost stream of all the rotor blade steam turbines from the high-temperature water injection nozzle (59b) using force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization An all-blade steam gas turbine combined engine characterized by jetting from the high temperature water injection nozzle (59b) to the uppermost stream of all the rotor blade steam turbines using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-rotor-steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all the rotor blade steam gas turbines from the high-temperature water injection nozzle (59b) using the vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-rotor-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-rotor-blade steam gas turbine from the high-temperature water injection nozzle (59b) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat from the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and explosion An all-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all the rotor blade steam gas turbines from a high-temperature water injection nozzle (59b) using force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization An all-blade steam gas turbine combined engine characterized by jetting into the uppermost stream of the entire bucket steam gas turbine from the high-temperature water injection nozzle (59b) using the vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-rotor-blade steam gas turbine combined engine characterized by being injected from a high-temperature water injection nozzle (59b) heated to a high temperature by a heating high-temperature means (101) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-blade steam gas turbine combined engine characterized by being injected from a high-temperature water injection nozzle (59b) heated to high temperature by a heating high-temperature means (101) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and vaporization explosion. An all-rotor-blade steam gas turbine combined engine characterized by jetting from a high-temperature water jet nozzle (59b) heated to a high temperature by a heating high-temperature means (101) using force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization An all-rotor-blade steam gas turbine combined engine characterized by jetting from a high-temperature water injection nozzle (59b) heated to a high temperature by a heating high-temperature means (101) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-rotor-steam gas turbine combined engine characterized by jetting into the uppermost stream of all the rotor blade steam turbines from a high-temperature water injection nozzle (59b) heated to a high temperature by the heating high-temperature means (101) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) The full-blade steam gas turbine is characterized in that it is jetted to the uppermost stream of the full-blade steam turbine from the high-temperature water injection nozzle (59b) heated to a high temperature by the heating high-temperature means (101) using vaporization explosive force. Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and vaporization explosion. An all-blade steam gas turbine combined engine characterized by jetting into the uppermost stream of all the rotor blade steam turbines from a high-temperature water injection nozzle (59b) heated to a high temperature by the heating high-temperature means (101) using force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization All-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all rotor blade steam turbines from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of the all-blade steam gas turbine from a high-temperature water injection nozzle (59b) heated to a high temperature by the heating high-temperature means (101) using vaporization explosive force . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) The moving blade steam gas is characterized in that it is injected into the uppermost stream of the entire blade steam gas turbine from the high temperature water injection nozzle (59b) heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and vaporization explosion. An all-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all the rotor blade steam gas turbines from a high-temperature water injection nozzle (59b) heated to a high temperature by a heating high-temperature means (101) using force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization Combined with all blade blade steam gas turbine, characterized in that it is jetted from the high temperature water injection nozzle (59b) heated to high temperature by the heating high temperature means (101) using vaporization explosive force to the uppermost stream of all blade blade gas gas turbines organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all-rotor-blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by a heating high-temperature means (101) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) An all-blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by a heating high-temperature means (101) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and vaporization explosion. An all-rotor-blade steam gas turbine combined engine characterized by jetting from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by a heating high-temperature means (101) using force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization An all-rotor-blade steam gas turbine combined engine characterized by jetting from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by a heating high-temperature means (101) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat Combined with all blade blade steam gas turbine, characterized in that it is injected into the uppermost stream of all blade blade steam turbines from a plurality of high temperature water injection nozzles (59b) heated to high temperature by means of heating high temperature means (101) using vaporization explosive force organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) The moving blade steam is characterized in that it is injected into the uppermost stream of the entire moving blade steam turbine from a plurality of high temperature water injection nozzles (59b) heated to a high temperature by the heating high temperature means (101) using vaporization explosive force. Gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and vaporization explosion. An all-blade steam gas turbine combined engine, characterized in that it is injected into the uppermost stream of all the rotor blade steam turbines from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by a heating high-temperature means (101) using force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization An all blade steam gas turbine characterized in that it is injected into the uppermost stream of the entire blade steam turbine from a plurality of high temperature water injection nozzles (59b) heated to high temperature by the heating high temperature means (101) using vaporization explosive force Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high-temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the high-temperature water supply heat amount, including the recovered heat amount of vaporization latent heat recovery device (66a), to the minimum, evaporating heat An all blade steam gas turbine characterized in that it is injected into the uppermost stream of the entire blade steam gas turbine from a plurality of high temperature water injection nozzles (59b) heated to a high temperature by the heating high temperature means (101) using vaporization explosive force. Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water such as supercritical temperature by combustor and heat exchanger (4), and heat of vaporization with minimum supercritical pressure high temperature water supply heat including recovered heat of vaporization latent heat recovery unit (66a) The moving blades are characterized in that they are injected into the uppermost stream of all the moving blade steam gas turbines from a plurality of high temperature water injection nozzles (59b) heated to a high temperature by the heating high temperature means (101) using vaporization explosive force. Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the heat supplied from the high-temperature water including the recovered heat of the vaporization latent heat recovery unit (66a) is brought close to the heat of vaporization and vaporization explosion. The all-blade steam gas turbine combined engine characterized by jetting into the uppermost stream of the all-blade steam gas turbine from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101) using force . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Convert to high temperature water with multiple temperatures such as supercritical temperature by combustor and heat exchanger (4), and bring the supercritical pressure high temperature water supply heat, including the recovered heat of vaporization latent heat recovery unit (66a), closer to the heat of vaporization The total moving blade steam gas is characterized in that it is injected into the uppermost stream of the entire moving blade steam gas turbine from a plurality of high temperature water injection nozzles (59b) heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by being close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is an all-rotor-blade steam gas turbine combined engine characterized by bringing the heat to vaporization heat to a minimum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized by being close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is an all-rotor-blade steam gas turbine combined engine that is characterized by being close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by being injected near the vaporization heat and injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is a full-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of the full-blade steam turbine close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized by being injected near the heat and injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is a combined full-blade steam gas turbine engine characterized by being injected near the vaporization heat into the uppermost stream of the full-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is a combined full-blade steam gas turbine engine that is characterized by being injected into the uppermost stream of the full-blade steam gas turbine close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized by being injected near the heat and injected into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is an all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by utilizing vaporization explosive power close to vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is an all-rotor-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-bladed steam gas turbine combined engine characterized by utilizing vaporization explosive power close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is an all-bladed steam gas turbine combined engine characterized by utilizing vaporization explosive power close to vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor and heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized by using vaporization explosive power by injecting into the uppermost stream of the all-blade steam turbine close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is a full-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive power by injecting it to the uppermost stream of the full-blade steam turbine with the least heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine, which is characterized by utilizing vaporization explosive power by injecting it into the uppermost stream of the all-blade steam turbine close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is a full-blade steam gas turbine combined engine characterized by using the vaporization explosive force by injecting the gas into the uppermost stream of the full-blade steam turbine close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by injecting into the uppermost stream of the all-blade steam gas turbine close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is a full-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by injecting it into the uppermost stream of the full-blade steam gas turbine with the minimum of vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by injecting it into the uppermost stream of the all-blade steam gas turbine close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is a full-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by injecting the gas into the uppermost stream of the full-blade steam gas turbine close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by being injected from a high-temperature water injection nozzle (59b) using vaporization explosive force in the vicinity of the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is an all-rotor-blade steam gas turbine combined engine characterized by being injected from the high-temperature water injection nozzle (59b) by utilizing the vaporization explosive force and approaching the minimum vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-steam gas turbine combined engine, characterized by being injected from a high-temperature water injection nozzle (59b) using vaporization explosive force close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is a full-blade steam gas turbine combined engine characterized by being injected from the high-temperature water injection nozzle (59b) using vaporization explosive force close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of all the rotor blade steam turbines from the high-temperature water injection nozzle (59b) by utilizing the vaporization explosive force in the vicinity of the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is a full-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of the full-blade steam turbine from the high-temperature water injection nozzle (59b) by utilizing the vaporization explosive force by approaching the minimum heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of all the rotor blade steam turbines from a high-temperature water injection nozzle (59b) using vaporization explosive force approaching heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is an all-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all the rotor blade steam turbines from the high-temperature water injection nozzle (59b) by using the vaporization explosive force close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all the rotor blade steam gas turbines from the high-temperature water injection nozzle (59b) using vaporization explosive force in the vicinity of the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is a full-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of the full-blade steam gas turbine from the high-temperature water injection nozzle (59b) by using the vaporization explosive force by approaching the minimum heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-rotor-blade steam gas turbine from a high-temperature water injection nozzle (59b) by using vaporization explosive force close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is an all-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of all the rotor blade steam gas turbines from the high-temperature water injection nozzle (59b) using vaporization explosive force by approaching the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-rotor-blade steam gas turbine combined engine characterized by being injected from a high-temperature water injection nozzle (59b) heated to a high temperature by a heating high-temperature means (101) using vaporization explosive force close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is a full rotor blade steam gas turbine combined engine characterized by being injected from a high temperature water injection nozzle (59b) heated to a high temperature by means of a high temperature heating means (101) using the vaporization explosive force close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-blade steam gas turbine combined engine characterized by being injected from a high-temperature water injection nozzle (59b) heated to high temperature by a heating high-temperature means (101) using vaporization explosive force approaching heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is injected from the high-temperature water injection nozzle (59b) heated to high temperature by the high temperature heating means (101) using the vaporization explosive force close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The entire moving blade is characterized in that it is injected into the uppermost stream of the entire moving blade steam turbine from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high temperature means (101) using the vaporization explosive force close to the heat of vaporization. Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass The high temperature water injection nozzle (59b), which is heated to high temperature by the heating high temperature means (101) using the vaporization explosive force with the minimum vaporization heat, is jetted to the uppermost stream of all rotor blade steam turbines. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A full blade steam gas characterized by being injected into the uppermost stream of a full blade steam turbine from a high temperature water injection nozzle (59b) heated to high temperature by a heating high temperature means (101) using vaporization explosive force close to heat Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is characterized in that it is injected into the uppermost stream of the full blade steam turbine from the high temperature water injection nozzle (59b) heated to high temperature by the high temperature heating means (101) using the vaporization explosive force close to the heat of vaporization. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The full dynamics characterized in that the high temperature water injection nozzle (59b), which is heated to high temperature by the heating high temperature means (101) by using the vaporization explosive force close to the heat of vaporization, is injected into the uppermost stream of the all blade steam gas turbine. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is injected into the uppermost stream of all the blade steam gas turbines from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force with the minimum heat of vaporization. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Whole blade steam characterized by being jetted to the uppermost stream of all blade steam gas turbines from a high temperature water injection nozzle (59b) heated to high temperature by a heating high temperature means (101) using vaporization explosive force close to heat Gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass The high temperature water injection nozzle (59b) which is heated to high temperature by the heating high temperature means (101) using the vaporization explosive force close to the heat of vaporization is jetted to the uppermost stream of all the moving blade steam gas turbines. Rotor steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-rotor-blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by a high-temperature heating means (101) using vaporization explosive force close to vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is combined with a plurality of high temperature water jet nozzles (59b) that are heated to high temperature by means of a high temperature heating means (101) using the vaporization explosive force close to the heat of vaporization. organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by a heating high-temperature means (101) using vaporization explosive force close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is a full moving blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by a heating high temperature means (101) using vaporization explosive force close to vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. In addition, it is characterized by being injected into the uppermost stream of all rotor blade steam turbines from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high temperature means (101) using vaporization explosive force close to vaporization heat. Rotor steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Can be injected into the uppermost stream of all the blade steam turbines from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force and approaching the minimum heat of vaporization. The featured all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A full moving blade characterized in that it is injected into the uppermost stream of all the moving blade steam turbines from a plurality of high temperature water injection nozzles (59b) heated to high temperature by a heating high temperature means (101) using vaporization explosive force close to heat. Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is injected into the uppermost stream of all rotor blade steam turbines from a plurality of high-temperature water injection nozzles (59b) that are heated to high temperature by the heating high temperature means (101) using vaporization explosive force close to the heat of vaporization. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. It is characterized in that it is injected into the uppermost stream of all the moving blade steam gas turbines from a plurality of high temperature water injection nozzles (59b) heated to high temperature by the heating high temperature means (101) using vaporization explosive force close to the heat of vaporization. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is injected into the uppermost stream of all the moving blade steam gas turbines from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force with the minimum heat of vaporization. This is an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Full dynamics characterized by being injected into the uppermost stream of all blade steam gas turbines from a plurality of high temperature water injection nozzles (59b) that are heated to high temperature by the heating high temperature means (101) using vaporization explosive force close to heat Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is injected into the uppermost stream of all the moving blade steam gas turbines from a plurality of high temperature water injection nozzles (59b) heated to high temperature by the heating high temperature means (101) using vaporization explosive force close to the heat of vaporization. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized in that it is close to the heat of vaporization and communicates with each high-temperature water control valve (7a). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is an all-rotor-steam gas turbine combined engine characterized in that it is connected to each high-temperature water control valve (7a) with a minimum of vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-blade steam gas turbine combined engine characterized by close contact with heat and communicating with each high-temperature water control valve (7a). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) close to the heat of vaporization, and is a full rotor blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-rotor-blade steam gas turbine combined engine characterized in that it approaches the vaporization heat and communicates with each high-temperature water control valve (7a) and injects it into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a), and is injected into the uppermost stream of all the rotor blade steam turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized in that it is brought close to heat and communicates with each high-temperature water control valve (7a) to be injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the respective high-temperature water control valves (7a) and is injected into the uppermost stream of all the blade steam turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized in that it approaches the vaporization heat and communicates with each high-temperature water control valve (7a) to inject it into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a), and is injected into the uppermost stream of all the moving blade steam gas turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized in that it is brought close to heat and communicated with each high-temperature water control valve (7a) to be injected into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a), and is injected into the uppermost stream of the whole blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-rotor-steam gas turbine combined engine characterized by close to the heat of vaporization and communicating with each high-temperature water control valve (7a) and injecting it into the uppermost stream of all the rotor blade gas turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass The full-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of the full-blade gas turbine in contact with the respective high-temperature water control valves (7a), with a minimum of vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized in that it is brought close to heat and connected to each high-temperature water control valve (7a) and injected into the uppermost stream of all the blade gas turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a), and is injected into the uppermost stream of the entire blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-rotor-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by contacting the respective high-temperature water control valves (7a) close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass This is an all-rotor-steam gas turbine combined engine characterized by utilizing the vaporization explosive force by contacting each of the high-temperature water control valves (7a) close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by contacting each high-temperature water control valve (7a) close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the respective high-temperature water control valves (7a), and uses the vaporization explosive force, and is a full moving blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized in that it uses vaporization explosive power by injecting into the uppermost stream of all the rotor blade steam turbines by approaching the respective high-temperature water control valves (7a) in the vicinity of the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a), and is injected into the uppermost stream of the whole blade steam turbine to utilize the vaporization explosive force. Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-steam gas turbine combined engine characterized by utilizing the vaporization explosive force by approaching heat and contacting each high-temperature water control valve (7a) and injecting it into the uppermost stream of the all-rotor-steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) near the heat of vaporization and injected into the uppermost stream of the whole blade steam turbine to utilize the vaporization explosive force, and the all blade steam gas turbine combined engine . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by injecting into the uppermost stream of the all-blade steam gas turbine by contacting the respective high-temperature water control valves (7a) close to the heat of vaporization . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass The full blade steam gas is characterized by utilizing the vaporization explosive force by injecting it into the uppermost stream of the full blade steam gas turbine by contacting the respective high-temperature water control valves (7a). Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-steam gas turbine combined engine characterized by utilizing the vaporization explosive force by approaching heat and contacting each high-temperature water control valve (7a) and injecting it into the uppermost stream of the all-steam steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) in the vicinity of the heat of vaporization and injected into the uppermost stream of the full blade steam gas turbine to utilize the vaporization explosive force, organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by approaching the vaporization heat and contacting each high-temperature water control valve (7a) and injecting it into the uppermost stream of the entire bucket gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass The full-blade steam gas turbine is characterized by utilizing the vaporization explosive force by injecting it into the uppermost stream of the full-blade gas turbine by contacting each of the high-temperature water control valves (7a). Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by approaching heat and contacting each high-temperature water control valve (7a) and injecting it into the uppermost stream of all the rotor blade gas turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して全動翼ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) near the heat of vaporization and injected into the uppermost stream of the whole blade gas turbine to utilize the vaporization explosive force, and the all blade blade gas gas turbine combined engine . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized in that it is in contact with each high-temperature water control valve (7a) close to the heat of vaporization and injected from the high-temperature water injection nozzle (59b) using the vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) with the minimum vaporization heat, and is injected from the high-temperature water injection nozzle (59b) using the vaporization explosive force. Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized in that it is brought close to heat and communicated with each high-temperature water control valve (7a) and injected from the high-temperature water injection nozzle (59b) using vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) near the heat of vaporization, and is injected from the high-temperature water injection nozzle (59b) using the vaporization explosive force. . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. It is characterized by being in contact with each high-temperature water control valve (7a) in the vicinity of the heat of vaporization and using the vaporization explosive force to inject the high-temperature water injection nozzle (59b) into the uppermost stream of all rotor blade steam turbines. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) with the minimum heat of vaporization, and is injected into the uppermost stream of all rotor blade steam turbines from the high-temperature water injection nozzle (59b) using the vaporization explosive force. This is an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass It is close to heat and communicates with each high-temperature water control valve (7a), and uses the vaporization explosive force to inject from the high-temperature water injection nozzle (59b) to the uppermost stream of all blade steam turbines. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) close to the heat of vaporization, and the high-temperature water injection nozzle (59b) is injected into the uppermost stream of all rotor blade steam turbines using the vaporization explosive force. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. , Close to the heat of vaporization, contact each high-temperature water control valve (7a), using the high-pressure water injection nozzle (59b) to inject to the uppermost stream of all blade steam gas turbine using the vaporization explosive force All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the respective high-temperature water control valves (7a) with the minimum heat of vaporization, and is injected into the uppermost stream of all blade steam gas turbines from the high-temperature water injection nozzle (59b) using the vaporization explosive force. It is characterized by an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Close to heat, contact each high-temperature water control valve (7a) and use the vaporization explosive force to inject from the high-temperature water injection nozzle (59b) to the uppermost stream of all rotor blade steam gas turbines. Rotor steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzle (59b) is injected into the uppermost stream of the whole blade steam gas turbine using the vaporization explosive force. The featured all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. It is characterized by being in contact with each high-temperature water control valve (7a) in the vicinity of the heat of vaporization and using the vaporization explosive force to inject the high-temperature water injection nozzle (59b) into the uppermost stream of all the blade gas turbines. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) with the minimum heat of vaporization and injected into the uppermost stream of all blade gas turbines from the high-temperature water injection nozzle (59b) using the vaporization explosive force. This is an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Full dynamics characterized by coming close to heat and contacting each high-temperature water control valve (7a) and using the vaporization explosive force to inject the high-temperature water injection nozzle (59b) to the uppermost stream of all blade gas turbines Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) close to the heat of vaporization, and the high-temperature water injection nozzle (59b) is injected into the uppermost stream of all rotor blade gas turbines using the vaporization explosive force. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. Then, the vaporization heat is brought close to the respective high-temperature water control valves (7a) and injected from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. The featured all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high-temperature water control valve (7a) with the minimum heat of vaporization, and is injected from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass It is characterized by being in contact with each high-temperature water control valve (7a) close to heat and spraying from the high-temperature water spray nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to each high temperature water control valve (7a) close to the heat of vaporization, and is injected from the high temperature water injection nozzle (59b) heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. This is an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. , Close to the heat of vaporization, contact each high-temperature water control valve (7a), using the vaporization explosive force, the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101), An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the respective high-temperature water control valves (7a) with a minimum of vaporization heat, and are all heated from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a rotor blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Close to the heat, contact each high-temperature water control valve (7a), and by using the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force, An all-rotor-blade steam gas turbine combined engine characterized by injection into the uppermost stream. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the respective high-temperature water control valves (7a) close to the heat of vaporization, and all the moving blades from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. , Close to the heat of vaporization, contact each high-temperature water control valve (7a), using the vaporization explosive force, the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101), An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the respective high-temperature water control valves (7a) with a minimum of vaporization heat, and are all heated from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of a bucket steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass All blade steam gas turbines are connected to the respective high-temperature water control valves (7a) close to heat and heated from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. All-blade steam gas turbine combined engine characterized by being injected into the uppermost stream. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the respective high-temperature water control valves (7a) close to the heat of vaporization, and all the moving blades from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. , Close to the heat of vaporization, contact each high-temperature water control valve (7a), and use the vaporization explosive force to heat all the blade gas from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the respective high-temperature water control valves (7a) with a minimum of vaporization heat, and are all heated from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a rotor blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Close to heat, contact each high-temperature water control valve (7a) and use the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-rotor-blade steam gas turbine combined engine characterized by injection into the uppermost stream. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the respective high-temperature water control valves (7a) close to the heat of vaporization, and all the moving blades from the high-temperature water injection nozzle (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-rotor-blade steam gas turbine combined engine characterized by close to the heat of vaporization and communicating with the high-temperature water pipe (6a) of each high-temperature water control valve (7a). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass The all-rotor-blade steam gas turbine combined engine characterized in that it is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with a minimum of vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-blade steam gas turbine combined engine characterized by coming close to heat and communicating with the high-temperature water pipe (6a) of each high-temperature water control valve (7a). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized in that it approaches the vaporization heat and communicates with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and injects into the uppermost stream of all the rotor blade steam turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and is injected into the uppermost stream of the all-blade steam turbine. organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized in that it is brought close to heat and communicates with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) to be injected into the uppermost stream of all the rotor blade steam turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and is injected into the uppermost stream of all the rotor blade steam turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized by being in contact with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and injecting it to the uppermost stream of all the rotor-blade steam gas turbines close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and is injected into the uppermost stream of the full-blade steam gas turbine. Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized in that it is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and injected into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) near the vaporization heat, and is injected into the uppermost stream of the full-blade steam gas turbine. . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-blade steam gas turbine combined engine characterized in that it is in contact with the high-temperature water pipe (6a) of each of the high-temperature water control valves (7a) in the vicinity of the heat of vaporization and injected into the uppermost stream of all the rotor blade gas turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and injected into the uppermost stream of all the blade gas turbines. organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-blade steam gas turbine combined engine characterized in that it is in contact with the high-temperature water pipe (6a) of each of the high-temperature water control valves (7a) and injected into the uppermost stream of all the rotor blade gas turbines close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and is injected into the uppermost stream of all the blade gas turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. An all-rotor-blade steam gas turbine combined engine characterized in that the vaporization explosive force is utilized by contacting the high-temperature water pipe (6a) of each high-temperature water control valve (7a) close to the heat of vaporization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass The all-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by contacting the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with a minimum of vaporization heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass An all-rotor-blade steam gas turbine combined engine characterized by utilizing the vaporization explosive force by contacting the high-temperature water pipe (6a) of each high-temperature water control valve (7a) close to heat. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) in close proximity to the heat of vaporization, and is an all-rotor steam gas turbine combined engine characterized by utilizing the vaporization explosive force. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. All the moving blades characterized by utilizing vaporization explosive force by approaching the high temperature water pipe (6a) of each high temperature water control valve (7a) and injecting it into the uppermost stream of all the moving blade steam turbines near the heat of vaporization Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a), and is injected into the uppermost stream of all rotor blade steam turbines to utilize the vaporization explosive force. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A full blade steam gas characterized by utilizing the vaporization explosive force by approaching the heat and contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) and injecting it into the uppermost stream of the full blade steam turbine Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気タービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) in the vicinity of the heat of vaporization, and is injected into the uppermost stream of the all blade steam turbine to utilize the vaporization explosive force. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The full motion is characterized by using vaporization explosive force by approaching the heat of vaporization and contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) and injecting it into the uppermost stream of the full blade steam gas turbine. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and is injected into the uppermost stream of all blade steam gas turbines to utilize the vaporization explosive force. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A full blade steam characterized by utilizing the vaporization explosive force by injecting into the uppermost stream of a full blade steam gas turbine by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) close to heat Gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼蒸気ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) in the vicinity of the heat of vaporization and injected into the uppermost stream of all blade steam gas turbines to use the vaporization explosive force. Rotor steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. All the moving blades characterized by utilizing the vaporizing explosive force by approaching the vaporization heat and contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) and injecting it into the uppermost stream of all the moving blade gas turbines Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and is injected into the uppermost stream of all the moving blade gas turbines to utilize the vaporization explosive force. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A full blade steam gas characterized by utilizing the vaporization explosive force by approaching heat and contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) and injecting it into the uppermost stream of the whole blade gas turbine Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して全動翼ガスタービンの最上流に噴射して気化爆発力を利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) in the vicinity of the heat of vaporization and injected into the uppermost stream of all blade gas turbines to utilize the vaporization explosive force. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The moving blades are characterized in that they approach the vaporization heat and contact the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and inject them from the high-temperature water injection nozzle (59b) using the vaporization explosive force. Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) close to the heat of vaporization, and is injected from the high-temperature water injection nozzle (59b) using the vaporization explosive force. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A full blade steam gas characterized by being in contact with the high temperature water pipe (6a) of each high temperature water control valve (7a) close to heat and injecting from the high temperature water injection nozzle (59b) using vaporization explosive force Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) close to the heat of vaporization, and is jetted from the high-temperature water injection nozzle (59b) using the vaporization explosive force. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. , Approaching the heat of vaporization, contact the high-temperature water pipe (6a) of each high-temperature water control valve (7a), and use the vaporization explosive force from the high-temperature water injection nozzle (59b) to the uppermost stream of all rotor blade steam turbines An all-blade steam gas turbine combined engine characterized by injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and by utilizing the vaporization explosive force, the high-pressure water injection nozzle (59b) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) approaching heat, it injects into the uppermost stream of all rotor blade steam turbines from the high temperature water injection nozzle (59b) using the vaporization explosive force. It is characterized by an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) close to the heat of vaporization, and the uppermost stream of all blade steam turbines from the high-temperature water injection nozzle (59b) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected into the engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. , Approaching the heat of vaporization, contact the high-temperature water pipe (6a) of each high-temperature water control valve (7a), utilizing the vaporization explosive force from the high-temperature water injection nozzle (59b), the uppermost stream of all blade steam gas turbine An all-blade steam gas turbine combined engine characterized by being injected into the engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and the entire blade steam gas turbine from the high-temperature water injection nozzle (59b) using the vaporization explosive force All-blade steam gas turbine combined engine characterized by being injected into the uppermost stream. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Close to heat, contact the high temperature water pipe (6a) of each high temperature water control valve (7a), and inject into the uppermost stream of all blade steam gas turbines from the high temperature water injection nozzle (59b) using vaporization explosive force An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) in the vicinity of the heat of vaporization, and the highest temperature of the all-blade steam gas turbine from the high-temperature water injection nozzle (59b) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injection upstream. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. , Approaching the heat of vaporization, contact the high-temperature water pipe (6a) of each high-temperature water control valve (7a), and use the vaporization explosive force from the high-temperature water injection nozzle (59b) to the uppermost stream of all rotor blade gas turbines An all-blade steam gas turbine combined engine characterized by injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and by utilizing the vaporization explosive force, the high-temperature water injection nozzle (59b) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) approaching heat, it injects into the uppermost stream of all rotor blade gas turbines from the high temperature water injection nozzle (59b) using the vaporization explosive force. It is characterized by an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) close to the heat of vaporization, and the uppermost stream of all the blade gas turbines from the high-temperature water injection nozzle (59b) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected into the engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) All-rotor-blade steam gas turbine combined engine characterized by more injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization An all-blade steam gas turbine combined engine characterized by injection from a nozzle (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) an all-blade steam gas turbine combined engine characterized by injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) A full-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a full-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization An all-blade steam gas turbine combined engine characterized by injection from the nozzle (59b) into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) an all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization An all-blade steam gas turbine combined engine characterized by being injected from the nozzle (59b) into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine from 59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization An all-blade steam gas turbine combined engine characterized by being injected from the nozzle (59b) into the uppermost stream of the all-blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of all-blade gas turbines. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) an all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ), And a combustion gas (10) is supplied to the most upstream stage of the whole blade steam gas turbine and supplied to the middle stage optimum stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization An all-rotor-blade steam gas turbine combined engine, characterized in that it is injected from the nozzle (59b) into the uppermost stream of the all-blade steam gas turbine and supplies the combustion gas (10) to the optimum middle-stream stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-rotor-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine and supplying combustion gas (10) to the middle-stage optimum stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) an all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine and supplying the combustion gas (10) to the middle stage optimum stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ), A full-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the full-blade gas turbine and supplying the combustion gas (10) to the middle-stage optimum stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization An all-rotor-steam gas turbine combined engine characterized by being injected from the nozzle (59b) into the uppermost stream of the all-blade gas turbine and supplying the combustion gas (10) to the optimum middle-stream stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine and supplying the combustion gas (10) to the optimum middle-stream stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) an all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine and supplying the combustion gas (10) to the optimum middle-stream stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ), Which is injected into the uppermost stream of the all-blade steam gas turbine, supplies the combustion gas (10) to the optimum stage in the middle stream, and is cooled with high-temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization A combined full-blade steam gas turbine, characterized in that it is injected from the nozzle (59b) into the uppermost stream of the full-blade steam gas turbine, supplied with the combustion gas (10) to the optimum stage in the middle stream, and cooled with high-temperature water (5b) organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force A full-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the full-blade steam gas turbine, supplying the combustion gas (10) to the middle stage optimum stage, and cooling with high-temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine from 59b), supplying the combustion gas (10) to the optimum middle-stream stage, and cooling with high-temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ), Which is injected into the uppermost stream of the whole blade gas turbine, supplied with the combustion gas (10) to the optimum middle stage, and cooled with high temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization An all-blade steam gas turbine combined engine characterized in that it is injected from the nozzle (59b) into the uppermost stream of the all-blade gas turbine, supplied with the combustion gas (10) to the optimum middle stage and cooled with high-temperature water (5b). . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine, supplying the combustion gas (10) to the middle stage optimum stage and cooling with high-temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine from 59b), supplying the combustion gas (10) to the middle-stream optimum stage and cooling with high-temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the whole blade steam gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to aggregate moisture. The featured all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization It is injected from the nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force It is injected into the uppermost stream of the all blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. From 59b), it is injected into the uppermost stream of the all-blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. This is an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the whole rotor blade gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to aggregate moisture All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization It is injected from the nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. It is characterized by an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force It is injected into the uppermost stream of all rotor blade gas turbines, supplied with combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into low temperature combustion gas to aggregate moisture. Rotor steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the optimum middle stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. The featured all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the full blade steam gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with hot water (5b), expanded into the low temperature combustion gas, and condensed and recovered moisture. An all-blade steam gas turbine combined engine characterized by enabling water vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization It is injected from the nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. All-blade steam gas turbine combined engine characterized by enabling condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force Injected into the uppermost stream of the all-blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high-temperature water (5b), expanded into the low-temperature combustion gas, condensed water, and condensed into a condenser An all-blade steam gas turbine combined engine characterized by enabling vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) is injected into the uppermost stream of the all-blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), expanded into the low temperature combustion gas, and condensed water An all-blade steam gas turbine combined engine characterized by enabling condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the intermediate stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture and condense An all-rotor-blade steam gas turbine combined engine characterized by enabling vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization It is injected from the nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. This is an all-bladed steam gas turbine combined engine characterized by enabling condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force Injected into the uppermost stream of all rotor blade gas turbines, supplied with combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), expanded into low temperature combustion gas to condense moisture, and condenser vacuum It is possible to feature all-rotor blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense the moisture and recover. An all-blade steam gas turbine combined engine characterized by enabling water vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the full blade steam gas turbine, the combustion gas (10) is supplied to the intermediate stage optimum stage, cooled with the high temperature water (5b), expanded into the low temperature combustion gas, and the water is condensed and CO2 is condensed. An all-blade steam gas turbine combined engine characterized by approaching zero exhaust. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization It is injected from the nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. And all-blade steam gas turbine combined engine characterized by bringing CO2 and other exhausts close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force Injected into the uppermost stream of the full-blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with hot water (5b), expanded into the low-temperature combustion gas, condensed water, and CO2 etc. An all-blade steam gas turbine combined engine, characterized by exhaust emissions approaching zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) is injected into the uppermost stream of the all-blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), expanded into the low temperature combustion gas, and condensed water An all-rotor-blade steam gas turbine combined engine characterized by bringing the exhaust gas such as CO2 close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), expanded into the low temperature combustion gas, and the water is condensed to condense the CO2 etc. All-blade steam gas turbine combined engine characterized by bringing the exhaust of the engine close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization It is injected from the nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. This is an all-blade steam gas turbine combined engine characterized by bringing the exhaust gas such as CO2 close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force Injected into the uppermost stream of all rotor blade gas turbines, supplied with combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), expanded into low temperature combustion gas, condensed moisture and exhausted CO2 etc. An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense the moisture to CO2 An all-blade steam gas turbine combined engine characterized by approaching zero exhaust. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force (59b) An all-blade steam gas turbine combined engine characterized by injection from (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected from a water injection nozzle (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) All-rotor-blade steam gas turbine combined engine characterized by more injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injection from a nozzle (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force (59b) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected from the water injection nozzle (59b) into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) A full-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a full-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injection from the nozzle (59b) into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ) A full-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a full-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization An all-blade steam gas turbine combined engine characterized by injection from the nozzle (59b) into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) an all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam turbine from (59b) and recovering heat by the vaporization latent heat recovery device (66a) after the output is generated. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. A full-blade steam gas turbine combined engine characterized in that it is injected from the water injection nozzle (59b) to the uppermost stream of the full-blade steam turbine, and heat is recovered by the vaporization latent heat recovery device (66a) after the output is generated. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ), And the combined steam and steam gas turbine combined engine is characterized in that heat is recovered by the vaporization latent heat recovery device (66a) after the output is generated. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force A full-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of a full-blade steam turbine from a nozzle (59b) and recovering heat by a vaporization latent heat recovery device (66a) after output is generated. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and is connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force. ), And the combined steam and steam gas turbine combined engine is characterized in that heat is recovered by the vaporization latent heat recovery device (66a) after the output is generated. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization A full-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of a full-blade steam turbine from a nozzle (59b) and recovering heat by a vaporization latent heat recovery device (66a) after output is generated. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam turbine and recovering heat by a vaporization latent heat recovery unit (66a) after the output is generated. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b), a full-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of a full-blade steam turbine and recovering heat by a vaporization latent heat recovery unit (66a) after generating power. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force The whole blade steam gas which is injected into the uppermost stream of the whole blade steam turbine from (59b), recovers heat by the vaporization latent heat recovery device (66a) after the output is generated, and is supplied to the combustor / heat exchanger 4 Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. Full motion is characterized in that it is injected from the water injection nozzle (59b) to the uppermost stream of the all blade steam turbine, and after the output is generated, heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the all blade steam turbine, and after the output is generated, the heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4. organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force Whole blade steam that is injected from the nozzle (59b) to the uppermost stream of the whole blade steam turbine, and is recovered by the vaporization latent heat recovery unit (66a) after the output is generated and supplied to the combustor / heat exchanger 4 Gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force ) Is injected into the uppermost stream of the all blade steam turbine, and after the output is generated, the heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4. organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization Whole blade steam that is injected from the nozzle (59b) to the uppermost stream of the whole blade steam turbine, and is recovered by the vaporization latent heat recovery unit (66a) after the output is generated and supplied to the combustor / heat exchanger 4 Gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of the all-blade steam turbine, and heat is recovered by the vaporization latent heat recovery device (66a) after the output is generated and supplied to the combustor / heat exchanger 4. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b), which is injected into the uppermost stream of the whole blade steam turbine, and after the output is generated, the heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4. Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給すると共に、需要家に温熱として供給することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force From (59b), it is injected into the uppermost stream of the whole blade steam turbine, and after generating the output, heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to the consumer as hot heat. It is characterized by an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給すると共に、需要家に温熱として供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. It is injected from the water injection nozzle (59b) to the uppermost stream of the whole rotor blade steam turbine, and after output is generated, the heat is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor / heat exchanger 4, while It can be supplied as an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給すると共に、需要家に温熱として供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the entire rotor blade steam turbine, and after output is generated, heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to the consumer as hot heat. The featured all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給すると共に、需要家に温熱として供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force It is injected from the nozzle (59b) to the uppermost stream of the entire rotor blade steam turbine, and after output is generated, heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to the consumer as hot heat. An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給すると共に、需要家に温熱として供給することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. The high temperature water injection nozzle (59b) which is brought close to the heat of vaporization and connected to the high temperature water pipe (6a) of each high temperature water control valve (7a) and heated to high temperature by the heating high temperature means (101) using the vaporization explosive force ) Is injected into the uppermost stream of the entire rotor blade steam turbine, and after output is generated, heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to the consumer as hot heat. The featured all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給すると共に、需要家に温熱として供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass High temperature water jet that is heated to high temperature by means of heating high temperature means (101) using the vaporization explosive force by contacting the high temperature water pipe (6a) of each high temperature water control valve (7a) with minimum heat of vaporization It is injected from the nozzle (59b) to the uppermost stream of the entire rotor blade steam turbine, and after output is generated, heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to the consumer as hot heat. An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給すると共に、需要家に温熱として供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass From the high-temperature water injection nozzle (59b) which is brought close to heat and communicated with the high-temperature water pipe (6a) of each high-temperature water control valve (7a) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force It is injected into the uppermost stream of all rotor blade steam turbines, and after generating power, heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to the consumer as hot heat. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より全動翼蒸気タービンの最上流に噴射し、出力発生後に気化潜熱回収器（６６ａ）により熱回収して燃焼器兼熱交換器４に供給すると共に、需要家に温熱として供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and the high-temperature water injection nozzles (101) are heated to high-temperature water injection nozzles (101) using the vaporization explosive force. 59b) is injected into the uppermost stream of all rotor blade steam turbines, and after output is generated, heat is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor / heat exchanger 4 and supplied to the consumer as hot heat. This is an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade steam gas turbine from (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected from the water injection nozzle (59b) into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected from the nozzle (59b) into the uppermost stream of the all-blade steam gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force (59b) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected from the water injection nozzle (59b) into the uppermost stream of the all-blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected from the nozzle (59b) into the uppermost stream of the all-blade gas turbine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force The whole blade steam gas turbine combined engine characterized in that it is injected into the uppermost stream of the whole blade steam gas turbine from (59b), supplied with the combustion gas (10) to the middle stage optimum stage and cooled with high temperature water (5b) . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. A full blade steam gas characterized by being injected from the water injection nozzle (59b) to the uppermost stream of the full blade steam gas turbine, supplying the combustion gas (10) to the middle stage optimum stage and cooling with high temperature water (5b) Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ), Which is injected into the uppermost stream of the all-blade steam gas turbine, supplies the combustion gas (10) to the optimum stage in the middle stream, and is cooled with high-temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force A combined full-blade steam gas turbine, characterized in that it is injected from the nozzle (59b) into the uppermost stream of the full-blade steam gas turbine, supplied with the combustion gas (10) to the optimum stage in the middle stream, and cooled with high-temperature water (5b) organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected into the uppermost stream of the all-blade gas turbine from (59b), supplying the combustion gas (10) to the optimum middle-stream stage, and cooling with high-temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. A full blade steam gas turbine characterized in that it is injected from the water injection nozzle (59b) into the uppermost stream of the whole blade gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage and cooled with high temperature water (5b). Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ), Which is injected into the uppermost stream of the whole blade gas turbine, supplied with the combustion gas (10) to the optimum middle stage, and cooled with high temperature water (5b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized in that it is injected from the nozzle (59b) into the uppermost stream of the all-blade gas turbine, supplied with the combustion gas (10) to the optimum middle stage and cooled with high-temperature water (5b). . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force From (59b), it is injected into the uppermost stream of the whole blade steam gas turbine, and the combustion gas (10) is supplied to the intermediate stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. It is characterized by an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. Water is injected from the water injection nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, the combustion gas (10) is supplied to the optimum stage of the middle flow, cooled by the high temperature water (5b), and expanded into the low temperature combustion gas to be moisture. It is characterized by agglomerating all rotor blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the whole blade steam gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to aggregate moisture. The featured all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force It is injected from the nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force From (59b), it is injected into the uppermost stream of the whole blade gas turbine, the combustion gas (10) is supplied to the optimum middle stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. This is an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. It is injected from the water injection nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to absorb moisture. An all-blade steam gas turbine combined engine characterized by agglomeration. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the whole rotor blade gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to aggregate moisture All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force It is injected from the nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. It is characterized by an all-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force From (59b), it is injected into the uppermost stream of the all-blade steam gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to aggregate moisture. This is an all-bladed steam gas turbine combined engine characterized by enabling condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. Water is injected from the water injection nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, the combustion gas (10) is supplied to the optimum stage of the middle flow, cooled by the high temperature water (5b), and expanded into the low temperature combustion gas to be moisture. An all-rotor steam gas turbine combined engine characterized by coagulating and allowing condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the full blade steam gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with hot water (5b), expanded into the low temperature combustion gas, and condensed and recovered moisture. An all-blade steam gas turbine combined engine characterized by enabling water vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force It is injected from the nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. All-blade steam gas turbine combined engine characterized by enabling condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force From (59b), it is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense the moisture. An all-blade steam gas turbine combined engine characterized by enabling condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. It is injected from the water injection nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to absorb moisture. An all-blade steam gas turbine combined engine characterized by coagulation and enabling condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the intermediate stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture and condense An all-rotor-blade steam gas turbine combined engine characterized by enabling vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集して復水器真空を可能にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force It is injected from the nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. This is an all-bladed steam gas turbine combined engine characterized by enabling condenser vacuum. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force From (59b), it is injected into the uppermost stream of the all-blade steam gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to aggregate moisture. This is an all-blade steam gas turbine combined engine characterized by bringing the exhaust gas such as CO2 close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. Water is injected from the water injection nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, the combustion gas (10) is supplied to the optimum stage of the middle flow, cooled by the high temperature water (5b), and expanded into the low temperature combustion gas to be moisture. An all-blade steam gas turbine combined engine characterized in that the exhaust gas such as CO2 is brought close to 0 by agglomerating 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the full blade steam gas turbine, the combustion gas (10) is supplied to the intermediate stage optimum stage, cooled with the high temperature water (5b), expanded into the low temperature combustion gas, and the water is condensed and CO2 is condensed. An all-blade steam gas turbine combined engine characterized by approaching zero exhaust. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼蒸気ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force It is injected from the nozzle (59b) to the uppermost stream of the whole blade steam gas turbine, supplied with the combustion gas (10) to the middle stage optimum stage, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. And all-blade steam gas turbine combined engine characterized by bringing CO2 and other exhausts close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Minimize the amount of heat supplied to the high-temperature water, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at a plurality of temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass. A plurality of high-temperature water injection nozzles that are brought into contact with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force From (59b), it is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to condense the moisture. An all-rotor-blade steam gas turbine combined engine characterized by bringing the exhaust gas such as CO2 close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を最少の、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Is connected to the high-temperature water pipe (6a) of each high-temperature water control valve (7a) with the minimum heat of vaporization, and a plurality of high temperatures heated by the high-temperature heating means (101) using the vaporization explosive force. It is injected from the water injection nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), and expanded into the low temperature combustion gas to absorb moisture. An all-blade steam gas turbine combined engine characterized by agglomerating and bringing CO2 and other exhausts close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization of high-temperature water supply heat, including the amount of heat recovered by the vaporization latent heat recovery unit (66a), which is converted to high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass A plurality of high-temperature water injection nozzles (59b) that are brought close to heat and communicated with the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) Is injected into the uppermost stream of the whole rotor blade gas turbine, the combustion gas (10) is supplied to the middle stage optimum stage, cooled with the high temperature water (5b), expanded into the low temperature combustion gas, and the water is condensed to condense the CO2 etc. All-blade steam gas turbine combined engine characterized by bringing the exhaust of the engine close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、燃料燃焼質量を低減する気化潜熱回収器（６６ａ）の回収熱量を含めて超臨界圧力高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）の高温水管（６ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より全動翼ガスタービンの最上流に噴射し、中流最適段に燃焼ガス（１０）を供給して高温水（５ｂ）で冷却し、低温燃焼ガスに膨張して水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water supply heat quantity including the heat quantity recovered from the vaporization latent heat recovery unit (66a), which is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor / heat exchanger (4) and reduces the fuel combustion mass Are connected to the high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) close to the heat of vaporization, and a plurality of high-temperature water jets heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force It is injected from the nozzle (59b) to the uppermost stream of the whole rotor blade gas turbine, supplied with the combustion gas (10) to the optimum stage of the middle flow, cooled with high temperature water (5b), and expanded into the low temperature combustion gas to condense moisture. This is an all-blade steam gas turbine combined engine characterized by bringing the exhaust gas such as CO2 close to zero. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water jets connected to the gas turbine and the respective hot water reservoirs (32a) at the most upstream of the spraying principle (91e) and heated to a high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injection from a nozzle (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force by contacting the steam gas turbine and a plurality of high-temperature water reservoirs (32a) in the most upstream of the principle of spraying (91e) An all-blade steam gas turbine combined engine characterized by being injected from an injection nozzle (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles (heated high-temperature means (101) using a gas-explosive force and heated to a high-temperature water reservoir (32a) in the uppermost stream of the gas turbine and the mist spraying principle (91e). 59b) an all-blade steam gas turbine combined engine characterized by injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles which are connected to the uppermost high-temperature water reservoir (32a) of the steam gas turbine and the spraying principle (91e) and are heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force (59b) An all-blade steam gas turbine combined engine characterized by injection from (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water jets connected to the gas turbine and the respective hot water reservoirs (32a) at the most upstream of the spraying principle (91e) and heated to a high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected from a nozzle (59b) and supplying combustion gas to an optimum middle stage and outputting it. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force by contacting the steam gas turbine and a plurality of high-temperature water reservoirs (32a) in the most upstream of the principle of spraying (91e) An all-rotor-blade steam gas turbine combined engine characterized by being injected from an injection nozzle (59b), supplying combustion gas to an optimum middle stage and outputting it. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles (heated high-temperature means (101) using a gas-explosive force and heated to a high-temperature water reservoir (32a) in the uppermost stream of the gas turbine and the mist spraying principle (91e). 59b), an all-rotor-blade steam gas turbine combined engine characterized in that combustion gas is supplied to and output from an optimum middle stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles which are connected to the uppermost high-temperature water reservoir (32a) of the steam gas turbine and the spraying principle (91e) and are heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized in that it is injected from (59b) and supplies combustion gas to the optimum middle stage and outputs it. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the amount of heat supplied to the high temperature water is brought close to the heat of vaporization. A plurality of high-temperature water injection nozzles (59b) which are connected to the uppermost high-temperature water reservoirs (32a) of the plurality of spraying principles (91e) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) All-rotor-blade steam gas turbine combined engine, which is characterized by being injected and supplying combustion gas to the optimum midstream stage for output. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And a plurality of high-temperature water injection nozzles (heated high-temperature means (101) using the vaporization explosive force and heated to high temperature water nozzles (32a) in contact with the most upstream hot water reservoirs (32a) of the plurality of spraying principles (91e) 59b), an all-rotor-blade steam gas turbine combined engine characterized in that combustion gas is supplied to and output from an optimum middle stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the amount of heat supplied to the high temperature water is brought close to the heat of vaporization. From a plurality of high-temperature water injection nozzles (59b) that are connected to the hot water reservoirs (32a) at the most upstream of the spraying principle (91e) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting and supplying combustion gas to the optimum midstream stage and outputting it. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And a plurality of high-temperature water injection nozzles (59b) which are connected to the uppermost high-temperature water reservoirs (32a) of the principle of spraying (91e) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. An all-rotor-steam gas turbine combined engine characterized in that it is more injected and supplies combustion gas to the optimum midstream stage and outputs it. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力する夫々前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water jets connected to the gas turbine and the respective hot water reservoirs (32a) at the most upstream of the spraying principle (91e) and heated to a high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by injecting and propelling forward air that is injected from a nozzle (59b) and supplies combustion gas to an optimum middle stage and outputs it. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力する夫々前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force by contacting the steam gas turbine and a plurality of high-temperature water reservoirs (32a) in the most upstream of the principle of spraying (91e) An all-blade steam gas turbine combined engine characterized by injecting propulsion by injecting forward air that is injected from an injection nozzle (59b), supplies combustion gas to an optimal middle stage, and outputs the gas. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力する夫々前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles (heated high-temperature means (101) using a gas-explosive force and heated to a high-temperature water reservoir (32a) in the uppermost stream of the gas turbine and the mist spraying principle (91e). 59b) an all-rotor-blade steam gas turbine combined engine characterized in that the combustion gas is supplied to and output from the optimum midstream stage, and the air in front is sucked and propelled for injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力する夫々前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles which are connected to the uppermost high-temperature water reservoir (32a) of the steam gas turbine and the spraying principle (91e) and are heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force (59b) An all-rotor-blade steam gas turbine combined engine characterized by sucking forward air and injecting and propelling the fuel, which is injected from (59b) and supplied to and output the combustion gas to the optimum midstream stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力する夫々前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the amount of heat supplied to the high temperature water is brought close to the heat of vaporization. A plurality of high-temperature water injection nozzles (59b) which are connected to the uppermost high-temperature water reservoirs (32a) of the plurality of spraying principles (91e) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ) A full moving blade steam gas turbine combined engine characterized in that the combustion gas is supplied to the optimum middle stage, and the combustion gas is supplied to and output from the front stage to suck and propel the air forward. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力する夫々前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And a plurality of high-temperature water injection nozzles (heated high-temperature means (101) using the vaporization explosive force and heated to high temperature water nozzles (32a) in contact with the most upstream hot water reservoirs (32a) of the plurality of spraying principles (91e) 59b) an all-rotor-blade steam gas turbine combined engine characterized in that the combustion gas is supplied to and output from the optimum midstream stage, and the air in front is sucked and propelled for injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力する夫々前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the amount of heat supplied to the high temperature water is brought close to the heat of vaporization. From a plurality of high-temperature water injection nozzles (59b) that are connected to the hot water reservoirs (32a) at the most upstream of the spraying principle (91e) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-rotor-blade steam gas turbine combined engine characterized by injecting and propelling by injecting the air in front of the fuel, supplying the combustion gas to the optimum middle stage, and outputting it. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、最適中流段に燃焼ガスを供給して出力する夫々前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And a plurality of high-temperature water injection nozzles (59b) which are connected to the uppermost high-temperature water reservoirs (32a) of the principle of spraying (91e) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized in that it is further injected and sucked and propelled by sucking forward air that is supplied to and output combustion gas to the optimum midstream stage. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water jets heated to high temperatures by the high-temperature heating means (101) using the vaporization explosive force in contact with the uppermost hot water reservoir (32a) of the steam turbine and the plurality of spraying principles (91e) An all-blade steam gas turbine combined engine characterized by being injected from a nozzle (59b) and injecting a combustion gas (10) in an annular combustion gas reservoir (9) from a spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force by contacting the steam gas turbine and a plurality of high-temperature water reservoirs (32a) in the most upstream of the principle of spraying (91e) An all-blade steam gas turbine combined engine characterized by being injected from an injection nozzle (59b) and injecting a combustion gas (10) in an annular combustion gas reservoir (9) from the principle of spraying (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles (heated high-temperature means (101) heated to high-temperature water injection nozzles (32a) utilizing the vaporization explosive force by contacting the uppermost hot water reservoir (32a) of the steam turbine and the spraying principle (91e) An all-blade steam gas turbine combined engine characterized by being injected from 59b) and injecting the combustion gas (10) in the annular combustion gas reservoir (9) from the spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles which are connected to the uppermost high-temperature water reservoir (32a) of the steam gas turbine and the spraying principle (91e) and are heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force An all-blade steam gas turbine combined engine characterized by being injected from (59b) and injecting the combustion gas (10) in the annular combustion gas reservoir (9) from the spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the supply heat quantity of the high temperature water is brought close to the heat of vaporization. A plurality of high-temperature water injection nozzles (59b) which are connected to the uppermost high-temperature water reservoirs (32a) of the plurality of spraying principles (91e) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ), And the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And a plurality of high-temperature water injection nozzles (heated high-temperature means (101) using the vaporization explosive force and heated to high temperature water nozzles (32a) in contact with the most upstream hot water reservoirs (32a) of the plurality of spraying principles (91e) An all-blade steam gas turbine combined engine characterized by being injected from 59b) and injecting the combustion gas (10) in the annular combustion gas reservoir (9) from the spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the supply heat quantity of the high temperature water is brought close to the heat of vaporization. From a plurality of high-temperature water injection nozzles (59b) that are connected to the hot water reservoirs (32a) at the most upstream of the spraying principle (91e) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-rotor-blade steam gas turbine combined engine characterized by injecting and injecting the combustion gas (10) in the annular combustion gas reservoir (9) from the spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And a plurality of high-temperature water injection nozzles (59b) which are connected to the uppermost high-temperature water reservoirs (32a) of the principle of spraying (91e) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. A full moving blade steam gas turbine combined engine characterized in that the combustion gas (10) in the annular combustion gas reservoir (9) is injected by the spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び複数の霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). In contact with the most upstream of the steam turbine and the plurality of spraying principles (91e), spraying from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using vaporization explosive force, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the principle of spraying (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). The steam gas turbine and a plurality of spray nozzles (91e) are connected to the most upstream and sprayed from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by a heating high-temperature means (101) using vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting the combustion gas (10) in the annular combustion gas reservoir (9) from the spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). In contact with the uppermost stream of the steam turbine and spraying principle (91e), the vaporized explosive force is used to inject from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101). An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the combustion gas reservoir (9) is injected from the principle of spraying (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). In contact with the most upstream of the principle of the steam gas turbine and spraying (91e), it is injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the combustion gas reservoir (9) is injected from the spraying principle (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び複数の霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the supply heat quantity of the high temperature water is brought close to the heat of vaporization. In contact with the most upstream of the plurality of spraying principles (91e), the vaporized explosive force is injected from the plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101), and annular combustion An all-blade steam gas turbine combined engine characterized by injecting combustion gas (10) in a gas reservoir (9) from the principle of spraying (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And spraying from the plurality of high temperature water injection nozzles (59b) heated to the high temperature by the heating high temperature means (101) using the vaporization explosive force, in contact with the most upstream of the plurality of spraying principles (91e), An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the combustion gas reservoir (9) is injected from the principle of spraying (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the supply heat quantity of the high temperature water is brought close to the heat of vaporization. In contact with the most upstream of the principle of spraying (91e), it is injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using vaporization explosive force, and an annular combustion gas reservoir An all-blade steam gas turbine combined engine characterized by injecting the combustion gas (10) of (9) from the principle of spraying (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). In addition, the annular combustion gas is injected from a plurality of high-temperature water injection nozzles (59b) that are heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force, in contact with the most upstream of the principle of spraying (91e). An all-blade steam gas turbine combined engine characterized by injecting combustion gas (10) in a reservoir (9) from the principle of spraying (91b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water jets heated to high temperatures by the high-temperature heating means (101) using the vaporization explosive force in contact with the uppermost hot water reservoir (32a) of the steam turbine and the plurality of spraying principles (91e) It is injected from the nozzle (59b), the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b), and the forward air is sucked and propelled by each of them. Rotor steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force by contacting the steam gas turbine and a plurality of high-temperature water reservoirs (32a) in the most upstream of the principle of spraying (91e) It is characterized by being injected from the injection nozzle (59b), injecting the combustion gas (10) in the annular combustion gas reservoir (9) from the spraying principle (91b), and sucking the front air and propelling it for injection. All-blade steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles (heated high-temperature means (101) heated to high-temperature water injection nozzles (32a) utilizing the vaporization explosive force by contacting the uppermost hot water reservoir (32a) of the steam turbine and the spraying principle (91e) 59b), the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b), and the forward moving blades are characterized by sucking forward air and propelling them for injection. Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). A plurality of high-temperature water injection nozzles which are connected to the uppermost high-temperature water reservoir (32a) of the steam gas turbine and the spraying principle (91e) and are heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force Injected from (59b), the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b), and the forward air is sucked forward and propelled by each of them. Wing steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the supply heat quantity of the high temperature water is brought close to the heat of vaporization. A plurality of high-temperature water injection nozzles (59b) which are connected to the uppermost high-temperature water reservoirs (32a) of the plurality of spraying principles (91e) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. ), The combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b), and the forward moving air is characterized by sucking forward air and propelling it forward. Gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And a plurality of high-temperature water injection nozzles (heated high-temperature means (101) using the vaporization explosive force and heated to high temperature water nozzles (32a) in contact with the most upstream hot water reservoirs (32a) of the plurality of spraying principles (91e) 59b), the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b), and the forward moving blades are characterized by sucking forward air and propelling them for injection. Steam gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the supply heat quantity of the high temperature water is brought close to the heat of vaporization. From a plurality of high-temperature water injection nozzles (59b) that are connected to the hot water reservoirs (32a) at the most upstream of the spraying principle (91e) and heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine characterized by injecting and injecting the combustion gas (10) in the annular combustion gas reservoir (9) from the spraying principle (91b) and sucking forward air by each of them Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). And a plurality of high-temperature water injection nozzles (59b) which are connected to the uppermost high-temperature water reservoirs (32a) of the principle of spraying (91e) and heated to high temperatures by the heating high-temperature means (101) using the vaporization explosive force. The entire blade steam gas is characterized in that the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b), and the air is sucked forward and propelled by each of them. Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び複数の霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). In contact with the most upstream of the steam turbine and the plurality of spraying principles (91e), spraying from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using vaporization explosive force, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b) and the front air is sucked and propelled by each of them. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). The steam gas turbine and a plurality of spray nozzles (91e) are connected to the most upstream and sprayed from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by a heating high-temperature means (101) using vaporization explosive force. An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the annular combustion gas reservoir (9) is injected from the spraying principle (91b), and the front air is sucked and propelled by each. . 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). In contact with the uppermost stream of the steam turbine and spraying principle (91e), the vaporized explosive force is used to inject from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101). An all-rotor-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the combustion gas reservoir (9) is injected by the spraying principle (91b), and the front air is sucked and propelled by each. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply calorie is brought close to the heat of vaporization, and all blades are moved by the respective high-temperature water control valves (7a). In contact with the most upstream of the principle of the steam gas turbine and spraying (91e), it is injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the combustion gas reservoir (9) is injected from the spraying principle (91b) and the front air is sucked and propelled for injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び複数の霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the supply heat quantity of the high temperature water is brought close to the heat of vaporization. In contact with the most upstream of the plurality of spraying principles (91e), the vaporized explosive force is injected from the plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101), and annular combustion An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the gas reservoir (9) is injected from the spraying principle (91b) and the front air is sucked and propelled by each. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を、気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び複数の霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply calorie is brought close to the heat of vaporization, and all blade steam gas is supplied by the respective high-temperature water control valves (7a). In contact with the most upstream of the principle of the turbine and the plurality of spray sprayers (91e), it is injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using vaporization explosive force, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the combustion gas reservoir (9) is injected from the spraying principle (91b) and the front air is sucked and propelled for injection. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気タービン及び霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  The high temperature water is converted into high temperature water such as a supercritical temperature by the combustor and heat exchanger (4), and the supply heat quantity of the high temperature water is brought close to the heat of vaporization. In contact with the most upstream of the principle of spraying (91e), it is injected from a plurality of high-temperature water injection nozzles (59b) heated to high temperature by the heating high-temperature means (101) using vaporization explosive force, and an annular combustion gas reservoir An all-blade steam gas turbine combined engine characterized by injecting the combustion gas (10) of (9) from the principle of spraying (91b) and sucking forward air and propelling it forward. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により全動翼蒸気ガスタービン及び霧吹きの原理（９１ｅ）の最上流に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、環状の燃焼ガス溜（９）の燃焼ガス（１０）を霧吹きの原理（９１ｂ）より噴射し、夫々により前方の空気を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water with multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the high-temperature water supply heat quantity is brought close to the heat of vaporization, and the full-scale blade steam gas turbine is driven by each high-temperature water control valve (7a). In addition, the annular combustion gas is injected from a plurality of high-temperature water injection nozzles (59b) that are heated to high temperature by the heating high-temperature means (101) using the vaporization explosive force, in contact with the most upstream of the principle of spraying (91e). An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) in the reservoir (9) is injected from the spraying principle (91b), and the front air is sucked and propelled by each. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high-temperature water reservoir (32a) at the uppermost stream of the blade steam turbine and the uppermost and middle hot-water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the respective high-temperature water reservoirs (32a) at the uppermost stream and the high-temperature heating means ( 101) A full moving blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by 101). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The uppermost hot water reservoir (32a) of the wing steam turbine and the uppermost and middle hot water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the hot water reservoirs (32a), and a plurality of hot waters are utilized by utilizing vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected from an injection nozzle (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high temperature water reservoir (32a) of the uppermost stream of the blade steam turbine and the hot water reservoir (32a) of the uppermost stream and the middle stream of the spraying principle (91c) are connected to the hot water reservoir (32a) of the middle stream, and the heating high temperature means (101) using vaporization explosive force. An all-rotor-blade steam gas turbine combined engine characterized by being injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) A plurality of high temperature water injection nozzles utilizing vaporization explosive force in communication with the uppermost hot water reservoir (32a) of the blade steam turbine and the uppermost and middle hot water reservoirs (32a) of the spraying principle (91c). (59b) An all-blade steam gas turbine combined engine characterized by injection from (59b). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high-temperature water reservoir (32a) at the uppermost stream of the blade steam turbine and the uppermost and middle hot-water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the respective high-temperature water reservoirs (32a) at the uppermost stream and the high-temperature heating means ( 101) All blade steam gas, characterized in that it is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by 101), and all combustion gas (10) is injected from one or more nozzles of the spraying principle (91d). Turbine coalescence engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The uppermost hot water reservoir (32a) of the wing steam turbine and the uppermost and middle hot water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the hot water reservoirs (32a), and a plurality of hot waters are utilized by utilizing vaporization explosive force. An all-blade steam gas turbine combined engine characterized by being injected from an injection nozzle (59b) and injecting all combustion gas (10) from one or more nozzles of the spraying principle (91d). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high temperature water reservoir (32a) of the uppermost stream of the blade steam turbine and the hot water reservoir (32a) of the uppermost stream and the middle stream of the spraying principle (91c) are connected to the hot water reservoir (32a) of the middle stream, and the heating high temperature means (101) using vaporization explosive force. The all-swing-blade steam gas turbine combination characterized in that it is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by one, and the entire combustion gas (10) is injected from one or more nozzles of the spraying principle (91d) organ. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) A plurality of high temperature water injection nozzles utilizing vaporization explosive force in communication with the uppermost hot water reservoir (32a) of the blade steam turbine and the uppermost and middle hot water reservoirs (32a) of the spraying principle (91c). An all-blade steam gas turbine combined engine characterized in that the entire combustion gas (10) is injected from one or more nozzles of the spraying principle (91d). 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high-temperature water reservoir (32a) at the uppermost stream of the blade steam turbine and the uppermost and middle hot-water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the respective high-temperature water reservoirs (32a) at the uppermost stream and the high-temperature heating means ( 101) is sprayed from a plurality of high-temperature water spray nozzles (59b) heated to a high temperature, and all of the combustion gas (10) is sprayed from one or more nozzles of the spraying principle (91d) to suck the water ahead. An all-blade steam gas turbine combined engine characterized by propulsion. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The uppermost hot water reservoir (32a) of the wing steam turbine and the uppermost and middle hot water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the hot water reservoirs (32a), and a plurality of hot waters are utilized by utilizing vaporization explosive force. Whole blade steam, characterized in that it is injected from the injection nozzle (59b), injects all of the combustion gas (10) from one or more nozzles of the spraying principle (91d), and sucks forward water for injection propulsion. Gas turbine combined engine. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high temperature water reservoir (32a) of the uppermost stream of the blade steam turbine and the hot water reservoir (32a) of the uppermost stream and the middle stream of the spraying principle (91c) are connected to the hot water reservoir (32a) of the middle stream, and the heating high temperature means (101) using vaporization explosive force. Injected from a plurality of high-temperature water injection nozzles (59b) heated at a high temperature by one or more, one or more nozzles of the spraying principle (91d), injecting all of the combustion gas (10), and sucking water in front of each to propel the injection An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) A plurality of high temperature water injection nozzles utilizing vaporization explosive force in communication with the uppermost hot water reservoir (32a) of the blade steam turbine and the uppermost and middle hot water reservoirs (32a) of the spraying principle (91c). An all-blade steam gas turbine characterized in that the combustion gas (10) is injected from one or more nozzles of the spraying principle (91d) and the front water is sucked and injected and propelled. Combined organization. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進し、全動翼蒸気タービン排気で浮上推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high-temperature water reservoir (32a) at the uppermost stream of the blade steam turbine and the uppermost and middle hot-water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the respective high-temperature water reservoirs (32a) at the uppermost stream and the high-temperature heating means ( 101) is sprayed from a plurality of high-temperature water spray nozzles (59b) heated to a high temperature, and all of the combustion gas (10) is sprayed from one or more nozzles of the spraying principle (91d) to suck the water ahead. An all-blade steam gas turbine combined engine characterized by propelling and propelling with all-blade steam turbine exhaust. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進し、全動翼蒸気タービン排気で浮上推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The uppermost hot water reservoir (32a) of the wing steam turbine and the uppermost and middle hot water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the hot water reservoirs (32a), and a plurality of hot waters are utilized by utilizing vaporization explosive force. Injecting from the injection nozzle (59b), injecting all of the combustion gas (10) from one or more nozzles of the spraying principle (91d), sucking forward water, and propelling the injection, An all-blade steam gas turbine combined engine characterized by levitation propulsion. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進し、全動翼蒸気タービン排気で浮上推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high temperature water reservoir (32a) of the uppermost stream of the blade steam turbine and the hot water reservoir (32a) of the uppermost stream and the middle stream of the spraying principle (91c) are connected to the hot water reservoir (32a) of the middle stream, and the heating high temperature means (101) using vaporization explosive force. Injected from a plurality of high-temperature water injection nozzles (59b) heated at a high temperature by one or more, one or more nozzles of the spraying principle (91d), injecting all of the combustion gas (10), and sucking water in front of each to propel the injection The all-blade steam gas turbine combined engine is characterized by being levitated and propelled by all-blade steam turbine exhaust. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進し、全動翼蒸気タービン排気で浮上推進することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) A plurality of high temperature water injection nozzles utilizing vaporization explosive force in communication with the uppermost hot water reservoir (32a) of the blade steam turbine and the uppermost and middle hot water reservoirs (32a) of the spraying principle (91c). Inject from (59b), inject all of the combustion gas (10) from one or more nozzles of the spraying principle (91d), suck the water in front of each, and propel it to propulsion. An all-blade steam gas turbine combined engine characterized by 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進し、燃焼ガスで水を冷却してＣＯ２等を海底などに供給することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high-temperature water reservoir (32a) at the uppermost stream of the blade steam turbine and the uppermost and middle hot-water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the respective high-temperature water reservoirs (32a) at the uppermost stream and the high-temperature heating means ( 101) is sprayed from a plurality of high-temperature water spray nozzles (59b) heated to a high temperature, and all of the combustion gas (10) is sprayed from one or more nozzles of the spraying principle (91d) to suck the water ahead. An all-rotor blade steam gas turbine combined engine characterized by propelling and cooling water with combustion gas and supplying CO2 etc. to the seabed. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び複数の霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進し、燃焼ガスで水を冷却してＣＯ２等を海底などに供給することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The uppermost hot water reservoir (32a) of the wing steam turbine and the uppermost and middle hot water reservoirs (32a) of the plurality of spraying principles (91c) are connected to the hot water reservoirs (32a), and a plurality of hot waters are utilized by utilizing vaporization explosive force. Injected from the injection nozzle (59b), injected all of the combustion gas (10) from one or more nozzles of the spraying principle (91d), sucked forward water, respectively, propelled and propelled, cooled the water with the combustion gas All-blade steam gas turbine combined engine characterized by supplying CO2 etc. to the seabed. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進し、燃焼ガスで水を冷却してＣＯ２等を海底などに供給することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) The high temperature water reservoir (32a) of the uppermost stream of the blade steam turbine and the hot water reservoir (32a) of the uppermost stream and the middle stream of the spraying principle (91c) are connected to the hot water reservoir (32a) of the middle stream, and the heating high temperature means (101) using vaporization explosive force. Injected from a plurality of high-temperature water injection nozzles (59b) heated at a high temperature by one or more, one or more nozzles of the spraying principle (91d), injecting all of the combustion gas (10), and sucking water in front of each to propel the injection An all-blade steam gas turbine combined engine characterized by cooling water with combustion gas and supplying CO2 etc. to the seabed. 燃焼器兼熱交換器（４）により超臨界温度等複数温度の高温水に変換して、超臨界圧力高温水供給熱量を気化熱に近付けて夫々の高温水加減弁（７ａ）により、全動翼蒸気タービンの最上流の高温水溜（３２ａ）及び霧吹きの原理（９１ｃ）の最上流及び中流の夫々の高温水溜（３２ａ）に連絡して、気化爆発力を利用して複数の高温水噴射ノズル（５９ｂ）より噴射し、霧吹きの原理（９１ｄ）の１以上のノズルより燃焼ガス（１０）全部を噴射して夫々前方の水を吸引して噴射推進し、燃焼ガスで水を冷却してＣＯ２等を海底などに供給することが特徴の全動翼蒸気ガスタービン合体機関。  It is converted into high-temperature water at multiple temperatures such as supercritical temperature by the combustor and heat exchanger (4), and the supercritical pressure high-temperature water supply heat is brought close to the heat of vaporization, and each high-temperature water control valve (7a) A plurality of high temperature water injection nozzles utilizing vaporization explosive force in communication with the uppermost hot water reservoir (32a) of the blade steam turbine and the uppermost and middle hot water reservoirs (32a) of the spraying principle (91c). (59b), the combustion gas (10) is entirely injected from one or more nozzles of the spraying principle (91d), the water in front is sucked and propelled, and the water is cooled with the combustion gas to reduce CO2. All-wheel blade steam gas turbine combined engine characterized by supplying 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A full moving blade characterized by injecting high-temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) Steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is characterized in that supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature is jetted from a high temperature water jet nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high temperature means (101). All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  It is characterized in that high temperature water (5b) having a plurality of temperatures such as supercritical temperature is jetted from a high temperature water jet nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by a heating high temperature means (101). Rotor steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature can be injected from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by a heating high temperature means (101). The featured all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Then, an all-blade steam gas turbine combined engine characterized by acceleration like machine gun bullets and snowstorms. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. All-blade steam gas turbine combined engine, which is characterized by accelerating in the nozzle like machine gun bullets or snowstorms. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force An all-blade steam gas turbine combined engine characterized by accelerating in the nozzle like a machine gun bullet or snowstorm. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). An all-blade steam gas turbine combined engine characterized by accelerating in the nozzle like a bullet of a machine gun or a snowstorm. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Is an all-bladed steam gas turbine combined engine that accelerates like a bullet or snowstorm of a machine gun and accelerates like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. The all-blade steam gas turbine combined engine is characterized in that it accelerates like a bullet or snowstorm of a machine gun inside the nozzle and accelerates like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force An all-bladed steam gas turbine combined engine that accelerates like a bullet or snowstorm of a machine gun inside the nozzle and accelerates like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). An all-blade steam gas turbine combined engine characterized by accelerating like a bullet or snowstorm of a machine gun inside the nozzle by explosive force and accelerating like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Is an all-bladed steam gas turbine combined engine that accelerates like a bullet of a machine gun or a snowstorm and accelerates like a shot rocket or a snowstorm outside the nozzle to optimally use latent heat of vaporization. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. This is an all-rotor steam gas turbine combined engine that accelerates like a bullet or snowstorm of a machine gun inside the nozzle and accelerates like a shot rocket or snowstorm outside the nozzle to optimally use the latent heat of vaporization. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force An all-rotor steam gas turbine combined engine that accelerates like a bullet or snowstorm of a machine gun inside the nozzle and accelerates like a shot rocket or snowstorm outside the nozzle to optimally use the latent heat of vaporization. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). All-blade steam gas turbine combined with the feature that it accelerates like a bullet of a machine gun or blowing snow inside the nozzle by explosive force and accelerates like a shot rocket or snowstorm outside the nozzle to optimally use the latent heat of vaporization organ. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. The all-blade steam gas turbine combined engine is characterized in that it accelerates like a bullet of a machine gun or a snowstorm, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects it to all the rotor blades. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. The all-blade steam gas turbine combined engine is characterized in that it accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects it to all the rotor blades. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force An all-blade steam gas turbine combined engine that accelerates like a bullet or snowstorm of a machine gun inside the nozzle and accelerates like a shot rocket or snowstorm outside the nozzle and injects it to all the rotor blades. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). All-blade steam gas turbine combined with the feature that it accelerates like a bullet of a machine gun or snowstorm inside the nozzle by explosive force, and accelerates like a shot rocket or snowstorm outside the nozzle and injects it to all rotor blades organ. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. The all-blade steam gas turbine combined engine is characterized in that it accelerates like a bullet of a machine gun or a snowstorm, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects it into the uppermost stream of all the rotor blades. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. All-blade steam gas turbine is characterized in that it accelerates like a bullet of a machine gun or a snowstorm inside the nozzle, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects it to the uppermost stream of all the blades Combined organization. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force All-blade steam gas turbine combination that accelerates like a bullet or snowstorm of a machine gun inside the nozzle and accelerates like a shot rocket or snowstorm outside the nozzle and injects it to the most upstream of all the rotor blades organ. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Full-wing blade steam characterized by accelerating like a bullet or snowstorm of a machine gun inside the nozzle by explosive force and accelerating like a shot rocket or snowstorm outside the nozzle and spraying it to the uppermost stream of all the moving blades Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerates like machine gun bullets and snowstorms, and accelerates like shot rockets and snowstorms outside the nozzle and injects into the most upstream of all blade gas turbines organ. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a machine gun bullet or snowstorm inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and jets into the uppermost stream of all blade gas turbines Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force All blade steam gas is characterized by accelerating inside the nozzle like a bullet of a machine gun or blowing snow, and accelerating like a shot rocket or snowstorm outside the nozzle and injecting it into the uppermost stream of all blade gas turbines Turbine coalescence engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Full dynamics characterized by accelerating like a bullet or snowstorm of a machine gun inside the nozzle due to explosive force, and accelerating like a shot rocket or snowstorm outside the nozzle and injecting it to the uppermost stream of all blade gas turbines Wing steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Is a full-blade steam gas turbine that is accelerated like a bullet of a machine gun or a snowstorm, and is accelerated like a shot rocket or a snowstorm outside the nozzle and injected into the uppermost stream of the full-blade steam gas turbine. Combined organization. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a machine gun bullet or snowstorm inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects into the uppermost stream of all blade steam gas turbine Steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Whole blade steam, which is characterized by accelerating inside the nozzle like a bullet of a machine gun or blowing snow, and accelerating like a shot rocket or blowing snow outside the nozzle and injecting it into the uppermost stream of a full blade steam gas turbine Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). The explosive force accelerates inside the nozzle like a bullet of a machine gun or a snowstorm, and accelerates like a shot rocket or snowstorm outside the nozzle and injects it to the uppermost stream of a full blade steam gas turbine. Rotor steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerates like machine gun bullets and snowstorms, and accelerates like shot rockets and snowstorms outside the nozzle and injects into the most upstream of all rotor blade steam turbines organ. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a gun bullet or snowstorm inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and sprays it to the uppermost stream of all blade steam turbine. Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force All blade steam gas is characterized by accelerating inside the nozzle like a bullet of a machine gun or blowing snow, and accelerating like a shot rocket or snowstorm outside the nozzle and injecting it into the uppermost stream of the all blade steam turbine. Turbine coalescence engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Full dynamics characterized by accelerating like nozzles and snowstorms of machine guns inside nozzles by explosive force, and accelerating like shot rockets and snowstorms outside nozzles and injecting into the uppermost stream of all blade steam turbines Wing steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. In this case, the full-blade steam is characterized in that it accelerates like a bullet of a machine gun or a snowstorm, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects downstream from the most upstream of the full-blade gas turbine. Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. It accelerates like a bullet of a machine gun or snowstorm inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade gas turbines. Rotor steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It is accelerated like a bullet or snowstorm of a machine gun inside the nozzle, and accelerated like a shot rocket or snowstorm outside the nozzle and injected sequentially downstream from the uppermost stream of the all blade gas turbine. Wing steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Accelerates like a bullet or snowstorm of a machine gun inside the nozzle due to explosive force, and accelerates like a shot rocket or snowstorm outside the nozzle and injects sequentially downstream from the uppermost stream of all rotor blade gas turbines All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. , Which accelerates like a bullet of a machine gun or a snowstorm, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of the all-blade steam gas turbine. Steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerating inside the nozzle like a bullet of a machine gun or snowstorm, etc., and accelerating like a shot rocket or snowstorm outside the nozzle and injecting it sequentially downstream from the uppermost stream of the all blade steam gas turbine All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of the full blade steam gas turbine. Rotor steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). The explosive force accelerates like a bullet of a machine gun or snowstorm inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and sequentially injects downstream from the uppermost stream of the all blade steam gas turbine. The featured all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. In this case, the full-blade steam is characterized in that it accelerates like a bullet of a machine gun or a snowstorm, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects sequentially downstream from the uppermost stream of the full-blade steam turbine. Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerating inside the nozzle like a bullet of a machine gun or blowing snow, and accelerating like a shot rocket or blowing snow outside the nozzle and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines. Rotor steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It is accelerated like a bullet or snowstorm of a machine gun inside the nozzle, and accelerated like a shot rocket or snowstorm outside the nozzle and injected downstream from the uppermost stream of all rotor blade steam turbines. Wing steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Accelerates like a bullet of a machine gun or snowstorm inside the nozzle due to explosive force, and accelerates like a shot rocket or snowstorm outside the nozzle and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject them downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. The featured all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a bullet of a machine gun or a snowstorm inside the nozzle, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output An all-blade steam gas turbine combined engine characterized by 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output It is characterized by an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and outside the nozzle accelerates like a shot rocket or snowstorm, etc. It is characterized by the generation of an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all blade steam gas turbines to generate rotational output. This is an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside of the nozzle like a shot rocket or snowstorm, etc. An all-blade steam gas turbine combined engine characterized by the generation. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output An all-blade steam gas turbine combined engine characterized by 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). The explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside the nozzle like a shot rocket or snowstorm, and then injects and rotates sequentially from the uppermost stream of the all blade steam gas turbine. An all-blade steam gas turbine combined engine characterized by generating output. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output. The featured all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a machine gun bullet or snowstorm inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output An all-blade steam gas turbine combined engine characterized by 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output It is characterized by an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects it downstream from the most upstream of all rotor blade steam turbines for rotation output It is characterized by the generation of an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to rotate to adiabatic expansion atmospheric pressure. It is characterized by the generation of an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerate like a machine gun bullet or snowstorm inside the nozzle, and accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam turbines to adiabatic expansion atmospheric pressure An all-blade steam gas turbine combined engine characterized by generating rotational output up to. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized by generating rotational output. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines for adiabatic expansion An all-blade steam gas turbine combined engine characterized by generating rotational output up to atmospheric pressure. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to rotate to adiabatic expansion atmospheric pressure. And an all-rotor-steam gas turbine combined engine characterized in that the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a). 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerate like a machine gun bullet or snowstorm inside the nozzle, and accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam turbines to adiabatic expansion atmospheric pressure The all-rotor-blade steam gas turbine combined engine characterized in that the rotation output is generated until the vaporization latent heat recovery unit (66a) recovers the vaporization latent heat. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to the adiabatic expansion atmospheric pressure. An all-rotor-steam gas turbine combined engine characterized in that it generates rotational output and recovers the latent heat of vaporization with a vaporization latent heat recovery unit (66a). 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines for adiabatic expansion An all-rotor-blade steam gas turbine combined engine characterized by generating rotational output up to atmospheric pressure and recovering the latent heat of vaporization by the vaporization latent heat recovery unit (66a). 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to rotate to adiabatic expansion atmospheric pressure. And an all-blade steam gas turbine combined engine that collects the latent heat of vaporization with a vaporization latent heat recovery unit (66a) and supplies it to the combustor and heat exchanger (4) of the full blade gas turbine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerate like a machine gun bullet or snowstorm inside the nozzle, and accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam turbines to adiabatic expansion atmospheric pressure The combined rotary blade steam gas turbine is characterized in that the rotation output is generated until the latent heat of vaporization is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor and heat exchanger (4) of the full blade gas turbine. organ. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized in that it generates rotational output, collects the vaporization latent heat with a vaporization latent heat recovery unit (66a), and supplies it to the combustor and heat exchanger (4) of the all blade gas turbine. . 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines for adiabatic expansion Total moving blade steam gas, characterized in that it generates rotational output up to atmospheric pressure, recovers the latent heat of vaporization with a vaporization latent heat recovery unit (66a), and supplies it to the combustor and heat exchanger (4) of the total blade gas turbine. Turbine coalescence engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to rotate to adiabatic expansion atmospheric pressure. And the combined latent steam heat turbine (66a) recovers the latent heat of vaporization and supplies it to the combustor and heat exchanger (4) of the full rotor blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerate like a machine gun bullet or snowstorm inside the nozzle, and accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam turbines to adiabatic expansion atmospheric pressure The rotary blade steam gas turbine is characterized in that the rotational output is generated until the vaporization latent heat recovery unit (66a) recovers the vaporization latent heat and supplies it to the combustor / heat exchanger (4) of the full blade steam gas turbine. Combined organization. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to the adiabatic expansion atmospheric pressure. Combined with all-blade steam gas turbine, characterized in that it generates rotational output, collects latent heat of vaporization with a vaporization latent heat recovery unit (66a), and supplies it to the combustor and heat exchanger (4) of the full blade steam gas turbine organ. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines for adiabatic expansion Full rotor blade steam characterized by generating rotational output to atmospheric pressure, recovering latent heat of vaporization with a vaporization latent heat recovery device (66a) and supplying it to the combustor and heat exchanger (4) of the full blade steam gas turbine Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to rotate to adiabatic expansion atmospheric pressure. The whole blade steam is characterized in that the latent heat of vaporization is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor and heat exchanger (4) of the full blade gas turbine to be heated to high temperature water. Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerate like a machine gun bullet or snowstorm inside the nozzle, and accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam turbines to adiabatic expansion atmospheric pressure The rotation output is generated until the vaporization latent heat recovery unit (66a) recovers the vaporization latent heat and supplies it to the combustor and heat exchanger (4) of the whole rotor blade gas turbine to produce heated high-temperature water. Rotor steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to the adiabatic expansion atmospheric pressure. It is characterized by generating rotational output, recovering latent heat of vaporization with a vaporization latent heat recovery unit (66a) and supplying it to a combustor and heat exchanger (4) of a full blade gas turbine to produce heated high-temperature water. Wing steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines for adiabatic expansion Rotational output is generated up to atmospheric pressure, and the latent heat of vaporization is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor and heat exchanger (4) of the all blade gas turbine to produce heated high-temperature water. All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to rotate to adiabatic expansion atmospheric pressure. And the latent heat of vaporization is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor and heat exchanger (4) of the full blade steam gas turbine to be heated high temperature water. Steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerate like a machine gun bullet or snowstorm inside the nozzle, and accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam turbines to adiabatic expansion atmospheric pressure The rotation output is generated until the vaporization latent heat recovery unit (66a) recovers the vaporization latent heat and supplies it to the combustor and heat exchanger (4) of the all blade steam gas turbine to produce heated high-temperature water. All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to the adiabatic expansion atmospheric pressure. It is characterized by generating a rotating output, recovering the latent heat of vaporization by the vaporization latent heat recovery unit (66a) and supplying it to the combustor and heat exchanger (4) of the whole blade steam gas turbine to form heated high temperature water. Rotor steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines for adiabatic expansion Rotational output is generated up to atmospheric pressure, and the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to be heated to high temperature water. The featured all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to rotate to adiabatic expansion atmospheric pressure. The vaporization latent heat is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor and heat exchanger (4) of the whole blade gas turbine to be heated high-temperature water, and each high-temperature water control valve (7a All-blade steam gas turbine combined engine characterized by 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerate like a machine gun bullet or snowstorm inside the nozzle, and accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam turbines to adiabatic expansion atmospheric pressure Rotational output is generated, and the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor and heat exchanger (4) of the all blade gas turbine to be heated high temperature water. An all-blade steam gas turbine combined engine characterized by communicating with a valve (7a). 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to the adiabatic expansion atmospheric pressure. Rotational output is generated, and the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor and heat exchanger (4) of the all blade gas turbine to be heated high temperature water. An all-blade steam gas turbine combined engine characterized by contacting (7a). 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines for adiabatic expansion Rotational output is generated up to atmospheric pressure, and the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor and heat exchanger (4) of the all blade gas turbine to be heated high temperature water. An all-blade steam gas turbine combined engine characterized by communicating with a water control valve (7a). 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerate like machine gun bullets and snowstorms, etc., and accelerate outside shots like shot rockets and snowstorms, and inject downstream from the uppermost stream of all rotor blade steam turbines to rotate to adiabatic expansion atmospheric pressure. And the vaporization latent heat is recovered by the vaporization latent heat recovery device (66a) and supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to be heated high temperature water. An all-blade steam gas turbine combined engine characterized by contacting 7a). 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerate like a machine gun bullet or snowstorm inside the nozzle, and accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam turbines to adiabatic expansion atmospheric pressure Rotational output is generated, and the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to be heated high temperature water. An all-rotor-steam gas turbine combined engine characterized by communicating with the control valve (7a). 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force It accelerates like a bullet or snowstorm of a machine gun inside the nozzle, and accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade steam turbines to the adiabatic expansion atmospheric pressure. Rotational output is generated, and the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor / heat exchanger (4) of the all blade steam gas turbine to be heated high temperature water. An all-blade steam gas turbine combined engine characterized by communicating with a valve (7a). 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines for adiabatic expansion Rotational output is generated up to atmospheric pressure, and the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to be heated high temperature water. An all-rotor-blade steam gas turbine combined engine characterized by communicating with a high-temperature water control valve (7a). 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerates like machine gun bullets and snowstorms, etc., and accelerates like a shot rocket and snowstorms outside the nozzle and injects downstream from the most upstream of all rotor blade gas turbines to generate rotational output, optimal An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) to the middle stage. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a bullet of a machine gun or a snowstorm inside the nozzle, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output And an all-blade steam gas turbine combined engine characterized by supplying the combustion gas (10) to the optimum middle stage. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) to the optimum midstream stage. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and outside the nozzle accelerates like a shot rocket or snowstorm, etc. And an all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) to the optimum midstream stage. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Then, it accelerates like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of the all blade steam gas turbine to generate rotational output, An all-rotor-blade steam gas turbine combined engine characterized by supplying combustion gas (10) to the optimum middle stage. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside of the nozzle like a shot rocket or snowstorm, etc. An all-rotor-steam gas turbine combined engine that is characterized in that it generates and supplies combustion gas (10) to the optimum midstream stage. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output And an all-blade steam gas turbine combined engine characterized by supplying the combustion gas (10) to the optimum middle stage. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). The explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside the nozzle like a shot rocket or snowstorm, and then injects and rotates sequentially from the uppermost stream of the all blade steam gas turbine. An all-rotor-steam gas turbine combined engine characterized by generating an output and supplying combustion gas (10) to the optimum middle stage. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerates like machine gun bullets and snowstorms, etc., and accelerates like a shot rocket and snowstorms outside the nozzle and injects downstream from the most upstream of all rotor blade gas turbines to generate rotational output, optimal An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the middle flow stage and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a bullet of a machine gun or a snowstorm inside the nozzle, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output An all-rotor-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimum midstream stage and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimum middle stage and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and outside the nozzle accelerates like a shot rocket or snowstorm, etc. The all-blade steam gas turbine combined engine is characterized in that the combustion gas (10) is supplied to the optimum middle stage and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Then, it accelerates like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of the all blade steam gas turbine to generate rotational output, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimum midstream stage and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside of the nozzle like a shot rocket or snowstorm, etc. An all-rotor-blade steam gas turbine combined engine characterized in that it is generated and supplied with combustion gas (10) to the optimum midstream stage and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output An all-rotor-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimum midstream stage and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). The explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside the nozzle like a shot rocket or snowstorm, and then injects and rotates sequentially from the uppermost stream of the all blade steam gas turbine. An all-rotor-blade steam gas turbine combined engine characterized by generating an output, supplying combustion gas (10) to the optimum middle-stream stage, and cooling with high-temperature water. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerates like machine gun bullets and snowstorms, etc., and accelerates like a shot rocket and snowstorms outside the nozzle and injects downstream from the most upstream of all rotor blade gas turbines to generate rotational output, optimal An all-blade steam gas turbine combined engine characterized in that combustion gas (10) is supplied to the middle stage and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a bullet of a machine gun or a snowstorm inside the nozzle, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimum middle stage and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimum middle stage and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and outside the nozzle accelerates like a shot rocket or snowstorm, etc. The all-blade steam gas turbine combined engine is characterized in that the combustion gas (10) is supplied to the optimum midstream stage and is cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Then, it accelerates like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of the all blade steam gas turbine to generate rotational output, An all-rotor-blade steam gas turbine combined engine characterized in that combustion gas (10) is supplied to an optimal middle stage and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside of the nozzle like a shot rocket or snowstorm, etc. An all-rotor-blade steam gas turbine combined engine characterized by generating combustion output (10) in an optimal midstream stage and generating rotational output by cooling with high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimum middle stage and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). The explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside the nozzle like a shot rocket or snowstorm, and then injects and rotates sequentially from the uppermost stream of the all blade steam gas turbine. An all-rotor-blade steam gas turbine combined engine characterized by generating an output, supplying a combustion gas (10) to an optimum midstream stage and cooling with high-temperature water to generate a rotational output. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerates like machine gun bullets and snowstorms, etc., and accelerates like a shot rocket and snowstorms outside the nozzle and injects downstream from the most upstream of all rotor blade gas turbines to generate rotational output, optimal An all-rotor-steam gas turbine combined engine characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as a core in the process of supplying combustion gas (10) to the middle stage and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a bullet of a machine gun or a snowstorm inside the nozzle, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output In addition, the entire blade steam gas turbine is characterized in that the combustion gas (10) is supplied to the optimum middle stage, cooled by high temperature water, and moisture is condensed using the adiabatic expansion low temperature combustion gas as a core in the process of generating the rotational output. Combined organization. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. Combined with a moving blade steam gas turbine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of supplying combustion gas (10) to the optimum middle stage and cooling with high-temperature water to generate rotational output organ. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and outside the nozzle accelerates like a shot rocket or snowstorm, etc. All-blade steam characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of generating combustion power (10) to the optimum middle stage and cooling with high-temperature water to generate rotational output Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Then, it accelerates like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of the all blade steam gas turbine to generate rotational output, An all-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of supplying combustion gas (10) to the optimum middle stage and cooling with high-temperature water to generate rotational output . 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside of the nozzle like a shot rocket or snowstorm, etc. A full moving blade steam gas characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of generating and supplying rotation gas by supplying combustion gas (10) to the optimum middle stage and cooling with high-temperature water Turbine coalescence engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output In addition, the entire blade steam gas turbine is characterized in that the combustion gas (10) is supplied to the optimum middle stage, cooled by high temperature water, and moisture is condensed using the adiabatic expansion low temperature combustion gas as a core in the process of generating the rotational output. Combined organization. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). The explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside the nozzle like a shot rocket or snowstorm, and then injects and rotates sequentially from the uppermost stream of the all blade steam gas turbine. All rotor blades characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of generating output, supplying combustion gas (10) to the optimum middle stage and cooling with high-temperature water to generate rotational output Steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Accelerates like machine gun bullets and snowstorms, etc., and accelerates like a shot rocket and snowstorms outside the nozzle and injects downstream from the most upstream of all rotor blade gas turbines to generate rotational output, optimal It is characterized by supplying combustion gas (10) to the middle stage and cooling with high-temperature water to agglomerate moisture in the process of adiabatic expansion low-temperature combustion gas in the process of generating rotational output and bring exhaust such as CO2 close to zero All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates like a bullet of a machine gun or a snowstorm inside the nozzle, and accelerates like a shot rocket or a snowstorm outside the nozzle and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output In the process of supplying combustion gas (10) to the optimum middle stage and cooling with high-temperature water to generate rotational output, agglomerates moisture with the adiabatic expansion low-temperature combustion gas as the core and brings CO2 and other exhausts close to zero. This is an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. In the process of supplying combustion gas (10) to the optimum middle stage and cooling with high temperature water to generate rotational output, agglomerates moisture with the adiabatic expansion low temperature combustion gas as the core and brings CO2 and other exhausts close to zero. The featured all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). Explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and outside the nozzle accelerates like a shot rocket or snowstorm, etc. In the process of supplying combustion gas (10) to the optimal middle stage and cooling with high temperature water to generate rotational output, moisture agglomerates with the adiabatic expansion low temperature combustion gas as the core and exhausts CO2 etc. to zero An all-blade steam gas turbine combined engine characterized by the approach. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) using a spraying principle (91e) heated to a high temperature by the heating high temperature means (101) is used to inject high temperature water (5b) at a plurality of temperatures such as a supercritical temperature into the nozzle by vaporization explosive force. Then, it accelerates like a bullet or snowstorm of a machine gun, accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of the all blade steam gas turbine to generate rotational output, A feature is that the combustion gas (10) is supplied to the optimum middle stage, cooled by high temperature water, and the agglomeration of water with the adiabatic expansion low temperature combustion gas as the core in the process of generating the rotation output brings CO2 and other exhausts close to zero. All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) at multiple temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) using the spraying principle (91e) heated to high temperature by the heating high-temperature means (101) to evaporate and explode. Accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside of the nozzle like a shot rocket or snowstorm, etc. In the process of generating and supplying the combustion gas (10) to the optimum middle stage and cooling with high temperature water to generate the rotational output, the adiabatic expansion low temperature combustion gas is condensed into moisture and the exhaust gas such as CO2 is brought close to zero. It is characterized by an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from a high-temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to high temperature by the heating high-temperature means (101), and vaporized explosive force Accelerates like a machine gun bullet or snowstorm inside the nozzle, accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output In the process of supplying combustion gas (10) to the optimum middle stage and cooling with high-temperature water to generate rotational output, agglomerates moisture with the adiabatic expansion low-temperature combustion gas as the core and brings CO2 and other exhausts close to zero. This is an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の霧吹きの原理（９１ｅ）を利用した高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Vaporization is performed by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b) using a plurality of spraying principles (91e) heated to a high temperature by the heating high temperature means (101). The explosive force accelerates inside the nozzle like a bullet of a machine gun or snowstorm, and accelerates outside the nozzle like a shot rocket or snowstorm, and then injects and rotates sequentially from the uppermost stream of the all blade steam gas turbine. In the process of generating output, supplying combustion gas (10) to the optimum middle stage and cooling with high-temperature water to generate rotational output, moisture agglomerates using the adiabatic expansion low-temperature combustion gas as the core and exhausts CO2 etc. to 0 An all-rotor-blade steam gas turbine combined engine characterized by being close to 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that high temperature water (5b) having a plurality of temperatures such as supercritical temperature is injected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101). 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) having a plurality of temperatures such as supercritical temperature is injected from a high-temperature water injection nozzle (59b) heated to high temperature by a heating high-temperature means (101). 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized by injecting high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by a heating high-temperature means (101). 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A full moving blade steam gas turbine combination characterized by injecting supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature from a plurality of high temperature water injection nozzles (59b) heated to a high temperature by a heating high temperature means (101) organ. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. This is an all-bladed steam gas turbine combined engine characterized by acceleration. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by acceleration like a snowstorm. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-wheel blade steam gas turbine combined engine characterized by acceleration like 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by acceleration like bullets and snowstorms. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. All-blade steam gas turbine combined engine characterized by acceleration like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. This is an all-bladed steam gas turbine combined engine that accelerates like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-bladed steam gas turbine combined engine that accelerates like a bullet or snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. The all-bladed steam gas turbine combined engine is characterized by the fact that it accelerates like a shot rocket or snowstorm outside the nozzle and optimally uses the latent heat of vaporization. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle to optimally use the latent heat of vaporization. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket and blowing snow outside the nozzle and optimally utilizing the latent heat of vaporization. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a bullet or snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle to optimally use latent heat of vaporization. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm outside the nozzle and spraying to all the rotor blades. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle and injects it into all the rotor blades. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket and accelerating like a shot rocket or snowstorm outside the nozzle. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a bullet or snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle and injects it to all the rotor blades. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. The all-blade steam gas turbine combined engine is characterized in that it is accelerated like a shot rocket or snowstorm outside the nozzle and injected into the uppermost stream of all the rotor blades. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle and injects it into the uppermost stream of all the rotor blades. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine, which is characterized by being accelerated like a shot rocket and blowing snow outside the nozzle and injected into the uppermost stream of all the rotor blades. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-rotor steam gas turbine combined engine that accelerates like a bullet or snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle and injects it into the uppermost stream of all the rotor blades. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. The all-blade steam gas turbine combined engine is characterized in that it is accelerated like a shot rocket or snowstorm outside the nozzle and injected into the uppermost stream of the all-blade gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-rotor steam gas turbine combined engine that accelerates like a snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle and injects it into the uppermost stream of all the rotor blade gas turbines. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket and blowing snow outside the nozzle and injecting it into the uppermost stream of all-blade gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a bullet or snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle and injects it into the uppermost stream of a full-blade gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. The all-blade steam gas turbine combined engine is characterized in that it is accelerated like a shot rocket or snowstorm outside the nozzle and injected into the uppermost stream of the all-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and accelerating like a shot rocket or snowstorm outside the nozzle and injecting it into the uppermost stream of the all-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting it into the uppermost stream of the all-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a bullet or snowstorm and accelerating like a shot rocket or snowstorm outside the nozzle and injecting it into the uppermost stream of a full-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. The all-blade steam gas turbine combined engine is characterized in that it is accelerated like a shot rocket or snowstorm outside the nozzle and injected into the uppermost stream of the all-blade steam turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and accelerating like a shot rocket or snowstorm outside the nozzle and injecting it into the uppermost stream of the all-blade steam turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting it into the uppermost stream of the all-blade steam turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a bullet or snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle and injects it into the uppermost stream of a full-blade steam turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm outside the nozzle and injecting sequentially downstream from the most upstream of the all-blade gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine that accelerates like a snowstorm and accelerates like a shot rocket or snowstorm outside the nozzle and injects it downstream from the most upstream of the all-blade gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a bullet or blowing snow, and accelerating like a shot rocket or blowing snow outside the nozzle and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine . 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. The all-blade steam gas turbine combined engine is characterized by accelerating like a shot rocket or snowstorm outside the nozzle and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm, and accelerating like a shot rocket or snowstorm outside the nozzle and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Combined with a full-swing steam gas turbine, characterized by acceleration like bullets and snowstorms, and acceleration outside shots like shot rockets and snowstorms, which are then injected downstream from the uppermost stream of all-swing steam gas turbines. organ. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm outside the nozzle and injecting sequentially downstream from the uppermost stream of the all-blade steam turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and accelerating like a shot rocket or snowstorm outside the nozzle and sequentially injecting downstream from the uppermost stream of the all-blade steam turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas turbine combined engine characterized by accelerating like a shot rocket and snowstorm outside the nozzle and injecting downstream from the uppermost stream of the all-blade steam turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a bullet or snowstorm and accelerating like a shot rocket or snowstorm outside the nozzle and injecting sequentially downstream from the uppermost stream of the all-blade steam turbine . 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. All-blade steam gas turbine combined with the feature that it accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the most upstream of the all-blade gas turbine to generate rotational output organ. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Whole blade steam, which is characterized by accelerating like a snowstorm, etc., and accelerating like a shot rocket or snowstorm outside the nozzle and injecting it downstream from the uppermost stream of the whole blade gas turbine to generate rotational output Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas is characterized in that it accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of the all-blade gas turbine to generate rotational output. Turbine coalescence engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Full dynamics characterized by acceleration such as bullets and snowstorms, and acceleration outside of the nozzles such as shot rockets and snowstorms, which are sequentially injected downstream from the uppermost stream of all rotor blade gas turbines. Wing steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. The full-blade steam gas turbine is characterized in that it accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of the full-blade steam gas turbine to generate rotational output. Combined organization. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. All rotor blades characterized by accelerating like a snowstorm, etc., and accelerating like a shot rocket or snowstorm outside the nozzle and injecting them sequentially downstream from the uppermost stream of all rotor blade steam gas turbines Steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All blade blade steam is characterized by the fact that it accelerates like a shot rocket or snowstorm outside the nozzle and injects it downstream from the uppermost stream of the all blade steam gas turbine to generate rotational output. Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, etc., and accelerates like shot rockets and snowstorms outside the nozzle and injects downstream from the uppermost stream of all blade steam gas turbines to generate rotational output. Rotor steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. All-blade steam gas turbine combined with the feature that it accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of the all-blade steam turbine to generate rotational output organ. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Whole blade steam, which is characterized by acceleration like a snowstorm, etc., and acceleration outside a nozzle like a shot rocket or snowstorm, which in turn is injected downstream from the uppermost stream of the whole blade steam turbine to generate rotational output. Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. All-blade steam gas is characterized in that it accelerates like a shot rocket or snowstorm outside the nozzle and injects downstream from the uppermost stream of the all-blade steam turbine to generate rotational output. Turbine coalescence engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Full dynamics characterized by acceleration such as bullets and snowstorms, and acceleration outside of the nozzles such as shot rockets and snowstorms, which are sequentially injected downstream from the uppermost stream of all blade steam turbines. Wing steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to adiabatic expansion atmospheric pressure. Wing steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. It accelerates like a shot rocket, snowstorm, etc. outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to adiabatic expansion atmospheric pressure. All-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerate like bullets and snowstorms, and accelerate like shot rockets and snowstorms outside the nozzle, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure This is an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized by recovering latent heat of vaporization in 66a). 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines, generating rotational output to adiabatic expansion atmospheric pressure, and latent heat of vaporization An all-rotor-blade steam gas turbine combined engine characterized by recovering latent heat of vaporization with a recovery device (66a). 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, recovering latent heat of vaporization All rotor blade steam gas turbine combined engine characterized in that latent heat of vaporization is recovered by a vessel (66a). 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerate like bullets and snowstorms, accelerate like shot rockets and snowstorms outside the nozzle, and inject sequentially downstream from the uppermost stream of all blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, An all-blade steam gas turbine combined engine characterized by recovering latent heat of vaporization with a vaporization latent heat recovery unit (66a). 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized by recovering latent heat of vaporization in 66a) and supplying condensed water to the combustor and heat exchanger (4) of the all-blade gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines, generating rotational output to adiabatic expansion atmospheric pressure, and latent heat of vaporization A full blade steam gas turbine combined engine characterized in that latent heat of vaporization is recovered by a recovery unit (66a) and condensed water is supplied to a combustor and heat exchanger (4) of a full blade gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, recovering latent heat of vaporization An all-blade steam gas turbine combined engine characterized in that latent heat of vaporization is recovered by the vessel (66a) and condensed water is supplied to the combustor and heat exchanger (4) of the all-blade gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerate like bullets and snowstorms, accelerate like shot rockets and snowstorms outside the nozzle, and inject sequentially downstream from the uppermost stream of all blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, A full blade steam gas turbine combined engine characterized by recovering vaporization latent heat with a vaporization latent heat recovery device (66a) and supplying condensed water to a combustor and heat exchanger (4) of a full blade gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized in that the latent heat of vaporization is recovered in 66a) and the condensed water is supplied to the combustor and heat exchanger (4) of the all-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines, generating rotational output to adiabatic expansion atmospheric pressure, and latent heat of vaporization A full blade steam gas turbine combined engine characterized in that latent heat of vaporization is recovered by a collector (66a) and condensed water is supplied to a combustor and heat exchanger (4) of a full blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, recovering latent heat of vaporization An all-blade steam gas turbine combined engine characterized in that the latent heat of vaporization is recovered by the vessel (66a) and condensed water is supplied to the combustor and heat exchanger (4) of the all-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerate like bullets and snowstorms, accelerate like shot rockets and snowstorms outside the nozzle, and inject sequentially downstream from the uppermost stream of all blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, A full-blade steam gas turbine combined engine characterized in that the latent heat of vaporization is recovered by a vaporization latent heat recovery unit (66a) and condensed water is supplied to the combustor and heat exchanger (4) of the full-blade steam gas turbine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized in that the latent heat of vaporization is recovered in 66a) and condensed water is supplied to a combustor and heat exchanger (4) of the all-blade gas turbine to form heated high-temperature water. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines, generating rotational output to adiabatic expansion atmospheric pressure, and latent heat of vaporization Combined with a moving blade steam gas turbine characterized in that the latent heat of vaporization is recovered by a recovery unit (66a) and condensed water is supplied to a combustor and heat exchanger (4) of a total moving blade gas turbine to form heated high-temperature water. organ. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, recovering latent heat of vaporization All-blade steam gas turbine combined engine characterized in that the latent heat of vaporization is recovered by the gas generator (66a) and the condensed water is supplied to the combustor and heat exchanger (4) of the full-blade gas turbine to form heated high-temperature water. . 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerate like bullets and snowstorms, accelerate like shot rockets and snowstorms outside the nozzle, and inject sequentially downstream from the uppermost stream of all blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, Total blade steam gas characterized in that latent heat of vaporization is recovered by a vaporization latent heat recovery unit (66a) and condensed water is supplied to a combustor and heat exchanger (4) of a full blade gas turbine to form heated high-temperature water. Turbine coalescence engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to the adiabatic expansion atmospheric pressure. 66a), which is characterized in that the latent heat of vaporization is recovered and the condensed water is supplied to the combustor and heat exchanger (4) of the full blade steam gas turbine to form heated high-temperature water. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines, generating rotational output to adiabatic expansion atmospheric pressure, and latent heat of vaporization A full blade steam gas turbine characterized in that latent heat of vaporization is recovered by a recovery unit (66a) and condensed water is supplied to a combustor and heat exchanger (4) of a full blade steam gas turbine to form heated high-temperature water. Combined organization. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, recovering latent heat of vaporization Combined full-blade steam gas turbine, characterized in that the latent heat of vaporization is recovered by the vessel (66a) and the condensed water is supplied to the combustor and heat exchanger (4) of the full-blade steam gas turbine to form heated high-temperature water organ. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerate like bullets and snowstorms, accelerate like shot rockets and snowstorms outside the nozzle, and inject sequentially downstream from the uppermost stream of all blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, Total blade steam characterized by recovering latent heat of vaporization with a vaporization latent heat recovery unit (66a) and supplying condensed water to a combustor and heat exchanger (4) of a full blade steam gas turbine to produce heated high-temperature water. Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to the adiabatic expansion atmospheric pressure. In 66a), the latent heat of vaporization is recovered and the condensed water is supplied to the combustor and heat exchanger (4) of the whole rotor blade gas turbine to be heated high temperature water, which is communicated to each high temperature water control valve (7a). The featured all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines, generating rotational output to adiabatic expansion atmospheric pressure, and latent heat of vaporization The latent heat of vaporization is recovered by the recovery unit (66a), and the condensed water is supplied to the combustor and heat exchanger (4) of the all blade blade gas turbine to be heated hot water, which is communicated to each high temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, recovering latent heat of vaporization The latent heat of vaporization is recovered by the vessel (66a), and the condensed water is supplied to the combustor and heat exchanger (4) of the whole blade gas turbine to form heated high-temperature water, which is communicated to the respective high-temperature water control valves (7a). It is characterized by an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerate like bullets and snowstorms, accelerate like shot rockets and snowstorms outside the nozzle, and inject sequentially downstream from the uppermost stream of all blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, The latent heat of vaporization is recovered by the vaporization latent heat recovery device (66a), and the condensed water is supplied to the combustor and heat exchanger (4) of the whole blade gas turbine to be heated high temperature water, and each high temperature water control valve (7a). All-rotor blade steam gas turbine combined engine characterized by contact with. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerates like a shot rocket or snowstorm outside the nozzle and injects it sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to the adiabatic expansion atmospheric pressure. In 66a), the latent heat of vaporization is recovered and the condensed water is supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to form heated hot water, which is then communicated to the respective hot water control valves (7a). This is an all-blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade steam turbines, generating rotational output to adiabatic expansion atmospheric pressure, and latent heat of vaporization The latent heat of vaporization is recovered by the recovery unit (66a), and the condensed water is supplied to the combustor and heat exchanger (4) of the whole blade steam gas turbine to be heated high-temperature water, and is supplied to each high-temperature water control valve (7a). An all-rotor-blade steam gas turbine combined engine characterized by contact. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, recovering latent heat of vaporization The latent heat of vaporization is recovered by the gas generator (66a), and the condensed water is supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to form heated high-temperature water, which is communicated to each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerate like bullets and snowstorms, accelerate like shot rockets and snowstorms outside the nozzle, and inject sequentially downstream from the uppermost stream of all blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a), and the condensed water is supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to be heated high temperature water. All-blade steam gas turbine combined engine characterized by 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate outside the nozzle like a shot rocket or snowstorm, etc., and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10) is injected into the optimum midstream stage. An all-blade steam gas turbine combined engine characterized by supply. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all blade gas turbines to generate rotational output, and the combustion gas ( 10) An all-blade steam gas turbine combined engine characterized by supplying 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10 ) All-wheel blade steam gas turbine combined engine characterized by 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, accelerates like a shot rocket and snowstorms outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output and burns to the optimal midstream stage An all-blade steam gas turbine combined engine characterized by supplying gas (10). 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and to the optimum middle stage combustion gas (10) It is characterized by supplying all the moving blade steam gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and combustion gas in the optimum middle stage (10) An all-blade steam gas turbine combined engine characterized by supplying (10). 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket, snowstorm, etc. outside the nozzle, and inject sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and the combustion gas ( 10) An all-blade steam gas turbine combined engine characterized by supplying 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, etc., and accelerates like shot rockets and snowstorms outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, achieving the optimum middle stage An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10). 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate outside the nozzle like a shot rocket or snowstorm, etc., and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10) is injected into the optimum midstream stage. An all-blade steam gas turbine combined engine characterized by being supplied and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all blade gas turbines to generate rotational output, and the combustion gas ( 10) An all-blade steam gas turbine combined engine characterized in that it is supplied with water and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10 ) And is cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, accelerates like a shot rocket and snowstorms outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output and burns to the optimal midstream stage An all-blade steam gas turbine combined engine characterized by supplying gas (10) and cooling with high-temperature water. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and to the optimum middle stage combustion gas (10) All-blade steam gas turbine combined engine characterized by supplying 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and combustion gas in the optimum middle stage An all-blade steam gas turbine combined engine characterized by supplying (10) and cooling with high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket, snowstorm, etc. outside the nozzle, and inject sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and the combustion gas ( 10) An all-blade steam gas turbine combined engine characterized in that it is supplied with water and cooled by high-temperature water. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, etc., and accelerates like shot rockets and snowstorms outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, achieving the optimum middle stage An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) and cooling with high-temperature water. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate outside the nozzle like a shot rocket or snowstorm, etc., and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10) is injected into the optimum midstream stage. An all-blade steam gas turbine combined engine characterized in that it is supplied and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all blade gas turbines to generate rotational output, and the combustion gas ( An all-blade steam gas turbine combined engine characterized in that 10) is supplied and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10 ) And cooling with high temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, accelerates like a shot rocket and snowstorms outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output and burns to the optimal midstream stage An all-blade steam gas turbine combined engine characterized by supplying gas (10) and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and to the optimum middle stage combustion gas (10) Is an all-blade steam gas turbine combined engine characterized in that it is cooled by high-temperature water and generates rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and combustion gas in the optimum middle stage An all-rotor-steam gas turbine combined engine characterized in that (10) is supplied and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket, snowstorm, etc. outside the nozzle, and inject sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and the combustion gas ( An all-blade steam gas turbine combined engine characterized in that 10) is supplied and cooled by high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, etc., and accelerates like shot rockets and snowstorms outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, achieving the optimum middle stage An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate outside the nozzle like a shot rocket or snowstorm, etc., and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10) is injected into the optimum midstream stage. An all-rotor-steam gas turbine combined engine characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as a core in the process of supplying and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all blade gas turbines to generate rotational output, and the combustion gas ( 10) A fully moving blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of supplying 10) and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10 ) And cooling with high-temperature water to produce a rotating output, an all-bladed steam gas turbine combined engine characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as a core. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, accelerates like a shot rocket and snowstorms outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output and burns to the optimal midstream stage An all-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of supplying gas (10) and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and to the optimum middle stage combustion gas (10) This is an all-bladed steam gas turbine combined engine characterized by agglomerating water with adiabatic expansion and low-temperature combustion gas as a core in the process of supplying rotating and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and combustion gas in the optimum middle stage (10) An all-blade steam gas turbine combined engine characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as a core in the process of supplying rotary cooling and generating rotational output by supplying (10). 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket, snowstorm, etc. outside the nozzle, and inject sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and the combustion gas ( 10) A fully moving blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of supplying 10) and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, etc., and accelerates like shot rockets and snowstorms outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, achieving the optimum middle stage An all-blade steam gas turbine combined engine characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as a core in the process of supplying combustion gas (10) and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate outside the nozzle like a shot rocket or snowstorm, etc., and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10) is injected into the optimum midstream stage. An all-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core and bringing exhaust such as CO2 close to 0 in the process of supplying and cooling with high-temperature water to generate rotational output. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects sequentially downstream from the uppermost stream of all blade gas turbines to generate rotational output, and the combustion gas ( 10) is a full-rotor steam gas turbine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core and bringing CO2 and other exhausts close to 0 in the process of supplying rotary cooling and generating rotational output Combined organization. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerating like a shot rocket, blowing snow, etc. outside the nozzle and injecting it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and the combustion gas (10 ) And cooling with high-temperature water to produce rotational output, aggregating moisture with adiabatic expansion low-temperature combustion gas as a core and bringing CO2 and other exhausts close to zero organ. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, accelerates like a shot rocket and snowstorms outside the nozzle, and injects sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output and burns to the optimal midstream stage Whole blade steam characterized by supplying gas (10) and cooling with high-temperature water to generate rotational output and agglomerate moisture with adiabatic expansion low-temperature combustion gas as the core to bring CO2 and other exhausts close to zero Gas turbine combined engine. 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (59b) heated to a high temperature by the heating high temperature means (101) injects high temperature water (5b) at a plurality of temperatures such as supercritical temperature, etc., and a bullet such as a bullet of a machine gun or a snowstorm is generated in the nozzle by the vaporization explosive force. Accelerate like a shot rocket or snowstorm outside the nozzle and inject downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and to the optimum middle stage combustion gas (10) All rotor blade steam gas turbine combined engine, characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core and bringing exhaust such as CO2 close to 0 in the process of supplying rotary and cooling with high temperature water . 加熱高温手段（１０１）により加熱高温とした高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A supercritical pressure high temperature water (5b) having a plurality of temperatures such as a supercritical temperature is ejected from a high temperature water injection nozzle (59b) heated to a high temperature by a heating high temperature means (101), and a bullet of a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like a snowstorm, etc., accelerates like a shot rocket or snowstorm outside the nozzle, and injects downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and combustion gas in the optimum middle stage (10) is a whole blade steam gas characterized in that in the process of supplying rotary cooling with high-temperature water and generating rotational output, moisture agglomerates with the adiabatic expansion low-temperature combustion gas as the core and the exhaust gas such as CO2 approaches zero Turbine coalescence engine. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of high-temperature water injection nozzles (59b) heated at a high temperature by the heating high-temperature means (101) are used to inject high-temperature water (5b) such as a supercritical temperature to cause bullets and snowstorms of machine guns in the nozzles by vaporization explosive force. Accelerate like a shot rocket, snowstorm, etc. outside the nozzle, and inject sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and the combustion gas ( 10) is a full-rotor steam gas turbine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core and bringing CO2 and other exhausts close to 0 in the process of supplying rotary cooling and generating rotational output Combined organization. 加熱高温手段（１０１）により加熱高温とした複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  Supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is injected from a plurality of high-temperature water injection nozzles (59b) heated to a high temperature by the heating high-temperature means (101), and a machine gun is generated in the nozzle by vaporization explosive force. Accelerates like bullets and snowstorms, etc., and accelerates like shot rockets and snowstorms outside the nozzle, and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, achieving the optimum middle stage All moving blades characterized by supplying combustion gas (10) and cooling with high-temperature water to generate rotational output and agglomerate moisture with adiabatic expansion low-temperature combustion gas as the core to bring CO2 and other exhausts close to zero Steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  An all blade steam gas turbine combined engine characterized by injecting high temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high temperature water injection nozzle (59b). 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized by injecting supercritical high-temperature water (5b) having a plurality of temperatures such as supercritical temperature from a high-temperature water injection nozzle (59b). 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized by injecting high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature from a plurality of high-temperature water injection nozzles (59b). 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射することが特徴の全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized by injecting supercritical pressure high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature from a plurality of high-temperature water injection nozzles (59b). 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A full moving blade characterized by jetting high temperature water (5b) at multiple temperatures such as supercritical temperature from a high temperature water jet nozzle (59b) and accelerating it like a bullet of a machine gun or snowstorm in the nozzle by vaporization explosive force Steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  It is characterized by jetting supercritical pressure high temperature water (5b) of multiple temperatures such as supercritical temperature from the high temperature water injection nozzle (59b) and accelerating it like a bullet of a machine gun or a snowstorm in the nozzle by vaporization explosive force All-blade steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  It is characterized by jetting high temperature water (5b) at a plurality of temperatures such as supercritical temperature from a plurality of high temperature water injection nozzles (59b) and accelerating like a bullet of a machine gun or a snowstorm in the nozzle by vaporization explosive force. Rotor steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b), such as a supercritical temperature, is injected from a plurality of high temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. The featured all-blade steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by acceleration like a snowstorm. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by acceleration such as shot rockets and snowstorms. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by acceleration such as rockets and snowstorms. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-rotor blade steam gas turbine combined engine characterized by acceleration like a shot rocket or snowstorm outside. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-bladed steam gas turbine combined engine characterized by optimal use of latent heat of vaporization by accelerating, such as blowing snow. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-rotor-steam gas turbine combined engine characterized by accelerating and using the latent heat of vaporization optimally like a shot rocket or snowstorm. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-rotor-steam gas turbine combined engine characterized by optimal use of latent heat of vaporization by accelerating like a rocket or snowstorm. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して気化潜熱を最適利用することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-rotor-blade steam gas turbine combined engine, which is characterized by the optimum use of latent heat of vaporization by accelerating like a shot rocket or snowstorm outside. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating and spraying to all the rotor blades, such as blowing snow. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating and injecting into all rotor blades like a shot rocket or snowstorm. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating and spraying to all rotor blades, such as rockets and snowstorms. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-rotor-blade steam gas turbine combined engine characterized by accelerating and injecting to all the rotor blades like a shot rocket or snowstorm. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating and injecting into the uppermost stream of all the rotor blades, such as a snowstorm. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-rotor steam gas turbine combined engine characterized by accelerating and injecting into the uppermost stream of all rotor blades, such as shot rockets and snowstorms. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-rotor steam gas turbine combined engine characterized by accelerating and injecting into the uppermost stream of all rotor blades like a rocket or snowstorm. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼の最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-rotor-blade steam gas turbine combined engine that is characterized by accelerating and injecting into the uppermost stream of all rotor blades, like shot rockets and snowstorms. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting it into the uppermost stream of the all-blade gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating and injecting into the uppermost stream of all-blade gas turbines, such as shot rockets and snowstorms. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating like a rocket or snowstorm and injecting it into the uppermost stream of all-blade gas turbines. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-rotor steam gas turbine combined engine characterized by accelerating and injecting into the uppermost stream of all rotor blade gas turbines, like shot rockets and snowstorms. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting it into the uppermost stream of the all-blade steam gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating it like a shot rocket or snowstorm and injecting it into the uppermost stream of the all-blade steam gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating like a rocket or a snowstorm and injecting it into the uppermost stream of a full-blade steam gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm outside and injecting it into the uppermost stream of all-blade steam gas turbines. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting it into the uppermost stream of the all-blade steam turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine, which is characterized by accelerating it like a shot rocket or snowstorm and injecting it into the uppermost stream of the all-blade steam turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-rotor steam gas turbine combined engine characterized by accelerating like a rocket or snowstorm and injecting it into the uppermost stream of all the rotor blade steam turbines. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-rotor steam gas turbine combined engine characterized by accelerating and injecting into the uppermost stream of all rotor blade steam turbines, like shot rockets and snowstorms. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating like a rocket or snowstorm and injecting it downstream from the uppermost stream of the all-blade gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-rotor steam gas turbine combined engine characterized by acceleration, like a shot rocket or snowstorm, and jetting sequentially downstream from the uppermost stream of the entire rotor blade gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm and injecting it sequentially downstream from the most upstream of the all-blade steam gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating like a rocket or snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm outside and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade steam turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-rotor-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm and injecting it sequentially downstream from the uppermost stream of the all-rotor steam turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating like a rocket or snowstorm and injecting it downstream from the uppermost stream of the all-blade steam turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-rotor-steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm outside and injecting it sequentially downstream from the uppermost stream of all-stainless-blade steam turbines. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting it sequentially downstream from the most upstream of the all-blade gas turbine to generate rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm and injecting it downstream from the most upstream of the all-blade gas turbine to generate rotational output. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by generating a rotational output by accelerating like a rocket or snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-blade steam gas turbine combined engine, which is characterized by accelerating like a shot rocket or snowstorm and injecting it downstream from the uppermost stream of the all-blade gas turbine to generate rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting it sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by generating a rotational output by accelerating like a shot rocket or snowstorm and injecting it downstream from the uppermost stream of the all-blade steam gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by generating a rotational output by accelerating like a rocket or snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-blade steam gas turbine combined engine characterized in that it accelerates like a shot rocket or snowstorm outside and injects it sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by generating a rotational output by accelerating like a shot rocket or snowstorm and then sequentially injecting it downstream from the uppermost stream of the all-blade steam turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by generating a rotational output by accelerating like a rocket or snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade steam turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-blade steam gas turbine combined engine characterized in that it accelerates like a shot rocket or snowstorm and injects it sequentially downstream from the uppermost stream of the all-blade steam turbine to generate rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a snowstorm and injecting it sequentially downstream from the most upstream of the all-blade steam turbine to generate rotational output up to the adiabatic expansion atmospheric pressure. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket or snowstorm and injecting sequentially downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to adiabatic expansion atmospheric pressure. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating like a rocket or snowstorm and injecting it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to the adiabatic expansion atmospheric pressure. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. An all-blade steam gas turbine combined engine characterized in that it accelerates like a shot rocket or snowstorm outside and injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate rotational output to adiabatic expansion atmospheric pressure . 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm, etc., injects sequentially downstream from the uppermost stream of all rotor blade steam turbines, generates rotational output to adiabatic expansion atmospheric pressure, and recovers the latent heat of vaporization with a latent heat recovery unit (66a). All-blade steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. Accelerate like a shot rocket or snowstorm, and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, and recover the latent heat of vaporization with the latent heat recovery unit (66a). It is characterized by an all-blade steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket, snowstorm, etc., inject sequentially downstream from the uppermost stream of all rotor blade steam turbines, generate rotational output to adiabatic expansion atmospheric pressure, and recover vaporization latent heat with vaporization latent heat recovery unit (66a) This is an all-blade steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc. and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. An all-rotor-blade steam gas turbine combined engine characterized by recovery. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization with a latent heat recovery unit (66a), and condensates Is provided to a combustor and heat exchanger (4) of a full blade gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, and recovers the latent heat of vaporization with the vaporization latent heat recovery unit (66a). And an all-blade steam gas turbine combined engine characterized by supplying condensed water to the combustor and heat exchanger (4) of the all-blade gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, and recover the latent heat of vaporization with a latent heat recovery unit (66a). An all-blade steam gas turbine combined engine characterized by supplying condensed water to a combustor and heat exchanger (4) of the all-blade gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc. and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized in that it collects and supplies condensed water to the combustor and heat exchanger (4) of the all-blade gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization with a latent heat recovery unit (66a), and condensates Is provided to a combustor and heat exchanger (4) of a full blade steam gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, and recovers the latent heat of vaporization with the vaporization latent heat recovery unit (66a). And an all-blade steam gas turbine combined engine characterized by supplying condensed water to the combustor and heat exchanger (4) of the all-blade steam gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, and recover the latent heat of vaporization with a latent heat recovery unit (66a). An all-blade steam gas turbine combined engine characterized by supplying condensed water to the combustor and heat exchanger (4) of the all-blade steam gas turbine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc. and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized by recovering and supplying condensed water to the combustor and heat exchanger (4) of the all-blade steam gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization with a latent heat recovery unit (66a), and condensates Is an all-blade steam gas turbine combined engine characterized by supplying high-temperature water to a combustor and heat exchanger (4) of the all-blade gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, and recovers the latent heat of vaporization with the vaporization latent heat recovery unit (66a). An all-blade steam gas turbine combined engine characterized in that the condensed water is supplied to a combustor and heat exchanger (4) of the all-blade gas turbine to form heated high-temperature water. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, and recover the latent heat of vaporization with a latent heat recovery unit (66a). A full-blade steam gas turbine combined engine characterized in that condensed water is supplied to a combustor and heat exchanger (4) of a full-blade gas turbine to form heated high-temperature water. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc. and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. An all-rotor steam gas turbine combined engine characterized in that it collects and supplies condensed water to a combustor and heat exchanger (4) of the all-blade gas turbine to produce heated high-temperature water. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization with a latent heat recovery unit (66a), and condensates Is a combined high temperature water steam gas turbine combined engine that is supplied to the combustor and heat exchanger (4) of the full dynamic blade steam gas turbine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, and recovers the latent heat of vaporization with the vaporization latent heat recovery unit (66a). An all-blade steam gas turbine combined engine characterized in that condensed water is supplied to a combustor and heat exchanger (4) of the all-blade steam gas turbine to form heated high-temperature water. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, and recover the latent heat of vaporization with a latent heat recovery unit (66a). An all-blade steam gas turbine combined engine characterized in that condensed water is supplied to a combustor and heat exchanger (4) of the all-blade steam gas turbine to form heated high-temperature water. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水にすることが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc. and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. An all-rotor-steam gas turbine combined engine characterized in that the recovered condensed water is supplied to a combustor and heat exchanger (4) of the all-steam steam gas turbine to form heated high-temperature water. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization with a latent heat recovery unit (66a), and condensates Is supplied to a combustor and heat exchanger (4) of a full-blade gas turbine to form heated high-temperature water, and communicates with each high-temperature water control valve (7a). 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. Then, the condensed water steam gas turbine is characterized in that the condensed water is supplied to the combustor and heat exchanger (4) of the all blade gas turbine to form heated high-temperature water and communicates with each high-temperature water control valve (7a). Combined organization. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, and recover the latent heat of vaporization with a latent heat recovery unit (66a). Combined full-blade steam gas turbine combined with the feature that the condensed water is supplied to the combustor and heat exchanger (4) of the full-blade gas turbine to be heated high-temperature water and communicated with each high-temperature water control valve (7a) organ. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc. and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. The whole blade steam, which is characterized in that the recovered condensed water is supplied to the combustor / heat exchanger (4) of the all blade gas turbine to be heated high temperature water and communicated to each high temperature water control valve (7a). Gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization with a latent heat recovery unit (66a), and condensates Is supplied to the combustor and heat exchanger (4) of the full-blade steam gas turbine to form heated high-temperature water, and communicates with each high-temperature water control valve (7a). . 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. The condensed blade steam gas is characterized in that the condensed water is supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to form heated high temperature water and communicates with each of the high temperature water control valves (7a). Turbine coalescence engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm and inject sequentially downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output to adiabatic expansion atmospheric pressure, and recover the latent heat of vaporization with a latent heat recovery unit (66a). A full blade steam gas turbine characterized in that condensed water is supplied to a combustor and heat exchanger (4) of a full blade steam gas turbine to form heated high temperature water and communicates with each high temperature water control valve (7a). Combined organization. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気タービンの最上流より順次下流に噴射して断熱膨張大気圧まで回転出力を発生し、気化潜熱回収器（６６ａ）で気化潜熱を回収して凝縮水を全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）に供給して加熱高温水とし、夫々の高温水加減弁（７ａ）に連絡することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc. and injects it downstream from the uppermost stream of all rotor blade steam turbines to generate rotational output up to the adiabatic expansion atmospheric pressure. All the moving blades characterized in that the recovered condensed water is supplied to the combustor and heat exchanger (4) of the all blade steam gas turbine to be heated high-temperature water and communicated with each high-temperature water control valve (7a). Steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Full blade steam gas, which is characterized in that it is accelerated like a snowstorm, etc., is injected sequentially downstream from the uppermost stream of the full blade gas turbine to generate rotational output, and the combustion gas (10) is supplied to the optimum midstream stage. Turbine coalescence engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. Full dynamics characterized by accelerating like a shot rocket or snowstorm, and injecting it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output and supplying combustion gas (10) to the optimal middle stage Wing steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Full rotor blades characterized by accelerating like a rocket or snowstorm, etc., and injecting downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output and supplying combustion gas (10) to the optimum middle stream stage Steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum middle stage All-blade steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. A full blade steam characterized by accelerating like a snowstorm and injecting it downstream from the most upstream of the full blade steam gas turbine to generate a rotational output and supplying combustion gas (10) to the optimum midstream stage Gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It is characterized by accelerating like a shot rocket, snowstorm, etc., and injecting it downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output and supplying the combustion gas (10) to the optimum midstream stage. Rotor steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Full dynamics characterized by accelerating like a rocket or snowstorm and injecting downstream from the uppermost stream of a full blade steam gas turbine to generate rotational output and supplying combustion gas (10) to the optimal middle stage Wing steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output and supply the combustion gas (10) to the optimum middle stage All-blade steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm, etc., injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, supplies combustion gas (10) to the optimum middle stage, and cools it with hot water All-blade steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. Accelerate like a shot rocket or snowstorm, etc., and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and supply combustion gas (10) to the optimal middle stream stage to cool with high temperature water It is characterized by an all-blade steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket, snowstorm, etc., and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and supply combustion gas (10) to the optimal midstream stage and cool with high temperature water This is an all-blade steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc., and injects it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum midstream stage by hot water. An all-blade steam gas turbine combined engine characterized by cooling. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm, etc., and injects downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and supplies the combustion gas (10) to the optimum midstream stage and cools it with hot water The featured all-blade steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. Accelerates like a shot rocket or snowstorm and injects it downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and supplies combustion gas (10) to the optimum middle stage and cools it with hot water An all-blade steam gas turbine combined engine characterized by 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm, etc., and inject sequentially downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, supply combustion gas (10) to the optimum midstream stage, and cool with hot water It is characterized by an all-blade steam gas turbine combined engine. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc., and injects it downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum middle stage to supply hot water All rotor blade steam gas turbine combined engine, characterized by cooling by. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, supplies combustion gas (10) to the optimum middle stage, cools it with high-temperature water, and rotates it. It is characterized by the generation of an all-blade steam gas turbine combined engine. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. It supplies combustion gas (10) to the optimum middle stage and cools it with hot water. This is an all-blade steam gas turbine combined engine characterized by generating rotational output. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm, etc. and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, supply combustion gas (10) to the optimal middle stream stage and cool with hot water An all-blade steam gas turbine combined engine characterized by generating rotational output. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc., and injects it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum midstream stage by hot water. An all-blade steam gas turbine combined engine characterized by cooling and generating rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm, etc., and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, supplies combustion gas (10) to the optimum midstream stage, cools with hot water, and rotates An all-blade steam gas turbine combined engine characterized by generating output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. Accelerates like a shot rocket or snowstorm and injects it downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and supplies combustion gas (10) to the optimum middle stage and cools it with hot water All-wheel blade steam gas turbine combined engine characterized by generating rotational output as a result. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerates like a rocket or snowstorm and injects downstream from the uppermost stream of all blade steam gas turbines to generate rotational output, supplies combustion gas (10) to the optimum middle stage and cools it with hot water This is an all-blade steam gas turbine combined engine characterized by generating rotational output. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc., and injects it downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum middle stage to supply hot water This is an all-bladed steam gas turbine combined engine characterized by being cooled by a cylinder and generating rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, supplies combustion gas (10) to the optimum middle stage, cools it with high-temperature water, and rotates it. An all-rotor-steam gas turbine combined engine characterized by agglomerating moisture in the process of adiabatic expansion and low-temperature combustion gas. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. It supplies combustion gas (10) to the optimum middle stage and cools it with hot water. All-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as the core in the process of generating rotational output. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm, etc. and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, supply combustion gas (10) to the optimal middle stream stage and cool with hot water An all-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as the core during the generation of rotational output. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc., and injects it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum midstream stage by hot water. An all-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of cooling and generating rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm, etc., and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, supplies combustion gas (10) to the optimum midstream stage, cools with hot water, and rotates An all-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as the core during the generation of output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. Accelerates like a shot rocket or snowstorm and injects it downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and supplies combustion gas (10) to the optimum middle stage and cools it with hot water All-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of generating rotational output. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerates like a rocket or snowstorm and injects downstream from the uppermost stream of all blade steam gas turbines to generate rotational output, supplies combustion gas (10) to the optimum middle stage and cools it with hot water All-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as the core in the process of generating rotational output. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集することが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc., and injects it downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum middle stage to supply hot water This is an all-rotor-steam gas turbine combined engine, characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as the core in the process of cooling and generating rotational output. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm and injects downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, supplies combustion gas (10) to the optimum middle stage, cools it with high-temperature water, and rotates it. An all-blade steam gas turbine combined engine characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as the core in the process of generating CO2 and other exhausts to approach zero. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. It accelerates like a shot rocket or snowstorm, and injects it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output. It supplies combustion gas (10) to the optimum middle stage and cools it with hot water. The all-blade steam gas turbine combined engine is characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of generating rotational output and bringing exhaust such as CO2 close to zero. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerate like a rocket or snowstorm, etc. and inject sequentially downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, supply combustion gas (10) to the optimal middle stream stage and cool with hot water An all-blade steam gas turbine combined engine characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as a core in the process of generating rotational output and bringing exhaust such as CO2 close to zero. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc., and injects it downstream from the uppermost stream of all rotor blade gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum midstream stage by hot water. An all-blade steam gas turbine combined engine characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as a core and bringing exhaust such as CO2 close to 0 in the process of generating rotational output by cooling. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b), such as supercritical temperature, is injected from the high-temperature water injection nozzle (59b), and is accelerated like a bullet or snowstorm of a machine gun inside the nozzle by the vaporization explosive force. Accelerates like a snowstorm, etc., and injects downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, supplies combustion gas (10) to the optimum midstream stage, cools with hot water, and rotates An all-blade steam gas turbine combined engine characterized by agglomerating moisture using adiabatic expansion low-temperature combustion gas as a core in the process of generating output and bringing exhaust such as CO2 close to zero. 高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water injection nozzle (59b) injects supercritical pressure high-temperature water (5b) at multiple temperatures, such as supercritical temperature, and accelerates like a bullet of a machine gun or snowstorm inside the nozzle by vaporization explosive force. Accelerates like a shot rocket or snowstorm and injects it downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, and supplies combustion gas (10) to the optimum middle stage and cools it with hot water In the process of generating rotational output, the all-rotor-blade steam gas turbine combined engine is characterized by agglomerating moisture with the adiabatic expansion low-temperature combustion gas as a core and bringing exhaust such as CO2 close to zero. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) with multiple temperatures such as supercritical temperature is injected from multiple high-temperature water injection nozzles (59b), and accelerated by vaporization explosive force like a bullet of a machine gun or snowstorm inside the nozzle. Accelerates like a rocket or snowstorm and injects downstream from the uppermost stream of all blade steam gas turbines to generate rotational output, supplies combustion gas (10) to the optimum middle stage and cools it with hot water The all-blade steam gas turbine combined engine is characterized by agglomerating moisture with adiabatic expansion low-temperature combustion gas as a core in the process of generating rotational output and bringing exhaust such as CO2 close to zero. 複数の高温水噴射ノズル（５９ｂ）より超臨界温度等複数温度の超臨界圧力高温水（５ｂ）を噴射して気化爆発力によりノズル内では機関銃の弾丸や吹雪等のように加速し、ノズル外では散弾ロケットや吹雪等のように加速して全動翼蒸気ガスタービンの最上流より順次下流に噴射して回転出力を発生し、最適中流段に燃焼ガス（１０）を供給して高温水により冷却して回転出力を発生の過程で断熱膨張低温燃焼ガスを核に水分を凝集してＣＯ２等の排気を０に近付けることが特徴の全動翼蒸気ガスタービン合体機関。  A plurality of supercritical pressure high temperature water (5b) such as a supercritical temperature is injected from a plurality of high temperature water injection nozzles (59b), and the nozzle is accelerated by a vaporization explosive force like a bullet of a machine gun or a snowstorm in the nozzle. Outside, it accelerates like a shot rocket, snowstorm, etc., and injects it downstream from the uppermost stream of all rotor blade steam gas turbines to generate rotational output, and supplies combustion gas (10) to the optimum middle stage to supply hot water An all-blade steam gas turbine combined engine characterized by aggregating moisture with adiabatic expansion low-temperature combustion gas as a core and bringing exhaust such as CO2 close to 0 in the process of generating rotational output by cooling by 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (16) and the inner compressor rotor blade group (17) which are integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized in that a water-repellent water cooling blade (87) is provided in the majority of the engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor rotor group (17) of the outer compressor blade group (17) and the inner compressor rotor group (17), which are integrally cast in a ring (84) to form an assembly structure. ) Is provided with a water-repellent water cooling blade (87) in a large part thereof. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade gas turbine, most of the outer compressor blade group (16) and the inner compressor blade group (17) formed into an assembly structure by integrally casting in a ring (84), An all-blade steam gas turbine combined engine provided with water-repellent water cooling blades (87). 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade steam gas turbine, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed in an annular shape (84) and assembled, An all-blade steam gas turbine combined engine provided with a water-repellent water cooling blade (87). 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (16) and the inner compressor rotor blade group (17) which are integrally cast in a ring (84) to form an assembly structure. The water-repellent water cooling blades (87) are provided annularly in each of the most parts, and one or more water-repellent water cooling blades per stage are cooled and then water-injected from the water-injecting means (56). Rotor steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor rotor group (17) of the outer compressor blade group (17) and the inner compressor rotor group (17), which are integrally cast in a ring (84) to form an assembly structure. ) Is provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and water is ejected from the water ejecting means (56) after cooling one or more water-repellent water cooling blades per paragraph. An all-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the all-blade compressor of the all-blade gas turbine, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast in a ring (84) to form an assembly structure, are repelled by most of them. An all-water-blade steam gas turbine characterized in that the water-based water cooling blades (87) are provided in an annular shape per stage, and water is injected from the water injection means (56) after cooling one or more water-repellent water cooling blades per stage. Combined organization. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade steam gas turbine, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed in an annular shape (84) and assembled, And a water-repellent water cooling blade (87) provided in an annular shape for each paragraph, and the water-repellent water-cooling blade is cooled by water injection means (56) after cooling one or more water-repellent water cooling blades per paragraph. Gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (16) and the inner compressor rotor blade group (17) which are integrally cast in a ring (84) to form an assembly structure. The water-repellent water cooling blades (87) are provided annularly in each paragraph in the most part of the water, and the water-repellent water cooling blades of the entire half or less in every paragraph are cooled and then water-injected by the water injection means (56). All-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor rotor group (17) of the outer compressor blade group (17) and the inner compressor rotor group (17), which are integrally cast in a ring (84) to form an assembly structure. ) Is provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and the water-repellent water cooling blades for each paragraph are less than half of the water-repellent water after being cooled and then water-injected by water injection means (56) An all-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade gas turbine, most of the outer compressor blade group (16) and the inner compressor blade group (17) formed into an assembly structure by integrally casting in a ring (84), A water-repellent water cooling blade (87) is provided in a ring shape for each paragraph, and the water-repellent water-cooling blade of half or less in every paragraph is cooled and then water-injected from the water-injecting means (56). Turbine coalescence engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade steam gas turbine, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed in an annular shape (84) and assembled, And a water-repellent water cooling blade (87) provided in an annular shape for each paragraph, and the water-repellent water-cooling blade of half or less in every paragraph is cooled and then water-injected from the water-injecting means (56). Gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17) most of the outer compressor blade group (17) that are integrally cast in a ring (84) and communicated with the water channel as an assembly structure. In addition, the water-repellent water cooling blade (87) is provided in an annular shape for each paragraph, and the water-repellent water-cooling blades of the entire half or less in each paragraph are jetted with water from the water jetting means (56) after cooling. Steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) in an annular shape and communicated with the water channel as an assembly structure. A water repellent water cooling blade (87) is provided in each part in an annular shape, and the water repellent water cooling blade of half or less of each stage is cooled and then water-injected by water injection means (56). Wing steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio, and a plurality of high temperatures such as a supercritical temperature such as a supercritical temperature provided with an electromagnetically heated turbine rotor blade (81). In an all blade gas turbine driven by water (5b), the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (17) and the inner compressor blade group (17) that are integrally cast in a ring (84) and communicated with the water channel as an assembly structure. Mostly, the water-repellent water cooling blades (87) are provided in a ring shape for each paragraph, and the water-repellent water cooling blades of the entire half or less in every paragraph are cooled and then water-injected from the water injection means (56). Rotor steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the all-blade steam gas turbine, water repellency is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally cast in a ring (84) and communicated with the water channel as an assembly structure. An all-swing-blade steam gas turbine combination characterized in that the water-cooling blades (87) are provided in an annular shape for each paragraph, and the water-repellent water-cooling blades of half or less in every paragraph are cooled and then water-injected from the water injection means (56) organ. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (16) and the inner compressor rotor blade group (17) which are integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by comprising a device that is provided with a water repellent water cooling blade (87) in an annular form for each stage and is driven by the output. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor rotor group (17) of the outer compressor blade group (17) and the inner compressor rotor group (17), which are integrally cast in a ring (84) to form an assembly structure. ), A water-repellent water cooling blade (87) is provided in a ring shape for each stage and is driven by the output. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade gas turbine, most of the outer compressor blade group (16) and the inner compressor blade group (17) formed into an assembly structure by integrally casting in a ring (84), An all-rotor-blade steam gas turbine combined engine comprising a device in which a water-repellent water cooling blade (87) is provided in an annular shape for each stage and driven by the output. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade steam gas turbine, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed in an annular shape (84) and assembled, An all-blade steam gas turbine combined engine comprising a device that is provided with a water repellent water cooling blade (87) in a ring shape and driven by the output. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (16) and the inner compressor rotor blade group (17) which are integrally cast in a ring (84) to form an assembly structure. The water-repellent water cooling blades (87) are provided annularly in each stage, and one or more water-repellent water cooling blades per stage are cooled and then sprayed with water from the water spraying means (56) and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising an apparatus for performing the above operation. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor rotor group (17) of the outer compressor blade group (17) and the inner compressor rotor group (17), which are integrally cast in a ring (84) to form an assembly structure. ) Is provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, water is injected from the water injection means (56) and the output is An all-blade steam gas turbine combined engine comprising a driving device. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade gas turbine, most of the outer compressor blade group (16) and the inner compressor blade group (17) formed into an assembly structure by integrally casting in a ring (84), A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph, and a device for driving one or more water-repellent water cooling blades at one or more stages after being cooled by water injection means (56) and driven by the output is provided. An all-blade steam gas turbine combined engine characterized by that. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the full blade compressor of the full blade steam gas turbine, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed in an annular shape (84) and assembled, A water repellent water cooling blade (87) is provided in each ring, and after cooling one or more water repellent water cooling blades per stage, water is injected from the water injection means (56) and driven by the output. An all-blade steam gas turbine combined engine characterized by that. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17) most of the outer compressor blade group (17) that are integrally cast in a ring (84) and communicated with the water channel as an assembly structure. In addition, a water-repellent water cooling blade (87) is provided in an annular shape for each paragraph, and a water-repellent water-cooling blade is cooled by the water jetting means (56) after cooling the water-repellent water cooling blades of less than half of each paragraph and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. 5b), the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) in an annular shape and communicated with the water channel as an assembly structure. The device is provided with a water-repellent water cooling blade (87) in each part in an annular shape, and after cooling the water-repellent water cooling blades of less than half of each paragraph, water is sprayed from the water spraying means (56) and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising: 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the whole rotor blade gas turbine, water repellent water is formed in most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) which are integrally cast in a ring (84) and communicated with the water channel as an assembly structure. A cooling blade (87) is provided in a ring for each paragraph, and a device for driving the water-repellent water cooling blade of less than half of each paragraph by water injection from the water injection means (56) after cooling after cooling is provided. An all-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the all-blade steam gas turbine, water repellency is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally cast in a ring (84) and communicated with the water channel as an assembly structure. Water cooling blades (87) are provided in a ring for each paragraph, and a device for driving the water-repellent water cooling blades, which are less than half of each paragraph, by water injection from the water injection means (56) after cooling is driven by the output. An all-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade steam gas turbine driven in 5b), the water injection means (56a) is thermally insulated in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) which is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by being provided as 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade steam gas turbine driven in 5b), the water injection means (56a) is thermally insulated in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) which is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by being provided as 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade gas turbine driven in 5b), the water injection means (56a) is thermally insulated in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) annularly. An all-blade steam gas turbine combined engine characterized by 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade gas turbine driven in 5b), the water injection means (56a) is insulated in the vicinity of the assembly annular connection of the outer turbine rotor blade group (19) which is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade steam turbine driven in 5b), the water injection means (56a) is insulated near the assembly annular connection portion of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine characterized by 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade steam turbine driven in 5b), the water injection means (56a) is insulated near the assembly annular connection portion of the outer turbine rotor blade group (19) which is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the all-blade steam gas turbine, the water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) that is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the all-blade steam gas turbine, the water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine characterized by 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the whole rotor blade gas turbine, the water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) which is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the all-blade gas turbine, the water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the whole blade steam turbine, the water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the whole blade steam turbine, the water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade steam gas turbine driven in 5b), the water injection means (56a) is thermally insulated in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) which is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized in that the superheated steam is cooled to reduce the volume and increase the unit mass. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade gas turbine driven in 5b), the water injection means (56a) is thermally insulated in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) annularly. An all-blade steam gas turbine combined engine characterized in that the superheated steam is cooled to reduce the volume and increase the unit mass. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water (such as supercritical temperature such as supercritical pressure) equipped with an electromagnetically heated turbine rotor blade (81) by coupling an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. In the all-blade steam turbine driven in 5b), the water injection means (56a) is insulated near the assembly annular connection portion of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine characterized in that the superheated steam is cooled to reduce the volume and increase the unit mass. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the all-blade steam gas turbine, the water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) that is integrally cast in a ring (84) to form an assembly structure, and is overheated. An all-blade steam gas turbine combined engine characterized by cooling steam and reducing the volume to increase unit mass. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the all-blade gas turbine, the water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting in a ring (84), and superheated steam is provided. The whole rotor blade steam gas turbine combined engine, wherein the unit mass is increased by cooling the engine and reducing the volume. 発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81). In the whole blade steam turbine, the superheated steam is provided by insulating the water injection means (56a) in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) annularly. The whole rotor blade steam gas turbine combined engine, wherein the unit mass is increased by cooling the engine and reducing the volume. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、低温燃焼ガスにより水道水を冷却して貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that, in an all-blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C, tap water is cooled and stored with low-temperature combustion gas. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、低温燃焼ガスにより水道水を冷却して貯蔵して水道水冷熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all blade blade gas turbine having a combustion gas exhaust temperature approaching −273 ° C., wherein tap water is cooled and stored with low-temperature combustion gas to supply tap water cooling heat to consumers. Combined organization. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the compressed air pressure of the combustor and heat exchanger 4 is raised to the limit by all the rotor blades in an all-blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C. . 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇し、低温燃焼ガスにより水道水を冷却して貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade gas turbine whose combustion gas exhaust temperature approaches −273 ° C., the compressed air pressure of the combustor / heat exchanger 4 is increased to the limit by all the blades, and the tap water is cooled and stored by the low temperature combustion gas. An all-blade steam gas turbine combined engine characterized by that. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇し、低温燃焼ガスにより水道水を冷却して貯蔵して水道水冷熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C, the compressed air pressure of the combustor / heat exchanger 4 is raised to the limit by all the blades, and tap water is cooled and stored by the low temperature combustion gas. This is an all-bladed steam gas turbine combined engine that supplies tap water cooling to customers. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により直接空気を冷却することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is approached to -273 ° C and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas and supply tap water to consumers, and direct air is supplied by the tap water cooling heat. An all-blade steam gas turbine combined engine characterized by cooling. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により直接空気を冷却して室内を冷却することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is approached to -273 ° C and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas and supply tap water to consumers, and direct air is supplied by the tap water cooling heat. An all-rotor-blade steam gas turbine combined engine characterized by cooling and cooling the room. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により圧縮空気を冷却することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas to supply tap water cooling heat to consumers, and compressed water is cooled by the tap water cooling heat. An all-blade steam gas turbine combined engine characterized by cooling. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により圧縮空気を冷却して室内を冷却することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas to supply tap water cooling heat to consumers, and compressed water is cooled by the tap water cooling heat. An all-rotor-blade steam gas turbine combined engine characterized by cooling and cooling the room. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により圧縮空気を冷却して冷凍設備にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas to supply tap water cooling heat to consumers, and compressed water is cooled by the tap water cooling heat. An all-blade steam gas turbine combined engine characterized by cooling to a refrigeration facility. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により圧縮空気を冷却して冷凍庫にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas to supply tap water cooling heat to consumers, and compressed water is cooled by the tap water cooling heat. An all-blade steam gas turbine combined engine characterized by cooling into a freezer. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により圧縮空気を冷却して冷蔵庫にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas to supply tap water cooling heat to consumers, and compressed water is cooled by the tap water cooling heat. An all-blade steam gas turbine combined engine characterized by cooling to a refrigerator. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により圧縮空気を冷却してクーラーにすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas to supply tap water cooling heat to consumers, and compressed water is cooled by the tap water cooling heat. An all-blade steam gas turbine combined engine characterized by cooling to a cooler. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により圧縮空気を冷却して家庭用クーラーにすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas to supply tap water cooling heat to consumers, and compressed water is cooled by the tap water cooling heat. An all-rotor-steam gas turbine combined engine characterized by cooling to a home-use cooler. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、低温燃焼ガスにより水道水を冷却して水道水冷熱を需要家に供給して、その水道水冷熱により圧縮空気を冷却して業務用クーラーにすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., and a cold heat recovery device (102) is used to cool tap water with low-temperature combustion gas to supply tap water cooling heat to consumers, and compressed water is cooled by the tap water cooling heat. An all-rotor-steam gas turbine combined engine that is cooled to a commercial cooler. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇し、ドライアイスを回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade gas turbine whose combustion gas exhaust temperature approaches −273 ° C., the compressed air pressure of the combustor and heat exchanger 4 is raised to the limit by all the blades, and dry ice can be recovered. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇し、液体窒素を回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine whose combustion gas exhaust temperature approaches −273 ° C., the compressed air pressure of the combustor / heat exchanger 4 is raised to the limit by all the rotor blades so that liquid nitrogen can be recovered. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、冷熱回収器（１０２）の低温燃焼ガスにより水道水を冷却して貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that in a full-blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C, tap water is cooled and stored by the low-temperature combustion gas of the cold-heat recovery unit (102). 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、冷熱回収器（１０２）の低温燃焼ガスにより水道水を冷却して貯蔵して水道水冷熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  In a full blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C, tap water is cooled and stored by the low-temperature combustion gas of the cold heat recovery unit (102), and the cold water of the tap water is supplied to consumers. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇して冷熱回収器（１０２）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In a full blade gas turbine whose combustion gas exhaust temperature is close to −273 ° C., the compressed air pressure of the combustor / heat exchanger 4 is increased to the limit by using all the blades, and a cold recovery device (102) is used. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇し、冷熱回収器（１０２）の低温燃焼ガスにより水道水を冷却して貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C, the compressed air pressure of the combustor / heat exchanger 4 is raised to the limit by all the blades, and water is supplied by the low-temperature combustion gas from the cold heat recovery unit (102). An all-blade steam gas turbine combined engine characterized by cooling and storing water. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇し、冷熱回収器（１０２）の低温燃焼ガスにより水道水を冷却して貯蔵して水道水冷熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C, the compressed air pressure of the combustor / heat exchanger 4 is raised to the limit by all the blades, and water is supplied by the low-temperature combustion gas from the cold heat recovery unit (102). An all-blade steam gas turbine combined engine that cools and stores water to supply tap water cooling heat to consumers. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇し、冷熱回収器（１０２）でドライアイスを回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C, the compressed air pressure of the combustor / heat exchanger 4 can be raised to the limit by all the rotor blades, and dry ice can be recovered by the cold-heat recovery unit (102) An all-rotor-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける全動翼ガスタービンにおいて、燃焼器兼熱交換器４の圧縮空気圧力を全動翼により極限まで上昇し、冷熱回収器（１０２）で液体窒素を回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine whose combustion gas exhaust temperature approaches -273 ° C, the compressed air pressure of the combustor / heat exchanger 4 can be raised to the limit by all the rotor blades, and liquid nitrogen can be recovered by the cold-heat recovery unit (102) An all-rotor-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized by using a cold-heat recovery device (102) with the combustion gas exhaust temperature approaching -273 ° C. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吸入側を真空にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the exhaust temperature of the combustion gas is brought close to -273 ° C, the cold heat recovery device (102) is used, and the suction side of the all-blade blade fan (103) is evacuated. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吸入側を真空にしてドライアイスの製造を容易にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Full-motion, characterized in that the combustion gas exhaust temperature is brought close to −273 ° C. and the cold-heat recovery device (102) is used, and the suction side of the whole blade fan (103) is evacuated to facilitate the production of dry ice. Wing steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吸入側を真空にして液体窒素の製造を容易にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Full-motion, characterized in that the combustion gas exhaust temperature is brought close to −273 ° C., the cold heat recovery device (102) is used, and the suction side of the whole blade fan (103) is evacuated to facilitate the production of liquid nitrogen. Wing steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吐出側を攪拌することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the exhaust temperature of the combustion gas is brought close to −273 ° C. and the cold-heat recovery device (102) is used to stir the discharge side of the all-blade fan (103). 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吐出側を攪拌して冷熱回収を容易にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Total blade steam, characterized in that the exhaust temperature of the combustion gas is brought close to −273 ° C. and the cold energy recovery device (102) is used, and the discharge side of the total blade blade fan (103) is stirred to facilitate the recovery of cold energy. Gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吐出側を攪拌して冷熱回収水道水を冷却することを特徴とする全動翼蒸気ガスタービン合体機関。  A total moving blade characterized in that the exhaust temperature of the combustion gas is brought close to −273 ° C., a cold heat recovery device (102) is used, and the discharge side of the whole moving blade blower (103) is stirred to cool the cold heat recovery tap water. Steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吐出側を昇圧してＣＯ２等の燃焼ガスを水中に移動することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., a cold recovery device (102) is used, and the discharge side of all blade rotors (103) is pressurized to move combustion gas such as CO 2 into water. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吐出側を昇圧してＣＯ２等の燃焼ガスを水中に溶解することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., a cold heat recovery device (102) is used, and the discharge side of all blade rotors (103) is pressurized to dissolve combustion gas such as CO 2 in water. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吐出側を昇圧してＣＯ２等の燃焼ガスを水に溶解合成することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., a cold heat recovery device (102) is used, and the discharge side of all blade impeller (103) is boosted to dissolve and synthesize combustion gas such as CO 2 in water. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて冷熱回収器（１０２）を使用し、全動翼送風機（１０３）の吐出側を昇圧してＣＯ２等の燃焼ガスを化学物質と共に水に合成溶解することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas exhaust temperature is brought close to −273 ° C., a cold recovery device (102) is used, and the discharge side of all rotor blade blower (103) is pressurized to synthesize and dissolve combustion gas such as CO2 in water together with chemical substances. An all-blade steam gas turbine combined engine characterized by 燃焼ガス排気温度を−２７３℃に近付けて使用する冷熱回収器（１０２）の全動翼送風機（１０３）を、全動翼圧縮機と略同様に構成することを特徴とする全動翼蒸気ガスタービン合体機関。  Total blade steam gas characterized in that the entire blade blower (103) of the cold heat recovery unit (102) used with the combustion gas exhaust temperature approaching −273 ° C. is configured in substantially the same manner as the entire blade compressor. Turbine coalescence engine. 燃焼ガス排気温度を−２７３℃に近付けて使用する冷熱回収器（１０２）の全動翼送風機（１０３）を、全動翼圧縮機と略同様に二重反転磁気摩擦動力伝達装置（１４）を具備することを特徴とする全動翼蒸気ガスタービン合体機関。  The rotor blade fan (103) of the cold recovery device (102) used with the exhaust temperature of the combustion gas approaching -273 ° C is replaced with the counter rotating magnetic friction power transmission device (14) in substantially the same manner as the rotor blade compressor. An all-blade steam gas turbine combined engine comprising: 燃焼ガス排気温度を−２７３℃に近付けて使用する冷熱回収器（１０２）の全動翼送風機（１０３）を、全動翼圧縮機と略同様に送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）を具備することを特徴とする全動翼蒸気ガスタービン合体機関。  The whole blade blower (103) of the cold heat recovery unit (102) used with the combustion gas exhaust temperature approaching -273 ° C is used as a water pump and counter-rotating magnetic friction power transmission device (substantially the same as the whole blade compressor) ( 14a), a full blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付けて使用する冷熱回収器（１０２）の全動翼送風機（１０３）を、全動翼圧縮機と略同様に二重反転磁気摩擦動力伝達装置（１４）を具備して全動翼を二重反転することを特徴とする全動翼蒸気ガスタービン合体機関。  The rotor blade fan (103) of the cold recovery device (102) used with the exhaust temperature of the combustion gas approaching -273 ° C is replaced with the counter rotating magnetic friction power transmission device (14) in substantially the same manner as the rotor blade compressor. An all-rotor-blade steam gas turbine combined engine characterized by comprising: 燃焼ガス排気温度を−２７３℃に近付けて使用する冷熱回収器（１０２）の全動翼送風機（１０３）を、全動翼圧縮機と略同様に送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）を具備して全動翼を二重反転することを特徴とする全動翼蒸気ガスタービン合体機関。  The whole blade blower (103) of the cold heat recovery unit (102) used with the combustion gas exhaust temperature approaching -273 ° C is used as a water pump and counter-rotating magnetic friction power transmission device (substantially the same as the whole blade compressor) ( 14a), a full moving blade steam gas turbine combined engine characterized in that all moving blades are double-reversed. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. An all-blade steam gas turbine combined engine characterized by agglomerating water and water vapor with the combustion gas as the core and making it possible to separate and collect them as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、石炭灰を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), the combustion gas exhaust temperature approaches -273 ° C. An all-blade steam gas turbine combined engine characterized in that low temperature combustion gas containing ash is condensed into water and water vapor so that it can be collected separately as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Harmful in all rotor blade gas turbines driven by high temperature water (5b) with multiple temperatures such as supercritical temperature such as supercritical pressure equipped with electromagnetically heated turbine rotor blades (81) that bring combustion gas exhaust temperature close to -273 ° C An all-rotor-blade steam gas turbine combined engine, characterized by agglomerating water and water vapor using a low-temperature combustion gas containing a substance as a core, and making it possible to separate and collect them as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集し、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. An all-rotor-steam gas turbine combined engine characterized by agglomerating water and water vapor using a low-temperature combustion gas as a core and making it possible to separate and collect them as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、石炭灰を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. An all-blade steam gas turbine combined engine characterized in that low temperature combustion gas containing coal ash is condensed into water and water vapor so that it can be collected separately as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. An all-rotor-blade steam gas turbine combined engine, characterized by agglomerating water and water vapor using a low-temperature combustion gas containing harmful substances as a core, and allowing them to be collected separately as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperature, equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. An all-rotor-steam gas turbine combined engine that aggregates water and water vapor and makes it possible to separate and collect them as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、石炭灰を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature combustion including coal ash in an all blade gas turbine driven by high temperature water (5b) with multiple temperatures such as supercritical temperature, equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by agglomerating water and water vapor using gas as a core and making it possible to separate and collect soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature combustion containing harmful substances in all blade gas turbines driven by high temperature water (5b) with multiple temperatures such as supercritical temperature equipped with electromagnetically heated turbine blades (81) that bring combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by agglomerating water and water vapor using gas as a core and making it possible to separate and collect soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集し、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) that brings the combustion gas exhaust temperature close to -273 ° C, the low-temperature combustion gas is the core An all-rotor-steam gas turbine combined engine that aggregates water and water vapor and makes it possible to separate and collect them as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、石炭灰を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature containing coal ash in an all blade steam gas turbine driven by high temperature water (5b) having multiple temperatures such as supercritical temperature and equipped with an electromagnetically heated turbine rotor blade (81) that brings the combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by agglomerating water and water vapor with the combustion gas as the core and making it possible to separate and collect them as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備し超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature containing harmful substances in all blade steam gas turbines equipped with electromagnetically heated turbine blades (81) driven by high temperature water (5b) of multiple temperatures such as supercritical temperature, which brings combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by agglomerating water and water vapor with the combustion gas as the core and making it possible to separate and collect them as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with a rotor blade (81), water and water vapor are aggregated using a low-temperature combustion gas as a core. An all-rotor-blade steam gas turbine combined engine that can be separated and collected as water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine that is driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperature such as supercritical pressure, equipped with a rotor blade (81), water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core. Then, the all-rotor-blade steam gas turbine combined engine characterized in that it can be separated and collected as dredging or water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with a rotor blade (81), water and water vapor are aggregated using a low temperature combustion gas as a core, An all-blade steam gas turbine combined engine that can be collected separately as dredging or water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature such as supercritical pressure equipped with a rotor blade (81), water and water vapor are generated using low-temperature combustion gas containing harmful substances as a core. An all-rotor-steam gas turbine combined engine characterized by agglomerating and making it possible to separate and collect as soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperatures, equipped with a rotor blade (81), water and water vapor are aggregated using low-temperature combustion gas as a core, and separated into soot, water droplets, etc. An all-blade steam gas turbine combined engine characterized in that it can be recovered. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as supercritical temperatures, equipped with a rotor blade (81), water and water vapor are aggregated using a low-temperature combustion gas containing a harmful substance as a core. An all-rotor-blade steam gas turbine combined engine characterized in that it can be collected separately as water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine that is driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperatures, equipped with a rotor blade (81), water and water vapor are aggregated using a low-temperature combustion gas as a core to produce soot, water droplets, etc. An all-blade steam gas turbine combined engine characterized by enabling separate collection. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature and equipped with a rotor blade (81), water and water vapor are aggregated using a low-temperature combustion gas containing harmful substances as a core. An all-rotor-blade steam gas turbine combined engine that can be separated and collected as water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In the all-blade gas turbine driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature, water and water vapor are agglomerated with the low-temperature combustion gas as the core, and can be collected separately as soot and water droplets Steam gas turbine coalescing engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In all blade gas turbines driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature, water and water vapor are aggregated by using low-temperature combustion gas containing harmful substances as a core, and can be collected separately as soot and water droplets An all-blade steam gas turbine combined engine characterized by: 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature, water and water vapor are aggregated by using low-temperature combustion gas as a core, and can be separated and collected as soot and water droplets. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In all blade turbine gas turbines driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature, water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core, and can be collected separately as soot and water droplets An all-rotor-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. The water cooling blades (87) are provided in a ring-like manner in most parts of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally cast (84) into an assembly structure. An all-blade steam gas turbine combined engine characterized by 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. Water cooling blades (87) are provided annularly in each stage on most of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by that. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) A steam turbine that is driven by high-temperature water (5b) having a plurality of temperatures, wherein water and water vapor are aggregated using a low-temperature combustion gas as a core and can be separately collected as soot and water droplets. Combined organization. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) The all-blade gas turbine driven by high-temperature water (5b) with multiple temperatures is characterized by agglomeration of water and water vapor using low-temperature combustion gas containing harmful substances as a core so that it can be separated and collected as soot and water droplets. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) Full-motion blade steam gas turbine driven by high-temperature water (5b) at multiple temperatures, characterized by agglomeration of water and water vapor using the low-temperature combustion gas as the core to enable separate collection as soot and water droplets Wing steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等として分別回収可能にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In a full-blade steam gas turbine driven by high-temperature water (5b) at multiple temperatures, water and water vapor are aggregated using a low-temperature combustion gas containing harmful substances as a core, and can be collected separately as soot and water droplets. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. A water cooling blade (87) is provided in a ring shape in each paragraph in most of the outer compressor blade group (16) and the inner compressor blade group (17). Rotor steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) A water cooling blade (87) is provided in each ring in the most part of each of the outer compressor blade group (16) and the inner compressor blade group (17) having an assembled structure. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. Each outer blade gas turbine equipped with blades (81) driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure is formed in an annular structure integrally cast (84) to form an outer structure. An all-swing-blade steam gas turbine combined engine, characterized in that a water cooling blade (87) is provided in a ring-like manner in most of the compressor blade group (16) and the inner compressor blade group (17). 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature such as a supercritical pressure, provided with a blade (81), each is integrally formed into a ring (84) to form an assembly structure. An all-rotor-steam gas turbine combined engine characterized in that a water cooling blade (87) is provided in a ring-like manner in most of the outer compressor blade group (16) and the inner compressor blade group (17). 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けたことが特徴の全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, the outer compressor blade group (16) and the inner compressor blades which are integrally cast in a ring (84) to form an assembly structure An all-rotor-blade steam gas turbine combined engine characterized in that a water repellent water cooling blade (87) is provided annularly in each stage in the majority of the group (17). 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に撥水性水冷却翼（８７）を段落毎環状に設けたことが特徴の全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, each outer compressor blade group (16) and inner compressor operation formed into an assembly structure by integrally casting (84) in an annular shape An all-rotor-blade steam gas turbine combined engine characterized in that a water repellent water cooling blade (87) is provided annularly in each stage in most of the blade group (17). 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water repellent water cooling blade (87) is provided in most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) and assembled into a structure. An all-blade steam gas turbine combined engine characterized in that after one or more water-repellent water cooling blades are cooled, water is injected from water injection means (56). 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water repellent water cooling blade (87) is provided on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) which are integrally cast annularly (84) to form an assembly structure. An all-rotor-blade steam gas turbine combined engine, wherein one or more water-repellent water cooling blades are cooled and then water-injected by water-injecting means (56). 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. Each outer compressor blade group (assumed to have an assembly structure formed by integrally casting in a ring (84)) in an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures and having blades (81). 16) and an entire compressor blade steam gas turbine combined engine, characterized in that a water cooling blade (87) is provided annularly in each stage in most of the inner compressor rotor blade group (17). 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. Each outer compressor rotor blade group having an assembly structure formed by annular casting integrally (84) in an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature provided with blades (81) (16) A water-cooled blade (87) is provided in most of the inner compressor rotor blade group (17) in a ring-like manner in the entire rotor blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けたことが特徴の全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade gas turbine driven by high-temperature water (5b) at a high temperature, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (17) formed into an assembly structure by integrally casting in a ring (84). An all-rotor-blade steam gas turbine combined engine characterized in that most of the water-repellent water cooling blades (87) are provided annularly in each stage. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に撥水性水冷却翼（８７）を段落毎環状に設けたことが特徴の全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In the all-blade steam gas turbine driven by high-temperature water (5b) at a high temperature, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed in an annular shape (84) to form an assembly structure, respectively. An all-rotor-blade steam gas turbine combined engine characterized in that the water-repellent water cooling blades (87) are provided annularly in each stage in the majority of the engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. The outer compressor blade group (16) and the inner compressor blade group (17) in the assembled structure are provided with water-repellent water cooling blades (87), and one or more repellents are provided for each paragraph. An all-rotor-blade steam gas turbine combined engine, wherein water-cooling blades are cooled and then water-injected from water-injecting means (56). 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) Most of each of the outer compressor blade group (16) and the inner compressor blade group (17) having an assembly structure is provided with a water-repellent water cooling blade (87), so that one or more of each An all-rotor-blade steam gas turbine combined engine, wherein the water-repellent water cooling blades are cooled and then water-injected by water-injecting means (56). 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with a blade (81), an annular structure is integrally cast (84) as an assembly structure. Most of the compressor blade group (16) and the inner compressor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling one or more water-repellent water cooling blades per stage, 56) A full moving blade steam gas turbine combined engine characterized by water injection. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with a blade (81), each is integrally cast (84) into an annular structure. A water-repellent water cooling blade (87) is provided in most of the outer compressor blade group (16) and the inner compressor blade group (17), and water injection is performed after cooling one or more water-repellent water cooling blades in each paragraph. An all-blade steam gas turbine combined engine characterized in that water is injected from the means (56). 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature, the outer compressor blade group (16) and the inner compressor blades are formed as an assembly structure by integrally casting in a ring (84). A water repellent water cooling blade (87) is provided in the majority of the group (17), and water is ejected from the water ejecting means (56) after cooling one or more water repellent water cooling blades per paragraph. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, the outer compressor blade group (16) and the inner compressor operation are integrally formed in an annular shape (84) to form an assembly structure. A water repellent water cooling blade (87) is provided in the majority of the blade group (17), and water is sprayed from the water spraying means (56) after cooling one or more water repellent water cooling blades per paragraph. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. As an assembly structure by integrally casting (84), water repellent water cooling blades (87) are provided in most of the outer compressor blade groups (16) and inner compressor blade groups (17), An all-rotor-blade steam gas turbine combined engine characterized in that the water-repellent water-cooling blades of half or less of all the water-repellent water-cooling blades are cooled and then water-injected from the water-injecting means (56). 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する撥水性水冷却翼（８７）を含めたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) as an assembly structure by integrally casting (84) in an annular shape, An all-blade steam gas turbine combined engine characterized by including a water-repellent water cooling blade (87) that injects water from the water-injecting means (56) after cooling the water-repellent water-cooling blades of less than half each. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as supercritical temperature, provided with blades (81), each outer compressor blade group ( 16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling one or more water-repellent water cooling blades per stage, water injection from the water injection means (56) An all-blade steam gas turbine combined engine characterized by: 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature provided with blades (81), each outer compressor blade group is formed into an assembly structure by integrally casting (84) annularly. (16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling one or more water-repellent water cooling blades per stage, from the water injection means (56) An all-blade steam gas turbine combined engine characterized by water injection. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade gas turbine driven by high-temperature water (5b) at a temperature, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (17) are integrally formed in an annular shape (84) as an assembly structure. Mostly provided with water-repellent water cooling blades (87), and water-injecting means (56) jets water after cooling one or more water-repellent water-cooling blades in each paragraph, and the moving blade steam gas is characterized in that Turbine coalescence engine. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) at a temperature, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are formed as an assembly structure by integrally casting annularly (84). A water-repellent water cooling blade (87) is provided in most of the above, and water is sprayed from the water spraying means (56) after cooling one or more water-repellent water cooling blades in each paragraph after the cooling. Gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. As an assembly structure, water repellent water cooling blades (87) are provided in most of the outer compressor blade groups (16) and the inner compressor blade groups (17), and half or less of each paragraph is provided. An all-rotor-blade steam gas turbine combined engine, wherein water-cooling blades are cooled and then water-injected from water-injecting means (56). 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する撥水性水冷却翼（８７）を含めたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) As an assembly structure, most of the outer compressor blade group (16) and the inner compressor blade group (17) are provided with water-repellent water cooling blades (87), and each paragraph is less than half. An all-rotor-blade steam gas turbine combined engine comprising a water-repellent water cooling blade (87) that injects water from a water injection means (56) after cooling the water-repellent water cooling blade. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する撥水性水冷却翼（８７）を含めたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with a blade (81), an annular structure is integrally cast (84) as an assembly structure. Most of the compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and the water-repellent water cooling means is provided after cooling the water-repellent water cooling blades less than half of each paragraph. (56) An all-blade steam gas turbine combined engine characterized by including a water-repellent water cooling blade (87) that injects water from (56). 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する撥水性水冷却翼（８７）を含めたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with a blade (81), each is integrally cast (84) into an annular structure. A water-repellent water cooling blade (87) is provided in most of the outer compressor blade group (16) and the inner compressor blade group (17), and water injection is performed after cooling the water-repellent water cooling blades of half or less in every paragraph. An all-blade steam gas turbine combined engine comprising a water-repellent water cooling blade (87) that injects water from means (56). 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する撥水性水冷却翼（８７）を含めたことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature, the outer compressor blade group (16) and the inner compressor blades are formed as an assembly structure by integrally casting in a ring (84). A water repellent water cooling blade (87) is provided in a large part of the group (17), and the water repellent water cooling blade (87) which jets water from the water spraying means (56) after cooling the water repellent water cooling blade of half or less in every paragraph after cooling. (87) including the entire moving blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, the outer compressor blade group (16) and the inner compressor operation are integrally formed in an annular shape (84) to form an assembly structure. A water repellent water cooling blade (87) is provided in a large part of the blade group (17), and the water repellent water cooling blade is cooled by the water injection means (56) after cooling the half or less of the water repellent water cooling blade in every paragraph. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water-repellent water cooling blade (87) is provided in an annular manner in each paragraph in most of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally cast (84). An all-blade steam gas turbine combined engine comprising a device driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water repellent water cooling blade (87) is annularly formed in each paragraph in most of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine comprising a device that is provided and driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する撥水性水冷却翼（８７）を含めたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as supercritical temperature, provided with blades (81), each outer compressor blade group ( 16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling the water-repellent water cooling blades less than half of each paragraph, water is injected from the water injection means (56). An all-blade steam gas turbine combined engine including a water-repellent water cooling blade (87) for injection. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する撥水性水冷却翼（８７）を含めたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature provided with blades (81), each outer compressor blade group is formed into an assembly structure by integrally casting (84) annularly. (16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling the water-repellent water cooling blades of less than half of each paragraph from the water injection means (56) An all-blade steam gas turbine combined engine including a water-repellent water cooling blade (87) for jetting water. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する撥水性水冷却翼（８７）を含めたことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade gas turbine driven by high-temperature water (5b) at a temperature, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (17) are integrally formed in an annular shape (84) as an assembly structure. In most cases, a water-repellent water cooling blade (87) is provided, and the water-repellent water cooling blade (87) for spraying water from the water spraying means (56) after cooling the water-repellent water cooling blade of half or less in every paragraph is included. An all-blade steam gas turbine combined engine characterized by that. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) at a temperature, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are formed as an assembly structure by integrally casting annularly (84). A water-repellent water cooling blade (87) is provided in a large part of the water-repellent water-cooling blade (87), and the water-repellent water-cooling blade of half or less in every paragraph is cooled and then sprayed from the water spray means (56). Gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. ) And water repellent water cooling blades (87) are provided in a ring-like manner in most of the outer compressor blade group (16) and the inner compressor blade group (17) in the assembled structure. An all-blade steam gas turbine combined engine comprising a driving device. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) Most of the outer compressor blade group (16) and the inner compressor blade group (17) having the assembled structure are provided with water-repellent water cooling blades (87) in a ring shape for each stage, and the output An all-blade steam gas turbine combined engine comprising a device driven by 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. Each outer blade gas turbine equipped with blades (81) driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure is formed in an annular structure integrally cast (84) to form an outer structure. A feature is that a water-repellent water-cooling blade (87) is provided in a ring-like manner in most of the compressor blade group (16) and the inner compressor blade group (17), and is driven by the output. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature such as a supercritical pressure, provided with a blade (81), each is integrally formed into a ring (84) to form an assembly structure. The outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a device that is provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph and is driven by the output. An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, the outer compressor blade group (16) and the inner compressor blades which are integrally cast in a ring (84) to form an assembly structure An all-rotor-blade steam gas turbine combined engine characterized in that a water-repellent water-cooled blade (87) is provided in the annular portion of each stage in most of the group (17) and is driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, each outer compressor blade group (16) and inner compressor operation formed into an assembly structure by integrally casting (84) in an annular shape An all-swing-blade steam gas turbine combined engine characterized in that a water-repellent water-cooling blade (87) is provided in the annular portion of each stage in most of the blade group (17) and is driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water repellent water cooling blade (87) is provided in most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) and assembled into a structure. An all-bladed-blade steam gas turbine combined engine comprising a device that cools one or more water-repellent water-cooled blades after being cooled by water-injecting means (56) and is driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water repellent water cooling blade (87) is provided on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) which are integrally cast annularly (84) to form an assembly structure. An all-bladed-blade steam gas turbine combined engine comprising a device in which at least one or more water-repellent water cooling blades are cooled and then water-injected by water-injecting means (56) and driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. Each outer compressor blade group (assumed to have an assembly structure formed by integrally casting in a ring (84)) in an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures and having blades (81). 16) and the whole compressor blade group (17), a water repellent water cooling blade (87) is provided in an annular form in each paragraph, and a device for driving with this output is provided. Gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. Each outer compressor rotor blade group having an assembly structure formed by annular casting integrally (84) in an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature provided with blades (81) (16) and the inner compressor rotor blade group (17), a water repellent water cooling blade (87) is provided in an annular form in each paragraph, and a device for driving with the output is provided. Steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade gas turbine driven by high-temperature water (5b) at a high temperature, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (17) formed into an assembly structure by integrally casting in a ring (84). An all-rotor-blade steam gas turbine combined engine characterized by comprising a device that is provided with a water-repellent water cooling blade (87) in an annular shape and is driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In the all-blade steam gas turbine driven by high-temperature water (5b) at a high temperature, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed in an annular shape (84) to form an assembly structure, respectively. An all-blade steam gas turbine combined engine comprising a device that is provided with a water-repellent water cooling blade (87) in an annular shape and driven by the output in a large part. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. The outer compressor blade group (16) and the inner compressor blade group (17) in the assembled structure are provided with water-repellent water cooling blades (87), and one or more repellents are provided for each paragraph. An all-rotor-blade steam gas turbine combined engine characterized by comprising a device that cools the water-based water cooling blades and then injects water from the water injection means (56) and drives the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) Most of each of the outer compressor blade group (16) and the inner compressor blade group (17) having an assembly structure is provided with a water-repellent water cooling blade (87), so that one or more of each An all-rotor-blade steam gas turbine combined engine comprising a device for driving water-repellent water cooling blades after cooling the water-repellent water-cooling blades from the water-injecting means (56) and driving with the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. Each outer blade gas turbine equipped with blades (81) driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure is formed in an annular structure integrally cast (84) to form an outer structure. Most of the compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and water jetting means is provided after cooling one or more water-repellent water cooling blades per paragraph. (56) An all-rotor-steam gas turbine combined engine comprising a device that injects water from the drive and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮動機翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature such as a supercritical pressure, provided with a blade (81), each is integrally formed into a ring (84) to form an assembly structure. Most of the outer compressor blade group (16) and the inner compressor blade group (17) are provided with water-repellent water cooling blades (87), and water is injected after cooling one or more water-repellent water cooling blades in each paragraph. An all-blade steam gas turbine combined engine characterized by comprising a device that injects water from the means (56) and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, the outer compressor blade group (16) and the inner compressor blades which are integrally cast in a ring (84) to form an assembly structure Most of the group (17) is provided with water-repellent water cooling blades (87). After cooling one or more water-repellent water cooling blades per stage, water is sprayed from the water spraying means (56), and the output is An all-blade steam gas turbine combined engine comprising a driving device. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, each outer compressor blade group (16) and inner compressor operation formed into an assembly structure by integrally casting (84) in an annular shape A water-repellent water cooling blade (87) is provided in the majority of the blade group (17), and after cooling one or more water-repellent water cooling blades per paragraph, water is sprayed from the water spraying means (56), and the output An all-blade steam gas turbine combined engine comprising a device driven by 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. As an assembly structure by integrally casting (84), water repellent water cooling blades (87) are provided in most of the outer compressor blade groups (16) and inner compressor blade groups (17), An all-rotor-blade steam gas turbine combined engine comprising a device that cools the water-repellent water cooling blades of less than half of the water and then injects water from the water-injecting means (56) and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) as an assembly structure by integrally casting (84) in an annular shape, An all-rotor-blade steam gas turbine combined engine characterized by comprising a device that cools the water-repellent water-cooling blades of half or less after each cooling operation and sprays water from the water-injecting means (56) and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. Each outer compressor blade group (assumed to have an assembly structure formed by integrally casting in a ring (84)) in an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures and having blades (81). 16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling one or more water-repellent water cooling blades per stage, water is injected from the water injection means (56). An all-blade steam gas turbine combined engine comprising a device for injecting and driving at the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮動機翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In each full-blade steam gas turbine having blades (81) driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, each outer compression motor blade group having an assembly structure formed by annular casting integrally (84) (16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling one or more water-repellent water cooling blades per stage, from the water injection means (56) An all-rotor-blade steam gas turbine combined engine comprising a device that injects water and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade gas turbine driven by high-temperature water (5b) at a high temperature, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (17) formed into an assembly structure by integrally casting in a ring (84). Mostly, a water-repellent water cooling blade (87) is provided, and after cooling one or more water-repellent water cooling blades per stage, water is sprayed from the water spraying means (56) and driven by the output. An all-blade steam gas turbine combined engine characterized by that. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In the all-blade steam gas turbine driven by high-temperature water (5b) at a high temperature, the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed in an annular shape (84) to form an assembly structure, respectively. A water-repellent water cooling blade (87) is provided in the majority of the water-cooling device, and after cooling one or more water-repellent water cooling blades per stage, water is sprayed from the water spraying means (56) and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. As an assembly structure, water repellent water cooling blades (87) are provided in most of the outer compressor blade groups (16) and the inner compressor blade groups (17), and half or less of each paragraph is provided. An all-rotor-blade steam gas turbine combined engine characterized by comprising a device that cools the water-based water cooling blades and then injects water from the water injection means (56) and drives the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) As an assembly structure, most of the outer compressor blade group (16) and the inner compressor blade group (17) are provided with water-repellent water cooling blades (87), and each paragraph is less than half. An all-rotor-blade steam gas turbine combined engine comprising a device for driving water-repellent water cooling blades after cooling the water-repellent water-cooling blades from the water-injecting means (56) and driving with the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with a blade (81), an annular structure is integrally cast (84) as an assembly structure. Most of the compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and the water-repellent water cooling means is provided after cooling the water-repellent water cooling blades less than half of each paragraph. (56) An all-rotor-steam gas turbine combined engine comprising a device that injects water from the drive and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮動機翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with a blade (81), each is integrally cast (84) into an annular structure. A water-repellent water cooling blade (87) is provided in most of the outer compressor blade group (16) and the inner compressor blade group (17), and water injection is performed after cooling the water-repellent water cooling blades of half or less in every paragraph. An all-blade steam gas turbine combined engine characterized by comprising a device that injects water from the means (56) and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature, the outer compressor blade group (16) and the inner compressor blades are formed as an assembly structure by integrally casting in a ring (84). Most of the group (17) is provided with water-repellent water cooling blades (87). After cooling the water-repellent water cooling blades of less than half of each stage, water is sprayed from the water spraying means (56). An all-blade steam gas turbine combined engine comprising a driving device. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that rotate in opposite directions with a generator that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and the supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, the outer compressor blade group (16) and the inner compressor operation are integrally formed in an annular shape (84) to form an assembly structure. Most of the blade group (17) is provided with a water-repellent water cooling blade (87), and after cooling the water cooling blades of less than half of every paragraph, water is injected from the water injection means (56) and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising an apparatus for performing the above operation. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as supercritical temperature, provided with blades (81), each outer compressor blade group ( 16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling the water-repellent water cooling blades less than half of each paragraph, water is injected from the water injection means (56). An all-blade steam gas turbine combined engine comprising a device for injecting and driving at the output. 燃焼ガス排気温度を−２７３℃に近付ける送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮動機翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions, are coupled at the optimum rotation ratio by the water pump and counter-rotating magnetic friction power transmission device (14a) that brings the exhaust temperature of the combustion gas close to −273 ° C. In the all blade vane steam gas turbine equipped with blades (81) and driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures, each outer compression motor blade group is formed as an assembly structure by integrally casting (84) annularly. (16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87), and after cooling the water-repellent water cooling blades of less than half of each paragraph from the water injection means (56) An all-rotor-blade steam gas turbine combined engine comprising a device that injects water and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade gas turbine driven by high-temperature water (5b) at a temperature, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (17) are integrally formed in an annular shape (84) as an assembly structure. Mostly, a water-repellent water cooling blade (87) is provided, and after cooling the water-repellent water cooling blade of half or less in every paragraph, water is sprayed from the water spraying means (56) and driven by the output. An all-blade steam gas turbine combined engine characterized by that. 燃焼ガス排気温度を−２７３℃に近付ける発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けて、段落毎全部以下半分の水冷却翼を冷却後に水噴射手段（５６）より水噴射して、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator whose combustion gas exhaust temperature approaches −273 ° C. at an optimum rotation ratio, and a plurality of supercritical temperatures including an electromagnetically heated turbine rotor blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) at a temperature, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are formed as an assembly structure by integrally casting annularly (84). The water-repellent water cooling blade (87) is provided in most of the water-cooling blades, and the water-cooling blades of half or less in every paragraph are cooled and then sprayed with water from the water spraying means (56) and driven by the output. An all-blade steam gas turbine combined engine characterized by that. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine equipped with a moving blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, an inner structure is formed by integrally casting (84) in an annular shape. In the vicinity of the assembly annular connection part of the turbine rotor blade group (20), a water injection means (56a) is thermally insulated to cool the superheated steam to reduce the volume and increase the unit mass. Wing steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine An all-blade steam gas turbine equipped with a moving blade (81) driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, etc. In the vicinity of the assembly annular connection part of the turbine rotor blade group (19), the water injection means (56a) is provided with heat insulation to cool the superheated steam, and the volume is reduced to increase the unit mass. Wing steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine Inner turbine having an assembly structure formed by integrally casting in a ring (84) in an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with a rotor blade (81) A total moving blade characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the moving blade group (20) so as to cool the combustion gas, thereby reducing the volume and increasing the unit mass. Steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with a rotor blade (81), an inner turbine rotor blade group having an assembly structure formed by annular casting (84). 20) An all-blade steam gas turbine combination characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection of 20) to cool the superheated steam to reduce the volume and increase the unit mass. organ. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine Outer turbine rotor blade group having an assembly structure by integrally casting (84) annularly in an all rotor blade steam gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with a rotor blade (81). 19) An all-rotor-steam steam gas turbine combination characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection in 19) to cool the superheated steam to reduce the volume and increase the unit mass. organ. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as supercritical temperatures, provided with a blade (81), an inner turbine blade group (20 And a water jet means (56a) is provided in the vicinity of the assembly annular connection to cool the combustion gas to reduce the volume and increase the unit mass. . 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine An all-blade gas turbine equipped with a moving blade (81) driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, etc., and an outer turbine formed into an assembly structure by integrally casting (84) in an annular shape A total moving blade characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection of the moving blade group (19) so as to cool the combustion gas, thereby reducing the volume and increasing the unit mass. Steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as the supercritical temperature of the inner turbine rotor blade group (20) assembled in an annular shape and integrally cast (84), an assembly annular connection portion An all-blade steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity so as to cool the superheated steam to reduce the volume and increase the unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, an assembly annular connection of an outer turbine rotor blade group (19) integrally assembled (84) into an annular structure An all-rotor-steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity to provide heat insulation to cool superheated steam and combustion gas, thereby reducing the volume and increasing the unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as the supercritical temperature of the inner turbine rotor blade group (20) in the vicinity of the assembly annular connection in the annular integral casting (84) to form an assembly structure And an all-blade steam gas turbine combined engine characterized in that the water injection means (56a) is insulated to cool the combustion gas to reduce the volume and increase the unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as the supercritical temperature of the outer turbine rotor blade group (19) in the vicinity of the assembly annular connection in the annular integral casting (84) into an assembly structure And an all-blade steam gas turbine combined engine characterized in that the water injection means (56a) is insulated to cool the combustion gas to reduce the volume and increase the unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting in a ring (84) to cool superheated steam and combustion gas, An all-blade steam gas turbine combined engine characterized by reducing the volume and increasing unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. In the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by integrally casting in a ring (84), the water injection means (56a) is thermally insulated to cool the superheated steam and the combustion gas, An all-blade steam gas turbine combined engine characterized by reducing the volume and increasing unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water injection means (56a) is provided in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) that is integrally cast (84) to form an assembly structure to cool the combustion gas and reduce the volume. And an all-blade steam gas turbine combined engine characterized in that the unit mass is increased. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by integrally casting (84) to cool the combustion gas and reduce the volume. And an all-blade steam gas turbine combined engine characterized in that the unit mass is increased. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) which is integrally cast (84) into an assembly structure to cool the combustion gas and is driven by the output. An all-blade steam gas turbine combined engine characterized by comprising an apparatus for performing the above operation. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. In the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) which is integrally cast (84) into the assembly structure, the water injection means (56a) is thermally insulated to cool the superheated steam and the combustion gas, An all-blade steam gas turbine combined engine comprising a device driven by output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. A water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting in a ring (84) to cool superheated steam and combustion gas, An all-blade steam gas turbine combined engine comprising a device driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. In the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by integrally casting in a ring (84), the water injection means (56a) is thermally insulated to cool the superheated steam and the combustion gas, An all-blade steam gas turbine combined engine comprising a device driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures and provided with a rotor blade (81), an outer turbine rotor blade group (19) that is integrally formed in a ring (84) to form an assembly structure And a water jet means (56a) is provided in the vicinity of the assembly annular connection to cool the combustion gas to reduce the volume and increase the unit mass. . 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection is performed in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed in an annular integral casting (84) into an assembly structure. An all blade turbine gas turbine combined engine characterized in that the means (56a) is insulated to cool the superheated steam to reduce the volume and increase the unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection is performed in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine characterized in that the means (56a) is insulated to cool the superheated steam and combustion gas, thereby reducing the volume and increasing the unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection means is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) that is integrally cast in a ring (84) to form an assembly structure. (56a) is provided with heat insulation to cool the combustion gas, and the volume is reduced to increase the unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection means is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by annular casting (84). (56a) is provided with heat insulation to cool the combustion gas, and the volume is reduced to increase the unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) In the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) having an assembly structure, the water injection means (56a) is thermally insulated to cool the superheated steam and combustion gas and reduce the volume. An all-blade steam gas turbine combined engine characterized by increasing unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) In the vicinity of the assembly annular connection of the outer turbine rotor blade group (19) having an assembly structure, the water injection means (56a) is thermally insulated to cool the superheated steam and combustion gas and reduce the volume. An all-blade steam gas turbine combined engine characterized by increasing unit mass. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. ) In the vicinity of the assembly annular connection part of the inner turbine blade group (20) having an assembly structure, the water injection means (56a) is thermally insulated to cool the combustion gas, reduce the volume, and increase the unit mass. An all-blade steam gas turbine combined engine characterized by: 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. ) In the vicinity of the assembly annular connection of the outer turbine rotor blade group (19) having an assembly structure, the water injection means (56a) is thermally insulated to cool the combustion gas, reduce the volume, and increase the unit mass. An all-blade steam gas turbine combined engine characterized by: 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. In the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) having an assembly structure, a water injection means (56a) is provided with heat insulation to cool the combustion gas and drive with the output. An all-blade steam gas turbine combined engine characterized by that. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with an electromagnetically heated turbine rotor blade (81), the exhaust gas temperature of the combustion gas approaches -273 ° C. ) In the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) having an assembly structure, a water injection means (56a) is thermally insulated to cool the superheated steam and combustion gas, and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising: 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) A water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) having an assembly structure to cool the superheated steam and the combustion gas, and is driven by the output. An all-blade steam gas turbine combined engine comprising the apparatus. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) whose combustion gas exhaust temperature approaches -273 ° C, it is integrally cast in a ring ( 84) A water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) having an assembly structure so as to cool the superheated steam and the combustion gas, and is driven by the output. An all-blade steam gas turbine combined engine comprising the apparatus. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine Inner turbine having an assembly structure formed by integrally casting in a ring (84) in an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with a rotor blade (81) Whole blade steam characterized by comprising a device for cooling the combustion gas by providing a water injection means (56a) in the vicinity of the assembly annular connection of the blade group (20) to cool the combustion gas and drive with the output. Gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine An all-blade gas turbine equipped with a moving blade (81) driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, etc., and an outer turbine formed into an assembly structure by integrally casting (84) in an annular shape Whole blade steam characterized by comprising a device for heat-injecting water injection means (56a) in the vicinity of the assembly annular connection of the blade group (19) to cool the combustion gas and drive it with the output. Gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine equipped with a moving blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, an inner structure is formed by integrally casting (84) in an annular shape. A water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the turbine rotor blade group (20) so as to cool the superheated steam and combustion gas, and is driven by the output. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine An all-blade steam gas turbine equipped with a moving blade (81) driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, etc. In the vicinity of the assembly annular connection part of the turbine rotor blade group (19), the water injection means (56a) is provided with heat insulation to cool the superheated steam and the combustion gas and to drive with the output. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as the supercritical temperature of the inner turbine rotor blade group (20) in the vicinity of the assembly annular connection in the annular integral casting (84) to form an assembly structure And a water jet means (56a) provided with heat insulation to cool the combustion gas and to drive with this output. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as the supercritical temperature of the outer turbine rotor blade group (19) in the vicinity of the assembly annular connection in the annular integral casting (84) into an assembly structure And a water jet means (56a) provided with heat insulation to cool the combustion gas and to drive with this output. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as the supercritical temperature of the inner turbine rotor blade group (20) that is integrally cast in an annular shape and in the vicinity of the assembly annular connection, An all-blade steam gas turbine combined engine characterized by comprising a device that insulates the water injection means (56a), cools superheated steam and combustion gas, and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as the supercritical temperature of the outer turbine rotor blade group (19) integrally cast in an annular shape in the vicinity of the assembly annular connection, An all-blade steam gas turbine combined engine characterized by comprising a device that insulates the water injection means (56a), cools superheated steam and combustion gas, and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as supercritical temperatures, provided with a blade (81), an inner turbine blade group (20 ), A water jet means (56a) is provided with heat insulation in the vicinity of the assembly annular connection portion to cool the combustion gas and drive with the output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures and provided with a rotor blade (81), an outer turbine rotor blade group (19) that is integrally formed in a ring (84) to form an assembly structure ), A water jet means (56a) is provided with heat insulation in the vicinity of the assembly annular connection portion to cool the combustion gas and drive with the output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, provided with a rotor blade (81), an inner turbine rotor blade group having an assembly structure formed by annular casting (84). 20) An all-blade steam gas characterized in that a water jet means (56a) is provided in the vicinity of the assembly annular connection of 20) so as to cool the superheated steam and combustion gas and drive with the output. Turbine coalescence engine. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine Outer turbine rotor blade group having an assembly structure by integrally casting (84) annularly in an all rotor blade steam gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with a rotor blade (81). 19) An all-blade steam gas characterized by comprising a device for heat-insulating water (56a) in the vicinity of the assembly annular connection of 19) to cool the superheated steam and combustion gas and drive with the output. Turbine coalescence engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection means is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) that is integrally cast in a ring (84) to form an assembly structure. (56a) is provided with heat insulation to cool the combustion gas, and is provided with a device driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection means is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by annular casting (84). (56a) is provided with heat insulation to cool the combustion gas, and is provided with a device driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) that is integrally cast in an annular shape to form an assembly structure. ) Is provided with heat insulation to cool the superheated steam and combustion gas, and is equipped with a device driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, a water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) integrally cast in an annular shape and assembled. ) Is provided with heat insulation to cool the superheated steam and combustion gas, and is equipped with a device driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  Harmful in all rotor blade gas turbines driven by high temperature water (5b) with multiple temperatures such as supercritical temperature such as supercritical pressure equipped with electromagnetically heated turbine rotor blades (81) that bring combustion gas exhaust temperature close to -273 ° C An all-rotor-blade steam gas turbine combined engine, characterized by agglomerating water and water vapor into a soot, water droplets, etc., with a low-temperature combustion gas containing a substance as a core. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、石炭灰や有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. An all-blade steam gas turbine combined engine characterized by agglomerating water and water vapor into low temperature combustion gas containing coal ash and toxic substances to form soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature combustion containing harmful substances in all blade gas turbines driven by high temperature water (5b) with multiple temperatures such as supercritical temperature equipped with electromagnetically heated turbine blades (81) that bring combustion gas exhaust temperature close to -273 ° C An all-rotor-blade steam gas turbine combined engine characterized by agglomerating water and water vapor with gas as a core to form soot and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、石炭灰や有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) that brings the combustion gas exhaust temperature close to -273 ° C, coal ash and harmful substances An all-rotor-steam gas turbine combined engine characterized by agglomerating water or water vapor into a soot or water droplets using a low-temperature combustion gas containing as a core. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine that is driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperature such as supercritical pressure, equipped with a rotor blade (81), water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core. And a full moving blade steam gas turbine combined engine characterized by using dredging or water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、石炭灰や有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine that is driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperature such as supercritical pressure, equipped with a rotor blade (81), water is generated using low-temperature combustion gas containing coal ash and harmful substances as a core. An all-blade steam gas turbine combined engine characterized by coagulating water vapor and water vapor into water droplets and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In the all-blade gas turbine driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature, water and water vapor are aggregated by using low-temperature combustion gas containing harmful substances as the core, and it is characterized as soot and water droplets An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、石炭灰や有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In a all-blade steam gas turbine driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature, water and water vapor are aggregated using low-temperature combustion gas containing coal ash and harmful substances as cores to form soot and water droplets An all-blade steam gas turbine combined engine characterized by that. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  Harmful in all rotor blade gas turbines driven by high temperature water (5b) with multiple temperatures such as supercritical temperature such as supercritical pressure equipped with electromagnetically heated turbine rotor blades (81) that bring combustion gas exhaust temperature close to -273 ° C The low-temperature combustion gas containing the substance is aggregated into water and water vapor and separated into soot and water droplets, etc., discharged into water containing the substance that promotes the synthesis and dissolution of the separated harmful substances, and released close to harmless An all-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質を該合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. The low-temperature combustion gas containing toxic substances is aggregated into water and water vapor and separated as soot and water droplets, and the separated toxic substances are discharged into water containing substances that promote the synthesis and dissolution, approaching harmless and released. An all-blade steam gas turbine combined engine characterized by: 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine driven by high-temperature water (5b), such as supercritical temperature, equipped with a moving blade (81), water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core, and soot and water droplets An all-blade steam gas turbine combined engine characterized by: 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、石炭灰や有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine driven by high-temperature water (5b), such as supercritical temperature, equipped with a rotor blade (81), water and water vapor are aggregated using low-temperature combustion gas containing coal ash and harmful substances as the core. An all-blade steam gas turbine combined engine characterized by the use of dredging and water droplets. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In a full blade gas turbine driven by high-temperature water (5b) at multiple temperatures, all blade blade steam is characterized by agglomerating water or water vapor into a soot or water droplets using a low-temperature combustion gas containing harmful substances as a core. Gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、石炭灰や有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とすることを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In a full rotor blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures, water or water vapor is aggregated using low-temperature combustion gas containing coal ash or harmful substances as a core to form soot or water droplets. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質を該合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature combustion containing harmful substances in all blade gas turbines driven by high temperature water (5b) with multiple temperatures such as supercritical temperature equipped with electromagnetically heated turbine blades (81) that bring combustion gas exhaust temperature close to -273 ° C Water and water vapor are aggregated using gas as a core and separated into soot and water droplets, etc., and the separated harmful substances are discharged into water containing substances that promote the synthesis and dissolution, and released close to harmlessness. All-blade steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature containing harmful substances in an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) that brings the combustion gas exhaust temperature close to -273 ° C It is characterized by the fact that the combustion gas is condensed into water and water vapor and separated into soot and water droplets, and then discharged into water containing substances that promote the synthesis and dissolution of the separated harmful substances, and released close to harmlessness. Rotor steam gas turbine combined engine. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine that is driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperature such as supercritical pressure, equipped with a rotor blade (81), water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core. Then, it is separated into soot and water droplets, etc., discharged into water containing substances that promote the synthesis and dissolution of the separated harmful substances, and released into the vicinity of harmless discharge. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質を、該合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature such as supercritical pressure equipped with a rotor blade (81), water and water vapor are generated using low-temperature combustion gas containing harmful substances as a core. All rotor blade steam gas turbine combined, characterized in that it aggregates and separates as soot and water droplets, etc., and the separated harmful substances are discharged into water containing substances that promote the synthetic dissolution and approached harmlessly and released organ. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質を、該合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In all blade gas turbines driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature, water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as cores and separated into soot and water droplets. An all-rotor-steam gas turbine combined engine characterized in that harmful substances are discharged into water containing a substance that promotes the synthetic dissolution, and released close to harmlessly. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質を、該合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In all blade steam gas turbines driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature, water and water vapor are aggregated using low-temperature combustion gas containing toxic substances as cores and separated into soot and water droplets. An all-rotor-blade steam gas turbine combined engine characterized in that the harmful substances discharged are discharged into water containing substances that promote the synthesis and dissolution, and released close to harmlessness. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Harmful in all rotor blade gas turbines driven by high temperature water (5b) with multiple temperatures such as supercritical temperature such as supercritical pressure equipped with electromagnetically heated turbine rotor blades (81) that bring combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by comprising a device that agitates water and water vapor using a core of a low-temperature combustion gas containing substances and separates them as soot and water droplets, and drives them with the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas exhaust temperature approaches -273 ° C. An all-rotor-steam gas turbine combined engine characterized by comprising a device for aggregating water and water vapor using a low-temperature combustion gas containing harmful substances as a core and separating them as soot and water droplets, and driving them with the output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine driven by high-temperature water (5b), such as supercritical temperature, equipped with a moving blade (81), water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core, and soot and water droplets An all-rotor-blade steam gas turbine combined engine characterized by being separated into equal parts, discharged into water containing substances that promote the synthesis and dissolution of separated harmful substances, and released close to harmlessness. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質を、該合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, equipped with a rotor blade (81), water and water vapor are aggregated using a low-temperature combustion gas containing harmful substances as a core. An all-rotor-steam gas turbine combined engine characterized in that it is separated as water droplets and the like, and the separated harmful substances are discharged into water containing substances that promote the synthesis and dissolution, and released close to harmlessness. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質を、該合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water and water vapor are agglomerated using a low-temperature combustion gas containing harmful substances as a core to separate them as soot and water droplets. An all-rotor-blade steam gas turbine combined engine, which is discharged into water containing a substance that promotes synthetic dissolution, and is released close to harmlessness. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、分別した有害物質を、該合成溶解を促進する物質を含む水中に排出して、無害に近付けて放出することを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) at multiple temperatures, the low-temperature combustion gas containing harmful substances is aggregated into water and water vapor and separated into soot and water droplets, and the separated harmful substances are separated. An all-rotor-blade steam gas turbine combined engine, wherein the engine is discharged into water containing a substance that promotes the synthetic dissolution, and is released close to harmlessly. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature combustion containing harmful substances in all blade gas turbines driven by high temperature water (5b) with multiple temperatures such as supercritical temperature equipped with electromagnetically heated turbine blades (81) that bring combustion gas exhaust temperature close to -273 ° C An all-rotor-blade steam gas turbine combined engine comprising a device that agglomerates water and water vapor into a core and separates them as soot and water droplets, and drives them with the output. 燃焼ガス排気温度を−２７３℃に近付ける、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Low temperature containing harmful substances in an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81) that brings the combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by comprising a device that agglomerates water and water vapor into a combustion gas and separates them as soot and water droplets and drives them with the output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine that is driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperature such as supercritical pressure, equipped with a rotor blade (81), water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core. And an all-blade steam gas turbine combined engine characterized by comprising a device that separates it as soot and water droplets and drives it with the output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine driven by high-temperature water (5b) with multiple temperatures such as supercritical temperature such as supercritical pressure equipped with a rotor blade (81), water and water vapor are generated using low-temperature combustion gas containing harmful substances as a core. An all-rotor-blade steam gas turbine combined engine comprising a device that agglomerates and separates as soot and water droplets and drives with the output. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) with multiple temperatures, such as supercritical temperature, water and water vapor are aggregated by using low-temperature combustion gas containing harmful substances as a core and separated into soot and water droplets. An all-blade steam gas turbine combined engine comprising a device driven by 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device that rotate in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., and the like, a supercritical pressure equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature, water and water vapor are aggregated by using a low-temperature combustion gas containing harmful substances as a core and separated into soot and water droplets. An all-blade steam gas turbine combined engine comprising a device driven by output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade gas turbine driven by high-temperature water (5b), such as supercritical temperature, equipped with a moving blade (81), water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core, and soot and water droplets An all-blade steam gas turbine combined engine characterized in that it comprises a device that is separated as a unit and driven by the output. 燃焼ガス排気温度を−２７３℃に近付ける、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An outer shaft device and an inner shaft device that are rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) that brings the combustion gas exhaust temperature close to −273 ° C. are coupled at an optimum rotation ratio, and an electromagnetic heating turbine In an all-blade steam gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature, equipped with a rotor blade (81), water and water vapor are aggregated using a low-temperature combustion gas containing harmful substances as a core. An all-rotor-blade steam gas turbine combined engine comprising a device that separates water droplets or the like and drives the output. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, an apparatus for aggregating water and water vapor using a low-temperature combustion gas containing harmful substances as a core and separating it as soot and water droplets, and driving with this output An all-blade steam gas turbine combined engine characterized by comprising. 燃焼ガス排気温度を−２７３℃に近付ける、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、有害物質を含む低温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等として分別し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, bringing the combustion gas exhaust temperature close to −273 ° C., etc., and a supercritical temperature equipped with an electromagnetically heated turbine blade (81) In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, a device that agitates water and water vapor using a low-temperature combustion gas containing harmful substances as a core and separates it as soot and water droplets, and drives with this output An all-blade steam gas turbine combined engine characterized by comprising: 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade (81) In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, an inner turbine rotor blade having an assembly structure formed by annular casting integrally (84) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection of group (20). 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade (81) In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, an inner turbine rotor blade having an assembly structure formed by annular casting integrally (84) An all-blade steam gas turbine comprising a device for heat-insulating water (56a) in the vicinity of the assembly annular connection of the group (20) to cool the superheated steam and drive with the output Combined organization. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade (81) In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, an outer turbine rotor blade having an assembly structure formed by annular casting integrally (84) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection of group (19). 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade (81) In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, an outer turbine rotor blade having an assembly structure formed by annular casting integrally (84) An all-blade steam gas turbine characterized by comprising a device that cools the superheated steam by providing a water injection means (56a) in the vicinity of the assembly annular connection of the group (19), cools the superheated steam, and drives with the output. Combined organization. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are adiabatically expanded to a condenser vacuum and rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and are equipped with an electromagnetically heated turbine blade (81). In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a critical temperature, water injection means is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) integrally formed in an annular shape and assembled. An all-blade steam gas turbine combined engine provided with heat insulation (56a). 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are adiabatically expanded to a condenser vacuum and rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and are equipped with an electromagnetically heated turbine blade (81). In an all blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as critical temperature, in the vicinity of the assembly annular connection of the inner turbine blade group (20) formed into an assembly structure by annular casting (84), An all-blade steam gas turbine combined engine characterized by comprising a device that insulates the water injection means (56a), cools the superheated steam, and drives with the output. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are adiabatically expanded to a condenser vacuum and rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and are equipped with an electromagnetically heated turbine blade (81). In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a critical temperature, water injection means is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19) integrally cast in an annular structure. An all-blade steam gas turbine combined engine provided with heat insulation (56a). 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are adiabatically expanded to a condenser vacuum and rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and are equipped with an electromagnetically heated turbine blade (81). In an all blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as critical temperature, in the vicinity of the assembly annular connection of the outer turbine blade group (19) formed into an assembly structure by annularly casting integrally (84), An all-blade steam gas turbine combined engine characterized by comprising a device that insulates the water injection means (56a), cools the superheated steam, and drives with the output. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade (81) of an inner turbine rotor blade group (20) in an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature and integrally assembled (84) in an annular structure. An all-rotor-steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection in a thermally insulated manner. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade (81) of an inner turbine rotor blade group (20) in an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature and integrally assembled (84) in an annular structure. An all-rotor-blade steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection so as to be insulated to cool the superheated steam and is driven by the output. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade (81) of an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc. An all-rotor-steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection in a thermally insulated manner. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade (81) of an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc. An all-rotor-blade steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection so as to be insulated to cool the superheated steam and is driven by the output. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  Multi-temperature such as supercritical temperature equipped with electromagnetically heated turbine rotor blade (81), which combines the outer shaft device and the inner shaft device, which are adiabatically expanded to the condenser vacuum, rotating in opposite directions by the generator at the optimum rotation ratio In the all-blade steam turbine driven by high-temperature water (5b), the water injection means (56a) is thermally insulated near the assembly annular connection portion of the inner turbine rotor blade group (20) which is integrally cast into an annular structure. An all-blade steam gas turbine combined engine characterized by being provided as 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Multi-temperature such as supercritical temperature equipped with electromagnetically heated turbine rotor blade (81), which combines the outer shaft device and the inner shaft device, which are adiabatically expanded to the condenser vacuum, rotating in opposite directions by the generator at the optimum rotation ratio In the all-blade steam turbine driven by the high-temperature water (5b), the water injection means (56a) is provided in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) which is integrally cast in a ring (84) to form an assembly structure. ) Is provided in a thermally insulated manner to cool the superheated steam and is driven by the output. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  Multi-temperature such as supercritical temperature equipped with electromagnetically heated turbine rotor blade (81), which combines the outer shaft device and the inner shaft device, which are adiabatically expanded to the condenser vacuum, rotating in opposite directions by the generator at the optimum rotation ratio In the all-blade steam turbine driven by high-temperature water (5b), the water injection means (56a) is insulated near the assembly annular connection portion of the outer turbine rotor blade group (19) which is integrally cast in an annular shape and assembled. An all-blade steam gas turbine combined engine characterized by being provided as 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Multi-temperature such as supercritical temperature equipped with electromagnetically heated turbine rotor blade (81), which combines the outer shaft device and the inner shaft device, which are adiabatically expanded to the condenser vacuum, rotating in opposite directions by the generator at the optimum rotation ratio In the all-blade steam turbine driven by high-temperature water (5b), water injection means (56a) is provided in the vicinity of the assembly annular connection of the outer turbine rotor blade group (19) formed into an assembly structure by integrally casting (84) annularly. ) Is provided in a thermally insulated manner to cool the superheated steam and is driven by the output. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade An inner turbine blade group having an assembly structure formed by annular casting (84) in an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure. An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is thermally insulated in the vicinity of the assembly annular connection of (20). 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade An inner turbine blade group having an assembly structure formed by annular casting (84) in an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure. (20) An all-blade steam gas turbine combination comprising a device for heat-insulating the water-injecting means (56a) in the vicinity of the assembly annular connection portion of (20) to cool the superheated steam and drive with the output. organ. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade Outer turbine rotor blade group having an assembly structure formed by annular casting (84) in an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure having (81) (19) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection of (19). 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade Outer turbine rotor blade group having an assembly structure formed by annular casting (84) in an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure having (81) (19) An all-blade steam gas turbine unit comprising a device for heat-insulating the water-heating means (56a) in the vicinity of the assembly annular connection of (19) to cool the superheated steam and drive it with the output. organ. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are adiabatically expanded to a condenser vacuum and rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and are equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as critical temperature, water is placed in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed into an assembly structure by annular casting (84). An all-blade steam gas turbine combined engine characterized in that the injection means (56a) is provided in a thermally insulated manner. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are adiabatically expanded to a condenser vacuum and rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and are equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as critical temperature, water is placed in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed into an assembly structure by annular casting (84). An all-blade steam gas turbine combined engine comprising a device that insulates the injection means (56a), cools the superheated steam, and drives with the output. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are adiabatically expanded to a condenser vacuum and rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and are equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as critical temperature, water is placed in the vicinity of the assembly annular connection of the outer turbine rotor blade group (19) formed into an assembly structure by annular casting (84). An all-blade steam gas turbine combined engine characterized in that the injection means (56a) is provided in a thermally insulated manner. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which are adiabatically expanded to a condenser vacuum and rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and are equipped with an electromagnetically heated turbine blade (81). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as critical temperature, water is placed in the vicinity of the assembly annular connection of the outer turbine rotor blade group (19) formed into an assembly structure by annular casting (84). An all-blade steam gas turbine combined engine comprising a device that insulates the injection means (56a), cools the superheated steam, and drives with the output. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade Assembling of the inner turbine rotor blade group (20) having an assembling structure by annular casting (84) in the all blade steam gas turbine driven by the high temperature water (5b) having a plurality of temperatures such as the supercritical temperature provided with (81) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the annular connection portion in a thermally insulated manner. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade Assembling of the inner turbine rotor blade group (20) having an assembling structure by annular casting (84) in the all blade steam gas turbine driven by the high temperature water (5b) having a plurality of temperatures such as the supercritical temperature provided with (81) An all-rotor-blade steam gas turbine combined engine comprising a device that insulates water injection means (56a) in the vicinity of the annular connection portion, cools the superheated steam, and drives with the output. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade Assembling of the outer turbine rotor blade group (19) having an assembly structure by annular casting (84) in an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature provided with (81) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the annular connection portion in a thermally insulated manner. 復水器真空まで断熱膨張させる、送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device, which rotate in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a), which are adiabatically expanded to a condenser vacuum, are coupled at an optimum rotation ratio, and an electromagnetically heated turbine blade Assembling of the outer turbine rotor blade group (19) having an assembly structure by annular casting (84) in an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature provided with (81) An all-rotor-blade steam gas turbine combined engine comprising a device that insulates water injection means (56a) in the vicinity of the annular connection portion, cools the superheated steam, and drives with the output. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  Multi-temperature such as supercritical temperature equipped with electromagnetically heated turbine rotor blade (81), which combines the outer shaft device and the inner shaft device, which are adiabatically expanded to the condenser vacuum, rotating in opposite directions by the generator at the optimum rotation ratio In the all-blade steam gas turbine driven by the high-temperature water (5b), the water injection means (56a) is provided in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed into an assembly structure by annular casting (84). An all-blade steam gas turbine combined engine characterized in that it is insulated. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Multi-temperature such as supercritical temperature equipped with electromagnetically heated turbine rotor blade (81), which combines the outer shaft device and the inner shaft device, which are adiabatically expanded to the condenser vacuum, rotating in opposite directions by the generator at the optimum rotation ratio In the all-blade steam gas turbine driven by the high-temperature water (5b), the water injection means (56a) is provided in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed into an assembly structure by annular casting (84). An all-blade steam gas turbine combined engine comprising a device that is provided with heat insulation to cool superheated steam and is driven by the output. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  Multi-temperature such as supercritical temperature equipped with electromagnetically heated turbine rotor blade (81), which combines the outer shaft device and the inner shaft device, which are adiabatically expanded to the condenser vacuum, rotating in opposite directions by the generator at the optimum rotation ratio In the all-blade steam gas turbine driven by the high-temperature water (5b), water injection means (56a) is provided near the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by annular casting (84). An all-blade steam gas turbine combined engine characterized in that it is insulated. 復水器真空まで断熱膨張させる、発電機により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Multi-temperature such as supercritical temperature equipped with electromagnetically heated turbine rotor blade (81), which combines the outer shaft device and the inner shaft device, which are adiabatically expanded to the condenser vacuum, rotating in opposite directions by the generator at the optimum rotation ratio In the all-blade steam gas turbine driven by the high-temperature water (5b), water injection means (56a) is provided near the assembly annular connection portion of the outer turbine rotor blade group (19) formed into an assembly structure by annular casting (84). An all-blade steam gas turbine combined engine comprising a device that is provided with heat insulation to cool superheated steam and is driven by the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンのタービン翼を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the turbine blades of the all-blade gas turbine driven in (5b) are heated to electromagnetic heat. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンのタービン翼を電磁加熱高温としたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the turbine blades of the all-blade steam gas turbine driven in (5b) are heated to electromagnetic heating. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンのタービン翼を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the turbine blades of the all-blade steam turbine driven in (5b) have a high electromagnetic heating temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの高温水噴射ノズル（５９ｂ）を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59b) of the all-blade gas turbine driven by (5b) is heated to electromagnetic heating. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの高温水噴射ノズル（５９ｂ）を電磁加熱高温としたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59b) of the all-blade steam gas turbine driven in (5b) is heated to an electromagnetic heating temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの高温水噴射ノズル（５９ｂ）を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59b) of the all-blade steam turbine driven by (5b) is heated to electromagnetic heating. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの電磁加熱噴口（８３）を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the electromagnetic heating nozzle (83) of the all-blade gas turbine driven in (5b) is heated to a high electromagnetic heating temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの電磁加熱噴口（８３）を電磁加熱高温としたことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the electromagnetic heating nozzle (83) of the all-blade steam gas turbine driven in (5b) has a high electromagnetic heating temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの電磁加熱噴口（８３）を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  High temperature water such as a supercritical temperature such as a supercritical pressure in which an outer shaft device and an inner shaft device rotated in opposite directions by a water pump and counter-rotating magnetic friction power transmission device (14a) are coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the electromagnetic heating nozzle (83) of the all-blade steam turbine driven in (5b) is heated to an electromagnetic heating high temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側タービン動翼群（１９）及び内側タービン動翼群（２０）としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures, etc., each outer turbine rotor blade group (19) and inner turbine formed into an assembly structure by annularly casting integrally (84) An all-blade steam gas turbine combined engine characterized by being a moving blade group (20). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側タービン動翼群（１９）及び内側タービン動翼群（２０）としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures, etc., each outer turbine rotor blade group (19) and inner structure formed into an assembly structure by annularly casting integrally (84) An all-blade steam gas turbine combined engine characterized by being a turbine rotor blade group (20). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor rotor blade group in an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., which is integrally cast in a ring (84). (16) and an inner compressor rotor blade group (17). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor blade of an all-blade steam gas turbine driven by a plurality of high-temperature water (5b) such as a supercritical temperature such as an annular structure integrally cast (84) An all-blade steam gas turbine combined engine characterized by comprising a group (16) and an inner compressor blade group (17). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor rotor blade group in an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., which is integrally cast in a ring (84). (16) A water-repellent water cooling blade (87) is provided in the majority of the inner compressor rotor blade group (17), and the entire rotor blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor blade of an all-blade steam gas turbine driven by a plurality of high-temperature water (5b) such as a supercritical temperature such as an annular structure integrally cast (84) An all-blade steam gas turbine combined engine characterized in that a water repellent water cooling blade (87) is provided in most of the group (16) and the inner compressor blade group (17). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンのタービン翼を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all-blade steam gas turbine combined engine, characterized in that the turbine blades of the all-blade gas turbine are heated to electromagnetic heating. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンのタービン翼を電磁加熱高温としたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the turbine blades of the all-blade steam gas turbine are heated to electromagnetically heated high temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンのタービン翼を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the turbine blades of all-blade steam turbines are heated to electromagnetic heating. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの高温水噴射ノズル（５９ｂ）を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59b) of the all-blade gas turbine to be heated to electromagnetic heating. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの高温水噴射ノズル（５９ｂ）を電磁加熱高温としたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59b) of the all-blade steam gas turbine that is heated to electromagnetically heated high temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの高温水噴射ノズル（５９ｂ）を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59b) of the all-blade steam turbine that is heated to electromagnetically heated high temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの電磁加熱噴口（８３）を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all rotor blade steam gas turbine combined engine characterized in that the electromagnetic heating nozzle (83) of the all rotor blade gas turbine is heated to an electromagnetic heating high temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの電磁加熱噴口（８３）を電磁加熱高温としたことを特徴とする全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the electromagnetic heating nozzle (83) of the all-blade steam gas turbine that is heated is set to an electromagnetic heating high temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を、最適回転比で結合した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの電磁加熱噴口（８３）を電磁加熱高温としたことが特徴の全動翼蒸気ガスタービン合体機関。  The outer shaft device and the inner shaft device rotating in opposite directions are driven by the water pump and counter-rotating magnetic friction power transmission device (14a) with high-temperature water (5b) at multiple temperatures such as supercritical temperature combined at the optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the electromagnetic heating nozzle (83) of the all-blade steam turbine is heated to a high electromagnetic heating temperature. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側タービン動翼群（１９）及び内側タービン動翼群（２０）としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all blade gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, the outer turbine blade group (19) and the inner turbine blade group (20 All-blade steam gas turbine combined engine characterized by the above. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした夫々の外側タービン動翼群（１９）及び内側タービン動翼群（２０）としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, the outer turbine blade group (19) and the inner turbine blade group (19) and the inner turbine blade group (assumed to be assembled integrally by annular casting (84)). 20) An all-rotor-blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of equal temperatures, each outer compressor rotor blade group (16) and an inner side are formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine characterized by being a compressor blade group (17). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In a full blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, each outer compressor blade group (16) formed into an assembly structure by integrally casting (84) annularly An all compressor blade steam gas turbine combined engine characterized by being an inner compressor rotor blade group (17). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of equal temperatures, each outer compressor rotor blade group (16) and an inner side are formed into an assembly structure by integrally casting (84) in an annular shape. An all-rotor-steam gas turbine combined engine characterized in that a water-repellent water-cooled blade (87) is provided in most of the compressor blade group (17). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In a full blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, each outer compressor blade group (16) formed into an assembly structure by integrally casting (84) annularly An all-blade steam gas turbine combined engine characterized in that a water repellent water cooling blade (87) is provided in a large part of the inner compressor blade group (17). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor rotor blade group in an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., which is integrally cast in a ring (84). (16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, water injection means (56) An all-blade steam gas turbine combined engine characterized by water injection from (56). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor blade of an all-blade steam gas turbine driven by a plurality of high-temperature water (5b) such as a supercritical temperature such as an annular structure integrally cast (84) Most of the group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and water injection is performed after cooling one or more water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine characterized in that water is injected from the means (56). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of equal temperatures, each outer compressor rotor blade group (16) and an inner side are formed into an assembly structure by integrally casting (84) in an annular shape. Most of the compressor rotor blade group (17) is provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, water is supplied from the water injection means (56). An all-blade steam gas turbine combined engine characterized by injection. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In a full blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, each outer compressor blade group (16) formed into an assembly structure by integrally casting (84) annularly Most of the inner compressor rotor blade group (17) is provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, the water injection means (56) An all-blade steam gas turbine combined engine characterized by water injection. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor rotor blade group in an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., which is integrally cast in a ring (84). (16) and most of the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and water jetting means is provided after cooling the water-repellent water cooling blades of less than half in every paragraph. (56) An all-blade steam gas turbine combined engine characterized by water injection from (56). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor blade of an all-blade steam gas turbine driven by a plurality of high-temperature water (5b) such as a supercritical temperature such as an annular structure integrally cast (84) Most of the group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and water injection is performed after cooling the half of the water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine characterized in that water is injected from the means (56). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of equal temperatures, each outer compressor rotor blade group (16) and an inner side are formed into an assembly structure by integrally casting (84) in an annular shape. Most of the compressor blade groups (17) are provided with water-repellent water cooling blades (87) in an annular shape for each stage, and after cooling the water-repellent water cooling blades of half or less for each stage, water is supplied from the water injection means (56). An all-blade steam gas turbine combined engine characterized by injection. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In a full blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, each outer compressor blade group (16) formed into an assembly structure by integrally casting (84) annularly Most of the inner compressor rotor blade group (17) is provided with a water-repellent water cooling blade (87) in an annular shape for each stage, and after cooling the water-repellent water cooling blades of less than half of each stage, the water injection means (56) An all-blade steam gas turbine combined engine characterized by water injection. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor blade group (16) which is integrally cast in a ring (84) and communicates with the water channel as an assembly structure in an all blade gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature And most of the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and after the cooling of the water-repellent water cooling blades, which are less than half of each paragraph, An all-rotor-blade steam gas turbine combined engine characterized by water injection. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., each outer compressor blade group (16) integrally cast in a ring (84) and communicated with a water channel as an assembly structure. ) And most of the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in an annular shape for each stage, and after cooling the water-repellent water cooling blades for less than half of each stage, the water injection means (56 ) An all-blade steam gas turbine combined engine characterized by water injection. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all rotor blade gas turbine driven by high temperature water (5b) having a plurality of temperatures, the outer compressor blade groups (16) and the inner compressor blades which are integrally cast in a ring (84) and communicated with the water channel as an assembly structure Water repellent water cooling blades (87) are provided in the ring of each stage in the majority of the group (17), and water is sprayed from the water spraying means (56) after cooling the water-repellent water cooling blades of less than half of each stage. An all-blade steam gas turbine combined engine characterized by 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, each outer compressor blade group (16) and inner compressor motion that are integrally cast in a ring (84) and communicated with the water channel as an assembly structure Most of the blade group (17) is provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and after the cooling of the water-repellent water cooling blades of less than half of each paragraph, water is injected from the water injection means (56). An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor rotor blade group in an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., which is integrally cast in a ring (84). (16) and an inner compressor rotor blade group (17), a water-repellent water cooling blade (87) is provided in a ring-like manner in each paragraph and is driven by the output. Gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor blade of an all-blade steam gas turbine driven by a plurality of high-temperature water (5b) such as a supercritical temperature such as an annular structure integrally cast (84) A whole moving blade characterized in that a water repellent water cooling blade (87) is provided annularly in each stage and driven by the output in most of the group (16) and the inner compressor blade group (17). Steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of equal temperatures, each outer compressor rotor blade group (16) and an inner side are formed into an assembly structure by integrally casting (84) in an annular shape. An all-swing-blade steam gas turbine combined engine characterized in that a water-repellent water-cooling blade (87) is provided in a ring shape for each stage in a large part of the compressor rotor blade group (17) and driven by the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In a full blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, each outer compressor blade group (16) formed into an assembly structure by integrally casting (84) annularly A full-blade steam gas turbine combined engine characterized in that a water-repellent water-cooled blade (87) is provided annularly in each stage and driven by the output in the majority of the inner compressor blade group (17). . 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor rotor blade group in an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., which is integrally cast in a ring (84). (16) and most of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, water injection means (56) An all-blade steam gas turbine combined engine comprising a device for injecting water and driving with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor blade of an all-blade steam gas turbine driven by a plurality of high-temperature water (5b) such as a supercritical temperature such as an annular structure integrally cast (84) Most of the group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and water injection is performed after cooling one or more water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine comprising a device that injects water from the means (56) and drives with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5b) having a plurality of equal temperatures, each outer compressor rotor blade group (16) and an inner side are formed into an assembly structure by integrally casting (84) in an annular shape. Most of the compressor rotor blade group (17) is provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, water is supplied from the water injection means (56). An all-blade steam gas turbine combined engine comprising a device for injecting and driving at the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In a full blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, each outer compressor blade group (16) formed into an assembly structure by integrally casting (84) annularly Most of the inner compressor rotor blade group (17) is provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, the water injection means (56) An all-blade steam gas turbine combined engine comprising a device for jetting water and driving at the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Each outer compressor blade group (16) which is integrally cast in a ring (84) and communicates with the water channel as an assembly structure in an all blade gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature And most of the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in an annular shape for each paragraph, and after the cooling of the water-repellent water cooling blades, which are less than half of each paragraph, An all-blade steam gas turbine combined engine comprising a device that injects water more and drives with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., each outer compressor blade group (16) integrally cast in a ring (84) and communicated with a water channel as an assembly structure. ) And most of the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in an annular shape for each stage, and after cooling the water-repellent water cooling blades for less than half of each stage, the water injection means (56 And an all-blade steam gas turbine combined engine comprising a device for injecting water and driving at the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all blade gas turbine driven by high temperature water (5b) having a plurality of temperatures, the outer compressor blade groups (16) and the inner compressor blades that are integrally cast in a ring (84) and communicated with the water channel as an assembly structure Most of the group (17) is provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and after the cooling of the water-repellent water cooling blades of less than half of each paragraph, water is injected from the water injection means (56). An all-blade steam gas turbine combined engine comprising a device driven by the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, each outer compressor blade group (16) and inner compressor motion that are integrally cast in a ring (84) and communicated with the water channel as an assembly structure Most of the blade group (17) is provided with a water-repellent water cooling blade (87) in an annular shape for each stage, and after the cooling of the water-repellent water cooling blades of less than half of each stage, the water jetting means (56) sprays water. And an all-blade steam gas turbine combined engine comprising a device driven by the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures, etc., water injection is performed on the inner turbine rotor blade group (20) which is integrally formed in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine provided with means (56a). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, water injection is performed on the outer turbine rotor blade group (19) which is integrally formed in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine provided with means (56a). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as an inner turbine rotor blade group (20) formed into an assembly structure by annular casting (84), water injection means (56a) An all-blade steam gas turbine combined engine provided with (56a). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as an outer turbine rotor blade group (19) that is integrally cast (84) in an annular shape, (56a) An all-blade steam gas turbine combined engine provided with (56a). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as an inner turbine rotor blade group (20) formed into an assembly structure by integrally casting in a ring (84), water injection means (56a) An all-blade steam gas turbine combined engine provided with (56a). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures, water injection means is provided to the outer turbine rotor blade group (19) integrally formed in an annular shape (84) to form an assembly structure. (56a) An all-blade steam gas turbine combined engine provided with (56a). 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection means (56a) is provided in the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) in an annular shape. An all-blade steam gas turbine combined engine characterized by being provided. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of equal temperatures, a water injection means (56a) is provided on an outer turbine rotor blade group (19) formed into an assembly structure by integrally casting (84) in a ring. An all-blade steam gas turbine combined engine characterized by being provided. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection means (56a) is provided in the inner turbine rotor blade group (20) that is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high temperature water (5b) having a plurality of temperatures, water injection means (56a) is provided in an outer turbine rotor blade group (19) that is integrally cast in a ring (84) to form an assembly structure. An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam turbine driven by high temperature water (5b) having a plurality of equal temperatures, a water injection means (56a) is provided in the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) annularly. An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）に、水噴射手段（５６ａ）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection means (56a) is provided in the outer turbine rotor blade group (19) that is integrally cast (84) in an annular shape to form an assembly structure. An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., an assembly annular connection of an inner turbine blade group (20) formed into an assembly structure by annular casting integrally (84) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the section to insulate to cool the superheated steam, to reduce the volume and to increase the unit mass. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., an assembly annular connection portion of an inner turbine rotor blade group (20) formed into an assembly structure by annularly casting integrally (84) An all-blade steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity so as to cool the superheated steam to reduce the volume and increase the unit mass. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures, etc., an assembly annular connection portion of an inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) in an annular shape An all-blade steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity so as to cool the superheated steam to reduce the volume and increase the unit mass. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water is formed in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20) formed into an assembly structure by annularly casting integrally (84). An all-blade steam gas turbine combined engine characterized in that the injection means (56a) is provided so as to cool the superheated steam to reduce the volume and increase the unit mass. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, water injection is performed in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed into an assembly structure by integrally casting (84) in an annular shape. An all blade turbine gas turbine combined engine characterized in that the means (56a) is insulated to cool the superheated steam to reduce the volume and increase the unit mass. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小し単位質量を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam turbine driven by high-temperature water (5b) having a plurality of equal temperatures, water injection is performed in the vicinity of the assembly annular connection of the inner turbine rotor blade group (20) formed into an annular integral casting (84). An all blade turbine gas turbine combined engine characterized in that the means (56a) is insulated to cool the superheated steam to reduce the volume and increase the unit mass. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの内側軸装置を中空として、霧吹きの原理（９１）を利用して前方の空気を吸引噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The inner shaft device of the whole rotor blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is made hollow, and the forward air is sucked and injected by using the spraying principle (91). An all-blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの内側軸装置を中空として、霧吹きの原理（９１）を利用して前方の空気を吸引噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The inner shaft device of a full-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature is made hollow, and the front air is sucked and injected by using the spraying principle (91). An all-blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの内側軸装置を中空として、霧吹きの原理（９１）を利用して前方の空気を吸引噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The inside shaft device of the all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperature such as a hollow is made hollow, and the forward air is sucked and injected by using the spraying principle (91). An all-blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A total moving blade characterized in that a combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the entire moving blade gas turbine driven by high temperature water (5b) such as supercritical temperature such as Steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as supercritical temperature, etc. Wing steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A full blade provided with a combustion gas outlet (88) at the outlet of the combustor and heat exchanger of a full blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as supercritical temperature Steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、マイクロガスタービンを駆動することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the whole blade gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the micro gas turbine is driven. An all-blade steam gas turbine combined engine characterized by 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、マイクロガスタービンを駆動することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade vane steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature to drive the micro gas turbine An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに於いて、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In a full blade gas turbine driven by high temperature water (5b) with multiple temperatures such as supercritical temperature, etc., high temperature water is injected from one or more special devices (92a) using the spraying principle (91e) And an all-blade steam gas turbine combined engine characterized by sucking and injecting the air ahead. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに於いて、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical temperature, high-temperature water is supplied from one or more special devices (92a) using a spraying principle (91e). An all-blade steam gas turbine combined engine characterized by injecting and sucking and injecting forward air. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91b) An all-blade steam gas turbine combined engine characterized in that combustion gas is injected from one or more special devices (92b) using the above, and the air in front is sucked and injected. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91b) An all-blade steam gas turbine combined engine characterized in that combustion gas is injected from one or more special devices (92b) and the air in front is sucked and injected. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに於いて、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical temperature, high-temperature water is supplied from one or more water injection devices (93a) by using a spraying principle (91c). A full moving blade steam gas turbine combined engine characterized by injecting and sucking and injecting water in front. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに於いて、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., the hot water is more than one or more water injection devices (93a) using the spraying principle (91c). And an all-blade steam gas turbine combined engine characterized by sucking and injecting water in front. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91d) An all-blade steam gas turbine combined engine characterized in that combustion gas is injected from one or more water injection devices (93b) using the above, and water in front is sucked and injected. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of a full blade steam turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91d) An all-blade steam gas turbine combined engine characterized in that combustion gas is injected from one or more water injection devices (93b) and the water in front is sucked and injected. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91c) All blade blade steam characterized in that high temperature water and combustion gas are injected from each of one or more water injection devices (93a) and (93b) using (91d), and the water in front is sucked and injected. Gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade steam turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91c) ( 91d) is used to inject high temperature water and combustion gas from each of the one or more water injection devices (93a) and (93b), and suck and inject the water in front of the whole blade steam gas. Turbine coalescence engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91e) The whole blade steam gas is characterized in that high temperature water and combustion gas are injected from each of one or more special devices (92a) and (92b) by using (91b), and the air in front is sucked and injected. Turbine coalescence engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade steam turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91e) ( 91b) is used to inject high-temperature water and combustion gas from each of one or more special devices (92a) and (92b), and sucks and injects air in front of the entire moving blade steam gas turbine. Combined organization. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに於いて、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In a full blade gas turbine driven by high temperature water (5b) with multiple temperatures such as supercritical temperature, etc., high temperature water is injected from one or more special devices (92a) using the spraying principle (91e) And an all-blade steam gas turbine combined engine comprising a device for sucking forward air and propelling and propelling the air and driving with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに於いて、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures, etc., high-temperature water is supplied from one or more special devices (92a) using the spraying principle (91e). An all-rotor-blade steam gas turbine combined engine comprising a device that injects, sucks forward air, propels and propels the fuel, and drives with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91b) A moving blade steam gas characterized by comprising a device that injects combustion gas from one or more special devices (92b) using air and sucks forward air to propel the fuel and drives it with the output. Turbine coalescence engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91b) A full blade steam gas turbine characterized in that it comprises a device for injecting combustion gas from one or more special devices (92b) and sucking forward air to inject and propel it to drive at the output. Combined organization. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに於いて、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical temperature, high-temperature water is supplied from one or more water injection devices (93a) using a spraying principle (91c). An all-rotor-blade steam gas turbine combined engine comprising a device that injects, sucks forward water, propels and propels the fuel, and drives with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに於いて、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, etc., the hot water is more than one or more water injection devices (93a) using the spraying principle (91c). A full-blade steam gas turbine combined engine comprising a device that injects water, sucks forward water and propulses the fuel, and drives with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91d) A moving blade steam characterized in that it comprises a device that injects combustion gas from one or more water injection devices (93b) by utilizing the above, sucks forward water and injects and propels it, and drives with the output. Gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of a full blade steam turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91d) A full bucket blade gas characterized in that it comprises a device that injects combustion gas from one or more water injection devices (93b), and sucks forward water to inject and propel it, and is driven by the output. Turbine coalescence engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91c) (91d) is used to inject high-temperature water and combustion gas from each of the one or more water injection devices (93a) and (93b), suck forward water, inject and propel the device, and drive with the output. An all-blade steam gas turbine combined engine characterized by comprising. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade steam turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91c) ( 91d) is used to inject high-temperature water and combustion gas from each of the one or more water injection devices (93a) and (93b), suck the water in front, inject and propel it, and drive with this output An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91e) (91b) is used to inject high-temperature water and combustion gas from each of one or more special devices (92a) and (92b), suck air in front and propell it, and drive at that output. An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical pressure comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade steam turbine driven by high temperature water (5b) such as supercritical temperature such as supercritical temperature, and the principle of spraying (91e) ( 91b) is used to inject high-temperature water and combustion gas from each of one or more special devices (92a) and (92b), suck the air in front and inject and propel it, and drive with this output. An all-blade steam gas turbine combined engine characterized by that. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する超臨界圧力等の高温水（５ｂ）等で駆動する全動翼ガスタービンの内側軸装置を中空として、霧吹きの原理（９１）を利用して前方の空気を吸引噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). The inner shaft device of the all-blade gas turbine driven by high-temperature water (5b) or the like driven by high-temperature water (5b) having a plurality of temperatures, etc., is made hollow, and the front side using the spraying principle (91) All-blade steam gas turbine combined engine characterized by sucking and injecting air. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの内側軸装置を中空として、霧吹きの原理（９１）を利用して前方の空気を吸引噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Full-motion, characterized in that the inner shaft device of a full-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures is made hollow, and forward air is sucked and injected using the principle of spraying (91) Wing steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの内側軸装置を中空として、霧吹きの原理（９１）を利用して前方の空気を吸引噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A full moving blade characterized in that the inner shaft device of a full moving blade steam turbine driven by high temperature water (5b) having a plurality of temperatures is hollow, and the air in front is sucked and injected using the principle of spraying (91) Steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A full-blade steam gas turbine combined engine, characterized in that a combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures. . 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combining all rotor blade steam gas turbines, characterized in that a combustion gas outlet (88) is provided at the exit of the combustor / heat exchanger of all rotor blade steam gas turbines driven by high temperature water (5b) of a plurality of temperatures, etc. organ. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A full-blade steam gas turbine combined engine, characterized in that a combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures. . 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、マイクロガスタービンを駆動することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A micro gas turbine is driven by providing a combustion gas outlet (88) at the combustor / heat exchanger outlet of an all rotor blade gas turbine driven by high temperature water (5b) having a plurality of temperatures. Rotor steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、マイクロガスタービンを駆動することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of an all-blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures, and the micro gas turbine is driven. All-blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに於いて、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, spraying high-temperature water from one or more special devices (92a) using the spraying principle (91e) An all-blade steam gas turbine combined engine characterized by sucking and injecting. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに於いて、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all blade steam gas turbine driven by high temperature water (5b) of a plurality of equal temperatures, the hot water is jetted from one or more special devices (92a) using the spraying principle (91e) An all-blade steam gas turbine combined engine characterized by sucking and injecting air. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full-blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, and the atomizing principle (91b) is used for 1 An all-blade steam gas turbine combined engine characterized by injecting combustion gas from a plurality of special devices (92b) and sucking and injecting forward air. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures, and one or more using the spraying principle (91b) An all-blade steam gas turbine combined engine characterized by injecting combustion gas from a plurality of special devices (92b) and sucking and injecting forward air. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに於いて、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high temperature water (5b) having a plurality of temperatures, the high temperature water is injected from one or more water injection devices (93a) using the spraying principle (91c) An all-blade steam gas turbine combined engine characterized by sucking and injecting water. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに於いて、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures, the high temperature water is injected from one or more water injection devices (93a) using the spraying principle (91c) All-swing-blade steam gas turbine combined engine characterized by sucking and injecting water. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, and the atomizing principle (91d) is used. An all-blade steam gas turbine combined engine characterized by injecting combustion gas from a plurality of water injection devices (93b) and sucking and injecting water in front. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures, and one or more using the spraying principle (91d) An all-blade steam gas turbine combined engine characterized by injecting combustion gas from a plurality of water injection devices (93b) and sucking and injecting water in front. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all rotor blade gas gas turbines driven by high temperature water (5b), etc., using the spraying principle (91c) (91d) Then, the full moving blade steam gas turbine combined engine is characterized in that high temperature water and combustion gas are injected from each of the one or more water injection devices (93a) and (93b), and the water in front is sucked and injected. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade steam turbines driven by high temperature water (5b) of a plurality of temperatures, and the principle of spraying (91c) (91d) is used. A full moving blade steam gas turbine combined engine characterized in that high temperature water and combustion gas are injected from each of the one or more water injection devices (93a) and (93b) and the water in front is sucked and injected. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade vane steam gas turbine driven by high temperature water (5b), etc., and the spraying principle (91e) (91b) is used. Then, an all-blade steam gas turbine combined engine characterized by injecting high-temperature water and combustion gas from each of one or more special devices (92a) and (92b) and sucking and injecting air in front. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of all blade steam turbine driven by high temperature water (5b), etc., and the spraying principle (91e) (91b) is used. An all-blade steam gas turbine combined engine characterized by injecting high-temperature water and combustion gas from one or more special devices (92a) and (92b) and sucking and injecting forward air. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに於いて、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, spraying high-temperature water from one or more special devices (92a) using the spraying principle (91e) An all-blade steam gas turbine combined engine comprising a device that sucks and propels the fuel and drives it with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに於いて、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all blade steam gas turbine driven by high temperature water (5b) of a plurality of equal temperatures, the hot water is jetted from one or more special devices (92a) using the spraying principle (91e) An all-rotor-blade steam gas turbine combined engine characterized by comprising a device that sucks air and propulses and drives it with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full-blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, and the atomizing principle (91b) is used for 1 An all-blade steam gas turbine combined engine characterized by comprising a device that injects combustion gas from a plurality of special devices (92b), sucks forward air and propels it for injection, and drives with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures, and one or more using the spraying principle (91b) An all-blade steam gas turbine combined engine comprising a device that injects combustion gas from a plurality of special devices (92b), sucks forward air, and propels and injects it, and is driven by the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに於いて、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high temperature water (5b) having a plurality of temperatures, the high temperature water is injected from one or more water injection devices (93a) using the spraying principle (91c) An all-rotor-blade steam gas turbine combined engine comprising a device that sucks water and propels it for injection and is driven by the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに於いて、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). In an all-blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures, the high temperature water is injected from one or more water injection devices (93a) using the spraying principle (91c) An all-blade steam gas turbine combined engine comprising a device that sucks water and propels it for injection and drives it with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full blade steam gas turbine driven by high temperature water (5b) having a plurality of equal temperatures, and the atomizing principle (91d) is used. An all-blade steam gas turbine combined engine characterized by comprising a device that injects combustion gas from a plurality of water injection devices (93b), sucks forward water and propels it for injection, and drives with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of the full-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures, and one or more using the spraying principle (91d) An all-rotor-steam gas turbine combined engine comprising a device that injects combustion gas from a plurality of water injection devices (93b), sucks forward water and propels the injection, and drives with the output. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all rotor blade gas gas turbines driven by high temperature water (5b), etc., using the spraying principle (91c) (91d) And a device that injects high-temperature water and combustion gas from each of the one or more water injection devices (93a) and (93b), sucks forward water, injects and propels it, and drives with the output. An all-blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade steam turbines driven by high temperature water (5b) of a plurality of temperatures, and the principle of spraying (91c) (91d) is used. And a plurality of water injection devices (93a) and (93b) for injecting high-temperature water and combustion gas, sucking forward water and propelling and propelling it, and driving with the output. An all-blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the outlet of the combustor and heat exchanger of all blade vane steam gas turbine driven by high temperature water (5b), etc., and the spraying principle (91e) (91b) is used. And a device that injects high-temperature water and combustion gas from each of the one or more special devices (92a) and (92b), sucks forward air, and propels and jets the air, and drives with the output. An all-blade steam gas turbine combined engine. 送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により互いに反対方向に回転する外側軸装置と内側軸装置を最適回転比で結合し、電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A supercritical temperature comprising an electromagnetically heated turbine rotor blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a water pump and counter-rotating magnetic friction power transmission device (14a). Combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of all blade steam turbine driven by high temperature water (5b), etc., and the spraying principle (91e) (91b) is used. And a device for injecting high-temperature water and combustion gas from each of the one or more special devices (92a) and (92b), sucking forward air and injecting and propelling it, and driving with the output. All-blade steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of an all blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), an annular integral casting (84 A water repellent water cooling blade (87) is provided in an annular manner in each paragraph in most of the outer compressor blade group (16) and the inner compressor blade group (17) which are assembled as an assembly structure. An all-blade steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), it is integrally cast in a ring ( 84) A water-repellent water cooling blade (87) is provided in each of the paragraphs in the most part of each of the outer compressor blade group (16) and the inner compressor blade group (17) having an assembly structure. An all-blade steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade compressor of an all-blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), and is integrally cast (84) in an annular form. All of the outer compressor blade groups (16) and inner compressor rotor blade groups (17) are provided with water-repellent water cooling blades (87) in an annular form for each stage. Gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), it is integrally cast (84) and assembled in an annular shape. All the moving blades characterized in that a water-repellent water cooling blade (87) is provided in an annular form in each paragraph in most of the outer compressor blade group (16) and the inner compressor blade group (17). Steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of an all blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), an annular integral casting (84 ) Water repellent water cooling blades (87) are provided in a ring shape in each of the most part of the outer compressor blade group (16) and the inner compressor blade group (17) in the assembled structure. An all-rotor-blade steam gas turbine combined engine, wherein the plurality of water-repellent water cooling blades are cooled and then water-injected from the water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), it is integrally cast in a ring ( 84) Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) having the assembled structure are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph. An all-blade steam gas turbine combined engine characterized in that after one or more water-repellent water cooling blades are cooled, water is injected from water injection means (56). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade compressor of an all-blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), and is integrally cast (84) in an annular form. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and one or more water repellency per paragraph is provided. An all-rotor-blade steam gas turbine combined engine, wherein the water-cooling blade is cooled and then water-injected by water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), it is integrally cast (84) and assembled in an annular shape. Most of the outer compressor blade group (16) and the inner compressor blade group (17) having the structure are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and one or more repellents are provided for each paragraph. An all-rotor-blade steam gas turbine combined engine, wherein water-cooling blades are cooled and then water-injected from water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of an all blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), an annular integral casting (84 ) Water repellent water cooling blades (87) are provided in a ring-like manner in most of the outer compressor blade group (16) and the inner compressor blade group (17) in the assembled structure. An all-rotor-blade steam gas turbine combined engine characterized in that the water-repellent water cooling blades of the following half are cooled and then water-injected from the water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), it is integrally cast in a ring ( 84) Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) having the assembled structure are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph. An all-rotor-blade steam gas turbine combined engine characterized in that the water-repellent water-cooling blades of half or less of all the water-repellent water-cooling blades are cooled and then water-injected from the water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade compressor of an all-blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), and is integrally cast (84) in an annular form. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, so that the water repellency is less than half of all the paragraphs. An all-rotor-blade steam gas turbine combined engine, wherein the water-cooling blade is cooled and then water-injected by water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), it is integrally cast (84) and assembled in an annular shape. Most of the outer compressor blade group (16) and the inner compressor blade group (17) having the structure are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and the entire half of each paragraph is less than half An all-rotor-blade steam gas turbine combined engine, wherein water-cooling blades are cooled and then water-injected from water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature such as a supercritical pressure, provided with an electromagnetically heated turbine rotor blade (81), an annular integral casting (84) is used as an assembly structure. Most of the outer compressor blade groups (16) and inner compressor blade groups (17) communicating with the water channel are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph. An all-rotor-blade steam gas turbine combined engine, wherein the water-repellent water cooling blades are cooled and then water-injected by water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine equipped with an electromagnetically heated turbine rotor blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, is integrally cast (84) in an annular shape and assembled. In most of the outer compressor blade group (16) and the inner compressor blade group (17) communicating with the water channel, a water-repellent water cooling blade (87) is provided in a ring shape for each paragraph, and the entire half of each paragraph is less than half. An all-rotor-blade steam gas turbine combined engine, wherein the water-repellent water-cooling blades are cooled and then water-injected by water-injecting means (56). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine equipped with an electromagnetically heated turbine rotor blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, the water passage is communicated as an assembly structure by integrally casting (84) in an annular shape. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and half the water-repellent water cooling blades for all the paragraphs or less. An all-rotor-blade steam gas turbine combined engine, wherein water is injected from the water injection means (56) after cooling. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the water channel is communicated as an assembly structure by integrally casting (84) in an annular shape. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and the water-repellent water cooling is less than half for each paragraph. An all-blade steam gas turbine combined engine characterized in that water is injected from water injection means (56) after cooling the blades. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of an all blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), an annular integral casting (84 ) A water-repellent water cooling blade (87) is provided in a ring-like manner in most of the outer compressor blade group (16) and the inner compressor blade group (17), which are assembled into an assembly structure, and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising an apparatus for performing the above operation. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), it is integrally cast in a ring ( 84) Most of the outer compressor blade group (16) and the inner compressor blade group (17) having the assembled structure are provided with water-repellent water cooling blades (87) in a ring shape for each stage. An all-blade steam gas turbine combined engine comprising a driving device. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade compressor of an all-blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), and is integrally cast (84) in an annular form. Most of the outer compressor blade group (16) and the inner compressor blade group (17) were equipped with water repellent water cooling blades (87) in an annular form for each stage and driven by the output. An all-blade steam gas turbine combined engine characterized by that. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), it is integrally cast (84) and assembled in an annular shape. Most of the outer compressor blade group (16) and the inner compressor blade group (17) having a structure are provided with a water-repellent water cooling blade (87) in an annular form for each paragraph and driven by the output. An all-blade steam gas turbine combined engine characterized by that. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of an all blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), an annular integral casting (84 ) Water repellent water cooling blades (87) are provided in a ring shape in each of the most part of the outer compressor blade group (16) and the inner compressor blade group (17) in the assembled structure. An all-rotor-blade steam gas turbine combined engine comprising a device for driving the water-repellent water-cooled blades after cooling the water-repellent water-cooling blades from the water-injecting means (56) and driving with the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射し該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade compressor of a full blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81), it is integrally cast in a ring ( 84) Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) having the assembled structure are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph. An all-blade steam gas turbine combined engine comprising a device that cools one or more water-repellent water-cooling blades after being cooled and then sprays water from the water-injecting means (56) and drives the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade compressor of an all-blade gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), and is integrally cast (84) in an annular form. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and one or more water repellency per paragraph is provided. An all-blade steam gas turbine combined engine characterized by comprising a device that cools the water cooling blades and then injects water from the water injection means (56) and drives it with the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの全動翼圧縮機において、環状に一体鋳造（８４）して組立構造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射し該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5b) having multiple temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), it is integrally cast (84) and assembled in an annular shape. Most of the outer compressor blade group (16) and the inner compressor blade group (17) having the structure are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and one or more repellents are provided for each paragraph. An all-bladed-steam gas turbine combined engine comprising a device for injecting water from a water injection means (56) after driving the aqueous water cooling blade and driving with the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機翼群及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature such as a supercritical pressure, provided with an electromagnetically heated turbine rotor blade (81), an annular integral casting (84) is used as an assembly structure. Most of the outer compressor blade group and inner compressor blade group (17) communicating with the water channel are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and half or less of the water-repellent water for each paragraph. An all-blade steam gas turbine combined engine characterized by comprising a device that cools the cooling blades and then injects water from the water injection means (56) and drives it with the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機翼群及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine equipped with an electromagnetically heated turbine rotor blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, is integrally cast (84) in an annular shape and assembled. In most of the outer compressor blade group and the inner compressor rotor blade group (17) communicating with the water channel, a water-repellent water cooling blade (87) is provided in a ring shape for each paragraph, and the water repellency is less than half in all the paragraphs. An all-blade steam gas turbine combined engine characterized by comprising a device that cools the water cooling blades and then injects water from the water injection means (56) and drives it with the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機翼群及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine equipped with an electromagnetically heated turbine rotor blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, the water passage is communicated as an assembly structure by integrally casting (84) in an annular shape. In most of the outer compressor blade group and the inner compressor blade group (17), the water-repellent water cooling blades (87) are provided in a ring shape for each paragraph, and after cooling the water-repellent water cooling blades of less than half in each paragraph An all-blade steam gas turbine combined engine comprising a device for injecting water from a water injection means (56) and driving with the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造として水路を連通した夫々の外側圧縮機翼群及び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼（８７）を段落毎環状に設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射して該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the water channel is communicated as an assembly structure by integrally casting (84) in an annular shape. Most of the outer compressor blade group and the inner compressor blade group (17) are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph, and the water-repellent water-cooling blades for the entire half or less are cooled in each paragraph. An all-rotor-blade steam gas turbine combined engine comprising a device that later injects water from the water injection means (56) and drives with the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine equipped with an electromagnetically heated turbine rotor blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, is integrally cast (84) in an annular shape and assembled. An all-rotor-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the inner turbine rotor blade group (20). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine equipped with an electromagnetically heated turbine rotor blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, is integrally cast (84) in an annular shape and assembled. An all-rotor-blade steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection of the outer turbine rotor blade group (19). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine equipped with an electromagnetically heated turbine rotor blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, an annular integral casting (84) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all rotor blade gas turbine equipped with an electromagnetically heated turbine rotor blade (81) and driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure, an annular integral casting (84) An all-blade steam gas turbine combined engine characterized in that a water injection means (56a) is provided in the vicinity of the assembly annular connection portion of the outer turbine rotor blade group (19). 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) is integrally cast (84) in an annular shape and assembled. An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  Inner turbine motion in an all-blade steam gas turbine equipped with an electromagnetically heated turbine rotor blade (81) driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures and integrally assembled (84) in an annular shape An all-rotor-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection of the blade group (20). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine that is driven by high-temperature water (5b) having a plurality of temperatures, such as supercritical temperatures, equipped with an electromagnetically heated turbine rotor blade (81), an outer turbine motion that is integrally cast in a ring (84) to form an assembly structure An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection of the blade group (19). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  Inner turbine blade having an assembly structure formed by annular casting integrally (84) in an all blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, provided with an electromagnetically heated turbine blade (81) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection of group (20). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンにおいて、環状に一体鋳造（８４）して組立構造とした外側タービン動翼群（１９）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  Outer turbine rotor blade having an assembly structure formed by annular casting integrally (84) in an all rotor blade gas turbine having electromagnetic heating turbine rotor blade (81) driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection of group (19). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンにおいて、環状に一体鋳造（８４）して組立構造とした内側タービン動翼群（２０）の組立環状接続部付近に、水噴射手段（５６ａ）を断熱して設けたことを特徴とする全動翼蒸気ガスタービン合体機関。  Inner turbine blade having an assembly structure formed by annular casting integrally (84) in an all blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature, equipped with an electromagnetically heated turbine blade (81) An all-blade steam gas turbine combined engine characterized in that water injection means (56a) is provided in the vicinity of the assembly annular connection of group (20). 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), the principle of spraying (91e) An all-blade steam gas turbine combined engine characterized in that high-temperature water is injected from one or more special devices (92a) by using and sucking and injecting air in front. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with an electromagnetically heated turbine rotor blade (81), the principle of spraying (91c) An all-blade steam gas turbine combined engine characterized in that high-temperature water is injected from one or more water injection devices (93a) by using and sucking and injecting forward water. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the principle of spraying (91e) An all-blade steam gas turbine combined engine characterized in that high-temperature water is injected from one or more special devices (92a) by using the air and sucks and injects the air in front. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the principle of spraying (91c) An all-blade steam gas turbine combined engine characterized in that high-temperature water is injected from one or more water injection devices (93a) using the above, and the water in front is sucked and injected. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full-rotor-steam steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), a combustion gas is provided at the combustion gas outlet. An outlet (88) is provided, spraying hot water and combustion gas from each of the one or more special devices (92a) (92b) using the spraying principle (91e) (91b) An all-blade steam gas turbine combined engine characterized by suction and injection. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full-rotor-steam steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), a combustion gas is provided at the combustion gas outlet. An outlet (88) is provided, and hot water and combustion gas are injected from each of the one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d), and water in front An all-blade steam gas turbine combined engine characterized by sucking and injecting. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas is collected at the combustion gas outlet. An outlet (88) is provided and hot water and combustion gas are injected from each of one or more special devices (92a) and (92b) using the spraying principle (91e) and (91b), and the front air is sucked in. All-blade steam gas turbine combined engine characterized by 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas is collected at the combustion gas outlet. An outlet (88) is provided to inject high temperature water and combustion gas from each of the one or more water injection devices (93a) and (93b) using the spraying principle (91c) and (91d), An all-blade steam gas turbine combined engine characterized by suction and injection. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full-rotor-steam steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), a combustion gas is provided at the combustion gas outlet. An exhaust port (88) is provided and combustion gas is injected from one or more special devices (92b) using the spraying principle (91b), and the air in front is sucked and injected. Rotor steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full-rotor-steam steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), a combustion gas is provided at the combustion gas outlet. A take-out port (88) is provided, and the combustion gas is injected from one or more water injection devices (93b) using the spraying principle (91d), and the water in front is sucked and injected. All-blade steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas is collected at the combustion gas outlet. A full motion characterized by providing an outlet (88), injecting combustion gas from one or more special devices (92b) using the spraying principle (91b), and sucking and injecting air ahead Wing steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas is collected at the combustion gas outlet. An outlet (88) is provided, combustion gas is injected from one or more water injection devices (93b) using the spraying principle (91d), and water in front is sucked and injected. Rotor steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as supercritical temperature equipped with an electromagnetically heated turbine blade (81), the principle of atomization is used. An all-blade steam gas turbine combined engine comprising a device that injects high-temperature water from one or more special devices (92a), sucks forward air, and propels and jets the air, and drives with the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as supercritical temperature equipped with an electromagnetically heated turbine blade (81), the principle of atomization is used. An all-blade steam gas turbine combined engine comprising a device that injects high-temperature water from one or more water injection devices (93a), sucks forward water and propels the injection, and drives with the output. . 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all-blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the principle of spraying (91e) The whole blade steam gas comprising a device that injects high-temperature water from one or more special devices (92a) using air, sucks forward air, and propels and jets the air, and drives with the output. Turbine coalescence engine. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the principle of spraying (91c) A whole blade steam characterized by comprising a device for injecting and propelling high temperature water from one or more water injection devices (93a) by utilizing the above, sucking forward water and propelling and driving the output. Gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full-rotor-steam steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), a combustion gas is provided at the combustion gas outlet. An outlet (88) is provided, spraying hot water and combustion gas from each of the one or more special devices (92a) (92b) using the spraying principle (91e) (91b) An all-rotor-blade steam gas turbine combined engine comprising a device that sucks and propulses and drives with the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full-rotor-steam steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), a combustion gas is provided at the combustion gas outlet. An outlet (88) is provided, and hot water and combustion gas are injected from each of the one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d), and water in front An all-blade steam gas turbine combined engine comprising a device that sucks and propels the fuel and drives it with the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas is collected at the combustion gas outlet. An outlet (88) is provided and hot water and combustion gas are injected from each of one or more special devices (92a) and (92b) using the spraying principle (91e) and (91b), and the front air is sucked in. And an all-blade steam gas turbine combined engine characterized by comprising a device for propelling and driving with the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas is collected at the combustion gas outlet. An outlet (88) is provided to inject high temperature water and combustion gas from each of the one or more water injection devices (93a) and (93b) using the spraying principle (91c) and (91d), An all-rotor-blade steam gas turbine combined engine comprising a device that sucks and propulses and drives with the output. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full-rotor-steam steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), a combustion gas is provided at the combustion gas outlet. A take-out port (88) is provided, and combustion gas is injected from one or more special devices (92b) using the spraying principle (91b), and the front air is sucked in and propelled, and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising a device for 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full-rotor-steam steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), a combustion gas is provided at the combustion gas outlet. An outlet (88) is provided to inject combustion gas from one or more water injection devices (93b) using the principle of spraying (91d), suck water forward, and propel the injection. An all-blade steam gas turbine combined engine comprising a driving device. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas is collected at the combustion gas outlet. An outlet (88) is provided, and the combustion gas is injected from one or more special devices (92b) using the spraying principle (91b), the air in front is sucked and propelled, and driven by the output. An all-blade steam gas turbine combined engine comprising the apparatus. 電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as supercritical temperatures equipped with an electromagnetically heated turbine rotor blade (81), the combustion gas is collected at the combustion gas outlet. An outlet (88) is provided, and the combustion gas is injected from one or more water injection devices (93b) using the spraying principle (91d), the water in front is sucked and propelled, and driven by the output. An all-blade steam gas turbine combined engine characterized by comprising an apparatus for performing the above operation. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In a combustor and heat exchanger (4) of an all blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetic heating turbine blade (81), An all-rotor-blade steam gas turbine combined engine characterized by injecting hot water from one or more special devices (92a) using the principle (91e) and sucking and injecting air in front. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In a combustor and heat exchanger (4) of an all blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetic heating turbine blade (81), An all-rotor-blade steam gas turbine combined engine characterized in that high temperature water is injected from one or more water injection devices (93a) using the principle (91c), and the water in front is sucked and injected. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水を噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) An all-blade steam gas turbine combined engine characterized in that high-temperature water is injected from one or more special devices (92a) using the principle (91e) of the above, and the air in front is sucked and injected. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) An all-blade steam gas turbine combined engine characterized in that high-temperature water is injected from one or more water injection devices (93a) using the principle (91c), and the water in front is sucked and injected. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion in a combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) Combustion gas outlet (88) is provided at the gas outlet, and hot water and combustion gas are injected from each of one or more special devices (92a) and (92b) using the principle of spraying (91e) and (91b). An all-blade steam gas turbine combined engine characterized by sucking and injecting forward air. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion in a combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) Combustion gas outlet (88) is provided at the gas outlet, and high temperature water and combustion gas are injected from each of one or more water injection devices (93a) and (93b) using the spraying principle (91c) and (91d). And an all-blade steam gas turbine combined engine characterized by sucking and injecting water in front. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas in a combustor and heat exchanger (4) of an all blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) Combustion gas outlet (88) is provided at the outlet, and hot water and combustion gas are injected from each of one or more special devices (92a) (92b) using the principle of spraying (91e) (91b), An all-blade steam gas turbine combined engine characterized by sucking and injecting forward air. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas in a combustor and heat exchanger (4) of an all blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) A combustion gas outlet (88) is provided at the outlet, and hot water and combustion gas are injected from each of the one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d). An all-blade steam gas turbine combined engine characterized by sucking and injecting water ahead. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion in a combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) A combustion gas outlet (88) is provided at the gas outlet, and the combustion gas is injected from one or more special devices (92b) using the spraying principle (91b), and the front air is sucked and injected. An all-blade steam gas turbine combined engine characterized by 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion in a combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) A combustion gas outlet (88) is provided at the gas outlet, the combustion gas is injected from one or more water injection devices (93b) using the spraying principle (91d), and the water in front is sucked and injected. An all-blade steam gas turbine combined engine characterized by that. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas in a combustor and heat exchanger (4) of an all blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) Combustion gas outlet (88) is provided at the outlet, and the combustion gas is injected from one or more special devices (92b) using the spraying principle (91b), and the air in front is sucked and injected. An all-blade steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射することを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas in a combustor and heat exchanger (4) of an all blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) A combustion gas outlet (88) is provided at the outlet, and the combustion gas is injected from one or more water injection devices (93b) using the spraying principle (91d), and the water in front is sucked and injected. An all-blade steam gas turbine combined engine characterized by 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理を利用して１以上複数の特殊装置（９２ａ）より高温水（５ｂ）を噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In a combustor and heat exchanger (4) of an all blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetic heating turbine blade (81), It is characterized in that it comprises a device that injects hot water (5b) from one or more special devices (92a) by utilizing the principle, sucks forward air and propels it, and drives with the output. Rotor steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理を利用して１以上複数の水噴射装置（９３ａ）より高温水（５ｂ）を噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In a combustor and heat exchanger (4) of an all blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetic heating turbine blade (81), Utilizing the principle, the apparatus comprises a device that injects high temperature water (5b) from one or more water injection devices (93a), sucks forward water, and propels the injection, and drives with the output. All-blade steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｅ）を利用して１以上複数の特殊装置（９２ａ）より高温水（５ｂ）を噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) Using the principle (91e) of the above, a device for injecting high-temperature water (5b) from one or more special devices (92a), sucking forward air and propelling it, and driving with the output is provided. An all-blade steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、霧吹きの原理（９１ｃ）を利用して１以上複数の水噴射装置（９３ａ）より高温水を噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  In the combustor and heat exchanger (4) of an all blade steam gas turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) Using the principle (91c) of the present invention, the apparatus includes a device that injects high temperature water from one or more water injection devices (93a), sucks forward water and propels the injection, and drives with the output. An all-blade steam gas turbine combined engine. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion in a combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) Combustion gas outlet (88) is provided at the gas outlet, and hot water and combustion gas are injected from each of one or more special devices (92a) and (92b) using the principle of spraying (91e) and (91b). An all-blade steam gas turbine combined engine comprising a device for sucking forward air and propelling and propelling it and driving with the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion in a combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) Combustion gas outlet (88) is provided at the gas outlet, and high temperature water and combustion gas are injected from each of one or more water injection devices (93a) and (93b) using the spraying principle (91c) and (91d). And an all-blade steam gas turbine combined engine comprising a device that sucks water in front and propels it for injection and drives it with the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｅ）（９１ｂ）を利用して夫々の１以上複数の特殊装置（９２ａ）（９２ｂ）より高温水及び燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas in a combustor and heat exchanger (4) of an all blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) Combustion gas outlet (88) is provided at the outlet, and hot water and combustion gas are injected from each of one or more special devices (92a) (92b) using the principle of spraying (91e) (91b), An all-rotor-steam gas turbine combined engine comprising a device that sucks forward air and propels it for injection and is driven by the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｃ）（９１ｄ）を利用して夫々の１以上複数の水噴射装置（９３ａ）（９３ｂ）より高温水及び燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas in a combustor and heat exchanger (4) of an all blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) A combustion gas outlet (88) is provided at the outlet, and hot water and combustion gas are injected from each of the one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d). An all-blade steam gas turbine combined engine characterized by comprising a device that sucks forward water and propels it for injection and drives it with the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion in a combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) A combustion gas outlet (88) is provided at the gas outlet, and the combustion gas is injected from one or more special devices (92b) using the spraying principle (91b), and the front air is sucked and propelled for injection. An all-blade steam gas turbine combined engine comprising a device driven by the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion in a combustor and heat exchanger (4) of an all blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine blade (81) Combustion gas outlet (88) is provided at the gas outlet, and using the spraying principle (91d), combustion gas is injected from one or more water injection devices (93b), and the water in front is sucked and propelled. And an all-blade steam gas turbine combined engine comprising a device driven by the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｂ）を利用して１以上複数の特殊装置（９２ｂ）より燃焼ガスを噴射し、前方の空気を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas in a combustor and heat exchanger (4) of an all blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) Combustion gas outlet (88) is provided at the outlet, the combustion gas is injected from one or more special devices (92b) using the principle of spraying (91b), the air in front is sucked and propelled for injection, An all-blade steam gas turbine combined engine comprising a device driven by the output. 電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンの燃焼器兼熱交換器（４）において、燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの原理（９１ｄ）を利用して１以上複数の水噴射装置（９３ｂ）より燃焼ガスを噴射し、前方の水を吸引して噴射推進し、該出力で駆動する装置を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  Combustion gas in a combustor and heat exchanger (4) of an all blade steam turbine driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with an electromagnetically heated turbine rotor blade (81) A combustion gas outlet (88) is provided at the outlet, and the combustion gas is injected from one or more water injection devices (93b) using the spraying principle (91d), and the water in front is sucked and propelled. An all-blade steam gas turbine combined engine comprising a device driven by the output. 前記電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンに、電磁加熱噴口（８３）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with the electromagnetic heating turbine rotor blade (81) is provided with an electromagnetic heating nozzle (83). Wing steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに、電磁加熱噴口（８３）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-heated blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with the electromagnetically heated turbine rotor blade (81) is provided with an electromagnetically heated nozzle (83). Rotor steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに、電磁加熱噴口（８３）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with the electromagnetic heating turbine rotor blade (81) has an electromagnetic heating nozzle (83). Wing steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンに、加熱高温手段（１０１）により電磁加熱高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water injection nozzle (100) of electromagnetic heating and high temperature is heated by the high temperature heating means (101) to the whole blade steam turbine driven by the high temperature water (5b) having a plurality of temperatures such as supercritical temperature equipped with the electromagnetic heating turbine blade (81). 59b), a full moving blade steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに、加熱高温手段（１０１）により電磁加熱高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  High temperature water injection nozzle with high temperature electromagnetic heating by heating high temperature means (101) to all blade steam gas turbine driven by high temperature water (5b) with multiple temperatures such as supercritical temperature equipped with electromagnetic heating turbine blade (81) (59b) An all-blade steam gas turbine combined engine characterized by comprising: 前記電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに、加熱高温手段（１０１）により電磁加熱高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  A high temperature water injection nozzle (100) with electromagnetic heating by a high temperature heating means (101) is added to an all blade gas turbine driven by high temperature water (5b) having a plurality of temperatures such as supercritical temperature and provided with the electromagnetic heating turbine blade (81). 59b), a full moving blade steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンに、電磁加熱噴口（８３）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-heated blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with the electromagnetic heating turbine blade (81) has an electromagnetic heating nozzle (83). An all-blade steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）を具備した超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに、電磁加熱噴口（８３）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-heated blade steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature equipped with the electromagnetically heated turbine rotor blade (81) is provided with an electromagnetically heated nozzle (83). Rotor steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに、電磁加熱噴口（８３）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The entire blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with the electromagnetic heating turbine blade (81) is provided with an electromagnetic heating nozzle (83). An all-blade steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンに、加熱高温手段（１０１）により電磁加熱高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The electromagnetically heated high temperature means (101) is used to heat the high temperature water (5b) driven by a plurality of high temperature water (5b) such as a supercritical temperature such as a supercritical pressure equipped with the electromagnetically heated turbine rotor blade (81). An all-blade steam gas turbine combined engine comprising a high-temperature water injection nozzle (59b). 前記電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに、加熱高温手段（１０１）により電磁加熱高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The all heated blade steam gas turbine equipped with the electromagnetic heating turbine blade (81) driven by high temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure is heated by an electromagnetic heating high temperature means (101). An all-blade steam gas turbine combined engine comprising a high-temperature water injection nozzle (59b). 前記電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに、加熱高温手段（１０１）により電磁加熱高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature such as a supercritical pressure, provided with the electromagnetically heated turbine rotor blade (81) is heated by an electromagnetically heated high-temperature means (101). An all-blade steam gas turbine combined engine comprising a high-temperature water injection nozzle (59b). 前記電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気タービンに、加熱高温手段（１０１）により電気抵抗で高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The whole blade steam turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure equipped with the electromagnetic heating turbine rotor blade (81) is heated to high temperature by electric resistance by a heating high temperature means (101). An all-blade steam gas turbine combined engine comprising a high-temperature water injection nozzle (59b). 前記電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼蒸気ガスタービンに、加熱高温手段（１０１）により電気抵抗で高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-wheel steam gas turbine driven by high-temperature water (5b) having a plurality of temperatures, such as a supercritical temperature such as a supercritical pressure, provided with the electromagnetically heated turbine rotor blade (81) is heated by a heating high temperature means (101). An all-blade steam gas turbine combined engine comprising a high-temperature high-temperature water injection nozzle (59b). 前記電磁加熱タービン動翼（８１）を具備した超臨界圧力等の超臨界温度等複数温度の高温水（５ｂ）で駆動する全動翼ガスタービンに、加熱高温手段（１０１）により電気抵抗で高温の高温水噴射ノズル（５９ｂ）を具備したことを特徴とする全動翼蒸気ガスタービン合体機関。  The whole blade gas turbine driven by high-temperature water (5b) having a plurality of temperatures such as a supercritical temperature such as a supercritical pressure provided with the electromagnetically heated turbine blade (81) is heated to high temperature by electric resistance by a heating high temperature means (101). An all-blade steam gas turbine combined engine comprising a high-temperature water injection nozzle (59b). 前記加熱高温手段（１０１）は、高温水噴射ノズル（５９ｂ）に外嵌することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-heated blade steam gas turbine combined engine, wherein the heating high temperature means (101) is fitted on a high temperature water injection nozzle (59b). 前記加熱高温手段（１０１）は、高温水噴射ノズル（５９ｂ）に外嵌して加熱高温にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all-heated blade steam gas turbine combined engine, wherein the heating high temperature means (101) is fitted to the high temperature water injection nozzle (59b) to be heated to a high temperature. 前記加熱高温手段（１０１）は、高温水噴射ノズル（５９ｂ）に外嵌して電磁加熱高温にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The heating blade high temperature steam gas turbine combined engine characterized in that the heating high temperature means (101) is externally fitted to a high temperature water injection nozzle (59b) to be heated to electromagnetic heating. 前記加熱高温手段（１０１）は、高温水噴射ノズル（５９ｂ）に外嵌して電気抵抗により加熱高温にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The heating high temperature means (101) is fitted to the high temperature water injection nozzle (59b) and is heated to a high temperature by electric resistance. 前記高温水噴射ノズル（５９ｂ）は、加熱高温にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water jet nozzle (59b) is an all-rotor-blade steam gas turbine combined engine characterized by being heated to a high temperature. 前記高温水噴射ノズル（５９ｂ）は、銃身状ノズルにすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water spray nozzle (59b) is a full-blade steam gas turbine combined engine characterized by a barrel-shaped nozzle. 前記高温水噴射ノズル（５９ｂ）は、銃身状ノズルにして加熱高温にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water jet nozzle (59b) is a full-blade steam gas turbine combined engine characterized in that it is a barrel-shaped nozzle that is heated to a high temperature. 前記高温水噴射ノズル（５９ｂ）は、銃身状末広ノズルにすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water jet nozzle (59b) is a full-blade steam gas turbine combined engine characterized by a barrel-shaped divergent nozzle. 前記高温水噴射ノズル（５９ｂ）は、銃身状末広ノズルにして加熱高温にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water jet nozzle (59b) is a full-blade steam gas turbine combined engine characterized in that a high temperature water spray nozzle (59b) is a barrel-shaped divergent nozzle and is heated to a high temperature. 前記高温水噴射ノズル（５９ｂ）は、銃身状ノズルにして気化爆発力により高温水（５ｂ）を機関銃の弾丸のように加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water jet nozzle (59b) is a barrel-shaped nozzle and accelerates the high-temperature water (5b) like a bullet of a machine gun by vaporizing explosive force. 前記高温水噴射ノズル（５９ｂ）は、銃身状ノズルにして加熱高温にして気化爆発力により高温水（５ｂ）を機関銃の弾丸のように加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water jet nozzle (59b) is a barrel-shaped nozzle that is heated to a high temperature and accelerates the high-temperature water (5b) like a bullet of a machine gun by vaporizing explosive force. organ. 前記高温水噴射ノズル（５９ｂ）は、銃身状末広ノズルにして気化爆発力により高温水（５ｂ）を機関銃の弾丸のように加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water jet nozzle (59b) is a barrel-shaped divergent nozzle that accelerates the high-temperature water (5b) like a bullet of a machine gun by vaporizing explosive force. 前記高温水噴射ノズル（５９ｂ）は、銃身状末広ノズルにして加熱高温にして気化爆発力により高温水（５ｂ）を機関銃の弾丸のように加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water jet nozzle (59b) is a full-blade steam gas turbine characterized in that it is a barrel-shaped divergent nozzle and heated to a high temperature to accelerate the high-temperature water (5b) like a bullet of a machine gun by vaporizing explosive force. Combined organization. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and uses the feed water (3) for the cooling water. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を１００℃前後として冷却水に給水（３）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and uses the feed water (3) for cooling water with a saturation temperature of about 100 ° C. by an air extractor. Gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を８０℃前後として冷却水に給水（３）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and uses the water supply (3) for cooling water with a saturation temperature of about 80 ° C. by an air extractor. Gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を６０℃前後として冷却水に給水（３）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and uses the water supply (3) for cooling water with a saturation temperature of about 60 ° C. by an air extractor. Gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して海水温度等の上昇を廃止することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and uses the water supply (3) for the cooling water to eliminate the rise in the seawater temperature and the like, and the full moving blade steam gas turbine Combined organization. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して地球温暖化を防止することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser and uses a water supply (3) for cooling water to prevent global warming. . 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the water supply (3) for the cooling water, and supplies it to the combustor and heat exchanger (4). An all-blade steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し該凝縮水と共に、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the water supply (3) for the cooling water, and supplies it to the combustor and heat exchanger (4) together with the condensed water. An all-blade steam gas turbine combined engine characterized by: 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し該凝縮水と共に燃焼器兼熱交換器（４）に供給し、燃料燃焼質量を低減することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the water supply (3) for the cooling water, and supplies it to the combustor and heat exchanger (4) together with the condensed water. An all-blade steam gas turbine combined engine characterized by reducing fuel combustion mass. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度１００℃前後の凝縮水と共に、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using the feed water (3) for the cooling water, and condensate with a saturation temperature of about 100 ° C. as well as a combustor and heat exchanger. An all-blade steam gas turbine combined engine, characterized in that it is supplied to (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度８０℃前後の凝縮水と共に、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the feed water (3) for cooling water, and condensate with a saturation temperature of about 80 ° C. and a combustor / heat exchanger. An all-blade steam gas turbine combined engine, characterized in that it is supplied to (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度６０℃前後の凝縮水と共に、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the feed water (3) for the cooling water, and condensate with a saturation temperature of around 60 ° C., along with the combustor and heat exchanger. An all-blade steam gas turbine combined engine, characterized in that it is supplied to (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度１００℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the feed water (3) for the cooling water, and combustor and heat exchanger (with condensate having a saturation temperature of about 100 ° C.) The all-rotor-blade steam gas turbine combined engine, which is supplied to 4) and stored as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度８０℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the feed water (3) for the cooling water, and combustor and heat exchanger (with the condensed water having a saturation temperature of about 80 ° C.) The all-rotor-blade steam gas turbine combined engine, which is supplied to 4) and stored as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度６０℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the feed water (3) for the cooling water, and combustor and heat exchanger (with the condensed water having a saturation temperature of about 60 ° C.) The all-rotor-blade steam gas turbine combined engine, which is supplied to 4) and stored as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度１００℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the feed water (3) for the cooling water, and combustor and heat exchanger (with condensate having a saturation temperature of about 100 ° C.) The all-rotor-blade steam gas turbine combined engine, which is supplied to 4), stored as heat and supplied to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度８０℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the feed water (3) for the cooling water, and combustor and heat exchanger (with the condensed water having a saturation temperature of about 80 ° C.) The all-rotor-blade steam gas turbine combined engine, which is supplied to 4), stored as heat and supplied to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に給水（３）を使用して熱回収し飽和温度６０℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using the feed water (3) for the cooling water, and combustor and heat exchanger (with the condensed water having a saturation temperature of about 60 ° C.) The all-rotor-blade steam gas turbine combined engine, which is supplied to 4), stored as heat and supplied to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser and uses tap water (70) as cooling water. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を１００℃前後として冷却水に水道水（７０）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and tap water (70) is used as cooling water with a saturation temperature of about 100 ° C. by an air extractor. Steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を８０℃前後として冷却水に水道水（７０）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and tap water (70) is used as cooling water with a saturation temperature of about 80 ° C. by an air extractor. Steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を６０℃前後として冷却水に水道水（７０）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and uses tap water (70) as cooling water with a saturation temperature of about 60 ° C. by an air extractor. Steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して海水温度等の上昇を廃止することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser and uses tap water (70) as cooling water to eliminate the rise in seawater temperature or the like, and Turbine coalescence engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して地球温暖化を防止することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and uses tap water (70) as cooling water to prevent global warming. organ. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and supplies it to the combustor and heat exchanger (4). An all-blade steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し該凝縮水と共に、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and is supplied to the combustor and heat exchanger (4) together with the condensed water. An all-blade steam gas turbine combined engine characterized by being supplied. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し該凝縮水と共に燃焼器兼熱交換器（４）に供給し、燃料燃焼質量を低減することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and supplies it to the combustor and heat exchanger (4) together with the condensed water. And a moving blade steam gas turbine combined engine characterized by reducing the fuel combustion mass. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度１００℃前後の凝縮水と共に、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and condensate and heat exchange with condensate having a saturation temperature of around 100 ° C. An all-blade steam gas turbine combined engine, which is supplied to a vessel (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度８０℃前後の凝縮水と共に、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and condensate and heat exchange with condensed water having a saturation temperature of around 80 ° C. An all-blade steam gas turbine combined engine, which is supplied to a vessel (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度６０℃前後の凝縮水と共に、燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and condensate and heat exchange with condensed water having a saturation temperature of around 60 ° C. An all-blade steam gas turbine combined engine, which is supplied to a vessel (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度１００℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and combustor and heat exchanger together with condensed water having a saturation temperature of around 100 ° C. An all-blade steam gas turbine combined engine, which is supplied to (4) and stored as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度８０℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as the cooling water, and combustor and heat exchanger together with condensed water having a saturation temperature of around 80 ° C. An all-blade steam gas turbine combined engine, which is supplied to (4) and stored as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度６０℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, recovers heat by using tap water (70) as cooling water, and combustor and heat exchanger together with condensed water having a saturation temperature of around 60 ° C. An all-blade steam gas turbine combined engine, which is supplied to (4) and stored as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度１００℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and combustor and heat exchanger together with condensed water having a saturation temperature of around 100 ° C. An all-blade steam gas turbine combined engine that is supplied to (4), stored as hot heat, and supplied to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度８０℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as the cooling water, and combustor and heat exchanger together with condensed water having a saturation temperature of around 80 ° C. An all-blade steam gas turbine combined engine that is supplied to (4), stored as hot heat, and supplied to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し飽和温度６０℃前後の凝縮水と共に燃焼器兼熱交換器（４）に供給し、温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, recovers heat by using tap water (70) as cooling water, and combustor and heat exchanger together with condensed water having a saturation temperature of around 60 ° C. An all-blade steam gas turbine combined engine that is supplied to (4), stored as hot heat, and supplied to consumers. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that tap water is used as cooling water for the vaporization latent heat recovery unit (66a). 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して貯蔵し温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized by storing tap water as cooling water of the vaporization latent heat recovery unit (66a) and supplying hot heat to consumers. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して貯蔵し１００℃に近い温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized by supplying tap water to the cooling water of the vaporization latent heat recovery unit (66a) using tap water and supplying the customer with heat close to 100 ° C. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して貯蔵し１００℃以下の温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized by supplying tap water to the cooling water of the vaporization latent heat recovery unit (66a) using tap water and supplying a heat of 100 ° C. or less to consumers. 前記気化潜熱回収器（６６ａ）の凝縮水全部を燃焼器兼熱交換器（４）に供給して超臨界圧力高温水（５ｂ）にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all blade steam gas turbine combined engine characterized by supplying all the condensed water of the vaporization latent heat recovery unit (66a) to a combustor and heat exchanger (4) to form supercritical pressure high temperature water (5b). 前記気化潜熱回収器（６６ａ）の凝縮水全部を燃焼器兼熱交換器（４）に供給して高温水（５ｂ）にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that all the condensed water of the vaporization latent heat recovery unit (66a) is supplied to a combustor and heat exchanger (4) to form high-temperature water (5b). 前記気化潜熱回収器（６６ａ）の凝縮水全部を燃焼器兼熱交換器（４）に供給して燃料供給熱量を気化潜熱に近付けて低減し、超臨界圧力高温水（５ｂ）にすることを特徴とする全動翼蒸気ガスタービン合体機関。  Supplying all the condensed water of the vaporization latent heat recovery unit (66a) to the combustor and heat exchanger (4) to reduce the amount of heat supplied to the fuel close to the vaporization latent heat to form supercritical pressure high temperature water (5b). An all-blade steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）の凝縮水全部を燃焼器兼熱交換器（４）に供給して燃料供給熱量を気化潜熱に近付けて低減し、高温水（５ｂ）にすることを特徴とする全動翼蒸気ガスタービン合体機関。  All of the condensed water of the vaporization latent heat recovery unit (66a) is supplied to the combustor and heat exchanger (4) to reduce the amount of heat supplied to the fuel near the vaporization latent heat to form high-temperature water (5b). All-blade steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and uses tap water as cooling water. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を１００℃前後として冷却水に水道水を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and tap water is used as cooling water with a saturation temperature of about 100 ° C. by an air extractor. Combined organization. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を８０℃前後として冷却水に水道水を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and tap water is used as cooling water with a saturation temperature of about 80 ° C. by an air extractor. Combined organization. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を６０℃前後として冷却水に水道水を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and tap water is used as cooling water with a saturation temperature of about 60 ° C. by an air extractor. Combined organization. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して海水温度等の上昇を廃止することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and uses tap water as cooling water to eliminate the rise in seawater temperature and the like, and is a full-rotor steam gas turbine combined engine . 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して地球温暖化を防止することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and uses tap water as cooling water to prevent global warming. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収し、凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water as cooling water, and supplies condensed water to the combustor and heat exchanger (4). An all-blade steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収需要家に供給して、凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser and uses tap water as cooling water to supply heat recovery consumers, and condensate water is used as a combustor and heat exchanger (4). An all-blade steam gas turbine combined engine characterized by being supplied to 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収需要家に供給して、凝縮水を燃焼器兼熱交換器（４）に供給し、燃料燃焼質量を低減することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser and uses tap water as cooling water to supply heat recovery consumers, and condensate water is used as a combustor and heat exchanger (4). The all-blade steam gas turbine combined engine characterized in that the fuel combustion mass is reduced. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収需要家に供給して、飽和温度１００℃前後の凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser and uses tap water as cooling water to supply heat recovery consumers, and condensate having a saturation temperature of about 100 ° C. is also used as a combustor. An all-blade steam gas turbine combined engine, which is supplied to a heat exchanger (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収需要家に供給して、飽和温度８０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser and uses tap water as cooling water to supply heat recovery consumers, and condensate having a saturation temperature of about 80 ° C. is also used as a combustor. An all-blade steam gas turbine combined engine, which is supplied to a heat exchanger (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収需要家に供給して、飽和温度６０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser and supplies tap heat as cooling water to heat recovery consumers, and condensate having a saturation temperature of about 60 ° C. is also used as a combustor. An all-blade steam gas turbine combined engine, which is supplied to a heat exchanger (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収需要家に供給して、飽和温度１００℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser and uses tap water as cooling water to supply heat recovery consumers, and condensate having a saturation temperature of about 100 ° C. is also used as a combustor. An all-blade steam gas turbine combined engine, which is supplied to a heat exchanger (4) and stores tap water as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収需要家に供給して、飽和温度８０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser and uses tap water as cooling water to supply heat recovery consumers, and condensate having a saturation temperature of about 80 ° C. is also used as a combustor. An all-blade steam gas turbine combined engine, which is supplied to a heat exchanger (4) and stores tap water as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収し飽和温度６０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using tap water as cooling water, and condensates with a saturation temperature of about 60 ° C. as a combustor and heat exchanger (4). All-blade steam gas turbine combined engine, characterized in that it supplies water and stores tap water as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収し飽和温度１００℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water as cooling water, and condensates with a saturation temperature of about 100 ° C. as a combustor and heat exchanger (4). This is an all-bladed steam gas turbine combined engine that supplies water to customers and stores it as hot heat and supplies it to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収し飽和温度８０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water as cooling water, and condensates with a saturation temperature of about 80 ° C. as a combustor and heat exchanger (4). This is an all-bladed steam gas turbine combined engine that supplies water to customers and stores it as hot heat and supplies it to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水を使用して熱回収し飽和温度６０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using tap water as cooling water, and condensates with a saturation temperature of about 60 ° C. as a combustor and heat exchanger (4). This is an all-bladed steam gas turbine combined engine that supplies water to customers and stores it as hot heat and supplies it to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as a condenser, and uses tap water (70) as cooling water to supply heat to a consumer. Combined organization. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を１００℃前後として冷却水に水道水（７０）を使用して温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and supplies hot water to the customer by using tap water (70) as cooling water with a saturation temperature of about 100 ° C. by an air extractor. An all-blade steam gas turbine combined engine characterized by that. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を８０℃前後として冷却水に水道水（７０）を使用して温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and supplies hot water to the customer by using tap water (70) as cooling water with a saturation temperature of about 80 ° C. by an air extractor. An all-blade steam gas turbine combined engine characterized by that. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して空気抽出器により飽和温度を６０℃前後として冷却水に水道水（７０）を使用して温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and supplies hot water to the consumer by using tap water (70) as cooling water with a saturation temperature of about 60 ° C. by an air extractor. An all-blade steam gas turbine combined engine characterized by that. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して温熱を需要家に供給して海水温度等の上昇を廃止することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, and uses tap water (70) as cooling water to supply heat to consumers and eliminate the rise in seawater temperature and the like. An all-blade steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して温熱を需要家に供給して地球温暖化を防止することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery device (66a) is configured in substantially the same manner as a condenser, and uses tap water (70) as cooling water to supply heat to consumers to prevent global warming. An all-blade steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収し、凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, and supplies condensed water to the combustor and heat exchanger (4). An all-blade steam gas turbine combined engine characterized by: 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, supplies warm heat to consumers, and condensate water as a combustor. An all-blade steam gas turbine combined engine, which is supplied to a heat exchanger (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、凝縮水を燃焼器兼熱交換器（４）に供給し、燃料燃焼質量を低減することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, supplies warm heat to consumers, and condensate water as a combustor. An all-blade steam gas turbine combined engine, characterized in that it is supplied to a heat exchanger (4) to reduce the fuel combustion mass. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度１００℃前後の凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as the cooling water, supplies the heat to the customer, and has a saturation temperature of about 100 ° C. An all-blade steam gas turbine combined engine characterized by supplying condensed water to a combustor and heat exchanger (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度８０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as the cooling water, supplies the heat to the customer, and has a saturation temperature of about 80 ° C. An all-blade steam gas turbine combined engine characterized by supplying condensed water to a combustor and heat exchanger (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度６０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, supplies warm heat to consumers, and has a saturation temperature of around 60 ° C. An all-blade steam gas turbine combined engine characterized by supplying condensed water to a combustor and heat exchanger (4). 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度１００℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as the cooling water, supplies the heat to the customer, and has a saturation temperature of about 100 ° C. An all-blade steam gas turbine combined engine that supplies condensed water to a combustor and heat exchanger (4) and stores tap water as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度８０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as the cooling water, supplies the heat to the customer, and has a saturation temperature of about 80 ° C. An all-blade steam gas turbine combined engine that supplies condensed water to a combustor and heat exchanger (4) and stores tap water as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度６０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, supplies warm heat to consumers, and has a saturation temperature of around 60 ° C. An all-blade steam gas turbine combined engine that supplies condensed water to a combustor and heat exchanger (4) and stores tap water as heat. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度１００℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as the cooling water, supplies the heat to the customer, and has a saturation temperature of about 100 ° C. An all-blade steam gas turbine combined engine, which supplies condensed water to a combustor and heat exchanger (4), stores tap water as hot heat, and supplies it to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度８０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as the cooling water, supplies the heat to the customer, and has a saturation temperature of about 80 ° C. An all-blade steam gas turbine combined engine, which supplies condensed water to a combustor and heat exchanger (4), stores tap water as hot heat, and supplies it to consumers. 前記気化潜熱回収器（６６ａ）は、復水器と略同様に構成して冷却水に水道水（７０）を使用して熱回収して温熱を需要家に供給し、飽和温度６０℃前後の凝縮水を燃焼器兼熱交換器（４）に供給し、水道水を温熱としても貯蔵して需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  The vaporization latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat by using tap water (70) as cooling water, supplies warm heat to consumers, and has a saturation temperature of around 60 ° C. An all-blade steam gas turbine combined engine, which supplies condensed water to a combustor and heat exchanger (4), stores tap water as hot heat, and supplies it to consumers. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して水蒸気を冷却することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that tap water is used as cooling water for the vaporization latent heat recovery unit (66a) to cool water vapor. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して水蒸気を冷却して貯蔵し温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized in that tap water is used as cooling water for the vaporization latent heat recovery unit (66a) to cool and store water vapor and supply heat to consumers. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して水蒸気を冷却して貯蔵し１００℃に近い温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that tap water is used as cooling water for the vaporization latent heat recovery unit (66a) to cool and store water vapor, and supply heat to the consumer at a temperature close to 100 ° C. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して水蒸気を冷却して貯蔵し１００℃以下の温熱を需要家に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that tap water is used as cooling water for the vaporization latent heat recovery unit (66a) to cool and store water vapor and supply heat to 100 ° C. or less to consumers. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して水蒸気を冷却し、凝縮水全部を燃焼器兼熱交換器（４）に供給して超臨界圧力高温水（５ｂ）にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The tap water is used as the cooling water of the vaporization latent heat recovery device (66a) to cool the water vapor, and all the condensed water is supplied to the combustor and heat exchanger (4) to form supercritical pressure high temperature water (5b). An all-blade steam gas turbine combined engine characterized by that. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して水蒸気を冷却し、凝縮水全部を燃焼器兼熱交換器（４）に供給して高温水（５ｂ）にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The tap water is used as the cooling water of the vaporization latent heat recovery device (66a) to cool the water vapor, and all the condensed water is supplied to the combustor and heat exchanger (4) to form high-temperature water (5b). An all-blade steam gas turbine combined engine. 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して水蒸気を冷却し、凝縮水全部を燃焼器兼熱交換器（４）に供給して燃料供給熱量を気化潜熱に近付けて低減し、超臨界圧力高温水（５ｂ）にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The tap water is used as the cooling water for the vaporization latent heat recovery unit (66a) to cool the water vapor, and all the condensed water is supplied to the combustor and heat exchanger (4) to reduce the amount of heat supplied to the fuel close to the vaporization latent heat. And an all-blade steam gas turbine combined engine characterized by using supercritical pressure high-temperature water (5b). 前記気化潜熱回収器（６６ａ）の冷却水に水道水を使用して水蒸気を冷却し、凝縮水全部を燃焼器兼熱交換器（４）に供給して燃料供給熱量を気化潜熱に近付けて低減し、高温水（５ｂ）にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The tap water is used as the cooling water for the vaporization latent heat recovery unit (66a) to cool the water vapor, and all the condensed water is supplied to the combustor and heat exchanger (4) to reduce the amount of heat supplied to the fuel close to the vaporization latent heat. And an all-blade steam gas turbine combined engine characterized by using high-temperature water (5b). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種着磁摩擦車や各種磁着摩擦車は、回転方向上流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  Various magnetized friction wheels and various magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the upstream side in the rotation direction, and are used interchangeably as appropriate. And an all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種着磁摩擦車や各種磁着摩擦車は、回転方向上流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The magnetized friction wheel and the various magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the upstream side in the rotational direction so that they are interchangeable as appropriate. An all-rotor-blade steam gas turbine combined engine characterized in that, while being used, the waterway is communicated with water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種着磁摩擦車や各種磁着摩擦車は、回転方向下流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  Various magnetized friction wheels and various magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the downstream side in the rotation direction, and are used interchangeably as appropriate. And an all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種着磁摩擦車や各種磁着摩擦車は、回転方向下流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The magnetized friction wheel and the various magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the downstream side in the rotational direction so that they are appropriately interchangeable. An all-rotor-blade steam gas turbine combined engine characterized in that, while being used, the waterway is communicated with water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向上流側及び下流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with electromagnets (34) on the upstream side and the downstream side in the rotational direction, respectively. An all-blade steam gas turbine combined engine characterized in that the waterway is connected to the water injection means (56) while being used interchangeably. 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向上流側及び下流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with bar magnets (33) on the upstream side and the downstream side in the rotational direction, respectively. An all-rotor-blade steam gas turbine combined engine characterized by being used interchangeably as appropriate and having a waterway connected to water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向上流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and the various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the upstream side in the rotational direction so that they are appropriately interchangeable. The all-blade steam gas turbine combined engine characterized in that the intermediate waterway is connected to the water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向上流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the upstream side in the rotation direction, and are interchangeable as appropriate. The all-blade steam gas turbine combined engine characterized in that the intermediate waterway is connected to the water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向下流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the downstream side in the rotation direction, and are interchangeable as appropriate. The all-blade steam gas turbine combined engine characterized in that the intermediate waterway is connected to the water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向下流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the downstream side in the rotation direction, and are interchangeable as appropriate. The all-blade steam gas turbine combined engine characterized in that the intermediate waterway is connected to the water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により、燃焼器兼熱交換器（４）に供給する水を昇圧して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water supply pump and counter-rotating magnetic friction power transmission device (14a) boosts and uses the water supplied to the combustor and heat exchanger (4), and communicates the water channel to the water injection means (56). An all-blade steam gas turbine combined engine characterized by that. 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により、燃焼器兼熱交換器（４）に供給する水を多段に昇圧して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water supply pump and counter-rotating magnetic friction power transmission device (14a) uses the water supplied to the combustor and heat exchanger (4) by increasing the pressure in multiple stages, and the water channel is used as the water injection means (56). An all-blade steam gas turbine combined engine characterized by communication. 前記複数の送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により、燃焼器兼熱交換器（４）に供給する水を多段に昇圧して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  Water supplied to the combustor and heat exchanger (4) is boosted in multiple stages by the plurality of water pumps and counter-rotating magnetic frictional power transmission devices (14a) and used in the middle of the water channel. All-blade steam gas turbine combined engine characterized by 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water pump and counter-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor and heat exchanger (4), and communicates the water channel to the water injection means (56). An all-blade steam gas turbine combined engine. 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に、該水圧上昇により送水ポンプ（９７）を非接触に近付けると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water pump and counter-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor and heat exchanger (4), and brings the water pump (97) close to non-contact by the increase in water pressure. An all-blade steam gas turbine combined engine characterized in that the waterway is connected to the water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に、該水圧上昇により送水ポンプ（９７）を非接触に近付けて超高速回転に対応すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water pump and counter-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor and heat exchanger (4), and brings the water pump (97) close to non-contact by the increase in water pressure. An all-rotor-steam gas turbine combined engine that supports ultra-high speed rotation and that communicates a waterway along the way with water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に、該水温を上昇して使用すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water pump and counter-rotating magnetic frictional power transmission device (14a) uses water supplied to the combustor and heat exchanger (4), uses the water at an elevated temperature, and injects water in the middle of the water channel. An all blade steam gas turbine combined engine characterized in that it communicates with the means (56). 前記送水送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に水温を上昇して使用し、該水に物質を混入して公害低減し、潤滑すると共に、途中水路を水噴射手段（５６）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water / water pump and counter-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4) and increases the water temperature, and mixes substances into the water. The all-rotor-blade steam gas turbine combined engine characterized in that pollution is reduced, lubrication is performed, and the waterway is connected to the water injection means (56). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種着磁摩擦車や各種磁着摩擦車は、回転方向上流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  Various magnetized friction wheels and various magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the upstream side in the rotation direction, and are used interchangeably as appropriate. And an all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種着磁摩擦車や各種磁着摩擦車は、回転方向上流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The magnetized friction wheel and the various magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the upstream side in the rotational direction so that they are interchangeable as appropriate. An all-blade steam gas turbine combined engine characterized in that it is used and the waterway is communicated with water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種着磁摩擦車や各種磁着摩擦車は、回転方向下流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  Various magnetized friction wheels and various magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the downstream side in the rotation direction, and are used interchangeably as appropriate. And an all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種着磁摩擦車や各種磁着摩擦車は、回転方向下流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The magnetized friction wheel and the various magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the downstream side in the rotational direction so that they are appropriately interchangeable. An all-blade steam gas turbine combined engine characterized in that it is used and the waterway is communicated with water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向上流側及び下流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with electromagnets (34) on the upstream side and the downstream side in the rotational direction, respectively. An all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向上流側及び下流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with bar magnets (33) on the upstream side and the downstream side in the rotational direction, respectively. An all-rotor-blade steam gas turbine combined engine characterized by being used interchangeably as appropriate and having a waterway connected to water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向上流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and the various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the upstream side in the rotational direction so that they are appropriately interchangeable. The all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向上流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the upstream side in the rotation direction, and are interchangeable as appropriate. The all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向下流側に、電磁石（３４）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the downstream side in the rotation direction, and are interchangeable as appropriate. The all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）の各種内着磁摩擦車や各種内磁着摩擦車は、回転方向下流側に、棒磁石（３３）を設けて、夫々適宜に互換して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The various internally magnetized friction wheels and various internally magnetized friction wheels of the water pump and counter-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the downstream side in the rotation direction, and are interchangeable as appropriate. The all-blade steam gas turbine combined engine characterized in that the waterway is communicated with the water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により、燃焼器兼熱交換器（４）に供給する水を昇圧して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water supply pump and counter-rotating magnetic friction power transmission device (14a) boosts and uses the water supplied to the combustor and heat exchanger (4), and communicates the water channel to the water injection means (56a). An all-blade steam gas turbine combined engine characterized by that. 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により、燃焼器兼熱交換器（４）に供給する水を多段に昇圧して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water supply pump and counter-rotating magnetic friction power transmission device (14a) uses the water supplied to the combustor and heat exchanger (4) by increasing the pressure in multiple stages, and the water channel is used as the water injection means (56a). An all-blade steam gas turbine combined engine characterized by communication. 前記複数の送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）により、燃焼器兼熱交換器（４）に供給する水を多段に昇圧して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  Water supplied to the combustor and heat exchanger (4) is boosted and used in multiple stages by the plurality of water pumps and counter-rotating magnetic frictional power transmission devices (14a), and the water passages are arranged on the way along the water injection means (56a). All-blade steam gas turbine combined engine characterized by 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water pump and counter-rotating magnetic frictional power transmission device (14a) uses water supplied to the combustor / heat exchanger (4) and communicates the water channel to the water injection means (56a). An all-blade steam gas turbine combined engine. 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に、該水圧上昇により送水ポンプ（９７）を非接触に近付けると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water pump and counter-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor and heat exchanger (4), and brings the water pump (97) close to non-contact by the increase in water pressure. An all-rotor-blade steam gas turbine combined engine characterized in that the waterway is connected to the water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に、該水圧上昇により送水ポンプ（９７）を非接触に近付けて超高速回転に対応すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water pump and counter-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor and heat exchanger (4), and brings the water pump (97) close to non-contact by the increase in water pressure. An all-rotor-blade steam gas turbine combined engine characterized by responding to ultra-high-speed rotation and communicating a water channel on the way to water injection means (56a). 前記送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に、該水温を上昇して使用すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water pump and counter-rotating magnetic frictional power transmission device (14a) uses water supplied to the combustor and heat exchanger (4), uses the water at an elevated temperature, and injects water in the middle of the water channel. An all-blade steam gas turbine combined engine characterized in that it communicates with the means (56a). 前記送水送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）は、燃焼器兼熱交換器（４）に供給する水を使用すると共に水温を上昇して使用し、該水に物質を混入して公害低減し、潤滑すると共に、途中水路を水噴射手段（５６ａ）に連絡したことを特徴とする全動翼蒸気ガスタービン合体機関。  The water / water pump and counter-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4) and increases the water temperature, and mixes substances into the water. An all-rotor-blade steam gas turbine combined engine characterized in that pollution is reduced, lubrication is performed, and the waterway is communicated with water injection means (56a). 前記水噴射手段（５６）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で水路を接続使用することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) in an annular manner for each blade stage, and the water channel is connected and used at the assembly annular connection. An all-blade steam gas turbine combined engine having blades (81). 前記水噴射手段（５６）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で水路を接続使用し、該組立環状接続部付近から水噴射することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56) is provided in the vicinity of the assembly annular connection portion, and is integrally cast (84) in an annular manner for each blade stage, and a water channel is connected and used in the assembly annular connection portion. An all-blade steam gas turbine combined engine comprising an electromagnetically heated turbine rotor blade (81), characterized by being injected. 前記水噴射手段（５６）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で水路を接続使用し、該組立環状接続部付近から水噴射して圧縮空気を冷却し、熱回収することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56) is provided in the vicinity of the assembly annular connection portion, and is integrally cast (84) in an annular manner for each blade stage, and a water channel is connected and used in the assembly annular connection portion. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), which is jetted to cool compressed air and recover heat. 前記水噴射手段（５６）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で水路を接続使用し、該組立環状接続部付近から水噴射して圧縮空気を冷却し、熱回収した冷空気を略直線蛇行的に圧縮することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56) is provided in the vicinity of the assembly annular connection portion, and is integrally cast (84) in an annular manner for each blade stage, and a water channel is connected and used in the assembly annular connection portion. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), wherein the compressed air is injected and cooled to compress the heat-recovered cold air in a substantially linear meandering manner. 前記水噴射手段（５６）は組立環状接続部付近に設け、撥水性水冷却翼（８７）を冷却手段（５５）の水路で段落半分を冷却後に水噴射手段（５６）より水噴射する全動翼蒸気ガスタービン合体機関。  The water injection means (56) is provided in the vicinity of the assembly annular connection, and the water repellent water cooling blade (87) is fully moved to inject water from the water injection means (56) after cooling the half of the stage in the water passage of the cooling means (55). Wing steam gas turbine combined engine. 前記水噴射手段（５６）は組立環状接続部付近に設け、撥水性水冷却翼（８７）を冷却手段（５５）の水路で段落全部を冷却後に水噴射手段（５６）より水噴射する全動翼蒸気ガスタービン合体機関。  The water injection means (56) is provided in the vicinity of the assembly annular connection, and the water repellent water cooling blade (87) is fully moved to inject water from the water injection means (56) after cooling the entire stage in the water channel of the cooling means (55). Wing steam gas turbine combined engine. 前記水噴射手段（５６）は組立環状接続部付近に設け、撥水性水冷却翼（８７）を冷却手段（５５）の水路で段落複数を冷却後に水噴射手段（５６）より水噴射する全動翼蒸気ガスタービン合体機関。  The water injection means (56) is provided in the vicinity of the assembly annular connection, and the water repellent water cooling blade (87) is fully moved to inject water from the water injection means (56) after cooling a plurality of stages in the water channel of the cooling means (55). Wing steam gas turbine combined engine. 前記水噴射手段（５６）は組立環状接続部付近に設け、撥水性水冷却翼（８７）を冷却手段（５５）の水路で段落多数を冷却後に水噴射手段（５６）より水噴射する全動翼蒸気ガスタービン合体機関。  The water injection means (56) is provided in the vicinity of the assembly annular connection, and the water repellent water cooling blade (87) is cooled by the water passage of the cooling means (55), and then the water injection means (56) injects water from the water injection means (56). Wing steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  Combined moving blade steam gas turbine with electromagnetically heated turbine rotor blade (81), wherein water injection steam is cooled by water injection means (56a) and steam velocity is converted into water mass velocity energy organ. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  All the moving blades equipped with electromagnetically heated turbine blades (81), wherein water injection steam having a temperature equal to or lower than the saturation temperature is cooled by the water injection means (56a), and the steam velocity is converted into velocity energy of water mass. Steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して単位重力仕事率を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade (81) is provided, which cools water-injected steam from the water-injecting means (56a) and converts the steam velocity into water mass velocity energy to increase unit gravity power. All rotor blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して単位重力仕事率を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade that cools water-injected water vapor having a temperature equal to or lower than a saturation temperature from the water-injecting means (56a), converts the vapor velocity into velocity energy of water mass, and increases unit gravity power. 81) an all-blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade (81) is provided which cools water-injected steam from the water-injecting means (56a) and converts the steam velocity into water mass velocity energy to increase the total gravitational power. All rotor blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade that cools water-injected steam having a temperature equal to or lower than a saturation temperature from the water-injecting means (56a), converts the steam velocity into water mass velocity energy, and increases the total gravitational power. 81) an all-blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大して出力を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The electromagnetically heated turbine rotor blade is characterized in that the water jet steam is cooled by the water jet means (56a), the steam speed is converted into water mass speed energy, the total gravity power is increased, and the output is increased. (81) 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大して出力を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetic wave characterized in that water jet steam having a temperature equal to or lower than a saturation temperature is cooled from the water jet means (56a), the steam velocity is converted into velocity energy of water mass, the total gravity power is increased, and the output is increased. An all blade steam gas turbine combined engine equipped with a heated turbine blade (81). 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して単位重力仕事率を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the steam velocity is converted into water-mass velocity energy to increase the unit gravity power. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して単位重力仕事率を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that water jet steam having a temperature equal to or lower than a saturation temperature is cooled from the water jet means (56a), and the steam velocity is converted into velocity energy of water mass to increase unit gravity power. Combined organization. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the steam velocity is converted into velocity energy of water mass to increase the total gravity power. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine characterized by cooling water-injected steam below the saturation temperature from the water-injecting means (56a) and converting the steam velocity into water mass velocity energy to increase the total gravitational power. Combined organization. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大して出力を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  The total moving blade steam gas characterized in that the water jet steam is cooled by the water jet means (56a), the steam speed is converted into the speed energy of the water mass, the total gravity power is increased, and the output is increased. Turbine coalescence engine. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大して出力を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  The water jetting steam having a temperature equal to or lower than the saturation temperature is cooled by the water jetting means (56a), the steam velocity is converted into the velocity energy of the water mass, the total gravity power is increased, and the output is increased. Rotor steam gas turbine combined engine. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、排気排水温度を低下することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), wherein the water-injected steam below the saturation temperature is cooled by the water-injecting means (56a) to lower the exhaust drainage temperature. . 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、排気排水温度を低下して冷却水量を僅少とすることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  All of the electromagnetically heated turbine rotor blades (81) are provided, which cool water-injected steam below the saturation temperature from the water-injecting means (56a), lower the exhaust water temperature, and reduce the amount of cooling water. Rotor steam gas turbine combined engine. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、排気排水温度を低下して冷却水量を僅少とし、地球温暖化防止することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The electromagnetically heated turbine rotor blade (81) is characterized in that water jet steam having a temperature equal to or lower than a saturation temperature is cooled by the water jet means (56a), the exhaust water temperature is lowered, the amount of cooling water is reduced, and global warming is prevented. ) Equipped with all rotor blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、排気排水温度を低下することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that water injection steam having a temperature equal to or lower than a saturation temperature is cooled by the water injection means (56a) to lower the exhaust drainage temperature. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、排気排水温度を最低にして冷却水温度の上昇を僅少とすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized by cooling water-injected water vapor below the saturation temperature from the water-injecting means (56a) to minimize the exhaust water temperature and to minimize the rise in cooling water temperature. 前記水噴射手段（５６ａ）より飽和温度以下の水噴射水蒸気を冷却して、排気排水温度を最低にして冷却水温度の上昇を僅少とし、地球温暖化防止することを特徴とする全動翼蒸気ガスタービン合体機関。  Water-jet steam having a temperature equal to or lower than the saturation temperature is cooled by the water-injecting means (56a), the exhaust water temperature is minimized, the rise in cooling water temperature is minimized, and global warming is prevented. Gas turbine combined engine. 前記水噴射手段（５６ａ）より最終段飽和温度以下の水噴射水蒸気を冷却して、排気排水温度を最低にして冷却水温度の上昇を僅少とし、地球温暖化防止することを特徴とする全動翼蒸気ガスタービン合体機関。  Water movement water vapor below the final stage saturation temperature is cooled by the water injection means (56a), the exhaust water temperature is minimized, the rise in the cooling water temperature is minimized, and global warming is prevented. Wing steam gas turbine combined engine. 前記水噴射手段（５６ａ）より復水器真空最終段飽和温度以下の水噴射水蒸気を冷却して、排気排水温度を最低にして冷却水温度の上昇を僅少とし、地球温暖化防止することを特徴とする全動翼蒸気ガスタービン合体機関。  The water jet steam below the condenser vacuum final stage saturation temperature is cooled from the water jet means (56a), the exhaust water temperature is minimized, the rise in the coolant temperature is minimized, and global warming is prevented. An all-blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、水蒸気容積の増大を既存蒸気タービンの１／１００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the steam volume increases to 1/100 or less of that of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、水蒸気容積の増大を既存蒸気タービンの１／３００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the steam volume increases to 1/300 or less of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、水蒸気容積の増大を既存蒸気タービンの１／６００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) to increase the steam volume to 1/600 or less of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、水蒸気容積の増大を既存蒸気タービンの１／１０００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the steam volume increases to 1/1000 or less of that of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、全重力仕事率を既存ガスタービンの５００倍前後にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the total gravity power is about 500 times that of the existing gas turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、全重力仕事率を既存ガスタービンの４００倍前後にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the total gravity power is about 400 times that of the existing gas turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、全重力仕事率を既存ガスタービンの６００倍前後にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the total gravitational power is about 600 times that of the existing gas turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、全重力仕事率を既存ガスタービンの７００倍前後にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the total gravity power is about 700 times that of the existing gas turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、全重力仕事率を既存ガスタービンの８００倍前後にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the total gravitational power is about 800 times that of the existing gas turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、全重力仕事率を既存ガスタービンの１０００倍前後にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) and the total gravitational power is about 1000 times that of the existing gas turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、全重力仕事率を既存ガスタービンの３００倍前後にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the total gravity power is about 300 times that of the existing gas turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、全重力仕事率を既存ガスタービンの１００倍前後にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) to make the total gravity power about 100 times that of the existing gas turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力動翼面積を既存蒸気タービンの１／５００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the same output rotor blade area is 1/500 or less of that of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力動翼面積を既存蒸気タービンの１／４００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the same output rotor blade area is 1/400 or less of that of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力動翼面積を既存蒸気タービンの１／３００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the same output rotor blade area is 1/300 or less of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力動翼面積を既存蒸気タービンの１／２００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the same output rotor blade area becomes 1/200 or less of that of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力動翼面積を既存蒸気タービンの１／１００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the same output rotor blade area is 1/100 or less of that of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力動翼面積を既存蒸気タービンの１／５０以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) to make the same output rotor blade area 1/50 or less of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力動翼面積を既存蒸気タービンの１／２０以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the same output rotor blade area becomes 1/20 or less of that of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力動翼面積を既存蒸気タービンの１／１０以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a) so that the same output rotor blade area is 1/10 or less of that of the existing steam turbine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力冷却水温度例えば海水温度の上昇を既存蒸気タービンの１／１０００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the increase in the same-output cooling water temperature, for example, seawater temperature is 1/1000 or less of that of the existing steam turbine. . 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力冷却水温度例えば海水温度の上昇を既存蒸気タービンの１／５００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the increase in the same-output cooling water temperature, for example, seawater temperature is made 1/500 or less of the existing steam turbine. . 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力冷却水温度例えば海水温度の上昇を既存蒸気タービンの１／２００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the increase in the same-output cooling water temperature, for example, seawater temperature is 1/200 or less of that of the existing steam turbine. . 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力冷却水温度例えば海水温度の上昇を既存蒸気タービンの１／１００以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the increase in the same-output cooling water temperature, for example, seawater temperature is made 1/100 or less of that of the existing steam turbine. . 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力冷却水温度例えば海水温度の上昇を既存蒸気タービンの１／５０以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the increase in the same-output cooling water temperature, for example, seawater temperature is made 1/50 or less of the existing steam turbine. . 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力冷却水温度例えば海水温度の上昇を既存蒸気タービンの１／２０以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the increase in the same-output cooling water temperature, for example, seawater temperature is reduced to 1/20 or less of that of the existing steam turbine. . 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、同一出力冷却水温度例えば海水温度の上昇を既存蒸気タービンの１／１０以下にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the increase in the same-output cooling water temperature, for example, seawater temperature, is 1/10 or less of that of the existing steam turbine. . 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  Combined moving blade steam gas turbine with electromagnetically heated turbine rotor blade (81), wherein water injection steam is cooled by water injection means (56a) and steam velocity is converted into water mass velocity energy organ. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の重力仕事率に変換することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  A full-swing-blade steam gas turbine provided with an electromagnetically heated turbine rotor blade (81), wherein the water-injected steam is cooled by the water-injecting means (56a), and the steam speed is converted into the gravity power of water mass. Combined organization. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して単位重力仕事率を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade (81) is provided, which cools water-injected steam from the water-injecting means (56a) and converts the steam velocity into water mass velocity energy to increase unit gravity power. All rotor blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade (81) is provided which cools water-injected steam from the water-injecting means (56a) and converts the steam velocity into water mass velocity energy to increase the total gravitational power. All rotor blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大して出力を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The electromagnetically heated turbine rotor blade is characterized in that the water jet steam is cooled by the water jet means (56a), the steam speed is converted into water mass speed energy, the total gravity power is increased, and the output is increased. (81) 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度及を水質量の速度エネルギに変換して単位重力仕事率を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), the steam velocity and the water mass are converted into velocity energy, and the unit gravity power is increased. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the water-injected steam is cooled by the water-injecting means (56a), and the steam velocity is converted into velocity energy of water mass to increase the total gravity power. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度及び気化潜熱を水質量の速度エネルギに変換して全重力仕事率を増大して出力を増大することを特徴とする全動翼蒸気ガスタービン合体機関。  Water movement water vapor is cooled by the water injection means (56a), the vapor velocity and the latent heat of vaporization are converted into water mass velocity energy to increase the total gravitational power and increase the output. Wing steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度の大部分を水質量の速度エネルギに変換することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  All blade steam provided with an electromagnetically heated turbine rotor blade (81), wherein water spray water vapor is cooled by the water injection means (56a), and most of the steam velocity is converted into velocity energy of water mass. Gas turbine combined engine. 前記水噴射手段（５６ａ）より、水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して略直線蛇行的に噴射して出力を発生することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  Electromagnetic heating turbine operation characterized in that the water injection steam is cooled by the water injection means (56a), the steam velocity is converted into velocity energy of water mass and injected in a substantially linear meandering manner. An all-blade steam gas turbine combined engine having blades (81). 前記水噴射手段（５６ａ）より、水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して、略直線蛇行的に噴射して出力を発生することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The electromagnetically heated turbine which cools water-injected steam from the water-injecting means (56a), converts the steam velocity into water-mass velocity energy, and injects substantially linearly in a meandering manner to generate an output. An all-blade steam gas turbine combined engine equipped with a moving blade (81). 前記水噴射手段（５６ａ）より、水噴射水蒸気を冷却して、蒸気速度を水質量の重力仕事率に変換して、略直線蛇行的に噴射して出力を発生することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  Electromagnetic heating characterized by cooling water-injected water vapor from the water-injecting means (56a), converting the vapor velocity into the gravity power of water mass, and injecting substantially linearly meandering to generate output. An all-blade steam gas turbine combined engine equipped with a turbine rotor blade (81). 前記水噴射手段（５６ａ）より、水噴射水蒸気を冷却して、蒸気速度の大部分を水質量の速度エネルギに変換して略直線蛇行的に噴射して出力を発生することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The electromagnetic wave characterized in that the water injection means (56a) cools water injection water vapor, converts most of the vapor velocity into velocity energy of water mass, and injects it in a substantially linear meandering manner to generate an output. An all-blade steam gas turbine combined engine equipped with a heated turbine blade (81). 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続使用することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection portion, and is integrally cast (84) in an annular manner for each blade stage, and a water channel insulated by the assembly annular connection portion is connected and used. An all-blade steam gas turbine combined engine equipped with a turbine rotor blade (81). 前記水噴射手段（５６ａ）は、翼段落毎に環状に一体鋳造（８４）した外側タービン動翼群（１９）及び内側タービン動翼群（２０）の、いずれかの組立環状接続部付近に設けたことを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of an assembly annular connection portion of the outer turbine blade group (19) and the inner turbine rotor blade group (20) integrally cast (84) in an annular manner for each blade stage. An all rotor blade steam gas turbine combined engine comprising an electromagnetically heated turbine rotor blade (81) characterized by the above. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続使用し、該組立環状接続部付近から水噴射することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) in an annular manner for each blade stage, and a water passage insulated by the assembly annular connection is used for connection. An all-rotor-steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), wherein water is injected from 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続使用し、該組立環状接続部付近の水噴射手段（５６ａ）から水噴射して、燃焼ガス容積を縮小して質量を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) in an annular manner for each blade stage, and a water passage insulated by the assembly annular connection is used for connection. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81) characterized in that water is injected from the water injection means (56a) to reduce the combustion gas volume and increase the mass. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続使用し、該組立環状接続部付近の水噴射手段（５６ａ）から水噴射して、気化爆発水蒸気容積を縮小して質量を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) in an annular manner for each blade stage, and a water passage insulated by the assembly annular connection is used for connection. A full-blade steam gas turbine combined engine comprising an electromagnetically heated turbine rotor blade (81), wherein water is injected from the water injection means (56a) to reduce the volume of vaporized explosion steam and increase the mass. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続して使用し、該組立環状接続部付近の水噴射手段（５６ａ）から水噴射し、該水に有害物質合成溶解を促進する物質を含めたことを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) for each blade stage, and is used by connecting a water channel insulated by the assembly annular connection. All-blade steam gas turbine provided with an electromagnetically heated turbine rotor blade (81) characterized in that water is injected from a water injection means (56a) in the vicinity of the section and the water contains a substance that promotes synthesis and dissolution of harmful substances Combined organization. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続して使用し、該組立環状接続部付近から水噴射し、該水に有害物質合成溶解を促進する物質を含めて、無害に近付けて排出することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) for each blade stage, and is used by connecting a water channel insulated by the assembly annular connection. All-blade steam gas turbine equipped with electromagnetically heated turbine rotor blade (81), wherein water is jetted from the vicinity of the section, including a substance that promotes the synthesis and dissolution of harmful substances in the water, and exhausted close to harmlessness Combined organization. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  All the moving blades that generate output with high-temperature water (5b) such as supercritical pressure, wherein water-injected steam is cooled by the water-injecting means (56a), and the steam velocity is converted into velocity energy of water mass. Steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の重力仕事率に変換することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  Full motion that generates output with high-temperature water (5b) such as supercritical pressure, wherein the water-injected water vapor is cooled by the water-injecting means (56a), and the vapor velocity is converted into the gravity power of water mass. Wing steam gas turbine combined engine. 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して単位重力仕事率を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) such as supercritical pressure characterized by cooling water-injected water vapor from the water-injecting means (56a) and converting the vapor velocity into water mass velocity energy to increase unit gravity power. All-blade steam gas turbine combined engine that produces output at 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) such as supercritical pressure characterized in that the water-injected water vapor is cooled by the water-injecting means (56a), and the vapor velocity is converted into velocity energy of water mass to increase the total gravitational power. All-blade steam gas turbine combined engine that produces output at 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して全重力仕事率を増大して出力を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The supercritical pressure or the like is characterized by cooling the water-injected water vapor from the water-injecting means (56a), converting the vapor velocity into water mass velocity energy, increasing the total gravity power, and increasing the output. An all-blade steam gas turbine combined engine that generates output from high-temperature water (5b). 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度及を水質量の速度エネルギに変換して単位重力仕事率を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) such as supercritical pressure characterized in that the water-injected water vapor is cooled by the water-injecting means (56a), and the vapor velocity and the water mass are converted into velocity energy to increase unit gravity power. ) All-blade steam gas turbine combined engine that generates output at 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の重力仕事率に変換して全重力仕事率を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  High-temperature water (5b) such as supercritical pressure characterized in that the water-injected water vapor is cooled by the water-injecting means (56a), and the steam velocity is converted into the gravitational power of water mass to increase the total gravitational power. ) All-blade steam gas turbine combined engine that generates output at 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度を水質量の重力仕事率に変換して全重力仕事率を増大して出力を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  Supercritical pressure or the like characterized by cooling the water-injected water vapor from the water-injecting means (56a), converting the vapor velocity into the gravitational power of water mass and increasing the total gravity power to increase the output All-blade steam gas turbine combined engine that generates output with high-temperature water (5b). 前記水噴射手段（５６ａ）より水噴射水蒸気を冷却して、蒸気速度の大部分を水質量の速度エネルギに変換することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection steam is cooled by the water injection means (56a), and an output is generated by high-temperature water (5b) such as supercritical pressure characterized by converting most of the vapor velocity into velocity energy of water mass. All-blade steam gas turbine combined engine. 前記水噴射手段（５６ａ）より、水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して略直線蛇行的に噴射して出力を発生することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  Supercritical pressure, etc., characterized in that the water injection means (56a) cools the water injection water vapor, converts the vapor velocity into water mass velocity energy, and injects in a substantially linear meandering manner to generate an output. All-blade steam gas turbine combined engine that generates output with high-temperature water (5b). 前記水噴射手段（５６ａ）より、水噴射水蒸気を冷却して、蒸気速度を水質量の速度エネルギに変換して、略直線蛇行的に噴射して出力を発生することを特徴とする高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection means (56a) cools the water injection steam, converts the steam velocity into velocity energy of the water mass, and injects it in a substantially linear meandering manner to generate an output. An all-blade steam gas turbine combined engine that generates output in 5b). 前記水噴射手段（５６ａ）より、水噴射水蒸気を冷却して、蒸気速度を水質量の重力仕事率に変換して、略直線蛇行的に噴射して出力を発生することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  Supercriticality characterized in that the water injection means (56a) cools the water injection water vapor, converts the vapor velocity into the gravitational power of the water mass, and generates an output by substantially linearly meandering injection. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5b) such as pressure. 前記水噴射手段（５６ａ）より、水噴射水蒸気を冷却して、蒸気速度の大部分を水質量の速度エネルギに変換して略直線蛇行的に噴射して出力を発生することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water jet means (56a) cools the water jet steam, converts most of the steam velocity into water mass velocity energy, and jets in a substantially linear meander to produce an output. An all-blade steam gas turbine combined engine that generates output from high-temperature water (5b) such as critical pressure. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続使用することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection portion, and is integrally cast (84) in an annular manner for each blade stage, and a water passage insulated by the assembly annular connection portion is used for connection. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5b) such as pressure. 前記水噴射手段（５６ａ）は、翼段落毎に環状に一体鋳造（８４）した外側タービン動翼群（１９）及び内側タービン動翼群（２０）の、いずれかの組立環状接続部付近に設けたことを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of an assembly annular connection portion of the outer turbine blade group (19) and the inner turbine rotor blade group (20) integrally cast (84) in an annular manner for each blade stage. An all-blade steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続使用し、該組立環状接続部付近から水噴射することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) in an annular manner for each blade stage, and a water passage insulated by the assembly annular connection is used for connection. An all-rotor-steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure, wherein water is injected from 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続使用し、該組立環状接続部付近の水噴射手段（５６ａ）から水噴射して、燃焼ガス容積を縮小して質量を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) in an annular manner for each blade stage, and a water passage insulated by the assembly annular connection is used for connection. All-blade steam gas turbine for generating output with high-temperature water (5b) such as supercritical pressure, wherein water is injected from the water injection means (56a) of the engine and the mass is increased by reducing the volume of combustion gas Combined organization. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続使用し、該組立環状接続部付近の水噴射手段（５６ａ）から水噴射して、過熱蒸気容積を縮小して質量を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) in an annular manner for each blade stage, and a water passage insulated by the assembly annular connection is used for connection. All-blade steam gas turbine for generating output with high-temperature water (5b) such as supercritical pressure, wherein water is injected from the water injection means (56a) of the water and the mass of the superheated steam is reduced to increase the mass Combined organization. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続して使用し、該組立環状接続部付近の水噴射手段（５６ａ）から水噴射し、該水に有害物質合成溶解を促進する物質を含めたことを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) for each blade stage, and is used by connecting a water channel insulated by the assembly annular connection. Full-motion that generates output with high-temperature water (5b) such as supercritical pressure, characterized in that water is injected from the water injection means (56a) near the head and contains a substance that promotes the synthesis and dissolution of harmful substances. Wing steam gas turbine combined engine. 前記水噴射手段（５６ａ）は組立環状接続部付近に設け、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で断熱した水路を接続して使用し、該組立環状接続部付近から水噴射し、該水に有害物質合成溶解を促進する物質を含めて、無害に近付けて排出することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The water injection means (56a) is provided in the vicinity of the assembly annular connection, and is integrally cast (84) for each blade stage, and is used by connecting a water channel insulated by the assembly annular connection. Full motion that generates output in high-temperature water (5b) such as supercritical pressure, characterized by being ejected from the vicinity of the water, and containing water that promotes the synthesis and dissolution of harmful substances in the water. Wing steam gas turbine combined engine. 前記水により撥水性水冷却翼（８７）を冷却後に、組立環状接続部付近に設けた水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  After the water-repellent water cooling blade (87) is cooled by the water, the assembly annular connection portion for water injection from the water injection means (56) provided in the vicinity of the assembly annular connection portion is integrally cast annularly for each blade stage (84) An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), wherein the water passage of the cooling means (55) is connected and used at the assembly annular connection portion. 前記水により撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The assembly annular connection portion for injecting water from the water injection means (56) after cooling the water-repellent water cooling blade with the water is integrally cast (84) in an annular manner for each blade stage, and the assembly annular connection portion cools the cooling means ( 55) A water turbine steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), characterized in that the water passage of (55) is connected. 前記水により１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An assembly annular connection for water injection from the water injection means (56) after cooling one or more water-repellent water cooling blades with water is integrally cast (84) annularly for each blade stage, and the assembly annular connection And an all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), wherein the water passage of the cooling means (55) is connected and used. 前記水により段落全部の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The assembly annular connection for water injection from the water injection means (56) after cooling the water-repellent water cooling blades in the entire paragraph with the water is integrally cast (84) in an annular manner for each blade stage, An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), wherein the water passage of the cooling means (55) is connected and used. 前記水により段落半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  The assembly annular connection for water injection from the water injection means (56) after cooling the water-repellent water cooling blade of the half of the paragraph with water is integrally cast (84) in an annular form for each blade stage, An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), wherein the water passage of the cooling means (55) is connected and used. 前記水により撥水性水冷却翼（８７）を冷却後に、組立環状接続部付近に設けた水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  After the water-repellent water cooling blade (87) is cooled by the water, the assembly annular connection portion for water injection from the water injection means (56) provided in the vicinity of the assembly annular connection portion is integrally cast annularly for each blade stage (84) An all-blade steam gas turbine combined engine for generating output with high-temperature water (5b) such as supercritical pressure, wherein the water passage of the cooling means (55) is connected and used at the assembly annular connection. 前記水により撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The assembly annular connection portion for injecting water from the water injection means (56) after cooling the water-repellent water cooling blade with the water is integrally cast (84) in an annular manner for each blade stage, and the assembly annular connection portion cools the cooling means ( 55) The all-blade steam gas turbine combined engine which generates output with high-temperature water (5b) such as supercritical pressure, characterized in that the water passage of 55) is connected. 前記水により１以上複数の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  An assembly annular connection for water injection from the water injection means (56) after cooling one or more water-repellent water cooling blades with water is integrally cast (84) annularly for each blade stage, and the assembly annular connection And an all-blade steam gas turbine combined engine for generating output with high-temperature water (5b) such as supercritical pressure, wherein the water passage of the cooling means (55) is connected and used. 前記水により段落全部の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The assembly annular connection for water injection from the water injection means (56) after cooling the water-repellent water cooling blades in the entire paragraph with the water is integrally cast (84) in an annular manner for each blade stage, An all-rotor-blade steam gas turbine combined engine that generates output with high-temperature water (5b) such as supercritical pressure, wherein the water passage of the cooling means (55) is connected and used. 前記水により段落半分の撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴射する組立環状接続部は、翼段落毎に環状に一体鋳造（８４）して、該組立環状接続部で冷却手段（５５）の水路を接続使用することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The assembly annular connection for water injection from the water injection means (56) after cooling the water-repellent water cooling blade of the half of the paragraph with water is integrally cast (84) in an annular form for each blade stage, An all-rotor-blade steam gas turbine combined engine that generates output with high-temperature water (5b) such as supercritical pressure, wherein the water passage of the cooling means (55) is connected and used. 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼蒸気ガスタービンの熱回収量を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine unit equipped with an electromagnetically heated turbine rotor blade (81) is characterized in that the amount of heat recovery of the entire rotor blade steam gas turbine is increased by bringing the exhaust temperature of the combustion gas close to -273 ° C. organ. 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼ガスタービンの熱回収量を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81) characterized in that the amount of heat recovery of the entire rotor blade gas turbine is increased by bringing the combustion gas exhaust temperature close to -273 ° C. . 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼蒸気ガスタービンの排気近傍で、低温燃焼ガスによる水蒸気の冷却凝集を容易にすることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade (81) characterized by facilitating cooling and aggregation of water vapor by a low-temperature combustion gas in the vicinity of the exhaust of the entire rotor blade steam gas turbine by bringing the exhaust temperature of the combustion gas close to -273 ° C An all-blade steam gas turbine combined engine equipped with 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼ガスタービンの排気近傍で、低温燃焼ガスによる水蒸気の冷却凝集を容易にすることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade (81) characterized by facilitating the cooling and aggregation of water vapor by low-temperature combustion gas in the vicinity of the exhaust of all rotor blade gas turbines by bringing the exhaust temperature of the combustion gas close to -273 ° C. An all-blade steam gas turbine combined engine equipped. 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼ガスタービンの排気過程で、低温燃焼ガスによる水蒸気の冷却凝集を容易にすることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  An electromagnetically heated turbine rotor blade (81) characterized by facilitating cooling and aggregation of water vapor by a low-temperature combustion gas in the exhaust process of the entire rotor blade gas turbine by bringing the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine equipped. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収し、肥料として供給することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., water vapor is cooled and aggregated with low-temperature combustion gas, separated and recovered as water, etc., and supplied as fertilizer An all blade steam gas turbine combined engine equipped with a heated turbine blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収し、土や植物に固定して肥料として供給することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water, etc., fixed to soil and plants, and supplied as fertilizer An all rotor blade steam gas turbine combined engine comprising an electromagnetically heated turbine rotor blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収し、土や植物に固定して肥料として供給し、食物を増産することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water, etc., fixed to soil and plants, and supplied as fertilizer And an all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81) characterized in that the production of food is increased. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収し、土や植物に固定して肥料として供給し、植物を増産することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water, etc., fixed to soil and plants, and supplied as fertilizer And an all-heated blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81) characterized in that the plant is increased in production. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、海中に供給することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, in which the combustion gas exhaust temperature approaches -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and recovered as water or the like, and supplied to the sea An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収し、海中に供給して、海藻類を繁殖させることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, which brings the combustion gas exhaust temperature close to −273 ° C., water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water, etc., and supplied into the sea to breed seaweeds. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収し、海中に供給して、珊瑚類を繁殖させることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine coalescence engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water, etc., and supplied to the sea to breed moss An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収し、海中に供給して、魚介類を繁殖させることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, which brings the combustion gas exhaust temperature close to −273 ° C., water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water, etc., and supplied to the sea to breed fish and shellfish An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、海水を冷却する過程で酸素等を吸入して、海中に供給することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, which brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and agglomerated with the low-temperature combustion gas, separated and recovered as water, etc., in the process of cooling the seawater, oxygen etc. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81), which is sucked and supplied into the sea. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、酸素等と共に海中に供給して、海藻類を繁殖させることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and agglomerated with low-temperature combustion gas, separated and recovered as water, etc., and supplied to the sea along with oxygen, etc. An all-rotor steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81) characterized by breeding seaweeds. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、酸素等と共に海中に供給して、珊瑚類を繁殖させることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and agglomerated with low-temperature combustion gas, separated and recovered as water, etc., and supplied to the sea along with oxygen, etc. An all-blade steam gas turbine combined engine comprising an electromagnetically heated turbine rotor blade (81) characterized by breeding moss. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、酸素等と共に海中に供給して、微生物や魚介類を繁殖させることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and agglomerated with low-temperature combustion gas, separated and recovered as water, etc., and supplied to the sea along with oxygen, etc. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81) characterized by breeding microorganisms and seafood. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、水道水を冷却することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, the steam is cooled and agglomerated with the low-temperature combustion gas, separated and recovered as water, etc., and the tap water is cooled. An all rotor blade steam gas turbine combined engine comprising an electromagnetically heated turbine rotor blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、水道水を冷却して冷熱で貯蔵することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and aggregated with low-temperature combustion gas, separated and recovered as water, etc., and the tap water is cooled and stored with cold heat. An all rotor blade steam gas turbine combined engine comprising an electromagnetically heated turbine rotor blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、水道水を冷却して冷熱で貯蔵し、供給することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and aggregated with low-temperature combustion gas, separated and recovered as water, etc., and the tap water is cooled and stored with cold heat. And an all-heated blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水等として分別回収して、水道水を冷却して冷熱で貯蔵し、業務用家庭用として供給することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and aggregated with low-temperature combustion gas, separated and recovered as water, etc., and the tap water is cooled and stored with cold heat. And an all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine rotor blade (81), which is supplied for commercial use. 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼蒸気ガスタービンの熱回収量を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  All blades that generate output with high-temperature water (5b) such as supercritical pressure, which increase the heat recovery amount of all blade steam gas turbines by bringing the exhaust temperature of the combustion gas close to −273 ° C. Steam gas turbine combined engine. 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼ガスタービンの熱回収量を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  All blade steam generating power with high-temperature water (5b) such as supercritical pressure, which increases the heat recovery amount of all blade gas turbines by bringing the exhaust temperature of the combustion gas close to −273 ° C. Gas turbine combined engine. 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼蒸気ガスタービンの排気近傍で、低温燃焼ガスによる水蒸気の冷却凝集を容易にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  By bringing the exhaust temperature of the combustion gas close to −273 ° C., high-temperature water such as supercritical pressure is provided, which facilitates cooling and aggregation of water vapor by the low-temperature combustion gas in the vicinity of the exhaust of the all blade steam gas turbine. An all-blade steam gas turbine combined engine that generates output in 5b). 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼ガスタービンの排気近傍で、低温燃焼ガスによる水蒸気の冷却凝集を容易にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  By bringing the exhaust temperature of the combustion gas close to −273 ° C., high-temperature water (5b) such as supercritical pressure, which facilitates cooling and aggregation of water vapor by the low-temperature combustion gas in the vicinity of the exhaust of all blade gas turbines. ) All-blade steam gas turbine combined engine that generates output at 前記燃焼ガス排気温度を−２７３℃に近付けることで、全動翼ガスタービンの排気近傍で、低温燃焼ガスによる水蒸気の冷却凝集を容易にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  By bringing the exhaust temperature of the combustion gas close to −273 ° C., high-temperature water (5b) such as supercritical pressure, which facilitates cooling and aggregation of water vapor by the low-temperature combustion gas in the vicinity of the exhaust of all blade gas turbines. ) All-blade steam gas turbine combined engine that generates output at 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、海中に供給することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, the water vapor is cooled and aggregated by the low-temperature combustion gas, separated and collected as water droplets, and supplied to the sea. An all-blade steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収し、海中に供給して、海藻類を繁殖させることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, which brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and supplied into the sea to propagate seaweed An all-blade steam gas turbine combined engine that generates power with high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収し、海中に供給して、珊瑚類を繁殖させることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, which brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and aggregated by the low-temperature combustion gas, separated and collected as water droplets, etc., and supplied into the sea to breed moss An all-blade steam gas turbine combined engine that generates power with high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収し、海中に供給して、魚介類を繁殖させることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine coalescence engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and supplied to the sea to breed fish and shellfish An all-blade steam gas turbine combined engine that generates power with high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、海水を冷却する過程で酸素等を吸入して、海中に供給することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., in the process of cooling seawater, oxygen etc. An all-blade steam gas turbine combined engine that generates an output from high-temperature water (5b) such as supercritical pressure, which is sucked and supplied into the sea. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、酸素等と共に海中に供給して、海藻類を繁殖させることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and agglomerated with low-temperature combustion gas, separated and recovered as water droplets, etc., and supplied to the sea together with oxygen and the like, An all-rotor-steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure, characterized by breeding seaweeds. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、酸素等と共に海中に供給して、珊瑚類を繁殖させることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and agglomerated with low-temperature combustion gas, separated and recovered as water droplets, etc., and supplied to the sea together with oxygen and the like, An all-rotor-steam gas turbine combined engine that generates power from high-temperature water (5b) such as supercritical pressure, characterized by breeding moss. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、酸素等と共に海中に供給して、微生物や魚介類を繁殖させることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the water vapor is cooled and agglomerated with low-temperature combustion gas, separated and recovered as water droplets, etc., and supplied to the sea together with oxygen and the like, An all-bladed steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure, characterized by breeding microorganisms and seafood. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、肥料にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., the steam is cooled and agglomerated with the low-temperature combustion gas, separated and collected as water droplets, etc., and used as fertilizer. Rotor steam gas turbine combined engine. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収し、肥料にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  Supercriticality characterized in that, in an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and used as fertilizer An all-blade steam gas turbine combined engine that generates output with high-temperature water (5b) such as pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収し、生ゴミや泥土や植物片に固定して肥料にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and fixed to garbage, mud or plant fragments. An all-blade steam gas turbine combined engine characterized by using fertilizer. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収し、生ゴミや泥土や植物片に固定して肥料にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and fixed to garbage, mud or plant fragments. An all-rotor-steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure, characterized by using fertilizer. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、生ゴミに固定して肥料にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and agglomerated with low-temperature combustion gas, separated and collected as water droplets, etc., fixed to raw garbage, and used as fertilizer An all-rotor-steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、泥土に固定して肥料にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and fixed to mud to make fertilizer An all-rotor-steam gas turbine combined engine that generates power with high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、植物片に固定して肥料にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and fixed to a plant piece as fertilizer An all-rotor-steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、生ゴミに固定して肥料にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and agglomerated with low-temperature combustion gas, separated and collected as water droplets, etc., fixed to raw garbage, and used as fertilizer An all-blade steam gas turbine combined engine characterized by that. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、泥土に固定して肥料にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and fixed to mud to make fertilizer An all-blade steam gas turbine combined engine characterized by 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、植物片に固定して肥料にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and fixed to a plant piece as fertilizer An all-blade steam gas turbine combined engine characterized by that. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、水道水を冷却することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, in which the exhaust temperature of the combustion gas approaches -273 ° C, the steam is cooled and agglomerated with the low-temperature combustion gas, separated and recovered as water droplets, etc., and the tap water is cooled. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、水道水を冷却して冷熱で貯蔵することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and tap water is cooled and stored with cold heat An all-blade steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、水道水を冷却して冷熱で貯蔵し、供給することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and tap water is cooled and stored with cold heat An all-blade steam gas turbine combined engine that generates power with high-temperature water (5b) such as supercritical pressure. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、低温燃焼ガスにより水蒸気を冷却凝集して、水滴等として分別回収して、水道水を冷却して冷熱で貯蔵し、業務用家庭用として供給することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water vapor is cooled and aggregated with low-temperature combustion gas, separated and collected as water droplets, etc., and tap water is cooled and stored with cold heat And an all-blade steam gas turbine combined engine that generates output from high-temperature water (5b) such as supercritical pressure, which is supplied for commercial use. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、燃焼器兼熱交換器（４）で微粉炭燃料を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, the pulverized coal fuel is used in the combustor and heat exchanger (4), and the all-blade steam gas turbine combined organ. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、燃焼器兼熱交換器（４）で微粉炭燃料を燃焼させて超臨界圧力等の高温水（５ｂ）で熱回収して使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., pulverized coal fuel is combusted in a combustor and heat exchanger (4) and hot water (5b) such as supercritical pressure is used. An all-blade steam gas turbine combined engine characterized by heat recovery. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、燃焼器兼熱交換器（４）で微粉炭燃料を燃焼させて超臨界圧力等の高温水（５ｂ）で熱回収し、発電用として使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., pulverized coal fuel is combusted in a combustor and heat exchanger (4) and hot water (5b) such as supercritical pressure is used. An all-blade steam gas turbine combined engine that recovers heat and uses it for power generation. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、ゴミガス化燃料を補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine in which waste gasification fuel is supplementarily used in an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、ゴミガス化燃料を燃焼させて超臨界圧力等の高温水（５ｂ）で熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine in which the combustion gas exhaust temperature approaches -273 ° C, the waste gasification fuel is combusted, and heat is recovered with high-temperature water (5b) such as supercritical pressure for auxiliary use. An all-blade steam gas turbine combined engine. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、ゴミガス化燃料を燃焼させて超臨界圧力等の高温水（５ｂ）で熱回収して補助使用し、該燃焼ガス空気を全動翼圧縮機で圧縮することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine where the exhaust temperature of the combustion gas approaches −273 ° C., the waste gasification fuel is combusted, and heat is recovered with high-temperature water (5b) such as supercritical pressure for auxiliary use. A full blade steam gas turbine combined engine characterized by compressing gas air with a full blade compressor. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、ゴミガス化燃料を燃焼させて超臨界圧力等の高温水（５ｂ）で熱回収して補助使用し、該燃焼ガス空気を全動翼圧縮機で圧縮して燃焼器兼熱交換器（４）に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine where the exhaust temperature of the combustion gas approaches −273 ° C., the waste gasification fuel is combusted, and heat is recovered with high-temperature water (5b) such as supercritical pressure for auxiliary use. An all-blade steam gas turbine combined engine characterized in that gas air is compressed by an all-blade compressor and supplied to a combustor and heat exchanger (4). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、燃えるもの全部を燃料として補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine in which the combustion gas exhaust temperature is brought close to -273 ° C, and all burned fuel is auxiliary used as fuel. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、燃えるもの全部を燃料として燃焼させて超臨界圧力等の高温水（５ｂ）で熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine where the exhaust temperature of the combustion gas is close to -273 ° C, all the combustibles are burned as fuel, and heat is recovered with high-temperature water (5b) such as supercritical pressure for auxiliary use. An all-blade steam gas turbine combined engine characterized by 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、燃えるもの全部を燃料として燃焼させて超臨界圧力等の高温水（５ｂ）で熱回収して補助使用し、該燃焼ガス空気を全動翼圧縮機で圧縮することを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, in which the combustion gas exhaust temperature approaches -273 ° C, all the combustibles are combusted as fuel, and heat is recovered with high-temperature water (5b) such as supercritical pressure for auxiliary use. A full blade steam gas turbine combined engine, wherein the combustion gas air is compressed by a full blade compressor. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、燃えるもの全部を燃料として燃焼させて超臨界圧力等の高温水（５ｂ）で熱回収して補助使用し、該燃焼ガス空気を全動翼圧縮機で圧縮して燃焼器兼熱交換器４に供給することを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, in which the combustion gas exhaust temperature approaches -273 ° C, all the combustibles are combusted as fuel, and heat is recovered with high-temperature water (5b) such as supercritical pressure for auxiliary use. An all-blade steam gas turbine combined engine, wherein the combustion gas air is compressed by an all-blade compressor and supplied to the combustor / heat exchanger 4. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気タービンにおいて、起動時のみ全動翼ガスタービンとして使用することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that, in an all-blade steam turbine that brings the combustion gas exhaust temperature close to -273 ° C, it is used as an all-blade gas turbine only at startup. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービンにおいて、起動時のみ全動翼ガスタービンとして使用することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine, which is used as an all-blade gas turbine only at the time of start-up in an all-blade steam gas turbine whose combustion gas exhaust temperature approaches -273 ° C. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, the combustion gas is stored in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure. All-blade steam gas turbine combined engine. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで非常に安全なジエツト機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  It is very safe to store in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C. An all-blade steam gas turbine combined engine characterized in that it is a simple jet machine. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで非常に安全な宇宙往還親飛行機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  It is very safe to store in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C. All-wheeled wing steam gas turbine combined engine, which is characterized by the fact that it is a powerful space return parent plane. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで非常に安全な超音速飛行機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  It is very safe to store in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C. All-wing blade steam gas turbine combined engine characterized by a supersonic airplane. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで非常に安全な超音速旅客機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  It is very safe to store in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C. All-blade steam gas turbine combined engine characterized by a supersonic passenger aircraft. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで非常に安全な飛行船舶としたことを特徴とする全動翼蒸気ガスタービン合体機関。  It is very safe to store in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C. An all-wing-blade steam gas turbine combined engine characterized by being a unique flying vessel. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで非常に安全な飛行物体としたことを特徴とする全動翼蒸気ガスタービン合体機関。  It is very safe to store in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C. All-wing blade steam gas turbine combined engine characterized by being a flying object. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで火災を消火容易発生困難として、非常に安全なジエツト機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  Extinguishing the fire by storing it in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by an extremely safe jet machine that is difficult to generate easily. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで火災を消火容易発生困難として、非常に安全な宇宙往還親飛行機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  Extinguishing the fire by storing it in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C An all-rotor steam gas turbine combined engine characterized by an extremely safe space-returning parent plane that is difficult to generate easily. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで火災を消火容易発生困難として、非常に安全な超音速飛行機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  Extinguishing the fire by storing it in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by an extremely safe supersonic airplane that is difficult to generate easily. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで火災を消火容易発生困難として、非常に安全な超音速旅客機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  Extinguishing the fire by storing it in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by an extremely safe supersonic passenger aircraft that is difficult to generate easily. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで火災を消火容易発生困難として、非常に安全な飛行船舶としたことを特徴とする全動翼蒸気ガスタービン合体機関。  Extinguishing the fire by storing it in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C An all-rotor-blade steam gas turbine combined engine characterized by an extremely safe airship that is difficult to generate easily. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、超臨界圧力等の高温水（５ｂ）で燃焼器兼熱交換器（４）に貯蔵することで火災を消火容易発生困難として、非常に安全な飛行物体としたことを特徴とする全動翼蒸気ガスタービン合体機関。  Extinguishing the fire by storing it in the combustor and heat exchanger (4) with high-temperature water (5b) such as supercritical pressure in the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C An all-blade steam gas turbine combined engine characterized by being a very safe flying object because it is difficult to generate easily. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、特殊装置（９２ａ）によりラムジエツトを遥かに越える落差でバイパス噴射する全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine in which the combustion gas exhaust temperature is brought close to -273 ° C, and bypass injection is performed by a special apparatus (92a) with a head far exceeding the ramjet. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、複数の特殊装置（９２ａ）によりラムジエツトを遥かに越える落差でバイパス噴射する全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine in which the combustion gas exhaust temperature is brought close to -273 ° C, and bypass injection is performed with a drop far exceeding the ramjet by a plurality of special devices (92a). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、特殊装置（９２ｂ）によりラムジエツトを遥かに越える落差でバイパス噴射する全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine in which the combustion gas exhaust temperature is brought close to -273 ° C, and bypass injection is performed by a special apparatus (92b) with a head far exceeding the ramjet. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、複数の特殊装置（９２ｂ）によりラムジエツトを遥かに越える落差でバイパス噴射する全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine in which the combustion gas exhaust temperature is brought close to -273 ° C, and bypass injection is carried out with a head far exceeding the ramjet by a plurality of special devices (92b). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、水噴射装置（９３ｂ）により燃焼ガスをバイパス噴射する全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine in which the combustion gas exhaust temperature is close to -273 ° C, and the combustion gas is bypass-injected by a water injection device (93b). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、複数の水噴射装置（９３ｂ）により燃焼ガスをバイパス噴射する全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine in which the combustion gas exhaust temperature is brought close to -273 ° C, and the combustion gas is bypass-injected by a plurality of water injection devices (93b). 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、水噴射装置（９３ａ）により超臨界圧力等の高温水（５ｂ）をバイパス噴射する全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine coalescence engine that brings the combustion gas exhaust temperature close to -273 ° C, an all-blade steam gas turbine coalescence that bypass-injects high-temperature water (5b) such as supercritical pressure by a water injection device (93a) organ. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関において、複数の水噴射装置（９３ａ）により超臨界圧力等の高温水（５ｂ）をバイパス噴射する全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, the all-blade steam gas that bypass-injects high-temperature water (5b) such as supercritical pressure by a plurality of water injection devices (93a) Turbine coalescence engine. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼ガスタービンにおいて、燃料の燃焼ガス熱量の使用を略０にすることを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  In a full blade gas turbine in which the combustion gas exhaust temperature approaches -273 ° C, the use of the combustion gas calorie of the fuel is made substantially zero, and the whole blade having the electromagnetically heated turbine blade (81) Steam gas turbine combined engine. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼ガスタービンにおいて、燃料の燃焼ガス熱量の使用を略０にすることを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  In an all-blade gas turbine that brings the combustion gas exhaust temperature close to -273 ° C, the use of the combustion gas calorie of the fuel is made substantially zero, and the output is generated by high-temperature water (5b) such as supercritical pressure. An all-blade steam gas turbine combined engine. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関に於いて、低温燃焼ガスにより水蒸気を冷却凝集して水滴等として回収し、水道水を冷却して貯蔵して需要家に供給して業務用や家庭用のクーラーを全廃し、脱フロンにより地球温暖化防止することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, water vapor is cooled and aggregated by low-temperature combustion gas and collected as water droplets, etc., and tap water is cooled and stored for demand. An all-rotor-steam gas turbine combined engine, which is supplied to the house and completely eliminates the use of commercial and household coolers and prevents global warming by removing chlorofluorocarbons. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関に於いて、低温燃焼ガスにより水蒸気を冷却凝集して水滴等として回収し、水道水を冷却して貯蔵して需要家に供給して都市部を丸ごと冷却し、脱フロンにより地球温暖化防止することを特徴とする全動翼蒸気ガスタービン合体機関。  In an all-blade steam gas turbine combined engine where the combustion gas exhaust temperature approaches -273 ° C, water vapor is cooled and aggregated by low-temperature combustion gas and collected as water droplets, etc., and tap water is cooled and stored for demand. An all-swing-blade steam gas turbine combined engine that supplies the house to cool the whole city and prevents global warming by removing chlorofluorocarbons. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関に於いて、低温燃焼ガスにより水蒸気を冷却凝集して水滴等として回収し、水道水を５℃前後に冷却して貯蔵して需要家に供給して業務用や家庭用のクーラーを全廃し、脱フロンにより地球温暖化防止することを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, where the combustion gas exhaust temperature approaches -273 ° C, the water vapor is cooled and aggregated by the low-temperature combustion gas and collected as water droplets, and the tap water is cooled to around 5 ° C. An all-bladed steam gas turbine combined engine that is stored and supplied to consumers to completely abolish commercial and household coolers and to prevent global warming by removing chlorofluorocarbons. 前記燃焼ガス排気温度を−２７３℃に近付ける、全動翼蒸気ガスタービン合体機関に於いて、低温燃焼ガスにより水蒸気を冷却凝集して水滴等として回収し、水道水を５℃前後に冷却して貯蔵して需要家に供給して都市部を丸ごと冷却し、脱フロンにより地球温暖化防止することを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine combined engine, where the combustion gas exhaust temperature approaches -273 ° C, the water vapor is cooled and aggregated by the low-temperature combustion gas and collected as water droplets, and the tap water is cooled to around 5 ° C. An all-bladed steam gas turbine combined engine that stores and cools the whole city by cooling it and prevents global warming by removing CFCs. 前記全動翼蒸気ガスタービン合体機関で使用する水に、公害低減地球温暖化防止するため、物質を混入してＣＯ２等の公害ガスを水に合成溶解容易にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In order to reduce pollution and prevent global warming in the water used in the all-blade steam gas turbine combined engine, a pollutant gas such as CO2 can be easily synthesized and dissolved in water by mixing substances. Steam gas turbine combined engine. 前記全動翼蒸気ガスタービン合体機関で使用する水に、公害低減地球温暖化防止するため、化学物質を混入してＣＯ２等の公害ガスを水に合成溶解容易にすることを特徴とする全動翼蒸気ガスタービン合体機関。  In order to reduce pollution and prevent global warming in the water used in the all-blade steam gas turbine combined engine, chemical substances are mixed to easily synthesize and dissolve pollution gases such as CO2 in water. Wing steam gas turbine combined engine. 前記全動翼蒸気ガスタービン合体機関で使用する水に、公害低減地球温暖化防止するため、物質を混入してＣＯ２等の公害ガスを水に合成溶解して排出することを特徴とする全動翼蒸気ガスタービン合体機関。  In order to reduce pollution and prevent global warming in the water used in the all-blade steam gas turbine combined engine, substances are mixed and polluted gases such as CO2 are synthesized and dissolved in water and discharged. Wing steam gas turbine combined engine. 前記全動翼蒸気ガスタービン合体機関で使用する水に、公害低減地球温暖化防止するため、化学物質を混入してＣＯ２等の公害ガスを水に合成溶解して排出することを特徴とする全動翼蒸気ガスタービン合体機関。  In order to reduce pollution and prevent global warming in the water used in the all-blade steam gas turbine combined engine, chemical substances are mixed and polluted gases such as CO2 are synthesized and dissolved in water and discharged. Rotor steam gas turbine combined engine. 前記全動翼蒸気ガスタービン合体機関は、動力伝達装置に送水ポンプ兼二重反転磁気摩擦動力伝達装置（１４ａ）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine uses a water pump and counter-rotating magnetic friction power transmission device (14a) as a power transmission device. 前記全動翼蒸気ガスタービン合体機関は、動力伝達装置に送水ポンプ兼磁気摩擦動力伝達装置（１００ａ）を使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine uses a water pump / magnetic friction power transmission device (100a) as a power transmission device. 前記全動翼蒸気ガスタービン合体機関のタービン翼は、電磁加熱高温とすることで、水等との間の摩擦損失を低減してタービン翼を動圧反動駆動することを特徴とする全動翼蒸気ガスタービン合体機関。  The turbine blades of the all-blade steam gas turbine combined engine are electromagnetically heated to a high temperature to reduce friction loss with water and the like to drive the turbine blades by dynamic pressure reaction reaction Steam gas turbine combined engine. 前記全動翼蒸気ガスタービン合体機関の圧縮翼は、撥水性を良好とすることで、水等との間の摩擦損失を低減して、効率良く空気圧縮して冷却することを特徴とする全動翼蒸気ガスタービン合体機関。  The compressor blades of the all-blade steam gas turbine combined engine have good water repellency, reduce friction loss with water and the like, and efficiently compress air and cool it. Rotor steam gas turbine combined engine. 前記全動翼圧縮機の撥水性冷却翼（８７）は、撥水性金属・撥水性物質の被覆・撥水性セラミックス・撥水性加工の、何れかで構成して撥水性を良好とすることを特徴とする全動翼蒸気ガスタービン合体機関。  The water-repellent cooling blade (87) of the all-blade compressor is composed of any one of water-repellent metal, water-repellent substance coating, water-repellent ceramics, and water-repellent finish to improve water repellency. An all-blade steam gas turbine combined engine. 前記撥水性冷却翼（８７）は、撥水性金属・撥水性物質の被覆・撥水性セラミックス・撥水性加工の、何れか１以上で構成して撥水性を良好とすることを特徴とする全動翼蒸気ガスタービン合体機関。  The water repellent cooling blade (87) is composed of any one or more of water repellent metal, water repellent material coating, water repellent ceramics, and water repellent finish to improve water repellency. Wing steam gas turbine combined engine. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that superheated high-temperature water (5b) recovered from pulverized coal fuel is supplied to the combustor and heat exchanger 4. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine, wherein the combustor and heat exchanger 4 is supplied with hot water (5b) recovered from pulverized coal fuel. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with supercritical high-temperature water (5b) recovered from waste gasification fuel. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from waste gasification fuel. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from the refined garbage fuel. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine, wherein the combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from the refined garbage fuel. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with supercritical high-temperature water (5b) recovered from all the fuel that burns. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from all the fuel that burns. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with supercritical pressure hot water (5b) recovered from pulverized coal fuel to generate electric power. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with high-temperature water (5b) heat recovered from pulverized coal fuel and used as electric power, and is an all-rotor-steam gas turbine combined engine. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine, wherein the combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from waste gasification fuel to generate electric power. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from waste gasification fuel to generate electric power. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from the refined refuse fuel to generate electric power. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from the refined refuse fuel to generate electric power. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from all the fuels to be burned to generate electric power. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the combustor / heat exchanger 4 is supplied with high-temperature water (5b) recovered from all the fuels to be burned to generate electric power. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombusting in the exchanger 4. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with high-temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. All-blade steam gas turbine combined engine characterized by re-combustion at 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombusting in the exchanger 4. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from the waste gasification fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. All-blade steam gas turbine combined engine characterized by re-combustion at 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from the refined refuse fuel, and the combustion gas is also compressed by a full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombusting in the heat exchanger 4. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by a full blade compressor as electric power. The all-blade steam gas turbine combined engine characterized by re-combusting at No. 4. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by a full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the cum heat exchanger 4. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with high-temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by an all-blade compressor as electric power, thereby combustor / heat exchange. An all-rotor-blade steam gas turbine combined engine characterized by being re-combusted in the vessel 4. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine, which is characterized by recovering recombustion heat in the exchanger 4 and using it normally. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with high-temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. All-blade steam gas turbine combined engine that recovers heat from re-combustion and uses it normally. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine, which is characterized by recovering recombustion heat in the exchanger 4 and using it normally. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from the waste gasification fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. All-blade steam gas turbine combined engine that recovers heat from re-combustion and uses it normally. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from the refined refuse fuel, and the combustion gas is also compressed by a full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that reheated heat is recovered by a heat exchanger 4 and is normally used. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by a full blade compressor as electric power. The all-blade steam gas turbine combined engine, which is characterized in that it is re-combusted and recovered for normal use. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by a full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that the combined heat exchanger 4 recovers recombustion heat for normal use. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with high-temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by an all-blade compressor as electric power, thereby combustor / heat exchange. An all-blade steam gas turbine combined engine characterized in that the combustion heat is recovered by the regenerator 4 and used normally. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that the recombustion heat is recovered by the exchanger 4 and used auxiliary. 前記燃焼器兼熱交換器４には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with high-temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. All-blade steam gas turbine combined engine, which recovers the heat of combustion again and uses it as an auxiliary. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that the recombustion heat is recovered by the exchanger 4 and used auxiliary. 前記燃焼器兼熱交換器４には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from the waste gasification fuel, and the combustion gas is also compressed by an all-blade compressor as electric power. All-blade steam gas turbine combined engine, which recovers the heat of combustion again and uses it as an auxiliary. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from the refined refuse fuel, and the combustion gas is also compressed by a full blade compressor as electric power. An all-blade steam gas turbine combined engine, wherein the heat is re-combusted in the heat exchanger 4 for auxiliary use. 前記燃焼器兼熱交換器４には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with high-temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by a full blade compressor as electric power. 4. An all-blade steam gas turbine combined engine characterized in that the combustion heat is recovered in step 4 and used auxiliary. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor and heat exchanger 4 is supplied with supercritical pressure high-temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by a full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine, wherein the combined heat exchanger 4 recovers recombustion heat for auxiliary use. 前記燃焼器兼熱交換器４には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The combustor / heat exchanger 4 is supplied with high-temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by an all-blade compressor as electric power, thereby combustor / heat exchange. An all-blade steam gas turbine combined engine characterized in that the recombustion heat is recovered by the vessel 4 and used auxiliary. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine combined engine, wherein high-temperature water (5b) recovered from pulverized coal fuel is supplied to a high-temperature water reservoir (32a) of the full-blade steam turbine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine, wherein supercritical pressure high-temperature water (5b) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine combined engine, wherein high-temperature water (5b) recovered from pulverized coal fuel is supplied to a high-temperature water reservoir (32a) of the full-blade steam gas turbine. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) recovered from waste gasification fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine combined engine, wherein high-temperature water (5b) recovered from waste gasification fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam turbine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) recovered from waste gasification fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine combined engine, wherein high-temperature water (5b) recovered from waste gasification fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam gas turbine. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) heat-recovered from dust refined fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine combined engine characterized in that high-temperature water (5b) recovered from the refined refuse fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam turbine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) recovered from the refined garbage fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that high-temperature water (5b) recovered from the refined garbage fuel is supplied to a high-temperature water reservoir (32a) of the all-blade steam gas turbine. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) recovered from all the fuel that burns is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that high-temperature water (5b) recovered from all the fuel that burns is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) recovered from all the fuel that burns is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that high-temperature water (5b) recovered from all the fuel that burns is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5b) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam turbine to generate electric power. . 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that high-temperature water (5b) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine to generate electric power. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The whole blade steam gas turbine combined with the high temperature water reservoir (32a) of the all blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from the pulverized coal fuel to generate electric power. organ. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that high-temperature water (5b) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine to generate electric power. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full rotor blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from the waste gasification fuel to generate electric power, which is used as an electric power. . 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The all blade blade gas turbine combined engine characterized in that the high temperature water reservoir (32a) of the all blade blade steam turbine is supplied with high temperature water (5b) recovered from waste gasification fuel to generate electric power. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The whole blade steam gas turbine combination characterized in that the high temperature water reservoir (32a) of the all blade steam gas turbine is supplied with electric power by supplying supercritical pressure high temperature water (5b) recovered from waste gasification fuel. organ. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that high-temperature water (5b) recovered from waste gasification fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine to generate electric power. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The whole blade steam gas turbine combined with the high temperature water reservoir (32a) of the all blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from the dust refined fuel to generate electric power. organ. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with high-temperature water (5b) recovered from the refined dust fuel to generate electric power. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water reservoir (32a) of the full-blade steam gas turbine is supplied with supercritical pressure high-temperature water (5b) recovered from the refined refuse fuel to generate electric power, and the full-blade steam gas turbine is characterized in that Combined organization. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5b) recovered from the refined refuse fuel to generate electric power. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from all the fuels to be burned to generate electric power. Combined organization. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with high-temperature water (5b) recovered from all the fuel that burns to generate electric power. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical pressure high-temperature water (5b) recovered from all the fuel that burns to generate electric power, and is used as electric power. Turbine coalescence engine. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にすることを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5b) heat-recovered from all the fuel that burns to generate electric power. . 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  Supercritical pressure hot water (5b) recovered from pulverized coal fuel is supplied to the high temperature water reservoir (32a) of the full blade steam turbine, and the combustion gas is compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the combustor and heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombusting in the heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is compressed by the full blade compressor as electric power. And an all-blade steam gas turbine combined engine characterized by recombusting in the combustor and heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the cum heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with supercritical high temperature water (5b) recovered from the waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the combustor and heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombusting in the heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is compressed by the full blade compressor as electric power. And an all-blade steam gas turbine combined engine characterized by recombusting in the combustor and heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam gas turbine is supplied with high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the cum heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is compressed by the full blade compressor as electric power. And an all-blade steam gas turbine combined engine characterized by recombusting in the combustor and heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the cum heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by the full blade compressor as electric power. And recombusting in the combustor and heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5b) recovered from the dust refined fuel, and the combustion gas is compressed by the full blade compressor and burned as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by the full blade compressor as electric power. And recombusting in the combustor and heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is compressed by the full blade compressor and burned as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also converted into electric power by the full blade compressor. An all-blade steam gas turbine combined engine, which is compressed and recombusted in the combustor and heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all rotor blade steam gas turbine is supplied with high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized by recombustion in the combustor and heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  Supercritical pressure hot water (5b) recovered from pulverized coal fuel is supplied to the high temperature water reservoir (32a) of the full blade steam turbine, and the combustion gas is compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that the combustion heat and heat exchanger 4 recovers recombustion heat for normal use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that reheated heat is recovered by a heat exchanger 4 and is normally used. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that it is re-heated by the combustor and heat exchanger 4 and recovered for normal use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that the combined heat exchanger 4 recovers recombustion heat for normal use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with supercritical high temperature water (5b) recovered from the waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that the combustion heat and heat exchanger 4 recovers recombustion heat for normal use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that reheated heat is recovered by a heat exchanger 4 and is normally used. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that it is re-heated by the combustor and heat exchanger 4 and recovered for normal use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam gas turbine is supplied with high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that the combined heat exchanger 4 recovers recombustion heat for normal use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that it is re-heated by the combustor and heat exchanger 4 and recovered for normal use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that the combined heat exchanger 4 recovers recombustion heat for normal use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by the full blade compressor as electric power. Then, the all-blade steam gas turbine combined engine is characterized in that the combustion heat and heat exchanger 4 recovers the heat of recombustion for normal use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5b) recovered from the dust refined fuel, and the combustion gas is compressed by the full blade compressor and burned as electric power. An all-blade steam gas turbine combined engine, which is normally used after recovering recombustion heat in the heat exchanger 4. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by the full blade compressor as electric power. Then, the all-blade steam gas turbine combined engine is characterized in that the combustion heat and heat exchanger 4 recovers the heat of recombustion for normal use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is compressed by the full blade compressor and burned as electric power. An all-blade steam gas turbine combined engine, which is normally used after recovering recombustion heat in the heat exchanger 4. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also converted into electric power by the full blade compressor. An all-blade steam gas turbine combined engine, which is compressed and recombusted by a combustor and heat exchanger 4 for normal use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して通常使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all rotor blade steam gas turbine is supplied with high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine characterized in that the combustion heat and heat exchanger 4 recovers recombustion heat for normal use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  Supercritical pressure hot water (5b) recovered from pulverized coal fuel is supplied to the high temperature water reservoir (32a) of the full blade steam turbine, and the combustion gas is compressed by the full blade compressor as electric power. An all-rotor-steam gas turbine combined engine characterized in that the combustion heat and heat exchanger 4 recovers recombustion heat for auxiliary use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine, wherein the heat is re-combusted in the heat exchanger 4 for auxiliary use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that the combustion heat is recovered by the combustor and heat exchanger 4 and used auxiliary. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、微粉炭燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with high temperature water (5b) recovered from the pulverized coal fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine, wherein the combined heat exchanger 4 recovers recombustion heat for auxiliary use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with supercritical high temperature water (5b) recovered from the waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-rotor-steam gas turbine combined engine characterized in that the combustion heat and heat exchanger 4 recovers recombustion heat for auxiliary use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-blade steam gas turbine combined engine, wherein the heat is re-combusted in the heat exchanger 4 for auxiliary use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that the combustion heat is recovered by the combustor and heat exchanger 4 and used auxiliary. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミガス化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam gas turbine is supplied with high temperature water (5b) recovered from waste gasification fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine, wherein the combined heat exchanger 4 recovers recombustion heat for auxiliary use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that the combustion heat is recovered by the combustor and heat exchanger 4 and used auxiliary. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by the full blade compressor as electric power. An all-rotor-blade steam gas turbine combined engine, wherein the combined heat exchanger 4 recovers recombustion heat for auxiliary use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from the refined garbage fuel, and the combustion gas is also compressed by the full blade compressor as electric power. Then, the all-blade steam gas turbine combined engine is characterized in that the combustion heat is recovered by the combustor and heat exchanger 4 and used auxiliary. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、ゴミ微細化燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5b) recovered from the dust refined fuel, and the combustion gas is compressed by the full blade compressor and burned as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that the combustion heat is recovered by the regenerator / heat exchanger 4 for auxiliary use. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam turbine is supplied with supercritical pressure high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by the full blade compressor as electric power. Then, the all-blade steam gas turbine combined engine is characterized in that the combustion heat is recovered by the combustor and heat exchanger 4 and used auxiliary. 前記全動翼蒸気タービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all blade steam turbine is supplied with high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is compressed by the full blade compressor and burned as electric power. An all-rotor-blade steam gas turbine combined engine characterized in that the combustion heat is recovered by the regenerator / heat exchanger 4 for auxiliary use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した超臨界圧力高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the full blade steam gas turbine is supplied with supercritical pressure high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also converted into electric power by the full blade compressor. An all-blade steam gas turbine combined engine, which is compressed and reheated by the combustor and heat exchanger 4 for auxiliary use. 前記全動翼蒸気ガスタービンの高温水溜（３２ａ）には、燃えるもの全部の燃料から熱回収した高温水（５ｂ）を供給し、電力にして該燃焼ガスも全動翼圧縮機で圧縮して燃焼器兼熱交換器４で再燃焼熱回収して補助使用することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water reservoir (32a) of the all rotor blade steam gas turbine is supplied with high temperature water (5b) recovered from all the fuel that burns, and the combustion gas is also compressed by the full blade compressor as electric power. An all-rotor-steam gas turbine combined engine characterized in that the combustion heat and heat exchanger 4 recovers recombustion heat for auxiliary use. 前記噴射推進する全動翼蒸気ガスタービンは、空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine, wherein the all-blade steam gas turbine to be propelled is propelled by increasing the mass velocity of high-temperature water and combustion gas including air suction. 前記噴射推進する全動翼蒸気タービンは、空気吸引力を含めた噴射高温水の質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine, wherein the all-blade steam turbine to be propelled is propelled by increasing the mass velocity of the injected high-temperature water including the air suction force. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ａの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine to be propelled by injection is propelled by increasing the mass velocity of high-temperature water and combustion gas including the air suction force of the spraying principle 91a, and is combined with the all-blade steam gas turbine organ. 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ａの空気吸引力を含めた噴射高温水の質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the all-blade steam turbine for propulsion is propelled by increasing the mass velocity of the injected hot water including the air suction force of the spraying principle 91a. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ａ・９１ｂの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine to be propelled is propelled by increasing the mass velocity of high-temperature water and combustion gas including the air suction force of the spraying principle 91a and 91b. Turbine coalescence engine. 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ａ・９１ｂの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam turbine for propulsion is propelled by increasing the mass velocity of high-temperature water and combustion gas including the air suction force of the spraying principle 91a and 91b. Combined organization. 前記噴射推進する全動翼蒸気ガスタービンは、空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により船体を浮上させて噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine for propelling and jetting is an all-blade steam gas turbine combined with the hull lifted and propelled by increasing the mass velocity of high-temperature water and combustion gas including air suction force organ. 前記噴射推進する全動翼蒸気タービンは、空気吸引力を含めた噴射高温水の質量速度の増大により船体を浮上させて噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that the all-blade steam turbine for propulsion is lifted and propelled by increasing the mass velocity of the injected high-temperature water including the air suction force. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ｃ・９１ｄの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine to be propelled is propelled by increasing the mass velocity of high-temperature water and combustion gas including the water suction force of the spraying principle 91c and 91d. Turbine coalescence engine. 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ｃ・９１ｄの水吸引力を含めた噴射高温水の質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the all-blade steam turbine to be propelled is propelled by increasing the mass velocity of high-temperature jet water including the water suction force of the spraying principle 91c and 91d. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ｃの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all blade vane steam gas turbine to be propelled for injection is propulsion propelled by increasing the mass velocity of high temperature water and combustion gas including the water suction force of the spraying principle 91c. organ. 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ｄの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the all-blade steam gas turbine to be propelled is propelled by increasing the mass velocity of the high-temperature water and combustion gas including the water suction force of the spraying principle 91d. . 前記噴射推進する全動翼蒸気ガスタービンは、空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine for propelling and propelling the entire rotor blade is characterized in that the propulsion and propulsion is carried out while greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the air suction force. Steam gas turbine combined engine. 前記噴射推進する全動翼蒸気タービンは、空気吸引力を含めた噴射高温水の質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined with the propulsion is propelled by significantly reducing the fuel load by increasing the mass velocity of the injected high-temperature water including the air suction force. organ. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ａの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine to be propelled for propulsion is propulsion propelled by greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the air suction force of the spraying principle 91a. An all-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ａの空気吸引力を含めた噴射高温水の質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The full moving blade steam turbine for propelling and propelling the propulsion is propelled by greatly reducing the fuel loading amount by increasing the mass velocity of the injected hot water including the air suction force of the spraying principle 91a. Wing steam gas turbine combined engine. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ａ・９１ｂの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine to be propelled for propulsion is propulsion-promoted by greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the air suction force of the spraying principle 91a and 91b. An all-blade steam gas turbine combined engine characterized by 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ａ・９１ｂの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam turbine to be propelled for injection is propelled by significantly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the air suction force of the spraying principle 91a and 91b. An all-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気ガスタービンは、空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により船体を浮上させて燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine for propelling and propelling propells the hull by increasing the mass velocity of the high-temperature water and combustion gas including air suction force, and significantly propels the fuel loading. An all-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気タービンは、空気吸引力を含めた噴射高温水の質量速度の増大により船体を浮上させて燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam turbine for propulsion is propelled by propelling the hull by increasing the mass velocity of the injected high-temperature water including the air suction force and greatly reducing the fuel load. Wing steam gas turbine combined engine. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ｃ・９１ｄの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine to be propelled for propulsion is propulsion propelled by greatly reducing the fuel loading by increasing the mass velocity of the high-temperature water and combustion gas including the water suction force of the spraying principle 91c and 91d. An all-blade steam gas turbine combined engine characterized by 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ｃ・９１ｄの水吸引力を含めた噴射高温水の質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam turbine to be propelled for propulsion is propulsion propelled by greatly reducing the fuel load by increasing the mass velocity of the high-temperature jet water including the water suction force of the spraying principle 91c / 91d. All-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ｃの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine to be propelled for propulsion is propulsion propelled by greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the water suction force of the spraying principle 91c. An all-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ｄの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam turbine to be propelled for propulsion is propulsion propelled by greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the water suction force of the spraying principle 91d. An all-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気ガスタービンは、空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine for propelling and propelling is characterized in that the fuel load is greatly reduced by increasing the mass velocity of the high-temperature water and combustion gas including air suction force, and the propulsion is propelled very safely. An all-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気タービンは、空気吸引力を含めた噴射高温水の質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam turbine for propelling and propelling the entire rotor blade is characterized in that the fuel load is greatly reduced by increasing the mass velocity of the injected high-temperature water including the air suction force, and the propulsion is propelled very safely. Steam gas turbine combined engine. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ａの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine propelled by the jet propulsion is very safe by significantly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the air suction force of the spraying principle 91a. An all-blade steam gas turbine combined engine characterized by: 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ａの空気吸引力を含めた噴射高温水の質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The above-described all blade steam turbine for propulsion is characterized in that the fuel load is greatly reduced by increasing the mass velocity of the injected hot water including the air suction force of the spraying principle 91a, and the propulsion is propelled very safely. An all-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ａ・９１ｂの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine propelled by the injection is very safe by greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the air suction of the spraying principle 91a and 91b. An all-blade steam gas turbine combined engine characterized by propelling by injection. 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ａ・９１ｂの空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam turbine propelled by the above injection is very safe by significantly reducing the fuel load by increasing the mass velocity of the injection hot water and combustion gas including the air suction force of the spraying principle 91a and 91b. An all-blade steam gas turbine combined engine characterized by propulsion. 前記噴射推進する全動翼蒸気ガスタービンは、空気吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により船体を浮上させて燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine propelled by the jet propulsion is extremely safe by levitating the hull by increasing the mass velocity of the high-temperature jet water and combustion gas including air suction and greatly reducing the fuel load. An all-blade steam gas turbine combined engine characterized by: 前記噴射推進する全動翼蒸気タービンは、空気吸引力を含めた噴射高温水の質量速度の増大により船体を浮上させて燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam turbine for propelling and propelling jets very safely by levitating the hull by increasing the mass velocity of the injected hot water including air suction and greatly reducing the fuel load. An all-blade steam gas turbine combined engine. 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ｃ・９１ｄの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine propelled by the injection is very safe by greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the water suction of the spraying principle 91c and 91d. An all-blade steam gas turbine combined engine characterized by propelling by injection. 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ｃ・９１ｄの水吸引力を含めた噴射高温水の質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all rotor blade steam turbine to be propelled for injection is capable of propelling very safely by greatly reducing the fuel load by increasing the mass velocity of the high temperature water for injection including the water suction force of the spraying principle 91c / 91d. An all-blade steam gas turbine combined engine characterized by 前記噴射推進する全動翼蒸気ガスタービンは、霧吹きの原理９１ｃの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine propelled by the jet propulsion is very safe by greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the water suction force of the spraying principle 91c. An all-blade steam gas turbine combined engine characterized by: 前記噴射推進する全動翼蒸気タービンは、霧吹きの原理９１ｄの水吸引力を含めた噴射高温水と燃焼ガスの質量速度の増大により燃料積載量を大幅に低減して非常に安全に噴射推進することを特徴とする全動翼蒸気ガスタービン合体機関。  The above-described all-blade steam turbine for propulsion and injection propulsion is extremely safe by greatly reducing the fuel load by increasing the mass velocity of the high-temperature water and combustion gas including the water suction force of the spraying principle 91d. An all-blade steam gas turbine combined engine characterized by that. 前記低温燃焼ガスに石炭灰等を含めて、出力発生の過程で全重力仕事率を増大し、出力を増大することを特徴とする電磁加熱タービン動翼（８１）を具備した全動翼蒸気ガスタービン合体機関。  All-blade steam gas provided with an electromagnetically heated turbine rotor blade (81) characterized in that coal ash or the like is included in the low-temperature combustion gas to increase the total gravitational power in the process of generating power and increase the output. Turbine coalescence engine. 前記低温燃焼ガスに石炭灰等を含めて、出力発生の過程で全重力仕事率を増大し、出力を増大することを特徴とする超臨界圧力等の高温水（５ｂ）で出力を発生する全動翼蒸気ガスタービン合体機関。  The low-temperature combustion gas includes coal ash and the like, and increases the total gravitational power in the process of generating output, thereby increasing the output. Rotor steam gas turbine combined engine. 前記電磁加熱タービン動翼（８１）に換えて撥水性タービン動翼（８７ａ）で出力を発生する全動翼蒸気ガスタービン合体機関。  An all blade steam gas turbine combined engine that generates an output by a water repellent turbine blade (87a) instead of the electromagnetically heated turbine blade (81). 前記電磁加熱タービン動翼（８１）の一部を撥水性タービン動翼（８７ａ）に換えて出力を発生することを特徴とする全動翼蒸気ガスタービン合体機関。  An all rotor blade steam gas turbine combined engine characterized in that a part of the electromagnetically heated turbine rotor blade (81) is replaced with a water-repellent turbine rotor blade (87a) to generate an output. 前記全動翼蒸気ガスタービンに於いて、燃焼ガスの一部を冷房用等別用途に使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In the full blade steam gas turbine, a part of the combustion gas is used for other purposes such as cooling, etc. 前記全動翼蒸気ガスタービンに於いて、燃焼ガスの全部を冷房用等別用途に使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine, the all-blade steam gas turbine combined engine is characterized in that the entire combustion gas is used for other purposes such as cooling. 前記全動翼蒸気ガスタービンに於いて、燃焼ガスの一部を別用途に使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In the full-blade steam gas turbine, the full-blade steam gas turbine combined engine, wherein a part of the combustion gas is used for another purpose. 前記全動翼蒸気ガスタービンに於いて、燃焼ガスの全部を別用途に使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In the all-blade steam gas turbine, the all-blade steam gas turbine combined engine is characterized in that all of the combustion gas is used for another purpose. 前記全動翼蒸気ガスタービンに於いて、燃焼ガスの全部を別用途の全動翼ガスタービンで使用することを特徴とする全動翼蒸気ガスタービン合体機関。  In the full-blade steam gas turbine, the full-blade steam gas turbine combined engine is characterized in that all of the combustion gas is used in a full-blade gas turbine of another application. 前記全動翼蒸気ガスタービンに於いて、燃焼ガスの全部を別用途の全動翼ガスタービンで使用して電力を発生することを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that in the all-blade steam gas turbine, all of the combustion gas is used in an all-blade gas turbine for another purpose to generate electric power. 前記全動翼蒸気ガスタービンに於いて、燃焼ガスの全部を別用途の全動翼ガスタービンで使用してドライアイスを製造することを特徴とする全動翼蒸気ガスタービン合体機関。  In the full moving blade steam gas turbine, an all moving blade steam gas turbine combined engine is characterized in that dry ice is produced by using all of the combustion gas in an all moving blade gas turbine of another application. 前記全動翼蒸気ガスタービンに於いて、燃焼ガスの全部を別用途の全動翼ガスタービンで使用して液体窒素を製造することを特徴とする全動翼蒸気ガスタービン合体機関。  In the full-blade steam gas turbine, the full-blade steam gas turbine combined engine is characterized in that all of the combustion gas is used in a full-blade gas turbine for another purpose to produce liquid nitrogen. 前記気化潜熱回収器６６ａに換えて空冷式気化潜熱回収器６６ｂを使用することを特徴とする全動翼蒸気ガスタービン合体機関。  An all rotor blade steam gas turbine combined engine using an air-cooled vaporization latent heat recovery unit 66b instead of the vaporization latent heat recovery unit 66a. 前記気化潜熱回収器６６ａに換えて空冷式気化潜熱回収器６６ｂを使用する自動車としたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that it is an automobile that uses an air-cooled vaporization latent heat recovery unit 66b instead of the vaporization latent heat recovery unit 66a. 前記気化潜熱回収器６６ａに換えて空冷式気化潜熱回収器６６ｂを使用する輸送用機器としたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-rotor-blade steam gas turbine combined engine characterized in that it is a transport device that uses an air-cooled vaporization latent heat recovery unit 66b instead of the vaporization latent heat recovery unit 66a. 前記気化潜熱回収器６６ａに換えて空冷式気化潜熱回収器６６ｂを使用するプロペラ飛行機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A propeller airplane using an air-cooled latent heat recovery unit 66b instead of the vaporization latent heat recovery unit 66a. 前記気化潜熱回収器６６ａに換えて空冷式気化潜熱回収器６６ｂを使用するヘリコプターとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that a helicopter using an air-cooled vaporization latent heat recovery unit 66b instead of the vaporization latent heat recovery unit 66a is used. 前記気化潜熱回収器６６ａに換えて空冷式気化潜熱回収器６６ｂを使用する飛行物体としたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that it is a flying object that uses an air-cooled latent heat recovery unit 66b instead of the vaporization latent heat recovery unit 66a. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより昇圧することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted by a water pump and counter-rotating magnetic frictional power transmission device 14a. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump and counter-rotating magnetic frictional power transmission device 14a. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより昇圧して動力を伝達することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted by a water pump and counter-rotating magnetic frictional power transmission device 14a to transmit power, and is an all-blade steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧して動力を伝達することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump and counter-rotating magnetic frictional power transmission device 14a to transmit power, and is an all blade turbine steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより昇圧して超臨界温度等複数温度にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted by a water pump and counter-rotating magnetic frictional power transmission device 14a so as to have a plurality of temperatures such as a supercritical temperature. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump and counter-rotating magnetic frictional power transmission device 14a so as to have a plurality of temperatures such as a supercritical temperature. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより昇圧して超臨界温度等複数温度にして動力を伝達することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted by a water pump and counter-rotating magnetic frictional power transmission device 14a so as to transmit power at a plurality of temperatures such as a supercritical temperature, and transmits the power. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is a full-rotor-steam gas turbine characterized in that the water is pumped to a supercritical pressure or the like by a water pump and counter-rotating magnetic frictional power transmission device 14a to transmit the power to a plurality of temperatures such as a supercritical temperature. Combined organization. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump and counter-rotating magnetic frictional power transmission device 14a to transmit the power to a plurality of temperatures such as a supercritical temperature to obtain the double rotational speed of the existing technology. An all-blade steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の３倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump and counter-rotating magnetic friction power transmission device 14a to transmit the power to a plurality of temperatures such as a supercritical temperature, and the power is increased to three times the number of existing technologies. An all-blade steam gas turbine combined engine characterized by 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の５倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump and counter-rotating magnetic frictional power transmission device 14a to transmit the power to a plurality of temperatures such as a supercritical temperature, and the power is increased to 5 times that of the existing technology. An all-blade steam gas turbine combined engine characterized by 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の８倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump and counter-rotating magnetic frictional power transmission device 14a to transmit the power to a plurality of temperatures such as a supercritical temperature, so that the number of revolutions is 8 times that of the existing technology. An all-blade steam gas turbine combined engine characterized by 前記高温水５ｂは、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の１０倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump and counter-rotating magnetic frictional power transmission device 14a and transmitted to a plurality of temperatures such as a supercritical temperature to transmit the power to 10 times the number of revolutions of the existing technology. An all-blade steam gas turbine combined engine characterized by 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより昇圧することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted by a water pump / magnetic frictional power transmission device 100a. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより昇圧して動力を伝達することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted by a water pump / magnetic frictional power transmission device 100a to transmit power, and is an all-blade steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧して動力を伝達することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a to transmit power, and is an all-bladed steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより昇圧して超臨界温度等複数温度にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted by a water pump / magnetic friction power transmission device 100a so as to have a plurality of temperatures such as a supercritical temperature. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a so as to have a plurality of temperatures such as a supercritical temperature. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより昇圧して超臨界温度等複数温度にして動力を伝達することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted by a water pump / magnetic frictional power transmission device 100a and is transmitted to a plurality of temperatures such as a supercritical temperature to transmit power. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a and is transmitted to a plurality of temperatures such as a supercritical temperature to transmit power. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の２倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a and transmitted to a plurality of temperatures such as a supercritical temperature, and the power is transmitted to twice the rotational speed of the existing technology. An all-blade steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の３倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a and transmitted to a plurality of temperatures such as a supercritical temperature to transmit power to a triple rotational speed of the existing technology. An all-blade steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の５倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a and transmitted to a plurality of temperatures such as a supercritical temperature to transmit power to a fivefold rotational speed of the existing technology. An all-blade steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の８倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a and transmitted to a plurality of temperatures such as a supercritical temperature to transmit power to an eight times rotational speed of the existing technology. An all-blade steam gas turbine combined engine. 前記高温水５ｂは、送水ポンプ兼磁気摩擦動力伝達装置１００ａにより超臨界圧力等に昇圧して超臨界温度等複数温度にして動力を伝達し、既存技術の１０倍回転数にすることを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b is boosted to a supercritical pressure or the like by a water pump / magnetic frictional power transmission device 100a and transmitted to a plurality of temperatures such as a supercritical temperature to transmit power to a tenfold rotational speed of the existing technology. An all-blade steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is mixed with the high-temperature water 5b having the highest temperature arranged at the center. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is mixed with the high-temperature water 5b having the highest temperature such as the supercritical temperature at the center and mixed. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して１以上複数温度の高温水と混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is mixed with one or more high-temperature waters at one or more temperatures. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して１以上複数温度の高温水と混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high temperature water 5b having the highest temperature such as the supercritical temperature and mixed with one or more high temperature waters. Combined organization. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して９０度前後で合流混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high-temperature water 5b having the highest temperature, and is mixed and mixed at about 90 degrees. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して９０度前後で合流混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is mixed at about 90 degrees with the high-temperature water 5b having the highest temperature such as the supercritical temperature at the center. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して１以上複数温度の高温水と９０度前後で合流混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b having a plurality of temperatures such as the supercritical temperature has the highest temperature high temperature water 5b in the center and is mixed and mixed with one or more high temperature waters at around 90 degrees. Turbine coalescence engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して１以上複数温度の高温水と９０度前後で合流混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged such that the high temperature water 5b having the highest temperature such as the supercritical temperature is arranged at the center and mixed with one or more high temperature waters at about 90 degrees. Rotor steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して霧吹きの原理で合流混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is mixed at the center with the high-temperature water 5b having the highest temperature and being sprayed and mixed. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して霧吹きの原理で合流混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine characterized in that the high-temperature water 5b having a plurality of temperatures such as supercritical temperature is mixed and mixed on the principle of spraying by placing the high-temperature water 5b having the highest temperature such as supercritical temperature at the center. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して１以上複数温度の高温水と霧吹きの原理で合流混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b having a plurality of temperatures such as the supercritical temperature is formed by arranging the high temperature water 5b having the highest temperature in the center and mixing and mixing one or more high temperature waters and the high temperature water by the principle of spraying. Turbine coalescence engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して１以上複数温度の高温水と霧吹きの原理で合流混合することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is centered on the high-temperature water 5b having the highest temperature such as the supercritical temperature and is mixed and mixed with one or more high-temperature waters having a plurality of temperatures on the principle of spraying. Rotor steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して９０度前後で合流混合して高温水を加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high-temperature water 5b having the highest temperature, and is merged and mixed at about 90 degrees to accelerate the high-temperature water. organ. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して９０度前後で合流混合して高温水を加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high temperature water 5b having the highest temperature such as the supercritical temperature, and the high temperature water is accelerated by merging and mixing at around 90 degrees. Steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して１以上複数温度の高温水と９０度前後で合流混合して高温水を加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is characterized by accelerating the high-temperature water by arranging the high-temperature water 5b having the highest temperature in the center and mixing and mixing with one or more high-temperature waters at around 90 degrees. An all-blade steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して１以上複数温度の高温水と９０度前後で合流混合して高温水を加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high-temperature water 5b having the highest temperature such as a supercritical temperature, and is merged and mixed with one or more high-temperature waters at around 90 degrees to accelerate the high-temperature water. An all-blade steam gas turbine combined engine characterized by that. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して霧吹きの原理で合流混合して高温水を加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high temperature water 5b having the highest temperature, and is joined and mixed on the principle of spraying to accelerate the high temperature water. organ. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して霧吹きの原理で合流混合して高温水を加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged in such a manner that the high temperature water 5b having the highest temperature such as the supercritical temperature is arranged at the center, and the high temperature water is accelerated by merging and mixing on the principle of spraying. Steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して１以上複数温度の高温水と霧吹きの原理で合流混合して高温水を加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is characterized in that the high-temperature water 5b having the highest temperature is arranged at the center, and the high-temperature water is accelerated by merging and mixing with one or more high-temperature waters on the principle of spraying. An all-blade steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して１以上複数温度の高温水と霧吹きの原理で合流混合して高温水を加速することを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high-temperature water 5b having the highest temperature such as the supercritical temperature, and the high-temperature water is accelerated by merging and mixing with one or more high-temperature waters on the principle of spraying. An all-blade steam gas turbine combined engine characterized by that. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して９０度前後で合流混合して高温水を加速する高温水噴射ノズル５９ｂとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is a high-temperature water injection nozzle 59b in which the high-temperature water 5b having the highest temperature is arranged at the center and merged and mixed at around 90 degrees to accelerate the high-temperature water. All-blade steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して９０度前後で合流混合して高温水を加速する高温水噴射ノズル５９ｂとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is a high-temperature water injection nozzle 59b in which the high-temperature water 5b having the highest temperature such as the supercritical temperature is arranged at the center and merged and mixed at around 90 degrees to accelerate the high-temperature water. An all-blade steam gas turbine combined engine characterized by 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して１以上複数温度の高温水と９０度前後で合流混合して高温水を加速する高温水噴射ノズル５９ｂとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is a high-temperature water injection nozzle that accelerates the high-temperature water by arranging the high-temperature water 5b having the highest temperature at the center and merging and mixing with one or more high-temperature water at about 90 degrees. An all-blade steam gas turbine combined engine characterized by being 59b. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して１以上複数温度の高温水と９０度前後で合流混合して高温水を加速する高温水噴射ノズル５９ｂとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high-temperature water 5b having the highest temperature such as a supercritical temperature, and is merged and mixed with one or more high-temperature waters at around 90 degrees to accelerate the high-temperature water. An all-blade steam gas turbine combined engine characterized by a high-temperature water injection nozzle 59b. 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して霧吹きの原理で合流混合して高温水を加速する高温水噴射ノズル５９ｂとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is a high-temperature water injection nozzle 59b in which the high-temperature water 5b having the highest temperature is arranged at the center and merged and mixed by the spraying principle to accelerate the high-temperature water. All-blade steam gas turbine combined engine. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して霧吹きの原理で合流混合して高温水を加速する高温水噴射ノズル５９ｂとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is a high-temperature water injection nozzle 59b in which the high-temperature water 5b having the highest temperature such as the supercritical temperature is arranged at the center and merged and mixed by the spraying principle to accelerate the high-temperature water. An all-blade steam gas turbine combined engine characterized by 前記超臨界温度等複数温度の高温水５ｂは、中心に最高温度の高温水５ｂを配置して１以上複数温度の高温水と霧吹きの原理で合流混合して高温水を加速する高温水噴射ノズル５９ｂとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The high temperature water 5b having a plurality of temperatures such as the supercritical temperature is a high temperature water injection nozzle that arranges the high temperature water 5b having the highest temperature at the center and merges and mixes the high temperature water with one or more temperatures on the principle of spraying to accelerate the high temperature water. An all-blade steam gas turbine combined engine characterized by being 59b. 前記超臨界温度等複数温度の高温水５ｂは、中心に超臨界温度等最高温度の高温水５ｂを配置して１以上複数温度の高温水と霧吹きの原理で合流混合して高温水を加速する高温水噴射ノズル５９ｂとしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The high-temperature water 5b having a plurality of temperatures such as the supercritical temperature is arranged at the center with the high-temperature water 5b having the highest temperature such as the supercritical temperature, and the high-temperature water is accelerated by merging and mixing with one or more high-temperature waters on the principle of spraying. An all-blade steam gas turbine combined engine characterized by a high-temperature water injection nozzle 59b. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービンの、何れか１以上の出力で駆動する装置を、大中小各種発電設備としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas characterized in that the apparatus for driving at any one or more of the full-blade gas turbine, the full-blade steam turbine, and the full-blade steam gas turbine is a large, medium and small power generation facility. Turbine coalescence engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービンの、何れか１以上の出力で駆動する装置を、大中小各種熱と電気と冷熱の供給設備としたことを特徴とする全動翼蒸気ガスタービン合体機関。  The apparatus driven by any one or more of the all-blade gas turbine, all-blade steam turbine, and all-blade steam gas turbine is a supply facility for large, medium and small heat, electricity and cold. An all-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービンの何れか１以上の出力で駆動する装置を、大中小各種熱と電気の供給設備としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device for driving at least one of the all-blade gas turbine, all-blade steam turbine, and all-blade steam gas turbine is a large-, medium-, and small-scale heat and electricity supply facility. Wing steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種船舶としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device driven by one or more outputs of the full blade gas turbine, the full blade steam turbine, the full blade steam gas turbine, the special device, and the water injection device is a large / medium / small vessel. All-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種航空機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device that is driven by one or more outputs of the full blade gas turbine, the full blade steam turbine, the full blade steam gas turbine, the special device, and the water injection device is a variety of large, medium, and small aircrafts. All-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種超音速飛行機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device driven by one or more outputs of the all blade gas turbine, all blade steam turbine, all blade steam gas turbine, special device and water injection device is a supersonic airplane of various types of large, medium and small. An all-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種宇宙往還親飛行機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  The large-, medium-, and small-sized space-return parent airplanes are the devices that are driven by one or more outputs of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device. An all-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種車両としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device driven by one or more outputs of the all blade gas turbine, all blade steam turbine, all blade steam gas turbine, special device, and water injection device is a large, medium and small vehicle. All-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種自動車としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device driven by one or more outputs of the full blade gas turbine, the full blade steam turbine, the full blade steam gas turbine, the special device, and the water injection device is a large / medium / small vehicle. All-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種機械としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device driven by one or more outputs of the full blade gas turbine, the full blade steam turbine, the full blade steam gas turbine, the special device, and the water injection device is a variety of large, medium, and small machines. All-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種艦船としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device driven by one or more outputs of the all blade gas turbine, all blade steam turbine, all blade steam gas turbine, special device and water injection device is a large, medium and small ship. All-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種戦車としたことを特徴とする全動翼蒸気ガスタービン合体機関。  The large-, medium-, and small-sized tanks are the devices that are driven by any one or more of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device. All-blade steam gas turbine combined engine. 前記全動翼ガスタービン及び全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種戦闘機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A device driven by one or more outputs of the all blade gas turbine, all blade steam turbine, all blade steam gas turbine, special device, and water injection device is a large, medium and small fighter. An all-blade steam gas turbine combined engine. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種発電設備としたことを特徴とする全動翼蒸気ガスタービン合体機関。  The whole blade steam gas characterized in that the device driven by one or more outputs of the whole blade steam turbine, the whole blade steam gas turbine, the special device, and the water injection device is a large, medium and small power generation facility. Turbine coalescence engine. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービンの何れか１以上の出力で駆動する装置を、大中小各種熱と電気と冷熱の供給設備としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that a device driven by one or more outputs of the full-blade steam turbine and the full-blade steam gas turbine is a facility for supplying various types of heat, electricity and cold. Combined organization. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービンの何れか１以上の出力で駆動する装置を、大中小各種熱と電気の供給設備としたことを特徴とする全動翼蒸気ガスタービン合体機関。  An all-blade steam gas turbine combined engine characterized in that a device driven by one or more outputs of the all-blade steam turbine and the all-blade steam gas turbine is a heat and electricity supply facility for large, medium and small. . 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種船舶としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device driven by one or more outputs are large, medium, and small vessels. Combined organization. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種航空機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that the all-blade steam gas turbine, the full-blade steam gas turbine, the special device, and the water injection device are driven by any one or more outputs of various large, medium and small aircrafts. Combined organization. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種車両としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that a device driven by one or more outputs of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a vehicle of large, medium, and small sizes. Combined organization. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種自動車としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that a device driven by any one or more outputs of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a variety of large, medium, and small-sized automobiles. Combined organization. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種機械としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that the whole-blade steam turbine, the full-blade steam gas turbine, the special device, and the water jet device driven by one or more outputs are large, medium, and small machines. Combined organization. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種艦船としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that a device driven by one or more outputs of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a large / medium / small ship. Combined organization. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種戦車としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas turbine characterized in that a device driven by one or more outputs of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a large, medium, and small tank. Combined organization. 前記全動翼蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置及び水噴射装置の何れか１以上の出力で駆動する装置を、大中小各種戦闘機としたことを特徴とする全動翼蒸気ガスタービン合体機関。  A full-blade steam gas characterized in that a device driven by one or more outputs of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a large, medium, and small fighter. Turbine coalescence engine. 前記全動翼蒸気ガスタービン合体機関で燃焼させる燃料は、ガソリン・天然ガス・プロパンガス・アルコール・メタノール・メタン・水素・軽油・重油・微粉炭・ゴミガス化燃料・ゴミ微細化燃料・可燃物の内、何れか１種類にしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The fuel to be burned in the all-blade steam gas turbine combined engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil, heavy oil, pulverized coal, dust gasification fuel, dust refinement fuel, combustible material, etc. An all-blade steam gas turbine combined engine characterized in that any one of them is used. 前記全動翼蒸気ガスタービン合体機関で燃焼させる燃料は、ガソリン・天然ガス・プロパンガス・アルコール・メタノール・メタン・水素・軽油・重油・微粉炭・ゴミガス化燃料・ゴミ微細化燃料・可燃物の内、何れか２種類にしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The fuel to be burned in the all-blade steam gas turbine combined engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil, heavy oil, pulverized coal, dust gasification fuel, dust refinement fuel, combustible material, etc. An all-blade steam gas turbine combined engine characterized in that any two of them are used. 前記全動翼蒸気ガスタービン合体機関で燃焼させる燃料は、ガソリン・天然ガス・プロパンガス・アルコール・メタノール・メタン・水素・軽油・重油・微粉炭・ゴミガス化燃料・ゴミ微細化燃料・可燃物の内、何れか３種類以上にしたことを特徴とする全動翼蒸気ガスタービン合体機関。  The fuel to be burned in the all-blade steam gas turbine combined engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil, heavy oil, pulverized coal, dust gasification fuel, dust refinement fuel, combustible material, etc. Of these, all of the three or more types are combined with a moving blade steam gas turbine. 前記全動翼蒸気ガスタービン合体機関で燃焼させる燃料は、その種類を問わないことを特徴とする全動翼蒸気ガスタービン合体機関。  The fuel to be burned in the all-blade steam gas turbine combined engine is not limited to any kind, and the all-blade steam gas turbine combined engine is characterized in that 前記全動翼蒸気ガスタービン合体機関の出力で駆動する装置の種類を問わないことを特徴とする全動翼蒸気ガスタービン合体機関。  The all-blade steam gas turbine combined engine is not limited to any kind of device driven by the output of the all-blade steam gas turbine combined engine.
JP2003073042A 2003-01-09 2003-03-18 Various full rotor blade steam gas turbine combined engine Pending JP2005113683A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10605203B2 (en) 2014-09-25 2020-03-31 Patched Conics, LLC. Device, system, and method for pressurizing and supplying fluid

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10605203B2 (en) 2014-09-25 2020-03-31 Patched Conics, LLC. Device, system, and method for pressurizing and supplying fluid

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