JP2004100678A

JP2004100678A - Various full rotor blade steam gas turbine combined engine

Info

Publication number: JP2004100678A
Application number: JP2002349544A
Authority: JP
Inventors: Hiroyasu Tanigawa; 谷川　浩保
Original assignee: Individual
Current assignee: Individual
Priority date: 2002-01-22
Filing date: 2002-12-02
Publication date: 2004-04-02

Abstract

<P>PROBLEM TO BE SOLVED: To provide an various full rotor blade steam turbine combined engine in which a gas turbine exhaust temperature is approached -273°C, moisture is coagulated on a low temperature combustion gas as a nucleus, for differential recovery, combustion gas exhaust, such as CO<SB>2</SB>, etc. is approached zero, and which prevents a global warming from occurring at an electric rate of, for example, 1/10 as small as an ordinary rate. <P>SOLUTION: This various full rotor blade steam turbine combined engine high-pressure combustion heat exchanges without limit by a combustor-cum-heat exchanger of the engine, makes the combustion gas exhaust temperature approach -273°C, and recovers substantially all heat quantity of compressed air of -273°C or higher so that the heat recycling quantity of about twice as large as an existing boiler is set. The step of (amount of combustion gas heat quantity power generation)+(combustion gas mass power generation)=(an increase in the amount of 240-580 times as much as hypothetical power generation of the existing gas turbine) is performed by an electromagnetic heating turbine blade which is annularly cast at each step-down. A frictional loss between high temperature waters, such as 1,700 times as many gravity power as this is remarkably reduced, the structure is simplified and heat consumption is minimized, the moisture is coagulated with the low temperature combustion gas as the nucleus, differentiated as water droplets, and the combustion gas exhaust such as CO<SB>2</SB>, etc. is approached 0. <P>COPYRIGHT: (C)2004,JPO

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、重力パワーが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するのに加えて、超臨界圧力等に落差を増大しても、１００００００回転等は不可能なため、動翼の１０倍乃至２０倍前後も速度エネルギを消費し、回転仕事を全くしない静翼を１／２も設け、断熱膨張で騙して実は、ボイラで加熱した熱量全部で海水温度を上昇して、地球温暖化を加速する等、仮説出力を１／５００等に低減する無茶苦茶をしております。
【０００２】
そこで再熱を逆転して燃焼器兼熱交換器４により、超臨界圧力等の高温水回収熱量を最大にし、主として加熱高温手段１０１により加熱高温とした、高温水噴射ノズル５９ａより摩擦損失最少で高温水を噴射し、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、ノズル外では高温水を散弾ロケットのように加速して、気化潜熱を最適利用することで、大気圧重力パワーを最先端再熱蒸気タービンの１７００倍とし、重力仕事率を１７００倍に近付けることで、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、静翼で堰き止める無茶苦茶を全廃し、合理的な動翼面積の設計が可能な、全動翼蒸気タービン等とする技術に関する。
【０００３】
再熱蒸気タービンの復水器真空まで断熱膨張も逆転して、大気圧以下用途に合わせた断熱膨張の全動翼蒸気タービンにすることで、気化潜熱回収器（６６ａ）を設けて、１００℃以下の気化潜熱を含めて回収熱量を最大にし、１００℃に近い回収熱量と凝縮水全部を、燃焼器兼熱交換器４により、超臨界圧力等の高温水として、膨大な気化潜熱を繰返し使用することで、燃料燃焼質量を大幅に低減が可能な全動翼蒸気ガスタービン乃至、全動翼ガスタービンにして、膨大な冷熱の供給を可能にすると共に、膨大な温熱の供給が可能な全動翼蒸気タービンにより、海水温度の上昇を皆無にする技術に関する。
【０００４】
最先端ガスタービンも熱量を殆ど利用しない容積利用のため、燃焼ガスタービン入口温度の上昇を必須として、タービン耐熱限界温度の上昇により、落差の上昇が不可能なのに加えて、燃焼ガス質量の速度エネルギを回転力に変換する構成も、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も設けて損失を増大し、更に熱量が利用されないまま５００℃前後で排気され、出力を１／１００〜１／５００に低減して大損失です。
【０００５】
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兼熱交換器４とし、限り無く高圧燃焼熱交換冷却燃焼させて熱回収量を最大にすることで、静翼を逆転して全廃した全動翼ガスタービンの、燃焼ガスタービン入口温度を逆転最低として、該排気温度を−２７３℃に近付け（−温度略全部を含める）、圧縮した空気の保有熱量全部を含めて、既存ボイラの２倍前後の回収熱量や、気化潜熱回収器（６６ａ）の無限大に近い回収熱量を含めて、超臨界圧力等の高温水にする技術に関する。
【０００６】
例えば超臨界圧力等の高温水を、全動翼ガスタービンの最上流に供給して、加熱して高温として摩擦損失を最少とした、高温水噴射ノズル５９ａより高温水を噴射して、気化爆発エネルギにより水滴を弾丸やロケットのように加速して、全動翼ガスタービンを駆動し、中流最適段に低温燃焼ガスを供給して、断熱膨張復水器真空まで出力発生の過程で、極低温燃焼ガス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気化熱の冷却損失を最少とし、ＣＯ２等の燃焼ガス排気を０として、膨大な冷熱を回収する技術に関する。
【０００７】
そして燃料熱量の消費を０以下等として、超臨界圧力高温水等を含めた全動翼ガスタービンを駆動の過程で、全動翼により同一質量の燃焼ガスと高温水を略直線蛇行的に噴射して、機械効率を１０倍〜２０倍に上昇することで（既存ガスタービンの５倍落差×２倍質量×１０倍〜２０倍機械効率）＝（既存ガスタービンの１００倍〜２００倍仮説出力）＝（燃焼ガス質量＋高温水気化爆発力の出力）とし、最少の高温水を含めることで復水器真空まで膨張を可能にし、全動翼ガスタービン燃焼ガス質量出力の熱効率を無限上昇させ、熱力学により２０世紀中大停滞していた科学技術を、蘇えらせる技術に関する。
【０００８】
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、超臨界圧力等の高温水とし、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５ａを夫々の高温水溜３２ａ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５９ａより、高温水との間に気化膜を設けて摩擦損失最少で噴射し、気化爆発エネルギによりノズル内では弾丸のように高温水を加速し、ノズル外では高温水５ａをロケットのように加速して、重力パワーが最先端再熱蒸気タービンの大気圧１７００倍や、真空部１００００倍の重力仕事率に近付ける技術に関する。
【０００９】
高温水質量の気化爆発速度エネルギに変換して、全重力パワーを１００倍や、２００倍乃至５００倍に増大して出力を発生します。出力を発生の過程では、夫々の高温水噴射ノズル５９ａや電磁加熱噴口８３を含む、電磁加熱タービン翼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復水器真空まで膨張させて、機械効率を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）＝（４０倍〜１００倍質量重力パワー×５倍落差×２倍回収熱量質量×２０倍機械効率／４０）＝（既存ガスタービンの２００〜５００倍仮説発電量）等にする技術に関する。
【００１０】
本発明は全動翼タービン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・消費熱量最少・重力パワー最大で大気圧まで出力を発生して、構造が大幅に小型簡単な例えば輸送機器用としての、各種全動翼蒸気ガスタービン合体機関の、超臨界圧力高温水出力を、（同一燃料量既存ガスタービンの大気圧２０倍質量重力パワー×５倍落差×２倍回収熱量×１０倍〜２０倍機械効率／２０）＝（既存ガスタービンの１００倍〜２００倍仮説出力）等にする技術に関する。
【００１１】
本発明は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にすることで、撥水性水冷却翼８７と水等との間の摩擦損失を低減して、全動翼により略直線蛇行的に空気圧縮して、摩擦損失最小で空気を水冷却して圧縮し、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技術に関する。
【００１２】
そして燃焼ガスは冷却する程単位重力パワーが増大して、小型大出力に出来るため、各種全動翼蒸気ガスタービンの、燃焼器兼熱交換器４により限りなく高圧燃焼熱交換し、タービン燃焼ガス入口温度を最低とし、出力発生の過程でも燃焼ガスを高温水に合流して冷却し、断熱膨張極低温燃焼ガスに移行し、極低温燃焼ガスを核に水分を凝集して、氷の被覆をして燃焼ガス排気温度を−２７３℃に近付け、復水器真空まで膨張させるガスタービン技術に関する。
【００１３】
各種全動翼蒸気ガスタービンの、燃焼器兼熱交換器４により限りなく高圧燃焼熱交換し、圧縮空気保有熱量全部を含め、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圧力高温水として、各種全動翼蒸気ガスタービン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圧力を上昇し、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した技術に関する。
【００１４】
本発明は、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倍前後回収熱量の超臨界圧力高温水出力を、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倍〜２０倍機械効率＋１００〜２００倍出力）＝（１２０〜２４０倍仮説出力）として、大気圧で使用の全動翼蒸気ガスタービンを駆動する技術に関する。
【００１５】
回転出力輸送機器の自動車等の出力発生は、超臨界圧力等の高温水５ａ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、高温水噴射ノズル５９ａより高温水を噴射して、高温水との間に気化膜を設けて摩擦損失を最少とし、気化爆発エネルギによりノズル内では高温水を弾丸のように加速し、ノズル外では高温水をロケットのように加速して、電磁加熱高温とした全動翼を略直線蛇行的に加速噴射高温水駆動し、全動翼との間に気化膜を設けて摩擦損失最少で出力を発生し、最適中流段に低温燃焼ガスを供給して、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、低温燃焼ガスを核に水分を凝集して雹や水滴等とし、回転出力輸送機器でＣＯ２等の燃焼ガス排気を０に近付ける技術に関する。
【００１６】
回転出力輸送機器用等は、ＣＯ２等燃焼ガス排気を０として１２０倍や２４０倍出力等とする、極低温燃焼ガス被覆用の雹や水滴を最大にするため、全出力を全動翼蒸気ガスタービン回転出力として使用します。用途により送水する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、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、低温ＣＯ２等燃焼ガスを核に２０倍質量等の水分を凝集し、水滴等としてＣＯ２等燃焼ガス排気を０に近付けます。そして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、用途により中核技術として、全ての全動翼蒸気ガスタービン合体機関に含めて、水質量にＣＯ２等を溶解して排水する技術に関する。
【００１７】
噴射推進出力輸送機器用等としては、ＣＯ２等の燃焼ガス排気を０として、１２０倍や２４０倍仮説出力等とするため、燃焼器兼熱交換器により高圧燃焼熱交換して最大の熱回収量とし、熱回収した超臨界圧力等の高温水の一部で、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。残りの高温水の一部及び燃焼ガス全部を、夫々の霧吹きの原理９１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等に適宜に貯蔵して最適利用し、適宜に使用する噴射推進出力の各種輸送機器等として使用する技術に関する。
【００１８】
燃焼ガス全部をバイパス噴射推進する船舶等では、断熱膨張極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、更に酸素等の空気を吸引して供給し、水域を活性化して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。
【００１９】
【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、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１／１００や１／５００等に低減して、燃料電池の出力に近付き大損失です。
【００２０】
既存蒸気タービンも偶々出力を発生したものの改良で、超臨界圧力過熱蒸気を使用しても、熱量を全く利用しない容積利用のため、断熱膨張復水器真空では１００００倍以上に膨張し、単位重力パワーが１／１００００に低減し、同一出力に１００００倍の動翼面積が必要です。膨大な蒸気速度も全く利用不可のため、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１／１００や１／５００等に低減して、風力発電や燃料電池に発電原価が近付き、膨大な熱需要があるのに、ボイラで加熱した全熱量を断熱膨張し、全熱量で海水温度等を上昇して地球温暖化を加速し、ＣＯ２等をボイラから排気して大損失です。
【００２１】
又、先の出願としてガスタービン燃焼器を改良した、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号があります。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、限りなく燃焼熱交換して、燃焼ガス入り口温度を低下させることにより、燃焼ガス熱量と燃焼ガス質量を、別々に使用可能とし、過熱蒸気や燃焼ガスを水噴射冷却して、大気圧重力パワー１７００倍の凝縮水を最適最大とするものです。
【００２２】
【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、重力パワーが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、設計不可能な動翼面積や大蒸気速度のため、膨大な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、無茶苦茶な設計となります。更に問題なのは膨大な温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、断熱膨張させて回収熱量全部で海水温度を上昇して地球温暖化を加速し、発電量を１／１００や１／５００に低減して大損失していることです。
【００２３】
そこで既存ガスタービン燃焼器を燃焼器兼熱交換器４として、超臨界圧力等の高温水とした回収熱量を最大とし、超臨界圧力等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のように加速し、ノズル外では散弾ロケットのように高温水を加速して、大気圧単位容積の重力パワーを１７００倍に増大して出力を発生させます。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パワーを増大した出力発生とし、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や海水を使用し、通常は１００℃乃至５０℃前後の給水３や凝縮水として回収し、燃焼器兼熱交換器４に供給して同一熱量を繰り返し使用し、残りの膨大な温熱を需要家に供給し、可能な限り温熱の有効利用を拡大し、地球温暖化防止することを目的とします。
【００２４】
気化潜熱回収器６６ａにより同一熱量を繰返し熱回収して、燃焼器兼熱交換器４に供給して燃料燃焼質量を大幅に低減し、熱回収して得た超臨界圧力等の高温水５ａを、全動翼蒸気タービンの最上流の高温水溜３２ａに供給し、加熱高温手段１０１により加熱高温とした高温水噴射ノズル５９ａより、高温水との間に気化膜を設けて摩擦損失を最少とし、高温水の気化爆発力を利用して、ノズル内では機関銃の弾丸のように加速し、ノズル外では散弾ロケットのように高温水を加速して、落差や重力パワーを最大に近付けた出力発生とし、既存ガスタービンの５００倍仮設出力等に上昇させることを目的とします。
【００２５】
熱回収して回収熱量を繰返し再々使用する熱量が不明のため、計算を復水器真空まで使用する計算とし、単位容積重力パワーが、既存蒸気タービンの終段１００００倍重力パワーを、２０倍〜５０倍重力パワーに大幅に低減した計算で、高温水での仮説発電量を（既存ガスタービンの２倍回収熱量質量×２０倍〜５０倍質量重力パワー×５倍落差×１０〜２０倍機械効率／１０〜２０）＝（既存ガスタービンの２００倍〜５００倍仮説発電量）に上昇を目的とします。
【００２６】
そして最終段復水器真空での動翼面積の一部〜大部分を、１／１００００に縮小して、動翼面積を設計可能な動翼面積とします。そして電磁加熱高温とした、電磁加熱外側タービン動翼群及び電磁加熱内側タービン動翼群を具備した、全動翼蒸気タービンにより、略直線蛇行的に高温水５ａを噴射して、電磁加熱タービン動翼と水との間に気化膜を設けて、摩擦損失最少で出力を発生し、同一燃料消費量で２００倍乃至５００倍仮説発電量等に上昇することを目的とする。
【００２７】
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では、タービン入り口温度の上昇を必須とし、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、材料費の増大損失も膨大となり、排気温度が５００℃前後と非常に高く、単位動翼面積の重力仕事率が大幅に低減して、動翼面積の大幅な増大を必要とするため、膨大な静翼を設けて多段に堰き止めて風向きを反転させ、実用燃焼ガス速度に減速する無茶苦茶設計となり、熱量が全く利用出来ないため、出力が１／２００乃至１／５００の燃料電池や風力発電並出力に低減し、ＣＯ２等を排気して地球温暖化の加速も膨大となり大損失です。
【００２８】
そこで教育テレビで放映のように、熱量をより大きな（大落差×単位容積大質量重力仕事率）に変換して、仕事量を大幅に増大するため、既存ガスタービン燃焼器を燃焼器兼熱交換器として、限りなく高圧燃焼熱交換して、排気温度を−２７３℃に限り無く近付けて、低温燃焼ガスを核に水分を凝集し、５０倍質量等の水に燃焼ガスを溶解して排水し、ＣＯ２等の排気を０に近付けることを目的とします。
【００２９】
そして圧縮空気保有熱量−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、超臨界圧力等の高温水熱回収量として、全動翼蒸気タービン及び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、同一燃焼ガス質量×２倍落差×１０〜２０倍機械効率等の燃焼ガス出力を含めて、既存ガスタービンの５００倍仮説発電量等にし、地球温暖化防止することを目的とする。
【００３０】
【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、仮説数字で説明しますが、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、単位容積重力パワーが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です。
【００３１】
即ち実現不可能な動翼面積のため再熱を逆転して、超臨界圧力等の高温水の気化爆発エネルギにより出力を発生し、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て砲身状とした、高温水噴射ノズル５９ａより高温水の気化爆発力を利用して、ノズル内では機関銃の弾丸のように高温水を加速し、ノズル外では散弾ロケットのように高温水を加速して（既存ガスタービンの５倍落差×２倍回収熱量質量×２０倍〜５０倍質量重力パワー×１０〜２０倍機械効率／１０〜２０）＝（２００倍〜５００倍仮説出力）に増大します。
【００３２】
そして真空部重力パワー水蒸気の１００００倍の高温水質量を、最適の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１／１００００等に縮小します。超臨界圧力等の高温水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、全重力パワー５００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回転出力を発生し、高温水の気化爆発力により噴射速度を大幅に減速して、重力パワーを極限まで増大し、機械効率を１０〜２０倍に上昇して、略直線蛇行的に噴射する全動翼を通常設計が可能とし、５００倍仮説出力等とします。
【００３３】
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、全熱量を回収して有効利用します。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、限りなく高圧燃焼熱交換して燃焼ガス入口温度を最低にし、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、超臨界圧力高温水等として熱回収し、該排気温度を−２７３℃に近付けます。すると燃焼温度と容積の障壁が最低となり、圧縮圧力を既存ガスタービンの２倍以上の１０ＭＰａ以上として、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倍とします。
【００３４】
摩擦損失最少で出力を発生させるため、全動翼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、比透磁率の大きい材料で構成し、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と超臨界圧力高温水等との間に気化膜を設け、摩擦損失を最小の重力パワーを最大の最適速度で出力を発生します。
【００３５】
全動翼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無駄を全廃し、機械効率を１０倍〜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℃・６０℃以下等とし、冷却水も給水３と海水等を用途に合わせて使用して、気化潜熱回収器６６ａにより熱回収した給水３と凝縮水は、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使用を可能にして、燃料燃焼質量を最低に低減すると共に、膨大な温熱を需要家に供給可能にし、非常に安価な電力を供給すると共に、温熱の需要拡大を図り、不要な温熱量のみ海水温度等に変換します。
【００３６】
冷熱回収量を最大にしてＣＯ２等の燃焼ガス排気を０にするため、起動時のみ全動翼ガスタービンとして使用し、最大の冷熱を回収用の全動翼蒸気ガスタービンの最上流に、最適量の超臨界圧力高温水等を供給し、中流最適段に燃焼ガスを供給して、出力発生の過程で低温度最適量の水噴射し、高温水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、低温燃焼ガスを核に全水分を凝集することで、復水器真空まで膨張を可能とします。
【００３７】
最大量の冷熱を回収して水道水等を冷却しておき、業務用家庭用クーラーに変えて冷熱水道水管を配管し、送風機等で都市部を丸ごと冷却する等とし、冷房費用を１／１０等に低減し、膨大になり過ぎる冷熱で海水を冷却する過程では、ＣＯ２等により酸素等の空気を吸引して海底に最適量を供給し、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、地球温暖化を逆転して冷却します。
【００３８】
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にすることで、圧縮空気を略直線蛇行的に圧縮して、水噴射手段５６から水噴射して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して、燃焼ガスタービン入口温度を最低温度にします。
【００３９】
全動翼蒸気ガスタービンの燃焼ガス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も用途により水噴射手段５６ａより水噴射して、気化爆発水蒸気温度や燃焼ガス温度を冷却し、高温水の気化爆発水蒸気速度や燃焼ガス速度を、水質量の速度重力パワーにエネルギ変換し、最適速度に減速します。
【００４０】
最適速度に減速して１００倍〜５００倍仮説出力に増大し、膨張燃焼ガスによる水蒸気の冷却を僅少にして、低温燃焼ガスを核に水分を凝集する冷熱を最大にします。燃焼ガス排気温度は−２７３℃に近付け、低温燃焼ガスを核に水分を凝集して、自然現象と同様に雹や水滴として分別回収を可能にし、膨大な水道水等を熱交換冷却して貯蔵する過程で、燃焼ガスを水滴に溶解してＣＯ２等の排気０を可能にして、地球温暖化防止します。
【００４１】
燃焼ガス熱量出力＋燃焼ガス質量出力全部を回転出力とする場合は、全動翼蒸気ガスタービン合体機関の、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圧力等の高温水全部を、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、砲身状の高温水噴射ノズル５９ａより噴射して、ノズル内では機関銃の弾丸のように高温水を加速し、ノズル外では散弾ロケットのように高温水を加速して、加熱高温とした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潜熱爆発力を最適利用し、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。
【００４２】
大気圧重力パワー既存蒸気タービンの１７００倍の高温水質量を最大にし、中流最適段に最低温度の燃焼ガス質量出力として供給し、一瞬高温水５ａ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を核に水分を凝集して、ＣＯ２等の燃焼ガスを５０倍質量等の高温水に溶解して、ＣＯ２等の排気を０にすることで、復水器真空まで出力発生を可能にし、タービン動翼面積の一部乃至大部分を、大気圧部１／１７００や真空部１／１００００等に縮小します。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、合理的な回転数を可能にすると共にタービンの動翼面積も、通常設計が可能な動翼面積に縮小します。
【００４３】
有限の燃料資源を子孫にも残すため、発電用には安価微粉炭燃料の燃焼とし、燃焼灰の重力パワーにより全重力パワーを更に増大して、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して、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℃に近づけて、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、超臨界圧力等の高温水に変換して使用します。
【００４４】
そして同一燃料量燃焼ガス質量発電量（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）＝（４０〜８０倍燃焼ガス質量発電量）とします。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２００〜５００倍燃焼ガス熱量発電量）＝（既存ガスタービンの２４０〜５８０倍仮説発電量）とします。
【００４５】
輸送用機器の場合は飽和温度が１００℃前後に限定され、廃熱回収も困難のため、超臨界圧力高温水等の温度が過熱蒸気側に上昇し（同一燃料量既存ガスタービンの２０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／１０〜２０）＝（１００〜２００倍仮説出力）等となり、燃焼ガス質量出力（既存ガスタービンの２０〜４０倍仮設出力）を含めて（既存ガスタービンの１２０〜２４０倍仮設出力）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。
【００４６】
各種自動車や各種船舶や各種飛行機等として、実用化の過程で全高温水重力パワーを最大にし、燃焼ガス排気温度を−２７３℃に近付けて、低温燃焼ガスを核に水分を凝集して水滴等とし、１２０〜２４０倍仮説出力の、燃焼ガスの２０倍質量等の水分等に、燃焼ガスを溶解して排水し、ＣＯ２等燃焼ガス排気を０に近付けます。
【００４７】
回転出力＋噴射推進力利用の場合は、回転出力用の超臨界圧力高温水等の水温が、実用的な高温水気化爆発速度とするため比較的に低温になり、噴射推進出力用の超臨界圧力高温水等の水温は、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の重力パワーにエネルギ変換して、２００倍出力等が容易な全動翼蒸気タービンで、主として回転出力に変換し、用途により全動翼蒸気ガスタービンを使用します。
【００４８】
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、バルブ制御して熱交換して得た低温燃焼ガスを、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、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。
【００４９】
起動準備運転で熱交換して得た超臨界圧力高温水等の温度上昇時には、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圧力高温水等を、全動翼蒸気タービンの最上流に供給し、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速度質量を噴射推進力とし、限り無く高速飛行します。
【００５０】
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９１ａ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質量容積利用により、前方の空気を吸引して噴射推進し、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、噴射推進の過程で極低温燃焼ガスを核に水分を凝集して、雹等として海上等に希薄供給し、海域を活性化する工夫をします。
【００５１】
【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するが、数字に限定しません。
【００５２】
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、極低温燃焼ガスや水等で、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全動翼タービン動翼８１を使用します。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、−２７３℃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。
【００５３】
図１の全動翼蒸気タービンの第１実施例には、図２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大部分を、超臨界圧力等の高温水５ａ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の高温水溜３２ａ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５９ａにより、高温水５ａとの間に気化膜を設けて、摩擦損失最少で気化爆発エネルギにより高温水を加速して噴射します。
【００５４】
そして高温水噴射ノズル内では高温水を機関銃の弾丸のように加速し、ノズル外では散弾ロケットのように高温水を加速して、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×２０〜５０倍質量重力パワー×１０〜２０倍機械効率／１０〜２０）＝（２００〜５００倍仮設出力）等に増大し、出力発生の過程でも用途により水噴射して、高温水気化爆発による水蒸気５を冷却して、水蒸気容積を縮小し、蒸気速度の大部分は高温水質量の速度重力パワーにエネルギ変換し、最適速度に減速して、合理的な設計が可能な回転数にします。
【００５５】
上流の一部分乃至下流の大部分は、大気圧単位容積重力パワーを、最先端蒸気タービンの１７００倍や、真空部単位容積重力パワーを１００００倍以上の、高温水質量重力パワー×速度として減速し、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や１／１００００に縮小して、合理的な設計を可能な動翼面積にします。電磁加熱タービン動翼８１の動翼面積の大幅な縮小及び、全重力パワーの大幅な増大、高温水速度の大幅な減速により、全動翼蒸気タービンの合理的設計を可能にし、低速回転の可能や小型簡単大出力にします。
【００５６】
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、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、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、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とします。
【００５７】
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、重力パワー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、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、回転接点により通電して、電磁加熱噴口８３を含め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加熱高温にし、出力発生の過程で機械効率を１０〜２０倍に上昇します。
【００５８】
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、飽和温度を１００℃から復水器真空まで可能とし、飽和温度１００℃〜５０℃前後については、冷却水の海水に換えて給水３で熱回収することで、凝縮水に加えて給水３も燃焼器兼熱交換器４に供給し、一部の回収熱量を限り無く繰返し使用して、燃料燃焼質量を最低に節減すると共に、加えた燃料燃焼熱量全部を温熱として回収可能なため、膨大な温熱を需要家に供給しながら需要の拡大を図り、燃料燃焼熱量の海水移転を皆無として、地球温暖化防止します。
【００５９】
図２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圧力等の高温水５ａが皆無のため、燃焼ガス１０のみにより超臨界圧力高温水等を発生させる、全動翼ガスタービンとして使用し、図２の侭全動翼ガスタービンとして使用するか、図にない弁を設けて弁と高温水加減弁７ａの開閉制御により、燃焼ガスを高温水溜３２ａに供給して、全動翼ガスタービンとして使用します。
【００６０】
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とします。
【００６１】
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、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。
【００６２】
燃焼器兼熱交換器４で限りなく高圧燃焼熱交換熱回収して、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略２倍の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倍仮説出力）とし、熱効率を無限上昇として、熱力学洗脳により２０世紀に大停滞させた科学技術を、目覚めさせて蘇えらせます。
【００６３】
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、超臨界圧力高温水等として高温水加減弁７ａを介して、高温水溜３２ａ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、通常使用乃至通常使用に合流して補助使用し、熱回収量を増大して公害低減・地球温暖化を防止します。
【００６４】
発電用には安価微粉炭燃料の燃焼も可能として、あらゆる燃料を燃焼して、燃焼器兼熱交換器４により限り無く高圧燃焼熱交換して、燃焼ガス排気温度を−２７３℃に近付け、ＣＯ２等燃焼ガス排気を０にします。そして冷熱の回収量を最大にするため（全動翼蒸気タービン＋全動翼蒸気ガスタービン）として、大部分の高温水５ａは全動翼蒸気タービンで使用し、最適少量の高温水５ａ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、一瞬高温水で更に冷却して出力発生の過程で逆転し、全量の低温燃焼ガスを核に水分を凝集することで、冷熱の回収量を最大に増大します。
【００６５】
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、外側軸装置の通路を介して内側軸装置の内側より、図２の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内で超臨界圧力高温水等を保存貯金増大し、その高温水５ａの温度上昇時に、夫々の高温水加減弁７ａを開放制御して、高温水を夫々の高温水溜３２ａ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５９ａより、高温水５ａとの間に気化膜を設けて、摩擦損失最少で気化爆発エネルギにより高温水を加速して、通常の出力を発生します。
【００６６】
出力発生の過程では摩擦損失最少として、高温水噴射ノズル内では高温水を機関銃の弾丸のように加速し、ノズル外では散弾ロケットのように高温水を加速して、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、高温水質量の速度重力パワーにエネルギ変換して減速し、最適速度に低減します。そして排気前には低温燃焼ガスの微粉炭燃焼灰等も含めて、低温燃焼ガスを核に水分を凝集して雹や水滴を生成させることで、復水器真空まで膨張させて分別可能とし、ＣＯ２等の燃焼ガス排気０を可能とします。
【００６７】
分別回収した燃焼灰を含む膨大な雹や水滴は、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、電力の副産物で製造原価が略０の安価な冷熱を需要家に供給して、その販路を爆発させることで、既存の家庭用や業務用クーラーを全廃して、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て都市部等を丸ごと冷却します。
【００６８】
膨大な残りのＣＯ２や燃焼灰等を含む冷熱は別途海水を冷却して、海底にＣＯ２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、微生物や魚介類や海草類や海藻類を繁殖させて、食料の増産を図ります。
【００６９】
そ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×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＋２００倍乃至５００倍）＝（既存ガスタービンの２４０〜５８０倍全動翼蒸気ガスタービン仮説発電量）にします。
【００７０】
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で、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、陸海空の各種機器の用途には、通常の各種燃料を燃焼して、燃焼器兼熱交換器４で限りなく高圧燃焼熱交換熱回収し、熱交換して得た既存ボイラの２倍前後の燃焼ガス熱量を、超臨界圧力等の高温水５ａとして、全動翼蒸気ガスタービンの最上流に供給し、中流最適段に燃焼ガス質量出力の燃焼ガス１０を供給し、出力発生の過程で用途により、低温水噴射して気化爆発水蒸気５や燃焼ガス１０を冷却し、容積を縮小して全重力パワーを増大し、燃焼ガス排気温度を−２７３℃に近付けます。
【００７１】
そして（大気圧燃焼ガス熱量出力＋燃焼ガス質量出力）＝（既存ガスタービンの５倍落差×２倍回収熱量×１０〜２０倍質量重力パワー×１０〜２０倍機械効率／１０〜２０）＋（既存ガスタービンの２倍落差×１０〜２０倍機械効率）＝（既存ガスタービンの１２０〜２４０倍燃焼ガス熱量質量出力の全動翼蒸気ガスタービン合体機関仮説出力）とします。排気前には低温燃焼ガスを核に水分を凝集して、水滴等を生成させて分別回収を可能にし、該水に化学物質等を混入しておき、ＣＯ２等の燃焼ガスを水に合成溶解容易にして排出し、ＣＯ２等の燃焼ガス排気を０乃至僅少にします。
【００７２】
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、出力発生の過程で用途により、低温水噴射により水蒸気５を冷却し、水蒸気容積を縮小して、最低温度の高温水質量を増大します。そして最低温度の燃焼ガス１０を圧力に合わせて、最適中段に供給して出力を発生し、用途により低温水噴射冷却により、燃焼ガスや水蒸気容積を縮小して、排気前には蒸気速度の大部分を、高温水質量の速度パワーにエネルギ変換して最適減速し、全重力パワーや回転出力を大幅に増大します。
【００７３】
全重力パワーの大幅増大により、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５ａ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、重力パワー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夫々にコイル９８を設けて通電し、コイル９８の磁力線を夫々に集めて、磁力線の渦電流の電気抵抗により加熱高温とした、全動翼電磁加熱タービン動翼８１と、水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１０〜２０倍に上昇します。
【００７４】
図３の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る起動時には、内側軸装置の内側から燃焼ガス１０を、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。
【００７５】
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、低温空気として容積を縮小し、最も効率良く水冷却した低温空気を圧縮します。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、超臨界圧力等の高温水５ａにします。
【００７６】
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、燃焼ガス排気温度を−２７３℃に近付け、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倍の、１０ＭＰａ以上可能にして理論空燃比まで、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、同一燃料量既存ボイラの２倍前後の回収熱量として、超臨界圧力高温水等として回収します。
【００７７】
ＣＯ２等の燃焼ガス排気を０に近付けるため、超臨界圧力等の高温水５ａの貯蔵圧力上昇時に、高温水加減弁７ａを開放制御して通常の出力を発生し、例えば５／２５の高温水の一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燃焼ガス等を冷却し、水質量の速度パワーにエネルギ変換して最適減速し、低温度で燃焼ガス等を排気し、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て、噴射推進する出力発生の過程で、低温燃焼ガスを核に水分を凝集して、ＣＯ２等の排気を水滴に封印して、ＣＯ２等の燃焼ガス排気を０に近付けます。
【００７８】
１９／２４の超臨界圧力等の高温水５ａ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９１ａを利用して、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た、砲身状乃至末広砲身状の高温水噴射ノズル５９ａより、高温水の気化爆発力により火薬爆発と同様に、ノズル内では高温水を機関銃の弾丸のように加速し、ノズル外では高温水を散弾ロケットのように加速して、夫々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推進する夫々の特殊装置９２ａによりバイパス噴射して、用途に合わせて既存ガスタービンの１０倍噴射速度等で噴射推進します。
【００７９】
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、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、１０倍前後噴射速度で噴射推進します。超臨界圧力等高温水５ａの貯蔵圧力上昇により、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５ａ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等にします。
【００８０】
超臨界圧力等の高温水５ａの一部と燃焼ガス全部により、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５ａを、公知技術を含む複数の霧吹きの原理９１ａを利用して、夫々の特殊装置９２ａにより、ラムジェットを遥かに超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、超臨界圧力等の高温水気化爆発エネルギによる質量速度を、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噴射推進させるものです。
【００８１】
ＣＯ２等燃焼ガス排気を０にするため、噴射推進を含む全動翼蒸気ガスタービンでは、例えば５／２４の高温水５ａの一部と、燃焼ガス１０の全部により、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、最低温度で燃焼ガスや高温水５ａや水蒸気５を排気し、内側軸装置の中空部や外側軸装置外周部の空気を、吸引して噴射推進する出力発生の過程で、用途により低温水噴射して低温燃焼ガスを核に凝集する水温を低下させ、ＣＯ２等排気を水滴に封印して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水滴を供給します。
【００８２】
１９／２４前後の超臨界圧力等の高温水５ａ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９１ａを利用して、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た、高温水噴射ノズル５９ａより高温水の気化爆発力により、ノズル内では高温水を機関銃の弾丸のように加速し、ノズル外では高温水を散弾ロケットのように加速して、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推進する夫々の特殊装置９２ａにより、用途に合わせて既存ガスタービンの１０倍噴射速度等で噴射推進します。
【００８３】
図４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、燃焼ガス１０を高温水溜３２ａ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ます。燃焼器兼熱交換器４の超臨界圧力高温水等の圧力上昇時に、燃焼ガス１０から高温水５ａに切り替え弁閉制御して、高温水加減弁７ａを開放制御し、超臨界圧力高温水等の一部により、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、空気吸入出力と噴射推進出力を発生します。
【００８４】
燃焼ガス１０全部は複数の霧吹きの原理９１ｂを利用して、夫々の特殊装置９２ｂによりバイパス噴射して、前方の空気を多段に吸引して噴射推進力にします。残りの大部分の高温水５ａは、複数の霧吹きの原理９１ａを利用して、夫々の特殊装置９２ａによりバイパス噴射して、前方の空気を多段に吸引して、ラムジエツトの１０倍等の噴射速度で噴射し、空気吸入出力と噴射推進出力で噴射推進し、夫々の出力により既存ガスタービンの１２０〜２４０倍仮説出力の、ジェット機や飛行船舶や宇宙往還親飛行機等とするものです。
【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、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。
【００８６】
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、最も効率良く給水冷却して低温空気を圧縮します。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。
【００８７】
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、超臨界圧力高温水等、大きな落差や重力パワーでも合理的設計を可能にし、動圧出力を増大するため、単位重力パワーの増大を最重要とし、大気圧単位容積重力パワー最大を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を可能にます。
【００８８】
熱交換して得た超臨界圧力高温水等の一部により、全動翼圧縮機を含む全動翼蒸気タービンを駆動し、高温水や気化爆発排気の水蒸気５を噴射駆動力とし、内側軸装置の中空部前方や外側軸装置の外周部前方の空気を吸引して、空気吸引力と噴射質量速度を推進力にします。燃焼ガス１０の全部及び残りの高温水５ａは、夫々の霧吹きの原理９１ｂ・９１ａを利用して、夫々の特殊装置９２ｂや９２ａによりバイパス噴射し、前方の空気を夫々多段に吸引して、夫々の速度を直接空気質量の速度エネルギに変換し、既存ガスタービンの１０倍噴射質量速度等で噴射し、低温燃焼ガスを核に水分を凝集して、容積の一部乃至大部分を１／１７００等に縮小し、排気騒音が１／１０等僅少な超音速旅客機等とします。
【００８９】
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、超臨界圧力高温水等の回収熱量として最大に増大し、熱交換して得た（燃焼ガス熱量出力１００〜２００倍出力）＋（燃焼ガス質量出力２０〜４０倍出力）＝（既存ガスタービンの１２０〜２４０倍仮説出力）にします。
【００９０】
超臨界圧力高温水５ａ等としてその一部を、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を冷却し、水蒸気速度の一部分を、大気圧１７００倍単位重力パワーに変換して最適速度に減速し、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９１ａ・９１ｂを利用して、残りの高温水５ａと燃焼ガス１０を、夫々既存ガスタービンの１０倍や５倍速度でバイパス噴射し、１００倍以上出力にする過程で、低温燃焼ガスを核に水分を凝集して雹や水滴を生成し、ＣＯ２等燃焼ガス排気を０に近付けます。
【００９１】
図５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、低温空気を圧縮して燃焼器兼熱交換器４に供給します。
【００９２】
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熱回収して、燃焼ガス取出口８８の温度を最低に低下させ、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、超臨界圧力高温水５ａ等として、用途によりその一部を単位重力パワーが重要な、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水噴射して気化爆発水蒸気を冷却し、水蒸気速度の一部分を、大気圧１７００倍単位容積重力パワーに変換して最適減速し、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。
【００９３】
燃焼ガス１０全部及び残りの超臨界圧力高温水５ａを、夫々の霧吹きの原理９１ｃ・９１ｄ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９３ａ・９３ｂにより、各種高速船舶や各種高速水上移動機器を噴射推進させます。
【００９４】
燃焼ガス１０全部を夫々霧吹きの原理９１ｄを利用して、前方の水を多段に吸引して噴射し、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が大気圧−２７３℃に近付くため、海水等を冷却してＣＯ２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９１ｄを利用して、空気や酸素等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、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にします。
【００９５】
図６・図７・図８・図９を参照して、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。
【００９６】
このため、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する、送水ポンプ兼二重反転磁気摩擦動力伝達装置１４ａ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、超高圧少量送水ポンプとしても使用し、熱回収して送水します。
【００９７】
このため、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、転がり接触動力伝達装置とし、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ます。
【００９８】
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、熱回収して燃焼器兼熱交換器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。
【００９９】
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が必要です。
【０１００】
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た、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。
【０１０１】
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車を、ハスバ歯車に換えてハスバ凹凸４２車を、ヤマバ歯車に換えてヤマバ凹凸４３車を設ける。
【０１０２】
又は図に無い平内歯車に換えて平内凹凸４１ａ車を、ハスバ内歯車に換えてハスバ内凹凸４２ａ車を、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、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。
【０１０３】
図６ａ・図６ｂ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７の着磁摩擦車装置５１ｃ＋９７や図９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。
【０１０４】
図６ｃ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８の着磁摩擦車装置５１ｄ＋９７や図９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。
【０１０５】
図６ｄ・図６ｅ・図６ｆ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７・図８図９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。
【０１０６】
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７や図８や図９の二重反転磁気摩擦動力伝達装置１４と同様に外箱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。
【０１０７】
例えば図７・図８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。
【０１０８】
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で超臨界圧力高温水５ａ等とします。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。
【０１０９】
例えば、図９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。
【０１１０】
図９（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を、図９の実施例により説明する。図９（ａ）は、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、二重反転磁気摩擦動力伝達装置１４として使用します。
【０１１１】
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、又は両方より夫々回転出力を取り出し可能とします。
【０１１２】
図９（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、既存歯車ポンプと同様に外箱９４を設けます。
【０１１３】
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を含む上流側に送水路９６を設け、回転方向棒磁石３３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を含む上流側に送水路９６を設け、回転方向電磁石３４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。
【０１１４】
図１０により本発明による地球温暖化防止を説明する。世界の火力発電所では、例えばボイラ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、ボイラで加熱した熱量全部で海水温度を上昇する容積利用のため、超臨界圧力過熱蒸気から復水器真空まで断熱膨張させると、容積は１００００倍を超えて重力パワーが１／１００００以下となり、同一出力に１００００倍以上の動翼面積が必要なため、無茶苦茶設計による地球温暖化加速を避けられません。
【０１１５】
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して、燃焼ガス排気温度を−２７３℃に近付けると、膨大な冷熱を副産物として製造原価略０で得られるのに加えて、ＣＯ２等燃焼ガス排気を０等として、同一燃料量既存ボイラの２倍前後の回収熱量を、超臨界圧力高温水等として回収して燃焼ガス熱量出力とし、燃焼ガス質量出力も大幅に増大出来ます。
【０１１６】
そこで既存ボイラの２倍前後の超臨界圧力高温水５ａ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５ａ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ノズル内では、気化爆発力により高温水を機関銃の弾丸のように加速し、ノズル外では高温水を散弾ロケットのように加速して、重力仕事率を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５００倍仮説出力等に上昇します。
【０１１７】
全動翼蒸気タービンの副産物を簡略説明する、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、副産物の製造原価略０の温熱として水道水を１００℃近くに加熱貯蔵しておき、安価な電力と共に高温水道水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、気化熱全部で海水温度を上昇していた既存技術の無茶苦茶を全廃します。
【０１１８】
全動翼蒸気ガスタービンの副産物を簡略説明する、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して燃焼ガス排気温度を−２７３℃に近付け、低温燃焼ガスを核に水分を凝集して、燃焼ガス全部＋αの膨大な冷熱を回収して、副産物の製造原価略０の冷熱として水道水を冷却貯蔵しておき、安価な電力と共に低温水道水として需要家に供給し、業務用クーラーや家庭用クーラーを全廃して、都市部を丸ごと冷却する等、脱フロンにより地球温暖化防止すると共に、ＣＯ２等の燃焼ガス排気０を可能にします。
【０１１９】
図１１の各種全動翼蒸気ガスタービン合体機関の、回転力や噴射出力で駆動する、各種装置を説明する。燃焼ガス排気温度を−２７３℃に近付け、復水器真空まで断熱膨張させ、低温燃焼ガスを核に水分を凝集して、雹や水滴として分別回収可能にする、全動翼蒸気ガスタービン合体機関により、各種発電設備・各種熱と電気と冷熱の供給設備・各種熱と電気の供給設備等を駆動します。
【０１２０】
燃焼ガス排気温度を−２７３℃に近付け、大気圧まで断熱膨張させ、低温燃焼ガスを核に水分を凝集し、水滴として分別回収を可能にする、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。
【０１２１】
燃焼ガス排気温度を−２７３℃に近付け、水蒸気や燃焼ガスの１以上を霧吹きの原理を利用してバイパス噴射し、大気圧まで断熱膨張させ、低温燃焼ガスを核に水分を凝集して、水滴として分別可能にする、全動翼蒸気ガスタービン合体機関により、各種船舶・各種高速船舶・各種飛行機・各種艦船・各種戦闘機・各種宇宙往還親飛行機・各種超音速機・各種飛行機器等を駆動します。
【０１２２】
【発明の効果】
超臨界圧力高温水を利用するため、大気圧重力仕事率を１７００倍に近付けて、同一燃料量既存ガスタービンの５００倍仮説出力に増大する効果がある。
【０１２３】
超臨界圧力高温水を利用するため、大気圧重力仕事率を１７００倍に近付けて、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する効果がある。
【０１２４】
超臨界圧力高温水を利用するため、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により、ノズル内では高温水を機関銃の弾丸のように加速し、ノズル外では散弾ロケットのように加速して、同一燃料量既存ガスタービンの５００倍仮説出力に増大する効果がある。
【０１２５】
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、摩擦損失を僅少とするため、最も効率良く出力を発生する効果があります。
【０１２６】
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。
【０１２７】
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の増大を、確実容易にする効果があります。
【０１２８】
燃焼ガス排気温度を−２７３℃に近付けて、大きな単位重力パワーや全重力パワーにしても、電磁加熱タービン動翼等と高温水等との摩擦損失最小で、大きな出力を発生させる効果があります。
【０１２９】
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倍前後の１０ＭＰａ以上等に、上昇可能にする効果があります。
【０１３０】
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、超臨界圧力高温水等として回収可能にする効果がある。
【０１３１】
超臨界圧力高温水等として、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９２ａ・９２ｂを駆動して、最も効率良く空気を吸引して噴射推進する効果があります。
【０１３２】
超臨界圧力高温水等として、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９３ａ・９３ｂを駆動して、最も効率良く水を吸引して噴射推進する効果があります。
【０１３３】
燃焼ガス排気温度を−２７３℃に近付けて、全動翼蒸気ガスタービン合体機関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。
【０１３４】
水噴射気化爆発水蒸気や燃焼ガスを冷却して、高温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を、コンパクトに設計できる大きな効果があります。
【０１３５】
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することで、電気料金を低下させて、発電所等から排出されるＣＯ２等の地球温暖化燃焼ガスを、最も効率良く回収する効果もあります。
【０１３６】
事業用クーラーや家庭用クーラーを全廃して、脱フロンによる地球温暖化防止の効果もあります。
【０１３７】
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や窒素や酸素を供給して、海藻や魚類等を繁殖させて活性化する効果があります。金儲けのみが企業活動と感える誤りを逆転して、人類のために貢献する手法を皆で考える効果があります。
【０１３８】
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倍前後の１０ＭＰａ以上を可能にする効果があります。
【０１３９】
熱交換して得た燃焼ガスや高温水の気化爆発水蒸気を水冷却し、単位重力パワーが既存蒸気タービンの大気圧１７００倍、真空部１００００倍以上の高温水質量を最大最適に増大可能にする効果があります。
【０１４０】
既存蒸気タービン過熱蒸気の大気圧部１７００倍や真空部１００００倍等の、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。
【０１４１】
重力パワーを大気圧部１７００倍や真空部１００００倍等に増大することで、タービン動翼面積の一部乃至大部分を、１／１７００や１／１００００等に縮小して、構造を大幅に簡単に出来る大きな効果があります。
【０１４２】
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。
【０１４３】
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、水噴射気化爆発水蒸気や燃焼ガスを冷却して、高温水質量を増大するため、断熱膨張低温燃焼ガスを核に水分を凝集して、自然現象と同様に雹や水滴等として、膨大な水にＣＯ２等の燃焼ガスを合成溶解混合する過程で、物質を加えて無害で排出可能にする効果もあります。
【０１４４】
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、雹や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。
【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】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３】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４】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５】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６】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７】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８】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９】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１０】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１１】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　　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　　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　　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　　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　　９１ｂ：霧吹きの原理　　９１ｃ：霧吹きの原理　　９１ｄ：霧吹きの原理　　９２ａ：特殊装置　　９２ｂ：特殊装置　　９３ａ：水噴射装置　　９３ｂ：水噴射装置
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[0001]
TECHNICAL FIELD OF THE INVENTION
The present invention describes the idea by using hypothetical figures to explain clearly why the existing internal combustion engine technology competes with fuel cells and wind power generation with volume utilization that hardly uses heat, but the correct answer is an experimental value, Not limited to idea hypothetical numbers. For example, a state-of-the-art reheat steam turbine uses a volume that does not use any amount of heat, so it expands more than 10,000 times in the adiabatic expansion vacuum section, reduces the gravitational power to 1/10000 or less, and has 10,000 times the rotor blades at the same output. In addition to requiring an area, even if the head is increased in supercritical pressure, etc., it is impossible to perform 1,000,000 rotations, etc., so that speed energy is consumed about 10 to 20 times that of the moving blade, and rotation work is not performed. In fact, half of the stationary vanes are provided and deceived by adiabatic expansion. In fact, the hypothetical output is reduced to 1/500, etc. by raising the seawater temperature with all the heat heated by the boiler and accelerating global warming. I'm messed up.
[0002]
Therefore, the reheating is reversed to maximize the amount of high-temperature water recovery heat such as supercritical pressure by the combustor / heat exchanger 4 and to increase the heating temperature to a high temperature mainly by the heating and high-temperature means 101. By injecting high-temperature water and accelerating the high-temperature water inside the nozzle like a bullet of a machine gun by the vaporization explosion energy, and accelerating the high-temperature water outside the nozzle like a shot rocket, optimal use of latent heat of vaporization By making the atmospheric pressure gravitational power 1700 times that of the state-of-the-art reheat steam turbine and making the gravitational power close to 1700 times, part or most of the blade area can be reduced to 1/1700 of the existing reheat steam turbine. The present invention relates to a technique for completely abolishing unreasonable imperfections blocked by vanes and making it possible to design a rational moving blade area, such as a full moving blade steam turbine.
[0003]
The adiabatic expansion is also reversed up to the condenser vacuum of the reheat steam turbine, and the whole rotor blade steam turbine of the adiabatic expansion suitable for the application under the atmospheric pressure is provided. The maximum amount of recovered heat including the latent heat of vaporization below is maximized, and the recovered heat and condensed water close to 100 ° C are repeatedly used by the combustor / heat exchanger 4 as high-temperature water at a supercritical pressure or the like. By doing so, it becomes possible to supply enormous amount of cold heat and to supply all enormous heat while using an all-blade steam gas turbine or an all-blade gas turbine that can greatly reduce the fuel combustion mass. The present invention relates to a technique for eliminating rise in seawater temperature by using a moving blade steam turbine.
[0004]
The state-of-the-art gas turbine also uses a volume that uses little heat, so it is necessary to raise the temperature of the combustion gas turbine inlet. With the increase in turbine heat-resistant limit temperature, it is impossible to raise the head. Is also converted to a rotational force, the speed energy is consumed about 10 to 20 times that of the moving blade, and a half of the stationary blade that does not perform any rotating work is provided to increase the loss, and the heat is not used. It is exhausted at around 500 ° C as it is, and the output is reduced to 1/100 to 1/500, resulting in a large loss.
[0005]
Therefore, in order to minimize the inlet temperature of the combustion gas turbine by reversing the state-of-the-art gas turbine, use a gas turbine combustor / heat exchanger 4 to maximize the heat recovery by performing high-pressure combustion heat exchange cooling and combustion infinitely. Then, the exhaust gas temperature of the all-blade gas turbine, which was completely abolished by reversing the stationary blades, was set to the minimum reversal temperature of the combustion gas turbine, and the exhaust temperature was approached to -273 ° C. The present invention relates to a technology for producing high-temperature water such as supercritical pressure, including about twice the amount of recovered heat of an existing boiler, including the total amount of heat, and near-infinite recovered heat of a vaporizing latent heat recovery unit (66a).
[0006]
For example, high-temperature water such as supercritical pressure is supplied to the uppermost stream of the all-blade gas turbine, and high-temperature water is injected from a high-temperature water injection nozzle 59a, which is heated to a high temperature to minimize friction loss, thereby causing a vaporization explosion. Energy accelerates water droplets like a bullet or a rocket, drives the all-blade gas turbine, supplies low-temperature combustion gas to the middle-stage optimal stage, and generates power up to the vacuum of the adiabatic expansion condenser. The condensation of water with the combustion gas as the core enables expansion to the condenser vacuum, the use of the optimum minimum amount of high-temperature water minimizes the cooling loss of vaporization heat, and the emission of combustion gas such as CO2 is reduced to 0, resulting in enormous cooling Related to the technology for collecting wastewater.
[0007]
In the process of driving the all-blade gas turbine including supercritical high-temperature water, etc., with the consumption of fuel calorie below 0, etc., the same mass of combustion gas and high-temperature water are injected almost linearly meandering by all the blades in the process of driving. Then, the mechanical efficiency is increased by 10 to 20 times (5 times head of existing gas turbine × 2 times mass × 10 to 20 times mechanical efficiency) = (100 to 200 times hypothetical output of existing gas turbine) ) = (Combustion gas mass + high-temperature water vaporization explosive power output), including the minimum amount of high-temperature water to enable expansion to condenser vacuum, and infinitely increase the thermal efficiency of the combustion gas mass output of all blade gas turbines On technology to revive science and technology that had stagnated in the mid-20th century due to thermodynamics.
[0008]
In the process of driving the full-rotor steam turbine, which is the reverse of the reheat steam turbine, about twice the amount of heat recovered from the existing boiler is converted to high-temperature water such as supercritical pressure. In the process of generating output, each high-temperature water control valve is used. 7a through a high-temperature water pipe 6a, supply high-temperature water 5a to each high-temperature water reservoir 32a, and provide a vaporization film between the high-temperature water jet nozzle 59a heated by the high-temperature heating means 101 and the high-temperature water, respectively. Injection with minimal friction loss, high temperature water is accelerated like a bullet inside the nozzle by vaporization explosion energy, and high temperature water 5a is accelerated like a rocket outside the nozzle, and the gravitational power is the size of the most advanced reheat steam turbine. The present invention relates to a technique for approaching a gravity work rate of 1700 times the atmospheric pressure and 10000 times the vacuum part.
[0009]
It converts the hot water mass into the vaporization explosion velocity energy and increases the total gravity power by 100 times or 200 to 500 times to generate output. In the process of generating the output, a vaporization film is provided between the high-temperature water and the high-temperature water as a rotor blade steam turbine or the like of the electromagnetic heating turbine blade 81 including the respective high-temperature water injection nozzles 59a and the electromagnetic heating nozzles 83 to reduce friction loss. By minimizing the pressure, it is injected almost linearly meandering and expands to the condenser vacuum, increasing the mechanical efficiency by 20 times. Then, twice the recovered heat of the existing boiler (the same fuel amount, high-temperature water calorie mass output) = (40 to 100 times the mass gravity power × 5 times the head × 2 times the recovered heat mass × 20 times the mechanical efficiency / 40) = (existing The present invention relates to a technology for making a hypothetical power generation 200 to 500 times that of a gas turbine.
[0010]
In the present invention, in order to heat all the rotor blades to high temperature by electromagnetic induction heating, the coil 98 is provided and energized similarly to the electromagnetic cooker, and the magnetic flux 99 is collected in a material containing iron having a large relative magnetic permeability, and the vortex is collected. Joule heat is generated by the electric resistance due to the electric current, and constitutes the electromagnetically heated turbine blade 81 of various types of high temperature heating. Then, a vaporized film is provided between the electromagnetic heating turbine blade 81 and the high-temperature water, and a substantially linear meandering injection is performed by all the blades, and the output is reduced to the atmospheric pressure with the minimum friction loss, the minimum heat consumption, and the maximum gravity power. The supercritical pressure high-temperature water output of all-blade steam gas turbine combined engines, for example, for transportation equipment, which is much smaller and simpler in structure The present invention relates to a technique of (gravity power × 5 × head × 2 × recovered heat × 10 × to 20 × mechanical efficiency / 20) = (100 × to 200 × hypothetical output of existing gas turbine).
[0011]
The present invention provides a water-repellent water cooling blade 87 composed of any one or more of a water-repellent metal, a coating of a water-repellent substance, a water-repellent ceramic, and a water-repellent process, for the entire blade gas turbine compressor blade. The friction loss between the water-repellent water cooling blade 87 and water is reduced, the air is compressed substantially linearly and meandering by all the moving blades, and the air is water-cooled and compressed with the minimum friction loss, and the combustor is also used. The present invention relates to a technique for supplying low-temperature air to the heat exchanger 4 most efficiently.
[0012]
As the combustion gas cools, the unit gravity power increases and the size and the output can be increased. Therefore, the combustion gas and heat exchanger 4 of various all-blade steam gas turbines perform high-pressure combustion heat exchange without limitation, and the turbine combustion gas In the process of generating power, the inlet gas is cooled to a minimum, the combustion gas is combined with the high-temperature water and cooled, the adiabatic expanded cryogenic combustion gas is transferred, and moisture is agglomerated by the cryogenic combustion gas as a nucleus to cover the ice. To a gas exhaust gas temperature approaching −273 ° C. and expanding the condenser to vacuum.
[0013]
The high-pressure combustion heat exchange of the combustor / heat exchanger 4 of all all-blade steam gas turbines is infinitely high, and the entire calorific value of the fuel, including the total calorific value of the compressed air, and the calorific value of the compressed air are recovered, and the heat of the existing boiler is recovered. It drives various all-blade steam gas turbine combined engines as supercritical high temperature water with about twice the heat recovery. Since there is no high-temperature water at the time of startup, only the time of startup (combustion gas mass × 2 × head × 10 to 20 times mechanical efficiency) = (the same combustion gas mass as existing gas turbines 20 to 40 times the hypothesis output) Driven as a moving blade gas turbine, the heat consumption of fuel is reduced to 0 or less, and the heat efficiency is increased indefinitely. Also, the present invention relates to a technology that has been transferred to various all-blade steam gas turbine combined engines in which high-temperature water pressure is increased in the process of generating output and expanded to atmospheric pressure or condenser vacuum.
[0014]
The present invention is to reduce the combustion gas mass output of the lowest temperature obtained by infinitely high-pressure combustion heat exchange by the combustor / heat exchanger 4 + the supercritical pressure high temperature water output of about twice the recovered heat quantity of the existing boiler to the atmospheric pressure. (The same mass as the existing gas turbine, 2x head x 10x to 20x mechanical efficiency + 100x to 200x output) = (120x to 240x hypothetical output), and all blade steam gas turbines used at atmospheric pressure Related to driving technology.
[0015]
The output of an automobile or the like of the rotary output transportation device is generated by sending all of the high-temperature water 5a such as supercritical pressure through the high-temperature water pipe 6a from a plurality of high-temperature water control valves 7a to the respective high-temperature water reservoirs 32a of the all-blade steam gas turbine. And high-temperature water is injected from a high-temperature water injection nozzle 59a, which is heated to a high temperature by the respective high-temperature heating means 101, and a vaporization film is provided between the high-temperature water and the high-temperature water to minimize friction loss. Inside the nozzle, high-temperature water is accelerated like a bullet, and outside the nozzle, high-temperature water is accelerated like a rocket. A vaporization film is provided between the blades to generate output with minimum friction loss, supply low-temperature combustion gas to the optimal middle flow stage, generate output while cooling with high-temperature water, and burn in the process of power generation and adiabatic expansion Gas exhaust temperature close to -273 ° C Only, and hail or water droplets by agglomerating water low temperature combustion gases to the nucleus, the combustion gas exhaust of CO2, such as a technique close to 0 at a rotational output transportation equipment.
[0016]
For rotary output transportation equipment, etc., the total output is all rotor blade steam gas in order to maximize the hail and water droplets for cryogenic combustion gas coating by setting the exhaust gas such as CO2 to 120 times or 240 times as high as 0 for combustion gas exhaust such as CO2. Used as turbine rotation output. Mixing chemical substances etc. into high-temperature water injection water to be sent depending on the application to make it easy to synthesize and dissolve combustion gas such as CO2, and discharge pollutant gas such as CO2 from transportation equipment etc. in the process of power generation adiabatic expansion, Combustion gas exhaust temperature is approached to -273 ° C, and 20 times the mass of water is agglomerated with low-temperature CO2 and other combustion gas as nucleus, and CO2 and other combustion gas exhaust is brought close to 0 as water droplets. A water pump / magnetic friction power transmission device 100a and a water pump / counter-reversal magnetic friction power transmission device 14a, which transmit pressure in multiple stages and transmit ultra-high pressure small amount water while transmitting power, are all core technologies depending on the application. The present invention relates to a technology for dissolving CO2 or the like in water mass and draining the water in the combined turbine and steam turbine engine.
[0017]
For injection propulsion output transportation equipment, etc., the maximum amount of heat recovered by high-pressure combustion heat exchange by a combustor and heat exchanger in order to set the combustion gas exhaust such as CO2 to 0 and to achieve a hypothetical output of 120 times or 240 times, etc. A part of high-temperature water, such as supercritical pressure, from which heat has been recovered will drive all-blade steam turbines, including all-blade compressors, depending on the application. A part of the remaining high-temperature water and all of the combustion gas are bypass-injected and propelled using the respective spraying principles 91, and the remaining high-temperature water is appropriately stored in a combustor / heat exchanger or the like for optimal use. The present invention relates to a technique used as various transport equipment having a jet propulsion output used as appropriate.
[0018]
In a ship or the like that propulses all combustion gas by bypass injection, seawater is directly cooled by adiabatic expanded cryogenic combustion gas, and in the process of supplying all combustion gas such as CO2 to the seabed, air such as oxygen is further sucked and supplied. Activate the water area to increase food production such as algae and seafood. And various power generation equipment, heat and electricity and cold heat supply equipment, heat and electricity supply equipment and various general-purpose engines, various vehicles and various machines, various aircraft and various flights that use the rotation output and injection propulsion output The present invention relates to a technology that can be applied to various uses such as an object, various ships, various flying ships, and various flying vehicles.
[0019]
[Prior art]
The existing gas turbine, which generated power accidentally, was improved by using a volume that does not use any amount of heat, so it was restricted by the heat-resistant limit temperature of the turbine, making it impossible or difficult to increase the combustion gas head x mass = gravity power. In addition, the adiabatic expansion without the use of heat, at around 500 ° C, the gravitational power of the unit volume is significantly reduced, and high-temperature exhaust is performed. It is a design. Furthermore, the speed energy is consumed about 10 to 20 times that of the moving blade, and 1/2 of the stationary blade that does not perform any rotating work is provided, so that the total heat output is reduced to 1/100 or 1/500. Therefore, it is close to the output of the fuel cell and there is a large loss.
[0020]
Even though the existing steam turbine generated an accidental output, it was improved by using a supercritical pressure superheated steam. Even if supercritical pressure superheated steam was used, the adiabatic expansion condenser vacuum expanded more than 10,000 times due to volume utilization without using any heat, and the unit gravity The power is reduced to 1 / 10,000 and the same output requires 10,000 times the moving blade area. Since a huge steam speed is not available at all, it consumes about 10 to 20 times the speed energy of the moving blade, and half the stationary blades that do not perform any rotating work are provided. , It's too crazy. In a cycle that uses only the steam volume, a rational design is not possible, so the design is unreasonable, the total heat output is reduced to 1/100 or 1/500, etc. Is approaching, and there is a huge demand for heat, but adiabatic expansion of the total heat heated by the boiler increases seawater temperature, etc. with the total heat, accelerating global warming, and exhausting CO2, etc. from the boiler, causing large losses is.
[0021]
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, and Japanese Patent Application No. 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. 2001-313338, Japanese Patent Application No. 2001-336139, Japanese Patent Application No. There are 2002-12572, Japanese Patent Application No. 2002-118933 and Japanese Patent Application No. 2002-142270. The priority application based on the above-mentioned prior application generally includes all the combustors including all the moving blades and / or all the combustors of the gas turbine as the heat exchanger, and performs infinite combustion heat exchange to perform combustion. By lowering the gas inlet temperature, the calorific value of the combustion gas and the mass of the combustion gas can be used separately, and the superheated steam and the combustion gas are sprayed with water to cool the condensed water having an atmospheric pressure power of 1700 times the maximum. Thing.
[0022]
[Problems to be solved by the invention]
The existing state-of-the-art reheated steam turbine uses a volume that does not use any amount of heat, so the volume is increased by repeated reheating, and in the final stage condenser vacuum, the steam volume increases more than 10,000 times and the gravitational power is 1/10000, etc. The same output cannot be obtained at the same head unless the blade area is increased by 10,000 times to reduce the number of blades. In other words, due to the impossible rotor blade area and large steam velocity, a huge number of stationary blades are installed and blocked in multiple stages to reverse the wind direction and reduce the speed to the practical superheated steam velocity. Even more problematic is that, despite the huge demand for heat, the heat generated and recovered by the boiler is not used at all, but it is adiabatically expanded to raise the seawater temperature with all the recovered heat to accelerate global warming and reduce power generation by one. It is a large loss due to reduction to / 100 or 1/500.
[0023]
Therefore, the existing gas turbine combustor is used as the combustor / heat exchanger 4 to maximize the amount of heat recovered as high-temperature water such as supercritical pressure, and the high-temperature water vaporization energy such as supercritical pressure explodes the machine gun bullet inside the nozzle. It accelerates high-temperature water outside the nozzle like a shot rocket, and increases the gravitational power per unit of atmospheric pressure by 1700 times to generate output. Depending on the application, water is further injected in the process of generating power to cool steam, the volume is reduced to generate power with increased gravitational power, and in the process of exhausting, a vaporizing latent heat recovery unit 66a is provided in substantially the same manner as the condenser. Then, the temperature is adjusted to the saturation temperature according to the application by an air extractor, and the cooling water is also used as water 3 or condensed water, usually at around 100 ° C. to 50 ° C. The purpose is to supply the heat to the heat exchanger 4 and use the same amount of heat repeatedly, to supply the remaining enormous amount of heat to the customers, expand the effective use of heat as much as possible, and prevent global warming.
[0024]
The same amount of heat is repeatedly recovered by the latent heat recovery device 66a and supplied to the combustor / heat exchanger 4 to greatly reduce the fuel combustion mass, and the high temperature water 5a such as supercritical pressure obtained by the heat recovery is obtained. A high-temperature water jet nozzle 59a, which is supplied to the uppermost stream high-temperature water reservoir 32a of the all-blade steam turbine and is heated to a high temperature by the heating and high-temperature means 101, is provided with a vaporized film between the high-temperature water and the friction loss to minimize friction loss. Utilizing the vaporization and explosive power of high-temperature water, it accelerates inside the nozzle like a machine gun bullet, and outside the nozzle accelerates high-temperature water like a shot rocket, generating a drop and gravitational power close to the maximum The goal is to increase the temporary output to 500 times that of existing gas turbines.
[0025]
Since the amount of heat to be recovered and reused is repeatedly unknown, the calculation was made using the condenser up to the vacuum, and the unit volume gravitational power was 20 times higher than the final steam power of the existing steam turbine. Hypothetical power generation in high-temperature water is calculated by drastically reducing the power to 50 times the gravity power ((double heat recovery mass of existing gas turbine x 20 to 50 times mass gravity power x 5 times head drop x 10 to 20 times mechanical efficiency) / 10 to 20) = (200 to 500 times the hypothetical power generation of existing gas turbines).
[0026]
Then, part to most of the blade area in the final condenser vacuum is reduced to 1/10000 to make the blade area a designable blade area. Then, high-temperature water 5a is injected in a substantially linear meandering manner by a full-blade steam turbine provided with a group of electromagnetically heated outer turbine blades and a group of electromagnetically heated inner turbine blades at a high temperature. An object of the present invention is to provide a vaporization film between the blade and water to generate an output with a minimum friction loss, and to increase the power generation to 200 to 500 times the hypothetical power generation with the same fuel consumption.
[0027]
The existing state-of-the-art gas turbines also require an increase in turbine inlet temperature when using a volume that does not use any heat, and a rise in turbine heat-resistant limit temperature makes it impossible to increase the head, resulting in an enormous loss in material costs. Since the exhaust temperature is very high, around 500 ° C, the gravitational power of the unit moving blade area is greatly reduced and the moving blade area needs to be greatly increased. Stop and reverse the direction of the wind, the design becomes unreasonable to decelerate to the practical combustion gas speed, and since the calorie is not available at all, the output is reduced to 1/200 to 1/500, which is equivalent to the output of a fuel cell or wind power generation, and CO2 Exhausting the gas and accelerating global warming will be enormous, resulting in large losses.
[0028]
Therefore, as in the case of broadcasting on educational television, the existing gas turbine combustor is used as both a combustor and heat exchanger to convert the heat into a larger (large head x unit volume, large-mass gravity power) to greatly increase the work. As a vessel, heat exchange with high-pressure combustion is performed as much as possible, the exhaust gas temperature is approached as close as possible to -273 ° C, water is agglomerated with low-temperature combustion gas as the nucleus, and the combustion gas is dissolved in 50 times the mass of water and discharged. The purpose is to make exhaust such as CO2 and CO2 close to zero.
[0029]
The total moving blade steam turbine and the total moving blade gas turbine are used as a high-temperature water heat recovery amount such as supercritical pressure, which is about twice as much as that of the existing boiler, including a compressed air holding heat amount of -273 ° C or almost all. -Drive all rotor blade steam gas turbines, make the same combustion gas mass x 2 times drop x 10 to 20 times including combustion gas output such as mechanical efficiency, etc. The purpose is to prevent it.
[0030]
[Means for Solving the Problems]
The experimental numerical values are correct, but in order to clearly explain the idea of the previous stage, we will explain with hypothetical numbers, but we are not limited to the idea hypothetical numbers. When using a volume that reheats and uses no heat at all like an existing state-of-the-art reheated steam turbine, the steam speed is too large from supercritical pressure to the vacuum section, making effective use difficult or impossible. It expands 10000 times, etc., the unit volume gravitational power is reduced to 1/10000, and the blade area of 10000 times is required for the same head and the same output.
[0031]
That is, the reheating is reversed due to the impossible rotor blade area, an output is generated by the vaporization explosion energy of high-temperature water such as supercritical pressure, and a high-temperature water is formed between the high-temperature water and the high-temperature water by the high-temperature heating means 101. By using the hot water jet nozzle 59a to vaporize and explode the hot water from the hot water injection nozzle 59a to minimize the friction loss, the hot water is accelerated inside the nozzle like a machine gun bullet, and outside the nozzle Accelerate high-temperature water like a shot rocket (5 times head of existing gas turbine x 2 times recovered calorie mass x 20 to 50 times mass gravity power x 10 to 20 times mechanical efficiency / 10 to 20) = (200 times) ~ 500 times the hypothesis output).
[0032]
The mass of high-temperature water that is 10,000 times larger than that of the gravity power steam in the vacuum section will be reduced to one-ten thousandth of that of existing reheated steam turbines, with the optimal or maximum maximum and partial or large part of the moving blade area. By utilizing the explosive power of high-temperature water vaporization such as supercritical pressure, it is possible to design the whole rotor blade with a small increase in volume, and to achieve high-temperature water with a total gravity power of 500 times and electromagnetic heating of high temperature. A vaporizing film is provided between the outer turbine blade group 19 and the electromagnetically heated inner turbine blade group 20 to generate a rotational output by injecting in a substantially linear meandering manner with a minimum frictional loss, thereby evaporating the high-temperature water into a vaporized explosive power. Greatly reduces the injection speed, increases the gravitational power to the maximum, increases the mechanical efficiency by 10 to 20 times, and makes it possible to design all blades that spray in a substantially straight and meandering manner, and the hypothesis of 500 times Output etc.
[0033]
Existing state-of-the-art gas turbines also use a volume that does not use any amount of heat, so the output is small and the exhaust temperature is as high as around 500 ° C. To accelerate global warming by emitting CO2 etc., the entire amount of heat is recovered and used effectively To do. Therefore, first, the existing gas turbine combustor is used as the combustor / heat exchanger 4 to limit the combustion gas inlet temperature to the lowest by performing high-pressure combustion heat exchange, and to hold almost all of the compressed air holding heat -273 ° C or more. It recovers heat as supercritical high-temperature water, etc., which has about twice the amount of heat recovered by the boiler, and brings the exhaust temperature closer to -273 ° C. As a result, the barrier between combustion temperature and volume is minimized, the compression pressure is increased to 10 MPa or more, which is more than twice that of existing gas turbines, and the fuel combustion mass is almost four times that of existing gas turbines with the same compressed air amount up to the stoichiometric air-fuel ratio.
[0034]
In order to generate an output with a minimum frictional loss, a coil 98 is provided on the outer shaft device and the inner shaft device of the entire rotor blade electromagnetic heating turbine rotor blade 81, a rotating contact is provided by a known technique, and electricity is supplied. In substantially the same manner, the electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine blade group 20 including the annular electromagnetic heating nozzle 83 are made of a material having a large relative magnetic permeability. In addition, a vaporization film is installed between the electromagnetic heating turbine blade 81 and supercritical high-temperature water, etc., to generate the output with the minimum gravitational power and the optimal speed with the minimum friction loss.
[0035]
The entire rotor blade is heated in a substantially linear meandering manner by the electromagnetically heated turbine rotor blade 81, the waste is completely eliminated by optimally utilizing the vaporization and explosion energy, and the mechanical efficiency is increased by 10 to 20 times. The saturation temperature is set to 100 ° C / 80 ° C / 60 ° C or less according to the application by the air extractor of the vaporizing latent heat recovery unit 66a provided substantially in the same manner as the container, and the cooling water is adjusted to the supply water 3 and seawater according to the application. The feed water 3 and the condensed water recovered by the vaporizing latent heat recovery unit 66a are supplied to the combustor / heat exchanger 4 so that the same amount of heat can be used repeatedly without limit to reduce the fuel combustion mass. While reducing to the minimum, it is possible to supply enormous heat to customers, supply very inexpensive power, and expand the demand for heat, and convert only unnecessary heat to seawater temperature.
[0036]
It is used as an all-blade gas turbine only at startup to maximize the amount of cold energy recovered and reduce the emission of combustion gas such as CO2 to zero, and is optimal for the most upstream of all-blade steam gas turbines for recovery. Supply the amount of supercritical high-temperature water, etc., supply the combustion gas to the middle flow optimal stage, inject the low-temperature optimal amount of water in the process of power generation, cool the high temperature water vaporization explosion steam and combustion gas In addition to supplying the maximum amount of electric power, it can expand to a condenser vacuum by coagulating all moisture with low-temperature combustion gas as the core.
[0037]
The maximum amount of cold heat is collected to cool tap water, etc., and it is changed to a commercial home cooler, a cold hot water pipe is piped, and the entire city is cooled with a blower, etc., and the cooling cost is reduced to 1/10. In the process of cooling seawater with chilled heat that is excessively large, the air such as oxygen is sucked by CO2 and the like, the optimum amount is supplied to the seabed, and seaweed and seafood are bred to improve the seawater. We aim at activation and reverse global warming and cool.
[0038]
In the air compression process, the whole blade compressor is composed of the water-repellent water cooling blades 87, and the water-repellent material is composed of at least one of water-repellent metal, water-repellent material coating, water-repellent ceramics, and water-repellent processing. In the process of compressing the compressed air in a substantially linear meandering manner by using all the moving blades, and injecting water from the water jetting means 56 into low-temperature compressed air, the water between the water-repellent water cooling blade 87 and water or the like is reduced. By bringing the friction loss close to the minimum, the compressed air at the lowest temperature is supplied to the combustor / heat exchanger 4 and heat exchange is performed as high as possible to make the combustion gas turbine inlet temperature the lowest.
[0039]
By lowering the combustion gas inlet temperature of the all-blade steam gas turbine, the combustion gas exhaust temperature approaches -273 ° C. In the process of generating output, water is injected from the water injection means 56a depending on the application to cool the vaporized explosion steam temperature or the combustion gas temperature, and the vaporization explosion steam speed or the combustion gas speed of the high-temperature water is converted into the gravitational power of the water mass. Converts energy and decelerates to optimal speed.
[0040]
The speed is reduced to the optimal speed by 100 to 500 times the hypothetical output, and the cooling of the steam by the expanded combustion gas is reduced, and the cold heat which coagulates the water with the core of the low temperature combustion gas is maximized. Combustion gas exhaust temperature approaches -273 ° C, water is agglomerated by low-temperature combustion gas as a core, enabling separation and recovery as hail and water droplets in the same way as natural phenomena. During the process, the combustion gas is dissolved into water droplets, thereby eliminating CO2 and other emissions to prevent global warming.
[0041]
In the case where the entire combustion gas calorie output + combustion gas mass output is a rotational output, the combustor / heat exchanger is provided to the plurality of high-temperature water reservoirs 32a at the uppermost stream of the all blade steam gas turbine of the all blade steam gas turbine combined engine. 4. High temperature water such as supercritical pressure obtained by heat exchange in step 4 is supplied as combustion gas calorie output from the respective high temperature water control valves 7a, and heated to high temperature by the heating and high temperature means 101. Injection from the nozzle 59a accelerates high-temperature water inside the nozzle like a machine gun bullet, accelerates high-temperature water outside the nozzle like a shot rocket, and heats the nozzle between the high-temperature nozzle and the high-temperature water. The vaporization film is provided, the frictional loss is minimized, and the latent heat explosion power is optimally used. The vaporization film is also provided between the electromagnetically heated turbine rotor blade 81, which is heated to a high temperature, and the high-temperature water, and the gravitational power, which minimizes the friction loss, is provided. Approximately straight snake with maximum hot water velocity To the injection, and increased mechanical efficiency to 10 to 20 times.
[0042]
Atmospheric pressure gravitational power Maximizes the hot water mass of 1700 times that of existing steam turbines, supplies it to the middle stream optimal stage as the lowest temperature combustion gas mass output, cools the combustion gas 10 with the high temperature water 5a for a moment, and in the process of output generation Inverts to condense water with low-temperature combustion gas as the core, dissolves combustion gas such as CO2 in high-temperature water such as 50 times the mass, and reduces exhaust gas such as CO2 to 0 to output to condenser vacuum. It enables the generation and reduces a part or most of the turbine blade area to the atmospheric pressure part 1/1700 or the vacuum part 1/10000. In other words, by using the recovered heat as vaporizing explosive power of high-temperature water, it is possible to achieve a reasonable number of revolutions and reduce the blade area of the turbine to a normally designable blade area.
[0043]
In order to leave finite fuel resources to offspring, low-cost pulverized coal fuel is used for power generation, and the total gravitational power is further increased by the gravitational power of combustion ash to increase the combustion gas mass power generation, and Use resources most reasonably. The process of infinitely high-pressure combustion heat exchange in the combustor / heat exchanger 4 to minimize the combustion gas inlet temperature is the combustion of inexpensive pulverized coal fuel, the combustion gas exhaust temperature is brought close to -273 ° C, and the compressed air The amount of heat recovered, approximately twice as large as that of existing boilers, including almost all of the retained heat -273 ° C or higher, is converted into high-temperature water such as supercritical pressure for use.
[0044]
And the same fuel amount and combustion gas mass power generation (double head of existing gas turbine x 10 to 20 times mechanical efficiency x double mass including combustion ash) = (40 to 80 times combustion gas mass power generation). And (combustion gas mass power generation amount) + (combustion gas calorific power generation amount) = (40-80 times combustion gas mass power generation amount of existing gas turbine) + (200-500 times combustion gas calorific power generation amount of existing gas turbine) = ( 240-580 times hypothetical power generation of existing gas turbine).
[0045]
In the case of transportation equipment, the saturation temperature is limited to around 100 ° C, and the recovery of waste heat is difficult, so the temperature of supercritical high-temperature water rises to the superheated steam side (the same fuel amount, 20 times the mass of existing gas turbines). Gravity work rate × 5 times drop × 2 times recovered heat quantity × 10 to 20 times mechanical efficiency / 10 to 20) = (100 to 200 times hypothetical output), etc., and the combustion gas mass output (20 to 40 times temporary for existing gas turbines) Output) (including 120 to 240 times the temporary output of existing gas turbines).
[0046]
As a variety of cars, ships, and airplanes, maximize the high-temperature water gravitational power in the process of practical use, bring the combustion gas exhaust temperature close to -273 ° C, and coagulate water using the low-temperature combustion gas as nuclei to form water droplets, etc. Dissolves and discharges the combustion gas into 20 times the mass of the combustion gas, etc., which has a hypothetical output of 120 to 240 times, and reduces the emission of the combustion gas such as CO2 to zero.
[0047]
In the case of rotation output + injection propulsion power, the water temperature of the supercritical pressure high-temperature water for rotation output becomes relatively low to achieve a practical high-temperature water vaporization explosion rate, and the supercritical pressure for injection propulsion output Water temperatures, such as pressure hot water, approach superheated steam temperatures due to the availability of very high speeds. Therefore, in order to drive the air compressor of the all-blade steam gas turbine combined engine, the high-pressure water vaporization explosion energy is converted into the gravitational power of the rotational output, and the all-blade steam turbine is easy to output 200 times. It mainly converts to rotational output and uses an all-blade steam gas turbine depending on the application.
[0048]
A normal starting device drives a full-blade compressor including a full-blade steam turbine, inhales the air in front, exchanges infinitely high-pressure combustion heat with a combustor / heat exchanger 4, and only starts up at the time of startup. A low-temperature combustion gas obtained by using a moving blade steam turbine in an all moving blade gas turbine and performing valve-controlled heat exchange is supplied to the uppermost stream of the all moving blade steam turbine. And start preparation operation continues using the exhaust velocity mass as the injection propulsion force.
[0049]
When the temperature of the supercritical high-temperature water or the like obtained by heat exchange in the start-up preparation operation rises, the entire low-temperature combustion gas 10 having the mass of the combustion gas is bypass-injected by the valve control by the valve control and the air in front is sucked. The suction force and the injection velocity mass are used as the injection propulsion force, and supercritical pressure high-temperature water, etc. of the combustion gas calorie obtained by heat exchange is supplied to the uppermost stream of the all-blade steam turbine, and its rotation is performed. It drives the all-blade air compressor with its output, and uses its air suction force and exhaust speed mass as the jet propulsion force to fly without limit at high speed.
[0050]
All the combustion gas obtained by exchanging heat by the valve control and the remaining high-temperature water are bypass-injected by using the respective spraying principles 91b and 91a, and a large head mass volume far exceeding the adiabatic expansion ram jet is used to make the forward flow. The most efficient method of injecting and propelling air from a supersonic jet, including a supersonic flight, a space shuttle parent airplane, an airship, and a flying object. Moisture is condensed around the nucleus, and is supplied dilutely to the sea as hail, etc. to revitalize the sea area.
[0051]
BEST MODE FOR CARRYING OUT THE INVENTION
Embodiments and examples of the present invention will be described with reference to the drawings, and portions having substantially the same configuration as those of the already described embodiments and examples will be denoted by the same names or reference numerals, and redundant description. Are omitted, and characteristic portions and portions that are insufficiently described will be sequentially added and described. In addition, in order to specifically and clearly explain the intended purpose and anticipation of the invention, the idea is described by hypothetical numbers, but is not limited to the numbers.
[0052]
According to the present invention, the combustor / heat exchanger 4 that cools and compresses air efficiently, recovers heat, and uses it as low-temperature air in the simplest way is selected from the combustor / heat exchanger already applied for a patent according to the application. Use In addition, in order to generate the most efficient output from cryogenic combustion gas or water, the electromagnetically heated all-blade turbine blade 81 with high heating temperature is used. In addition, the combustion gas exhaust temperature is approached to -273 ° C to make cryogenic combustion gas. However, -273 ° C is used as the lowest practical temperature, and is expanded to all temperatures around -100 ° C and around -20 ° C. To use.
[0053]
In the first embodiment of the all-blade steam turbine shown in FIG. 1, most of the recovered heat amount obtained by exchanging heat with the combustor / heat exchanger 4 shown in FIG. Is supplied as high-temperature water 5a such as supercritical pressure through a high-temperature water pipe 6a through a high-temperature water control valve 7a to a high-temperature water reservoir 32a at the uppermost stream of the all blade steam turbine, and is provided via a heat insulating material 48a. A heating film is heated to a high temperature by direct electric resistance or electromagnetic heating, a heating film is heated to a high temperature by the heating and high temperature means 101, and a vaporizing film is provided between the high temperature water 5a and the high temperature water injection nozzle 59a in a barrel shape or a divergent barrel shape. High temperature water is accelerated and injected by vaporization explosion energy with minimum friction loss.
[0054]
Then, the high-temperature water is accelerated inside the high-temperature water injection nozzle like a bullet of a machine gun, and outside the nozzle, high-temperature water is accelerated like a shot rocket. To increase the mechanical efficiency by 10 to 20 times, for example, to reduce the combustion gas calorific output (5 times drop of existing gas turbine x 2 times recovered heat x 20 to 50 times). Double mass gravity power × 10 to 20 times mechanical efficiency / 10 to 20) = (200 to 500 times temporary output), etc., and even in the process of output generation, water is jetted depending on the application, and steam 5 due to high temperature water vaporization explosion is generated. Upon cooling, the steam volume is reduced and the majority of the steam velocity is converted into hot water mass velocity gravitational power and reduced to an optimal velocity, resulting in a reasonable design speed.
[0055]
Most of the upstream and downstream parts decelerate atmospheric pressure unit gravity power to 1700 times that of state-of-the-art steam turbines, and vacuum unit unit gravity power to 10,000 times or more, hot water mass gravity power x speed, A part or most of the blade area of the electromagnetically heated turbine blade 81 is reduced to 1/1700 or 1/10000 to make it possible to make a reasonable design. The drastic reduction of the rotor blade area of the electromagnetic heating turbine rotor blade 81, the drastic increase of the total gravitational power, and the drastic reduction of the high-temperature water velocity enable the rational design of the all-rotor blade steam turbine and enable low-speed rotation. And small and easy large output.
[0056]
By rational design, low-speed, large-output rotation and small-size, simple large-output, it is possible to perform almost linear and meandering injection as a full-blade airfoil, and also to use the electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine. The blade group 20 can be integrally cast 84 in a ring for each paragraph and fully automatic machining is also possible. Then, it is possible to cast the water injection means 56a provided insulated on the turbine blades and the like at the time of casting, and the water injection means 56a is provided near the connection between the outer diameter assembly annular portion 85 and the inner diameter assembly annular portion 86, The electromagnetically heated outer turbine blade group 19 and the electromagnetically heated turbine blade group 81 of the electromagnetically heated inner turbine blade group 20 for injecting water from an appropriate cooling means 55 not shown in the figure provided with heat insulation.
[0057]
The blade shape, blade width, and blade angle with the blade spacing expanded are adjusted to match the increased gravitational power. Then, the electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine blade group 20 can be integrally cast 84 and fully automatic processing in a ring for each paragraph. The electromagnetic heating turbine blade 81 during casting is made of a material mainly composed of iron, which easily allows magnetic flux to pass through, and the magnetic flux is collected and heated to a high temperature by an eddy current in substantially the same manner as an electromagnetic cooker. The outer shaft device and the inner shaft device are provided with a coil 98, energized by rotating contacts, and collect magnetic flux lines in the electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine blade group 20 including the electromagnetic heating nozzle 83. It increases the temperature by heating due to the electric resistance due to the eddy current, and increases the mechanical efficiency 10 to 20 times in the process of generating output.
[0058]
In the evacuation process, the saturation temperature can be set from 100 ° C. to the condenser vacuum by the air extractor of the vaporization latent heat recovery unit 66a provided substantially in the same manner as the existing condenser, and the saturation temperature is about 100 ° C. to 50 ° C. By supplying heat to the combustor / heat exchanger 4 in addition to the condensed water by supplying heat to the combustor / heat exchanger 4 by recovering heat with the feedwater 3 in place of the seawater of the cooling water, a part of the recovered heat is used endlessly and repeatedly. Since the combustion mass can be reduced to the minimum and the entire amount of added fuel combustion heat can be recovered as heat, the demand is expanded while supplying enormous heat to customers, and there is no seawater transfer of fuel combustion heat. Prevent global warming.
[0059]
The all-blade steam gas turbine or the all-blade gas turbine or the all-blade steam gas turbine combined engine shown in FIG. 2 uses the amount of heat including the first embodiment, so that the conventional gas turbine is eliminated. Since there is no high-temperature water 5a such as supercritical pressure at the time of start-up, it is used as an all-blade gas turbine that generates supercritical-pressure high-temperature water or the like only with the combustion gas 10, and is used as a full-blade gas turbine as shown in FIG. Use or use a valve not shown in the figure to supply combustion gas to the high-temperature water reservoir 32a by controlling the opening and closing of the valve and the high-temperature water control valve 7a to use it as an all-blade gas turbine.
[0060]
Outer compressor rotor blade group 16 and inner compressor rotor blade group 17, which are the main parts of all rotor compressors, are composed of at least one of water-repellent metal, water-repellent material coating, water-repellent ceramic, and water-repellent processing. The water repellent water cooling blades 87 and the like are passed through cooling means 55 (not shown) to cool the water, and the water is jetted from water jetting means 56 to directly contact and cool the compressed air. To recover the heat and reduce the air volume. By using a full-rotor blade composed of the water-repellent water cooling blades 87, the compressed air is efficiently compressed in a substantially linear meandering manner, and the frictional loss with water is minimized as a full-rotor blade airfoil having an increased blade interval. The water-repellent outer compressor rotor blade group 16 and the inner compressor rotor blade group 17 are integrally cast 84 in a ring shape for each stage.
[0061]
An annular integrated casting 84 assembly structure capable of fully automatic processing is provided, and the water passage of the cooling means 55 is connected at the annular casting assembly connection portion, and a water injection means 56 is provided near the assembly connection portion. After cooling the water-repellent water cooling wings 87 of one or more, or all or half of the paragraphs, the water passage of the cooling means 55, the water is jetted from the water jetting means 56 to directly cool the air, and the most efficient water-cooled low-temperature air is cooled. Compress. The high-temperature feed water and low-temperature compressed air from which heat has been recovered use the combustor / heat exchanger 4 to recover as much high-pressure combustion heat exchange heat as possible, thereby lowering the combustion gas inlet temperature of all bladed steam gas turbines to a minimum and reducing the amount of heat recovery. Increases the temperature of low-temperature combustion gas exhaust gas to approximately -273 ° C, about twice that of existing boilers.
[0062]
The combustor / heat exchanger 4 recovers high-pressure combustion heat exchange heat as much as possible, minimizes the disturbance of the temperature and volume of the combustion gas, sets the compression pressure to 10 MPa or more, almost twice that of existing gas turbines, and also reduces the fuel combustion mass. Up to the stoichiometric air-fuel ratio, the same compressed air amount combustion is almost four times that of the existing gas turbine, and the consumption of fuel combustion heat is set to 0 or less. The combustion gas mass output is (combustion gas mass output at the same compressed air amount lowest temperature) = ( 20x century by thermodynamic brainwashing, assuming 2x head of existing gas turbine x 4x mass x 10 to 20 times mechanical efficiency) = (80 to 160 times hypothetical output of the same compressed air amount of existing gas turbine) with infinite increase in thermal efficiency Awaken and revive the science and technology that was greatly stagnated.
[0063]
There is an urgent need to reduce pollution and prevent global warming.For example, in order to leave finite fuel resources to offspring, known garbage gasification fuel and garbage miniaturized fuel, and burning all burnable materials, using heat recovery aid, The water is supplied to the high-temperature water reservoir 32a via the high-temperature water control valve 7a as supercritical high-temperature water and converted into electric power. Then, the combustion gas air is also compressed by the all-blade compressor, cooled directly to low-temperature air by the water injection means 56, recombusted by the combustor / heat exchanger 4 and recovered for reheating, and is usually used or used. To reduce pollution and prevent global warming by increasing the amount of heat recovered.
[0064]
For power generation, it is possible to burn inexpensive pulverized coal fuel. All fuels are burned, and high-pressure combustion heat exchange is performed without limit by the combustor / heat exchanger 4 to bring the combustion gas exhaust temperature close to -273 ° C. Set the equal combustion gas exhaust to 0. In order to maximize the amount of cold heat recovered (all blade steam turbine + whole blade steam gas turbine), most of the high-temperature water 5a is used in the whole blade steam turbine, and the optimum small amount of high-temperature water 5a is completely used. The combustion gas 10 of the lowest temperature, which is supplied to the uppermost stream of the moving blade steam gas turbine and cooled to the middle stage optimal stage, is further cooled with high-temperature water for a moment and is reversed in the process of generating power, and the total amount of low-temperature combustion gas is reduced. By condensing water into the nucleus, the amount of cold energy recovered is maximized.
[0065]
At the time of start-up, the operation including the whole blade compressor is driven by a known start-up device, high-pressure combustion heat exchange is performed by the combustor / heat exchanger 4 without limit, and the combustion gas 10 having the lowest temperature is discharged from the annular combustion gas reservoir 9. From the inside of the inner shaft device through the passage of the outer shaft device, the power is supplied to the middle stage optimal stage in FIG. When the temperature of the high-temperature water 5a rises, each of the high-temperature water control valves 7a is controlled to open so that the high-temperature water is supplied to each high-temperature water reservoir 32a to be insulated. By means of the heating and high-temperature means 101 for heating to a high temperature, a vaporizing film is provided between the high-temperature water injection nozzle 59a and the high-temperature water 5a from the barrel-shaped or divergent-barrel-shaped high-temperature water injection nozzle, so that friction loss is minimized and vaporization explosion energy is applied. Accelerate the hot water to produce normal output .
[0066]
In the process of generating power, frictional loss is minimized, high-temperature water is accelerated inside a high-temperature water injection nozzle like a machine gun bullet, and outside the nozzle, high-temperature water is accelerated like a shot rocket, and a heated high-temperature electromagnetic heating turbine A vaporization film is provided between the moving blade 81 and the nozzle, and the jetting is performed in a substantially linear meandering manner with a minimum frictional loss, thereby increasing the mechanical efficiency by 10 to 20 times. A part or most of the speed is converted to energy of the hot water mass to the gravitational power and decelerated to reduce it to the optimum speed. And before exhaust, including the pulverized coal combustion ash of the low-temperature combustion gas, the low-temperature combustion gas is used as a nucleus to condense water and generate hail and water droplets. Enables zero emission of combustion gas such as CO2.
[0067]
A large amount of hail and water droplets, including combustion ash, collected separately are stored as cold heat by cooling tap water in part or all of them, and inexpensive cold heat with a production cost of almost 0 is produced by consumers as a by-product of electric power. Supply and explode the sales channel to completely eliminate the existing home and commercial coolers, prevent global warming by eliminating CFCs, and fill the cold and hot water pipes to cool down the entire city area. You.
[0068]
In the process of separately cooling seawater and supplying diluted cold heat such as CO2 to the sea floor, cryogenic heat containing a huge amount of remaining CO2 and combustion ash is supplied to the sea by sucking necessary substances such as oxygen into the sea. By thoroughly studying the ecology of living organisms, including microorganisms, we aim to increase the production of food by breeding microorganisms, seafood, seaweeds and seaweeds.
[0069]
Then, the combustion gas mass power generation is increased to (double head of existing gas turbine × double mass of coal ash etc. × 10-20 times mechanical efficiency) = (40-80 times combustion gas mass generation of existing gas turbine) , To make effective use of resources. Then, (the amount of combustion gas mass power generation + the amount of combustion gas calorific power generation) = (40 to 80 times + 200 to 500 times) = (240 to 580 times that of the existing gas turbine, all-blade steam gas turbine hypothetical power generation).
[0070]
Combined all-blade steam gas turbine engine that exhausts around the atmospheric pressure.For various land transportation equipment such as automobiles that use full power by rotational power and various land, sea, and air equipment, it burns various normal fuels. The heat and heat exchanger 4 recovers the heat of the high-pressure combustion heat exchange as much as possible, and the heat of the combustion gas, which is about twice that of the existing boiler obtained by heat exchange, is converted into high-temperature water 5a such as a supercritical pressure, and the entire moving blades. It is supplied to the uppermost stream of the steam gas turbine, and the combustion gas 10 with the combustion gas mass output is supplied to the middle stage optimal stage. In the process of generating the power, the low-temperature water is injected to cool the vaporized explosion steam 5 and the combustion gas 10 depending on the application. , Reducing the volume and increasing the total gravity power to bring the combustion gas exhaust temperature closer to -273 ° C.
[0071]
And (atmospheric pressure combustion gas calorie output + combustion gas mass output) = (5 times drop of existing gas turbine x 2 times recovered heat x 10 to 20 times mass gravity power x 10 to 20 times mechanical efficiency / 10 to 20) + ( 2x head of existing gas turbine x 10 to 20 times mechanical efficiency) = (hypothetical output of all rotor blade steam gas turbine combined engine with 120 to 240 times combustion gas calorie mass output of existing gas turbine). Before evacuation, water is coagulated by using low-temperature combustion gas as a nucleus to generate water droplets and enable separation and recovery. Chemical substances are mixed in the water, and combustion gas such as CO2 is synthesized and dissolved in water. Easily discharge and reduce the emission of combustion gas such as CO2 from 0 to very low.
[0072]
In the all-blade steam gas turbine combined engine that generates torque at all outputs, the saturated temperature of the exhaust steam 5 is as high as 100 ° C. Reduce volume and increase hot water mass at lowest temperature. Then, the combustion gas 10 having the lowest temperature is supplied to the optimum middle stage in accordance with the pressure to generate an output, and the volume of the combustion gas or steam is reduced by low-temperature water injection cooling according to the application, and the steam velocity is increased before exhaust. The energy is converted to the speed power of the hot water mass, and the speed is optimally decelerated, and the total gravity power and the rotation output are greatly increased.
[0073]
Due to the large increase in the total gravity power, the area of the electromagnetically heated turbine blade 81 can be greatly reduced, and the combined blade and steam gas turbine engine can be made compact, simple, and large-output and easy to design, and the steam 5, the high-temperature water 5a, the combustion gas 10, etc. In addition to making all blades airfoil injecting in a substantially straight and meandering manner and generating output, the blade spacing is expanded and the blade width, blade shape, and blade angle are adjusted to the shape according to the increase in gravitational power. Then, the electromagnetic heating outer turbine blade group 19 and the electromagnetic heating inner turbine blade group 20 are provided with coils 98 in substantially the same manner as the electromagnetic cooker, and are energized to collect the magnetic lines of force of the coils 98 respectively. An evaporation film is provided between the water and the entire rotor blade electromagnetically heated turbine blade 81, which is heated to a high temperature by the electric resistance of the eddy current, and minimizes friction loss, and generates an output by substantially linear meandering injection. And increase the mechanical efficiency by 10 to 20 times.
[0074]
In the second embodiment of the all-blade steam gas turbine combined engine shown in FIG. 3, at the time of startup by a normal startup device, the combustion gas 10 is supplied from the inside of the inner shaft device to the optimum middle stage to generate an output. Used as a moving blade gas turbine. An outer compressor rotor group 16 and an inner compressor rotor group consisting of water-repellent water cooling blades 87 that compress compressed air in a substantially linear meandering manner as a full blade airfoil having an increased blade interval by using all blades. 17 is made into an integral casting 84 in which the compressor blades for each paragraph are annularly formed. An annular integrated casting 84 assembly structure capable of full-automatic processing is connected to the water channel of the cooling means 55 at the annular casting assembly connection, and a water injection means 56 is provided near the assembly annular connection.
[0075]
The water repellent water cooling blades 87 and the like of the outer compressor rotor blade group 16 and the inner compressor rotor blade group 17 of the main part of the full rotor compressor are water-cooled by the water supply 3 by a cooling means 55 (not shown), and the water is supplied. The compressed air is directly cooled by injecting it from the water injecting means 56 to reduce the volume as low-temperature air and compress the most efficiently water-cooled low-temperature air. The high-pressure combustion heat exchange heat is recovered by the combustor / heat exchanger 4 as much as possible using the heat-recovered feed water 3 and the low-temperature compressed air to lower the combustion gas inlet temperature of all the bladed steam gas turbines to the minimum, and the same fuel amount is obtained. The recovered combustion gas calorie is converted to high-temperature water 5a such as supercritical pressure, which is about twice as much as the existing boiler.
[0076]
Combustion and heat exchanger 4 assures high-pressure combustion heat exchange and recovers heat, reduces combustion gas exhaust temperature to -273 ° C, minimizes temperature and volume disturbances, and doubles compressed air pressure compared to existing gas turbines It can burn 10 times more fuel than existing gas turbines up to stoichiometric air-fuel ratio. The total heat value of the conventional quadruple fuel obtained by the heat exchange plus -273 ° C. or more of the compressed air is recovered as supercritical pressure high-temperature water, etc., with the same fuel amount recovered as about twice as much as the existing boiler. To do.
[0077]
When the storage pressure of the high-temperature water 5a such as supercritical pressure rises, a normal output is generated by opening the high-temperature water control valve 7a to generate a normal output. Is supplied to the uppermost stream of the full-blade steam gas turbine, the entire lowest-temperature combustion gas 10 is supplied to the middle-stage optimum stage, and the full-blade steam gas turbine including the full-blade compressor is driven. In the process of generating output depending on the application, low temperature water is injected to cool combustion gas, etc., energy is converted to the speed power of water mass, optimal deceleration, combustion gas etc. is exhausted at low temperature, and the hollow part of the inner shaft device In the process of generating power for injecting and propelling the air at the outer periphery of the outer shaft device and the outer shaft unit, the water is agglomerated with the low-temperature combustion gas as the nucleus, and the exhaust gas such as CO2 is sealed in water droplets to burn CO2 gas etc. Bring gas exhaust close to zero.
[0078]
High-temperature water 5a having a supercritical pressure of 19/24 is supplied to each high-temperature water reservoir 32a from a plurality of high-temperature water control valves 7a by a five-fold drop of an existing gas turbine, and a plurality of spraying principles including known techniques Utilizing the hot water 91a, a high-temperature water is supplied from a high-temperature water injection nozzle 59a having a barrel shape or a divergent barrel shape, in which a vaporizing film is provided between the high-temperature water and the high-temperature water by the heating high-temperature means 101 to minimize friction loss. Similar to explosive explosion, high-temperature water is accelerated inside the nozzle like a machine gun bullet, and outside the nozzle, high-temperature water is accelerated like a shot rocket, drawing air in front of the nozzle in multiple stages. Injection is performed at an optimal speed, and bypass injection is performed by each special device 92a that performs injection and propulsion including air suction force. Injection and propulsion is performed at 10 times the injection speed of existing gas turbines according to the application.
[0079]
The process of jet propulsion of jet aircraft, airships, flying objects, etc. is directly converted into velocity energy of air mass, air is sucked most efficiently at a high speed far exceeding the ramjet, and jet propulsion is performed at a jet speed of about 10 times. You. By increasing the storage pressure of the high-temperature water 5a such as supercritical pressure, it is possible to promote very safe injection propulsion, reduce the fuel loading to 1/10, etc., reduce the usage to 1/100, etc., and cause a fire. Is reduced to 1/100, etc., and even in the event of a fire, the high-temperature water 5a is sprayed to make it easier to extinguish the fire, making it a very safe jet, airship or flying object.
[0080]
A part of the high-temperature water 5a having a supercritical pressure or the like and all the combustion gas drive the all-blade steam gas turbine to drive the all-blade compressor, suction the air in front and inject and propell. The high-temperature water 5a is bypass-injected by a special device 92a at a large head far beyond the ramjet by utilizing a plurality of spraying principles 91a including a known technology, and the air in front of each is suctioned in multiple stages. The mass velocity due to high-temperature water vaporization explosion energy such as supercritical pressure is directly converted to velocity energy of air mass to optimally decelerate and inject large-mass most efficiently at the optimal injection velocity. It is the one that applies power to promote optimal injection.
[0081]
In order to reduce the emission of combustion gas such as CO2 to zero, in a full-blade steam gas turbine including injection propulsion, for example, a part of the high-temperature water 5a of 5/24 and all of the combustion gas 10 include a full-blade compressor. An output that drives the full-blade steam gas turbine to exhaust the combustion gas, high-temperature water 5a, and water vapor 5 at the lowest temperature, and to suck and inject air from the hollow portion of the inner shaft device and the outer peripheral portion of the outer shaft device to jet and propell. In the process of generation, low-temperature water is injected depending on the application to lower the water temperature at which the low-temperature combustion gas is condensed on the nucleus. To supply water drops.
[0082]
High-temperature water 5a having a supercritical pressure of about 19/24 or the like is supplied to each high-temperature water reservoir 32a from a plurality of high-temperature water control valves 7a by a five-fold drop of an existing gas turbine or the like, and a plurality of sprays including a known technique are provided. Utilizing the principle 91a, the heating high temperature means 101 sets the heating high temperature, and a vaporizing film is provided between the high temperature water and the friction loss is minimized. Then, high-temperature water is accelerated like a machine gun bullet, and outside the nozzle, high-temperature water is accelerated like a shot rocket, and the air in front is suctioned in multiple stages and injected at the optimum speed, including the air suction force. Injection propulsion is carried out at 10 times the injection speed of existing gas turbines, etc., according to the application by each special device 92a for injection propulsion.
[0083]
Also in the third embodiment of the all-blade steam gas turbine combined engine shown in FIG. 4, at the time of startup, a valve (not shown) is opened and closed to supply the combustion gas 10 to the high-temperature water reservoir 32a and generate an output. Used as a gas turbine. When the pressure of the supercritical pressure high-temperature water or the like in the combustor / heat exchanger 4 rises, the combustion gas 10 is switched to the high-temperature water 5a, the valve is closed and the high-temperature water control valve 7a is opened, and the supercritical pressure high-temperature water or the like is opened. A part of the turbine drives a full-blade steam turbine, including a full-blade compressor, to exhaust high-temperature water and vaporized explosive steam to generate air intake output and injection propulsion output.
[0084]
The entire combustion gas 10 is bypass-injected by each of the special devices 92b by using a plurality of spraying principles 91b, and the forward air is suctioned in multiple stages to produce injection propulsion. Most of the remaining high-temperature water 5a is bypass-injected by each of the special devices 92a by using a plurality of spraying principles 91a, and the air in front is suctioned in multiple stages, so that the injection speed is 10 times the ram jet speed or the like. Injection and propulsion with air suction output and injection propulsion output, each output will be 120-240 times the hypothetical output of existing gas turbines, such as jet aircraft, airships and space shuttle parent aircraft.
[0085]
Water-repellent water cooling blades 87 and the like of the outer compressor rotor blade group 16 and the inner compressor rotor blade group 17, which are the main parts of the full rotor compressor, are boosted by the water pump and the contra-rotating magnetic friction power transmission device 14a. The cooling water 55 is passed through the cooling means 55 to cool the water, and the supplied water is injected from the water injection means 56 to directly cool the compressed air, and the heat is recovered to reduce the air volume as the supplied water. An outer compressor driven by a water-repellent water cooling blade 87 that compresses compressed air in a substantially linear meandering manner and compresses low-temperature air most efficiently as an all-blade airfoil having an increased blade interval by using all blades. The blade group 16 and the inner compressor blade group 17 are formed into an integral casting 84 in an annular shape for each paragraph.
[0086]
An annular integrated casting 84 assembly structure capable of full-automatic processing is connected to the water channel of the cooling means 55 at the annular casting assembly connection, and a water injection means 56 is provided near the assembly annular connection. After cooling the water-repellent water cooling blade 87 in the water channel of the cooling means 55, the water jetting means 56 performs water jet direct contact air cooling, cools the water supply most efficiently, and compresses the low-temperature air. The high-pressure combustion heat is exchanged by the combustor / heat exchanger 4 as much as possible with the heat-recovered feed water 3 and the low-temperature compressed air to recover about twice the heat of the existing boiler, and the annular combustion gas reservoir of the all-blade steam turbine. 9. Reduce the combustion gas temperature to the minimum according to the application.
[0087]
Rotary power engines driven by dynamic pressure or reaction such as all-rotor steam turbines can be designed rationally even with large heads and gravitational power, such as supercritical high-temperature water, to increase the dynamic pressure output. The most important thing is to increase the maximum atmospheric pressure unitary gravity power by 1700 times, to reduce a part or most of the blade area to 1/1700, and to design a reasonable whole blade. To
[0088]
A part of the supercritical pressure high-temperature water and the like obtained by heat exchange drives the all-blade steam turbine including the all-blade compressor, and uses high-temperature water and water vapor 5 of vaporized explosion exhaust as the injection driving force. It sucks air in front of the hollow part of the device and in front of the outer periphery of the outer shaft device, and uses the air suction force and the jet mass velocity as propulsion. All of the combustion gas 10 and the remaining high-temperature water 5a are bypass-injected by the respective special devices 92b and 92a using the respective spraying principles 91b and 91a, and the forward air is suctioned in multiple stages, respectively. Is directly converted into the velocity energy of the air mass, and injected at 10 times the injection mass velocity of the existing gas turbine, and the water is agglomerated by using the low-temperature combustion gas as a nucleus to reduce a part or a large part of the volume to 1/1700. And so on, and supersonic passenger aircraft with exhaust noise as low as 1/10.
[0089]
The heat is recovered by exchanging high-pressure combustion heat as much as possible in the combustor / heat exchanger 4, the temperature of the combustion gas at the combustion gas outlet 88 is reduced to the minimum, and the amount of recovered heat about twice that of the existing boiler is reduced to the supercritical pressure. The maximum amount of recovered heat such as high-temperature water increases, and heat exchange is performed to obtain (combustion gas calorie output 100 to 200 times output) + (combustion gas mass output 20 to 40 times output) = (120 to 240 of existing gas turbine) Double hypothesis output).
[0090]
Part of the supercritical high-temperature water 5a is supplied to the uppermost stream of the all-blade steam turbine, and water is injected according to the application in the process of generating power to cool the vaporized explosion steam. Atmospheric pressure is converted to gravitational power of 1700 times and decelerated to the optimum speed to generate the rotation output most efficiently. Then, using the respective spraying principles 91a and 91b, the remaining high-temperature water 5a and the combustion gas 10 are bypass-injected at 10 times or 5 times the speed of the existing gas turbine, respectively, and in the process of outputting 100 times or more, Water is agglomerated by using low-temperature combustion gas as a nucleus to generate hail and water droplets, and the emission of combustion gas such as CO2 approaches zero.
[0091]
In the fourth embodiment of the combined rotor blade steam gas turbine engine shown in FIG. 5, the outer compressor rotor blade group 16 and the inner compressor rotor blade group 17 are integrally cast 84 in each stage as a full blade airfoil, and are fully automatic. It has an assembly structure that can be machined. The water channel of the cooling means 55 is connected at the annular casting assembly connection part, and a water injection means 56 is provided near the assembly annular connection part. Then, half or all of the paragraphs or a plurality of paragraphs of the water-repellent water cooling blades 87 of the full blade compressor are passed through the cooling means 55 to be water-cooled, and the water is injected from the water injection means 56 to be compressed. The air is cooled by direct contact water cooling, and the heat is most efficiently recovered by the feed water 3 and supplied to the combustor / heat exchanger 4 by a water feed pump and a contra-rotating magnetic friction power transmission device 14a. Is compressed and supplied to the combustor / heat exchanger 4.
[0092]
The high temperature combustion heat exchange heat is recovered by the combustor / heat exchanger 4 as much as possible using the heat-recovered feed water 3 and the low-temperature compressed air to lower the temperature of the combustion gas outlet 88 to a minimum, and the same fuel amount of the existing boiler 2 The combustion gas calorie output of about twice the recovered calorie is supplied as supercritical high-temperature water 5a, etc., and a part of it is supplied to the uppermost stream of the all-blade steam turbine where unit gravity power is important depending on the application, and the power generation process Water vapor is sprayed depending on the application to cool the vaporized explosion steam, and a part of the steam velocity is converted to atmospheric pressure 1700 times the unit volume gravity power to decelerate optimally, generate rotational output most efficiently, and operate fully by rotational output The wing compressor is driven, and the exhaust injection output is the levitation propulsion output of ships, etc.
[0093]
The entire combustion gas 10 and the remaining supercritical high-temperature water 5a are suctioned and injected in multiple stages by using the respective spraying principles 91c and 91d, and the respective velocities are directly converted to the velocity mass of the water. Each high-speed ship and various high-speed water-moving equipment are propelled by one or more water injection devices 93a and 93b, each of which converts energy to optimal deceleration and suctions and jets a large amount of water most efficiently.
[0094]
In the process of sucking and injecting water forward in multiple stages using the principle of spraying 91d and spraying all of the combustion gas 10 and directly converting the energy into water velocity / mass, the combustion gas 10 approaches the atmospheric pressure of -273 ° C. Therefore, even in the process of dissolving combustion gas such as CO2 in a large amount of seawater by cooling seawater etc. and supplying it as cold heat to the sea floor etc., air and oxygen etc. are sucked into the sea using the principle 91d of spraying. Supply and thoroughly study the ecology of marine organisms down to microorganisms, breed microorganisms, fish and shellfish, seaweeds and seaweeds, increase food production, and reduce CO2 and other combustion gas emissions to zero.
[0095]
The water feed pump and contra-rotating magnetic friction power transmission device 14a will be described with reference to FIGS. Various power transmission devices including normal speed change and reverse rotation mainly use a gear device. For this reason, in order to require a sliding tooth surface including a large load on the tooth surface, in addition to requiring lubricating oil, friction heat loss is also very large, and transmission equipment for large power including high speed rotation is required. There is a problem that it cannot be used.
[0096]
For this reason, an ultra-high-speed, large-power transmission device by rolling contact is indispensable in order to commercialize an all-blade steam gas turbine combined engine. In order to enable an ultra-high-speed large-power transmission device and eliminate the need for lubricating oil, water-cooled frictional heat of rolling contact with the sliding tooth surface of the gear unit approaching zero was recovered and combined with combustion and heat. It is used as a water supply pump and a contra-rotating magnetic friction power transmission device 14a for supplying a multi-stage, multi-high pressure, small amount of water to be supplied to the exchanger 4, and combining an outer shaft device and an inner shaft device rotating in opposite directions to each other, It is also used as a high-pressure, small-volume water pump, recovering heat and sending water.
[0097]
For this reason, the rolling contact power transmission device is provided as the low unevenness 40 in which the meshing height of the gear is reduced as much as possible, and the bar magnet 33 or the electromagnet 34 is provided on the upstream and downstream sides in the rotation direction 35 or on the upstream or downstream side. You. Utilizing the strong attractive force of the magnet, various magnetized friction wheel devices 51, various magnetic friction wheel devices 90 not shown, various internal magnetized friction wheel devices 49, and various internal magnetized friction devices not shown Enables all meshing uses such as car equipment 89.
[0098]
Various water supply pumps and various contra-rotating magnetic friction power transmission devices 14a for ultra-high pressure small-volume water supply are provided, and a water suction passage 95 and a water supply passage 96 are provided in the outer box 94. Use That is, a water pump and a magnetic friction power transmission device for transmitting ultra-high-speed and large power, which is close to the rolling contact, greatly reduces frictional heat loss, and also collects self-heating as the water supply pump 97 for supplying a very small amount of ultra-high pressure water. 100a, a water pump and a contra-rotating magnetic friction power transmission device 14a, and a water pump that uses non-polluting water cooling instead of lubricating oil to recover heat and supply it to the combustor / heat exchanger 4 side. It is a counter-rotating magnetic friction power transmission device 14 that is also used for 97.
[0099]
Because it is a counter-rotating magnetic friction power transmission device 14 that transmits ultra-high-speed large power, generation of frictional heat is unavoidable even when approaching rolling contact. On the other hand, all-blade steam gas turbine combined engine transmits water at ultra-high speed and large power, and uses ultra-high pressure and small amount of water and large amount of heat to generate power. 97 is required.
[0100]
Therefore, instead of various gears, various types of magnetic friction wheels 37, various types of internal friction wheels 38, various types of magnetic friction wheels 39, various types of internal magnetic friction wheels 44 (not shown), and the like are used. In the process of use as the power transmission device 14, by providing the bar magnet 33 to the electromagnet 34 on the upstream and downstream sides or on the upstream or downstream side in the rotation direction, a magnetized friction wheel, a magnetized friction wheel, and an inner magnetized friction wheel are provided. Various water pumps and contra-rotating magnetic friction power transmission devices 14a and various water pumps that enable all combinations of vehicles and inner magnetic friction wheels to be used interchangeably with each other by the strong attraction of magnets. Used as magnetic friction power transmission device 100a.
[0101]
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 is provided with low irregularities 40. The low asperity 40 reduces the meshing height as much as possible, enabling shapes other than gears as rolling contact, and all meshing shapes not shown in the figure. Specifically, as the gear type low unevenness 40, 41 flat unevenness is provided in place of the spur gear, 42 helical unevenness is replaced in place of the helical gear, and 43 yamabe unevenness is replaced in place of the yamaba gear.
[0102]
Alternatively, a spur inner unevenness 41a wheel is provided instead of a spur internal gear not shown, a helical inner unevenness 42a wheel is replaced with a helical internal gear, and a yamaba inner unevenness 43a wheel is provided instead of a yamaba internal gear. As in the case of various known gear pumps, an outer box 94, a water suction passage 95 and a water supply passage 96 are provided, and a super-high-speed and large power is transmitted as a water supply pump 97 that collects frictional heat and supplies an ultra-high pressure and small amount of water. Used as various water pumps and contra-rotating magnetic friction power transmission device 14a and various water pumps and magnetic friction power transmission device 100a.
[0103]
In the embodiment of the magnetized friction wheel 37a shown in FIGS. 6a and 6b, the north and south poles of the magnetic poles are magnetized on the left and right sides in the radial direction of a ring-shaped ferromagnetic material, and both sides thereof are ring-shaped yoke. 47, it is extended and fixed to the outer radial power transmission surface 31. On the outer peripheral surface of the power transmission surface 31, flat irregularities 41 of the low irregularities 40, boss irregularities 42, and the like are provided, and the respective components are interchangeable as magnetized friction wheels 37a, 37a. A magnetized friction wheel 39 and a rolling contact magnetized friction wheel device 51 are provided with an outer box 94, a water absorption channel 95, a water supply channel 96, and the like, similarly to the magnetized friction wheel device 51c + 97 of FIG. 7 and 97 + 14 of FIG. Used as various water pumps and contra-rotating magnetic friction power transmission device 14a and various water pumps and magnetic friction power transmission device 100a.
[0104]
In the embodiment of the magnetized friction wheel 37b of FIG. 6C, the N pole and the S pole of the magnetic poles are magnetized on the inner and outer diameter sides of the annular cylindrical ferromagnetic material, and the yoke 47 is moved from the inner circumference side of the magnet. Extends to the right and left outer diameter power transmission surface 31. A friction increasing means 45 is annularly provided and fixed between the yoke and the magnet in the vicinity of the power transmission surface, and the Yamaba irregularities 43 of the low irregularities 40 are provided on the outer peripheral surface thereof, as magnetized friction wheels 37b and 37b, respectively. The outer box 94, the water absorption passage 95, the water supply passage 96, and the like are formed in the same manner as the magnetized friction wheel 39 and the magnetized friction wheel 37b, and the magnetized friction wheel device 51d + 97 in FIG. 8 and 97 + 14 in FIG. It is installed and used as various water pumps and contra-rotating magnetic friction power transmission device 14a and various water pumps and magnetic friction power transmission device 100a.
[0105]
In the embodiment of the magnetically attached friction wheel 39 shown in FIGS. 6d, 6e and 6f, a friction increasing means 45 is provided on the power transmission surface 31 of the outer diameter surface of the annular ferromagnetic material. Alternatively, the power transmission surface 31 is provided with flat irregularities 41 of low irregularities 40, boss irregularities 42, or Yamaba irregularities 43 on the outer peripheral surface thereof, so that various magnetically-attached friction wheels 39, 39, etc. are respectively provided. As shown in FIGS. 7 and 8 and FIG. 9, by providing the bar magnet 33 or the electromagnet 34 on the upstream side and the downstream side in the rotational direction, the respective elements are interchangeable with each other, and various types of magnetic friction of rolling contact without a figure are provided. The vehicle device 90 and various magnetic friction power transmission devices 100 are used.
[0106]
Alternatively, a friction increasing means 45 is provided on the power transmission surface 31 of the inner diameter surface of a ring-shaped ferromagnetic material not shown. Alternatively, the power transmission surface 31 is provided with flat irregularities 41 of low irregularities 40, boss irregularities 42, or yamaba irregularities 43 on the inner peripheral surface thereof to form various inner magnetized friction wheels 44, 44 and the like, respectively. The respective elements are interchangeable with each other to form various inner-magnetized friction wheel devices 89 of rolling contact and the like, and similarly to the contra-rotating magnetic friction power transmission device 14 of FIGS. A water absorption passage 95 and a large number of water supply passages 96 are provided and used as a water supply pump and a contra-rotating magnetic friction power transmission device 14a and a water supply pump and a magnetic friction power transmission device 100a.
[0107]
For example, in the first embodiment and the second embodiment of the various water pump / magnetic friction power transmission device 100a shown in FIGS. 7 and 8, the outer case 94 is provided in the magnetized friction wheel devices 51c and 51d similarly to the existing gear pump. A water supply pump 95 is provided for each of them, and various water supply pumps 97 are configured and used. Then, the water supply 3 is supplied from the water intake passage 95 to collect the heat generated in the various magnetic friction power transmission devices 100, and is supplied from the water supply passage 96 to the combustor / heat exchanger 4 side.
[0108]
However, due to the large number of various water pumps and the magnetic friction power transmission device 100a, such as the magnetized friction wheel devices 51c and 51d, the rotation speed also changes because the main power is the power transmission when the water pump is also used. Therefore, a known control device optimally controls one or more water supply passages 96 and water absorption passages 95 and supplies the water to the water injection means 56 and 56a in the process of increasing the pressure in one or more stages. Supercritical high temperature water 5a etc. That is, various water supply pumps and counter-rotating magnetic friction power transmission devices 14a, which collect frictional heat by one or more water supply pumps 97, perform self-water cooling, and transmit ultra-high pressure small amount water while transmitting ultra-high speed and large power, Used as various water pumps and magnetic friction power transmission device 100a.
[0109]
For example, the water supply pump and contra-rotating magnetic friction power transmission device 14a that transmits ultra-high speed and large power as shown in FIG. Since the water passage 96 and the numerous magnetized friction wheels 37a and the inner magnetized friction wheels 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, the peripheral speed of the same peripheral speed is merged. In this case, the pressure is controlled by increasing the pressure in two or multiple stages, and combined with another water pump according to the application. Water to the combustor / heat exchanger 4 side. It is used as various contra-rotating magnetic friction power transmission devices 14 that also serve as a water supply pump 97, which collects frictional heat with a number of water supply pumps 97, self-cools the water, and transmits ultra-high speed and large power.
[0110]
This will be described with reference to FIGS. 9 (a), 9 (b) and 9 (c). (B) and (c) are cc and dd views of (a), respectively, and show the rotational power of the inner shaft device and the outer shaft device of the combined rotor blade steam gas turbine combined engine rotating in opposite directions. The contra-rotating magnetic friction power transmission device 14 that combines the two will be described with reference to the embodiment of FIG. Fig. 9 (a) is used as a contra-rotating magnetic friction power transmission device 14 that collects frictional heat by a number of water pumps 97, self-cools the water, and transmits ultra-high speed and large power.
[0111]
The rotation of the first driven inner magnetized friction wheel 38a, including the magnet part 46 and the yoke 47, fixed to the outer shaft device of the all-blade steam gas turbine combined engine, rotates the shaft on the outer box 94 fixed to the engine body. The plurality of first driven magnetized friction wheels 37a fixed to the left end of the support shaft 50 are rotated, and the plurality of second driven magnetized friction wheels 37a fixed to the right end of the support shaft 50 are rotated by the rotation. The second driven magnetized friction wheel 37a, which rotates and is fixed to the inner shaft device by the rotation, rotates and combines the rotational force of the outer shaft device and the rotational force of the inner shaft device which rotate in opposite directions to each other. , Full rotation output from inner shaft device or outer shaft device, or rotation output from both.
[0112]
FIGS. 9 (b) and 9 (c) show the upstream and downstream sides in the rotational direction in the process of using as the contra-rotating magnetic friction power transmission device 14 which also serves as the water supply pump 97 and which transmits ultra-high-speed large power and water supply at a very high pressure and a small amount. Alternatively, by providing the bar magnet 33 to the electromagnet 34 on the upstream side or the downstream side, 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 can be used. By the strong attraction of the magnet, it can be used interchangeably. Like the existing gear pump, the outer case includes an inner magnetized friction wheel 38a fixed to the outer shaft device, a magnetized friction wheel 37a fixed to the inner shaft device, and a plurality of magnetized friction wheels 37a meshing with each other. 94 is provided.
[0113]
A plurality of magnetized friction wheels 37a meshing with the inner magnetized friction wheel 38a are provided with a water supply channel 96 on the upstream side including the rotating bar magnet 33, and a water absorption channel 95 provided on the downstream side including the rotating bar magnet 33, A water passage 96 is provided upstream of the plurality of magnetized friction wheels 37a meshing with the magnetized friction wheel 37a fixed to the inner shaft device, including the rotation direction electromagnet 34, and a water absorption path 95 is provided on the downstream side including the rotation direction electromagnet 34. It constitutes a water pump 97 and a contra-rotating magnetic friction power transmission device 14a that transmits ultra-high speed and large power.
[0114]
FIG. 10 illustrates prevention of global warming according to the present invention. At thermal power plants around the world, for example, supercritical superheated steam heated by a boiler is adiabatically expanded by a steam turbine, and the seawater temperature rises with the entire amount of heat heated by the boiler, using only the volume and no heat at all. When adiabatic expansion from supercritical pressure superheated steam to condenser vacuum is used to increase the volume, the volume exceeds 10,000 times and the gravitational power becomes 1 / 10,000 or less, and the blade area of 10,000 times or more is required for the same output. For this reason, it is inevitable that global warming will be accelerated due to the unreasonable design.
[0115]
The most devastating is that the speed energy is consumed 10 to 20 times that of the moving blade, and half of the stationary blades that do not perform any rotating work are provided, and the speed of the superheated steam is blocked to reduce the speed. is. Therefore, in order to effectively utilize the heat, the gas turbine combustor is also used as a heat exchanger, and the all-blade steam gas turbine combustor / heat exchanger 4 performs high-pressure combustion heat exchange infinitely to reduce the combustion gas exhaust temperature. When the temperature approaches -273 ° C, enormous cold energy can be obtained as a by-product at a production cost of approximately 0, and in addition, combustion gas exhaust such as CO2 can be reduced to 0, etc., and the amount of recovered heat, which is about twice that of existing boilers, can be increased. It can be recovered as critical pressure high-temperature water and used as combustion gas calorie output, greatly increasing combustion gas mass output.
[0116]
Therefore, the heat quantity of the supercritical pressure high-temperature water 5a, which is about twice that of the existing boiler, is supplied to the uppermost stream of the all-blade steam turbine, and the supercritical pressure high-temperature water 5a having the gravity power of 1700 times that of the existing atmospheric reheat steam turbine is supplied. In the nozzle, which minimizes friction loss by providing a vaporizing film between the heating high temperature and high temperature water, the high temperature water is accelerated like a machine gun bullet by the vaporization explosion force, and the high temperature water is shot outside the nozzle. By accelerating like a rocket, the gravity work rate approaches 1700 times, and the combustion gas calorie output + combustion gas mass output increases to 500 times the hypothetical output of an existing gas turbine with the same fuel amount.
[0117]
In order to collect and utilize all the heat added in the full-rotor steam turbine, which briefly describes the by-product of the all-rotor steam turbine, a vaporization latent heat recovery unit 66a is provided in substantially the same manner as the existing condenser, and for example, a saturation temperature of 100 ° C. After converting the heat of vaporization into seawater and cooling it with tap water, recovering the heat, all of the enormous vaporization heat obtained is stored at around 100 ° C with tap water heated to near 100 ° C as the heating cost of the by-product manufacturing cost. Supply high-temperature tap water to consumers along with a large amount of electricity to expand demand explosively. The entire condensed water is circulated and supplied to the combustor / heat exchanger 4 infinitely repeatedly, so that the combustor / heat exchanger 4 supplies only high-temperature water vaporization explosion energy and minimizes the fuel combustion mass. In addition, we will completely eliminate the useless technology of the existing technology, which had raised the seawater temperature with all the heat of vaporization.
[0118]
The combustion blade and heat exchanger 4, which briefly describes the by-products of the full-blade steam gas turbine, exchanges high-pressure combustion heat as much as possible to bring the combustion gas exhaust temperature close to -273 ° C. Water is coagulated around the nucleus to collect enormous cold energy of all combustion gas + α, and cools and stores tap water as cold energy with a production cost of almost 0 by-products. In addition to completely eliminating commercial and household coolers and cooling entire urban areas, the use of chlorofluorocarbons to prevent global warming and eliminate CO2 and other combustion gas emissions.
[0119]
Various devices that are driven by the rotational force and the injection output of the various combined rotor blade steam gas turbine engines shown in FIG. 11 will be described. Combined all-blade steam gas turbine engine with combustion gas exhaust temperature approaching -273 ° C, adiabatically expanded to condenser vacuum, aggregating water with low-temperature combustion gas as nucleus, and separating and collecting as hail and water droplets Drives various power generation facilities, various heat and electricity and cold heat supply facilities, various heat and electricity supply facilities, etc.
[0120]
A variety of automobiles with all-blade steam gas turbine combined engines that bring the combustion gas exhaust temperature close to -273 ° C, adiabatically expand to atmospheric pressure, coagulate moisture with low-temperature combustion gas as the core, and enable separate collection as water droplets -Drives various vehicles, various machines, various general-purpose engines, various tanks, etc.
[0121]
The exhaust temperature of the combustion gas is approached to -273 ° C, and one or more of steam and combustion gas is bypass-injected using the principle of spraying, adiabatically expanded to atmospheric pressure, and water is agglomerated with the core of the low-temperature combustion gas to form water droplets. All kinds of ships, various high-speed ships, various types of aircraft, various types of ships, various types of fighters, various types of space shuttle parent aircraft, various types of supersonic aircraft, various types of aircraft, etc. To do.
[0122]
【The invention's effect】
Since the supercritical pressure high-temperature water is used, the atmospheric gravity gravitational power is brought close to 1700 times, and there is an effect that the same fuel amount is increased to 500 times the hypothetical output of the existing gas turbine.
[0123]
Atmospheric pressure gravitational power is approached to 1700 times, and a part or most of the blade area is reduced to 1/1700 to use supercritical high-temperature water, and a reasonable blade area can be designed. Has the effect of doing
[0124]
In order to use supercritical high-temperature water, a high-temperature means is used to heat the high-temperature water, and a high-temperature water injection nozzle is used to form a vaporization film between the high-temperature water and the nozzle. In this case, high-temperature water is accelerated like a bullet of a machine gun, and outside the nozzle, it is accelerated like a shot rocket, which has the effect of increasing the output of the same fuel to 500 times the hypothetical output of an existing gas turbine.
[0125]
The electromagnetic heating turbine rotor blade 81 and the electromagnetic heating nozzle 83 are provided with a vaporized film between the electromagnetic heating high temperature and the high temperature water to minimize friction loss, so that the most efficient output is produced.
[0126]
The electromagnetically heated outer turbine blade group 19 and the electromagnetically heated inner turbine blade group 20 are integrally cast in a ring for each paragraph, which has the effect of easily and reliably raising the electromagnetic heating temperature.
[0127]
The casting of the water injection means 56a, which is provided insulated, has the effect of cooling the combustion gas and vaporized explosion water vapor by water injection, and has the effect of easily increasing the unit volume mass and the total mass easily.
[0128]
Even if the combustion gas exhaust temperature is approached to -273 ° C and a large unit gravity power or a total gravity power is used, it has the effect of generating a large output with minimal friction loss between the electromagnetically heated turbine blades and high-temperature water.
[0129]
By exchanging low-temperature and high-pressure air with high-pressure combustion heat using a combustor and heat exchanger, the fuel combustion mass is increased to about four times that of existing gas turbines up to the stoichiometric air-fuel ratio. Since the temperature of the combustion gas inlet and the temperature of the combustion gas outlet of the combustor / heat exchanger are minimized, the compression pressure can be raised to about 10 MPa or more, which is about twice as high.
[0130]
Approximately twice or more of compressed air -273 ° C or more is added to the calorific value of the combustion gas obtained by heat exchange, so that the same calorific value of the combustion gas calorie that is about twice that of the existing boiler can be recovered as supercritical high-temperature water or the like. There is.
[0131]
As supercritical pressure high-temperature water, it has the effect of driving the all-blade steam gas turbine, all-blade steam turbine, and special devices 92a and 92b to suck air in the most efficient manner and propulsion.
[0132]
It has the effect of driving the all-blade steam gas turbine, all-blade steam turbine, and water injectors 93a and 93b as the supercritical high-temperature water, etc., and sucking water most efficiently to promote injection.
[0133]
With the combustion gas exhaust temperature approaching -273 ° C, the combustion gas mass output of the combined turbine and steam gas turbine combined engine with the same fuel consumption of 0 or less was increased to 20 to 40 times the hypothetical output of the existing gas turbine. Has the effect of doing
[0134]
The water jet vaporization explosion steam and combustion gas are cooled and converted to high-speed water mass velocity power for optimal deceleration. This has the great effect of making it possible to design a compact all-blade steam gas turbine engine.
[0135]
By exchanging heat at high pressure with a combustor and heat exchanger as much as possible, and recovering twice as much heat as an existing boiler, it reduces electricity costs and reduces global warming such as CO2 emitted from power plants. It also has the effect of most efficiently recovering the combustion gas.
[0136]
Eliminating business and household coolers also has the effect of preventing global warming by eliminating CFCs.
[0137]
As the amount of power generation increases, the production of cryogenic combustion gas increases, so cooling seawater has the effect of supplying CO2, nitrogen and oxygen to the seabed, breeding and activating seaweed and fish. It is effective for everyone to think about ways to contribute to humanity by reversing the mistake that only money making can feel as a corporate activity.
[0138]
Combustion and heat exchangers of all-blade steam gas turbine combined engines, exchanging high-pressure combustion heat as much as possible to reduce the fuel combustion mass up to the stoichiometric air-fuel ratio to about four times that of existing gas turbines and increase the combustion gas inlet temperature Has the effect of enabling the compression pressure to be 10 MPa or more, which is about twice as high.
[0139]
Water-cooled combustion gas and high-temperature water vaporized explosion steam obtained by heat exchange, and the maximum gravitational power can maximize the mass of high-temperature water with an atmospheric pressure of 1700 times and a vacuum section of 10,000 times or more of the existing steam turbine at maximum. It has an effect.
[0140]
There is a great effect that the output can be generated by a large dynamic pressure, such as 1700 times the atmospheric pressure part and 10,000 times the vacuum part of the superheated steam of the existing steam turbine.
[0141]
By increasing the gravitational power to 1700 times the atmospheric pressure section or 10000 times the vacuum section, part or most of the turbine blade area can be reduced to 1/1700 or 1/10000, etc., greatly simplifying the structure. There is a big effect that can be done.
[0142]
The reheating of the existing reheat steam turbine and the stationary blades are completely eliminated, and this has a great effect that the structure can be simplified and all the blades can be made to have a large output.
[0143]
In the process of generating power in an all-blade steam gas turbine or a combined all-steam steam gas turbine engine, the adiabatic expanded low-temperature combustion gas is used to cool the water injection vaporized explosion steam and combustion gas and increase the mass of high-temperature water. Water is agglomerated with nuclei, and as a natural phenomenon, as a hail and water droplets, in the process of synthesizing, dissolving and mixing combustion gas such as CO2 into a huge amount of water, there is also an effect that it can be emitted harmlessly by adding substances. .
[0144]
It emits CO2 and other polluting combustion gas exhaust gas emitted from various vehicles, various ships, various airplanes, and various mechanical devices as hail and water droplets, which has the effect of significantly reducing CO2 and other exhaust gas.
[Brief description of the drawings]
FIG. 1 is a partial sectional view showing a first embodiment of an all-blade steam turbine.
FIG. 2 is a partial cross-sectional view showing a first embodiment of the combined rotor blade steam gas turbine engine.
FIG. 3 is a partial cross-sectional view showing a second embodiment of the combined rotor blade steam gas turbine engine.
FIG. 4 is a partial cross-sectional view showing a third embodiment of the combined rotor blade steam gas turbine engine.
FIG. 5 is a partial cross-sectional view showing a fourth embodiment of the combined rotor blade steam gas turbine engine.
FIG. 6 is a partial sectional view showing an embodiment of a magnetic friction wheel and a magnetic friction wheel.
FIG. 7 is a partial cross-sectional view of the first embodiment of the water pump and the magnetic friction power transmission device.
FIG. 8 is a partial sectional view of a second embodiment of the water pump and the magnetic friction power transmission device.
FIG. 9 is a partial sectional view of an embodiment of a water pump and a contra-rotating magnetic friction power transmission device.
FIG. 10 is an explanatory diagram for preventing global warming in a combined rotor blade steam gas turbine engine.
FIG. 11 is an explanatory view showing a device driven by a combined rotor blade steam gas turbine engine.
[Explanation of symbols]
1: water supply pipe 2: feed water pump 3: feed water 4: combustor and heat exchanger 5: steam 5a: high-temperature water 6: steam pipe 6a: high-temperature water pipe 7: steam control valve 7a: high-temperature water control valve 8: annular compression 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 group 19: Electromagnetic heating outer turbine rotor group 20: Electromagnetic heating inner turbine rotor group 21: Annular outlet 22: Annular socket 23: Annular socket
24: annular electromagnetic heating nozzle group 25: combustor outer box 26: water-cooled outer wall
27: Fuel vapor supply means 28: Bypass 31: Power transmission surface 32: Superheated vapor reservoir 32a: High temperature water reservoir 33: Bar magnet 34: Electromagnet 35: Rotating direction 36: Magnetic pole 37: Magnetized friction wheel 38: Inner magnetized friction wheel 39: Magnetized friction wheel 40: Low irregularity 41: Flat irregularity 42: Hasp groove irregularity 43: Yamaba irregularity 44: Inner magnetized friction wheel 45: Friction increasing and durable 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: Flange 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 cylinder port 59a: High-temperature water injection nozzle 60: Fuel injection port 61: Needle valve 62: Fuel small hole
63: fuel hole switch 64: air hole switch 65: air hole 66: condensed water heat exchanger 66a: vaporized latent heat recovery device 67: condenser 68: condensed water
69: Exhaust 70: Tap water 71: Hot 72: Cold 73: Cooling water
74: thrust 80: yoke 81: electromagnetic heating turbine rotor blade 83: electromagnetic heating nozzle 84: annularly integrated casting 85: outer diameter assembly annular portion 86: inner diameter assembly annular portion 87: water repellent water cooling blade 88: combustion gas outlet 89: Inner magnetized friction wheel device 90: Magnetically attached friction wheel device 91a: Principle of atomization 91b: Principle of atomization 91c: Principle of atomization 91d: Principle of atomization 92a: Special device 92b: Special device 93a: Water injection device 93b: Water injection device
94: Outer case 95: Water absorption passage 96: Water supply passage 97: Water supply pump 98: Coil 99: Magnetic force line 100: Magnetic friction power transmission device 100a: Water transmission pump and magnetic friction power transmission device 101: Heating high temperature means

Claims

An all-blade steam gas turbine combined engine characterized by maximizing high-temperature water recovery heat by a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized by maximizing supercritical pressure high temperature water recovery heat by a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized in that high-temperature water recovery heat is obtained by a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water recovery heat is obtained by a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized by utilizing a vaporization explosive power by maximizing high-temperature water recovery heat by a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized by utilizing a vaporization explosive power by maximizing supercritical pressure high temperature water recovery heat by a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized by utilizing vaporized explosive power as high-temperature water recovery heat by a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized by utilizing a vaporization explosive power as a supercritical pressure high-temperature water recovery heat by a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized in that high-temperature water recovery heat is maximized by a combustor / heat exchanger (4) and injected from a high-temperature water injection nozzle (59a) using vaporization explosive power.

Combined all-blade steam gas turbine, characterized in that the supercritical pressure high-temperature water recovery heat is maximized by the combustor / heat exchanger (4) and injected from the high-temperature water injection nozzle (59a) using vaporization explosion power. organ.

An all-blade steam gas turbine combined engine characterized in that the combustor / heat exchanger (4) injects high-temperature water recovery heat into high-temperature water injection nozzles (59a) using vaporization explosive power.

An all-blade steam / gas turbine combined engine characterized in that a combustor / heat exchanger (4) is used to convert superheated high-temperature water recovery heat into high-temperature water injection nozzles (59a) using vaporization explosive power.

High-temperature water recovery heat is maximized by the combustor / heat exchanger (4), and the high-temperature water is injected from the high-temperature water injection nozzle (59a) heated and heated by the high-temperature heating means (101) using vaporization explosive power. All-blade steam gas turbine combined engine.

The high-temperature water injection nozzle (59a) is heated to a high temperature by the high-temperature heating means (101) by utilizing the vaporization explosive force by maximizing the heat recovery of the supercritical pressure high-temperature water by the combustor / heat exchanger (4). This is a combined rotor blade steam gas turbine engine.

The high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion power by using the combustor / heat exchanger (4) to convert the high-temperature water recovery heat into heat, is used. Combined moving blade steam gas turbine engine.

The high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive power, is converted into the supercritical pressure high-temperature water recovery heat by the combustor / heat exchanger (4). All-blade steam gas turbine united engine.

Injection from a plurality of high-temperature water injection nozzles (59a), which maximizes the amount of high-temperature water recovery heat by a combustor / heat exchanger (4) and uses a vaporization explosive force to heat to a high temperature by a high-temperature heating means (101). All-blade steam gas turbine combined engine.

From a plurality of high-temperature water injection nozzles (59a) which maximize the supercritical pressure high-temperature water recovery heat by the combustor / heat exchanger (4) and use the vaporization explosive power to heat the high temperature by the high-temperature heating means (101). All-blade steam gas turbine combined engine characterized by injection.

The combustor / heat exchanger (4) is used for injecting from a plurality of high-temperature water injection nozzles (59a), which are heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive power to convert the high-temperature water recovery heat into heat. All-blade steam gas turbine combined engine.

A plurality of hot water injection nozzles (59a), which are heated to a high temperature by a high temperature heating means (101) by using a vaporizing explosive force by converting the heat of supercritical pressure high temperature water recovery to heat by a combustor / heat exchanger (4). This is a combined rotor blade steam gas turbine engine.

The combustor / heat exchanger (4) maximizes the amount of heat recovered from the high-temperature water and injects it from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade steam turbine using the vaporization explosive power. Combined moving blade steam gas turbine engine.

With the combustor / heat exchanger (4), the supercritical pressure high-temperature water recovery heat is maximized and the high-temperature water injection nozzle (59a) can use the vaporization explosion to inject the heat to the uppermost stream of the all-blade steam turbine. All-blade steam gas turbine united engine.

The all-rotor blade is characterized in that the combustor and heat exchanger (4) is used to convert the high-temperature water recovery heat into high-temperature water injection nozzles (59a) and inject it to the uppermost stream of the all-rotor steam turbine by utilizing vaporization explosive power. Steam gas turbine combined engine.

The combustor / heat exchanger (4) converts the supercritical pressure high-temperature water recovery heat into heat and injects it from the high-temperature water injection nozzle (59a) to the uppermost stream of the full-blade steam turbine using the vaporization explosive power. All blade steam gas turbine combined engine.

A high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) using a vaporizing explosive force by maximizing the amount of high-temperature water recovery heat by a combustor / heat exchanger (4) and using a whole blade steam turbine. An all-blade steam gas turbine united engine characterized by injection into the uppermost stream.

By the combustor / heat exchanger (4), the supercritical pressure high-temperature water recovery heat is maximized and the high-temperature water injection nozzle (59a) is heated and heated by the high-temperature heating means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a blade steam turbine.

The high-temperature water injection nozzle (59a), which has been heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion power by using the vaporizing explosive force, by using the combustor / heat exchanger (4) to convert the high-temperature water recovery heat, to the end of the entire blade steam turbine. An all-blade steam gas turbine combined engine characterized by injection upstream.

The high-temperature water injection nozzle (59a), which has been heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive power by using superheated high-temperature water recovery heat by the combustor / heat exchanger (4), and utilizing the vaporization explosion power, all blade steam An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the turbine.

A plurality of high-temperature water injection nozzles (59a), which maximize the amount of high-temperature water recovery heat by the combustor / heat exchanger (4) and use the vaporization explosive force to heat the high-temperature water by the high-temperature heating means (101), use the entire moving blade. An all-blade steam gas turbine united engine characterized by injection into the uppermost stream of a steam turbine.

From a plurality of high-temperature water injection nozzles (59a) which maximize the supercritical pressure high-temperature water recovery heat by the combustor / heat exchanger (4) and use the vaporization explosive power to heat the high temperature by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by injecting it into the uppermost stream of the all-blade steam turbine.

A full-blade steam turbine is supplied from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by a high-temperature heating means (101) using a vaporizing explosion force by converting a high-temperature water recovery heat amount by a combustor / heat exchanger (4). An all-blade steam gas turbine united engine characterized by injection into the uppermost stream.

The combustor / heat exchanger (4) is used to make a supercritical pressure high-temperature water recovery heat quantity and utilizes a vaporization explosion force to move the plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a blade steam turbine.

An all-blade steam / gas turbine combined engine characterized in that the combustor / heat exchanger (4) maximizes the amount of high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a).

An all-blade steam gas turbine combined engine characterized by using a combustor / heat exchanger (4) to maximize the heat recovery heat of supercritical high temperature water, including the heat recovery of the vaporization latent heat recovery device (66a).

An all-blade steam gas turbine combined engine characterized in that high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) is obtained by the combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine characterized in that a supercritical pressure high-temperature water recovery heat amount including a recovery heat amount of a vaporization latent heat recovery device (66a) is obtained by a combustor / heat exchanger (4).

A full-rotor blade characterized in that the combustor / heat exchanger (4) maximizes the amount of high-temperature water recovery heat, including the recovery heat of the vaporizing latent heat recovery unit (66a), and injects it into the uppermost stream of the all-rotor steam turbine. Steam gas turbine combined engine.

The combustor / heat exchanger (4) maximizes supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporizing latent heat recovery device (66a) and injects the heat to the uppermost stream of the all-blade steam turbine. All blade steam gas turbine combined engine.

The all-blade steam gas characterized in that the combustor / heat exchanger (4) converts the high-temperature water recovered heat including the recovered heat of the vaporization latent heat recovery unit (66a) to the uppermost stream of the all-blade steam turbine. Turbine united engine.

The super-high-pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) is injected by the combustor / heat exchanger (4) to the uppermost stream of the all-blade steam turbine. Wing steam gas turbine combined engine.

Combined all-blade steam gas turbine engine characterized in that the combustor / heat exchanger (4) maximizes the amount of high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) to utilize the vaporization explosive power. .

All rotor blade steam gas characterized by utilizing the vaporization explosive power by maximizing the supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) by the combustor / heat exchanger (4). Turbine united engine.

An all-blade steam / gas turbine combined engine characterized in that the combustor / heat exchanger (4) is used to generate high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) and utilize the vaporization explosive power.

Combination of all buckets / steam gas turbines characterized in that the combustor / heat exchanger (4) is used as supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) to utilize the vaporization explosive power. organ.

The combustor / heat exchanger (4) maximizes the amount of high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) and injects it into the uppermost stream of the all-blade steam turbine to utilize the vaporization explosive power. This is a combined rotor blade steam gas turbine engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) is maximized by the combustor / heat exchanger (4) and injected into the uppermost stream of the all-blade steam turbine to evaporate and explode. All-blade steam gas turbine combined engine characterized by utilizing

The combustor / heat exchanger (4) makes it possible to use the vaporized explosive power by injecting into the uppermost stream of the all-blade steam turbine with high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a). All-blade steam gas turbine united engine.

Using the combustor / heat exchanger (4), the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) is injected into the uppermost stream of the all-blade steam turbine to utilize the vaporization explosive power All-blade steam gas turbine combined engine characterized by

Using a combustor / heat exchanger (4) to maximize the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a), and inject from the high-temperature water injection nozzle (59a) using vaporization explosive power. All-blade steam gas turbine combined engine.

By using the combustor / heat exchanger (4) to maximize the supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) and utilizing the vaporization explosion power from the high temperature water injection nozzle (59a). All-blade steam gas turbine combined engine characterized by injection.

The combustor / heat exchanger (4) is used to convert the latent heat recovery from the vaporization latent heat recovery unit (66a) into high-temperature water recovery heat, and to inject it from the high-temperature water injection nozzle (59a) using vaporization explosive power. All-blade steam gas turbine combined engine.

The combustor / heat exchanger (4) makes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) and injects it from the high-temperature water injection nozzle (59a) using the vaporization explosive power. This is a combined rotor blade steam gas turbine engine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a), and utilizes the vaporization explosive power to make the entire blade from the high-temperature water injection nozzle (59a). An all-blade steam gas turbine united engine characterized by injection into the uppermost stream of a steam turbine.

By using the combustor / heat exchanger (4) to maximize the supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) and utilizing the vaporization explosion power from the high temperature water injection nozzle (59a). An all-blade steam gas turbine combined engine characterized by injecting it into the uppermost stream of the all-blade steam turbine.

By using the combustor / heat exchanger (4), the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) is used to make use of the vaporization explosive power and from the high-temperature water injection nozzle (59a). An all-blade steam gas turbine united engine characterized by injection into the uppermost stream.

Using the combustor / heat exchanger (4), the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) is converted to the high-temperature water injection nozzle (59a) by utilizing the vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a blade steam turbine.

The combustor / heat exchanger (4) maximizes the amount of high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a), and uses the vaporization explosion power to raise the temperature to high by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by injection from a high-temperature water injection nozzle (59a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) is maximized by the combustor / heat exchanger (4) and heated by the high temperature heating means (101) using the vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injecting from a hot water injection nozzle (59a) with a high temperature.

The combustor / heat exchanger (4) converts the high-temperature water to the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) and uses the vaporization explosive power to heat the high-temperature water to the high temperature by the high-temperature heating means (101) An all-blade steam gas turbine combined engine characterized by injection from an injection nozzle (59a).

The combustor / heat exchanger (4) makes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) and the high-temperature heating by the high-temperature heating means (101) using the vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injecting from a high temperature water injection nozzle (59a).

The combustor / heat exchanger (4) maximizes the amount of high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a), and uses the vaporization explosion power to raise the temperature to high by the high-temperature heating means (101). A combined rotor blade steam gas turbine engine characterized by injecting from a high temperature water injection nozzle (59a) to the uppermost stream of the rotor blade steam turbine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) is maximized by the combustor / heat exchanger (4) and heated by the high temperature heating means (101) using the vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injecting a high-temperature water injection nozzle (59a) into the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) converts the high-temperature water to the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) and uses the vaporization explosive power to heat the high-temperature water to the high temperature by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by injecting from the injection nozzle (59a) to the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) makes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) and the high-temperature heating by the high-temperature heating means (101) using the vaporization explosive power. And a high-temperature water injection nozzle (59a).

The combustor / heat exchanger (4) maximizes the amount of high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a), and uses the vaporization explosion power to raise the temperature to high by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by injection from a plurality of high-temperature water injection nozzles (59a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) is maximized by the combustor / heat exchanger (4) and heated by the high temperature heating means (101) using the vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injection from a plurality of high-temperature water injection nozzles (59a) having a high temperature.

The combustor / heat exchanger (4) is used to convert the latent heat of vaporization to the high-temperature water recovery heat including the recovered heat of the vaporizing latent heat recovery device (66a), and to use the vaporization explosive power to heat the high-temperature water by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by injection from a high-temperature water injection nozzle (59a).

The combustor / heat exchanger (4) makes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) and the high-temperature heating by the high-temperature heating means (101) using the vaporization explosive power. And a plurality of high-temperature water injection nozzles (59a).

The combustor / heat exchanger (4) maximizes the amount of high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a), and uses the vaporization explosion power to raise the temperature to high by the high-temperature heating means (101). An all-blade steam gas turbine combined engine characterized by injecting a plurality of high-temperature water injection nozzles (59a) to the uppermost stream of the all-blade steam turbine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) is maximized by the combustor / heat exchanger (4) and heated by the high temperature heating means (101) using the vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injecting a plurality of high-temperature water injection nozzles (59a) into the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) is used to convert the latent heat of vaporization to the high-temperature water recovery heat including the recovered heat of the vaporizing latent heat recovery device (66a), and to use the vaporization explosive power to heat the high-temperature water by the high-temperature heating means (101). A combined rotor blade steam gas turbine engine characterized by injecting from a high temperature water injection nozzle (59a) to the uppermost stream of the rotor blade steam turbine.

Combined all-blade steam gas turbine engine characterized in that the combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass. .

A full-blade steam gas characterized by maximizing supercritical pressure high temperature water recovery heat including recovery heat of a vaporization latent heat recovery unit (66a) that reduces fuel combustion mass by a combustor / heat exchanger (4). Turbine united engine.

An all-blade steam gas turbine combined engine, characterized in that the combustor / heat exchanger (4) is used to recover the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass.

Combination of all rotor blade steam gas turbines characterized by supercritical pressure high temperature water recovery heat including recovery heat of vaporization latent heat recovery device (66a) for reducing fuel combustion mass by combustor / heat exchanger (4) organ.

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) and injected into the uppermost stream of the all blade steam turbine. All-blade steam gas turbine combined engine.

The combustor / heat exchanger (4) maximizes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and becomes the most upstream flow of the all blade steam turbine. All-blade steam gas turbine combined engine characterized by injection.

The combustor and heat exchanger (4) is characterized in that high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass is injected into the uppermost stream of the all-blade steam turbine. All-blade steam gas turbine combined engine.

The combustor and heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery device (66a), which reduces the fuel combustion mass, into supercritical high-temperature water recovery heat, and injects it into the uppermost stream of the all-blade steam turbine. This is a combined rotor blade steam gas turbine engine.

Combustor / heat exchanger (4) maximizes high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) that reduces fuel combustion mass and utilizes vaporization explosive power. Wing steam gas turbine combined engine.

The combustor / heat exchanger (4) maximizes the supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and utilizes the vaporization explosive power. All-blade steam gas turbine combined engine.

The all-rotor blade steam is characterized in that the combustor / heat exchanger (4) is used as the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and utilizing the vaporization explosive power. Gas turbine combined engine.

The combustor / heat exchanger (4) makes use of the vaporization explosive power as the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass. Combined moving blade steam gas turbine engine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass, and injects it to the uppermost stream of the all-blade steam turbine. An all-blade steam gas turbine combined engine characterized by utilizing vaporization explosive power.

The combustor / heat exchanger (4) maximizes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and becomes the most upstream flow of the all blade steam turbine. An all-blade steam gas turbine combined engine characterized by injecting and using vaporization explosive power.

The combustor / heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery unit (66a), which reduces the fuel combustion mass, into high-temperature water recovery heat, and injects it into the uppermost stream of the all-blade steam turbine to vaporize and explode. An all-blade steam gas turbine combined engine that uses power.

The combustor / heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery unit (66a), which reduces the fuel combustion mass, into supercritical pressure high-temperature water recovery heat, and injects it into the uppermost stream of the all-blade steam turbine. An all-blade steam gas turbine combined engine characterized by utilizing vaporizing explosive power.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and utilizes the vaporization explosion power to use the high-temperature water injection nozzle ( 59a) An all-blade steam gas turbine combined engine characterized by injection.

The combustor / heat exchanger (4) maximizes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and utilizes the vaporization explosive power to generate high-temperature water. An all-blade steam gas turbine combined engine characterized by injection from an injection nozzle (59a).

The combustor / heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery unit (66a) that reduces the fuel combustion mass into high-temperature water recovery heat, and utilizes the vaporization explosive power to use the high-temperature water injection nozzle (59a). All-blade steam gas turbine combined engine characterized by more injection.

A high-temperature water injection nozzle utilizing a vaporization explosion force by making a supercritical pressure high-temperature water recovery heat including a recovery heat of a vaporization latent heat recovery unit (66a) for reducing a fuel combustion mass by a combustor / heat exchanger (4). (59a) An all-blade steam gas turbine combined engine characterized by injection from (59a).

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and utilizes the vaporization explosion power to use the high-temperature water injection nozzle ( 59a) A combined rotor blade steam gas turbine engine characterized by injecting into the uppermost stream of the rotor blade steam turbine.

The combustor / heat exchanger (4) maximizes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and utilizes the vaporization explosive power to generate high-temperature water. An all-blade steam gas turbine combined engine characterized by injecting from the injection nozzle (59a) to the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery unit (66a) that reduces the fuel combustion mass into high-temperature water recovery heat, and utilizes the vaporization explosive power to use the high-temperature water injection nozzle (59a). An all-blade steam gas turbine combined engine characterized by being injected more upstream of the all-blade steam turbine.

A high-temperature water injection nozzle utilizing a vaporization explosion force by making a supercritical pressure high-temperature water recovery heat including a recovery heat of a vaporization latent heat recovery unit (66a) for reducing a fuel combustion mass by a combustor / heat exchanger (4). (59a) A combined rotor blade steam gas turbine engine characterized by injecting into the uppermost stream of the rotor blade steam turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass, and utilizes the vaporization explosive power to heat the high-temperature heating means (101). ), Wherein the high-temperature water injection nozzle (59a), which is heated to a high temperature, injects fuel from the high-pressure water injection nozzle (59a).

The combustor / heat exchanger (4) maximizes the supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and uses the vaporization explosive power to heat and heat it. An all-blade steam gas turbine combined engine characterized by injecting from a high-temperature water injection nozzle (59a) heated to a high temperature by means (101).

The combustor / heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery unit (66a), which reduces the fuel combustion mass, into high-temperature water recovery heat, and utilizes the vaporization explosive power to heat the high-temperature means (101). An all-blade steam gas turbine combined engine characterized by injecting from a hot water injection nozzle (59a) heated to a high temperature.

The combustor / heat exchanger (4) makes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass, and uses the vaporization explosive power to heat the high-temperature heating means ( 101) An all-blade steam gas turbine combined engine characterized by injecting from a high-temperature water injection nozzle (59a) heated to a high temperature according to 101).

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass, and utilizes the vaporization explosive power to heat the high-temperature heating means (101). A) a high-temperature water injection nozzle (59a), which is heated to a high temperature by (1), injects the gas into the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) maximizes the supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and uses the vaporization explosive power to heat and heat it. An all-blade steam gas turbine combined engine characterized in that a high-temperature water injection nozzle (59a) heated to a high temperature by means (101) injects it into the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery unit (66a), which reduces the fuel combustion mass, into high-temperature water recovery heat, and utilizes the vaporization explosive power to heat the high-temperature means (101). An all-blade steam gas turbine combined engine characterized in that a high-temperature water injection nozzle (59a) heated to a high temperature is injected to the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) makes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass, and uses the vaporization explosive power to heat the high-temperature heating means ( 101) A combined rotor blade steam gas turbine engine characterized in that a high temperature water injection nozzle (59a) heated to a high temperature according to 101) injects it to the uppermost stream of the full rotor blade steam turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass, and utilizes the vaporization explosive power to heat the high-temperature heating means (101). ), Wherein a plurality of high-temperature water injection nozzles (59a) are heated to a high temperature to inject fuel from the plurality of high-temperature water injection nozzles (59a).

The combustor / heat exchanger (4) maximizes the supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and uses the vaporization explosive power to heat and heat it. An all-blade steam gas turbine combined engine characterized by injecting from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by means (101).

The combustor / heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery unit (66a), which reduces the fuel combustion mass, into high-temperature water recovery heat, and utilizes the vaporization explosive power to heat the high-temperature means (101). An all-blade steam gas turbine combined engine characterized by injection from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature.

The combustor / heat exchanger (4) makes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass, and uses the vaporization explosive power to heat the high-temperature heating means ( 101) An all-blade steam gas turbine combined engine characterized by injection from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by 101).

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass, and utilizes the vaporization explosive power to heat the high-temperature heating means (101). ), A plurality of high-temperature water injection nozzles (59a) heated to a high temperature for injecting into the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) maximizes the supercritical pressure high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass, and uses the vaporization explosive power to heat and heat it. A combined rotor blade steam gas turbine engine characterized in that a plurality of high temperature water injection nozzles (59a) heated to a high temperature by means (101) inject the same to the uppermost stream of the full blade steam turbine.

The combustor / heat exchanger (4) converts the recovered heat of the vaporizing latent heat recovery unit (66a), which reduces the fuel combustion mass, into high-temperature water recovery heat, and utilizes the vaporization explosive power to heat the high-temperature means (101). An all-blade steam gas turbine combined engine characterized in that a plurality of high-temperature water injection nozzles (59a) heated to a high temperature are injected to the uppermost stream of the all-blade steam turbine.

The combustor / heat exchanger (4) makes the supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass, and uses the vaporization explosive power to heat the high-temperature heating means ( 101) A combined turbine blade and steam gas turbine engine characterized in that a plurality of high-temperature water injection nozzles (59a) heated to a high temperature according to 101) inject the same to the uppermost stream of the full blade steam turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass, and communicates with each high-temperature water control valve (7a). This is a combined rotor blade steam gas turbine engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). All-blade steam gas turbine united engine characterized by contacting

By using the combustor / heat exchanger (4), the amount of recovered heat of the vaporizing latent heat recovery device (66a) for reducing the fuel combustion mass can be converted into high-temperature water recovery heat and communicated to the respective high-temperature water control valves (7a). All-blade steam gas turbine combined engine.

Supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is connected to each high-temperature water control valve (7a) by the combustor / heat exchanger (4). All-blade steam gas turbine combined engine characterized by

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the all-blade steam turbine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is maximized by the combustor / heat exchanger (4), and the respective high-temperature water control valves (7a). The combined turbine and steam turbine combined engine is characterized in that it is contacted with and injected into the uppermost stream of the turbine bucket.

By using the combustor / heat exchanger (4), the amount of heat recovered by the latent heat recovery unit (66a) for reducing the fuel combustion mass is converted into high-temperature water recovery heat and communicated to each high-temperature water control valve (7a). This is an all-steam steam gas turbine combined engine characterized by injection into the uppermost stream of the moving blade steam turbine.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). The combined rotor blade steam gas turbine engine is characterized by being injected into the uppermost stream of the rotor blade steam turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by injecting it into the uppermost stream of the all-blade steam gas turbine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A combined rotor blade steam gas turbine engine characterized by injecting it into the uppermost stream of all rotor blade steam gas turbines.

By using the combustor / heat exchanger (4), the amount of heat recovered by the latent heat recovery unit (66a) for reducing the fuel combustion mass is converted into high-temperature water recovery heat and communicated to each high-temperature water control valve (7a). An integrated all-swing steam gas turbine engine characterized by injection into the uppermost stream of the moving blade steam gas turbine.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). A combined turbine and steam turbine engine that is characterized by being injected into the uppermost stream of the turbine blade steam gas turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine that injects fuel into the uppermost stream of the all-blade gas turbine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by injecting it into the uppermost stream of the all-blade gas turbine by contacting it.

By using the combustor / heat exchanger (4), the amount of heat recovered by the latent heat recovery unit (66a) for reducing the fuel combustion mass is converted into high-temperature water recovery heat and communicated to each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of a moving blade gas turbine.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). The all-blade steam gas turbine combined engine is characterized by being injected into the uppermost stream of the all-blade gas turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by utilizing vaporizing explosive power.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). An all-blade steam gas turbine combined engine that uses vaporization and explosion power to contact.

With the combustor / heat exchanger (4), the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) for vaporization. An all-blade steam gas turbine combined engine that uses explosive power.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by utilizing vaporization explosive power.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by utilizing the vaporized explosive power by injecting it into the uppermost stream of the all-blade steam turbine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by injecting it into the uppermost stream of the all-blade steam turbine to utilize vaporization explosive power.

By using the combustor / heat exchanger (4), the amount of heat recovered by the latent heat recovery unit (66a) for reducing the fuel combustion mass is converted into high-temperature water recovery heat and communicated to each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by injecting into the uppermost stream of a bucket steam turbine and utilizing vaporization explosive power.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). An all-wing steam gas turbine combined engine characterized by using the vaporized explosive power by injecting it into the uppermost stream of the all-wing steam turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by injecting into the uppermost stream of the all-blade steam gas turbine to utilize vaporization explosive power.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by injecting it into the uppermost stream of the all-blade steam gas turbine to utilize vaporization explosive power.

By using the combustor / heat exchanger (4), the amount of heat recovered by the latent heat recovery unit (66a) for reducing the fuel combustion mass is converted into high-temperature water recovery heat and communicated to each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine that uses the vaporization and explosive power by injecting it into the uppermost stream of the bucket steam gas turbine.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). An all-wing steam gas turbine combined engine characterized by using the vaporized explosive power by injecting it into the uppermost stream of the all-wing steam gas turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by utilizing the vaporized explosive power by injecting it into the uppermost stream of the all-blade gas turbine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). Combined all-blade steam gas turbine engine characterized by injecting it into the uppermost stream of the all-blade gas turbine and utilizing vaporized explosive power.

By using the combustor / heat exchanger (4), the amount of heat recovered by the latent heat recovery unit (66a) for reducing the fuel combustion mass is converted into high-temperature water recovery heat and communicated to each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by utilizing the vaporized explosive power by injecting it into the uppermost stream of the moving blade gas turbine.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). An all-blade steam gas turbine combined engine characterized by using the vaporized explosive power by injecting it into the uppermost stream of the all-blade gas turbine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). And a high-pressure water injection nozzle (59a) for injecting the steam using a vaporizing explosive force.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). And a high-pressure water injection nozzle (59a) for injecting using a vaporizing explosive force.

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by injecting from a high-temperature water injection nozzle (59a) using vaporization explosive power.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). And a high-pressure water injection nozzle (59a) for injecting the steam using a vaporizing explosive force.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) for injecting the steam to the uppermost stream of the all-blade steam turbine by utilizing vaporization explosive power.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). And a high-pressure water injection nozzle (59a) for injecting into the uppermost stream of the full-blade steam turbine by utilizing vaporization explosive power.

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by injecting from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade steam turbine using vaporization explosive power.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) for injecting the steam into the uppermost stream of the all-blade steam turbine by utilizing vaporization explosive power.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). A high-temperature water injection nozzle (59a) for injecting into the uppermost stream of the all-blade steam gas turbine utilizing vaporization explosive power.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). And a high-pressure water injection nozzle (59a) for injecting into the uppermost stream of the full-blade steam gas turbine by utilizing the vaporization and explosion power.

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by injecting from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade steam gas turbine using vaporization explosive power.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) for injecting the steam into the uppermost stream of the all-blade steam gas turbine using vaporization explosive power.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) for injecting into the uppermost stream of the all-blade gas turbine by utilizing vaporization explosive power.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). And a high-pressure water injection nozzle (59a) for injecting the gas into the uppermost stream of the full-blade gas turbine by utilizing vaporization explosive power.

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by injecting from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade gas turbine using vaporization explosive power.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) for injecting the gas into the uppermost stream of the all-blade gas turbine using vaporization explosive power.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power, and injects the same from a high-pressure water jet nozzle (59a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using vaporization and explosion power, and injects the steam from the high-speed water injection nozzle (59a).

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by injecting from a high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) using vaporization explosive power.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) using vaporization explosive power to inject the steam from the high-speed water injection nozzle (59a).

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) using vaporization explosive power to inject the most upstream steam of the all-blade steam turbine. organ.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-pressure water jet nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power, is injected into the uppermost stream of the all-rotor steam turbine. Gas turbine combined engine.

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized in that a high-temperature water injection nozzle (59a), which is heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force, is injected to the uppermost stream of the all-blade steam turbine.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) utilizing vaporization and explosive power to inject into the uppermost stream of all the blade steam turbines. Coalition organization.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force to inject the most upstream of the all-blade steam gas turbine. Coalition organization.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization and explosive power to inject all rotor blades into the uppermost stream of the steam gas turbine. Steam gas turbine combined engine.

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) by the combustor / heat exchanger (4). A combined bladed steam gas turbine engine characterized in that a high temperature water injection nozzle (59a) heated to a high temperature by a heating and high temperature means (101) utilizing vaporization explosive power is injected into the uppermost stream of the all bladed steam gas turbine. .

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power to inject the most upstream steam of the all-blade steam gas turbine. Turbine united engine.

The combustor / heat exchanger (4) maximizes the high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass and communicates with each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power to inject the most-rotated gas turbine into the uppermost stream of the all-bladed gas turbine. organ.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force to inject the most upstream steam of the all-blade gas turbine. Gas turbine combined engine.

The high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is communicated to the respective high-temperature water control valves (7a) by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized in that a high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) utilizing vaporization explosion force is injected into the uppermost stream of the all-blade gas turbine.

Combustor / heat exchanger (4) converts supercritical pressure high-temperature water recovery heat including recovery heat of vaporization latent heat recovery unit (66a) for reducing fuel combustion mass to each high-temperature water control valve (7a). And a high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) utilizing vaporization explosive force to inject the most upstream of the all-blade gas turbine. Coalition organization.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. An all-blade steam gas turbine combined engine, characterized by contacting (6a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a).

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ) Combined all-blade steam gas turbine engine characterized by contact

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by communicating with a water pipe (6a).

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) An all-blade steam gas turbine combined engine characterized by injecting into the uppermost stream of the all-blade steam turbine in contact with (6a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a) and injecting it into the uppermost stream of the all-blade steam turbine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects into the uppermost stream of the all-blade steam turbine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized in that it is connected to a water pipe (6a) and is injected into the uppermost stream of the all-blade steam turbine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) A combined rotor blade steam gas turbine engine characterized by injecting into the uppermost stream of the all blade steam gas turbine in contact with (6a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a) and injecting it into the uppermost stream of the all-blade steam gas turbine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects into the uppermost stream of the all-blade steam gas turbine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by being connected to a water pipe (6a) and injecting it into the uppermost stream of the all-blade steam gas turbine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) An all-blade steam gas turbine combined engine characterized by injecting into the uppermost stream of the all-blade gas turbine in contact with (6a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a) and injecting it into the uppermost stream of the all-blade gas turbine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects into the uppermost stream of the all-blade gas turbine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized in that it is connected to a water pipe (6a) and is injected into the uppermost stream of the all-blade gas turbine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) An all-blade steam gas turbine combined engine characterized by utilizing vaporized explosive power in contact with (6a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-pressure water pipe (6a) for utilizing the vaporization and explosive power of the all-blade steam gas turbine combined engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ) Is a combined engine of all blade steam gas turbines characterized by utilizing vaporization explosive power by contacting.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by utilizing vaporization explosive power by contacting a water pipe (6a).

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) An integrated all-swing steam gas turbine engine characterized by utilizing the vaporized explosive power by injecting it into the uppermost stream of the all-swing blade steam turbine in contact with (6a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a) for injecting into the uppermost stream of the all-blade steam turbine to utilize vaporized explosive power, thereby combining the all-blade steam gas turbine engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And is combined with an all-blade steam gas turbine by injecting it into the uppermost stream of the all-blade steam turbine to utilize vaporized explosive power.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized in that it is connected to a water pipe (6a) and is injected into the uppermost stream of the all-blade steam turbine to utilize vaporization explosive power.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) An all-wing steam gas turbine combined engine characterized by utilizing the vaporized explosive power by injecting it into the uppermost stream of the all-wing steam gas turbine in contact with (6a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a) for injecting into the uppermost stream of the all-blade steam gas turbine to utilize vaporization explosive power, thereby combining the all-blade steam gas turbine engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), Which is combined with the all-blade steam gas turbine to inject it into the uppermost stream of the all-blade steam gas turbine to utilize vaporization explosive power.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A combined bladed steam gas turbine engine characterized in that it is connected to a water pipe (6a) and is injected into the uppermost stream of the bladed steam gas turbine to utilize vaporized explosive power.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) A combined all-blade steam gas turbine engine characterized in that it is injected into the uppermost stream of the all-blade gas turbine in contact with (6a) to utilize vaporized explosive power.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a) for injecting the gas into the uppermost stream of the all-blade gas turbine to utilize the vaporized explosive power.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), Which is characterized by injecting it into the uppermost stream of the all-blade gas turbine and utilizing the vaporized explosive power.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine, characterized in that it is connected to a water pipe (6a) and is injected into the uppermost stream of the all-blade gas turbine to utilize vaporization explosive power.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) An all-blade steam gas turbine combined engine characterized by injecting from a high-temperature water injection nozzle (59a) by utilizing vaporization and explosive power in contact with (6a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a) and injecting it from a high-temperature water injection nozzle (59a) using vaporization explosive power.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects from a high-temperature water injection nozzle (59a) using vaporization explosive power.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by being connected to a water pipe (6a) and injecting from a high-temperature water injection nozzle (59a) using vaporization explosive power.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) An all-blade steam gas turbine combined engine characterized by injecting from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade steam turbine by utilizing vaporization explosive force.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a), and injecting it from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade steam turbine using vaporization explosive power.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects the hot air from the high-temperature water injection nozzle (59a) to the uppermost stream of the full-blade steam turbine using the vaporization explosive power.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by being connected to a water pipe (6a) and injecting from a high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade steam turbine using vaporization explosive power.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) A combined all-blade steam gas turbine engine characterized in that high-temperature water injection nozzles (59a) are used to inject the most upstream steam gas turbine of the all-blade steam gas turbine by utilizing vaporization explosion force.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a), and injecting it from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade steam gas turbine using vaporization explosive power. .

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects the hot air from the high-temperature water injection nozzle (59a) to the uppermost stream of the full-blade steam gas turbine by utilizing the vaporization explosive power.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by being connected to a water pipe (6a) and injecting from a high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade steam gas turbine by utilizing vaporization explosive power.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) An all-blade steam gas turbine combined engine characterized by injecting from a high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade gas turbine by utilizing vaporization and explosion power.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a), and injecting it from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade gas turbine using vaporization explosive power.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects from the high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade gas turbine using vaporization explosive power.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by being connected to a water pipe (6a) and injecting from a high-temperature water injection nozzle (59a) to the uppermost stream of the all-blade gas turbine using vaporization explosive power.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) The all-blade steam gas turbine combined engine characterized in that it is injected from a high-temperature water injection nozzle (59a) which is heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive force.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) and injecting it from a high-temperature water injection nozzle (59a) heated and heated by a high-temperature heating means (101) using vaporization explosive force. organ.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects from a high-temperature water injection nozzle (59a) heated to a high temperature by a heating and high-temperature means (101) using vaporization explosive force.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). An all-blade steam gas turbine combined engine characterized by being connected to a water pipe (6a) and injecting from a high-temperature water injection nozzle (59a) heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), and the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the vaporization explosive force to inject into the uppermost stream of the full-blade steam turbine. Combined moving blade steam gas turbine engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the high-temperature water pipe (6a), and the high-temperature water injection nozzle (59a), which has been heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive force, can be injected into the uppermost stream of the full-blade steam turbine. All-blade steam gas turbine united engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force, injects it to the uppermost stream of the all-blade steam turbine. Steam gas turbine combined engine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). The high-temperature water injection nozzle (59a), which is connected to the water pipe (6a) and heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power, is injected to the uppermost stream of the all-blade steam turbine. All blade steam gas turbine combined engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosive force to inject the gas into the uppermost stream of the all-blade steam gas turbine. All blade steam gas turbine combined engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is maximized by the combustor / heat exchanger (4), and the respective high-temperature water control valves (7a). High-temperature water pipe (6a), and injecting it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force to the uppermost stream of the all-blade steam gas turbine. All-blade steam gas turbine combined engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects the hot air from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive force to the uppermost stream of the all-blade steam gas turbine. Wing steam gas turbine combined engine.

A supercritical pressure high-temperature water recovery heat amount including a recovery heat amount of a vaporization latent heat recovery device (66a) for reducing a fuel combustion mass by the combustor / heat exchanger (4) is used to increase the high temperature of each high-temperature water control valve (7a). The high-temperature water injection nozzle (59a), which is connected to the water pipe (6a) and heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force, is injected into the uppermost stream of the all-blade steam gas turbine. All-blade steam gas turbine combined engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosive force to inject the uppermost stream of the full-blade gas turbine. Combined moving blade steam gas turbine engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and the high-temperature water injection nozzle (59a), which has been heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive force, can inject it to the uppermost stream of all blade gas turbines. All-blade steam gas turbine united engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects the hot air from the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive force, to the uppermost stream of the all-blade gas turbine. Steam gas turbine combined engine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). The high-temperature water injection nozzle (59a), which is connected to the water pipe (6a) and is heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force, is injected to the uppermost stream of the all-blade gas turbine. All blade steam gas turbine combined engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), and injects the hot air from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and optimizes the middle flow. An all-blade steam gas turbine combined engine characterized by supplying a combustion gas (10) to the engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine using the vaporizing and explosive force, An all-blade steam gas turbine combined engine characterized by supplying the combustion gas (10) to the middle stage optimal stage.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and burns to the middle stage optimal stage An all-blade steam gas turbine combined engine characterized by supplying gas (10).

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It communicates with the water pipe (6a) and injects it from the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force, to the uppermost stream of the all-blade steam gas turbine to optimize the middle stream. An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) to a stage.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) and injecting it into the uppermost stream of all the blade gas turbines from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporizing explosive force to achieve the middle stage optimal stage. An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force to the uppermost stream of the all-blade gas turbine, An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) to an optimal stage.

The high-temperature water pipe (6a) of each high-temperature water control valve (7a) is converted into high-temperature water recovery heat including the heat of vaporization latent heat recovery (66a) by the combustor / heat exchanger (4). ), And injects the hot gas from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporizing explosive force to the uppermost stream of the all-blade gas turbine, and the combustion gas reaches the middle stream optimal stage. An all-blade steam gas turbine combined engine characterized by supplying (10).

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A high-temperature water injection nozzle (59a), which is heated to a high temperature by a high-temperature heating means (101) using a vaporizing explosive force, is injected to the uppermost stream of all the blade gas turbines by utilizing a vaporizing explosive force, and is connected to a water pipe (6a). An all-blade steam gas turbine combined engine characterized by supplying a combustion gas (10) to the engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), and injects the hot air from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and optimizes the middle flow. An all-blade steam gas turbine combined engine, characterized in that a combustion gas (10) is supplied to the engine and cooled by high-temperature water (5a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine using the vaporizing and explosive force, An all-blade steam gas turbine combined engine characterized in that a combustion gas (10) is supplied to a middle flow optimum stage and cooled by high-temperature water (5a).

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and burns to the middle stage optimal stage An all-blade steam gas turbine combined engine characterized by supplying a gas (10) and cooling it with high-temperature water (5a).

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It communicates with the water pipe (6a) and injects it from the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force, to the uppermost stream of the all-blade steam gas turbine to optimize the middle stream. An all-blade steam gas turbine combined engine, characterized in that combustion gas (10) is supplied to the stage and cooled by high-temperature water (5a).

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) and injecting it into the uppermost stream of all the blade gas turbines from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporizing explosive force to achieve the middle stage optimal stage. An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) and cooling with high-temperature water (5a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is maximized by the combustor / heat exchanger (4), and the respective high-temperature water control valves (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force to the uppermost stream of the all-blade gas turbine, An all-blade steam gas turbine combined engine characterized in that combustion gas (10) is supplied to an optimal stage and cooled by high-temperature water (5a).

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects the hot gas from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive power to the uppermost stream of the all-blade gas turbine, and the combustion gas reaches the middle stream optimal stage. An all-blade steam gas turbine combined engine characterized by supplying (10) and cooling with high-temperature water (5a).

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A high-temperature water injection nozzle (59a), which is heated to a high temperature by a high-temperature heating means (101) using a vaporizing explosive force, is injected to the uppermost stream of all the blade gas turbines by utilizing a vaporizing explosive force, and is connected to a water pipe (6a). An all-blade steam gas turbine combined engine, characterized in that a combustion gas (10) is supplied to the engine and cooled by high-temperature water (5a).

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), and injects the hot air from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and optimizes the middle flow. An all-blade steam gas turbine combined engine characterized in that a combustion gas (10) is supplied to the cooling blade and cooled by high-temperature water (5a), and expands into a low-temperature combustion gas to coagulate moisture.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine using the vaporizing and explosive force, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the middle stage optimal stage, cooled by the high temperature water (5a), expanded into the low temperature combustion gas, and coagulates moisture.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and burns to the middle stage optimal stage An all-blade steam gas turbine combined engine characterized by supplying a gas (10), cooling it with high-temperature water (5a), expanding into a low-temperature combustion gas, and coagulating water.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It communicates with the water pipe (6a) and injects it from the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force, to the uppermost stream of the all-blade steam gas turbine to optimize the middle stream. An all-blade steam gas turbine combined engine characterized in that a combustion gas (10) is supplied to a stage, cooled by high-temperature water (5a), and expanded into a low-temperature combustion gas to coagulate moisture.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) and injecting it into the uppermost stream of all the blade gas turbines from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporizing explosive force to achieve the middle stage optimal stage. An all-blade steam gas turbine combined engine characterized by supplying a combustion gas (10), cooling it with high-temperature water (5a), expanding into a low-temperature combustion gas, and coagulating moisture.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force to the uppermost stream of the all-blade gas turbine, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimal stage, cooled by the high-temperature water (5a), expanded into the low-temperature combustion gas, and coagulate moisture.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects the hot gas from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive power to the uppermost stream of the all-blade gas turbine, and the combustion gas reaches the middle stream optimal stage. An all-blade steam gas turbine combined engine characterized in that (10) is supplied, cooled with high-temperature water (5a), expanded into low-temperature combustion gas, and coagulated with water.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A high-temperature water injection nozzle (59a), which is heated to a high temperature by a high-temperature heating means (101) using a vaporizing explosive force, is injected to the uppermost stream of all the blade gas turbines by utilizing a vaporizing explosive force, and is connected to a water pipe (6a). An all-blade steam gas turbine combined engine characterized in that a combustion gas (10) is supplied to the cooling blade and cooled by high-temperature water (5a), and expands into a low-temperature combustion gas to coagulate moisture.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), and injects the hot air from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and optimizes the middle flow. The combustion blade (10) is supplied to the turbine and cooled by the high-temperature water (5a), and expands to the low-temperature combustion gas to condense the water to enable a condenser vacuum, thereby enabling a condenser vacuum. organ.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine using the vaporizing and explosive force, A full-blade steam characterized in that the combustion gas (10) is supplied to the middle-stage optimum stage, cooled with high-temperature water (5a), expanded into low-temperature combustion gas, and coagulates moisture to enable condenser vacuum. Gas turbine combined engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and burns to the middle stage optimal stage An all-blade steam gas turbine combined engine characterized in that the gas (10) is supplied and cooled by the high-temperature water (5a), and expands into a low-temperature combustion gas to coagulate moisture to enable a condenser vacuum.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It communicates with the water pipe (6a) and injects it from the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force, to the uppermost stream of the all-blade steam gas turbine to optimize the middle stream. A full-blade steam gas turbine characterized in that a combustion gas (10) is supplied to a stage, cooled by high-temperature water (5a), expanded into a low-temperature combustion gas, and coagulates moisture to enable condenser vacuum. Coalition organization.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) and injecting it into the uppermost stream of all the blade gas turbines from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporizing explosive force to achieve the middle stage optimal stage. Combined all-blade steam gas turbine engine characterized in that a combustion gas (10) is supplied and cooled by high-temperature water (5a), and expands into a low-temperature combustion gas to coagulate moisture to enable condenser vacuum. .

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force to the uppermost stream of the all-blade gas turbine, The all-blade steam gas is characterized in that the combustion gas (10) is supplied to the optimal stage, cooled with the high-temperature water (5a), expanded into the low-temperature combustion gas, and condensed with water to enable a condenser vacuum. Turbine united engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects the hot gas from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive power to the uppermost stream of the all-blade gas turbine, and the combustion gas reaches the middle stream optimal stage. (10) is supplied, cooled by high-temperature water (5a), expanded into low-temperature combustion gas, and coagulates moisture to enable condenser vacuum, thereby enabling a combined steam turbine and turbine engine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A high-temperature water injection nozzle (59a), which is heated to a high temperature by a high-temperature heating means (101) using a vaporizing explosive force, is injected to the uppermost stream of all the blade gas turbines by utilizing a vaporizing explosive force, and is connected to a water pipe (6a). The combustion blade (10) is supplied to the turbine and cooled by the high-temperature water (5a), and expands to the low-temperature combustion gas to condense the water to enable a condenser vacuum, thereby enabling a condenser vacuum. organ.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), and injects the hot air from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and optimizes the middle flow. The combustion blade (10) is supplied to the cooling blade, cooled by high-temperature water (5a), expanded into a low-temperature combustion gas, coagulated with water, and the exhaust gas such as CO2 is brought close to zero. organ.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine using the vaporizing and explosive force, The all-blade steam is characterized in that the combustion gas (10) is supplied to the middle-stage optimum stage, cooled with high-temperature water (5a), expanded into low-temperature combustion gas, and coagulates moisture to bring exhaust such as CO2 close to zero. Gas turbine combined engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporizing explosive force to the uppermost stream of the all-blade steam gas turbine, and burns to the middle stage optimal stage An all-blade steam gas turbine combined engine characterized by supplying a gas (10), cooling with high-temperature water (5a), expanding into a low-temperature combustion gas, coagulating moisture, and reducing exhaust such as CO2 to zero.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It communicates with the water pipe (6a) and injects it from the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force, to the uppermost stream of the all-blade steam gas turbine to optimize the middle stream. An all-blade steam gas turbine characterized in that a combustion gas (10) is supplied to a stage, cooled with high-temperature water (5a), expanded into a low-temperature combustion gas, and condensed with water to make exhaust gas such as CO2 close to zero. Coalition organization.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a) and injecting it into the uppermost stream of all the blade gas turbines from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporizing explosive force to achieve the middle stage optimal stage. Combined all-blade steam gas turbine engine characterized in that the combustion gas (10) is supplied and cooled by the high-temperature water (5a), expanded to the low-temperature combustion gas and coagulates the water to make the exhaust gas such as CO2 close to zero. .

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosion force to the uppermost stream of the all-blade gas turbine, All blade steam gas characterized in that the combustion gas (10) is supplied to the optimal stage, cooled with high-temperature water (5a), expanded into a low-temperature combustion gas, coagulates moisture, and makes exhaust such as CO2 close to zero. Turbine united engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects the hot gas from the high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive power to the uppermost stream of the all-blade gas turbine, and the combustion gas reaches the middle stream optimal stage. (10) is supplied, cooled by high-temperature water (5a), expanded into low-temperature combustion gas, coagulates water, and makes exhaust gas such as CO2 close to zero, whereby the combined turbine and steam gas turbine engine is characterized.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A high-temperature water injection nozzle (59a), which is heated to a high temperature by a high-temperature heating means (101) using a vaporizing explosive force, is injected to the uppermost stream of all the blade gas turbines by utilizing a vaporizing explosive force, and is connected to a water pipe (6a). The combustion blade (10) is supplied to the cooling blade, cooled by high-temperature water (5a), expanded into a low-temperature combustion gas, coagulated with water, and the exhaust gas such as CO2 is brought close to zero. organ.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), and a plurality of high-temperature water injection nozzles (59a), which are heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force, and are injected from the plurality of high-pressure water-jet nozzles (59a). .

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). A high-temperature water pipe (6a), and a plurality of high-temperature water jet nozzles (59a), which are heated and heated to a high temperature by a heating and high-temperature means (101) using vaporization explosive force, and are injected. Turbine united engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). Combined with a water pipe (6a), a plurality of high-temperature water injection nozzles (59a), which are heated and heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force, are injected. organ.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosive force to inject the uppermost stream of the full-blade steam turbine. All-blade steam gas turbine combined engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the high-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosion force to inject the uppermost stream of the full-blade steam turbine. This is a combined rotor blade steam gas turbine engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization and explosive power to inject the uppermost stream of the full-blade steam turbine. Combined moving blade steam gas turbine engine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). By communicating with the water pipe (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive force can be injected into the uppermost stream of the all-blade steam turbine. All-blade steam gas turbine united engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade steam turbine to generate output. An all-blade steam gas turbine combined engine characterized in that heat is recovered later by a vaporization latent heat recovery device (66a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the high-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosion force are injected to the uppermost stream of the all-blade steam turbine. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery unit (66a) after output is generated.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporizing explosive force to inject the uppermost stream of the all-blade steam turbine, and vaporize after generating power. An all-blade steam gas turbine combined engine characterized by recovering heat with a latent heat recovery device (66a).

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected to the uppermost stream of the all-blade steam turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power and output. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery device (66a) after generation.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), the hot-water injection nozzle (59a) heated to a high temperature by the heating / high-temperature means (101) utilizing the vaporizing explosive force, injects it into the uppermost stream of the all-blade steam turbine, and vaporizes after output is generated An all-blade steam gas turbine combined engine characterized by recovering heat with a latent heat recovery device (66a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization and explosion force, and is injected into the uppermost stream of the all-blade steam turbine to output power. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery device (66a) after generation.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive power to the uppermost stream of the all-blade steam turbine, and recovers the latent heat of vaporization after the output is generated. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a vessel (66a).

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A high-temperature water injection nozzle (59a), which is connected to a water pipe (6a) and heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force, is injected to the uppermost stream of all the blade steam turbines. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a vaporization latent heat recovery device (66a).

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade steam turbine to generate output. An all-blade steam gas turbine combined engine characterized in that heat is later recovered by a vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the high-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosion force are injected to the uppermost stream of the all-blade steam turbine. A combined blade / steam gas turbine engine characterized in that after output is generated, heat is recovered by a vaporizing latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporizing explosive force to inject the uppermost stream of the all-blade steam turbine, and vaporize after generating power. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected to the uppermost stream of the all-blade steam turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power and output. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery unit (66a) after generation and supplied to the combustor / heat exchanger 4.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), the hot-water injection nozzle (59a) heated to a high temperature by the heating / high-temperature means (101) utilizing the vaporizing explosive force, injects it into the uppermost stream of the all-blade steam turbine, and vaporizes after output is generated An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization and explosion force, and is injected into the uppermost stream of the all-blade steam turbine to output power. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery unit (66a) after generation and supplied to the combustor / heat exchanger 4.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive power to the uppermost stream of the all-blade steam turbine, and recovers the latent heat of vaporization after the output is generated. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a heat exchanger (66a) and supplied to the combustor / heat exchanger 4.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A high-temperature water injection nozzle (59a), which is connected to a water pipe (6a) and heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force, is injected to the uppermost stream of all the blade steam turbines. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade steam turbine to generate output. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to consumers as warm heat.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the high-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosion force are injected to the uppermost stream of the all-blade steam turbine. A combined rotor blade steam gas turbine engine characterized in that after the output is generated, heat is recovered by a vaporizing latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to the customer as warm heat.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporizing explosive force to inject the uppermost stream of the all-blade steam turbine, and vaporize after generating power. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to consumers as warm heat.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected to the uppermost stream of the all-blade steam turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power and output. A combined rotor blade steam gas turbine engine characterized in that heat is recovered by a vaporization latent heat recovery unit (66a) after the generation and supplied to the combustor / heat exchanger 4 and supplied to the customer as warm heat.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), the hot-water injection nozzle (59a) heated to a high temperature by the heating / high-temperature means (101) utilizing the vaporizing explosive force, injects it into the uppermost stream of the all-blade steam turbine, and vaporizes after output is generated An all-blade steam gas turbine combined engine characterized in that heat is recovered by a latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to consumers as warm heat.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the high-temperature water injection nozzle (59a), which is heated to a high temperature by the high-temperature heating means (101) using the vaporization and explosion force, and is injected into the uppermost stream of the all-blade steam turbine to output power. A combined rotor blade steam gas turbine engine characterized in that heat is recovered by a vaporization latent heat recovery unit (66a) after the generation and supplied to the combustor / heat exchanger 4 and supplied to the customer as warm heat.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And injects it from the high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive power to the uppermost stream of the all-blade steam turbine, and recovers the latent heat of vaporization after the output is generated. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a unit (66a) and supplied to the combustor / heat exchanger 4 and supplied to consumers as warm heat.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). A high-temperature water injection nozzle (59a), which is connected to a water pipe (6a) and heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force, is injected to the uppermost stream of all the blade steam turbines. An all-blade steam gas turbine combined engine characterized in that heat is recovered by a vaporization latent heat recovery device (66a) and supplied to the combustor / heat exchanger 4 and supplied to consumers as warm heat.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force to inject the uppermost stream of the full-blade steam gas turbine. All-blade steam gas turbine united engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization and explosive power to inject the uppermost stream of the full-blade steam gas turbine. All-blade steam gas turbine combined engine characterized by

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive force to inject the uppermost stream of the all-blade steam gas turbine. All blade steam gas turbine combined engine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). Communicating with the water pipe (6a) and injecting it to the uppermost stream of the all-blade steam gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power. All-blade steam gas turbine combined engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive force to inject the gas into the uppermost stream of all blade gas turbines. All-blade steam gas turbine combined engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is used to inject into the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101) using vaporization explosive power. This is a combined rotor blade steam gas turbine engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive force to inject the uppermost stream of the full blade gas turbine. Combined moving blade steam gas turbine engine.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). By communicating with the water pipe (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosion force can be injected to the uppermost stream of the all-blade gas turbine. All-blade steam gas turbine united engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade steam gas turbine, and An all-blade steam gas turbine combined engine characterized in that combustion gas (10) is supplied to an optimal stage and cooled by high-temperature water (5a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization and explosive power to inject the uppermost stream of the full-blade steam gas turbine. And an all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the middle stage optimal stage and cooled by the high-temperature water (5a).

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization and explosion force to inject the uppermost stream of the all-blade steam gas turbine, and to optimize the middle stream An all-blade steam gas turbine combined engine, characterized in that a combustion gas (10) is supplied to the engine and cooled by high-temperature water (5a).

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected from the plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine utilizing the vaporization and explosion power, An all-blade steam gas turbine combined engine characterized in that a combustion gas (10) is supplied to a middle flow optimum stage and cooled by high-temperature water (5a).

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade gas turbine, and optimize the middle stream. An all-blade steam gas turbine combined engine, characterized in that combustion gas (10) is supplied to the stage and cooled by high-temperature water (5a).

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization and explosive power. An all-blade steam gas turbine combined engine, characterized in that the combustion gas (10) is supplied to the middle stage optimal stage and cooled by the high-temperature water (5a).

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization and explosion force to inject the uppermost stream of the all-blade gas turbine to the middle stage optimal stage. An all-blade steam gas turbine combined engine characterized by supplying combustion gas (10) and cooling with high-temperature water (5a).

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected to the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive force. An all-blade steam gas turbine combined engine characterized in that combustion gas (10) is supplied to an optimal stage and cooled by high-temperature water (5a).

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade steam gas turbine, and An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimal stage, cooled by the high-temperature water (5a), expanded into the low-temperature combustion gas, and coagulate moisture.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization and explosive power to inject the uppermost stream of the full-blade steam gas turbine. An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the middle stage optimal stage, cooled by the high-temperature water (5a), expanded into the low-temperature combustion gas, and coagulates moisture.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization and explosion force to inject the uppermost stream of the all-blade steam gas turbine, and to optimize the middle stream An all-blade steam gas turbine combined engine characterized in that a combustion gas (10) is supplied to the cooling blade and cooled by high-temperature water (5a), and expands into a low-temperature combustion gas to coagulate moisture.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected from the plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine utilizing the vaporization and explosion power, An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the middle stage optimal stage, cooled by the high temperature water (5a), expanded into the low temperature combustion gas, and coagulates moisture.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade gas turbine, and optimize the middle stream. An all-blade steam gas turbine combined engine characterized in that a combustion gas (10) is supplied to a stage, cooled by high-temperature water (5a), and expanded into a low-temperature combustion gas to coagulate moisture.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization and explosive power. An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the middle stage optimal stage, cooled by the high-temperature water (5a), expanded into the low-temperature combustion gas, and coagulates moisture.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization and explosion force to inject the uppermost stream of the all-blade gas turbine to the middle stage optimal stage. An all-blade steam gas turbine combined engine characterized by supplying a combustion gas (10), cooling it with high-temperature water (5a), expanding into a low-temperature combustion gas, and coagulating moisture.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected to the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive force. An all-blade steam gas turbine combined engine characterized in that the combustion gas (10) is supplied to the optimal stage, cooled by the high-temperature water (5a), expanded into the low-temperature combustion gas, and coagulate moisture.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade steam gas turbine, and The all-blade steam gas is characterized in that the combustion gas (10) is supplied to the optimal stage, cooled with the high-temperature water (5a), expanded into the low-temperature combustion gas, and condensed with water to enable a condenser vacuum. Turbine united engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization and explosive power to inject the uppermost stream of the full-blade steam gas turbine. Then, the combustion gas (10) is supplied to the middle stage optimal stage, cooled by the high-temperature water (5a), expanded into the low-temperature combustion gas, and coagulates moisture to enable a condenser vacuum. Wing steam gas turbine combined engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization and explosion force to inject the uppermost stream of the all-blade steam gas turbine, and to optimize the middle stream The combustion blade (10) is supplied to the turbine and cooled by the high-temperature water (5a), and expands to the low-temperature combustion gas to condense the water to enable a condenser vacuum, thereby enabling a condenser vacuum. organ.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected from the plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine utilizing the vaporization and explosion power, A full-blade steam characterized in that the combustion gas (10) is supplied to the middle-stage optimum stage, cooled with high-temperature water (5a), expanded into low-temperature combustion gas, and coagulates moisture to enable condenser vacuum. Gas turbine combined engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade gas turbine, and optimize the middle stream. A full-blade steam gas turbine characterized in that a combustion gas (10) is supplied to a stage, cooled by high-temperature water (5a), expanded into a low-temperature combustion gas, and coagulates moisture to enable condenser vacuum. Coalition organization.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization and explosive power. The whole rotor blade is characterized in that the combustion gas (10) is supplied to the middle stage optimal stage, cooled by the high-temperature water (5a), expanded into the low-temperature combustion gas, and coagulates moisture to enable a condenser vacuum. Steam gas turbine combined engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization and explosion force to inject the uppermost stream of the all-blade gas turbine to the middle stage optimal stage. Combined all-blade steam gas turbine engine characterized in that a combustion gas (10) is supplied and cooled by high-temperature water (5a), and expands into a low-temperature combustion gas to coagulate moisture to enable condenser vacuum. .

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected to the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive force. The all-blade steam gas is characterized in that the combustion gas (10) is supplied to the optimal stage, cooled with the high-temperature water (5a), expanded into the low-temperature combustion gas, and condensed with water to enable a condenser vacuum. Turbine united engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade steam gas turbine, and All blade steam gas characterized in that the combustion gas (10) is supplied to the optimal stage, cooled with high-temperature water (5a), expanded into a low-temperature combustion gas, coagulates moisture, and makes exhaust such as CO2 close to zero. Turbine united engine.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). High-temperature water pipe (6a), and a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization and explosive power to inject the uppermost stream of the full-blade steam gas turbine. Then, the combustion gas (10) is supplied to the middle flow optimal stage, cooled by the high-temperature water (5a), expanded into the low-temperature combustion gas, and the water is agglomerated to make the exhaust gas such as CO2 close to zero. Wing steam gas turbine combined engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization and explosion force to inject the uppermost stream of the all-blade steam gas turbine, and to optimize the middle stream The combustion blade (10) is supplied to the cooling blade, cooled by high-temperature water (5a), expanded into a low-temperature combustion gas, coagulated with water, and the exhaust gas such as CO2 is brought close to zero. organ.

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected from the plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101) to the uppermost stream of the all-blade steam gas turbine utilizing the vaporization and explosion power, The all-blade steam is characterized in that the combustion gas (10) is supplied to the middle-stage optimum stage, cooled with high-temperature water (5a), expanded into low-temperature combustion gas, and coagulates moisture to bring exhaust such as CO2 close to zero. Gas turbine combined engine.

The high temperature water pipe of each high temperature water control valve (7a) is maximized by the combustor / heat exchanger (4) to maximize the high temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) for reducing the fuel combustion mass. (6a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosion force to inject the uppermost stream of the all-blade gas turbine, and optimize the middle stream. An all-blade steam gas turbine characterized in that a combustion gas (10) is supplied to a stage, cooled with high-temperature water (5a), expanded into a low-temperature combustion gas, and condensed with water to make exhaust gas such as CO2 close to zero. Coalition organization.

The supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery unit (66a) that reduces the fuel combustion mass is maximized by the combustor / heat exchanger (4) to increase the high-temperature water control valve (7a). The high-temperature water pipe (6a) is connected to the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization and explosive power. The entire moving blade is characterized in that the combustion gas (10) is supplied to the middle stage optimal stage, cooled with the high-temperature water (5a), expanded into the low-temperature combustion gas, coagulates moisture, and makes exhaust such as CO2 close to zero. Steam gas turbine combined engine.

The high-temperature water pipes (6a) of the respective high-temperature water control valves (7a) are converted into high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass by the combustor / heat exchanger (4). ), And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization and explosion force to inject the uppermost stream of the all-blade gas turbine to the middle stage optimal stage. Combined all-blade steam gas turbine engine characterized in that the combustion gas (10) is supplied and cooled by the high-temperature water (5a), expanded to the low-temperature combustion gas and coagulates the water to make the exhaust gas such as CO2 close to zero. .

A supercritical pressure high-temperature water recovery heat including the recovery heat of the vaporization latent heat recovery device (66a) for reducing the fuel combustion mass is obtained by the combustor / heat exchanger (4). It is connected to the water pipe (6a), and is injected to the uppermost stream of the all-blade gas turbine from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive force. All blade steam gas characterized in that the combustion gas (10) is supplied to the optimal stage, cooled with high-temperature water (5a), expanded into a low-temperature combustion gas, coagulates moisture, and makes exhaust such as CO2 close to zero. Turbine united engine.

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water control valve (7a) is used. An all-blade steam gas turbine characterized in that it is connected to a high-temperature water reservoir (32a) and is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by a high-temperature heating means (101) using vaporization explosive power. Coalition organization.

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the highest flow of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). A high-temperature water reservoir (32a), and injecting from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force. Turbine united engine.

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and each high-temperature water reservoir at the uppermost stream of the all-blade gas turbine and the principle of spraying (91a) by each high-temperature water control valve (7a). (32a), and a plurality of high-temperature water injection nozzles (59a), which are heated and heated to a high temperature by a high-temperature heating means (101) using vaporization and explosive power, and are injected from the plurality of moving blade steam gas turbine combined engines. .

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water of the most upstream of the all-blade steam gas turbine and the principle of spraying (91a) is obtained by each high-temperature water control valve (7a). Combined with a plurality of high-pressure water jet nozzles (59a), which are connected to a water reservoir (32a) and heated to a high temperature by a high-temperature heating means (101) using vaporization explosive force, and are injected from a plurality of high-temperature water injection nozzles (59a). organ.

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water control valve (7a) is used. Communicating to the high-temperature water reservoir (32a), it injects from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101) using vaporization explosive power, and supplies combustion gas to the optimum middle flow stage. All-blade steam gas turbine combined engine characterized by output.

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the highest flow of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). High-temperature water reservoir (32a), and injects from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive force to supply combustion gas to the optimum middle flow stage. An all-blade steam gas turbine combined engine characterized by output.

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and each high-temperature water reservoir at the uppermost stream of the all-blade gas turbine and the principle of spraying (91a) by each high-temperature water control valve (7a). (32a), the fuel is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power, and combustion gas is supplied to an optimal middle stage and output. All-blade steam gas turbine combined engine characterized by

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water of the most upstream of the all-blade steam gas turbine and the principle of spraying (91a) is obtained by each high-temperature water control valve (7a). By contacting the water reservoir (32a) and injecting from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power, the combustion gas is supplied to the optimum middle flow stage. An all-blade steam gas turbine combined engine characterized by output.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water sump (7a) and the most upstream high-temperature water reservoir (91a) of the all-blade gas turbine and the plurality of spraying principles (91a). 32a), the fuel is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive force, and the combustion gas is supplied to and output to the optimum middle flow stage. This is a combined rotor blade steam gas turbine engine.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat quantity to the high-temperature water sump of each of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). (32a), the fuel is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power, and combustion gas is supplied to an optimal middle stage and output. All-blade steam gas turbine combined engine characterized by

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water control valve (7a) and the uppermost stream high-temperature water reservoir (32a) of the all-blade gas turbine and the principle of spraying (91a). And a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power to inject the combustion gas to the optimum middle-stage and output it. All-blade steam gas turbine united engine.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water control valve (7a). ), Injecting from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power, and supplying and outputting combustion gas to an optimal middle stage. All-blade steam gas turbine combined engine.

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water control valve (7a) is used. Communicating to the high-temperature water reservoir (32a), it injects from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101) using vaporization explosive power, and supplies combustion gas to the optimum middle flow stage. An all-blade steam gas turbine united engine characterized by suctioning and injecting air in front of each output air.

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the highest flow of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). High-temperature water reservoir (32a), and injects from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive force to supply combustion gas to the optimum middle flow stage. An all-blade steam gas turbine combined engine characterized by suctioning and injecting and propelling air in front of each output.

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and each high-temperature water reservoir at the uppermost stream of the all-blade gas turbine and the principle of spraying (91a) by each high-temperature water control valve (7a). (32a), the fuel is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power, and combustion gas is supplied to an optimal middle stage and output. An all-blade steam gas turbine combined engine characterized by sucking forward air and propelling it.

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water of the most upstream of the all-blade steam gas turbine and the principle of spraying (91a) is obtained by each high-temperature water control valve (7a). By contacting the water reservoir (32a) and injecting from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power, the combustion gas is supplied to the optimum middle flow stage. An all-blade steam gas turbine united engine characterized by sucking the air in front of each output air and propelling it.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water sump (7a) and the most upstream high-temperature water reservoir (91a) of the all-blade gas turbine and the plurality of spraying principles (91a). 32a), the fuel is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using the vaporization explosive force, and the combustion gas is supplied to and output to the optimum middle flow stage. An all-blade steam gas turbine combined engine characterized by sucking forward air and propelling it.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat quantity to the high-temperature water sump of each of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). (32a), the fuel is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive power, and combustion gas is supplied to an optimal middle stage and output. An all-blade steam gas turbine combined engine characterized by sucking forward air and propelling it.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water control valve (7a). And injects from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force, and supplies and outputs combustion gas to an optimal middle stage. An all-blade steam gas turbine combined engine characterized by sucking air and propelling it.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water control valve (7a) and the uppermost stream high-temperature water reservoir (32a) of the all-blade steam gas turbine and the principle of spraying (91a). ), And injects from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power to supply and output combustion gas to an optimal middle stage. An all-blade steam gas turbine combined engine characterized by sucking forward air for jet propulsion.

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water control valve (7a) is used. A high-temperature water reservoir (32a) is contacted and is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by a high-temperature heating means (101) using vaporization and explosive power to form an annular combustion gas reservoir (9). An all-blade steam gas turbine combined engine characterized by injecting combustion gas (10) by the principle of spraying (91b).

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the highest flow of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). The high-temperature water reservoir (32a) is connected to the combustion gas reservoir (9) using a vaporizing explosive force to inject from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101). The combustion gas (10) is injected by the spraying principle (91b).

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and each high-temperature water reservoir at the uppermost stream of the all-blade steam turbine and the principle of spraying (91a) is obtained by each high-temperature water control valve (7a). (32a), and is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive force, and the combustion gas in the annular combustion gas reservoir (9) is discharged. An integrated all-blade steam gas turbine engine characterized in that (10) is injected by the principle of spraying (91b).

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water of the most upstream of the all-blade steam gas turbine and the principle of spraying (91a) is obtained by each high-temperature water control valve (7a). Communicating with the water reservoir (32a), the fuel is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive power, and the annular combustion gas reservoir (9) is burned. An all-blade steam gas turbine combined engine characterized by injecting gas (10) by the principle of spraying (91b).

The combustor / heat exchanger (4) converts the amount of high-temperature water recovered to heat, and the respective high-temperature water control valves (7a). 32a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosive force to inject the combustion gas (59) in the annular combustion gas reservoir (9). 10) is an all-blade steam gas turbine combined engine characterized by injecting by the principle of spraying (91b).

The combustor / heat exchanger (4) converts the high-temperature water recovery heat quantity to the high-temperature water sump of each of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). (32a), and is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive force, and the combustion gas in the annular combustion gas reservoir (9) is discharged. An integrated all-blade steam gas turbine engine characterized in that (10) is injected by the principle of spraying (91b).

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water control valve (7a) and the uppermost stream high-temperature water reservoir (32a) of the all-blade steam turbine and the principle of spraying (91a). The combustion gas (10) is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the vaporization explosive force, and the annular combustion gas reservoir (9). All-blade steam gas turbine combined engine characterized by injecting gas from the spraying principle (91b).

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water control valve (7a) and the uppermost stream high-temperature water reservoir (32a) of the all-blade steam gas turbine and the principle of spraying (91a). ), And is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive force, and the combustion gas (10) in the annular combustion gas reservoir (9) is discharged. ) Is injected by the principle of spraying (91b).

Combustor / heat exchanger (4) is used to convert the superheated high-temperature water recovery heat into supercritical pressure high-temperature water control valve (7a) and communicate with the uppermost stream of all-blade steam turbine and multiple spraying principles (91a). The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed by spraying from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injection according to the principle (91b).

Combustor / heat exchanger (4), supercritical pressure high-temperature water recovery heat quantity, each hot-water control valve (7a) communicates with all rotor blade steam gas turbine and the uppermost stream of multiple atomization principle (91a) Then, the combustion gas (10) in the annular combustion gas reservoir (9) is atomized by spraying from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injecting according to the principle (91b).

Combustor / heat exchanger (4), supercritical pressure high-temperature water recovery heat quantity, each hot-water control valve (7a) communicates with the uppermost stream of all-blade steam turbine and the principle of spraying (91a), The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the vaporization explosive force. 91b) All-blade steam gas turbine combined engine characterized by injection from

Combustor / heat exchanger (4) is used to convert the supercritical pressure high-temperature water recovery heat quantity to the highest flow of the all-blade steam gas turbine and the principle of atomization (91a) by each high-temperature water control valve (7a). The principle of spraying the combustion gas (10) in the annular combustion gas reservoir (9) by injecting it from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive force. (91b) An all-blade steam gas turbine combined engine characterized by injecting from the (91b).

The combustor / heat exchanger (4) is used to convert the high-temperature water recovery heat to the all-blade steam turbine and the uppermost stream of the plurality of spraying principles (91a) via respective high-temperature water control valves (7a) for vaporization. The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the explosive force. ) An all-blade steam gas turbine combined engine characterized by more injection.

The combustor / heat exchanger (4) is used to convert the high-temperature water recovery heat quantity to the uppermost stream of the all-blade steam gas turbine and the plurality of spraying principles (91a) through respective high-temperature water control valves (7a). The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the vaporization explosive force. 91b) All-blade steam gas turbine combined engine characterized by injection from

The combustor / heat exchanger (4) is used to convert the high-temperature water recovery heat into high-temperature water control valves (7a) and communicate with the uppermost stream of the all-blade steam turbine and the principle of mist spraying (91a) by vaporization and explosion power. The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating high-temperature means (101) using the principle of spraying (91b). All-blade steam gas turbine combined engine characterized by injection.

The combustor / heat exchanger (4) is used to convert the high-temperature water recovery heat to the uppermost stream of the all-blade steam gas turbine and the principle of spraying (91a) via the respective high-temperature water control valves (7a) to evaporate and explode. The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using the force. All-blade steam gas turbine combined engine characterized by more injection.

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water control valve (7a) is used. A high-temperature water reservoir (32a) is contacted and is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by a high-temperature heating means (101) using vaporization and explosive power to form an annular combustion gas reservoir (9). An all-blade steam gas turbine combined engine characterized by injecting the combustion gas (10) by the principle of spraying (91b) and sucking forward air to propelle the injection.

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the highest flow of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). The high-temperature water reservoir (32a) is connected to the combustion gas reservoir (9) using a vaporizing explosive force to inject from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101). A combustion blade (91b) for spraying the combustion gas (10) according to the principle of spraying, and sucking forward air to propelle and inject the combustion gas.

Supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and each high-temperature water reservoir at the uppermost stream of the all-blade steam turbine and the principle of spraying (91a) by each high-temperature water control valve (7a). (32a), and is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive force, and the combustion gas in the annular combustion gas reservoir (9) is discharged. (10) The all-blade steam gas turbine combined engine characterized by injecting (10) based on the principle of spraying (91b), and sucking forward air to propelle and inject.

A supercritical pressure high-temperature water recovery heat quantity is obtained by a combustor / heat exchanger (4), and a high-temperature water of the most upstream of the all-blade steam gas turbine and the principle of spraying (91a) is obtained by each high-temperature water control valve (7a). Communicating with the water reservoir (32a), the fuel is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive power, and the annular combustion gas reservoir (9) is burned. An all-blade steam gas turbine combined engine characterized by injecting gas (10) according to the principle of spraying (91b) and sucking forward air to eject and propelle.

The combustor / heat exchanger (4) converts the amount of high-temperature water recovered to heat, and the respective high-temperature water control valves (7a). 32a), a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing the vaporization explosive force to inject the combustion gas (59) in the annular combustion gas reservoir (9). 10) is injected by the principle of spraying (91b), and the forward blade air is suctioned by each of them to propelle and inject.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat quantity to the high-temperature water sump of each of the all-blade steam gas turbine and the plurality of atomization principles (91a) by the respective high-temperature water control valves (7a). (32a), and is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the high-temperature heating means (101) utilizing vaporization explosive force, and the combustion gas in the annular combustion gas reservoir (9) is discharged. (10) The all-blade steam gas turbine combined engine characterized by injecting (10) based on the principle of spraying (91b), and sucking forward air to propelle and inject.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water control valve (7a), and the uppermost stream high-temperature water reservoir (32a) of the all-blade steam turbine and the principle of spraying (91a). The combustion gas (10) is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the vaporization explosive force, and the annular combustion gas reservoir (9). All steam turbine combined engines characterized by injecting air through the principle of spraying (91b), suctioning the air in front, and injecting and propelling.

The combustor / heat exchanger (4) converts the high-temperature water recovery heat into the high-temperature water control valve (7a) and the uppermost stream high-temperature water reservoir (32a) of the all-blade steam gas turbine and the principle of spraying (91a). ), And is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive force, and the combustion gas (10) in the annular combustion gas reservoir (9) is discharged. ) Is sprayed according to the principle of spraying (91b), and the forward blade air is suctioned by each of the spraying and the jetting is propelled.

Combustor / heat exchanger (4) is used to convert the superheated high-temperature water recovery heat into supercritical pressure high-temperature water control valve (7a) and communicate with the uppermost stream of all-blade steam turbine and multiple spraying principles (91a). The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed by spraying from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting according to the principle (91b) and sucking forward air by each injecting and propelling.

Combustor / heat exchanger (4), supercritical pressure high-temperature water recovery heat quantity, each hot-water control valve (7a) communicates with all rotor blade steam gas turbine and the uppermost stream of multiple atomization principle (91a) Then, the combustion gas (10) in the annular combustion gas reservoir (9) is atomized by spraying from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power. The all-blade steam gas turbine combined engine is characterized by injecting according to the principle (91b), suctioning the air in front of each, and injecting and propelling.

Combustor / heat exchanger (4), supercritical pressure high-temperature water recovery heat quantity, each hot-water control valve (7a) communicates with the uppermost stream of all-blade steam turbine and the principle of spraying (91a), The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the vaporization explosive force. 91b) An all-blade steam gas turbine combined engine characterized by injecting air from each of them and sucking forward air to propelle the air.

Combustor / heat exchanger (4) is used to convert the supercritical pressure high-temperature water recovery heat quantity to the highest flow of the all-blade steam gas turbine and the principle of atomization (91a) by each high-temperature water control valve (7a). The principle of spraying the combustion gas (10) in the annular combustion gas reservoir (9) by injecting it from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using the vaporization explosive force. (91b) An all-blade steam gas turbine combined engine characterized by injecting from above and sucking forward air to inject and propulse.

The combustor / heat exchanger (4) is used to convert the high-temperature water recovery heat to the all-blade steam turbine and the uppermost stream of the plurality of spraying principles (91a) via respective high-temperature water control valves (7a) for vaporization. The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the explosive force. ) All-blade steam gas turbine combined engines characterized by injecting more air and sucking forward air to promote injection.

The combustor / heat exchanger (4) is used to convert the high-temperature water recovery heat quantity to the uppermost stream of the all-blade steam gas turbine and the plurality of spraying principles (91a) through respective high-temperature water control valves (7a). The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) utilizing the vaporization explosive force. 91b) An all-blade steam gas turbine combined engine characterized by injecting air from each of them and sucking forward air to propelle the air.

The combustor / heat exchanger (4) is used to convert the high-temperature water recovery heat into high-temperature water control valves (7a) and communicate with the uppermost stream of the all-blade steam turbine and the principle of mist spraying (91a) by vaporization and explosion power. The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating high-temperature means (101) using the principle of spraying (91b). An all-blade steam gas turbine combined engine characterized by injecting and sucking forward air by each to propel the jet.

The combustor / heat exchanger (4) is used to convert the high-temperature water recovery heat to the uppermost stream of the all-blade steam gas turbine and the principle of spraying (91a) via the respective high-temperature water control valves (7a) to evaporate and explode. The combustion gas (10) in the annular combustion gas reservoir (9) is sprayed from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) using the force. An all-blade steam gas turbine combined engine characterized by injecting more air and sucking forward air to propelle each.

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). A plurality of high-temperature water jet nozzles (59a) are connected to the high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) and heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force. All-blade steam gas turbine combined engine characterized by injection.

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). The all-blade steam gas is characterized in that the hot-water sump (32a) of each of the uppermost stream and the middle stream of the principle (91c) is connected to and injected from a plurality of high-temperature water injection nozzles (59a) by utilizing vaporization explosive power. Turbine united engine.

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are jetted from a plurality of high-temperature water jet nozzles (59a) which have been heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive force. This is a combined rotor blade steam gas turbine engine.

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). 91b) Combined with all the high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c), and are injected from a plurality of high-temperature water injection nozzles (59a) using vaporization explosive force. organ.

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). A plurality of high-temperature water jet nozzles (59a) are connected to the high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) and heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting all combustion gas (10) from one or more nozzles based on the principle of spraying and spraying (91d).

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) are connected to each other, and are sprayed from a plurality of high-temperature water injection nozzles (59a) by utilizing vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting all of the combustion gas (10) from the above nozzles.

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are jetted from a plurality of high-temperature water jet nozzles (59a) which have been heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injecting all combustion gas (10) from one or more nozzles based on the principle of spraying (91d).

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are sprayed from a plurality of high-temperature water spray nozzles (59a) by using vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting all combustion gas (10) from a nozzle.

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). A plurality of high-temperature water jet nozzles (59a) are connected to the high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) and heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting the entire combustion gas (10) from one or more nozzles based on the principle of spraying and spraying (91d), sucking water in front of the combustion gas, and propelling the water.

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) are connected to each other, and are sprayed from a plurality of high-temperature water injection nozzles (59a) by utilizing vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting all of the combustion gas (10) from the above nozzles, sucking forward water, and injecting the water.

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are jetted from a plurality of high-temperature water jet nozzles (59a) which have been heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power. An all-blade steam gas turbine combined engine characterized by injecting all combustion gas (10) from one or more nozzles based on the principle of spraying (91d), sucking water in front of each, and propelling the jet.

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are sprayed from a plurality of high-temperature water spray nozzles (59a) by using vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting all of the combustion gas (10) from a nozzle, sucking water in front of each, and propelling the jet.

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). A plurality of high-temperature water jet nozzles (59a) are connected to the high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) and heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force. It is characterized by injecting all the combustion gas (10) from one or more nozzles based on the principle of spraying and spraying (91d), suctioning water in front of each, and injecting and propelling, and floating and propelling with exhaust from all blade steam turbine. All-blade steam gas turbine combined engine.

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) are connected to each other, and are sprayed from a plurality of high-temperature water injection nozzles (59a) by utilizing vaporization explosive force. A combined rotor blade steam gas turbine engine characterized by injecting all of the combustion gas (10) from the above nozzles, suctioning water in front of each nozzle, and injecting and propelling the same, and floating and propelling with exhaust from the entire rotor blade steam turbine.

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are jetted from a plurality of high-temperature water jet nozzles (59a) which have been heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power. The feature of the invention is that all the combustion gas (10) is injected from one or more nozzles based on the principle of spraying (91d), water in front of each nozzle is sucked and injected for propulsion. Combined moving blade steam gas turbine engine.

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are sprayed from a plurality of high-temperature water spray nozzles (59a) by using vaporization explosive force. An all-blade steam gas turbine combined engine characterized by injecting all of the combustion gas (10) from a nozzle, sucking water in front of each nozzle, and jetting and propelling the same, and floating and propelling with exhaust from the all-blade steam turbine.

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). A plurality of high-temperature water jet nozzles (59a) are connected to the high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) and heated to a high temperature by the high-temperature heating means (101) using vaporization explosive force. Inject and burn all the combustion gas (10) from one or more nozzles based on the principle of spraying (91d), suction the water in front of each, and propulse the spray, cool the water with the combustion gas and reduce CO2 etc. to the sea floor etc. An all-blade steam gas turbine combined engine that can be supplied to

The combustor / heat exchanger (4) converts the superheated high-temperature water recovery heat into a supercritical pressure high-temperature water control valve (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of the principle (91c) are connected to each other, and are sprayed from a plurality of high-temperature water injection nozzles (59a) by utilizing vaporization explosive force. All blades steam characterized by injecting all of the combustion gas (10) from the above nozzles, sucking water in front of each and propelling the water, cooling water with the combustion gas and supplying CO2 and the like to the sea floor and the like. Gas turbine combined engine.

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are jetted from a plurality of high-temperature water jet nozzles (59a) which have been heated to a high temperature by the heating and high-temperature means (101) using vaporization explosive power. Injecting all combustion gas (10) from one or more nozzles based on the principle of spraying (91d), sucking water in front of each, propelling and jetting, cooling water with combustion gas and supplying CO2 etc. to the sea floor etc. All-blade steam gas turbine combined engine characterized by

The superheated high-temperature water reservoir (32a) and the principle of spraying (32a) at the uppermost stream of the all-blade steam turbine are converted to the supercritical pressure high-temperature water recovery heat quantity by the combustor / heat exchanger (4) and the respective high-temperature water control valves (7a). The high-temperature water reservoirs (32a) of the uppermost stream and the middle stream of 91c) are connected to each other, and are sprayed from a plurality of high-temperature water spray nozzles (59a) by using vaporization explosive force. An all-blade steam gas turbine characterized by injecting all of the combustion gas (10) from the nozzles, sucking the water in front of each nozzle, propelling the water, cooling the water with the combustion gas, and supplying CO2 or the like to the sea floor or the like. Coalition organization.

An all-blade steam gas turbine combined engine characterized by injecting high-temperature water from a high-temperature water injection nozzle (59a) heated to a high temperature by a heating high-temperature means (101).

An all-blade steam gas turbine combined engine characterized by injecting supercritical high-temperature water from a high-temperature water injection nozzle (59a) heated to a high temperature by a heating high-temperature means (101).

An all-blade steam gas turbine combined engine characterized by injecting high-temperature water from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by a heating and high-temperature means (101).

An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by a heating high-temperature means (101).

The all-blade steam gas is characterized in that high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated in the nozzle like a machine gun bullet by a vaporization explosion force. Turbine united engine.

A supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by a heating high-temperature means (101), and accelerated in the nozzle by a vaporization explosion force like a bullet of a machine gun. Wing steam gas turbine combined engine.

A high-temperature water injection nozzle (59a) heated to a high temperature by the high-temperature heating means (101) injects high-temperature water from the plurality of high-temperature water injection nozzles (59a) and accelerates in the nozzle by a vaporizing explosion force like a bullet of a machine gun. Steam gas turbine combined engine.

It is characterized in that supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated to a high temperature by the heating and high-temperature means (101) and accelerated in the nozzle like a machine gun bullet in the nozzle by vaporization explosion. All blade steam gas turbine combined engine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. All-blade steam gas turbine combined engine characterized by acceleration.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. An all-blade steam gas turbine combined engine characterized by acceleration as follows.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. All-blade steam gas turbine combined engine characterized by acceleration.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized by acceleration like a shot rocket.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. An all-blade steam gas turbine combined engine characterized by optimal acceleration and utilization of latent heat of vaporization.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. An all-blade steam gas turbine combined engine characterized by optimal acceleration and utilization of latent heat of vaporization.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. All-blade steam gas turbine combined engine characterized by optimal acceleration and optimal use of latent heat of vaporization.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized by the optimal use of latent heat of vaporization by accelerating like a shot rocket.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. All-blade steam gas turbine combined engine characterized by acceleration and injection to all buckets.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. An all-blade steam gas turbine combined engine characterized by acceleration and injection to all buckets.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. All-blade steam gas turbine combined engine characterized by acceleration and injection to all buckets.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized by acceleration and injection to all buckets like a shot rocket.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. All-blade steam gas turbine combined engine characterized by accelerating and injecting into the uppermost stream of all blades.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating and injecting it into the uppermost stream of all the buckets.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. All-blade steam gas turbine combined engine that is accelerated and injected to the uppermost stream of all buckets.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket and injecting it into the uppermost stream of all buckets.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. An integrated all-blade steam gas turbine engine that is accelerated and injected into the uppermost stream of the all-blade gas turbine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. The combined rotor blade steam gas turbine engine is characterized by accelerating and injecting it into the uppermost stream of the rotor blade gas turbine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. All-blade steam gas turbine combined engine characterized in that it is accelerated and injected into the uppermost stream of the all-blade gas turbine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine that accelerates like a shot rocket and injects it into the uppermost stream of the all-blade gas turbine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. An all-blade steam gas turbine combined engine that is accelerated and injected into the uppermost stream of the all-blade steam gas turbine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. The combined bladed steam gas turbine engine is characterized in that it is accelerated and injected into the uppermost stream of the bladed steam gas turbine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. The combined bladed steam gas turbine engine is characterized in that it is accelerated and injected into the uppermost stream of the bladed steam gas turbine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized by being accelerated like a shot rocket and injected into the uppermost stream of the all-blade steam gas turbine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. A combined rotor blade steam gas turbine engine that is accelerated and injected into the uppermost stream of the rotor blade steam turbine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. An all-blade steam gas turbine combined engine characterized by accelerating and injecting into the uppermost stream of the all-blade steam turbine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. All-blade steam gas turbine combined engine, characterized in that it is accelerated and injected into the uppermost stream of all-blade steam turbine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine that accelerates like a shot rocket and injects it into the uppermost stream of the all-blade steam turbine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. An integrated all-steam steam gas turbine engine characterized by accelerating and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. The combined steam turbine engine is characterized by accelerating and injecting sequentially downstream from the uppermost stream of all blade gas turbines.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. The all-blade steam gas turbine combined engine is characterized by accelerating and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. A combined rotor blade steam gas turbine engine characterized in that it is accelerated and injected sequentially downstream from the uppermost stream of the rotor blade steam gas turbine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. The combined bladed steam gas turbine engine is characterized in that it is accelerated and injected sequentially downstream from the uppermost stream of the bladed steam gas turbine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. The combined bladed steam gas turbine engine is characterized in that it is accelerated and injected sequentially downstream from the uppermost stream of the bladed steam gas turbine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine that accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam gas turbine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. An integrated all-swing steam gas turbine engine that accelerates and injects sequentially downstream from the uppermost stream of the all-swing steam turbine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. The combined blade steam gas turbine engine is characterized by accelerating and injecting sequentially downstream from the uppermost stream of the bucket.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. In this case, the engine is accelerated and injected sequentially downstream from the uppermost stream of the turbine blade.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket and injecting sequentially downstream from the uppermost stream of the all-blade steam turbine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. An all-blade steam gas turbine combined engine characterized in that it is accelerated and injected sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. The combined rotor blade steam gas turbine engine is characterized in that it is accelerated as described above and is sequentially injected downstream from the uppermost stream of the all blade gas turbine to generate rotational output.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. In this manner, the engine is accelerated and sequentially injected downstream from the uppermost stream of the all-blade gas turbine to generate a rotational output.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized by accelerating like a shot rocket and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. A combined rotor blade steam gas turbine engine characterized in that it accelerates and sequentially injects downstream from the uppermost stream of the rotor blade steam gas turbine to generate rotational output.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. A combined rotor blade steam gas turbine engine characterized in that the rotor blades are accelerated and injected sequentially downstream from the uppermost stream of the rotor blade steam gas turbine to generate rotational output.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. The combined rotor blade steam gas turbine engine is characterized in that the rotor blades are accelerated in such a manner that they are sequentially injected downstream from the uppermost stream of the rotor blade steam gas turbine to generate rotational output.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. A combined rotor blade steam gas turbine engine characterized in that it accelerates like a shot rocket and injects it sequentially downstream from the uppermost stream of the rotor blade steam gas turbine to generate rotational output.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. A combined rotor blade steam gas turbine engine characterized in that it is accelerated and sequentially injected downstream from the uppermost stream of the rotor blade steam turbine to generate rotational output.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. The combined rotor blade steam gas turbine engine is characterized in that it is accelerated as described above and is sequentially injected downstream from the uppermost stream of the all blade steam turbine to generate a rotational output.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. The combined rotor blade steam gas turbine engine is characterized in that the rotor blades are accelerated in such a manner that they are sequentially injected downstream from the uppermost stream of the rotor blade steam turbine to generate a rotational output.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. A combined rotor blade steam gas turbine engine characterized by the fact that it accelerates like a shot rocket and injects it sequentially downstream from the uppermost stream of the rotor blade steam turbine to generate rotational output.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. A combined bladed steam gas turbine engine characterized in that it accelerates and injects sequentially downstream from the uppermost stream of the bladed steam turbine to generate rotational output up to adiabatic expanded atmospheric pressure.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. A combined rotor blade steam gas turbine engine characterized in that it is accelerated and injected sequentially downstream from the uppermost stream of the rotor blade steam turbine to generate rotational output up to the adiabatic expansion atmospheric pressure.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. A combined rotor blade steam gas turbine engine characterized in that it is accelerated in such a manner as to sequentially inject downstream from the uppermost stream of the all blade steam turbine to generate rotational output up to adiabatic expansion atmospheric pressure.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. An all-blade steam gas turbine combined engine characterized in that it accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to adiabatic expanded atmospheric pressure.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. All blade steam is characterized in that it is accelerated and sequentially injected downstream from the uppermost stream of the all blade steam turbine to generate a rotational output up to adiabatic expansion atmospheric pressure, and the vaporization latent heat is recovered by the vaporization latent heat recovery unit (66a). Gas turbine combined engine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. Is accelerated as described above and sequentially injected downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, and the latent heat of vaporization is recovered by the vaporized latent heat recovery device (66a). Combined moving blade steam gas turbine engine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. In this manner, the fuel is sequentially accelerated in the downstream direction from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, and the latent heat of vaporization is recovered by the vaporized latent heat recovery device (66a). Wing steam gas turbine combined engine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It is accelerated like a shot rocket and injected sequentially downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to the adiabatic expansion atmospheric pressure, and the latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a). All-blade steam gas turbine combined engine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. It accelerates and injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) to combust the all-blade gas turbine. An all-blade steam gas turbine combined engine characterized in that it is supplied to a heat exchanger (4).

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and the whole blade gas is recovered. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) of a turbine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. Is accelerated in such a manner as to be sequentially injected downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, and to collect the latent heat of vaporization by the vaporization latent heat recovery unit (66a) to collect the whole blade gas turbine. An all-blade steam gas turbine united engine characterized in that it is supplied to the combustor / heat exchanger (4) of the above.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to the adiabatic expanded atmospheric pressure, recovers the latent heat of vaporization with the vaporizing latent heat recovery unit (66a), and operates the entire turbine. An all-blade steam gas turbine united engine characterized in that it is supplied to a combustor / heat exchanger (4) of a blade gas turbine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. It accelerates and injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporization latent heat recovery unit (66a), and generates the rotating blade. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4).

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. , And sequentially injects downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a), and the whole blade steam is recovered. An all-blade steam gas turbine combined engine characterized in that it is supplied to a gas turbine combustor / heat exchanger (4).

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. Is accelerated in such a manner as to be sequentially injected downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) of a turbine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to the adiabatic expanded atmospheric pressure, recovers the latent heat of vaporization with the vaporizing latent heat recovery unit (66a), and operates the entire turbine. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) of a blade steam gas turbine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. It accelerates and injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) to combust the all-blade gas turbine. An all-blade steam gas turbine combined engine characterized in that it is supplied to a heat exchanger (4) to produce heated high-temperature water.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and the whole blade gas is recovered. An all-blade steam gas turbine united engine characterized in that it is supplied to a combustor / heat exchanger (4) of a turbine to produce heated high-temperature water.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. Is accelerated in such a manner as to be sequentially injected downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, and to collect the latent heat of vaporization by the vaporization latent heat recovery unit (66a) to collect the whole blade gas turbine. The combined blade and steam gas turbine engine is characterized in that it is supplied to the combustor / heat exchanger (4) to be heated to high-temperature water.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to the adiabatic expanded atmospheric pressure, recovers the latent heat of vaporization with the vaporizing latent heat recovery unit (66a), and operates the entire turbine. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) of a blade gas turbine to produce heated high-temperature water.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. It accelerates and injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporization latent heat recovery unit (66a), and generates the rotating blade. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) to produce heated high-temperature water.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. , And sequentially injects downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a), and the whole blade steam is recovered. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) of a gas turbine to produce heated high-temperature water.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. Is accelerated in such a manner as to be sequentially injected downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, and to collect the latent heat of vaporization by the vaporization latent heat recovery unit (66a) to collect the all-blade steam gas. An all-blade steam gas turbine united engine characterized in that it is supplied to a combustor / heat exchanger (4) of a turbine to produce heated high-temperature water.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to the adiabatic expanded atmospheric pressure, recovers the latent heat of vaporization with the vaporizing latent heat recovery unit (66a), and operates the entire turbine. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) of a blade steam gas turbine to produce heated high-temperature water.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. It accelerates and injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) to combust the all-blade gas turbine. An all-blade steam gas turbine combined engine characterized in that it is supplied to a heat exchanger (4) to produce heated high-temperature water and communicates with each high-temperature water control valve (7a).

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a) and the whole blade gas is recovered. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) of a turbine to produce heated high-temperature water and communicates with each high-temperature water control valve (7a).

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. Is accelerated in such a manner as to be sequentially injected downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, and to collect the latent heat of vaporization by the vaporization latent heat recovery unit (66a) to collect the whole blade gas turbine. The combined rotor / steam gas turbine engine characterized in that it is supplied to the combustor / heat exchanger (4) to be heated high-temperature water and connected to the respective high-temperature water control valves (7a).

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized by supplying heated high-temperature water to a combustor / heat exchanger (4) of a blade gas turbine and communicating with each high-temperature water control valve (7a).

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. It accelerates and injects sequentially downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporization latent heat recovery unit (66a), and generates the rotating blade. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) to produce heated high-temperature water and communicates with each high-temperature water control valve (7a).

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. , And sequentially injects downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a), and the whole blade steam is recovered. An all-blade steam gas turbine combined engine characterized by supplying heated high-temperature water to a combustor / heat exchanger (4) of a gas turbine and communicating with each high-temperature water control valve (7a).

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. Is accelerated in such a manner as to be sequentially injected downstream from the uppermost stream of the all-blade steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized in that it is supplied to a combustor / heat exchanger (4) of a turbine to produce heated high-temperature water and communicates with each high-temperature water control valve (7a).

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam turbine to generate rotational output up to the adiabatic expanded atmospheric pressure, recovers the latent heat of vaporization with the vaporizing latent heat recovery unit (66a), and operates the entire turbine. An all-blade steam gas turbine combined engine characterized by supplying heated high-temperature water to a combustor / heat exchanger (4) of a blade steam gas turbine and communicating with each high-temperature water control valve (7a).

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. A combined rotor blade steam gas turbine engine characterized in that it is accelerated and sequentially injected downstream from the uppermost stream of the rotor blade gas turbine to generate a rotational output and supply combustion gas (10) to an optimum middle stage.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. , And injects sequentially downstream from the uppermost stream of the all-blade gas turbine to generate a rotational output, and supplies the combustion gas (10) to the optimum middle-stream stage. organ.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. , And injects sequentially downstream from the uppermost stream of the all-blade gas turbine to generate a rotational output, and supplies the combustion gas (10) to the optimal middle-stream stage. .

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. A full-blade steam gas characterized in that it accelerates like a shot rocket and sequentially injects downstream from the uppermost stream of the all-blade gas turbine to generate a rotational output, and supplies combustion gas (10) to the optimum middle stage. Turbine united engine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. A combined rotor blade steam gas turbine engine characterized in that it is accelerated and sequentially injected downstream from the uppermost stream of the rotor blade steam gas turbine to generate a rotational output and supply combustion gas (10) to an optimal middle stage.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. The rotor blade steam gas turbine is characterized in that it is accelerated as described above and is sequentially injected downstream from the uppermost stream of the rotor blade steam gas turbine to generate a rotational output and supply the combustion gas (10) to the optimum middle stage. Coalition organization.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. , And injects sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output, and supplies the combustion gas (10) to the optimum middle-stream stage. organ.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. A full-blade steam characterized in that it accelerates like a shot rocket and sequentially injects downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output, and supplies combustion gas (10) to the optimum middle stage. Gas turbine combined engine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. All blade steam is characterized in that it is accelerated and sequentially injected downstream from the uppermost stream of the all blade gas turbine to generate a rotational output, and the combustion gas (10) is supplied to the optimal middle stage and cooled by high-temperature water. Gas turbine combined engine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. As described above, the engine is accelerated and injected sequentially downstream from the uppermost stream of the full-blade gas turbine to generate a rotational output, and the combustion gas (10) is supplied to the optimum middle stage and cooled by high-temperature water. Combined moving blade steam gas turbine engine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. In this manner, the engine is accelerated in such a manner as to sequentially inject the gas downstream from the uppermost stream of the all-blade gas turbine to generate a rotational output, supply the combustion gas (10) to the optimum middle-stage, and cool it with hot water. Wing steam gas turbine combined engine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It is accelerated like a shot rocket and injected sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output. The combustion gas (10) is supplied to the optimum middle stage and cooled by high-temperature water. All-blade steam gas turbine combined engine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. All blades are accelerated and sequentially injected downstream from the uppermost stream of a steam gas turbine to generate rotational output, and supply combustion gas (10) to an optimum middle stage to be cooled by high-temperature water. Steam gas turbine combined engine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And then sequentially injects downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output. The combustion gas (10) is supplied to the optimal middle stage and cooled by high-temperature water. All blade steam gas turbine combined engine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. In this manner, the fuel is accelerated in such a manner as to be sequentially injected downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output, and the combustion gas (10) is supplied to the optimal middle stage and cooled by high-temperature water. Combined moving blade steam gas turbine engine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. Like a shot rocket, it accelerates and injects it sequentially 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 high-temperature water. All-blade steam gas turbine united engine.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. It is possible to generate a rotational output by accelerating and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine to generate a rotational output by supplying the combustion gas (10) to the optimum middle stage and cooling it with high-temperature water. All-blade steam gas turbine united engine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And then injects sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output, supplies combustion gas (10) to the optimal middle stage and cools it with high-temperature water to generate rotational output All-blade steam gas turbine combined engine characterized by

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. Is accelerated in such a manner as to sequentially jet downstream from the uppermost stream of the all-blade gas turbine to generate a rotational output, and supply the combustion gas (10) to the optimal middle stage and cool it with high-temperature water to generate a rotational output. This is a combined rotor blade steam gas turbine engine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and injects it sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output. The combustion gas (10) is supplied to the optimal middle stage, cooled by high-temperature water, and rotated. All-blade steam gas turbine combined engine characterized by generating.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. Accelerate and inject sequentially downstream from the uppermost stream of a full-blade steam gas turbine to generate rotational output, supply combustion gas (10) to the optimum middle stage, cool with high-temperature water, and generate rotational output. All-blade steam gas turbine combined engine.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And then injects sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output. The combustion gas (10) is supplied to the optimum middle flow stage and cooled by high-temperature water to reduce the rotational output. An all-blade steam gas turbine united engine characterized by the generation.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. To generate a rotational output by injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine, supplying combustion gas (10) to the optimal middle stage and cooling it with high-temperature water to generate a rotational output All-blade steam gas turbine combined engine characterized by

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output. The combustion gas (10) is supplied to the optimum middle stage, cooled by high-temperature water and rotated. An all-blade steam gas turbine combined engine characterized by generating power.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. It accelerates and injects sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output, supplies combustion gas (10) to the optimal middle stage, cools it with high-temperature water, and generates rotational output. An all-blade steam gas turbine combined engine characterized by aggregating moisture with adiabatic expanded low-temperature combustion gas as the core.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And then injects sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output, supplies combustion gas (10) to the optimal middle stage and cools it with high-temperature water to generate rotational output An all-blade steam gas turbine combined engine characterized in that water is agglomerated with adiabatic expanded low-temperature combustion gas as the core during the process.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. As described above, the engine is accelerated and sequentially injected downstream from the uppermost stream of the all-blade gas turbine to generate a rotation output. The combustion gas (10) is supplied to the optimum middle flow stage, cooled by high-temperature water, and the rotation output is generated. An all-blade steam gas turbine combined engine characterized by agglomeration of water with adiabatic expanded low-temperature combustion gas as the core during the process.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and injects it sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output. The combustion gas (10) is supplied to the optimal middle stage, cooled by high-temperature water, and rotated. The all-blade steam gas turbine combined engine characterized in that water is agglomerated by adiabatic expanded low-temperature combustion gas as a nucleus in the process of generating.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. The process of accelerating and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, supplying combustion gas (10) to the optimum middle stage, cooling with high-temperature water, and generating rotational output An all-blade steam gas turbine combined engine characterized in that water is agglomerated with adiabatic expanded low-temperature combustion gas as the core.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And then injects sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output. The combustion gas (10) is supplied to the optimum middle flow stage and cooled by high-temperature water to reduce the rotational output. An all-blade steam gas turbine combined engine characterized by agglomeration of water with adiabatic expanded low-temperature combustion gas as the core during its generation.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. To generate a rotational output by injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine, supplying combustion gas (10) to the optimal middle stage and cooling it with high-temperature water to generate a rotational output An all-blade steam gas turbine combined engine characterized in that water is agglomerated with adiabatic expanded low-temperature combustion gas as the core during the process.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output. The combustion gas (10) is supplied to the optimum middle stage, cooled by high-temperature water and rotated. An all-blade steam gas turbine combined engine characterized by aggregating moisture with adiabatic expanded low-temperature combustion gas as the core during the process of generating power.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. In the process of accelerating and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output, supplying combustion gas (10) to the optimal middle stage and cooling with high-temperature water to generate rotational output An all-blade steam gas turbine combined engine characterized in that water is agglomerated with adiabatic expanded low-temperature combustion gas as a nucleus and exhaust such as CO2 is brought close to zero.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And then injects sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output, supplies combustion gas (10) to the optimal middle stage and cools it with high-temperature water to generate rotational output In this process, an adiabatic expanded low-temperature combustion gas is used as a nucleus to condense water to reduce exhaust gas such as CO2 to zero.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. As described above, the rotation is generated by sequentially accelerating and injecting sequentially downstream from the uppermost stream of the all-blade gas turbine, and supplying the combustion gas (10) to the optimum middle stage and cooling it with high-temperature water to generate the rotation output. An all-blade steam gas turbine combined engine characterized in that water is agglomerated by using adiabatic expanded low-temperature combustion gas as a nucleus in the process and exhaust gas such as CO2 approaches zero.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and injects it sequentially downstream from the uppermost stream of the all-blade gas turbine to generate rotational output. The combustion gas (10) is supplied to the optimal middle stage, cooled by high-temperature water, and rotated. The all-blade steam gas turbine combined engine characterized in that the adiabatic expanded low-temperature combustion gas is used as a nucleus in the process of generating water to condense water to reduce exhaust gas such as CO2 to zero.

High-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating and high-temperature means (101), and accelerated inside the nozzle by a vaporizing explosive force like a bullet of a machine gun, and outside the nozzle like a shot rocket. The process of accelerating and injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate rotational output, supplying combustion gas (10) to the optimum middle stage, cooling with high-temperature water, and generating rotational output An all-blade steam gas turbine combined engine characterized in that water is agglomerated with adiabatic expanded low-temperature combustion gas as a nucleus and exhaust such as CO2 approaches zero.

Supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) heated to a high temperature by the heating high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by a vaporization explosion force, and a shot rocket outside the nozzle. And then injects sequentially downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output. The combustion gas (10) is supplied to the optimum middle flow stage and cooled by high-temperature water to reduce the rotational output. An all-blade steam gas turbine combined engine characterized in that water is agglomerated by using adiabatic expanded low-temperature combustion gas as a nucleus in the process of generation and exhaust gas such as CO2 approaches zero.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerated inside the nozzle like a machine gun bullet by the vaporization and explosion force. To generate a rotational output by injecting sequentially downstream from the uppermost stream of the all-blade steam gas turbine, supplying combustion gas (10) to the optimal middle stage and cooling it with high-temperature water to generate a rotational output In this process, an adiabatic expanded low-temperature combustion gas is used as a nucleus to condense water to reduce exhaust gas such as CO2 to zero.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) heated and heated by the heating and high-temperature means (101), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosion. It accelerates like a shot rocket and sequentially injects it downstream from the uppermost stream of the all-blade steam gas turbine to generate a rotational output. The combustion gas (10) is supplied to the optimum middle stage, cooled by high-temperature water and rotated. An all-blade steam gas turbine combined engine, characterized in that water is agglomerated by using adiabatic expanded low-temperature combustion gas as a nucleus in the process of generating output to make exhaust such as CO2 close to zero.

An all-blade steam gas turbine combined engine characterized by injecting high-temperature water from a high-temperature water injection nozzle (59a).

An all-blade steam gas turbine combined engine characterized by injecting supercritical high-temperature water from a high-temperature water injection nozzle (59a).

An all-blade steam gas turbine combined engine characterized by injecting high-temperature water from a plurality of high-temperature water injection nozzles (59a).

An all-blade steam gas turbine combined engine characterized by injecting supercritical high-temperature water from a plurality of high-temperature water injection nozzles (59a).

An all-blade steam gas turbine combined engine characterized by injecting high-temperature water from a high-temperature water injection nozzle (59a) and accelerating like a machine gun bullet in the nozzle by vaporization explosion force.

An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water is injected from a high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a machine gun bullet by vaporization and explosive power.

An all-blade steam gas turbine combined engine characterized in that high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated in the nozzles by a vaporizing explosion force like a machine gun bullet.

An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzles like a machine gun bullet by vaporization and explosive power.

A high-pressure water jet nozzle (59a) injects high-temperature water and accelerates like a machine gun bullet inside the nozzle due to vaporization and explosive power, and accelerates like a shot rocket outside the nozzle. Turbine united engine.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a machine gun bullet by vaporization and explosive force, and accelerated outside the nozzle like a shot rocket. Wing steam gas turbine combined engine.

A high-speed water jet is injected from a plurality of high-temperature water jet nozzles (59a), and accelerates like a machine gun bullet inside the nozzle due to vaporization and explosive force, and accelerates like a shot rocket outside the nozzle by a vaporizing explosive force. Steam gas turbine combined engine.

It is characterized in that supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) to accelerate like a machine gun bullet inside the nozzle by vaporization and explosive force, and to accelerate like a shot rocket outside the nozzle. All blade steam gas turbine combined engine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated like a machine gun bullet inside the nozzle by vaporization explosion force, and accelerated like a shot rocket outside the nozzle to optimize the use of latent heat of vaporization. All-blade steam gas turbine united engine.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates like a machine gun bullet inside the nozzle by vaporization explosion force, and accelerates like a shot rocket outside the nozzle to optimize use of latent heat of vaporization All-blade steam gas turbine combined engine characterized by

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization explosion force, and accelerates outside the nozzle like a shot rocket to optimize use of latent heat of vaporization. This is a combined rotor blade steam gas turbine engine.

Supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerates like a machine gun bullet inside the nozzle by vaporization explosive force, and accelerates like a shot rocket outside the nozzle to reduce latent heat of vaporization. All-blade steam gas turbine combined engine characterized by optimal use.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosive power, and outside the nozzle accelerates like a shot rocket and sprays it on all blades. All-blade steam gas turbine united engine.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive power, and outside the nozzle accelerates like a shot rocket and sprays it on all blades All-blade steam gas turbine combined engine characterized by

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive power, and outside the nozzle accelerates like a shot rocket and injects it to all blades. This is a combined rotor blade steam gas turbine engine.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. All-blade steam gas turbine united engine characterized by injection into

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive power, and outside the nozzle accelerates like a shot rocket and injects it to the uppermost stream of all blades All-blade steam gas turbine combined engine characterized by

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a), and accelerates inside the nozzle like a machine gun bullet due to vaporization and explosive power, and outside the nozzle like a shot rocket, accelerating like a shot rocket. An all-blade steam gas turbine combined engine characterized by injection upstream.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosion force, and accelerates outside the nozzle like a shot rocket and is the most upstream of all blades All-blade steam gas turbine united engine characterized by injection into

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine united engine characterized by injection into the uppermost stream.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive force, and accelerates outside the nozzle like a shot rocket and is the uppermost stream of a full blade gas turbine. All-blade steam gas turbine united engine characterized by injection into

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun by vaporization and explosion force, and accelerates outside the nozzle like a shot rocket, and the whole rotor blade gas turbine An all-blade steam gas turbine united engine characterized by injection into the uppermost stream.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a machine gun bullet, and outside the nozzle like a shot rocket to accelerate the whole blade gas turbine. All-blade steam gas turbine combined engine characterized by injection at the most upstream.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. All-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the gas turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun. Outside the nozzle, it is accelerated like a shot rocket. An all-blade steam gas turbine combined engine characterized by injection upstream.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet by vaporization and explosive power, and outside the nozzle like a shot rocket, all-blade steam gas An all-blade steam gas turbine combined engine characterized by injection into the uppermost stream of the turbine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle is accelerated like a shot rocket, and the whole blade steam gas turbine An all-blade steam gas turbine united engine characterized by injection into the uppermost stream.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine united engine characterized by injection into the uppermost stream of a steam gas turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. All-blade steam gas turbine united engine characterized by injection into

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine An all-blade steam gas turbine united engine characterized by injection into the uppermost stream.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. All-blade steam gas turbine combined engine characterized by injection at the most upstream.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine united engine characterized by injection into the uppermost stream of a steam turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive force, and accelerates outside the nozzle like a shot rocket and is the uppermost stream of a full blade gas turbine. An all-blade steam gas turbine combined engine characterized by sequential injection downstream.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun by vaporization and explosion force, and accelerates outside the nozzle like a shot rocket, and the whole rotor blade gas turbine An all-blade steam gas turbine combined engine that injects sequentially downstream from the uppermost stream.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a machine gun bullet, and outside the nozzle like a shot rocket to accelerate the whole blade gas turbine. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the most upstream.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream of the gas turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun. Outside the nozzle, it is accelerated like a shot rocket. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from upstream.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet by vaporization and explosive power, and outside the nozzle like a shot rocket, all-blade steam gas An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream of the turbine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle is accelerated like a shot rocket, and the whole blade steam gas turbine An all-blade steam gas turbine combined engine that injects sequentially downstream from the uppermost stream.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream of the steam gas turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. An all-blade steam gas turbine combined engine characterized by sequential injection downstream.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine An all-blade steam gas turbine combined engine that injects sequentially downstream from the uppermost stream.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the most upstream.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream of the steam turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive force, and accelerates outside the nozzle like a shot rocket and is the uppermost stream of a full blade gas turbine. An integrated all-blade steam gas turbine engine characterized by generating rotation output by sequentially injecting downstream.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun by vaporization and explosion force, and accelerates outside the nozzle like a shot rocket, and the whole rotor blade gas turbine An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream to generate rotational output.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a machine gun bullet, and outside the nozzle like a shot rocket to accelerate the whole blade gas turbine. An all-blade steam gas turbine combined engine characterized by generating rotational output by injecting sequentially downstream from the uppermost stream.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by generating rotation output by sequentially injecting gas downstream from the uppermost stream of the gas turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun. Outside the nozzle, it is accelerated like a shot rocket. An all-blade steam gas turbine combined engine characterized by generating rotational output by injecting sequentially downstream from upstream.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet by vaporization and explosive power, and outside the nozzle like a shot rocket, all-blade steam gas An integrated all-blade steam gas turbine engine characterized by generating rotational output by injecting sequentially downstream from the uppermost stream of the turbine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle is accelerated like a shot rocket, and the whole blade steam gas turbine An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream to generate rotational output.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized in that rotation is generated by sequentially injecting steam downstream from the uppermost stream of the steam gas turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. An integrated all-blade steam gas turbine engine characterized by generating rotation output by sequentially injecting downstream.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream to generate rotational output.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. An all-blade steam gas turbine combined engine characterized by generating rotational output by injecting sequentially downstream from the uppermost stream.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by sequentially injecting steam downstream from the uppermost stream of the steam turbine to generate rotational output.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream to generate rotational output up to the adiabatic expanded atmospheric pressure.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine An all-blade steam gas turbine combined engine characterized by generating a rotational output up to the adiabatic expansion atmospheric pressure by injecting sequentially downstream from the uppermost stream.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. An all-blade steam gas turbine combined engine characterized by injecting sequentially from the upstream to the downstream to generate rotational output up to the adiabatic expanded atmospheric pressure.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by generating a rotational output up to the adiabatic expansion atmospheric pressure by injecting sequentially downstream from the uppermost stream of the steam turbine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. An all-blade steam gas turbine combined engine characterized by sequentially injecting downstream to generate rotational output up to adiabatic expanded atmospheric pressure and recovering latent heat of vaporization by a vaporizing latent heat recovery device (66a).

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine An all-blade steam gas turbine combined engine characterized by generating a rotational output up to the adiabatic expansion atmospheric pressure by sequentially injecting the gas from the uppermost stream to the downstream and recovering the latent heat of vaporization by the vaporized latent heat recovery unit (66a).

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream to generate rotational output up to the adiabatic expansion atmospheric pressure and recovering the latent heat of vaporization by the vaporized latent heat recovery device (66a).

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized in that the steam is injected sequentially downstream from the uppermost stream of the steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure, and the latent heat of vaporization is recovered by the vaporized latent heat recovery device (66a).

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. The fuel is sequentially injected downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure, the latent heat of vaporization is recovered by the vaporizing latent heat recovery device (66a), and supplied to the combustor / heat exchanger (4) of the all blade gas turbine. This is a combined rotor blade steam gas turbine engine.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine Injects sequentially downstream from the uppermost stream to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporized latent heat recovery unit (66a), and combustors and heat exchangers (4) of all blade gas turbines An all-blade steam gas turbine combined engine that can be supplied to

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. Injection is performed sequentially from the uppermost stream to the downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized by the supply.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. The steam is sequentially injected downstream from the uppermost stream of the steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporized latent heat recovery unit (66a), and the combustor and heat exchanger of the all blade gas turbine ( 4) An all-blade steam gas turbine combined engine characterized in that it is supplied to 4).

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. Injection is performed sequentially downstream to generate rotational output up to the adiabatic expansion atmospheric pressure. 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. An all-blade steam gas turbine combined engine characterized by

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine Injects sequentially downstream from the uppermost stream to generate a rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporizing latent heat recovery unit (66a), and recovers the combustor / heat exchanger (4) of the all blade steam gas turbine. ) Is a combined turbine and steam gas turbine engine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. Injection is performed sequentially from the uppermost stream to the downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery device (66a), and the combustor and heat exchanger of the all-blade steam gas turbine (4) An all-blade steam gas turbine combined engine that can be supplied to

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. Injection is performed sequentially downstream from the uppermost stream of the steam turbine to generate rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a), and the combustor and heat exchanger of the all-blade steam gas turbine are recovered. (4) An all-blade steam gas turbine combined engine that is supplied to (4).

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. The fuel is sequentially injected downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporizing latent heat recovery device (66a) and supplied to the combustor / heat exchanger (4) of the all blade gas turbine. All-blade steam gas turbine united engine characterized by heating to high-temperature water.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine Injects sequentially downstream from the uppermost stream to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporized latent heat recovery unit (66a), and combustors and heat exchangers (4) of all blade gas turbines An all-blade steam gas turbine united engine characterized by supplying heat to high-temperature water.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. Injection is performed sequentially from the uppermost stream to the downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine united engine characterized by supplying heated high-temperature water.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. The steam is sequentially injected downstream from the uppermost stream of the steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporized latent heat recovery unit (66a), and the combustor and heat exchanger of the all blade gas turbine ( 4) An all-blade steam gas turbine combined engine characterized in that it is supplied to 4) to produce heated high-temperature water.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. Injection is performed sequentially downstream to generate rotational output up to the adiabatic expansion atmospheric pressure. 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. An all-blade steam gas turbine combined engine characterized by heating to high-temperature water.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine Injects sequentially downstream from the uppermost stream to generate a rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporizing latent heat recovery unit (66a), and recovers the combustor / heat exchanger (4) of the all blade steam gas turbine. ) To produce heated high-temperature water and heated rotor steam gas turbine combined engine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. Injection is performed sequentially from the uppermost stream to the downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery device (66a), and the combustor and heat exchanger of the all-blade steam gas turbine (4) An all-blade steam gas turbine united engine characterized by supplying heat to high-temperature water.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. Injection is performed sequentially downstream from the uppermost stream of the steam turbine to generate rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a), and the combustor and heat exchanger of the all-blade steam gas turbine are recovered. An all-blade steam gas turbine combined engine characterized in that it is supplied to (4) to produce heated high-temperature water.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. The fuel is sequentially injected downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporizing latent heat recovery device (66a) and supplied to the combustor / heat exchanger (4) of the all blade gas turbine. A combined high-temperature steam gas turbine engine characterized in that the high-temperature water is heated and connected to each high-temperature water control valve (7a).

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine Injects sequentially downstream from the uppermost stream to generate rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporized latent heat recovery unit (66a), and combustors and heat exchangers (4) of all blade gas turbines The steam turbine combined engine of all blades is characterized in that the steam is supplied to the high-temperature water and is connected to the respective high-temperature water control valves (7a).

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. Injection is performed sequentially from the uppermost stream to the downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure. An all-blade steam gas turbine combined engine characterized in that it supplies heated high-temperature water and communicates with each high-temperature water control valve (7a).

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. The steam is sequentially injected downstream from the uppermost stream of the steam turbine to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporized latent heat recovery unit (66a), and the combustor and heat exchanger of the all blade gas turbine ( 4) A combined rotor blade steam gas turbine engine characterized in that it is supplied to the high temperature water by supplying it to the high temperature water control valve (7a).

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosion power, and accelerated outside the nozzle like a shot rocket and the most upstream of a full-blade steam turbine. Injection is performed sequentially downstream to generate rotational output up to the adiabatic expansion atmospheric pressure. 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. A combined high-temperature steam gas turbine and a high-temperature water control valve (7a).

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle like a bullet of a machine gun by vaporization and explosive power, and accelerated outside the nozzle like a shot rocket, and all-blade steam turbine Injects sequentially downstream from the uppermost stream to generate a rotational output up to the adiabatic expansion atmospheric pressure, recovers the latent heat of vaporization by the vaporizing latent heat recovery unit (66a), and recovers the combustor / heat exchanger (4) of the all blade steam gas turbine. ) To produce heated high-temperature water and communicate with each high-temperature water control valve (7a).

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle like a shot rocket to accelerate the whole blade steam turbine. Injection is performed sequentially from the uppermost stream to the downstream to generate a rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery device (66a), and the combustor and heat exchanger of the all-blade steam gas turbine (4) The steam turbine combined engine of all blades is characterized in that the steam is supplied to the high-temperature water and is connected to the respective high-temperature water control valves (7a).

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. Injection is performed sequentially downstream from the uppermost stream of the steam turbine to generate rotational output up to the adiabatic expansion atmospheric pressure. The latent heat of vaporization is recovered by the vaporization latent heat recovery unit (66a), and the combustor and heat exchanger of the all-blade steam gas turbine are recovered. (4) An all-blade steam gas turbine combined engine characterized in that it is supplied to (4) to be heated high-temperature water and connected to each high-temperature water control valve (7a).

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive force, and accelerates outside the nozzle like a shot rocket and is the uppermost stream of a full blade gas turbine. An all-blade steam gas turbine combined engine characterized by sequentially injecting downstream to generate rotational output and supplying combustion gas (10) to an optimum middle stage.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun by vaporization and explosion force, and accelerates outside the nozzle like a shot rocket, and the whole rotor blade gas turbine An all-blade steam gas turbine combined engine characterized by generating rotation output by sequentially injecting downstream from the uppermost stream to supply combustion gas (10) to an optimal middle stream stage.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a machine gun bullet, and outside the nozzle like a shot rocket to accelerate the whole blade gas turbine. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream to generate a rotational output and to supply combustion gas (10) to an optimum middle stage.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by sequentially injecting gas downstream from the uppermost stream of a gas turbine to generate rotational output and supplying combustion gas (10) to an optimal middle stream stage.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun. Outside the nozzle, it is accelerated like a shot rocket. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from upstream to generate rotational output and supplying combustion gas (10) to an optimal middle stage.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet by vaporization and explosive power, and outside the nozzle like a shot rocket, all-blade steam gas An all-blade steam gas turbine combined engine characterized by sequentially injecting downstream from the uppermost stream of the turbine to generate rotational output and supplying combustion gas (10) to an optimum middle stage.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle is accelerated like a shot rocket, and the whole blade steam gas turbine An all-blade steam gas turbine combined engine characterized by generating rotation output by sequentially injecting downstream from the uppermost stream to supply combustion gas (10) to an optimal middle stream stage.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by injecting sequentially downstream from the uppermost stream of the steam gas turbine to generate a rotational output and supplying the combustion gas (10) to the optimum middle stage.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive force, and accelerates outside the nozzle like a shot rocket and is the uppermost stream of a full blade gas turbine. An all-blade steam gas turbine combined engine characterized by sequentially injecting downstream to generate rotational output, supplying combustion gas (10) to an optimal middle stage, and cooling with high-temperature water.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun by vaporization and explosion force, and accelerates outside the nozzle like a shot rocket, and the whole rotor blade gas turbine An all-blade steam gas turbine combined engine characterized in that it sequentially injects downstream from the uppermost stream to generate rotational output, supplies combustion gas (10) to the optimum middle stream, and cools it with high-temperature water.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a machine gun bullet, and outside the nozzle like a shot rocket to accelerate the whole blade gas turbine. An all-blade steam gas turbine combined engine characterized by generating rotation output by injecting sequentially downstream from the uppermost stream, supplying combustion gas (10) to the optimal middle flow stage, and cooling with high-temperature water.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized in that a rotating output is generated by sequentially injecting the gas from the uppermost stream of the gas turbine to the downstream, a combustion gas (10) is supplied to an optimal middle stream stage, and cooled by high-temperature water.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun. Outside the nozzle, it is accelerated like a shot rocket. An all-blade steam gas turbine combined engine characterized by injecting sequentially from upstream to downstream to generate rotational output, supplying combustion gas (10) to an optimum middle stage, and cooling with high-temperature water.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet by vaporization and explosive power, and outside the nozzle like a shot rocket, all-blade steam gas An all-blade steam gas turbine combined engine characterized in that a rotating output is generated by sequentially injecting the steam downstream from the uppermost stream of the turbine, a combustion gas (10) is supplied to an optimum middle stream stage, and cooled by high-temperature water.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle is accelerated like a shot rocket, and the whole blade steam gas turbine An all-blade steam gas turbine combined engine characterized in that it sequentially injects downstream from the uppermost stream to generate rotational output, supplies combustion gas (10) to the optimum middle stream, and cools it with high-temperature water.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam gas turbine combined engine characterized by generating a rotational output by sequentially injecting the steam downstream from the uppermost stream of the steam gas turbine, supplying the combustion gas (10) to the optimal middle stream stage, and cooling it with high-temperature water.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive force, and accelerates outside the nozzle like a shot rocket and is the uppermost stream of a full blade gas turbine. An all-blade steam gas turbine combined engine characterized in that the rotating blades are sequentially injected downstream to generate a rotational output, and the combustion gas (10) is supplied to an optimal middle flow stage and cooled by high-temperature water to generate a rotational output.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun by vaporization and explosion force, and accelerates outside the nozzle like a shot rocket, and the whole rotor blade gas turbine All-blade steam gas turbine characterized in that a rotary output is generated by sequentially injecting downstream from the uppermost stream of the turbine, and a combustion gas (10) is supplied to an optimal middle flow stage and cooled by high-temperature water to generate a rotary output. Coalition organization.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a machine gun bullet, and outside the nozzle like a shot rocket to accelerate the whole blade gas turbine. The all-blade steam gas turbine combination characterized in that a rotary output is generated by sequentially injecting the gas from the upstream to the downstream to generate a rotational output, and the combustion gas (10) is supplied to the optimum middle flow stage and cooled by high-temperature water to generate a rotary output. organ.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-blade steam characterized by generating a rotational output by injecting sequentially downstream from the uppermost stream of the gas turbine to generate a rotational output, supplying a combustion gas (10) to an optimal middle flow stage, and cooling by high-temperature water to generate a rotational output. Gas turbine combined engine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun. Outside the nozzle, it is accelerated like a shot rocket. An all-blade steam gas turbine combined engine characterized in that a rotating output is generated by injecting sequentially from upstream to downstream, and a combustion gas (10) is supplied to an optimum middle flow stage and cooled by high-temperature water to generate a rotating output. .

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet by vaporization and explosive power, and outside the nozzle like a shot rocket, all-blade steam gas The all-blade steam gas is characterized in that it is injected sequentially downstream from the uppermost stream of the turbine to generate a rotational output, and the combustion gas (10) is supplied to the optimum middle stage and cooled by high-temperature water to generate a rotational output. Turbine united engine.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle is accelerated like a shot rocket, and the whole blade steam gas turbine All-blade steam gas turbine characterized in that a rotary output is generated by sequentially injecting downstream from the uppermost stream of the turbine, and a combustion gas (10) is supplied to an optimal middle flow stage and cooled by high-temperature water to generate a rotary output. Coalition organization.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. An all-rotor blade characterized in that a rotating output is generated by sequentially injecting the steam downstream from the uppermost stream of the steam gas turbine, and a combustion gas (10) is supplied to an optimum middle stage and cooled by high-temperature water to generate a rotating output. Steam gas turbine combined engine.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive force, and accelerates outside the nozzle like a shot rocket and is the uppermost stream of a full blade gas turbine. Injecting sequentially downstream to generate rotational output, supplying combustion gas (10) to the optimal middle flow stage, cooling with high-temperature water, and coagulating moisture with adiabatic expanded low-temperature combustion gas as a nucleus in the process of generating rotational output All-blade steam gas turbine combined engine characterized by

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun by vaporization and explosion force, and accelerates outside the nozzle like a shot rocket, and the whole rotor blade gas turbine Injects sequentially downstream from the uppermost stream to generate rotational output, supplies combustion gas (10) to the optimum middle stage, cools with high-temperature water, and generates a rotational output. All-blade steam gas turbine combined engine characterized by coagulation of moisture.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a machine gun bullet, and outside the nozzle like a shot rocket to accelerate the whole blade gas turbine. The rotation output is generated by sequentially injecting the rotation from the uppermost stream to the downstream, and the combustion gas (10) is supplied to the optimum middle flow stage, cooled by the high-temperature water, and the adiabatic expanded low-temperature combustion gas is used as the core in the process of generating the rotation output. All-rotor steam gas turbine united engine characterized by coagulation.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. The rotational output is generated by sequentially injecting the gas into the downstream from the uppermost stream of the gas turbine, and the combustion gas (10) is supplied to the optimum middle flow stage, cooled by high-temperature water, and the adiabatic expanded low-temperature combustion gas is generated in the process of generating the rotational output. An all-blade steam gas turbine combined engine characterized by coagulation of moisture in the nucleus.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun. Outside the nozzle, it is accelerated like a shot rocket. Injection is performed sequentially from upstream to downstream to generate rotational output, and the combustion gas (10) is supplied to the optimum middle flow stage, cooled by high-temperature water, and the adiabatic expanded low-temperature combustion gas is used as a core in the process of generating rotational output to remove moisture. All-blade steam gas turbine combined engine characterized by aggregation.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet by vaporization and explosive power, and outside the nozzle like a shot rocket, all-blade steam gas Injection is performed downstream from the uppermost stream of the turbine to generate rotational output, and the combustion gas (10) is supplied to the optimum middle flow stage, cooled by high-temperature water, and adiabatic expanded low-temperature combustion gas is generated in the process of generating rotational output. All-blade steam gas turbine combined engine characterized by coagulation of water.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle is accelerated like a shot rocket, and the whole blade steam gas turbine Injects sequentially downstream from the uppermost stream to generate rotational output, supplies combustion gas (10) to the optimum middle stage, cools with high-temperature water, and generates a rotational output. All-blade steam gas turbine combined engine characterized by coagulation of moisture.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. Injection sequentially downstream from the uppermost stream of the steam gas turbine to generate rotational output, supply combustion gas (10) to the optimum middle stage, cool with high-temperature water, and generate a rotational output to produce adiabatic expanded low-temperature combustion gas. An all-blade steam gas turbine combined engine characterized by aggregating moisture around the core.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun due to vaporization and explosive force, and accelerates outside the nozzle like a shot rocket and is the uppermost stream of a full blade gas turbine. Injecting sequentially downstream to generate rotational output, supplying combustion gas (10) to the optimal middle flow stage, cooling with high-temperature water, and coagulating moisture with adiabatic expanded low-temperature combustion gas as a nucleus in the process of generating rotational output All-blade steam gas turbine united engine characterized in that exhaust gas such as CO2 approaches zero.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a bullet of a machine gun by vaporization and explosion force, and accelerates outside the nozzle like a shot rocket, and the whole rotor blade gas turbine Injects sequentially downstream from the uppermost stream to generate rotational output, supplies combustion gas (10) to the optimum middle stage, cools with high-temperature water, and generates a rotational output. An all-blade steam gas turbine combined engine characterized by coagulating moisture to make exhaust gas such as CO2 close to zero.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a machine gun bullet, and outside the nozzle like a shot rocket to accelerate the whole blade gas turbine. The rotation output is generated by sequentially injecting the rotation from the uppermost stream to the downstream, and the combustion gas (10) is supplied to the optimum middle flow stage, cooled by the high-temperature water, and the adiabatic expanded low-temperature combustion gas is used as the core in the process of generating the rotation output. Coalescing engine, characterized in that exhaust gas such as CO2 is brought close to zero by coagulation.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. The rotational output is generated by sequentially injecting the gas into the downstream from the uppermost stream of the gas turbine, and the combustion gas (10) is supplied to the optimum middle flow stage, cooled by high-temperature water, and the adiabatic expanded low-temperature combustion gas is generated in the process of generating the rotational output. An all-blade steam gas turbine combined engine characterized by condensing water into the nucleus and reducing the exhaust such as CO2 to zero.

High-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun. Outside the nozzle, it is accelerated like a shot rocket. Injection is performed sequentially from upstream to downstream to generate rotational output, and the combustion gas (10) is supplied to the optimum middle flow stage, cooled by high-temperature water, and the adiabatic expanded low-temperature combustion gas is used as a core in the process of generating rotational output to remove moisture. An all-blade steam gas turbine combined engine characterized by agglomeration to reduce exhaust gas such as CO2 to zero.

Supercritical pressure high-temperature water is injected from the high-temperature water injection nozzle (59a) and accelerates inside the nozzle like a machine gun bullet by vaporization and explosive power, and outside the nozzle like a shot rocket, all-blade steam gas Injection is performed downstream from the uppermost stream of the turbine to generate rotational output, and the combustion gas (10) is supplied to the optimum middle flow stage, cooled by high-temperature water, and adiabatic expanded low-temperature combustion gas is generated in the process of generating rotational output. An all-blade steam gas turbine combined engine characterized in that water is agglomerated to make exhaust gas such as CO2 close to zero.

High-temperature water is injected from a plurality of high-temperature water injection nozzles (59a) and accelerated inside the nozzle by a vaporizing explosion force like a bullet of a machine gun, and outside the nozzle is accelerated like a shot rocket, and the whole blade steam gas turbine Injects sequentially downstream from the uppermost stream to generate rotational output, supplies combustion gas (10) to the optimum middle stage, cools with high-temperature water, and generates a rotational output. An all-blade steam gas turbine combined engine characterized by coagulating moisture to make exhaust gas such as CO2 close to zero.

The supercritical pressure high-temperature water is injected from a plurality of high-temperature water injection nozzles (59a), and accelerates like a machine gun bullet inside the nozzle by vaporization and explosive force, and accelerates like a shot rocket outside the nozzle, and all rotor blades. Injection sequentially downstream from the uppermost stream of the steam gas turbine to generate rotational output, supply combustion gas (10) to the optimum middle stage, cool with high-temperature water, and generate a rotational output to produce adiabatic expanded low-temperature combustion gas. An all-blade steam gas turbine united engine characterized in that water is condensed around the core and exhaust such as CO2 is brought close to zero.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure 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 are heated to a high temperature by electromagnetic heating.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine, wherein the turbine blades of the all-blade steam gas turbine are heated to a high temperature by electromagnetic heating.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure 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 are heated to a high temperature by electromagnetic heating.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59a) of the all-blade gas turbine is electromagnetically heated to a high temperature.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine, wherein the high-temperature water injection nozzle (59a) of the all-blade steam gas turbine is set at a high temperature by electromagnetic heating.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the high-temperature water injection nozzle (59a) of the all-blade steam turbine is electromagnetically heated to a high temperature.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure 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 is heated to a high temperature by electromagnetic heating.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine, wherein the electromagnetic heating nozzle (83) of the all-blade steam gas turbine is heated to a high temperature by electromagnetic heating.

The outer shaft device and the inner shaft device rotating in opposite directions by the water pump and the contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like having a supercritical pressure 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 is heated to a high temperature by electromagnetic heating.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer turbine blade group (19) and the inner turbine blade group (20) is formed into an integrated structure by annular casting (84). An all-blade steam gas turbine combined engine, characterized in that:

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer turbine bucket group (19) and the inner turbine bucket group (20) formed into an integrated structure by annular casting (84). ). An all-blade steam gas turbine combined engine, characterized in that:

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade compressor of the all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor blade groups (16) and the inner compressor is integrally formed annularly (84) into an assembled structure. A combined rotor blade steam gas turbine engine comprising a rotor blade group (17).

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor groups (16) and the inner compressor is integrally formed into a ring (84) and assembled. An all-blade steam gas turbine combined engine comprising a compressor blade group (17).

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade compressor of the all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor blade groups (16) and the inner compressor is integrally formed annularly (84) into an assembled structure. An all-blade steam gas turbine combined engine, wherein a water-repellent water cooling blade (87) is provided in a large part of the blade group (17).

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor groups (16) and the inner compressor is integrally formed into a ring (84) and assembled. An all-blade steam gas turbine combined engine, wherein a water-repellent water cooling blade (87) is provided in a large part of the compressor blade group (17).

An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a water feed pump and a contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the turbine blades are heated to a high temperature by electromagnetic heating.

A full-blade steam gas that drives an outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) with high-temperature water (5a) or the like coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine, wherein the turbine blades of the turbine are heated to a high temperature by electromagnetic heating.

An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine characterized in that the turbine blades are heated to a high temperature by electromagnetic heating.

An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a water feed pump and a contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like coupled at an optimum rotation ratio. A high-temperature water injection nozzle (59a) is heated by electromagnetic heating at a high temperature.

A full-blade steam gas that drives an outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) with high-temperature water (5a) or the like coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine, wherein a high-temperature water injection nozzle (59a) of a turbine is heated to a high temperature by electromagnetic heating.

An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like coupled at an optimum rotation ratio. A high-temperature water injection nozzle (59a) is heated by electromagnetic heating at a high temperature.

An all-blade gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a water feed pump and a contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like coupled at an optimum rotation ratio. A combined rotor blade steam gas turbine engine characterized in that the electromagnetic heating nozzle (83) is heated to a high temperature by electromagnetic heating.

A full-blade steam gas that drives an outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) with high-temperature water (5a) or the like coupled at an optimum rotation ratio. An all-blade steam gas turbine combined engine, wherein the electromagnetic heating nozzle (83) of the turbine is heated to a high temperature by electromagnetic heating.

An all-blade steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) are driven by high-temperature water (5a) or the like coupled at an optimum rotation ratio. A combined rotor blade steam gas turbine engine characterized in that the electromagnetic heating nozzle (83) is heated to a high temperature by electromagnetic heating.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, wherein the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20) are formed into an integrated structure by integrally casting (84) into an annular shape. All-blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20) which are integrally formed in an annular shape (84) into an assembled structure. All-blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer compressor rotor group (16) and the inner compressor rotor group (17), each of which is integrally assembled in an annular shape (84) into an assembled structure. ). An all-blade steam gas turbine combined engine, characterized in that:

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer rotor blade group (16) and the inner compressor rotor group (16) each having an assembled structure formed by integrally casting (84) into an annular shape. 17) An all-blade steam gas turbine combined engine according to (17).

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer compressor rotor group (16) and the inner compressor rotor group (17), each of which is integrally assembled in an annular shape (84) into an assembled structure. ) Is provided with a water-repellent water cooling blade (87) in the majority thereof.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer rotor blade group (16) and the inner compressor rotor group (16) each having an assembled structure formed by integrally casting (84) into an annular shape. 17) 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 (17).

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade gas turbine, a large part of each of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) formed into an integrated structure by being integrally formed into a ring (84) is repelled. An all-blade steam gas turbine combined engine comprising an aqueous water cooling blade (87).

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade steam gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) which are integrally formed in an annular shape (84) and are assembled into an assembled structure, An all-blade steam gas turbine combined engine comprising a water-repellent water cooling blade (87).

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically-heated turbine blade (81), it is integrally cast in a ring (84) to form an assembly structure. A water repellent water cooling blade (87) provided in a ring shape for each stage in most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17). Turbine united engine.

An all-blade compressor of an all-blade steam gas turbine equipped with an electromagnetically heated turbine blade (81) driven by high-temperature water (5a) or the like at a supercritical pressure or the like, and is integrally formed in an annular shape (84). A water repellent water cooling blade (87) is provided in a large part of each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) in a ring shape for each paragraph. Gas turbine combined engine.

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 full blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81) is provided. In the whole rotor compressor, most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed into a ring (84) and assembled, are provided with a water-repellent water cooling blade ( 87), wherein a combined rotor blade steam gas turbine engine is provided.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). Of the outer rotor blade group (16) and the inner compressor blade group (17), which are integrally formed into an annular structure by integral casting (84), water-repellent water cooling blades (87) An all-blade steam gas turbine combined engine characterized by the provision of (87).

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer compressions is integrally formed into a ring (84) and assembled. An all-blade steam / gas turbine combined engine, wherein a water-repellent water cooling blade (87) is provided annularly for each stage in most of the rotor blade group (16) and the inner compressor rotor group (17).

In an all-blade compressor of an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer sides is formed into an integrated structure (84) in an annular shape. An all-blade steam gas turbine combined engine, wherein a water-repellent water cooling blade (87) is provided in a ring shape for each stage in most of the compressor blade group (16) and the inner compressor blade group (17).

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade compressor of the all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor blade groups (16) and the inner compressor is integrally formed annularly (84) into an assembled structure. Water-repellent water cooling blades (87) are provided in a large part of the moving blade group (17) in a ring 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). An all-blade steam gas turbine combined engine characterized in that:

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor groups (16) and the inner compressor is integrally formed into a ring (84) and assembled. A water-repellent water cooling blade (87) is provided in a large part of the compressor rotor blade group (17) 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 a water injection means (56). An all-blade steam gas turbine combined engine characterized by injecting.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer compressor rotor group (16) and the inner compressor rotor group (17), each of which is integrally assembled in an annular shape (84) into an assembled structure. In most cases, the water-repellent water cooling blades (87) are provided annularly for each paragraph, and after cooling at least one or more water-repellent water cooling blades for each paragraph, water is injected from the water injection means (56). All-blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer rotor blade group (16) and the inner compressor rotor group (16) each having an assembled structure formed by integrally casting (84) into an annular shape. Most of 17), the water-repellent water cooling blades (87) are provided in a ring shape for each paragraph, and one or more water-repellent water cooling blades for each paragraph are cooled and then water-injected from the water injection means (56). All-blade steam gas turbine combined engine.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) which are integrally formed in an annular shape (84) into an assembled structure have water repellency. A water-cooling blade (87) is provided in a ring shape for each paragraph, and water is injected from a water injection means (56) after cooling at least one or more water-repellent water-cooling blades for each paragraph; organ.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade steam gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) which are integrally formed in an annular shape (84) and are assembled into an assembled structure, A water-repellent water cooling blade (87) is provided in a ring shape for each paragraph, and one or more water-repellent water cooling blades for each paragraph are cooled and then water-injected from a water injection means (56). Turbine united engine.

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically-heated turbine blade (81), it is integrally cast in a ring (84) to form an assembly structure. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph, and one or more water-repellent water groups are provided for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling a cooling blade.

An all-blade compressor of an all-blade steam gas turbine equipped with an electromagnetically heated turbine blade (81) driven by high-temperature water (5a) or the like at a supercritical pressure or the like, and is integrally formed in an annular shape (84). Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling a water cooling blade.

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 full blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81) is provided. In the all-rotor compressor, most of the outer compressor rotor group (16) and the inner compressor rotor group (17), which are integrally formed into a ring (84) and assembled, are provided with water-repellent water cooling blades (87). ) Is provided annularly 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) after cooling.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). Of the outer rotor blade group (16) and the inner compressor blade group (17), which are integrally formed into an annular structure by integral casting (84), water-repellent water cooling blades (87) is provided annularly 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) after cooling, and the combined turbine and steam gas turbine engine.

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer compressions is integrally formed into a ring (84) and assembled. Most of the rotor blade group (16) and 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 cooling one or more water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56).

In an all-blade compressor of an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer sides is formed into an integrated structure (84) in an annular shape. Most of the compressor blade group (16) and the inner compressor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring-like shape for each paragraph to cool one or more water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) later.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade compressor of the all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor blade groups (16) and the inner compressor is integrally formed annularly (84) into an assembled structure. A water-repellent water cooling blade (87) is provided annularly for each paragraph in a large part of the moving blade group (17), and water is injected from the water injection means (56) after cooling less than half of the water-repellent water cooling blade for each paragraph. All-blade steam gas turbine combined engine characterized by the following.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor groups (16) and the inner compressor is integrally formed into a ring (84) and assembled. A water-repellent water cooling blade (87) is provided annularly for each paragraph in a large part of the compressor rotor blade group (17), and after cooling less than half of the water-repellent water cooling blade for each paragraph, water is supplied from the water injection means (56). An all-blade steam gas turbine combined engine characterized by injecting.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer compressor rotor group (16) and the inner compressor rotor group (17), each of which is integrally assembled in an annular shape (84) into an assembled structure. In most cases, the water-repellent water cooling blades (87) are provided in a ring-like shape for each paragraph, and the water-repellent water-cooling blades for all the paragraphs are cooled by less than half of the water-repellent water cooling blades. All-blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer rotor blade group (16) and the inner compressor rotor group (16) each having an assembled structure formed by integrally casting (84) into an annular shape. Most of 17), the water-repellent water cooling blades (87) are provided in a ring shape for each paragraph, and the water-repellent water cooling blades are cooled by half or less for each paragraph and then water-jetted from the water injection means (56). All-blade steam gas turbine combined engine.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade gas turbine, a large part of each of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) formed into an integrated structure by being integrally formed into a ring (84) is repelled. An all-blade steam gas turbine characterized in that an aqueous water cooling blade (87) is provided in a ring shape for each paragraph, and water is injected from a water injection means (56) after cooling the water-repellent water cooling blades of all less than half of each paragraph. Coalition organization.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade steam gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) which are integrally formed in an annular shape (84) and are assembled into an assembled structure, A water-repellent water cooling blade (87) is provided in a ring shape for each paragraph, and water is injected from a water injection means (56) after cooling the water-repellent water cooling blades of all less than half of each paragraph. Turbine united engine.

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically-heated turbine blade (81), it is integrally cast in a ring (84) to form an assembly structure. Most of the outer compressor rotor blade group (16) and inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring-like shape for each paragraph, and the water-repellent water for each paragraph is less than half. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling a cooling blade.

An all-blade compressor of an all-blade steam gas turbine equipped with an electromagnetically heated turbine blade (81) driven by high-temperature water (5a) or the like at a supercritical pressure or the like, and is integrally formed in an annular shape (84). Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph, and the water repellency is reduced to half or less for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling a water cooling blade.

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 full blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81) is provided. In the whole rotor compressor, most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed into a ring (84) and assembled, are provided with a water-repellent water cooling blade ( 87) is provided in each stage in a ring shape, and after cooling the water-repellent water cooling blades of each half or less of each stage, water is injected from the water injection means (56) after the cooling, and the combined turbine and steam turbine combined engine is characterized.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). Of the outer rotor blade group (16) and the inner compressor blade group (17), which are integrally formed into an annular structure by integral casting (84), water-repellent water cooling blades (87) is provided in a ring for each paragraph, and after cooling all or less half of the water-repellent water cooling blades for each paragraph, water is injected from the water injection means (56) after cooling, so that the combined rotor blade steam gas turbine engine is provided.

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer compressions is integrally formed into a ring (84) and assembled. Most of the rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph, and after cooling all or less half of the water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56).

In an all-blade compressor of an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer sides is formed into an integrated structure (84) in an annular shape. Most of the compressor blade group (16) and the inner compressor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring-like shape for each paragraph, and the whole water-repellent water-cooling blade for each paragraph is cooled by half or less. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) later.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). Rotor blade group (16) and inner compressor blade group each of which is integrally cast in a ring (84) and communicates with the water passage as an assembled structure in a full-blade gas turbine driven by high-temperature water (5a) or the like. In most of (17), the water-repellent water cooling blades (87) are provided in a ring shape for each paragraph, and the water-repellent water cooling blades are cooled by half or less for each paragraph, and water is injected from the water injection means (56) after cooling. All-blade steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). Rotor steam turbines driven by high-temperature water (5a) or the like, the outer compressor rotor blades (16) and the inner compressor rotor blades each of which is integrally cast in a ring (84) and communicates with the water passage as an assembled structure. A water-repellent water cooling blade (87) is provided in a loop for each paragraph in most of the group (17), and water is injected from the water injection means (56) after cooling all the water-repellent water cooling blades of each half or less. An all-blade steam gas turbine combined engine characterized by the following.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17), each of which is integrally formed in an annular shape (84) and communicates with the water passage as an assembled structure, are provided with water-repellent water cooling. An all-blade steam / gas turbine combined engine, wherein the blades (87) are provided in a ring shape for each paragraph, and water is injected from the water injection means (56) after cooling the water-repellent water cooling blades of all less than half of each paragraph.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade steam gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17), each of which is integrally formed in an annular shape (84) and communicates with the water passage as an assembled structure, are provided with water-repellent water. A cooling blade (87) is provided in a ring shape for each stage, and water is injected from a water injection means (56) after cooling the water-repellent water cooling blades of the whole and less than half of each stage. .

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), each of which is integrally cast in a ring (84) and communicates with the water passage as an assembly structure. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring-like shape for each paragraph, and half or less of the water-repellent water cooling blade for each paragraph is provided. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling.

In a full-blade steam gas turbine having electromagnetic heating turbine blades (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, each is integrally cast in a ring (84) and communicates with water passages as an assembly structure. Water-repellent water cooling blades (87) are provided annularly for each paragraph in most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), and less than half the water-repellent water cooling blades for each paragraph. Wherein the water is injected from the water injection means (56) after cooling.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer compressor rotor blade group (16) and the inner compressor rotor group (17), each of which is integrally cast in a ring (84) and communicates with the water passage as an assembled structure, are large. A water-repellent water cooling blade (87) is provided in each section in a ring shape for each paragraph, and water is injected from the water injection means (56) after cooling less than half of the water-repellent water cooling blade for each paragraph. Wing steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, in each 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 assembled structure. In most cases, the water-repellent water cooling blades (87) are provided annularly for each paragraph, and the water-repellent water-cooling blades are cooled and the water-repellent water cooling blades for all the stages are cooled by water jetting means (56). Combined moving blade steam gas turbine engine.

An all-rotor gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine rotor blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. A water-repellent water cooling blade (87) is provided on a large part of each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are annularly integrally cast (84) and communicated with the water channel as an assembled structure. An all-blade steam gas turbine combined engine, wherein a water-repellent water cooling blade, which is provided in each stage in a ring shape, is cooled by half of the water-repellent water cooling blades and then water is injected from a water injection means (56).

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). , Water-repellent water cooling blades (87) are provided on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), each of which has an annularly integrated casting (84) and communicates with the water passage as an assembled structure. , Wherein the water-repellent water cooling blades, which are less than half of each stage, are cooled and then water-injected from the water injection means (56).

In an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer compressor blade groups each of which is integrally cast in a ring (84) and communicates with the water passage as an assembled structure. A water-repellent water cooling blade (87) is provided annularly for each paragraph in (16) and a large part of the inner compressor rotor blade group (17). (56) An integrated all-blade steam gas turbine engine that performs more water injection.

In an all-blade steam gas turbine that is driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer compressor blades is integrally formed in a ring (84) and communicates with the water passage as an assembled structure. Water repellent water cooling blades (87) are provided annularly for each paragraph in most of the group (16) and the inner compressor rotor blade group (17), and the water repellent water cooling blades for each paragraph are cooled by less than half of the water repellent water cooling blades. An all-blade steam gas turbine combined engine, wherein water is injected from the means (56).

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade compressor of the all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor blade groups (16) and the inner compressor is integrally formed annularly (84) into an assembled structure. An all-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 blade group (17) and is driven by the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor groups (16) and the inner compressor is integrally formed into a ring (84) and assembled. A combined rotor blade steam gas turbine engine, characterized in that a water repellent water cooling blade (87) is provided annularly for each stage in a majority of the compressor blade group (17) and is driven by the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer compressor rotor group (16) and the inner compressor rotor group (17), each of which is integrally assembled in an annular shape (84) into an assembled structure. ), A hydrodynamic water cooling blade (87) is provided annularly for each stage, and a device driven by the output is provided.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer rotor blade group (16) and the inner compressor rotor group (16) each having an assembled structure formed by integrally casting (84) into an annular shape. 17) An all-blade steam / gas turbine combined engine, characterized in that a water-repellent water cooling blade (87) is provided in an annular shape for each stage and driven by the output.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade gas turbine, a large part of each of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) formed into an integrated structure by being integrally formed into a ring (84) is repelled. An all-blade steam gas turbine combined engine, comprising: a device provided with an aqueous water cooling blade (87) in an annular shape for each stage and driven by the output.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade steam gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) which are integrally formed in an annular shape (84) and are assembled into an assembled structure, An all-blade steam gas turbine combined engine, comprising: a device for providing a water-repellent water cooling blade (87) in an annular shape for each stage and driving with the output.

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically-heated turbine blade (81), it is integrally cast in a ring (84) to form an assembly structure. Most of the outer compressor rotor blades group (16) and the inner compressor rotor blade group (17) provided with a device which is provided with a water-repellent water cooling blade (87) annularly for each paragraph and driven by the output. An all-blade steam gas turbine combined engine characterized by the following.

An all-blade compressor of an all-blade steam gas turbine equipped with an electromagnetically heated turbine blade (81) driven by high-temperature water (5a) or the like at a supercritical pressure or the like, and is integrally formed in an annular shape (84). Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) were provided with a device that provided a water-repellent water cooling blade (87) in a ring shape for each paragraph and driven by the output. An all-blade steam gas turbine combined engine, characterized in that:

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 full blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81) is provided. In the whole rotor compressor, most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed into a ring (84) and assembled, are provided with a water-repellent water cooling blade ( 87), wherein a unit is provided for each stage in a ring shape and a device driven by the output is provided.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). Of the outer rotor blade group (16) and the inner compressor blade group (17), which are integrally formed into an annular structure by integral casting (84), water-repellent water cooling blades (87) An all-blade steam gas turbine combined engine, comprising: a device which is provided in a ring shape for each paragraph and driven by the output.

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer compressions is integrally formed into a ring (84) and assembled. Most of the 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 a ring shape for each stage and driven by the output. Combined moving blade steam gas turbine engine.

In an all-blade compressor of an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer sides is formed into an integrated structure (84) in an annular shape. Most of the compressor blade group (16) and the inner compressor blade group (17) are provided with a device that is provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph and driven by the output. All blade steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade compressor of the all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor blade groups (16) and the inner compressor is integrally formed annularly (84) into an assembled structure. Water-repellent water cooling blades (87) are provided in a large part of the moving blade group (17) in a ring 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 an apparatus driven by the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade compressor of a full-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor groups (16) and the inner compressor is integrally formed into a ring (84) and assembled. A water-repellent water cooling blade (87) is provided in a large part of the compressor rotor blade group (17) 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 a water injection means (56). An all-blade steam gas turbine combined engine, comprising: a device for injecting and driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer compressor rotor group (16) and the inner compressor rotor group (17), each of which is integrally assembled in an annular shape (84) into an assembled structure. In most cases, the water-repellent water cooling blades (87) are provided in a ring shape for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, water is jetted from the water jetting means (56) to output the water. An all-blade steam gas turbine combined engine comprising a driving device.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer rotor blade group (16) and the inner compressor rotor group (16) each having an assembled structure formed by integrally casting (84) into an annular shape. 17), a water-repellent water cooling blade (87) is provided annularly for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, water is injected from a water injection means (56) to output the cooling water. An all-blade steam gas turbine combined engine, characterized by comprising a device driven by:

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade gas turbine, a large part of each of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) formed into an integrated structure by being integrally formed into a ring (84) is repelled. A water-based water cooling blade (87) is provided in a ring shape for each paragraph, and a device is provided for driving one or more water-repellent water cooling blades for each paragraph by cooling the water-repellent water cooling blade and then jetting water from the water injection means (56). An all-blade steam gas turbine combined engine characterized by the following.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the entire moving blade compressor of the moving blade steam gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17) which are integrally formed in an annular shape (84) and are assembled into an assembled structure, A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph, and a device is provided which cools one or more water-repellent water cooling blades for each paragraph and then jets water from a water injection means (56) to drive the cooling water with the output. An all-blade steam gas turbine combined engine, characterized in that:

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically-heated turbine blade (81), it is integrally cast in a ring (84) to form an assembly structure. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph, and one or more water-repellent water groups are provided for each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) after cooling the cooling blades and driving with the output.

An all-blade compressor of an all-blade steam gas turbine equipped with an electromagnetically heated turbine blade (81) driven by high-temperature water (5a) or the like at a supercritical pressure or the like, and is integrally formed in an annular shape (84). Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) after cooling the water cooling blades and driving with the output.

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 full blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81) is provided. In the whole rotor compressor, most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed into a ring (84) and assembled, are provided with a water-repellent water cooling blade ( 87) is provided annularly for each paragraph, and after cooling one or more water-repellent water cooling blades for each paragraph, a device for injecting water from the water injection means (56) and driving with this output is provided. Combined moving blade steam gas turbine engine.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). Of the outer rotor blade group (16) and the inner compressor blade group (17), which are integrally formed into an annular structure by integral casting (84), water-repellent water cooling blades (87) is provided in a ring shape for each paragraph, and a device for cooling and cooling one or more water-repellent water cooling blades for each paragraph and injecting water from a water injection means (56) to drive the cooling water with the output is provided. All blade steam gas turbine combined engine.

In an all-blade compressor of an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer compressions is integrally formed into a ring (84) and assembled. Most of the rotor blade group (16) and 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 cooling one or more water-repellent water cooling blades for 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.

In an all-blade compressor of an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer sides is formed into an integrated structure (84) in an annular shape. Most of the compressor blade group (16) and the inner compressor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring-like shape for each paragraph to cool one or more water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine, characterized by further comprising a device for injecting water from a water injection means (56) and driving with the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). Rotor blade group (16) and inner compressor blade group each of which is integrally cast in a ring (84) and communicates with the water passage as an assembled structure in a full-blade gas turbine driven by high-temperature water (5a) or the like. In most of (17), a water-repellent water cooling blade (87) is provided in a ring shape for each paragraph. An all-blade steam gas turbine combined engine comprising a device driven by an output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). Rotor steam turbines driven by high-temperature water (5a) or the like, the outer compressor rotor blades (16) and the inner compressor rotor blades each of which is integrally cast in a ring (84) and communicates with the water passage as an assembled structure. In most of the 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 for all the paragraphs less than or equal to half, water is injected from the water injection means (56). An all-blade steam gas turbine combined engine comprising a device driven by the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, the outer compressor rotor blade group (16) and the inner compressor rotor group (17), each of which is integrally cast in a ring (84) and communicates with the water passage as an assembled structure, are large. A device in which a water-repellent water cooling blade (87) is provided in an annular shape in each section, and the water-repellent water-cooling blades, which are less than half of each paragraph, are cooled and then jetted with water from a water jetting means (56) to be driven by the output. An all-blade steam gas turbine combined engine comprising:

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, in each 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 assembled structure. For the most part, the water-repellent water cooling blades (87) are provided annularly for each paragraph, and after cooling all the water-repellent water cooling blades of each half or less for each paragraph, water is injected from the water injection means (56) and driven by the output. An all-blade steam gas turbine combined engine provided with a device.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17), each of which is integrally formed in an annular shape (84) and communicates with the water passage as an assembled structure, are provided with water-repellent water cooling. A wing (87) is provided in a ring shape for each paragraph, and a device is provided which is driven by the water injection means (56) after cooling all the water-repellent water cooling wings of each half or less, after cooling. All-blade steam gas turbine combined engine.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade steam gas turbine, most of the outer compressor moving blade group (16) and the inner compressor moving blade group (17), each of which is integrally formed in an annular shape (84) and communicates with the water passage as an assembled structure, are provided with water-repellent water. A cooling wing (87) is provided in a ring shape for each paragraph, and a device is provided which drives all of the water-repellent water cooling wings, which are half or less of each paragraph, by cooling the water-repellent water cooling wings and then jetting water with the water jetting means (56). All-blade steam gas turbine combined engine.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), each of which is integrally cast in a ring (84) and communicates with the water passage as an assembly structure. Most of the outer compressor blade group and the inner compressor blade group (17) are provided with a water-repellent water cooling blade (87) in each stage in a ring shape. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from an injection means (56) and driven by the output.

In a full-blade steam gas turbine having electromagnetic heating turbine blades (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, each is integrally cast in a ring (84) and communicates with water passages as an assembly structure. Most of the outer compressor blade group and inner compressor rotor group (17) are provided with a water-repellent water cooling blade (87) annularly for each paragraph, and after cooling the water-repellent water cooling blades of all less than half of each paragraph after cooling. 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.

An all-rotor gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine rotor blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. A water-repellent water cooling blade (87) is provided on a large part of each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are annularly integrally cast (84) and communicated with the water channel as an assembled structure. All-blade steam provided with a device which is provided annularly for each paragraph and which is driven by the water-injection means (56) by cooling the water-repellent water cooling blades of each half or less of each paragraph and then driving by the output. Gas turbine combined engine.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). , Water-repellent water cooling blades (87) are provided on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), each of which has an annularly integrated casting (84) and communicates with the water passage as an assembled structure. All the blades are provided in a ring shape for each paragraph, and a device for driving the water-repellent water cooling blades by cooling by cooling the water-repellent water cooling blades of each half or less of each paragraph and injecting water with the water injection means (56). Steam gas turbine combined engine.

In an all-blade gas turbine that is driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), each of the outer compressor blade groups that is integrally cast in a ring (84) and communicates with the water passage as an assembly structure. Water-repellent water cooling blades (87) are provided annularly for each paragraph in most of the inner compressor rotor blade group (17), and water injection means (56) after cooling less than half of the water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting more water and driving with the output.

In an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), each of the outer compressor blades is integrally cast in a ring (84) and communicates with the water passage as an assembly structure. Water repellent water cooling blades (87) are provided annularly for each paragraph in most of the group and the inner compressor rotor blade group (17). A) an all-blade steam gas turbine combined engine, characterized by comprising a device for injecting more water and driving with this output.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine united engine characterized in that water and water vapor are aggregated and can be separated and collected as hail and water droplets.

A low-temperature combustion gas containing coal ash in a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure 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 in that water and water vapor are coagulated around the core and can be separated and collected as hail or water droplets.

A low-temperature combustion gas containing harmful substances in a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure 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 in that water and water vapor are coagulated around the core and can be separated and collected as hail or water droplets.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C, low-temperature combustion gas is used as a core. An all-blade steam gas turbine combined engine that aggregates water and water vapor and makes it possible to separate and collect it as hail and water droplets.

Low-temperature combustion including coal ash in a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure 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, wherein water and steam are aggregated using gas as a nucleus and can be separated and collected as hail or water droplets.

Low-temperature combustion containing harmful substances in a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine, wherein water and steam are aggregated using gas as a nucleus and can be separated and collected as hail or water droplets.

In a full-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., water and steam coagulate with low-temperature combustion gas as a core. And an all-blade steam gas turbine combined engine characterized in that it can be separated and collected as hail or water droplets.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically-heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., water and water are generated by using low-temperature combustion gas containing coal ash as a core. An all-blade steam gas turbine combined engine wherein steam is agglomerated and can be separated and collected as hail, water droplets, and the like.

In an all-blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., water and nucleus contain low-temperature combustion gas containing harmful substances. An all-blade steam gas turbine combined engine wherein steam is agglomerated and can be separated and collected as hail, water droplets, and the like.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., water and steam coagulate with low-temperature combustion gas as the core. And an all-blade steam gas turbine combined engine that can be separated and collected as hail, water droplets, and the like.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., water is cooled by using low-temperature combustion gas containing coal ash as a core. An all-blade steam gas turbine united engine characterized in that water and water vapor are aggregated and can be separated and collected as hail and water droplets.

In a full-blade steam gas turbine having an electromagnetically heated turbine blade (81) and driven by high-temperature water (5a) or the like, which has a combustion gas exhaust temperature approaching −273 ° C., water is cooled by using low-temperature combustion gas containing harmful substances as a core. An all-blade steam gas turbine united engine characterized in that water and water vapor are aggregated and can be separated and collected as hail and water droplets.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-rotor blade gas turbine that is driven by high-temperature water (5a) with supercritical pressure or the like equipped with a rotor blade (81), water and steam are agglomerated with low-temperature combustion gas as a nucleus, and separated and collected as hail and water droplets. An all-blade steam gas turbine combined engine characterized by being made possible.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) having a supercritical pressure or the like having a moving blade (81), water or water vapor is aggregated with a low-temperature combustion gas containing a harmful substance as a nucleus, and hail and water droplets are formed. An all-blade steam gas turbine combined engine characterized in that it can be separated and recovered as such.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine equipped with a moving blade (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, water or steam is aggregated using low-temperature combustion gas as a nucleus, and separated as hail or water droplets. An all-blade steam gas turbine combined engine characterized by being recoverable.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade steam gas turbine that is driven by high-temperature water (5a) having a supercritical pressure or the like and includes a moving blade (81), water and steam are agglomerated by using a low-temperature combustion gas containing a harmful substance as a nucleus to form a hail. An all-blade steam gas turbine combined engine, which can be separated and collected as water droplets or the like.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade gas turbine driven by high-temperature water (5a) or the like equipped with a moving blade (81), water and steam are aggregated by using low-temperature combustion gas as a nucleus, and can be separated and collected as hail, water droplets, and the like. All-blade steam gas turbine combined engine.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-rotor blade gas turbine driven by high-temperature water (5a) equipped with a rotor blade (81), water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as the core, and can be separated and collected as hail, water droplets, etc. An all-blade steam gas turbine combined engine characterized by:

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a moving blade (81), water or steam is agglomerated with low-temperature combustion gas as a nucleus, and can be separated and collected as hail, water droplets, and the like. An all-blade steam gas turbine combined engine characterized by the following.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with a bucket (81), water and steam are agglomerated with low-temperature combustion gas containing harmful substances as nuclei and separated and collected as hail and water droplets. An all-blade steam gas turbine combined engine characterized by being made possible.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. A steam turbine combined with a turbine blade driven by high-temperature water (5a) or the like, wherein water and steam are aggregated by using a low-temperature combustion gas as a nucleus and can be separated and collected as hail, water droplets and the like. organ.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In a full-blade gas turbine driven by high-temperature water (5a) or the like, water and water vapor are aggregated with low-temperature combustion gas containing harmful substances as nuclei, and can be separated and collected as hail and water droplets. All blade steam gas turbine combined engine.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. A rotor blade driven by high-temperature water (5a) or the like, characterized in that water and water vapor are aggregated with a low-temperature combustion gas as a nucleus and can be separated and recovered as hail, water droplets and the like. Steam gas turbine combined engine.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, water and water vapor are aggregated using low-temperature combustion gas containing harmful substances as a nucleus, and can be separated and collected as hail or water droplets. All-blade steam gas turbine combined engine.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water cooling blade (87) is provided in a ring shape for each stage on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) which are assembled into a structure. Wing steam gas turbine combined engine.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water cooling blade (87) is provided in a ring shape for each stage on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) which are assembled and assembled. Combined moving blade steam gas turbine engine.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. A steam-turbine combined engine, wherein water and steam are agglomerated with low-temperature combustion gas as a nucleus and can be separated and collected as hail, water droplets, etc.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., in which all water and steam are aggregated using low-temperature combustion gas containing harmful substances as cores, and can be separated and recovered as hail, water droplets, etc. Turbine united engine.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., in which a low-temperature combustion gas is used as a nucleus to agglomerate water and water vapor so that they can be separated and collected as hail, water droplets, etc. .

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., in which all water and steam are agglomerated using low-temperature combustion gas containing harmful substances as cores and can be separated and collected as hail, water droplets, etc. Gas turbine combined engine.

An all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. A water-cooled blade (87) is provided in each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) in a ring shape for each stage. organ.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). A water cooling blade (87) provided in a ring shape for each stage in most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17). Coalition organization.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine having blades (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, each outer compressor blade group (16 ) And an inner compressor moving blade group (17), in which a water cooling blade (87) is provided in an annular shape for each paragraph in a stage.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine having blades (81) and driven by high-temperature water (5a) at supercritical pressure or the like, each outer compressor blade group ( 16) A combined turbine blade and steam gas turbine engine in which water cooling blades (87) are provided annularly for each paragraph in most of the inner compressor rotor blade group (17).

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed in an annular shape (84) into an assembled structure, is large. An all-blade steam gas turbine combined engine characterized in that a water-repellent water cooling blade (87) is provided in a ring in each section.

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) formed into an integrated structure by annularly casting (84). An all-blade steam gas turbine combined engine characterized in that most of the water-repellent water cooling blades (87) are provided annularly for each paragraph.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are assembled and assembled, are provided with water-repellent water cooling blades (87), and one or more water-repellent water repellent units are provided for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling a water cooling blade.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) 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) in the assembled structure to provide one or more repellent members for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling the aqueous water cooling blades.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine driven by high-temperature water (5a) or the like having blades (81), each of the outer compressor blade groups (16) and the inner compressor motion which are integrally formed in an annular shape (84) and assembled. An all-blade steam gas turbine combined engine, wherein a water cooling blade (87) is provided in a ring shape for each stage in most of the blade group (17).

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having blades (81), each of the outer compressor rotor blade groups (16) and the inner compressor has an annularly integrally cast (84) and assembled structure. An all-blade steam gas turbine combined engine, wherein a water cooling blade (87) is provided in a ring shape for each stage in a large part of the bucket group (17).

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. Of the outer compressor blade group (16) and the inner compressor blade group (17), which are formed integrally by annularly casting (84) into an annular structure, the water repellency of the entire rotor blade gas turbine. An all-blade steam gas turbine combined engine characterized in that a water cooling blade (87) is provided in an annular shape for each paragraph.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. Of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), each of which is integrally formed in an annular shape (84) and assembled, in the entire moving blade steam gas turbine. An all-blade steam gas turbine combined engine characterized in that a water cooling blade (87) is provided in an annular shape for each paragraph.

An all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. Water-repellent water cooling blades (87) are provided on most of the outer compressor rotor blade group (16) and inner compressor rotor blade group (17) to cool one or more water-repellent water cooling blades per paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) later.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). 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), and one or more water-repellent water cooling blades are provided for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with a blade (81), each of the outer compressor blade groups (16 ) And the majority 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 for each paragraph, water is injected from the water injection means (56). An all-blade steam gas turbine combined engine, characterized in that:

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine having blades (81) driven by high-temperature water (5a) at a supercritical pressure or the like, each of the outer compressor blades ( 16) and a large part of the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87), and after cooling one or more water-repellent water cooling blades per paragraph, water is supplied from a water injection means (56). An all-blade steam gas turbine combined engine characterized by injecting.

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-rotor blade gas turbine driven by high-temperature water (5a) or the like, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are formed as an integral structure by annularly casting (84). A water-repellent water cooling blade (87) is provided at a portion, and water is injected from a water injection means (56) after cooling at least one water-repellent water cooling blade for each paragraph. Coalition organization.

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) is integrally formed annularly (84) to form an assembly structure. A water-repellent water cooling blade (87) is provided for the most part, and water is injected from a water injection means (56) after cooling one or more water-repellent water cooling blades for each paragraph. Turbine united engine.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) As an assembled structure, 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), so that the whole section has less than half water repellency. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) after cooling a water cooling blade.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) As an assembled structure, water-repellent water cooling blades (87) are provided on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), so that the repellency is less than half of each paragraph. An all-blade steam gas turbine combined engine including a water-repellent water cooling blade (87) for injecting water from a water injection means (56) after cooling the aqueous water cooling blade.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine that is driven by high-temperature water (5a) or the like equipped with blades (81), the outer compressor blade group (16) and the inner compressor blade are integrally formed in an annular shape (84) to form an assembly structure. Water-repellent water cooling blades (87) are provided in most of the blade group (17), and water is injected from the water injection means (56) after cooling one or more water-repellent water cooling blades for each paragraph. All blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine that is driven by high-temperature water (5a) or the like having blades (81), the outer compressor rotor blade group (16) and the inner compressor are integrally formed into an annular structure (84) to form an assembly structure. A water-repellent water cooling blade (87) is provided in most of the moving blade group (17), and water is injected from the water injection means (56) after cooling at least one or more water-repellent water cooling blades for each paragraph. All-blade steam gas turbine combined engine.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by, for example, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are largely water-repellent as an assembled structure by being integrally cast in a ring (84). An all-blade steam gas turbine combined engine, comprising: a water cooling blade (87); and cooling water from a water injection means (56) after cooling one or more water-repellent water cooling blades for each paragraph.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. In an all-blade steam gas turbine driven by, for example, a ring-shaped integral casting (84) and an assembling structure, a large part of each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) is repelled. An all-blade steam gas turbine combined engine, comprising: an aqueous water cooling blade (87); and cooling the one or more water-repellent water cooling blades per stage and then water injection from a water injection means (56).

In an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., it is integrally assembled into a ring (84) to form an assembly structure. 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) to cool less than half of the water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine, wherein water is injected from a water injection means (56) later.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with the water-repellent water cooling blades (87), and half or less of the water-repellent water cooling blades are provided for each paragraph. An all-blade steam gas turbine combined engine including a water-repellent water cooling blade (87) for injecting water from a water injection means (56) after cooling.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with a blade (81), each of the outer compressor blade groups (16 ) And the majority of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87). An all-blade steam gas turbine combined engine including a water-repellent water cooling blade (87).

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine having blades (81) driven by high-temperature water (5a) at a supercritical pressure or the like, each of the outer compressor blades ( Water repellent water cooling blades (87) are provided on most of the 16) and inner compressor rotor blade groups (17). An all-blade steam gas turbine combined engine including a water-repellent water cooling blade (87) for injection.

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-rotor blade gas turbine driven by high-temperature water (5a) or the like, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are formed as an integral structure by annularly casting (84). A water-repellent water cooling wing (87) is provided in the portion, and the water-repellent water-cooling wing (87) for jetting water from the water jetting means (56) after cooling the water-repellent water cooling wings of all the lower half in every paragraph. An all-blade steam gas turbine combined engine, characterized in that:

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) is integrally formed annularly (84) to form an assembly structure. A water-repellent water cooling blade (87) is provided for the most part, and water is injected from a water injection means (56) after cooling all the water-repellent water cooling blades of each half or less in every paragraph. Turbine united engine.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water-repellent water cooling blade (87) is provided for each stage in a ring shape in most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) which are assembled and assembled, and driven by the output. An all-blade steam gas turbine combined engine, comprising:

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water-repellent water cooling blade (87) is provided for each stage in a ring shape on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are assembled and assembled, and the output power An all-blade steam gas turbine combined engine comprising a driving device.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine that is driven by high-temperature water (5a) or the like equipped with blades (81), the outer compressor blade group (16) and the inner compressor blade are integrally formed in an annular shape (84) to form an assembly structure. Water-repellent water cooling wings (87) are provided on most of the wing group (17), and water-repellent water cooling is performed by jetting water from the water jetting means (56) after cooling the water-repellent water cooling wings of each half or less in every paragraph. An all-blade steam gas turbine combined engine including a blade (87).

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine that is driven by high-temperature water (5a) or the like having blades (81), the outer compressor rotor blade group (16) and the inner compressor are integrally formed into an annular structure (84) to form an assembly structure. A water-repellent water cooling wing (87) is provided on most of the moving blade group (17), and water-repellent water is jetted from the water jetting means (56) after cooling less than half of the water-repellent water cooling wings for each paragraph. An all-blade steam gas turbine combined engine including a cooling blade (87).

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by, for example, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are largely water-repellent as an assembled structure by being integrally cast in a ring (84). A water cooling blade (87) is provided, and a water-repellent water cooling blade (87) that sprays water from the water injection means (56) after cooling the water-repellent water cooling blades in all the lower half of each paragraph is included. All blade steam gas turbine combined engine.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. In an all-blade steam gas turbine driven by, for example, a ring-shaped integral casting (84) and an assembling structure, a large part of each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) is repelled. An all-blade steam / gas turbine combined engine, comprising an aqueous water cooling blade (87), and cooling water of less than half of the water-repellent water cooling blades for each paragraph and then water injection from a water injection means (56).

An all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) were provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph, and a device driven by the output was provided. An all-blade steam gas turbine combined engine, characterized in that:

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph, and are driven by the output. An all-bladed steam gas turbine combined engine characterized by the following.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine having blades (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, each outer compressor blade group (16 ) And the majority of the inner compressor rotor group (17) are provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph, and a device driven by the output is provided. Turbine united engine.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine having blades (81) and driven by high-temperature water (5a) at supercritical pressure or the like, each outer compressor blade group ( 16) and the entire compressor rotor blade group (17) is provided with a water-repellent water cooling blade (87) in a ring shape for each paragraph and provided with a device driven by the output. Gas turbine combined engine.

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed in an annular shape (84) into an assembled structure, is large. An all-blade steam gas turbine combined engine, characterized in that a water-repellent water cooling blade (87) is provided in an annular shape in each section, and a device driven by the output is provided.

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) formed into an integrated structure by annularly casting (84). An all-blade steam gas turbine combined engine, characterized in that a water-repellent water cooling blade (87) is provided for the most part in an annular shape for each stage and a device driven by the output is provided.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are assembled and assembled, are provided with water-repellent water cooling blades (87), and one or more water-repellent water repellent units are provided for each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) after cooling the water cooling blades and driving with the output.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) 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) in the assembled structure to provide one or more repellent members for each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) after cooling the aqueous water cooling blades and driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine driven by high-temperature water (5a) or the like having blades (81), each of the outer compressor blade groups (16) and the inner compressor motion which are integrally formed in an annular shape (84) and assembled. An all-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 blade group (17) and a device driven by the output is provided.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having blades (81), each of the outer compressor rotor blade groups (16) and the inner compressor has an annularly integrally cast (84) and assembled structure. An all-blade steam gas turbine combined engine, characterized in that a water-repellent water cooling blade (87) is provided annularly for each stage in a majority of the blade groups (17) and a device driven by the output is provided.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. Of the outer compressor blade group (16) and the inner compressor blade group (17), which are formed integrally by annularly casting (84) into an annular structure, the water repellency of the entire rotor blade gas turbine. An all-blade steam gas turbine combined engine, comprising a water cooling blade (87) provided annularly for each stage and a device driven by the output.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. And the like, the outer compressor rotor blade group (16) and the inner compressor rotor group (17) are repelled by a large part of each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed into a ring (84) and assembled. An all-blade steam gas turbine combined engine, comprising: an aqueous water cooling blade (87) provided annularly for each stage; and a device driven by the output.

An all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. Water-repellent water cooling blades (87) are provided on most of the outer compressor rotor blade group (16) and inner compressor rotor blade group (17) to cool one or more water-repellent water cooling blades per paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) later and driving with the output.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). 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), and one or more water-repellent water cooling blades are provided for each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) after cooling and for driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine having blades (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, each outer compressor blade group (16 ) And the majority of the inner compressor blade group (17) are provided with a water-repellent water cooling blade (87), and after cooling one or more water-repellent water cooling blades for 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.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine having blades (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, each of the outer compressor blades (84) is integrally formed annularly into an assembled structure (84). 16) and a large part of the inner compressor rotor blade group (17) are provided with a water-repellent water cooling blade (87), and after cooling one or more water-repellent water cooling blades per paragraph, water is supplied from a water injection means (56). An all-blade steam gas turbine combined engine, comprising: a device for injecting and driving with the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed in an annular shape (84) into an assembled structure, is large. A water-repellent water cooling blade (87) is provided in the portion, and after cooling one or more of the plurality of water-repellent water cooling blades for each paragraph, water is injected from the water injection means (56) and the device is driven by the output. An all-blade steam gas turbine combined engine, characterized in that:

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) formed into an integrated structure by annularly casting (84). A water-repellent water cooling blade (87) is provided for the most part, and a device for injecting water from the water injection means (56) after cooling one or more water-repellent water cooling blades for each paragraph and driving with the output is provided. An all-bladed steam gas turbine combined engine characterized by the following.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) As an assembled structure, 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), so that the whole section has less than half water repellency. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) after cooling the water cooling blades and driving with the output.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) As an assembled structure, water-repellent water cooling blades (87) are provided on most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), so that the repellency is less than half of each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) after cooling the aqueous water cooling blades and driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine driven by high-temperature water (5a) or the like having blades (81), each of the outer compressor blade groups (16) and the inner compressor motion which are integrally formed in an annular shape (84) and assembled. A water-repellent water cooling blade (87) is provided on a large part of the blade group (17), and after cooling one or more water-repellent water cooling blades for each paragraph, water is jetted from a water jetting means (56) to output the water. An all-blade steam gas turbine combined engine, characterized by comprising a device driven by:

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine that is driven by high-temperature water (5a) or the like equipped with a wing (81), each of the outer compression motive blade groups (16) and the inner compression that are integrally formed into an annular shape (84) and assembled. A water-repellent water cooling blade (87) is provided on most of the moving blade group (17), and after cooling one or more water-repellent water cooling blades per paragraph, water is injected from a water injection means (56). An all-blade steam gas turbine combined engine comprising a device driven by an output.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. Of the outer compressor blade group (16) and the inner compressor blade group (17), which are formed integrally by annularly casting (84) into an annular structure, the water repellency of the entire rotor blade gas turbine. A water cooling blade (87) is provided, and one or more water-repellent water cooling blades for each paragraph are cooled, and then water is injected from a water injection means (56), and a device driven by the output is provided. All blade steam gas turbine combined engine.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. And the like, the outer compressor rotor blade group (16) and the inner compressor rotor group (17) are repelled by a large part of each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally formed into a ring (84) and assembled. A water-based water cooling blade (87) is provided, and after cooling one or more water-repellent water-cooled blades per paragraph, water is injected from a water injection means (56), and a device driven by the output is provided. All-blade steam gas turbine combined engine.

In an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., it is integrally assembled into a ring (84) to form an assembly structure. 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) to cool less than half of the water-repellent water cooling blades for each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) later and driving with the output.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). Most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are provided with the water-repellent water cooling blades (87), and half or less of the water-repellent water cooling blades are provided for each paragraph. An all-blade steam gas turbine combined engine, comprising: a device for injecting water from a water injection means (56) after cooling and for driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with a blade (81), each of the outer compressor blade groups (16 ) And the majority of the inner compressor rotor blade group (17) are provided with water-repellent water cooling blades (87). An all-blade steam gas turbine combined engine comprising a device driven by the output.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine having blades (81) driven by high-temperature water (5a) or the like having a supercritical pressure or the like, each of the outer compression rotor blades ( Water repellent water cooling blades (87) are provided on most of the 16) and inner compressor rotor blade groups (17). An all-blade steam gas turbine combined engine, comprising: a device for injecting and driving with the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-rotor blade gas turbine driven by high-temperature water (5a) or the like, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are formed as an integral structure by annularly casting (84). A water-repellent water cooling blade (87) is provided in the portion, and a device for driving the water-repellent water-cooling blade in all stages by cooling the water-repellent water cooling blades in the following half after cooling by water injection from the water injection means (56). An all-blade steam gas turbine combined engine, characterized in that:

An outer shaft device and an inner shaft device that rotate in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. are connected at an optimum rotation ratio, and a supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like, each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) is integrally formed annularly (84) to form an assembly structure. A water-repellent water cooling blade (87) is provided for the most part, and a device for driving by the output is provided by injecting water from the water injection means (56) after cooling the water cooling blades of the lower half in every paragraph after cooling. An all-blade steam gas turbine combined engine characterized by the following.

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with a blade (81), the outer compressor rotor blade group (16) and the inner compressor A water-repellent water cooling wing (87) is provided on most of the wing group (17), and after cooling the water-repellent water-cooling wings of each half or less for each paragraph, water is jetted from a water jetting means (56) to output the water. An all-blade steam gas turbine combined engine, characterized by comprising a device driven by:

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 a contra-rotating magnetic friction power transmission device (14a) for bringing the combustion gas exhaust temperature to -273 ° C. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having wings (81), the outer compression motive blade group (16) and the inner compression A water-repellent water cooling blade (87) is provided in the majority of the moving blade group (17), and after cooling the water-repellent water cooling blades of each half or less in every paragraph, water is injected from the water injection means (56). An all-blade steam gas turbine combined engine comprising a device driven by an output.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by, for example, the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are largely water-repellent as an assembled structure by being integrally cast in a ring (84). A water cooling blade (87) is provided, and a device driven by the output is provided by injecting water from the water injection means (56) after cooling the water-repellent water cooling blades of all less than half of each paragraph after cooling. All blade steam gas turbine combined engine.

High-temperature water (5a) with an electromagnetically heated turbine blade (81) combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator that brings the combustion gas exhaust temperature close to -273 ° C. In an all-blade steam gas turbine driven by, for example, a ring-shaped integral casting (84) and an assembling structure, a large part of each of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) is repelled. A water-based water cooling blade (87) is provided, and a device driven by the output is provided by injecting water from the water injection means (56) after cooling all the water cooling blades in each half or less for each paragraph. Combined moving blade steam gas turbine engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, a water injection means (56a) is provided in an inner turbine blade group (20) which is integrally formed into an annular shape (84) and assembled. An all-blade steam gas turbine united engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, a water injection means (56a) is provided in an outer turbine bucket group (19) which is integrally formed into an annular shape (84) and assembled. An all-blade steam gas turbine united engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In an all-blade gas turbine driven by high-temperature water (5a) or the like, a water injection means (56a) is provided in an inner turbine blade group (20) formed into an integrated structure by annularly casting (84). An all-blade steam gas turbine combined engine, characterized in that:

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade gas turbine driven by high-temperature water (5a) or the like, a water injection means (56a) is provided in an outer turbine blade group (19) which is integrally formed into an annular shape (84) and assembled. An all-blade steam gas turbine combined engine, characterized in that:

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam turbine driven by high-temperature water (5a) or the like, a water injection means (56a) is provided on an inner turbine blade group (20) which is integrally formed into an annular shape (84) and assembled. An all-blade steam gas turbine combined engine, characterized in that:

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam turbine driven by high-temperature water (5a) or the like, a water injection means (56a) is provided in an outer turbine blade group (19) formed into an integrated structure by annularly casting (84). An all-blade steam gas turbine combined engine, characterized in that:

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, characterized in that a water injection means (56a) is provided in an inner turbine rotor blade group (20) which is integrally formed into an annular shape (84) and assembled. All-blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) and the like, wherein a water injection means (56a) is provided in an outer turbine rotor blade group (19) which is integrally formed in an annular shape (84) into an assembled structure. All-blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), etc., in which a water injection means (56a) is provided in an inner turbine blade group (20) which is integrally assembled in an annular shape (84) and assembled. All blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), etc., in which a water injection means (56a) is provided in an outer turbine rotor blade group (19) which is integrally formed into an annular shape (84) and assembled. All blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), etc., in which a water injection means (56a) is provided in an inner turbine blade group (20) which is integrally formed annularly (84) into an assembled structure. All blade steam gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), etc., in which a water injection means (56a) is provided in an outer turbine rotor blade group (19) which is integrally formed into an annular shape (84) and has an assembled structure. All blade steam gas turbine combined engine.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade steam gas turbine, the water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine moving blade group (20) which is integrally formed in an annular shape (84). All-blade steam gas turbine combined engine.

An inner turbine blade having an electromagnetic heating turbine blade (81), which is driven by high-temperature water (5a) at a supercritical pressure or the like and which is driven by high-temperature water (5a) or the like, and which is integrally formed into a ring (84) and assembled. An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of the assembled annular connection part of the group (20) with heat insulation.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade steam gas turbine, the water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine moving blade group (19) which is integrally formed into an annular structure (84). All-blade steam gas turbine combined engine.

An outer turbine rotor blade having an electromagnetically heated turbine rotor blade (81) and integrally assembled in an annular shape (84) in an all-rotor blade steam gas turbine driven by high-temperature water (5a) at a supercritical pressure or the like. An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of the assembled annular connection part of the group (19) with heat insulation.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade gas turbine, a water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine moving blade group (20) which is integrally formed into an annular structure (84). All-blade steam gas turbine combined engine.

A group of inner turbine blades which are integrally formed in an annular shape (84) in an all-blade gas turbine driven by high-temperature water (5a) at a supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81). (20) A combined turbine and steam turbine engine in which a water injection means (56a) is provided in the vicinity of the assembling annular connection part insulated.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade gas turbine, a water injection means (56a) is insulated and provided in the vicinity of an assembled annular connection portion of an outer turbine moving blade group (19) which is integrally formed into an annular structure (84). All-blade steam gas turbine combined engine.

An outer turbine blade group having an electromagnetically-heated turbine blade (81), which is driven by high-temperature water (5a) at a supercritical pressure or the like and which is driven by a supercritical pressure or the like, and which is integrally assembled (84) into an annular structure. (19) A combined steam turbine and all-blade engine, wherein a water injection means (56a) is provided in the vicinity of the assembled annular connection part insulated.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade steam turbine, a water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine moving blade group (20) which is integrally formed into an annular structure (84). All-blade steam gas turbine combined engine.

A group of inner turbine blades which are integrally formed in an annular shape (84) in an all-blade steam turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetic heating turbine blade (81). (20) A combined turbine and steam turbine engine in which a water injection means (56a) is provided in the vicinity of the assembling annular connection part insulated.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade steam turbine, a water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine moving blade group (19) which is integrally formed into an annular structure (84). All-blade steam gas turbine combined engine.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). Wherein the water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) which is integrally formed into an annular shape (84). Wing steam gas turbine combined engine.

In an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), an inner turbine blade group (20) having an annularly-integrated casting (84) and an assembled structure. An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of the assembled annular connection part insulated.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). Wherein the water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) which is integrally formed into an annular shape (84). Wing steam gas turbine combined engine.

In an all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), an outer turbine blade group (19) is integrally formed into a ring (84) and assembled. An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of the assembled annular connection part insulated.

An all-rotor gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine rotor blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. A water injection means (56a) insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into an annular shape (84). Steam gas turbine combined engine.

Assembling of an inner turbine moving blade group (20) having an assembling structure by integrally casting (84) into an annular shape in a full moving blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine moving blade (81). An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of an annular connection part insulated.

An all-rotor gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine rotor blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. A water injection means (56a) insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) formed into an annular structure by integral casting (84). Steam gas turbine combined engine.

Assembling of an outer turbine blade group (19) having an assembly structure by integrally casting (84) into an annular structure in a full blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of an annular connection part insulated.

An all-spindle steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81). A water injection means (56a) insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into an annular shape (84). Steam gas turbine combined engine.

Assembling of an inner turbine moving blade group (20) having an integrated structure by integrally casting (84) into an annular shape in a full moving blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine moving blade (81). An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of an annular connection part insulated.

An all-spindle steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81). A water injection means (56a) insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) formed into an annular structure by integral casting (84). Steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, water is injected near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into a ring (84) and assembled. An all-blade steam gas turbine combined engine characterized in that the means (56a) is provided insulated to cool superheated steam, reduce the volume and increase the unit mass.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In the all-blade gas turbine driven by high-temperature water (5a) or the like, the water injection means is provided near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into an annular shape (84) and assembled. (56a) is provided insulated to cool the superheated steam, reduce the volume and increase the unit mass, and the combined rotor blade steam gas turbine engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam turbine driven by high-temperature water (5a) or the like, water injection means is provided near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into an annular shape (84) and assembled. (56a) is provided insulated to cool the superheated steam, reduce the volume and increase the unit mass, and the combined rotor blade steam gas turbine engine.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade steam gas turbine, a water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine moving blade group (20) which is integrally formed in an annular shape (84) to assemble superheated steam. , The volume of which is reduced and the unit mass is increased.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade gas turbine, a water injection means (56a) is provided in an insulated manner near the assembled annular connection portion of the inner turbine moving blade group (20) which is integrally formed in an annular shape (84) to assemble superheated steam. An all-blade steam gas turbine combined engine that cools, reduces the volume, and increases the unit mass.

An outer shaft device and an inner shaft device rotating in opposite directions by a generator are connected at an optimum rotation ratio, and are driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) at a supercritical pressure or the like. In the moving blade steam turbine, a water injection means (56a) is provided in an insulated manner near the assembled annular connection portion of the inner turbine moving blade group (20) which is integrally formed in an annular shape (84) to assemble superheated steam. An all-blade steam gas turbine combined engine that cools, reduces the volume, and increases the unit mass.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine having a moving blade (81) driven by high-temperature water (5a) or the like having a supercritical pressure or the like, an inner turbine moving blade group (20) having an annularly integrated casting (84) and an assembled structure is provided. ), Wherein a water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection to cool the superheated steam, reduce the volume and increase the unit mass, and combine the all-blade steam gas turbine combined engine. .

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine equipped with a moving blade (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, an outer turbine moving blade group (19) having an annularly integrated casting (84) and an assembled structure (19) ), Wherein a water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection to cool the superheated steam, reduce the volume and increase the unit mass, and combine the all-blade steam gas turbine combined engine. .

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. An inner turbine blade group (20) having an integral structure in an annularly integrated casting (84) in an all-rotor blade gas turbine having a rotor blade (81) and driven by high-temperature water (5a) at a supercritical pressure or the like. A combined turbine / steam gas turbine engine in which a water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection part to cool the combustion gas, reduce the volume and increase the unit mass.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), the water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed in an annular shape (84) and assembled. An all-blade steam gas turbine combined engine, which is provided with heat insulation to cool superheated steam, reduce the volume and increase the unit mass.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), the water injection means (56a) is thermally insulated in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into a ring (84) and assembled. A superheated steam is cooled to reduce the volume of the superheated steam and increase the unit mass thereof.

An all-rotor steam gas turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like having an electromagnetically heated turbine rotor blade (81). In the above, a water injection means (56a) is insulated and provided near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into an annular shape (84) to cool the superheated steam. An all-blade steam gas turbine combined engine characterized by reducing the volume and increasing the unit mass.

An all-rotor gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine rotor blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio. A water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into an annular shape (84) to cool the superheated steam, and A combined rotor blade steam gas turbine engine characterized by reducing the size and increasing the unit mass.

An all-spindle steam turbine in which an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio and driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81). A water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into an annular shape (84) to cool the superheated steam, and A combined rotor blade steam gas turbine engine characterized by reducing the size and increasing the unit mass.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having a moving blade (81), an assembled annular connection of an inner turbine moving blade group (20) integrally formed into a ring (84) and assembled. A steam turbine combined engine with all blades, characterized in that a water injection means (56a) is insulated and provided in the vicinity of a section to cool superheated steam, reduce the volume and increase the unit mass.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having a moving blade (81), an assembled annular connection of an outer turbine moving blade group (19) integrally formed in a ring (84) and assembled. A steam turbine combined engine with all blades, characterized in that a water injection means (56a) is insulated and provided in the vicinity of a section to cool superheated steam, reduce the volume and increase the unit mass.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like provided with a moving blade (81), an assembled annular connection portion of an inner turbine moving blade group (20) formed into an integrated structure by annularly casting (84). An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided insulated in the vicinity to cool the combustion gas, reduce the volume and increase the unit mass.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. Outer turbine blade group (19) which is integrally formed annularly (84) into an assembled structure in a whole blade gas turbine driven by high-temperature water (5a) at a supercritical pressure or the like having a blade (81). A combined turbine / steam gas turbine engine in which a water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection part to cool the combustion gas, reduce the volume and increase the unit mass.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, water injection means is provided near an assembled annular connection portion of an inner turbine blade group (20) which is integrally formed in an annular shape (84) and assembled. (56a) is provided insulated to cool the superheated steam, reduce the volume and increase the unit mass, and the combined rotor blade steam gas turbine engine.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, a water injection means is provided near an annular connection portion of an outer turbine blade group (19) integrally formed in a ring (84) and assembled. (56a) is provided with heat insulation to cool superheated steam and combustion gas, reduce the volume and increase the unit mass, and a combined rotor blade steam gas turbine engine.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by high-temperature water (5a) or the like, the water injection means ( 56a), wherein the combustion gas is cooled to reduce the volume and the unit mass is increased so as to increase the unit mass.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by the high-temperature water (5a) or the like, the water injection means ( 56a), wherein the combustion gas is cooled to reduce the volume and the unit mass is increased so as to increase the unit mass.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) formed as an assembled structure to insulate the superheated steam and the combustion gas by reducing the volume by reducing the volume. An all-blade steam gas turbine combined engine characterized by increasing mass.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) Water cooling means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) having the assembled structure to cool the superheated steam or the combustion gas, thereby reducing the volume. An all-blade steam gas turbine combined engine characterized by increasing mass.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) formed as an assembled structure to cool the combustion gas, thereby reducing the volume and increasing the unit mass. An all-blade steam gas turbine combined engine, characterized in that:

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) formed as an assembled structure to cool the combustion gas, thereby reducing the volume and increasing the unit mass. An all-blade steam gas turbine combined engine, characterized in that:

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water injection means (56a) is insulated and provided near the assembled annular connection portion of the inner turbine blade group (20) having the assembled structure to cool the combustion gas and to be driven by the output. An all-blade steam gas turbine combined engine characterized by the following.

In a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) having the assembled structure to cool the superheated steam or combustion gas and to be driven by the output. An all-blade steam gas turbine combined engine, comprising:

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A device for cooling the superheated steam or combustion gas by providing a water injection means (56a) in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having the assembled structure to cool the superheated steam and the combustion gas, and to drive by the output. An all-blade steam gas turbine combined engine comprising:

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure and provided with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., an annularly integrated casting (84) A water-injecting means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) which is assembled to cool the superheated steam or combustion gas and is driven by the output. An all-blade steam gas turbine combined engine comprising:

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with a moving blade (81), an assembled annular connection portion of an outer turbine moving blade group (19) formed into an integrated structure by annularly casting (84). An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided insulated in the vicinity to cool the combustion gas, reduce the volume and increase the unit mass.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the water injection means (56a) is insulated near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed in an annular shape (84) and assembled. A superheated steam is cooled to reduce the volume of the superheated steam and increase the unit mass thereof.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the water injection means (56a) is insulated near the annular connection portion of the outer turbine blade group (19) which is integrally formed annularly (84) and assembled. A superheated steam or a combustion gas is cooled to reduce the volume and increase the unit mass of the combined rotor blade steam gas turbine engine.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the water injection means (56a) is insulated near the assembled annular connection portion of the inner turbine blade group (20), which is integrally formed in an annular shape (84) and assembled. A combined turbine and steam gas turbine engine for cooling combustion gas, reducing the volume and increasing the unit mass.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the water injection means (56a) is insulated in the vicinity of the assembled annular connection of the outer turbine blade group (19) which is integrally formed in an annular shape (84) and assembled. A combined turbine and steam gas turbine engine for cooling combustion gas, reducing the volume and increasing the unit mass.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). A water injection means (56a) is insulated and provided near the assembled annular connection portion of the inner turbine blade group (20) to cool superheated steam and combustion gas, thereby reducing the volume and increasing the unit mass. An all-blade steam gas turbine combined engine characterized by the following.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) which is insulated to cool superheated steam and combustion gas, thereby reducing the volume and increasing the unit mass. An all-blade steam gas turbine combined engine characterized by the following.

An all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. A water injection means (56a) is provided in the vicinity of the assembled annular connection of the inner turbine blade group (20) insulated to cool the combustion gas, reduce the volume, and increase the unit mass. All blade steam gas turbine combined engine.

An all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) insulated to cool the combustion gas, reduce the volume and increase the unit mass. All blade steam gas turbine combined engine.

An all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) insulated to cool combustion gas and to be driven by the output. Combined moving blade steam gas turbine engine.

An all-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) insulated to cool superheated steam or combustion gas and to be driven by the output. All-blade steam gas turbine combined engine.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). In the vicinity of the assembled annular connection portion of the inner turbine blade group (20), a water injection means (56a) is provided insulated to cool superheated steam or combustion gas and driven by the output. All-blade steam gas turbine combined engine.

An all-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., and is integrally assembled in an annular shape (84). A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) which is insulated to cool superheated steam or combustion gas and is driven by the output. All-blade steam gas turbine combined engine.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. An inner turbine blade group (20) having an integral structure in an annularly integrated casting (84) in an all-rotor blade gas turbine having a rotor blade (81) and driven by high-temperature water (5a) at a supercritical pressure or the like. A steam turbine combined engine with all blades, characterized in that a water injection means (56a) is provided in the vicinity of the assembled annular connection part insulated to cool combustion gas and to be driven by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. Outer turbine blade group (19) which is integrally formed annularly (84) into an assembled structure in a whole blade gas turbine driven by high-temperature water (5a) at a supercritical pressure or the like having a blade (81). A steam turbine combined engine with all blades, characterized in that a water injection means (56a) is provided in the vicinity of the assembled annular connection part insulated to cool combustion gas and to be driven by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine having a moving blade (81) driven by high-temperature water (5a) or the like having a supercritical pressure or the like, an inner turbine moving blade group (20) having an annularly integrated casting (84) and an assembled structure is provided. ), An all-blade steam gas turbine characterized in that a water injection means (56a) is provided insulated near the annular connection part to cool superheated steam or combustion gas and to be driven by the output. Coalition organization.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine equipped with a moving blade (81) and driven by high-temperature water (5a) at a supercritical pressure or the like, an outer turbine moving blade group (19) having an annularly integrated casting (84) and an assembled structure (19) ), An all-blade steam gas turbine characterized in that a water injection means (56a) is provided insulated near the annular connection part to cool superheated steam or combustion gas and to be driven by the output. Coalition organization.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by high-temperature water (5a) or the like, the water injection means ( 56a). A combined rotor blade steam gas turbine engine characterized by comprising a device for cooling combustion gas by providing 56a) insulated and driving by the output.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by the high-temperature water (5a) or the like, the water injection means ( 56a). A combined rotor blade steam gas turbine engine characterized by comprising a device for cooling combustion gas by providing 56a) insulated and driving by the output.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In the all-blade steam gas turbine driven by the high-temperature water (5a) or the like, a water injection means (56a) is provided near the assembled annular connection portion of the inner turbine blade group (20) integrally formed in an annular shape and assembled. An all-blade steam gas turbine combined engine, comprising: a device that insulates and heats superheated steam or combustion gas and drives the device with the output.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In the all-blade steam gas turbine driven by the high-temperature water (5a) or the like, a water injection means (56a) is provided near the assembled annular connection portion of the outer turbine blade group (19) integrally formed in an annular shape and assembled. An all-blade steam gas turbine combined engine, comprising: a device that insulates and heats superheated steam or combustion gas and drives the device with the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like provided with a moving blade (81), an assembled annular connection portion of an inner turbine moving blade group (20) formed into an integrated structure by annularly casting (84). An all-blade steam gas turbine combined engine, comprising: a device for cooling a combustion gas by providing a water injection means (56a) in an insulated manner in the vicinity thereof and driving by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like equipped with a moving blade (81), an assembled annular connection portion of an outer turbine moving blade group (19) formed into an integrated structure by annularly casting (84). An all-blade steam gas turbine combined engine, comprising: a device for cooling a combustion gas by providing a water injection means (56a) in an insulated manner in the vicinity thereof and driving by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having a moving blade (81), an assembled annular connection of an inner turbine moving blade group (20) integrally formed into a ring (84) and assembled. An all-blade steam gas turbine combined engine, comprising a device for cooling superheated steam or combustion gas by providing a water injection means (56a) in an insulated manner in the vicinity of the unit, and driving the superheated steam or combustion gas with the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having a moving blade (81), an assembled annular connection of an outer turbine moving blade group (19) integrally formed in a ring (84) and assembled. An all-blade steam gas turbine combined engine, comprising a device for cooling superheated steam or combustion gas by providing a water injection means (56a) in an insulated manner in the vicinity of the unit, and driving the superheated steam or combustion gas with the output.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the water injection means (56a) is insulated near the assembled annular connection portion of the inner turbine blade group (20), which is integrally formed in an annular shape (84) and assembled. An all-blade steam gas turbine combined engine, characterized by comprising a device for cooling the combustion gas and driving the combustion gas with the output.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the water injection means (56a) is insulated in the vicinity of the assembled annular connection of the outer turbine blade group (19) which is integrally formed in an annular shape (84) and assembled. An all-blade steam gas turbine combined engine, characterized by comprising a device for cooling the combustion gas and driving the combustion gas with the output.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the water injection means (56a) is provided insulated near the assembled annular connection portion of the inner turbine blade group (20), which is integrally formed in an annular shape and assembled. An all-blade steam gas turbine combined engine, comprising: a device that cools superheated steam or combustion gas by using the power and drives the steam turbine with the output.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the water injection means (56a) is provided insulated near the assembled annular connection portion of the outer turbine blade group (19) which is integrally formed in an annular shape and assembled. An all-blade steam gas turbine combined engine, comprising: a device that cools superheated steam or combustion gas by using the power and drives the steam turbine with the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. Assembling of an inner turbine blade group (20) having an integrated structure by integrally casting (84) in an annular shape in an all-blade steam turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with (81). An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of an annular connection part insulated.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. Assembling of an inner turbine blade group (20) having an integrated structure by integrally casting (84) in an annular shape in an all-blade steam turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with (81). An all-blade steam gas turbine combined engine, comprising: a device that insulates a water injection means (56a) in the vicinity of an annular connection portion to cool superheated steam and drives the superheated steam by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. Assembling of the outer turbine blade group (19) having an integrated structure by integrally casting (84) into a ring in a full blade steam turbine driven by high temperature water (5a) or the like having a supercritical pressure equipped with (81). An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of an annular connection part insulated.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. Assembling of the outer turbine blade group (19) having an integrated structure by integrally casting (84) into a ring in a full blade steam turbine driven by high temperature water (5a) or the like having a supercritical pressure equipped with (81). An all-blade steam gas turbine combined engine, comprising: a device that insulates a water injection means (56a) in the vicinity of an annular connection portion to cool superheated steam and drives the superheated steam by the output.

The outer shaft device and the inner shaft device rotating in opposite directions by a generator are adiabatically expanded to a condenser vacuum, and the outer shaft device and the inner shaft device are coupled at an optimum rotation ratio, and a high temperature such as supercritical pressure equipped with an electromagnetically heated turbine blade (81) is provided. In the all-blade steam turbine driven by water (5a) or the like, the water injection means (56a) is insulated near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed in an annular shape and assembled. An all-blade steam gas turbine combined engine, characterized in that:

The outer shaft device and the inner shaft device rotating in opposite directions by a generator are adiabatically expanded to a condenser vacuum, and the outer shaft device and the inner shaft device are coupled at an optimum rotation ratio, and a high temperature such as supercritical pressure equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam turbine driven by water (5a) or the like, a water injection means (56a) is provided near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into a ring (84) and assembled. Characterized in that it is provided with a device that insulates the superheated steam to cool the superheated steam and drives the superheated steam with the output.

The outer shaft device and the inner shaft device rotating in opposite directions by a generator are adiabatically expanded to a condenser vacuum, and the outer shaft device and the inner shaft device are coupled at an optimum rotation ratio, and a high temperature such as supercritical pressure equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam turbine driven by water (5a) or the like, water injection means (56a) is insulated near the assembled annular connection portion of the outer turbine blade group (19) which is integrally formed in an annular shape and assembled. An all-blade steam gas turbine combined engine, characterized in that:

The outer shaft device and the inner shaft device rotating in opposite directions by a generator are adiabatically expanded to a condenser vacuum, and the outer shaft device and the inner shaft device are coupled at an optimum rotation ratio, and a high temperature such as supercritical pressure equipped with an electromagnetically heated turbine blade (81) is provided. In an all-blade steam turbine driven by water (5a) or the like, a water injection means (56a) is provided near the assembled annular connection portion of the outer turbine blade group (19) formed into an integrated structure by annularly casting (84). Characterized in that it is provided with a device that insulates the superheated steam to cool the superheated steam and drives the superheated steam with the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In an all-blade steam turbine driven by high-temperature water (5a) or the like equipped with (81), near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into a ring (84) and assembled. And a water jet means (56a) provided with heat insulation.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In an all-blade steam turbine driven by high-temperature water (5a) or the like equipped with (81), near the assembled annular connection portion of the inner turbine blade group (20) which is integrally formed into a ring (84) and assembled. And a device for cooling the superheated steam by providing the water injection means (56a) insulated and driving the steam turbine with the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In an all-blade steam turbine driven by high-temperature water (5a) or the like provided with (81), near the assembled annular connection portion of the outer turbine blade group (19) formed into an integrated structure (84) in an annular shape. And a water jet means (56a) provided with heat insulation.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In an all-blade steam turbine driven by high-temperature water (5a) or the like provided with (81), near the assembled annular connection portion of the outer turbine blade group (19) formed into an integrated structure (84) in an annular shape. And a device for cooling the superheated steam by providing the water injection means (56a) insulated and driving the steam turbine with the output.

High-temperature water (5a) with electromagnetic heating turbine blades (81), combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator, adiabatically expanding to a condenser vacuum, and having an electromagnetic heating turbine blade (81) That the water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) which is integrally formed in an annular shape and is assembled in the turbine blade driven by the turbine. All-blade steam gas turbine combined engine.

High-temperature water (5a) with electromagnetic heating turbine blades (81), combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator, adiabatically expanding to a condenser vacuum, and having an electromagnetic heating turbine blade (81) The water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20), which is integrally formed in an annular shape (84) in the assembled structure in the turbine blade driven by the above. A combined steam turbine engine with all rotor blades, comprising: a device for cooling superheated steam and driving by the output.

High-temperature water (5a) with electromagnetic heating turbine blades (81), combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator, adiabatically expanding to a condenser vacuum, and having an electromagnetic heating turbine blade (81) That the water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19), which is integrally formed in an annular shape and assembled in the turbine blade driven by the turbine. All-blade steam gas turbine combined engine.

High-temperature water (5a) with electromagnetic heating turbine blades (81), combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator, adiabatically expanding to a condenser vacuum, and having an electromagnetic heating turbine blade (81) The water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19), which is integrally formed in an annular shape (84) in an assembled structure, in the all blade steam turbine driven by A combined steam turbine engine with all rotor blades, comprising: a device for cooling superheated steam and driving by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with (81), an annular ring (84) is assembled into an assembled annular turbine blade group (20) having an assembled structure. An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of a connection part insulated.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with (81), an annular ring (84) is assembled into an assembled annular turbine blade group (20) having an assembled structure. An all-blade steam gas turbine combined engine, comprising: a device for cooling a superheated steam by providing a water injection means (56a) insulated near a connection portion and driving the superheated steam by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with (81), an annular ring (84) and an annular assembly of the outer turbine bucket group (19) formed into an assembled structure. An all-blade steam gas turbine combined engine, wherein a water injection means (56a) is provided in the vicinity of a connection part insulated.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In an all-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with (81), an annular ring (84) and an annular assembly of the outer turbine bucket group (19) formed into an assembled structure. An all-blade steam gas turbine combined engine, comprising: a device for cooling a superheated steam by providing a water injection means (56a) insulated near a connection portion and driving the superheated steam by the output.

The outer shaft device and the inner shaft device rotating in opposite directions by a generator are adiabatically expanded to a condenser vacuum, and the outer shaft device and the inner shaft device are coupled at an optimum rotation ratio, and a high temperature such as supercritical pressure equipped with an electromagnetically heated turbine blade (81) is provided. In the all-blade steam gas turbine driven by water (5a) or the like, a water injection means (56a) is provided near the assembled annular connection portion of the inner turbine blade group (20) formed by annular casting (84). An all-blade steam gas turbine combined engine characterized by being provided with heat insulation.

The outer shaft device and the inner shaft device rotating in opposite directions by a generator are adiabatically expanded to a condenser vacuum, and the outer shaft device and the inner shaft device are coupled at an optimum rotation ratio, and a high temperature such as supercritical pressure equipped with an electromagnetically heated turbine blade (81) is provided. In the all-blade steam gas turbine driven by water (5a) or the like, a water injection means (56a) is provided near the assembled annular connection portion of the inner turbine blade group (20) formed by annular casting (84). An all-blade steam gas turbine combined engine, comprising a device that is provided insulated to cool superheated steam and is driven by the output.

The outer shaft device and the inner shaft device rotating in opposite directions by a generator are adiabatically expanded to a condenser vacuum, and the outer shaft device and the inner shaft device are coupled at an optimum rotation ratio, and a high temperature such as supercritical pressure equipped with an electromagnetically heated turbine blade (81) is provided. In a full-blade steam gas turbine driven by water (5a) or the like, a water injection means (56a) is provided near the assembled annular connection portion of the outer turbine blade group (19) formed by annular casting (84). An all-blade steam gas turbine combined engine characterized by being provided with heat insulation.

The outer shaft device and the inner shaft device rotating in opposite directions by a generator are adiabatically expanded to a condenser vacuum, and the outer shaft device and the inner shaft device are coupled at an optimum rotation ratio, and a high temperature such as supercritical pressure equipped with an electromagnetically heated turbine blade (81) is provided. In a full-blade steam gas turbine driven by water (5a) or the like, a water injection means (56a) is provided near the assembled annular connection portion of the outer turbine blade group (19) formed by annular casting (84). An all-blade steam gas turbine combined engine, comprising a device that is provided insulated to cool superheated steam and is driven by the output.

A low-temperature combustion gas containing harmful substances in a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure 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, wherein water and steam are agglomerated to form hail, water droplets and the like with the core as a core.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., coal ash and harmful substances are removed. An all-blade steam gas turbine combined engine, wherein water and steam are agglomerated into a hail, a water droplet, and the like using a low-temperature combustion gas containing the core as a core.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In the all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with (81), near the assembled annular connection portion of the inner turbine blade group (20) formed into an annular structure by the annular casting (84), An all-blade steam gas turbine combined engine, wherein the water injection means (56a) is provided insulated.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In the all-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with (81), near the assembled annular connection portion of the inner turbine blade group (20) formed into an annular structure by the annular casting (84), An all-blade steam gas turbine combined engine, comprising: a device for cooling a superheated steam by providing a water injection means (56a) insulated and driving by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In the all-blade steam gas turbine driven by high-temperature water (5a) or the like provided with (81), near the assembled annular connection portion of the outer turbine blade group (19) formed into an annular structure by annular casting (84), An all-blade steam gas turbine combined engine, wherein the water injection means (56a) is provided insulated.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that adiabatically expand to a condenser vacuum are coupled at an optimal rotation ratio, and the electromagnetically heated turbine rotor blades. In the all-blade steam gas turbine driven by high-temperature water (5a) or the like provided with (81), near the assembled annular connection portion of the outer turbine blade group (19) formed into an annular structure by annular casting (84), An all-blade steam gas turbine combined engine, comprising: a device for cooling a superheated steam by providing a water injection means (56a) insulated and driving by the output.

High-temperature water (5a) with electromagnetic heating turbine blades (81), combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator, adiabatically expanding to a condenser vacuum, and having an electromagnetic heating turbine blade (81) The water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) which is formed by annular casting (84) in the assembled structure. An all-blade steam gas turbine combined engine, characterized in that:

High-temperature water (5a) with electromagnetic heating turbine blades (81), combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator, adiabatically expanding to a condenser vacuum, and having an electromagnetic heating turbine blade (81) A water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) formed into an annular structure by the annular casting (84). An all-blade steam gas turbine combined engine comprising a device for cooling superheated steam and driving the superheated steam with the output.

High-temperature water (5a) with electromagnetic heating turbine blades (81), combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator, adiabatically expanding to a condenser vacuum, and having an electromagnetic heating turbine blade (81) The water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) which is formed by annular casting (84) in the assembled structure. An all-blade steam gas turbine combined engine, characterized in that:

High-temperature water (5a) with electromagnetic heating turbine blades (81), combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator, adiabatically expanding to a condenser vacuum, and having an electromagnetic heating turbine blade (81) A water injection means (56a) is insulated and provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) formed into an annular structure by the annular casting (84). An all-blade steam gas turbine combined engine comprising a device for cooling superheated steam and driving the superheated steam with the output.

In an all-blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., water and nucleus contain low-temperature combustion gas containing harmful substances. An all-blade steam gas turbine combined engine, wherein steam is agglomerated into hail and water droplets.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C., low-temperature combustion gas containing coal ash and harmful substances is removed. An all-blade steam gas turbine combined engine wherein water and steam are aggregated into nuclei to form hail and water droplets.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with a blade (81), water or steam is aggregated by using low-temperature combustion gas containing harmful substances as a nucleus to produce hail, water droplets, etc. An all-blade steam gas turbine combined engine characterized by the following.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with a bucket (81), water and steam are aggregated using a low-temperature combustion gas containing coal ash and harmful substances as a core. An all-blade steam gas turbine combined engine characterized by hail and water droplets.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. Blade gas turbine driven by high-temperature water (5a) or the like, characterized in that water and steam are agglomerated into hail and water droplets using low-temperature combustion gas containing harmful substances as nuclei. Turbine united engine.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. A rotor blade steam gas turbine driven by high-temperature water (5a) or the like, wherein water and steam are agglomerated into a hail and water droplets by using low-temperature combustion gas containing coal ash and harmful substances as a core. Combined moving blade steam gas turbine engine.

A low-temperature combustion gas containing harmful substances in a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C. All rotor blades are characterized by aggregating water and water vapor on the core and separating them as hail and water droplets, discharging into separated water containing substances that promote the synthesis and dissolution of harmful substances, and approaching harmlessly to release. Steam gas turbine combined engine.

Low-temperature combustion containing harmful substances in a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C. It is characterized by aggregating water and water vapor with gas as the core and separating it as hail and water droplets, discharging the separated harmful substances into water containing the substance that promotes the synthetic dissolution, and releasing it close to harmless. All blade steam gas turbine combined engine.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a moving blade (81), water or water vapor is aggregated into a hail or water droplets using a low-temperature combustion gas containing a harmful substance as a core. All-blade steam gas turbine combined engine.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with a bucket (81), water or steam is agglomerated using low-temperature combustion gas containing coal ash or harmful substances as a nucleus to produce hail or water droplets. All-blade steam gas turbine combined engine characterized by the following.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine characterized in that water and steam are aggregated into hail and water droplets by using a low-temperature combustion gas containing a harmful substance as a nucleus in the all-blade gas turbine driven by the above method.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., in which a low-temperature combustion gas containing coal ash and harmful substances is used as a nucleus to aggregate water and steam to form hail and water droplets. Coalition organization.

In an all-blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., water and nucleus contain low-temperature combustion gas containing harmful substances. An all-blade steam gas turbine characterized in that steam is agglomerated and separated as hail or water droplets, and the separated harmful substances are discharged into water containing a substance that promotes the synthetic dissolution, and discharged in a non-hazardous manner. Coalition organization.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., water is cooled by using low-temperature combustion gas containing harmful substances as a nucleus. Rotor blade steam gas turbine combined, characterized in that water and water vapor are coagulated and separated as hail and water droplets, discharged into water containing the separated harmful substances and substances that promote dissolution, and approached harmlessly organ.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with a blade (81), water or steam is aggregated by using low-temperature combustion gas containing harmful substances as a nucleus to produce hail, water droplets, etc. An all-blade steam gas turbine combined engine, which discharges into water containing a substance that promotes the synthesis and dissolution of harmful substances that have been separated, and discharges it harmlessly.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade steam gas turbine that is driven by high-temperature water (5a) having a supercritical pressure or the like equipped with a bucket (81), water or steam is aggregated with a low-temperature combustion gas containing a harmful substance as a nucleus to produce hail or water droplets. An all-blade steam gas turbine combined engine, wherein harmful substances that have been separated and separated are discharged into water containing the substance that promotes the synthesis and dissolution, and discharged in a harmless manner.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In a full-blade gas turbine driven by high-temperature water (5a) or the like, low-temperature combustion gas containing harmful substances is used as a nucleus to separate water and water vapor to separate them as hail and water droplets. An all-blade steam gas turbine combined engine, which discharges into water containing a substance that promotes dissolution and discharges it harmlessly.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, low-temperature combustion gas containing harmful substances is used as a nucleus to aggregate water and water vapor to separate them as hail and water droplets. An all-blade steam gas turbine combined engine, which discharges into water containing a substance that promotes synthetic dissolution and releases it harmlessly.

A low-temperature combustion gas containing harmful substances in a full-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure 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, comprising: a device for aggregating water and water vapor with a nucleus as a core, separating the water and water vapor as hail, water droplets, and the like, and driving the device with the output.

Low-temperature combustion containing harmful substances in a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetically heated turbine blade (81) that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine, comprising: a device that drives water and steam by aggregating water and steam with gas as a nucleus and separating the water and steam into the hail and water droplets.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a moving blade (81), water and steam are aggregated by using low-temperature combustion gas containing harmful substances as a nucleus and separated as hail or water droplets, and separated. An all-blade steam gas turbine combined engine, characterized in that it is discharged into water containing a substance that promotes the dissolution and synthesis of harmful substances, and is discharged harmlessly.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with a bucket (81), water and steam are aggregated using a low-temperature combustion gas containing a harmful substance as a nucleus and separated as hail or water droplets, An all-blade steam gas turbine combined engine, wherein separated harmful substances are discharged into water containing the substance that promotes the synthetic dissolution, and discharged in a harmless manner.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by the above method, water and steam are agglomerated by using low-temperature combustion gas containing harmful substances as a nucleus and separated as hail and water droplets, and the separated harmful substances are substances that promote the synthetic dissolution. An all-blade steam gas turbine combined engine, which discharges water containing water and releases it harmlessly.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., the low-temperature combustion gas containing harmful substances is used as a nucleus to separate water and steam to separate them as hail and water droplets, and to promote the synthetic dissolution of the separated harmful substances. An all-blade steam gas turbine combined engine, which discharges into water containing substances and releases it harmlessly.

In an all-blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., water and nucleus contain low-temperature combustion gas containing harmful substances An all-blade steam gas turbine combined engine, comprising: a device for aggregating water vapor to separate it as hail, water droplets, or the like, and driving with the output.

In a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), which brings the combustion gas exhaust temperature close to -273 ° C., water is cooled by using low-temperature combustion gas containing harmful substances as a core. An all-blade steam gas turbine combined engine, comprising: a device for aggregating water and water vapor to separate as hail, water droplets, and the like, and driving with the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with a blade (81), water or steam is aggregated by using low-temperature combustion gas containing harmful substances as a nucleus to produce hail, water droplets, etc. An all-blade steam gas turbine combined engine, comprising: a device driven by the output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade steam gas turbine that is driven by high-temperature water (5a) having a supercritical pressure or the like equipped with a bucket (81), water or steam is aggregated with a low-temperature combustion gas containing a harmful substance as a nucleus to produce hail or water droplets. An all-blade steam gas turbine combined engine, comprising a device that is separated as such and driven by the output.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In the all-blade gas turbine driven by high-temperature water (5a) or the like, there is provided a device that separates water and water vapor by using low-temperature combustion gas containing harmful substances as a nucleus to separate as hail and water droplets, and drives with the output. An all-bladed steam gas turbine combined engine characterized by the following.

A supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) by combining an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio to bring the combustion gas exhaust temperature close to -273 ° C. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, water and water vapor are aggregated with a low-temperature combustion gas containing a harmful substance as a nucleus and separated as hail or water droplets. An all-blade steam gas turbine combined engine, comprising:

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In an all-blade gas turbine driven by high-temperature water (5a) or the like having a moving blade (81), water or water vapor is aggregated by using low-temperature combustion gas containing harmful substances as a nucleus and separated as hail or water droplets. An all-blade steam gas turbine combined engine comprising a device driven by an output.

An outer shaft device and an inner shaft device that rotate in opposite directions by a water pump and a contra-rotating magnetic friction power transmission device (14a) that bring the combustion gas exhaust temperature close to -273 ° C. are connected at an optimal rotation ratio, and an electromagnetic heating turbine is used. In a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with a bucket (81), water and steam are aggregated using a low-temperature combustion gas containing a harmful substance as a nucleus and separated as hail or water droplets, An all-blade steam gas turbine combined engine comprising a device driven by the output.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. And the like, characterized in that there is provided a device that is driven by the output by separating water and steam by using low-temperature combustion gas containing harmful substances as a nucleus to separate water and steam as hail and water droplets. All-blade steam gas turbine combined engine.

The high temperature water (5a) having an electromagnetically heated turbine blade (81) with an outer shaft device and an inner shaft device rotating in opposite directions by a power generator, which brings the combustion gas exhaust temperature close to -273 ° C. ), Etc., characterized in that a device is provided which is driven by the output by separating water and steam by using low-temperature combustion gas containing harmful substances as a nucleus to separate water and steam as hail and water droplets. All-blade steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). The rotor blade steam is characterized in that the inner shaft device of the rotor blade gas turbine driven by high-temperature water (5a) or the like is hollow, and the forward air is sucked and injected using the principle of spraying (91). Gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). The inner shaft device of a full blade steam gas turbine driven by high-temperature water (5a) or the like is hollow, and suctions and injects forward air using the principle of spraying (91). Steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). The inner shaft device of a rotor blade steam turbine driven by high-temperature water (5a) or the like is hollow, and suctions and injects forward air using the principle of spraying (91). Gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). An all-blade steam gas turbine combined engine, wherein a combustion gas outlet (88) is provided at a combustor / heat exchanger outlet of an all-blade gas turbine driven by high-temperature water (5a) or the like.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) provided at an outlet of a combustor / heat exchanger of an all-blade steam gas turbine driven by high-temperature water (5a) or the like. .

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). An all-blade steam gas turbine combined engine, wherein a combustion gas outlet (88) is provided at a combustor / heat exchanger outlet of an all-blade steam turbine driven by high-temperature water (5a) or the like.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at an outlet of a combustor / heat exchanger of an all-blade gas turbine driven by high-temperature water (5a) or the like to drive a micro gas turbine. Wing steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at a combustor / heat exchanger outlet of a full-blade steam gas turbine driven by high-temperature water (5a) or the like to drive a micro gas turbine. Combined moving blade steam gas turbine engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade gas turbine driven by high-temperature water (5a) or the like, high-temperature water is injected from one or more special devices (92a) using the principle of spraying (91a), and the air in front is blown. An all-blade steam gas turbine combined engine characterized by suction and injection.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, high-temperature water is injected from one or more special devices (92a) using the principle of spraying (91a) to produce air in front of the turbine. All-blade steam gas turbine combined engine that sucks and injects air.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor and heat exchanger of a full-blade steam gas turbine driven by high-temperature water (5a), etc. An all-blade steam gas turbine combined engine, wherein combustion gas is injected from a plurality of special devices (92b), and air in front is sucked and injected.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor / heat exchanger of a full-blade steam turbine driven by high-temperature water (5a) or the like. A combustion apparatus for injecting combustion gas from a special device (92b), and sucking and injecting air in front of the combustion device for injection.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade gas turbine driven by high-temperature water (5a) or the like, high-temperature water is injected from one or more water injection devices (93a) using the principle of spraying (91c), and the All-blade steam gas turbine combined engine that sucks and injects air.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, high-temperature water is injected from one or more water injection devices (93a) using the principle of spraying (91c), An all-blade steam gas turbine combined engine that sucks and injects water.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of a full-blade steam gas turbine driven by high-temperature water (5a), etc. An all-blade steam gas turbine combined engine, wherein combustion gas is injected from a plurality of water injection devices (93b), and water in front is suctioned and injected.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor / heat exchanger of a full-blade steam turbine driven by high-temperature water (5a) or the like. A combustion gas is injected from a water injection device (93b), and water is sucked and injected in front of the combustion gas.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor and heat exchanger of a full-blade steam gas turbine driven by high-temperature water (5a) or the like using the principle of spraying (91c) (91d). And a plurality of water injection devices (93a) and (93b) for injecting high-temperature water and combustion gas from each of the plurality of water injection devices, and sucking and injecting water in front thereof for injection.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of a full-blade steam turbine driven by high-temperature water (5a) or the like, using the principle of atomization (91c) (91d). An all-blade steam gas turbine combined engine wherein high-temperature water and combustion gas are injected from each of one or more water injection devices (93a) and (93b), and water in front is sucked and injected.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor and heat exchanger of a full-blade steam gas turbine driven by high-temperature water (5a) or the like, and uses the principle of spraying (91a) (91b). And a high-pressure water and combustion gas are injected from one or more special devices (92a) and (92b), and the air in front of the device is sucked and injected.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor / heat exchanger of a full-blade steam turbine driven by high-temperature water (5a) or the like, using the principle of spraying (91a) (91b). An all-blade steam gas turbine combined engine wherein high-temperature water and combustion gas are injected from one or more special devices (92a) and (92b), and front air is sucked and injected.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade gas turbine driven by high-temperature water (5a) or the like, high-temperature water is injected from one or more special devices (92a) using the principle of spraying (91a), and the air in front is blown. An all-blade steam gas turbine combined engine, comprising: a device for sucking, propelling and injecting, and driving with the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, high-temperature water is injected from one or more special devices (92a) using the principle of spraying (91a) to produce air in front of the turbine. Characterized in that it is provided with a device for sucking and injecting and injecting and for driving the steam turbine by the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor and heat exchanger of a full-blade steam gas turbine driven by high-temperature water (5a), etc. An all-blade steam gas turbine combined engine, comprising: a device for injecting combustion gas from a plurality of special devices (92b), sucking forward air for injection and propulsion, and driven by the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor / heat exchanger of a full-blade steam turbine driven by high-temperature water (5a) or the like. A combined device for injecting combustion gas from a special device (92b), sucking forward air to inject and propell, and driving with the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade gas turbine driven by high-temperature water (5a) or the like, high-temperature water is injected from one or more water injection devices (93a) using the principle of spraying (91c), and the Characterized in that it is provided with a device for sucking and injecting and injecting and for driving the steam turbine by the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). In a full-blade steam gas turbine driven by high-temperature water (5a) or the like, high-temperature water is injected from one or more water injection devices (93a) using the principle of spraying (91c), An all-blade steam gas turbine combined engine, comprising: a device for sucking water, injecting and propelling the water, and driving with the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of a full-blade steam gas turbine driven by high-temperature water (5a), etc. An all-blade steam gas turbine combined engine, comprising: a device that injects combustion gas from a plurality of water injection devices (93b), suctions forward water, propulses the water, and drives with the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor / heat exchanger of a full-blade steam turbine driven by high-temperature water (5a) or the like. A combined turbine and steam turbine in which a combustion gas is injected from a water injection device (93b), water is sucked in front of the device, the injection is propelled, and the device is driven by the output.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor and heat exchanger of a full-blade steam gas turbine driven by high-temperature water (5a) or the like using the principle of spraying (91c) (91d). And at least one of a plurality of water injection devices (93a) and (93b) for injecting high-temperature water and combustion gas, sucking forward water for injection and propulsion, and being driven by the output. All-blade steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of a full-blade steam turbine driven by high-temperature water (5a) or the like, using the principle of atomization (91c) (91d). High-temperature water and combustion gas are injected from each of the one or more water injection devices (93a) and (93b), water in front is sucked and injected, and the device is driven by the output. All blade steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor and heat exchanger of a full-blade steam gas turbine driven by high-temperature water (5a) or the like, and uses the principle of spraying (91a) (91b). And a device for injecting high-temperature water and combustion gas from at least one of each of the plurality of special devices (92a) and (92b), sucking forward air to propulse the jet, and driving by the output. All blade steam gas turbine combined engine.

A supercritical pressure having an electromagnetically heated turbine blade (81) in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimal rotation ratio by a water pump and a contra-rotating magnetic friction power transmission device (14a). A combustion gas outlet (88) is provided at the outlet of a combustor / heat exchanger of a full-blade steam turbine driven by high-temperature water (5a) or the like, using the principle of spraying (91a) (91b). High-temperature water and combustion gas are injected from each of the one or more special devices (92a) and (92b), the air in front is sucked and injected, and the device is driven by the output. Combined moving blade steam gas turbine engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), etc., the inner shaft device of a full-blade gas turbine driven by high-temperature water (5a) or the like driven by supercritical pressure or the like is made hollow, and the air in front is suction-injected using the principle of spraying (91). An all-blade steam gas turbine combined engine, characterized in that:

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), etc., wherein the inner shaft device of the full-blade steam gas turbine driven by the method described above is hollow, and the forward air is sucked and injected using the principle of spraying (91). .

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combined rotor blade steam gas turbine engine, characterized in that the inner shaft device of the rotor blade steam turbine driven by 5a) or the like is hollow, and the forward air is sucked and injected using the principle of spraying (91).

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. An all-blade steam gas turbine combined engine, wherein a combustion gas outlet (88) is provided at a combustor / heat exchanger outlet of the all-blade gas turbine driven by 5a) or the like.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) An all-blade steam gas turbine combined engine characterized in that a combustion gas outlet (88) is provided at an outlet of a combustor / heat exchanger of the all-blade steam gas turbine driven by 5a) or the like.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. An all-blade steam gas turbine combined engine characterized in that a combustion gas outlet (88) is provided at an outlet of a combustor / heat exchanger of the all-blade steam turbine driven by 5a) or the like.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combustion gas outlet (88) is provided at the outlet of a combustor / heat exchanger of a full blade gas turbine driven by 5a) or the like to drive a micro gas turbine, and the combined combination of all blade steam gas turbines. organ.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combustion gas outlet (88) is provided at an outlet of a combustor / heat exchanger of a full blade steam gas turbine driven by 5a) to drive a micro gas turbine. Coalition organization.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. In the all-blade gas turbine driven by 5a) or the like, high-temperature water is injected from one or more special devices (92a) using the principle of spraying (91a), and air in front is sucked and injected. An all-blade steam gas turbine combined engine, characterized in that:

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) In a full-blade steam gas turbine driven by, for example, high-temperature water is injected from one or more special devices (92a) using the principle of spraying (91a), and the air in front is sucked and injected. All-blade steam gas turbine combined engine characterized by the following.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) The combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the all-blade steam gas turbine driven by the method described above, and one or more special devices ( 92b) An all-blade steam gas turbine combined engine, which injects combustion gas from above and suctions and injects air in front.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), a combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the full-blade steam turbine, and one or more special devices (92b) are used by using the principle of spraying (91b). ), Wherein the combustion gas is injected more, and the air in front is suctioned and injected.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. In the all-blade gas turbine driven by 5a) or the like, high-temperature water is injected from one or more water injection devices (93a) using the principle of spraying (91c), and water is sucked and injected in front. All-blade steam gas turbine combined engine characterized by the following.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) In a full-blade steam gas turbine driven by, for example, high-temperature water is injected from one or more water injection devices (93a) using the principle of spraying (91c), and water in front is sucked. An all-blade steam gas turbine combined engine characterized by injecting.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the full-blade steam gas turbine driven by the method described above, and one or more water injection devices are provided by utilizing the principle of spraying (91d). (93b) An all-blade steam gas turbine combined engine, which injects combustion gas from above and suctions and injects water ahead.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the all-blade steam turbine driven by 5a) or the like, and one or more water injection devices (91d) are used by using the principle of spraying (91d). 93b) Combined all-blade steam gas turbine engine that injects combustion gas from above and suctions and injects water ahead.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the all-blade steam gas turbine driven by the method described above, and one or more of each of the combustion gas outlets (91c) and (91d) is used by using the spraying principle (91c) (91d). An all-blade steam gas turbine combined engine wherein high-temperature water and combustion gas are injected from a plurality of water injection devices (93a) and (93b), and water in front is sucked and injected.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), a combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the all-blade steam turbine, and at least one of each of the plurality of the turbines is sprayed using the principle of spraying (91c) (91d). A high-pressure water and combustion gas are injected from the water injection devices (93a) and (93b), and water in front thereof is suctioned and injected.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the full-blade steam gas turbine driven by the method described above, and one or more of each of the combustion gas outlets (91a) and (91b) is used by using the spraying principle (91a) (91b). An all-blade steam gas turbine combined engine wherein high-temperature water and combustion gas are injected from a plurality of special devices (92a) and (92b), and front air is sucked and injected.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), a combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the full-blade steam turbine, and at least one of each of the plurality is provided by utilizing the principle of spraying (91a) (91b). A high-pressure water and combustion gas is injected from the special devices (92a) and (92b), and air is sucked and injected in front of the high-speed water and the combustion gas.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) In a full-blade gas turbine driven by, for example, high-temperature water is injected from one or more special devices (92a) using the principle of atomization (91a), and air is sucked in front to promote injection. An all-blade steam gas turbine combined engine comprising a device driven by the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) In a full-blade steam gas turbine driven by, for example, high-temperature water is injected from one or more special devices (92a) using the principle of spraying (91a), and the air in front is sucked and injected. An all-blade steam gas turbine combined engine comprising a device for propulsion and driving at the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) The combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the all-blade steam gas turbine driven by the method described above, and one or more special devices ( 92b) An all-blade steam gas turbine combined engine, comprising: a device for injecting combustion gas from above, sucking forward air for injection and propulsion, and driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), a combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the full-blade steam turbine, and one or more special devices (92b) are used by using the principle of spraying (91b). A) a combined rotor blade steam gas turbine engine comprising: a device for injecting combustion gas, sucking forward air for injection and propulsion, and driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. In the all-blade gas turbine driven by 5a) or the like, high-temperature water is injected from one or more water injection devices (93a) using the principle of spraying (91c), and water is sucked and injected in front. An all-blade steam gas turbine combined engine comprising a device for propulsion and driving at the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) In a full-blade steam gas turbine driven by, for example, high-temperature water is injected from one or more water injection devices (93a) using the principle of spraying (91c), and water in front is sucked. An all-blade steam gas turbine combined engine, comprising: a device for injecting and propelling and driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the full-blade steam gas turbine driven by the method described above, and one or more water injection devices are provided by utilizing the principle of spraying (91d). (93b) An all-blade steam gas turbine combined engine, comprising: a device for injecting combustion gas from there, sucking water in front of it, and propelling it, and driving with the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the all-blade steam turbine driven by 5a) or the like, and one or more water injection devices (91d) are used by using the principle of spraying (91d). 93b) An all-blade steam gas turbine combined engine, characterized by comprising a device for injecting combustion gas from above, sucking forward water for injection and propulsion, and driven by the output.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the all-blade steam gas turbine driven by the method described above, and one or more of each of the combustion gas outlets (91c) and (91d) is used by using the spraying principle (91c) (91d). A full-blade steam comprising a device for injecting high-temperature water and combustion gas from a plurality of water injection devices (93a) and (93b), sucking forward water for injection and propulsion, and driving with the output. Gas turbine combined engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), a combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the all-blade steam turbine, and at least one of each of the plurality of the turbines is sprayed using the principle of spraying (91c) (91d). A high-pressure water and combustion gas is injected from water injection devices (93a) and (93b), suction water in front is sucked and injected, and the device is driven by the output. Turbine united engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a) A combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the full-blade steam gas turbine driven by the method described above, and one or more of each of the combustion gas outlets (91a) and (91b) is used by using the spraying principle (91a) (91b). A full-blade steam gas comprising a device for injecting high-temperature water and combustion gas from a plurality of special devices (92a) and (92b), sucking forward air to inject and propulse, and driving with the output. Turbine united engine.

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 a contra-rotating magnetic friction power transmission device (14a), and high-temperature water (81) having an electromagnetically heated turbine blade (81) is connected. 5a), a combustion gas outlet (88) is provided at the outlet of the combustor / heat exchanger of the full-blade steam turbine, and at least one of each of the plurality is provided by utilizing the principle of spraying (91a) (91b). All-blade steam gas turbine, characterized by comprising a device for injecting high-temperature water and combustion gas from special devices (92a) and (92b), sucking forward air for injection and propulsion, and driven by the output. Coalition organization.

In a combustor / heat exchanger (4) of a full-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), one or more of the combustors and the heat exchanger (91a) are utilized by using the principle of spraying (91a). A high-speed water jet from a special device (92a), and suction and jet of air in front of the special device (92a).

In a combustor / heat exchanger (4) of an all-blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), one or more of the combustors and the heat exchanger (91c) are used by using the principle of spraying (91c). A high-pressure water jet from a water jet device (93a), and suction and jet of water in front of the water jet device (93a).

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), one or more of the combustors and heat exchangers use the principle of spraying (91a). An all-blade steam gas turbine combined engine, which injects high-temperature water from a plurality of special devices (92a) and sucks and injects air in front.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), one or more of the combustors and the heat exchanger (91c) are used by using the principle of spraying (91c). An all-blade steam gas turbine combined engine, wherein high-temperature water is injected from a plurality of water injection devices (93a), and front water is suctioned and injected.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), a combustion gas outlet (88) is provided at a combustion gas outlet. Injecting high-temperature water and combustion gas from each of one or more special devices (92a) (92b) using the principle of spraying (91a) (91b) and sucking and injecting air in front An all-blade steam gas turbine combined engine characterized by the following.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), a combustion gas outlet (88) is provided at a combustion gas outlet. High-temperature water and combustion gas are injected from one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d), and the water in front is sucked and injected. An all-blade steam gas turbine combined engine, characterized in that:

A combustion gas outlet (88) is provided at a combustion gas outlet in a combustor / heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). By using the principle of spraying (91a) (91b), one or more special devices (92a) (92b) inject high-temperature water and combustion gas, and inhale and inject air in front. All-blade steam gas turbine combined engine.

A combustion gas outlet (88) is provided at a combustion gas outlet in a combustor / heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). Injecting high-temperature water and combustion gas from each of one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d), and sucking and injecting water in front. An all-blade steam gas turbine combined engine characterized by the following.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), a combustion gas outlet (88) is provided at a combustion gas outlet. A combination of all bladed steam gas turbines, wherein combustion gas is injected from one or more special devices (92b) utilizing the principle of spraying (91b), and air is sucked and injected forward. organ.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), a combustion gas outlet (88) is provided at a combustion gas outlet. An all-blade steam gas turbine, wherein combustion gas is injected from one or more water injection devices (93b) by utilizing the principle of spraying (91d), and water is sucked and injected forward. Coalition organization.

A combustion gas outlet (88) is provided at a combustion gas outlet in a combustor / heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). Wherein the combustion gas is injected from one or more special devices (92b) using the principle of spraying (91b), and the air in front is suctioned and injected, and is combined with an all-blade steam gas turbine combined engine. .

A combustion gas outlet (88) is provided at a combustion gas outlet in a combustor / heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). A combustion gas is injected from one or more water injection devices (93b) using the principle of spraying (91d), and water is sucked and injected in front of the combustion gas turbine to combine the blades. organ.

In a combustor / heat exchanger (4) of a full-blade gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetic heating turbine blade (81), one or more special devices utilizing the principle of atomization (92a) An all-blade steam gas turbine combined engine, comprising: a device for injecting higher-temperature water, sucking forward air for jet propulsion, and driven by the output.

In a combustor / heat exchanger (4) of an all-blade gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), one or more water injections are made using the principle of spraying. An all-blade steam gas turbine combined engine, comprising: a device that injects high-temperature water from a device (93a), suctions water in front of the device, propulses the water, and is driven by the output.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like equipped with an electromagnetically heated turbine blade (81), one or more of the combustors and heat exchangers use the principle of spraying (91a). An all-blade steam gas turbine combined engine, comprising: a device for injecting high-temperature water from a plurality of special devices (92a), sucking forward air to eject and propell, and driven by the output.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), one or more of the combustors and the heat exchanger (91c) are used by using the principle of spraying (91c). An all-blade steam gas turbine combined engine, comprising: a device for injecting high-temperature water from a plurality of water injection devices (93a), sucking forward water for jet propulsion, and driven by the output.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), a combustion gas outlet (88) is provided at a combustion gas outlet. High-temperature water and combustion gas are injected from each of one or more special devices (92a) and (92b) utilizing the principle of spraying (91a) and (91b), and the air in front is sucked and propelled. , An all-blade steam gas turbine combined engine comprising a device driven by the output.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), a combustion gas outlet (88) is provided at a combustion gas outlet. High-temperature water and combustion gas are injected from one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d), and the water in front is sucked to promote injection. An all-blade steam gas turbine combined engine comprising a device driven by the output.

A combustion gas outlet (88) is provided at a combustion gas outlet in a combustor / heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). By using the principle of spraying (91a) (91b), high-temperature water and combustion gas are injected from each of one or more special devices (92a) (92b), and the air in front is sucked and injected and propelled. An all-blade steam gas turbine combined engine comprising a device driven by the output.

A combustion gas outlet (88) is provided at a combustion gas outlet in a combustor / heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). Then, high-temperature 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 the water in front is sucked to promote injection. , An all-blade steam gas turbine combined engine comprising a device driven by the output.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), a combustion gas outlet (88) is provided at a combustion gas outlet. A device that injects combustion gas from one or more special devices (92b) utilizing the principle of spraying (91b), sucks forward air, propulses the injection, and drives with the output. An all-blade steam gas turbine combined engine characterized by the following.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having an electromagnetically heated turbine blade (81), a combustion gas outlet (88) is provided at a combustion gas outlet. And a device for injecting combustion gas from one or more water injection devices (93b) by utilizing the principle of spraying (91d), sucking forward water for injection and propulsion, and driving with the output. An all-blade steam gas turbine combined engine, characterized in that:

A combustion gas outlet (88) is provided at a combustion gas outlet in a combustor / heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). And a device for injecting combustion gas from one or more special devices (92b) utilizing the principle of spraying (91b), sucking forward air to inject and propulse, and driving with the output. All-blade steam gas turbine combined engine.

A combustion gas outlet (88) is provided at a combustion gas outlet in a combustor / heat exchanger (4) of a full blade steam turbine driven by high-temperature water (5a) or the like having an electromagnetic heating turbine blade (81). And a device for injecting combustion gas from one or more water injection devices (93b) using the principle of spraying (91d), sucking forward water to propulse the injection, and driving with the output. An all-blade steam gas turbine combined engine characterized by the following.

An all-blade steam gas turbine combined engine comprising an electromagnetic heating nozzle (83) and a full-blade steam turbine driven by high-temperature water (5a) or the like having the electromagnetically heated turbine blade (81). .

An all-blade steam gas turbine combined with an all-blade steam nozzle (83), which is provided with an electromagnetic heating nozzle (83) to be driven by high-temperature water (5a) or the like having the above-mentioned electromagnetically heated turbine blade (81). organ.

An all-blade steam gas turbine combined engine comprising an electromagnetic heating nozzle (83) and a full-blade gas turbine driven by high-temperature water (5a) or the like having the electromagnetically heated turbine blade (81). .

A high-temperature water injection nozzle (59a) for electromagnetic heating and high-temperature by a high-temperature heating means (101) is provided on a full-blade steam turbine driven by high-temperature water (5a) or the like having the electromagnetic heating turbine blade (81). An all-blade steam gas turbine combined engine characterized by the following.

A high-temperature water jet nozzle (59a) for electromagnetic heating and high temperature by a high-temperature heating means (101) is provided for a full-blade steam gas turbine driven by high-temperature water (5a) or the like having the electromagnetic heating turbine blade (81). An all-blade steam gas turbine combined engine, characterized in that:

A high-temperature water injection nozzle (59a) for electromagnetic heating and high-temperature by a high-temperature heating means (101) is provided in a full-blade gas turbine driven by high-temperature water (5a) or the like having the electromagnetic heating turbine blade (81). An all-blade steam gas turbine combined engine characterized by the following.

Utilizing the principle of spraying (91a) in the combustor and heat exchanger (4) of a full-blade gas turbine driven by high-temperature water (5a) with supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) And a high-speed water jet from one or more special devices (92a), and a suction and jet of air in front of the high-speed water jet.

Utilizing the principle of spraying (91c) in the combustor and heat exchanger (4) of an all-blade gas turbine driven by high-temperature water (5a) with supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81) A steam turbine combined engine for all blades, wherein high-temperature water is injected from one or more water injection devices (93a), and water in front is sucked and injected.

In a combustor / heat exchanger (4) of an all-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), the principle of spraying (91a) is described. An all-blade steam gas turbine combined engine, wherein high-temperature water is injected from one or more special devices (92a) and air in front is sucked and injected.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetic heating turbine blade (81), the principle of spraying (91c) is described. An all-blade steam gas turbine combined engine, wherein high-temperature water is injected from one or more water injection devices (93a), and water in front is suctioned and injected.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. An outlet (88) is provided, and high-temperature water and combustion gas are injected from each of one or more special devices (92a) (92b) using the principle of spraying (91a) (91b) to suck air in front. An all-blade steam gas turbine combined engine characterized by injection.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. An outlet (88) is provided, and high-temperature 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 of the water is injected. An all-blade steam gas turbine combined engine characterized by suction and injection.

In a combustor / heat exchanger (4) of a full-blade steam turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. (88), high-temperature water and combustion gas are injected from each of one or more special devices (92a) and (92b) using the principle of spraying (91a) (91b), and the air in front is sucked. An all-blade steam gas turbine combined engine characterized by injection.

In a combustor / heat exchanger (4) of a full-blade steam turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. (88), high-temperature water and combustion gas are injected from one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d), and water in front is sucked. An all-blade steam gas turbine combined engine characterized by injection.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. An outlet (88) is provided, in which combustion gas is injected from one or more special devices (92b) using the principle of spraying (91b), and air is sucked and injected in front of the device. Wing steam gas turbine combined engine.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. An outlet (88) is provided, and combustion gas is injected from one or more water injection devices (93b) using the principle of spraying (91d), and water is sucked and injected in front. Combined moving blade steam gas turbine engine.

In a combustor / heat exchanger (4) of a full-blade steam turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. (88) is provided, wherein the combustion gas is injected from one or more special devices (92b) using the principle of spraying (91b), and the front air is sucked and injected. Steam gas turbine combined engine.

In a combustor / heat exchanger (4) of a full-blade steam turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. (88) is provided, in which combustion gas is injected from one or more water injection devices (93b) using the principle of spraying (91d), and water is sucked and injected in front of the water injection device. Wing steam gas turbine combined engine.

In a combustor / heat exchanger (4) of an all-blade gas turbine driven by high-temperature water (5a) or the like having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), the principle of atomization is used. A combination of a plurality of special devices (92a) for injecting high-temperature water (5a), suction of forward air for injection and propulsion, and a device driven by the output; organ.

In a combustor / heat exchanger (4) of an all-blade gas turbine driven by high-temperature water (5a) or the like having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), the principle of atomization is used. All-blade steam gas turbine, characterized by comprising a device for injecting high-temperature water (5a) from a plurality of water injection devices (93a), sucking forward water for injection and propulsion, and driving with the output. Coalition organization.

In a combustor / heat exchanger (4) of an all-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), the principle of spraying (91a) is described. A high-pressure water (5a) jetted from one or more special devices (92a) using the device, and a device driven by the output by sucking the air in front and jetting and propelling the hot water (5a). Steam gas turbine combined engine.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure equipped with an electromagnetic heating turbine blade (81), the principle of spraying (91c) is described. A full-blade steam gas comprising a device for injecting high-temperature water from one or more water injection devices (93a), sucking forward water for jet propulsion, and driving with the output. Turbine united engine.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. An outlet (88) is provided, and high-temperature water and combustion gas are injected from each of one or more special devices (92a) (92b) using the principle of spraying (91a) (91b) to suck air in front. A combined turbine and steam turbine driven engine, comprising: a device for propelling and injecting and driving with the output.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. An outlet (88) is provided, and high-temperature 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 of the water is injected. An all-blade steam gas turbine combined engine, comprising: a device for sucking, propelling and injecting, and driving with the output.

In a combustor / heat exchanger (4) of a full-blade steam turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. (88), high-temperature water and combustion gas are injected from each of one or more special devices (92a) and (92b) using the principle of spraying (91a) (91b), and the air in front is sucked. A combined turbine and steam turbine engine having a device for propelling and injecting and driving with the output.

In a combustor / heat exchanger (4) of a full-blade steam turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. (88), high-temperature water and combustion gas are injected from one or more water injection devices (93a) and (93b) using the principle of spraying (91c) and (91d), and water in front is sucked. A combined turbine and steam turbine driven engine, comprising: a device for propelling and injecting and driving with the output.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. An outlet (88) is provided, and 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 injected for propulsion, and the output is driven. An all-blade steam gas turbine combined engine provided with a device.

In a combustor / heat exchanger (4) of a full-blade steam gas turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetic heating turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. An outlet (88) is provided, and combustion gas is injected from one or more water injection devices (93b) using the principle of spraying (91d), water in front is sucked, and injection is propelled, and the output is driven. An all-blade steam gas turbine combined engine, comprising:

In a combustor / heat exchanger (4) of a full-blade steam turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. (88), a device that injects combustion gas from one or more special devices (92b) by utilizing the principle of spraying (91b), sucks forward air to inject and propulse, and drives with the output. An all-blade steam gas turbine combined engine comprising:

In a combustor / heat exchanger (4) of a full-blade steam turbine driven by high-temperature water (5a) having supercritical pressure or the like equipped with an electromagnetically heated turbine blade (81), a combustion gas outlet is provided at a combustion gas outlet. (88) is provided, the combustion gas is injected from one or more water injection devices (93b) using the principle of spraying (91d), the water in front is sucked, the injection is propelled, and the output is driven. An all-blade steam gas turbine combined engine provided with a device.

A full-blade steam turbine driven by high-temperature water (5a) or the like having supercritical pressure or the like having the electromagnetic-heated turbine blade (81), further comprising an electromagnetic heating nozzle (83). Steam gas turbine combined engine.

A full-rotor blade gas turbine having an electromagnetic heating nozzle (83), the all-rotor blade gas turbine driven by high-temperature water (5a) or the like having a supercritical pressure or the like having the electromagnetic heating turbine blade (81). Steam gas turbine combined engine.

A high-temperature water injection nozzle (59a) with electromagnetic heating and high temperature is heated by a high-temperature heating means (101) to a full-blade steam turbine driven by high-temperature water (5a) or the like having supercritical pressure or the like having the electromagnetic heating turbine blade (81). ). A combined rotor blade steam gas turbine engine comprising:

A high-temperature water injection nozzle of electromagnetic heating and high temperature is heated by a high-temperature heating means (101) to a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure or the like equipped with the electromagnetic heating turbine blade (81). 59a) An all-blade steam gas turbine combined engine comprising:

A high-temperature water injection nozzle (59a) with electromagnetic heating and high temperature is heated by a high-temperature heating means (101) to a full-blade gas turbine driven by high-temperature water (5a) or the like having supercritical pressure or the like equipped with the electromagnetic heating turbine blade (81). ). A combined rotor blade steam gas turbine engine comprising:

A high-temperature water injection nozzle (101) having a high electric resistance and high electric resistance by a heating high-temperature means (101) is applied to a full-blade steam turbine driven by high-temperature water (5a) having a supercritical pressure or the like having the electromagnetic heating turbine blade (81). 59a) An all-blade steam gas turbine combined engine comprising:

A high-temperature water jet nozzle having high resistance and high electric resistance by a heating high-temperature means (101) is applied to a full-blade steam gas turbine driven by high-temperature water (5a) or the like having supercritical pressure or the like equipped with the electromagnetic heating turbine blade (81). An all-blade steam gas turbine combined engine comprising (59a).

A high-temperature water injection nozzle (81) having a high electric resistance and high electric resistance by a heating high-temperature means (101) is provided to a full-blade gas turbine driven by high-temperature water (5a) having a supercritical pressure or the like provided with the electromagnetic heating turbine blade (81). 59a) An all-blade steam gas turbine combined engine comprising:

The all-blade steam gas turbine combined engine, wherein the heating / high temperature means (101) is externally fitted to the high temperature water injection nozzle (59a).

The all-blade steam gas turbine combined engine, wherein the heating and high-temperature means (101) is externally fitted to the high-temperature water injection nozzle (59a) to heat to a high temperature.

The all-blade steam gas turbine combined engine, wherein the heating and high temperature means (101) is externally fitted to the high temperature water injection nozzle (59a) to make electromagnetic heating high temperature.

The all-blade steam gas turbine combined engine, wherein the heating / high temperature means (101) is externally fitted to the high-temperature water injection nozzle (59a) and heats to high temperature by electric resistance.

The all-blade steam gas turbine combined engine, wherein the high-temperature water injection nozzle (59a) is heated to a high temperature.

The all-blade steam gas turbine combined engine, wherein the high-temperature water injection nozzle (59a) is a barrel-shaped nozzle.

The high-temperature water injection nozzle (59a) is a barrel-shaped nozzle for heating to a high temperature.

The all-blade steam gas turbine combined engine, wherein the high-temperature water injection nozzle (59a) is a barrel-shaped divergent nozzle.

The high-temperature water injection nozzle (59a) is a barrel-shaped divergent nozzle for heating to a high temperature.

The high-temperature water injection nozzle (59a) is a barrel-shaped nozzle, and accelerates the high-temperature water (5a) like a bullet of a machine gun by vaporization and explosive force.

The high-temperature water injection nozzle (59a) is a barrel-shaped nozzle, and is heated to a high temperature to accelerate high-temperature water (5a) as a bullet of a machine gun by vaporization and explosive force. organ.

The high-temperature water injection nozzle (59a) is a barrel-shaped divergent nozzle for accelerating the high-temperature water (5a) as a bullet of a machine gun by vaporization and explosive force.

The all-blade steam gas turbine characterized in that the high-temperature water injection nozzle (59a) is a barrel-shaped divergent nozzle and is heated to a high temperature to accelerate high-temperature water (5a) by a vaporizing explosion force like a bullet of a machine gun. Coalition organization.

The all-blade steam gas turbine combined engine, wherein the vaporizing latent heat recovery device (66a) is configured substantially in the same manner as a condenser and uses feed water (3) as cooling water.

The all-blade steam is characterized in that the vaporizing latent heat recovery device (66a) is configured substantially in the same manner as a condenser and uses a water supply (3) as cooling water at a saturation temperature of about 100 ° C. by an air extractor. Gas turbine combined engine.

The all-blade steam is characterized in that the vaporizing latent heat recovery device (66a) is configured substantially in the same manner as a condenser and uses a feed water (3) as cooling water at a saturation temperature of about 80 ° C. by an air extractor. Gas turbine combined engine.

The all-blade steam is characterized in that the vaporizing latent heat recovery device (66a) is configured substantially in the same manner as a condenser and uses a water supply (3) as cooling water at a saturation temperature of about 60 ° C. by an air extractor. Gas turbine combined engine.

The all-blade steam gas turbine is characterized in that the vaporizing latent heat recovery device (66a) is configured substantially in the same manner as a condenser and uses feed water (3) for cooling water to eliminate an increase in seawater temperature and the like. Coalition organization.

The all-blade steam gas turbine combined engine, characterized in that the vaporizing latent heat recovery device (66a) is configured substantially in the same manner as a condenser and uses cooling water to supply water (3) to prevent global warming. .

The vaporizing latent heat recovery device (66a) is configured in substantially the same manner as the condenser, recovers heat using cooling water (3), and supplies the cooling water to the combustor / heat exchanger (4). All-blade steam gas turbine combined engine.

The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using the water supply (3) to the cooling water, and supplies it to the combustor / heat exchanger (4) together with the condensed water. All-blade steam gas turbine combined engine characterized by the following.

The vaporizing latent heat recovery device (66a) is configured in substantially the same manner as the condenser, recovers heat using the supply water (3) for the cooling water, and supplies it to the combustor / heat exchanger (4) together with the condensed water. An all-blade steam gas turbine combined engine characterized by reducing fuel combustion mass.

The vaporizing latent heat recovery device (66a) is constructed in substantially the same manner as the condenser, recovers heat using the water supply (3) as the cooling water, and, together with condensed water having a saturation temperature of around 100 ° C., as well as a combustor / heat exchanger. (4) An all-blade steam gas turbine combined engine, which is supplied to (4).

The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using the water supply (3) as the cooling water, and, together with the condensed water having a saturation temperature of about 80 ° C., as well as a combustor / heat exchanger. (4) An all-blade steam gas turbine combined engine, which is supplied to (4).

The vaporizing latent heat recovery device (66a) is constructed in substantially the same manner as the condenser, recovers heat using the water supply (3) as the cooling water, and, together with condensed water having a saturation temperature of around 60 ° C., as well as a combustor / heat exchanger. (4) An all-blade steam gas turbine combined engine, which is supplied to (4).

The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using the water supply (3) as cooling water, and collects heat with condensed water having a saturation temperature of about 100 ° C. as a combustor / heat exchanger ( 4) A combined turbine and steam gas turbine engine characterized in that it is supplied to the above (4) and stored as hot heat.

The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using the water supply (3) as cooling water, and collects heat with condensed water having a saturation temperature of about 80 ° C. as a combustor / heat exchanger ( 4) A combined turbine and steam gas turbine engine characterized in that it is supplied to the above (4) and stored as hot heat.

The vaporizing latent heat recovery device (66a) is configured in substantially the same manner as the condenser, recovers heat using the supply water (3) as the cooling water, and, together with the condensed water having a saturation temperature of about 60 ° C., also serves as a combustor / heat exchanger ( 4) A combined turbine and steam gas turbine engine characterized in that it is supplied to the above (4) and stored as hot heat.

The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using the water supply (3) as cooling water, and collects heat with condensed water having a saturation temperature of about 100 ° C. as a combustor / heat exchanger ( (4) A combined bladed steam gas turbine engine, characterized in that it is supplied to a customer, stored as heat, and supplied to a customer.

The vaporizing latent heat recovery unit (66a) is configured in substantially the same manner as the condenser, recovers heat using the water supply (3) as cooling water, and collects heat with condensed water having a saturation temperature of about 80 ° C. as a combustor / heat exchanger ( (4) A combined bladed steam gas turbine engine, characterized in that it is supplied to a customer, stored as heat, and supplied to a customer.

The vaporizing latent heat recovery device (66a) is configured in substantially the same manner as the condenser, recovers heat using the supply water (3) as the cooling water, and, together with the condensed water having a saturation temperature of about 60 ° C., also serves as a combustor / heat exchanger ( (4) A combined bladed steam gas turbine engine, characterized in that it is supplied to a customer, stored as heat, and supplied to a customer.

Various magnetized friction wheels and various magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the upstream side in the rotation direction, and are used as appropriate and interchangeable. And an all-blade steam gas turbine united engine wherein the waterway is connected to a water injection means (56).

Various magnetized friction wheels and various magnetized friction wheels of the water feed pump and contra-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the upstream side in the rotation direction, and are appropriately interchangeable with each other. An all-blade steam gas turbine combined engine, wherein the combined use of a water channel and a water injection means (56) is used.

Various magnetized friction wheels and various magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the downstream side in the rotation direction, and are used as appropriate. And an all-blade steam gas turbine united engine wherein the waterway is connected to a water injection means (56).

Various magnetized friction wheels and various magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with bar magnets (33) on the downstream side in the rotation direction, and are appropriately interchangeable with each other. An all-blade steam gas turbine combined engine, wherein the combined use of a water channel and a water injection means (56) is used.

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with electromagnets (34) on the upstream side and the downstream side in the rotation direction, respectively. An all-blade steam gas turbine combined engine characterized in that it is used interchangeably with (i) and the waterway is connected to water injection means (56).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with bar magnets (33) on the upstream and downstream sides in the rotational direction, respectively. An all-blade steam gas turbine combined engine, wherein the all-blade steam gas turbine is used while being appropriately interchanged with each other and a waterway is connected to a water injection means (56).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water pump and contra-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the upstream side in the rotation direction, and are appropriately interchangeable. And a water passage connected to the water injection means (56).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water feed pump and contra-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the upstream side in the rotation direction, and are appropriately interchangeable. A combined turbine and steam turbine in which a waterway is connected to a water injection means (56).

The various internal magnetized friction wheels and the various internal magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the downstream side in the rotation direction, and are appropriately interchangeable. And a water passage connected to the water injection means (56).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water pump and contra-rotating magnetic friction power transmission device (14a) are provided with bar magnets (33) on the downstream side in the rotation direction, and are appropriately interchangeable. A combined turbine and steam turbine in which a waterway is connected to a water injection means (56).

The water supplied to the combustor / heat exchanger (4) was boosted and used by the water pump and the contra-rotating magnetic friction power transmission device (14a), and the waterway was connected to the water injection means (56). An all-blade steam gas turbine combined engine, characterized in that:

The water to be supplied to the combustor and heat exchanger (4) is used in a multi-stage pressure by the water pump and the contra-rotating magnetic friction power transmission device (14a). An all-blade steam gas turbine united engine characterized by having been contacted.

The water supplied to the combustor / heat exchanger (4) is multi-staged and used by the plurality of water pumps and the contra-rotating magnetic friction power transmission device (14a), and the water channel is formed by water injection means (56). A combined steam turbine turbine engine, characterized in that:

The water pump and the contra-rotating magnetic friction power transmission device (14a) uses water supplied to a combustor / heat exchanger (4) and connects a water passage on the way to a water injection means (56). All-blade steam gas turbine combined engine.

The water feed pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4), and brings the water feed pump (97) closer to non-contact by increasing the water pressure. An all-blade steam gas turbine combined engine, wherein the waterway is connected to the water injection means (56).

The water feed pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4) and brings the water feed pump (97) closer to non-contact by the increase in water pressure. An all-blade steam gas turbine combined engine which supports ultra-high-speed rotation and has a waterway connected to a water injection means (56).

The water feed pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4), increases the temperature of the water, and injects water along the way. An all-blade steam gas turbine combined engine characterized by communicating with means (56).

The water / water pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4) and raises the temperature of the water to mix substances into the water. An all-blade steam gas turbine combined engine characterized by reducing pollution, lubricating, and connecting a waterway to water injection means (56).

Various magnetized friction wheels and various magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the upstream side in the rotation direction, and are used as appropriate and interchangeable. And an all-blade steam gas turbine united engine wherein the waterway is connected to the water injection means (56a).

Various magnetized friction wheels and various magnetized friction wheels of the water feed pump and contra-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the upstream side in the rotation direction, and are appropriately interchangeable with each other. An all-blade steam gas turbine combined engine, which is used and has a waterway connected to a water injection means (56a).

Various magnetized friction wheels and various magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the downstream side in the rotation direction, and are used as appropriate. And an all-blade steam gas turbine united engine wherein the waterway is connected to the water injection means (56a).

Various magnetized friction wheels and various magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with bar magnets (33) on the downstream side in the rotation direction, and are appropriately interchangeable with each other. An all-blade steam gas turbine combined engine, which is used and has a waterway connected to a water injection means (56a).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with electromagnets (34) on the upstream side and the downstream side in the rotation direction, respectively. An all-blade steam gas turbine combined engine characterized in that it is used interchangeably with (i) and the waterway is connected to a water injection means (56a).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with bar magnets (33) on the upstream and downstream sides in the rotational direction, respectively. An all-blade steam gas turbine combined engine, wherein the engines are used appropriately interchangeably and the waterway is connected to a water injection means (56a).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water pump and contra-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the upstream side in the rotation direction, and are appropriately interchangeable. A combined turbine and steam gas turbine engine, wherein a waterway is connected to a water injection means (56a).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water feed pump and contra-rotating magnetic friction power transmission device (14a) are provided with a bar magnet (33) on the upstream side in the rotation direction, and are appropriately interchangeable. A combined turbine and steam gas turbine engine characterized in that a waterway is connected to a water injection means (56a).

The various internal magnetized friction wheels and the various internal magnetized friction wheels of the water pump and the contra-rotating magnetic friction power transmission device (14a) are provided with an electromagnet (34) on the downstream side in the rotation direction, and are appropriately interchangeable. A combined turbine and steam gas turbine engine, wherein a waterway is connected to a water injection means (56a).

Various internal magnetized friction wheels and various internal magnetized friction wheels of the water pump and contra-rotating magnetic friction power transmission device (14a) are provided with bar magnets (33) on the downstream side in the rotation direction, and are appropriately interchangeable. A combined turbine and steam gas turbine engine characterized in that a waterway is connected to a water injection means (56a).

The water supplied to the combustor / heat exchanger (4) was boosted and used by the water pump and the contra-rotating magnetic friction power transmission device (14a), and the waterway was connected to the water injection means (56a). An all-blade steam gas turbine combined engine, characterized in that:

The water supplied to the combustor / heat exchanger (4) is used in a multi-stage pressure by the water pump and the contra-rotating magnetic friction power transmission device (14a), and the water passage is provided to the water injection means (56a). An all-blade steam gas turbine united engine characterized by having been contacted.

The water supplied to the combustor / heat exchanger (4) is used in a multi-stage manner by the plurality of water pumps and the contra-rotating magnetic friction power transmission device (14a). A combined steam turbine turbine engine, characterized in that:

The water pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to a combustor / heat exchanger (4), and connects a waterway on the way to a water injection means (56a). All-blade steam gas turbine combined engine.

The water feed pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4), and brings the water feed pump (97) closer to non-contact by increasing the water pressure. An all-blade steam gas turbine combined engine, wherein the waterway is connected to a water injection means (56a).

The water feed pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4) and brings the water feed pump (97) closer to non-contact by the increase in water pressure. An all-blade steam gas turbine combined engine which supports ultra-high-speed rotation and connects a waterway on the way to a water injection means (56a).

The water feed pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4), increases the temperature of the water, and injects water along the way. All-blade steam gas turbine combined engine characterized by communicating with means (56a).

The water / water pump and contra-rotating magnetic friction power transmission device (14a) uses water supplied to the combustor / heat exchanger (4) and raises the temperature of the water to mix substances into the water. An all-blade steam gas turbine combined engine, wherein pollution is reduced and lubrication is performed, and a waterway is connected to a water injection means (56a).

The said water injection means (56) is provided in the vicinity of the assembled annular connection portion, and is integrally cast in a ring for each blade stage (84), and a water passage is connected and used at the assembled annular connection portion. An all-blade steam gas turbine combined engine equipped with blades (81).

The water injection means (56) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84). A water channel is connected and used at the assembled annular connection part. An all-blade steam gas turbine combined engine including an electromagnetically heated turbine blade (81) characterized by injecting.

The water injection means (56) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84). A water channel is connected and used at the assembled annular connection part. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81), which cools compressed air by injecting and recovers heat.

The water injection means (56) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84). A water channel is connected and used at the assembled annular connection part. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81), characterized in that the compressed air is injected to cool the compressed air, and the cold air that has recovered heat is compressed in a substantially linear meandering manner.

The water injection means (56) is provided in the vicinity of the assembled annular connection part, and the water-repellent water cooling blade (87) is cooled by cooling the half of the paragraph in the water channel of the cooling means (55), and then the water injection means (56) is fully driven. Wing steam gas turbine combined engine.

The water injection means (56) is provided in the vicinity of the assembled annular connection part, and the water-repellent water cooling blades (87) are cooled by the water path of the cooling means (55), and after cooling the entire paragraph, water is injected from the water injection means (56). Wing steam gas turbine combined engine.

The water injection means (56) is provided in the vicinity of the assembled annular connection part, and the water-repellent water cooling blade (87) is cooled by cooling a plurality of paragraphs in the water channel of the cooling means (55), and then the water injection means (56) performs water injection. Wing steam gas turbine combined engine.

The water injection means (56) is provided in the vicinity of the assembled annular connection part, and the water-repellent water cooling blade (87) is cooled by cooling a number of paragraphs in the water channel of the cooling means (55), and then the water injection means (56) water-injects water. Wing steam gas turbine combined engine.

A combined steam turbine turbine having an electromagnetically heated turbine blade (81), characterized in that the water jet steam is cooled by the water injection means (56a) and the steam velocity is converted into velocity energy of water mass. organ.

A rotor blade provided with an electromagnetically heated turbine blade (81), wherein water jet steam having a temperature not higher 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.

An electromagnetically heated turbine blade (81) characterized in that the water jet steam is cooled by the water jetting means (56a), and the steam velocity is converted into velocity energy of water mass to increase the unit gravity power. All blade steam gas turbine combined engine.

An electromagnetically heated turbine blade (81) characterized in that water jet steam having a temperature not higher than the saturation temperature is cooled by the water jetting means (56a), and the steam velocity is converted into velocity energy of water mass to increase unit gravity power. ) Is provided with an all-blade steam gas turbine combined engine.

The electromagnetically-heated turbine blade (81) is characterized in that the water-jet steam is cooled by the water-jetting means (56a) and the steam velocity is converted into velocity energy of water mass to increase the total gravity power. All blade steam gas turbine combined engine.

An electromagnetically heated turbine blade (81) characterized in that water jet steam having a temperature not higher than the saturation temperature is cooled by the water jet means (56a), and the steam velocity is converted into velocity energy of water mass to increase the total gravity power. ) Is provided with an all-blade steam gas turbine combined engine.

The electromagnetically-heated turbine blade (1) is characterized in that the water-jet steam is cooled by the water-jetting means (56a), the steam velocity is converted into velocity energy of water mass, the total gravity power is increased, and the output is increased. 81) A combined turbine and steam gas turbine engine comprising:

Electromagnetic heating, wherein water jet steam having a temperature not higher than the saturation temperature is cooled by the water jetting means (56a), and the steam velocity is converted into velocity energy of water mass to increase the total gravity power to increase the output. An all-steam steam gas turbine combined engine including a turbine blade (81).

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a), and steam velocity is converted into velocity energy of water mass to increase unit gravity power.

A water jet steam having a temperature not higher than a saturation temperature is cooled by the water jetting means (56a), and a steam velocity is converted into velocity energy of water mass to increase a unit gravity power, so that all bladed steam gas turbine united. organ.

An all-blade steam gas turbine combined engine, wherein water vapor injected from the water injection means (56a) is cooled to convert steam velocity into velocity energy of water mass to increase total gravitational power.

A combined steam turbine turbine with all blades, characterized in that water jet steam having a temperature not higher than the saturation temperature is cooled by the water jetting means (56a), and the steam velocity is converted into velocity energy of water mass to increase the total gravity power. organ.

An all-blade steam gas turbine, wherein the water jet steam is cooled by the water jet means (56a), and the steam velocity is converted into velocity energy of water mass to increase the total gravity power to increase the output. Coalition organization.

A water jet steam having a temperature not higher than a saturation temperature is cooled by the water jetting means (56a), the steam velocity is converted into velocity energy of water mass, the total gravity power is increased, and the output is increased. Wing steam gas turbine combined engine.

A combined steam turbine engine with an electromagnetically heated turbine blade (81), characterized in that water jet steam having a temperature equal to or lower than the saturation temperature is cooled by the water injection means (56a) to lower the exhaust water temperature. .

A water jet steam having a temperature not higher than the saturation temperature is cooled by the water jetting means (56a), and the temperature of the exhaust water is lowered to reduce the amount of cooling water; Combined moving blade steam gas turbine engine.

An electromagnetically heated turbine blade (81) characterized in that water jet steam having a temperature not higher than the saturation temperature is cooled by the water jetting means (56a) to lower the exhaust water temperature to reduce the amount of cooling water and to prevent global warming. ) Is provided with an all-blade steam gas turbine combined engine.

An all-blade steam gas turbine combined engine, wherein water jet steam having a temperature equal to or lower than a saturation temperature is cooled by the water jetting means (56a) to lower the exhaust water temperature.

An all-blade steam gas turbine combined engine, wherein water jet steam having a temperature not higher than the saturation temperature is cooled by the water jetting means (56a), and the temperature of exhaust water is minimized to minimize the rise in cooling water temperature.

A water jet steam having a temperature not higher than a saturation temperature by the water jet means (56a), thereby minimizing a rise in cooling water temperature by minimizing an exhaust water temperature and preventing global warming; Gas turbine combined engine.

The water jetting means (56a) cools water jet steam having a temperature not higher than the final saturation temperature to minimize the temperature of exhaust water and minimize the rise in cooling water temperature to prevent global warming. Wing steam gas turbine combined engine.

The water injection means (56a) cools the water injection steam below the saturation temperature of the condenser vacuum final stage, minimizes the temperature of the exhaust water, minimizes the rise in cooling water temperature, and prevents global warming. All-blade steam gas turbine combined engine.

An all-blade steam gas turbine combined engine, wherein the water jet steam is cooled by the water jetting means (56a) to increase the steam volume to 1/100 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein the water jet steam is cooled by the water jetting means (56a) to increase the steam volume to 1/300 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, characterized in that water jet steam is cooled by the water jet means (56a) to increase the steam volume to 1/600 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jet means (56a) to increase the steam volume to 1/1000 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein the water injection steam is cooled by the water injection means (56a), and the total gravitational power is made about 500 times that of the existing gas turbine.

An all-blade steam gas turbine combined engine, wherein the water injection steam is cooled by the water injection means (56a) so that the total gravitational power is about 400 times that of an existing gas turbine.

An all-blade steam gas turbine combined engine, characterized in that water jet steam is cooled by the water jet means (56a) so that the total gravity power is about 600 times that of an existing gas turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) so that the total gravity power is about 700 times that of an existing gas turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) to make the total gravitational power about 800 times that of an existing gas turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) to make the total gravitational power about 1000 times that of an existing gas turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) so that the total gravity power is about 300 times that of an existing gas turbine.

An all-blade steam / gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) so that the total gravity power is about 100 times that of an existing gas turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) and the same output blade area is reduced to 1/500 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein the water jet steam is cooled by the water jetting means (56a) so that the same output blade area is reduced to 1/400 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) and the same output blade area is reduced to 1/300 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) and the same output blade area is reduced to 1/200 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, characterized in that water jet steam is cooled by the water jetting means (56a) and the same output blade area is reduced to 1/100 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein the water jet steam is cooled by the water jetting means (56a) so that the same output blade area is reduced to 1/50 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein water jet steam is cooled by the water jetting means (56a) to reduce the same output blade area to 1/20 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, characterized in that water jet steam is cooled by the water jetting means (56a) and the same output blade area is reduced to 1/10 or less of the existing steam turbine.

An all-blade steam gas turbine combined engine, wherein the water jet steam is cooled by the water jet means (56a), and the rise of the same output cooling water temperature, for example, the seawater temperature, is reduced to 1/1000 or less of the existing steam turbine. .

An all-blade steam gas turbine combined engine, wherein the water jet steam is cooled by the water jetting means (56a) so that the rise of the same output cooling water temperature, for example, the seawater temperature, is 1/500 or less of that of the existing steam turbine. .

An all-blade steam gas turbine combined engine wherein the water jet steam is cooled by the water jetting means (56a) so that the same output cooling water temperature, for example, the rise of seawater temperature is made 1/200 or less of the existing steam turbine. .

An all-blade steam gas turbine combined engine wherein the water jet steam is cooled by the water jetting means (56a) so that a rise in the same output cooling water temperature, for example, the seawater temperature, is made 1/100 or less of that of the existing steam turbine. .

An all-blade steam gas turbine combined engine, wherein the water jet steam is cooled by the water jetting means (56a) so that a rise in the same output cooling water temperature, for example, the seawater temperature, is 1/50 or less of that of the existing steam turbine. .

An all-blade steam gas turbine combined engine, wherein the water injection steam is cooled by the water injection means (56a) so that a rise in the same output cooling water temperature, for example, the seawater temperature, is made 1/20 or less of that of the existing steam turbine. .

An all-blade steam gas turbine combined engine wherein the water jet steam is cooled by the water jet means (56a) so that the same output cooling water temperature, for example, the rise of seawater temperature is made 1/10 or less of the existing steam turbine. .

An all-blade steam gas turbine combined engine, wherein the water jet steam is cooled by the water jetting means (56a), and the unit gravitational power is increased by converting the steam velocity and velocity energy of water mass.

The all-rotor blade, wherein the water jet steam is cooled by the water jetting means (56a), and the steam velocity and the latent heat of vaporization are converted into velocity energy of water mass to increase the total gravity power to increase the output. Steam gas turbine combined engine.

A whole-blade steam provided with an electromagnetically heated turbine blade (81), characterized in that the water jet steam is cooled by the water injection means (56a) and a large part of the steam velocity is converted into velocity energy of water mass. Gas turbine combined engine.

The electromagnetically heated turbine is 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 the steam is injected in a substantially linear meandering manner to generate an output. An all-blade steam gas turbine combined engine equipped with blades (81).

An electromagnetic heating turbine for cooling the water-injected steam from the water-injecting means (56a), converting the steam velocity into velocity energy of water mass, and injecting the water in a substantially linear meandering manner to generate an output. An all-blade steam gas turbine combined engine including a bucket (81).

The water jetting means (56a) cools water jet steam, converts most of the steam velocity into velocity energy of water mass, and ejects the water in a substantially linear meandering manner to generate an output. An integrated steam turbine combined engine equipped with a heated turbine rotor blade (81).

The said water injection means (56a) is provided in the vicinity of the assembled annular connection part, and is integrally cast annularly (84) for each blade stage to connect and use a water path insulated at the assembled annular connection part. An all-steam steam gas turbine combined engine including a turbine blade (81).

The water injection means (56a) is provided in the vicinity of one of the assembled annular connection portions of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20) that are integrally cast (84) annularly for each blade stage. A combined steam turbine turbine engine comprising an electromagnetically heated turbine blade (81).

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84) to connect and use a water path insulated by the assembled annular connection part. An integrated steam turbine driven engine equipped with an electromagnetically heated turbine blade (81), characterized by injecting water from a steam turbine.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84) to connect and use a water path insulated by the assembled annular connection part. A combined steam turbine engine equipped with electromagnetically heated turbine blades (81), characterized in that water is injected from the water injection means (56a) to reduce the combustion gas volume and increase the mass.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84) to connect and use a water path insulated by the assembled annular connection part. A combined turbine blade and an electromagnetically heated turbine blade (81), characterized in that the water is injected from the water injection means (56a) to reduce the volume of the vaporized explosion steam and increase the mass.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, is integrally cast in a ring for each blade stage (84), and is used by connecting a water path insulated at the assembled annular connection part. A rotor blade steam gas turbine equipped with an electromagnetically heated turbine blade (81), characterized in that water is injected from a water injection means (56a) in the vicinity of the part, and the water contains a substance that promotes the synthesis and dissolution of harmful substances. Coalition organization.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, is integrally cast in a ring for each blade stage (84), and is used by connecting a water path insulated at the assembled annular connection part. A rotor blade steam gas turbine equipped with an electromagnetically heated turbine blade (81), characterized in that water is injected from the vicinity of the part, and the water contains a substance that promotes the dissolution and synthesis of harmful substances, and is discharged harmlessly. Coalition organization.

After the water-repellent water cooling blades (87) are cooled by the water, the assembled annular connection portion for injecting water from the water injection means (56) provided near the assembly annular connection portion is integrally cast into a ring for each blade stage (84). A combined turbine blade and steam turbine combined engine having an electromagnetically heated turbine blade (81), characterized in that a water channel of a cooling means (55) is connected and used at the assembled annular connection part.

After the water-repellent water cooling blades have been cooled by the water, the assembled annular connection portion for injecting water from the water injection means (56) is integrally cast into a ring for each blade stage (84), and the cooling means ( 55. A combined rotor blade steam gas turbine engine equipped with an electromagnetically heated turbine rotor blade (81), characterized by connecting and using the water channel according to (55).

The assembled annular connecting portion for injecting water from the water injection means (56) after cooling the at least one or more water-repellent water cooling blades with water is integrally cast into a ring for each blade stage (84). An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81), characterized in that a water passage of a cooling means (55) is connected and used.

After the water-repellent water cooling blades of all the stages have been cooled by the water, the assembled annular connection portion for injecting water from the water injection means (56) is integrally cast into a ring for each blade stage (84). An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81), characterized by connecting and using a water channel of a cooling means (55).

The assembled annular connecting portion for jetting water from the water jetting means (56) after cooling the half-stage water-repellent water cooling blade with the water is integrally cast in a ring for each blade stage (84). An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81), characterized by connecting and using a water channel of a cooling means (55).

By bringing the combustion gas exhaust gas temperature close to -273 ° C., the heat recovery amount of the all-blade steam gas turbine is increased, and the all-blade steam gas turbine combined with the electromagnetically heated turbine blade (81) is characterized. organ.

A combined bladed steam gas turbine engine equipped with an electromagnetically heated turbine blade (81) characterized in that the combustion gas exhaust temperature is brought close to -273 ° C to increase the heat recovery amount of the bladed gas turbine. .

By bringing the exhaust temperature of the combustion gas close to -273 ° C., it is possible to facilitate aggregation of water and the like that agglomerate the low-temperature combustion gas into nuclei in the vicinity of the exhaust of the full-blade steam gas turbine. An all-blade steam gas turbine combined engine equipped with blades (81).

An electromagnetically heated turbine blade, wherein the combustion gas exhaust temperature is made to be close to -273 ° C., thereby facilitating aggregation of water or the like that coagulates a low-temperature combustion gas into a nucleus in the vicinity of the exhaust of the all blade gas turbine. An all-blade steam gas turbine combined engine comprising (81).

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is aggregated with water and the like as nuclei, separated and collected as water droplets, and supplied into the sea. An all-blade steam gas turbine combined engine comprising an electromagnetically heated turbine blade (81).

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are agglomerated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets and the like, supplied into the sea, All-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81) characterized by breeding.

In a combined rotor blade steam gas turbine engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are agglomerated with a low-temperature combustion gas as a nucleus, separated and recovered as water droplets and the like, supplied into the sea, and corals All-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81) characterized by breeding.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are agglomerated with a low-temperature combustion gas as a nucleus, separated and collected as water droplets, and supplied into the sea. All-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81) characterized by breeding.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are aggregated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets, etc. And the like, and supplies the underwater to the sea, provided with an electromagnetically heated turbine blade (81).

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are coagulated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets and the like, and supplied to the sea together with oxygen and the like. An all-blade steam gas turbine combined engine comprising an electromagnetically heated turbine blade (81) characterized by breeding seaweed.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are coagulated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets and the like, and supplied to the sea together with oxygen and the like. A steam turbine integrated unit having an electromagnetically heated turbine rotor blade (81) characterized by breeding corals.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are coagulated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets and the like, and supplied to the sea together with oxygen and the like. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81) characterized in that microorganisms and fish and shellfish are propagated.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is used as a nucleus to condense moisture and the like, and is separated and collected as water droplets and the like to cool tap water. A combined bladed steam gas turbine engine comprising an electromagnetically heated turbine blade (81).

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is used as a nucleus to condense moisture and the like, and is separated and collected as water droplets and the like. An integrated steam turbine driven engine comprising an electromagnetically heated turbine blade (81), characterized in that the blade is stored in the steam turbine.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is used as a nucleus to condense moisture and the like, and is separated and collected as water droplets and the like. An all-blade steam gas turbine combined engine equipped with an electromagnetically heated turbine blade (81), characterized in that the blade is stored and supplied.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is used as a nucleus to condense moisture and the like, and is separated and collected as water droplets and the like. A combined steam turbine engine equipped with an electromagnetically heated turbine rotor blade (81), which is stored at a factory and supplied for business use.

A cooling blade for cooling water jetted from the water jetting means (56a) and converting the steam speed into velocity energy of water mass; Steam gas turbine combined engine.

The water jet steam is cooled by the water jetting means (56a), and the steam velocity is converted into velocity energy of water mass to increase the unit gravity power. An all-blade steam gas turbine combined engine that generates output.

The high-temperature water (5a) such as a supercritical pressure characterized in that the water jet steam is cooled by the water jetting means (56a) and the steam velocity is converted into velocity energy of water mass to increase the total gravity power. An all-blade steam gas turbine combined engine that generates output.

The water jet steam is cooled by the water jetting means (56a), and the steam velocity is converted into velocity energy of water mass to increase the total gravitational power to increase the output. An all-blade steam gas turbine combined engine that generates output with water (5a).

A high-temperature water (5a) having a supercritical pressure or the like characterized in that the water jet steam is cooled by the water jetting means (56a) and the steam velocity and the water mass are converted into velocity energy to increase the unit gravity power. An all-blade steam gas turbine combined engine that generates power at

The water injection steam is cooled by the water injection means (56a), and a large part of the steam velocity is converted into velocity energy of water mass, and an output is generated by high temperature water (5a) such as supercritical pressure. All blade steam gas turbine combined engine.

A supercritical pressure or the like 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 the steam is injected in a substantially linear meandering manner to generate an output. All-blade steam gas turbine combined engine that generates output with high temperature water (5a).

A supercritical pressure, wherein the water injection steam is cooled by the water injection means (56a), the steam velocity is converted into velocity energy of water mass, and the output is generated by substantially linear meandering injection. All-blade steam gas turbine combined engine that generates output with high-temperature water (5a).

The water injection means (56a) cools the water injection steam, converts a large part of the steam velocity into velocity energy of water mass, and ejects the water in a substantially linear meandering manner to generate an output. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) such as a critical pressure.

The supercritical water injection means (56a) is provided in the vicinity of an assembled annular connection portion, and is integrally formed in an annular shape for each blade stage (84) to connect and use an insulated water channel at the assembled annular connection portion. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) such as pressure.

The water injection means (56a) is provided in the vicinity of one of the assembled annular connection portions of the outer turbine rotor blade group (19) and the inner turbine rotor blade group (20) that are integrally cast (84) annularly for each blade stage. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) such as supercritical pressure.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84) to connect and use a water path insulated by the assembled annular connection part. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) such as supercritical pressure, characterized by injecting water from a steam turbine.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84) to connect and use a water path insulated by the assembled annular connection part. All-blade steam gas turbine that generates power with high-temperature water (5a) at a supercritical pressure or the like characterized by reducing the combustion gas volume and increasing the mass by injecting water from the water injection means (56a). Coalition organization.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, and is integrally cast in a ring for each blade stage (84) to connect and use a water path insulated by the assembled annular connection part. All-blade steam gas turbine generating water with supercritical pressure or other high-temperature water (5a), wherein water is injected from water injection means (56a) to reduce superheated steam volume and increase mass. Coalition organization.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, is integrally cast in a ring for each blade stage (84), and is used by connecting a water path insulated at the assembled annular connection part. A water injection means (56a) in the vicinity of the water jetting means (56a), wherein the water contains a substance which promotes the dissolution and dissolution of harmful substances. Wing steam gas turbine combined engine.

The water injection means (56a) is provided in the vicinity of the assembled annular connection part, is integrally cast in a ring for each blade stage (84), and is used by connecting a water path insulated at the assembled annular connection part. A water jet is injected from the vicinity of the part, and the water containing a substance that promotes the dissolution and synthesis of harmful substances is discharged harmlessly close to the water. Wing steam gas turbine combined engine.

After the water-repellent water cooling blades (87) are cooled by the water, the assembled annular connection portion for injecting water from the water injection means (56) provided near the assembly annular connection portion is integrally cast into a ring for each blade stage (84). A combined turbine and steam gas turbine engine that generates output with high-temperature water (5a) such as supercritical pressure, characterized in that a water channel of a cooling means (55) is connected and used at the assembled annular connection portion.

After the water-repellent water cooling blades have been cooled by the water, the assembled annular connection portion for injecting water from the water injection means (56) is integrally cast into a ring for each blade stage (84), and the cooling means ( 55) An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) such as supercritical pressure, characterized by connecting and using the water channel of 55).

The assembled annular connecting portion for injecting water from the water injection means (56) after cooling the at least one or more water-repellent water cooling blades with water is integrally cast into a ring for each blade stage (84). A combined turbine and steam gas turbine engine that generates an output with high-temperature water (5a) having a supercritical pressure or the like, characterized by connecting and using a water passage of a cooling means (55).

After the water-repellent water cooling blades of all the stages have been cooled by the water, the assembled annular connection portion for injecting water from the water injection means (56) is integrally cast into a ring for each blade stage (84). An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) such as supercritical pressure, characterized by connecting and using a water path of a cooling means (55).

The assembled annular connecting portion for jetting water from the water jetting means (56) after cooling the half-stage water-repellent water cooling blade with the water is integrally cast in a ring for each blade stage (84). An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) such as supercritical pressure, characterized by connecting and using a water path of a cooling means (55).

A full-blade generating output with high-temperature water (5a) such as supercritical pressure characterized by increasing the heat recovery amount of a full-blade steam gas turbine by bringing the combustion gas exhaust temperature close to -273 ° C. Steam gas turbine combined engine.

The whole blade steam that generates output with high temperature water (5a) such as supercritical pressure characterized by increasing the heat recovery amount of the whole blade gas turbine by bringing the combustion gas exhaust temperature close to -273 ° C. Gas turbine combined engine.

By bringing the combustion gas exhaust temperature close to -273 ° C., in the vicinity of the exhaust of the all-blade steam gas turbine, it is easy to coagulate water or the like that coagulates the low-temperature combustion gas into the nucleus. All-blade steam gas turbine combined engine that generates output with high temperature water (5a).

By bringing the combustion gas exhaust temperature close to −273 ° C., in the vicinity of the exhaust of the all-blade gas turbine, facilitation of aggregation of water or the like that aggregates low-temperature combustion gas into nuclei is facilitated. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a).

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is aggregated with water and the like as nuclei, separated and collected as water droplets, and supplied into the sea. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) such as supercritical pressure.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are agglomerated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets and the like, supplied into the sea, All-blade steam gas turbine combined engine that generates output with high temperature water (5a) such as supercritical pressure characterized by breeding.

In a combined rotor blade steam gas turbine engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are agglomerated with a low-temperature combustion gas as a nucleus, separated and recovered as water droplets and the like, supplied into the sea, and corals All-blade steam gas turbine combined engine that generates output with high temperature water (5a) such as supercritical pressure characterized by breeding.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are agglomerated with a low-temperature combustion gas as a nucleus, separated and collected as water droplets, and supplied into the sea. All-blade steam gas turbine combined engine that generates output with high temperature water (5a) such as supercritical pressure characterized by breeding.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are aggregated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets, etc. And the like. The combined rotor blade steam gas turbine engine that generates power with high-temperature water (5a) at a supercritical pressure or the like characterized by sucking and supplying the water into the sea.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are coagulated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets and the like, and supplied to the sea together with oxygen and the like. And an all-blade steam gas turbine combined engine that generates power with high-temperature water (5a) at supercritical pressure or the like characterized by breeding seaweed.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are coagulated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets and the like, and supplied to the sea together with oxygen and the like. And a propeller steam gas turbine combined engine that generates power with high-temperature water (5a) at a supercritical pressure or the like characterized by breeding corals.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., water and the like are coagulated with the low-temperature combustion gas as a nucleus, separated and collected as water droplets and the like, and supplied to the sea together with oxygen and the like. And an all-blade steam gas turbine combined engine that generates power with high-temperature water (5a) such as supercritical pressure characterized by breeding microorganisms and seafood.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is used as a nucleus to condense moisture and the like, and is separated and collected as water droplets and the like to cool tap water. An all-blade steam gas turbine combined engine that generates power with high temperature water (5a) such as supercritical pressure.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is used as a nucleus to condense moisture and the like, and is separated and collected as water droplets and the like. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) at a supercritical pressure or the like characterized by being stored in a steam turbine.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is used as a nucleus to condense moisture and the like, and is separated and collected as water droplets and the like. An all-blade steam gas turbine combined engine that generates output with high-temperature water (5a) at a supercritical pressure or the like, characterized by being stored and supplied.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the low-temperature combustion gas is used as a nucleus to condense moisture and the like, and is separated and collected as water droplets and the like. An all-blade steam gas turbine combined engine that generates power with high-temperature water (5a) at supercritical pressure or the like, characterized in that the engine is stored at a factory and supplied for business use.

An all-blade steam gas turbine combined engine for bringing the combustion gas exhaust temperature close to -273 ° C., wherein pulverized coal fuel is used in a combustor / heat exchanger (4). organ.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the pulverized coal fuel is burned in a combustor / heat exchanger (4) and is heated with high-temperature water (5a) such as supercritical pressure. An all-blade steam gas turbine combined engine characterized by recovering heat for use.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the pulverized coal fuel is burned in a combustor / heat exchanger (4) and is heated with high-temperature water (5a) such as supercritical pressure. An integrated all-blade steam gas turbine engine that recovers heat and uses it for power generation.

A combined rotor blade steam gas turbine engine wherein the combustion gas exhaust gas temperature approaches -273 [deg.] C., wherein a waste gasification fuel is used in an auxiliary manner.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., waste gasified fuel is burned, and heat is recovered with high-temperature water (5a) such as supercritical pressure for auxiliary use. All-blade steam gas turbine combined engine.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., waste gasified fuel is burned, heat is recovered with high-temperature water (5a) having a supercritical pressure or the like, and is used for auxiliary use. An all-blade steam gas turbine combined engine, wherein gas air is compressed by an all-blade compressor.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., waste gasified fuel is burned, heat is recovered with high-temperature water (5a) having a supercritical pressure or the like, and is used for auxiliary use. An all-blade steam gas turbine combined engine, wherein gas air is compressed by a full-blade compressor and supplied to a combustor / heat exchanger (4).

An all-blade steam gas turbine combined engine wherein the combustion gas exhaust temperature approaches -273 [deg.] C., wherein all combustibles are used as fuel as auxiliary fuel.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., all the combustibles are burned as fuel, and heat is recovered with high-temperature water (5a) such as supercritical pressure for auxiliary use. An all-blade steam gas turbine combined engine characterized by the following.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., all the combustibles are burned as fuel, and heat is recovered with high-temperature water (5a) at a supercritical pressure or the like for auxiliary use, An all-blade steam gas turbine combined engine, wherein the combustion gas air is compressed by an all-blade compressor.

In an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., all the combustibles are burned as fuel, and heat is recovered with high-temperature water (5a) at a supercritical pressure or the like for auxiliary use, An all-blade steam gas turbine combined engine, wherein the combustion gas air is compressed by a full-blade compressor and supplied to the combustor / heat exchanger 4.

An all-blade steam gas turbine combined engine, wherein the all-blade steam turbine, which brings the combustion gas exhaust temperature close to -273 ° C., is used as the all-blade gas turbine only at startup.

An all-blade steam gas turbine combined engine, wherein the all-blade steam gas turbine is used as the all-blade steam gas turbine only at the time of start-up, in which the combustion gas exhaust temperature approaches -273 ° C.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the combustion gas is stored in the combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure. All blade steam gas turbine combined engine.

Very safe by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in a combined turbine and steam gas turbine engine that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine characterized by a simple jet machine.

Very safe by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in a combined turbine and steam gas turbine engine that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine united engine characterized by a unique space shuttle parent aircraft.

Very safe by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in a combined turbine and steam gas turbine engine that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine characterized by a supersonic airplane.

Very safe by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in a combined turbine and steam gas turbine engine that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine characterized by a supersonic passenger aircraft.

Very safe by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in a combined turbine and steam gas turbine engine that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine characterized by a unique flying ship.

Very safe by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in a combined turbine and steam gas turbine engine that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine combined engine characterized by being a simple flying object.

Extinguish a fire by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in an 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 a very safe jet machine that is difficult to generate easily.

Extinguish a fire by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in an 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 a very safe space shuttle parent airplane that is difficult to generate easily.

Extinguish a fire by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C. An all-wing steam gas turbine combined engine characterized by a very safe supersonic airplane, which is difficult to generate easily.

Extinguish a fire by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in an all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C. An all-blade steam gas turbine united engine characterized by a very safe supersonic airliner that is difficult to generate easily.

Extinguish a fire by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in an 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 a very safe flying ship that is difficult to generate easily.

Extinguish a fire by storing in a combustor / heat exchanger (4) with high-temperature water (5a) such as supercritical pressure in an 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 that is difficult to generate easily.

A combined rotor blade steam gas turbine engine in which the combustion gas exhaust temperature approaches -273 [deg.] C., wherein a special device (92a) performs bypass injection at a head far exceeding the ram jet by a special device (92a).

A combined rotor blade steam gas turbine engine in which the combustion gas exhaust temperature approaches -273 ° C., wherein a plurality of special devices (92a) perform bypass injection with a head far exceeding a ram jet by a plurality of special devices (92a).

A combined rotor blade steam gas turbine engine in which the combustion gas exhaust temperature approaches -273 ° C., wherein a special device (92b) performs bypass injection at a head far beyond the ram jet by a special device (92b).

A combined rotor blade steam gas turbine engine wherein the combustion gas exhaust temperature approaches -273 [deg.] C., wherein a plurality of special devices (92b) perform bypass injection at a head far exceeding a ram jet by a plurality of special devices (92b).

A combined rotor blade steam gas turbine engine in which the combustion gas exhaust temperature approaches -273 ° C., wherein the combustion gas is bypass-injected by a water injection device (93b).

An all-blade steam gas turbine combined engine, wherein the combustion gas exhaust temperature approaches -273 ° C., wherein the combustion gas is bypass-injected by a plurality of water injection devices (93b).

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C., the all-blade steam gas turbine combined with bypass injection of high-temperature water (5a) such as supercritical pressure by a water injection device (93a). organ.

In a combined blade / steam gas turbine combined engine that brings the combustion gas exhaust temperature close to −273 ° C., a plurality of water injection devices (93a) for bypass injection of high-temperature water (5a) such as supercritical pressure by a plurality of water injection devices (93a). Turbine united engine.

A full-blade gas turbine having an electromagnetically heated turbine blade (81), wherein the combustion gas exhaust temperature approaches -273 ° C., wherein the use of combustion gas calorific value of fuel is reduced to substantially zero. Steam gas turbine combined engine.

A full-blade steam gas turbine equipped with an electromagnetically heated turbine blade (81), wherein the low-temperature combustion gas includes coal ash and the like, and the total gravitational power is increased in the process of generating power to increase the output. Coalition organization.

In the all-blade gas turbine in which the combustion gas exhaust temperature approaches -273 ° C., the use of combustion gas calorie of fuel is reduced to substantially zero, and the output is generated by high-temperature water (5a) such as supercritical pressure. All-blade steam gas turbine combined engine.

The above-mentioned low-temperature combustion gas includes coal ash and the like, wherein the total gravitational power is increased in the process of generating the output, and the output is increased. Wing steam gas turbine combined engine.

A full-rotor steam gas characterized in that a device driven by any one or more of the outputs of the all-rotor blade gas turbine and the all-rotor steam turbine and the all-rotor steam gas turbine is a large, medium and small power generation facility. Turbine united engine.

The apparatus for driving the all-rotor blade gas turbine and the all-rotor blade steam turbine and the all-rotor blade steam gas turbine with any one or more outputs is a large, medium and small heat, electricity, and cold supply equipment. All-blade steam gas turbine combined engine.

A device driven by any one or more of the full-rotor gas turbine and the full-rotor steam turbine and the full-rotor steam gas turbine as a large and medium and small heat and electricity supply facility; Wing steam gas turbine combined engine.

A device driven by any one or more of the above-mentioned full-rotor blade gas turbine, full-rotor blade steam turbine, full-rotor blade steam gas turbine, special device, and water injection device is a large, medium, or small vessel. All blade steam gas turbine combined engine.

A device driven by at least one of the output of the full-rotor gas turbine, the full-rotor steam turbine, the full-rotor steam gas turbine, the special device, and the water injection device is a large, medium, or small aircraft. All blade steam gas turbine combined engine.

A device driven by any one or more of the all-rotor blade gas turbine, the all-rotor steam turbine, the all-rotor steam gas turbine, the special device, and the water injection device is a large, medium, or small supersonic aircraft. All-blade steam gas turbine combined engine.

The device driven by the output of any one or more of the all-rotating blade gas turbine, the all-rotating blade steam turbine, the all-rotating blade steam gas turbine, the special device, and the water injection device is assumed to be a large-, medium-, and small-sized space shuttle master aircraft. All-blade steam gas turbine combined engine.

A device driven by any one or more of the full-rotor blade gas turbine, the full-rotor blade steam turbine, the full-rotor blade steam gas turbine, the special device, and the water injection device is a large, medium, or small vehicle. All blade steam gas turbine combined engine.

A device driven by any one or more outputs of the full-rotor blade gas turbine, the full-rotor blade steam turbine, the full-rotor blade steam gas turbine, the special device, and the water injection device is a large, medium, or small vehicle. All blade steam gas turbine combined engine.

A device driven by one or more outputs of the full-rotor blade gas turbine, the full-rotor blade steam turbine, the full-rotor steam gas turbine, the special device, and the water injection device is a large, medium, or small machine. All blade steam gas turbine combined engine.

A device driven by any one or more of the full-rotor blade gas turbine, the full-rotor blade steam turbine, the full-rotor steam gas turbine, the special device, and the water injection device is a large, medium, or small ship. All blade steam gas turbine combined engine.

A device driven by any one or more of the full-rotor blade gas turbine, the full-rotor blade steam turbine, the full-rotor steam gas turbine, the special device, and the water injection device is a large, medium, or small tank. All blade steam gas turbine combined engine.

A device driven by any one or more of the all-rotor blade gas turbine, the all-rotor blade steam turbine, the all-rotor steam gas turbine, the special device, and the water injection device is a large, medium, or small fighter. All-blade steam gas turbine combined engine.

A device that is driven by any one or more outputs of the all-rotor steam turbine, the all-rotor steam gas turbine, the special device, and the water injection device; Turbine united engine.

An all-blade steam gas turbine, wherein a device driven by at least one output of the all-blade steam turbine and the all-blade steam gas turbine is a large, medium and small heat, electricity and cold heat supply facility. Coalition organization.

An all-blade steam gas turbine combined engine, characterized in that a device driven by at least one of the outputs of the full-blade steam turbine and the full-blade steam gas turbine is a large and medium and small heat and electricity supply facility. .

An all-rotor steam turbine, wherein the all-rotor steam turbine, the all-rotor steam gas turbine, and a device driven by any one or more of the special equipment and the water injection device are various large, medium and small vessels. Coalition organization.

An all-rotating steam turbine, wherein the all-rotating steam turbine, the all-rotating steam gas turbine, and a device driven by any one or more of the special device and the water injection device are various large, medium and small aircraft. Coalition organization.

An all-rotor steam turbine, wherein the all-rotor steam turbine, the all-rotor steam gas turbine, and a device driven by any one or more of the special device and the water injection device are various large, medium and small vehicles. Coalition organization.

An all-rotating steam turbine, wherein the all-rotating steam turbine, the all-rotating steam gas turbine, and a device driven by any one or more of the special device and the water injection device are various large, medium and small vehicles. Coalition organization.

An all-rotor steam turbine, an all-rotor steam gas turbine, and a device driven by any one or more of the special device and the water injection device; Coalition organization.

An all-rotating steam turbine, wherein the all-rotating steam turbine, the all-rotating steam gas turbine, and a device driven by any one or more of the special device and the water injection device are various large, medium and small ships. Coalition organization.

An all-rotor steam turbine, wherein the all-rotor steam turbine, the all-rotor steam gas turbine, and a device driven by any one or more of the special device and the water injection device are various large, medium and small tanks. Coalition organization.

A device driven by any one or more outputs of the all-blade steam turbine, the all-blade steam gas turbine, the special device, and the water injection device; Turbine united engine.

The fuel to be combusted by the all-blade steam gas turbine combined engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil, heavy oil, pulverized coal, refuse gasified fuel, refuse refined fuel, and combustible materials. An all-blade steam gas turbine combined engine, wherein any one of them is used.

The fuel to be combusted by the all-blade steam gas turbine combined engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil, heavy oil, pulverized coal, refuse gasified fuel, refuse refined fuel, and combustible materials. An all-blade steam gas turbine combined engine, wherein any one of the two types is used.

The fuel to be combusted by the all-blade steam gas turbine combined engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil, heavy oil, pulverized coal, refuse gasified fuel, refuse refined fuel, and combustible materials. An all-blade steam gas turbine combined engine, wherein at least three types are used.

The fuel to be burned in the all-blade steam gas turbine combined engine may be of any type, and is characterized in that it is not limited to the type.

An all-blade steam gas turbine combined engine, which does not matter what kind of device is driven by the output of the all-blade steam gas turbine combined engine.

All blades are characterized in that pollutants such as CO2 are easily synthesized and dissolved in water by mixing a substance to reduce pollution and prevent global warming in water used in the combined steam turbine engine. Steam gas turbine combined engine.

A chemical substance is mixed with water used in the all-blade steam gas turbine combined engine in order to reduce pollution and prevent global warming, thereby easily synthesizing and dissolving a pollutant gas such as CO2 in water. Wing steam gas turbine combined engine.

In order to reduce pollution and prevent global warming, water used in the all-blade steam gas turbine combined engine is mixed with a substance to synthesize and dissolve a pollutant gas such as CO2 into water and discharged. Wing steam gas turbine combined engine.

In order to reduce pollution and prevent global warming, water used in the combined rotor blade steam gas turbine engine is mixed with a chemical substance to synthesize and dissolve a pollutant gas such as CO2 into water and discharge the water. Combined moving blade steam gas turbine engine.

The combined rotor blade steam gas turbine engine uses a water pump and a contra-rotating magnetic friction power transmission device (14a) as a power transmission device.

The turbine blades of the all-blade steam gas turbine combined engine are characterized in that electromagnetic heating is performed at a high temperature to reduce friction loss with water or the like and to perform dynamic pressure reaction drive on the turbine blades. Steam gas turbine combined engine.

The compressor blade of the all-blade steam gas turbine combined engine has good water repellency, reduces friction loss with water or the like, and efficiently compresses and cools the air. Combined moving blade steam gas turbine engine.

The water-repellent cooling blade (87) of the all-blade compressor is made of any one of a water-repellent metal, a coating of a water-repellent substance, a water-repellent ceramic, and a water-repellent process to improve water repellency. All-blade steam gas turbine combined engine.

The water-repellent cooling blade (87) is made of at least one of a water-repellent metal, a coating of a water-repellent substance, a water-repellent ceramic, and a water-repellent processing to improve water repellency. Wing steam gas turbine combined engine.

An all-blade steam gas turbine combined engine, characterized in that supercritical pressure high temperature water (5a) recovered from pulverized coal fuel is supplied to the combustor / heat exchanger 4.

An all-blade steam gas turbine combined engine, wherein high temperature water (5a) recovered from pulverized coal fuel is supplied to the combustor / heat exchanger 4.

A high-pressure water turbine (32a) of the all-blade steam turbine is supplied with supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel.

A high-pressure water turbine (32a) of the full-rotor blade steam turbine is supplied with high-temperature water (5a) recovered from pulverized coal fuel by high-temperature water (5a).

A high-pressure water turbine (32a) of the all-blade steam gas turbine is supplied with supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel.

A combined rotor blade steam gas turbine engine, wherein high temperature water (5a) recovered from pulverized coal fuel is supplied to a high temperature water reservoir (32a) of the all blade steam gas turbine.

An all-blade steam gas turbine combined engine, characterized in that supercritical pressure high-temperature water (5a) recovered from waste gasified fuel is supplied to the combustor / heat exchanger 4.

A high-pressure steam gas turbine combined engine, wherein high temperature water (5a) recovered from waste gasified fuel is supplied to the combustor / heat exchanger 4.

A high-pressure water turbine (32a) of the all-blade steam turbine is supplied with supercritical pressure high-temperature water (5a) recovered from waste gasified fuel.

A high-pressure steam turbine combined engine, wherein high-temperature water (5a) recovered from waste gasified fuel is supplied to the high-temperature water reservoir (32a) of the all-rotor steam turbine.

An all-blade steam gas turbine combined engine, wherein supercritical pressure high-temperature water (5a) recovered from waste gasified fuel is supplied to a high-temperature water reservoir (32a) of the all-blade steam gas turbine.

A combined rotor blade steam gas turbine engine, characterized in that high temperature water (5a) recovered from waste gasified fuel is supplied to a high temperature water reservoir (32a) of the all blade steam gas turbine.

An all-blade steam gas turbine combined engine, characterized in that supercritical pressure high-temperature water (5a) heat-recovered from finely divided fuel is supplied to the combustor / heat exchanger 4.

An all-blade steam gas turbine combined engine, characterized in that high-temperature water (5a) recovered from heat-refined fuel is supplied to the combustor / heat exchanger 4.

A high-pressure water turbine (32a) of the all-blade steam turbine is supplied with supercritical pressure high-temperature water (5a) recovered by heat from finely divided fuel.

A combined rotor blade steam gas turbine engine, characterized in that high temperature water (5a) recovered from heat-refined fuel is supplied to the high temperature water reservoir (32a) of the all blade steam turbine.

A high-pressure water turbine (32a) of the all-blade steam gas turbine is supplied with supercritical pressure high-temperature water (5a) recovered by heat from finely divided fuel.

A high-pressure water turbine (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5a) recovered by heat from dust-reduced fuel.

An all-blade steam gas turbine combined engine, characterized in that the super combustor / heat exchanger 4 is supplied with supercritical high temperature water (5a) obtained by recovering heat from all burnable fuels.

An all-blade steam gas turbine combined engine, characterized in that the combustor / heat exchanger 4 is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels.

An all-blade steam gas turbine combined engine, wherein supercritical pressure high-temperature water (5a) obtained by recovering heat from all combustible fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine.

A high-pressure water turbine (32a) of the full-rotor steam turbine is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels.

An all-blade steam gas turbine combined engine, wherein supercritical pressure high-temperature water (5a) obtained by recovering heat from all combustible fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine.

A combined rotor blade steam gas turbine engine, wherein high temperature water (5a) obtained by recovering heat from all combustible fuel is supplied to the high temperature water reservoir (32a) of the all blade steam gas turbine.

An all-blade steam gas turbine combined engine, wherein the combustor / heat exchanger 4 is supplied with supercritical high-temperature water (5a) recovered from pulverized coal fuel and converted into electric power.

An all-blade steam gas turbine combined engine, wherein high-temperature water (5a) recovered from pulverized coal fuel is supplied to the combustor / heat exchanger 4 to generate electric power.

A high-pressure water turbine (32a) of the all-blade steam turbine is supplied with supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel to generate electric power, and is used as an all-blade steam gas turbine combined engine. .

A high-pressure water turbine (32a) of the full-rotor blade steam turbine is supplied with high-temperature water (5a) recovered from pulverized coal fuel to generate electric power.

A high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from pulverized coal fuel to generate electric power, and the electric power is combined with the all-blade steam gas turbine. organ.

A combined rotor blade steam gas turbine engine, wherein high temperature water (5a) recovered from pulverized coal fuel is supplied to a high temperature water reservoir (32a) of the all blade steam gas turbine to generate electric power.

An all-blade steam gas turbine combined engine characterized in that supercritical pressure high-temperature water (5a) recovered from waste gasified fuel is supplied to the combustor / heat exchanger 4 to generate electric power.

A combined rotor blade steam gas turbine engine characterized in that high temperature water (5a) recovered from waste gasified fuel is supplied to the combustor / heat exchanger 4 to generate electric power.

The high-temperature water sump (32a) of the all-blade steam turbine is supplied with supercritical pressure high-temperature water (5a) recovered from waste gasification fuel and converted into electric power, and is used as electric power. .

A high-pressure water turbine (32a) of the full-rotor steam turbine is supplied with high-temperature water (5a) recovered from waste gasified fuel and turned into electric power, to thereby generate electric power.

A high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical pressure high-temperature water (5a) recovered from waste gasified fuel to generate electric power, and is combined with the all-blade steam gas turbine. organ.

A combined rotor blade steam gas turbine engine, wherein high temperature water (5a) recovered from waste gasified fuel is supplied to a high temperature water reservoir (32a) of the all blade steam gas turbine to generate electric power.

An all-blade steam gas turbine combined engine, characterized in that supercritical pressure high-temperature water (5a) recovered from dust-refined fuel is supplied to the combustor / heat exchanger 4 to generate electric power.

An all-blade steam gas turbine combined engine, wherein high-temperature water (5a) recovered from waste fine fuel is supplied to the combustor / heat exchanger 4 to generate electric power.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical pressure high-temperature water (5a) recovered from heat of finely divided fuel and turned into electric power, and is combined with the all-blade steam gas turbine. organ.

A high-pressure water turbine (32a) of the full-rotor blade steam turbine is supplied with high-temperature water (5a) recovered from heat of dust-reduced fuel to generate electric power, and the electric power is supplied to the all-rotor steam turbine combined engine.

The high-temperature water reservoir (32a) of the all-rotor steam gas turbine is supplied with supercritical pressure high-temperature water (5a) recovered from heat of finely divided fuel to generate electric power. Coalition organization.

A combined rotor blade steam gas turbine engine, wherein high temperature water (5a) recovered from heat of finely divided fuel is supplied to a high temperature water reservoir (32a) of the all blade steam gas turbine to generate electric power.

An all-blade steam gas turbine combined engine, characterized in that supercritical pressure high-temperature water (5a) recovered from all burnable fuel is supplied to the combustor / heat exchanger 4 to generate electric power.

An all-blade steam gas turbine combined engine, characterized in that the combustor / heat exchanger 4 is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels to generate electric power.

A high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from all fuels to be burned, and is turned into electric power. Coalition organization.

A high-pressure water turbine (32a) of the full-rotor blade steam turbine is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels to generate electric power.

A high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) obtained by recovering heat from all fuels to be burned and turned into electric power. Turbine united engine.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels, and is turned into electric power. .

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power and the combustion gas is also compressed by the all-blade compressor to produce the combustor / heat exchanger 4. An all-blade steam gas turbine combined engine characterized by recombustion in an exchanger (4).

The high temperature water (5a) recovered from the pulverized coal fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power and the combustion gas is also compressed by the full blade compressor, and the combustor / heat exchanger 4 is used. An all-blade steam gas turbine combined engine characterized by recombustion at

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine characterized by recombustion in a combustor / heat exchanger 4.

High-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is converted into electric power and the combustion gas is compressed by the all-blade compressor to serve as a combustor. An all-blade steam gas turbine combined engine characterized by recombustion in a heat exchanger 4.

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam gas turbine, and the combustion gas is compressed by the full-blade compressor to generate electric power. An all-blade steam gas turbine combined engine characterized by recombustion in a combustor / heat exchanger (4).

High-temperature water (5a) recovered from pulverized coal fuel is supplied to a high-temperature water reservoir (32a) of the full-blade steam gas turbine, and the combustion gas is compressed by a full-blade compressor to generate electric power. An all-blade steam gas turbine combined engine characterized by recombustion in a heat exchanger (4).

Supercritical pressure high temperature water (5a) recovered from waste gasified fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power, and the combustion gas is also compressed by the full blade compressor so that the combustor / heat exchanger 4 is heated. An all-blade steam gas turbine combined engine characterized by recombustion in an exchanger (4).

The high temperature water (5a) recovered from the waste gasified fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power, and the combustion gas is also compressed by the full blade compressor, and the combustor / heat exchanger 4 is used. An all-blade steam gas turbine combined engine characterized by recombustion at

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from waste gasified fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recombustion in a combustor / heat exchanger 4.

High-temperature water (5a) recovered from waste gasified fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam turbine, and the high-temperature water (5a) is used as electric power, and the combustion gas is compressed by the full-blade compressor to serve as a combustor. An all-blade steam gas turbine combined engine characterized by recombustion in a heat exchanger 4.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from waste gasified fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recombustion in a combustor / heat exchanger (4).

High-temperature water (5a) recovered from waste gasified fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine characterized by recombustion in a heat exchanger (4).

The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5a) recovered from the finely divided fuel and heats it, and the combustion gas is also compressed by a full blade compressor to serve as a combustor / heat exchanger. An all-blade steam gas turbine combined engine characterized by recombustion in a heat exchanger 4.

The combustor / heat exchanger 4 is supplied with high-temperature water (5a) recovered from the dust-refined fuel, and the electric power is used to compress the combustion gas by the full-blade compressor, thereby producing the combustor / heat exchanger 4. 4. A combined turbine and steam turbine combined engine characterized by recombustion at 4.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from dust-reduced fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recombustion in a combustor / heat exchanger (4).

The high-temperature water (32a) of the all-blade steam turbine is supplied with high-temperature water (5a) recovered from the finely divided fuel by heating, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine characterized by recombustion in a heat exchanger (4).

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from the dust-reduced fuel, and the combustion gas is compressed by the all-blade compressor. An all-blade steam gas turbine combined engine, wherein the combined combustion and heat exchanger 4 performs recombustion.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5a) recovered from the finely divided fuel, and the electric power is used to compress the combustion gas by the all-blade compressor for combustion. An all-blade steam gas turbine united engine characterized by recombustion in a heat exchanger / exchanger 4.

The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5a) recovered from all the fuels burned, and is converted into electric power, and the combustion gas is also compressed by a full-blade compressor. An all-blade steam gas turbine combined engine characterized by recombustion in a heat exchanger (4).

The combustor / heat exchanger 4 is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels, and is turned into electric power, and the combustion gas is also compressed by a full-blade compressor to perform combustor / heat exchange. An all-blade steam gas turbine combined engine, wherein recombustion is performed by the steam generator 4.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) obtained by recovering heat from all burning fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine, wherein the combined combustion and heat exchanger 4 performs recombustion.

The high-temperature water (5a) obtained by recovering heat from all the burning fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is converted into electric power and the combustion gas is compressed by the all-blade compressor for combustion. An all-blade steam gas turbine united engine characterized by recombustion in a heat exchanger / exchanger 4.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) obtained by recovering heat from all burnable fuel, and the electric power is converted into the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine, which is compressed and recombusted in a combustor / heat exchanger 4.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels, and the power is converted into electric power to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recombustion in a combustor / heat exchanger 4.

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power and the combustion gas is also compressed by the all-blade compressor to produce the combustor / heat exchanger 4. An all-blade steam gas turbine combined engine characterized by recovering the reheated heat in the exchanger 4 and using it normally.

The high temperature water (5a) recovered from the pulverized coal fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power and the combustion gas is also compressed by the full blade compressor, and the combustor / heat exchanger 4 is used. An all-blade steam gas turbine combined engine characterized by recovering reheat heat and using it normally.

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the combustor / heat exchanger 4 and using it normally.

High-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is converted into electric power and the combustion gas is compressed by the all-blade compressor to serve as a combustor. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the heat exchanger 4 and using it normally.

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam gas turbine, and the combustion gas is compressed by the full-blade compressor to generate electric power. An all-blade steam gas turbine combined engine characterized by recovering the reburned heat in the combustor / heat exchanger 4 for normal use.

High-temperature water (5a) recovered from pulverized coal fuel is supplied to a high-temperature water reservoir (32a) of the full-blade steam gas turbine, and the combustion gas is compressed by a full-blade compressor to generate electric power. An all-blade steam gas turbine combined engine, wherein the combined heat and heat is recovered by a heat exchanger 4 and is normally used.

Supercritical pressure high temperature water (5a) recovered from waste gasified fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power, and the combustion gas is also compressed by the full blade compressor so that the combustor / heat exchanger 4 is heated. An all-blade steam gas turbine combined engine characterized by recovering the reheated heat in the exchanger 4 and using it normally.

The high temperature water (5a) recovered from the waste gasified fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power, and the combustion gas is also compressed by the full blade compressor, and the combustor / heat exchanger 4 is used. An all-blade steam gas turbine combined engine characterized by recovering reheat heat and using it normally.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from waste gasified fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the combustor / heat exchanger 4 and using it normally.

High-temperature water (5a) recovered from waste gasified fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam turbine, and the high-temperature water (5a) is used as electric power, and the combustion gas is compressed by the full-blade compressor to serve as a combustor. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the heat exchanger 4 and using it normally.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from waste gasified fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recovering the reburned heat in the combustor / heat exchanger 4 for normal use.

High-temperature water (5a) recovered from waste gasified fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine, wherein the combined heat and heat is recovered by a heat exchanger 4 and is normally used.

The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5a) recovered from the finely divided fuel and heats it, and the combustion gas is also compressed by a full blade compressor to serve as a combustor / heat exchanger. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the heat exchanger 4 and using it normally.

The combustor / heat exchanger 4 is supplied with high-temperature water (5a) recovered from the dust-refined fuel, and the electric power is used to compress the combustion gas by the full-blade compressor, thereby producing the combustor / heat exchanger 4. 4. An all-blade steam gas turbine united engine characterized by recovering the reheated heat in 4 and using it normally.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from dust-reduced fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recovering the reburned heat in the combustor / heat exchanger 4 for normal use.

The high-temperature water (32a) of the all-blade steam turbine is supplied with high-temperature water (5a) recovered from the finely divided fuel by heating, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine, wherein the combined heat and heat is recovered by a heat exchanger 4 and is normally used.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from the dust-reduced fuel, and the combustion gas is compressed by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recovering the reburned heat in the combustor / heat exchanger 4 for normal use.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5a) recovered from the finely divided fuel, and the electric power is used to compress the combustion gas by the all-blade compressor for combustion. An all-blade steam gas turbine combined engine characterized by recovering the reheated heat in the heat exchanger 4 and using it normally.

The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5a) recovered from all the fuels burned, and is converted into electric power, and the combustion gas is also compressed by a full-blade compressor. An all-blade steam gas turbine combined engine, wherein the combined heat and heat is recovered by a heat exchanger 4 and is normally used.

The combustor / heat exchanger 4 is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels, and is turned into electric power, and the combustion gas is also compressed by a full-blade compressor to perform combustor / heat exchange. An all-blade steam gas turbine combined engine characterized by recovering the reheated heat in the unit 4 and using it normally.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) obtained by recovering heat from all burning fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine united engine characterized by recovering the reburned heat in the combustor / heat exchanger 4 for normal use.

The high-temperature water (5a) obtained by recovering heat from all the burning fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is converted into electric power and the combustion gas is compressed by the all-blade compressor for combustion. An all-blade steam gas turbine combined engine characterized by recovering the reheated heat in the heat exchanger 4 and using it normally.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) obtained by recovering heat from all burnable fuel, and the electric power is converted into the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by being compressed and reheated by a combustor / heat exchanger 4 to recover the heat for normal use.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels, and the power is converted into electric power to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the combustor / heat exchanger 4 and using it normally.

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power and the combustion gas is also compressed by the all-blade compressor to produce the combustor / heat exchanger 4. An all-blade steam gas turbine combined engine, wherein reheated heat is recovered by the exchanger 4 and used for auxiliary use.

The high temperature water (5a) recovered from the pulverized coal fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power and the combustion gas is also compressed by the full blade compressor, and the combustor / heat exchanger 4 is used. An all-blade steam gas turbine combined engine characterized by recovering reheat heat and using it as an auxiliary.

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine, wherein recombustion heat is recovered by a combustor / heat exchanger 4 and used for auxiliary use.

High-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is converted into electric power and the combustion gas is compressed by the all-blade compressor to serve as a combustor. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the heat exchanger 4 and using it as an auxiliary.

Supercritical pressure high-temperature water (5a) recovered from pulverized coal fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam gas turbine, and the combustion gas is compressed by the full-blade compressor to generate electric power. An all-blade steam gas turbine combined engine, wherein recombustion heat is recovered by a combustor / heat exchanger 4 and used as auxiliary.

High-temperature water (5a) recovered from pulverized coal fuel is supplied to a high-temperature water reservoir (32a) of the full-blade steam gas turbine, and the combustion gas is compressed by a full-blade compressor to generate electric power. An all-blade steam gas turbine combined engine, wherein the combined heat and heat is recovered by a heat exchanger 4 and used for auxiliary use.

Supercritical pressure high temperature water (5a) recovered from waste gasified fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power, and the combustion gas is also compressed by the full blade compressor so that the combustor / heat exchanger 4 is heated. An all-blade steam gas turbine combined engine, wherein reheated heat is recovered by the exchanger 4 and used for auxiliary use.

The high temperature water (5a) recovered from the waste gasified fuel is supplied to the combustor / heat exchanger 4, and the combustion gas is converted into electric power, and the combustion gas is also compressed by the full blade compressor, and the combustor / heat exchanger 4 is used. An all-blade steam gas turbine combined engine characterized by recovering reheat heat and using it as an auxiliary.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from waste gasified fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine, wherein recombustion heat is recovered by a combustor / heat exchanger 4 and used for auxiliary use.

High-temperature water (5a) recovered from waste gasified fuel is supplied to the high-temperature water reservoir (32a) of the full-blade steam turbine, and the high-temperature water (5a) is used as electric power, and the combustion gas is compressed by the full-blade compressor to serve as a combustor. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the heat exchanger 4 and using it as an auxiliary.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from waste gasified fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine, wherein recombustion heat is recovered by a combustor / heat exchanger 4 and used as auxiliary.

High-temperature water (5a) recovered from waste gasified fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam gas turbine, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine, wherein the combined heat and heat is recovered by a heat exchanger 4 and used for auxiliary use.

The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5a) recovered from the finely divided fuel and heats it, and the combustion gas is also compressed by a full blade compressor to serve as a combustor / heat exchanger. An all-blade steam gas turbine combined engine characterized by recovering reheated heat in the heat exchanger 4 and using it as an auxiliary.

The combustor / heat exchanger 4 is supplied with high-temperature water (5a) recovered from the dust-refined fuel, and the electric power is used to compress the combustion gas by the full-blade compressor, thereby producing the combustor / heat exchanger 4. 4. An all-blade steam gas turbine combined engine characterized by recovering the reburning heat in 4 and using it as an auxiliary.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from dust-reduced fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine, wherein recombustion heat is recovered by a combustor / heat exchanger 4 and used as auxiliary.

The high-temperature water (32a) of the all-blade steam turbine is supplied with high-temperature water (5a) recovered from the finely divided fuel by heating, and the combustion gas is compressed by the all-blade compressor to generate electric power. An all-blade steam gas turbine combined engine, wherein the combined heat and heat is recovered by a heat exchanger 4 and used for auxiliary use.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) recovered from the dust-reduced fuel, and the combustion gas is compressed by the all-blade compressor. An all-blade steam gas turbine combined engine, wherein recombustion heat is recovered by a combustor / heat exchanger 4 for auxiliary use.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5a) recovered from the finely divided fuel, and the electric power is used to compress the combustion gas by the all-blade compressor for combustion. An all-blade steam gas turbine combined engine, wherein reburning heat is recovered by the heat exchanger 4 for auxiliary use.

The combustor / heat exchanger 4 is supplied with supercritical pressure high-temperature water (5a) recovered from all the fuels burned, and is converted into electric power, and the combustion gas is also compressed by a full-blade compressor. An all-blade steam gas turbine combined engine, wherein the combined heat and heat is recovered by a heat exchanger 4 and used for auxiliary use.

The combustor / heat exchanger 4 is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels, and is turned into electric power, and the combustion gas is also compressed by a full-blade compressor to perform combustor / heat exchange. An all-blade steam gas turbine combined engine, wherein reburning heat is recovered by the heat exchanger 4 and used as auxiliary.

The high-temperature water reservoir (32a) of the all-blade steam turbine is supplied with supercritical-pressure high-temperature water (5a) obtained by recovering heat from all burning fuel, and the electric power is used to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine, wherein recombustion heat is recovered by a combustor / heat exchanger 4 for auxiliary use.

The high-temperature water (5a) obtained by recovering heat from all the burning fuel is supplied to the high-temperature water reservoir (32a) of the all-blade steam turbine, and the combustion gas is converted into electric power and the combustion gas is compressed by the all-blade compressor for combustion. An all-blade steam gas turbine combined engine, wherein reburning heat is recovered by the heat exchanger 4 for auxiliary use.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with supercritical-pressure high-temperature water (5a) obtained by recovering heat from all burnable fuel, and the electric power is converted into the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine, which compresses and recovers reheated heat in a combustor / heat exchanger 4 for auxiliary use.

The high-temperature water reservoir (32a) of the all-blade steam gas turbine is supplied with high-temperature water (5a) obtained by recovering heat from all burnable fuels, and the power is converted into electric power to compress the combustion gas by the all-blade compressor. An all-blade steam gas turbine combined engine, wherein recombustion heat is recovered by a combustor / heat exchanger 4 and used for auxiliary use.

The combined rotor blade steam gas turbine engine is characterized in that the injection-propelled all-blade steam gas turbine performs injection and propulsion by increasing the mass velocity of the injected high-temperature water and combustion gas including the air suction force.

The all-wheel-steam steam turbine combined engine, wherein the injection-propelled all-blade steam turbine is propelled by increasing the mass velocity of the injected high-temperature water including the air suction force.

The above-mentioned all-blade steam gas turbine for jet-propulsion is characterized in that the jet-propulsion is performed by increasing the mass velocity of the high-temperature water and the combustion gas including the air suction force of the spraying principle 91a. organ.

The combined blade / steam gas turbine combined engine is characterized in that the injected / propelled all blade steam turbine performs the injection / propulsion by increasing the mass velocity of the injected high-temperature water including the air suction force of the principle of spraying 91a.

The above-described all-swing blade steam gas turbine is characterized in that the all-swing blade steam gas turbine performs the injection and propulsion by increasing the mass velocity of the injected high-temperature water and combustion gas including the air suction force of the spraying principles 91a and 91b. Turbine united engine.

The above-described all-rotating blade steam turbine is characterized in that the all-rotating blade steam turbine is configured to perform injection and propulsion by increasing the mass velocity of high-temperature water to be injected and combustion gas including the air suction force of the principle of spraying 91a and 91b. Coalition organization.

The all-blade steam gas turbine, wherein the jet-propelled all-blade steam gas turbine is characterized in that the jet-propulsion is performed by lifting the hull by increasing the mass velocity of the injected high-temperature water and combustion gas including the air suction force. organ.

The combined rotor blade steam gas turbine engine, wherein the all-rotor blade steam turbine for jetting and propelling lifts and injects the hull by increasing the mass velocity of the injected high-temperature water including the air suction force.

The above-described all-blade steam gas turbine is characterized in that the all-blade steam gas turbine is jet-propelled by increasing the mass velocity of the high-temperature water to be injected and the combustion gas including the water suction force of the principle of spraying 91c and 91d. Turbine united engine.

The all-wheel-steam steam turbine for jet-propulsion is characterized in that injection and propulsion are performed by increasing the mass velocity of the injected high-temperature water including the water suction force of the spraying principle 91c and 91d.

The above-mentioned all-blade steam gas turbine for jet-propulsion is characterized in that the jet-propulsion is performed by increasing the mass velocity of the high-temperature water to be injected and the combustion gas including the water suction force based on the principle of spraying 91c. organ.

The above-mentioned all-blade steam turbine for jet-propulsion is characterized in that the jet-propulsion is performed by increasing the mass velocity of the high-temperature water to be injected and the combustion gas including the water suction force based on the principle of spraying 91d. .

The above-described all-rotating steam turbine that performs the injection propulsion is characterized in that the fuel loading is significantly reduced by increasing the mass velocity of the injection high-temperature water including the air suction force and the combustion gas, and the injection and propulsion is performed. Steam gas turbine combined engine.

The above-mentioned all-blade steam turbine for jet propulsion is characterized in that fuel injection is drastically reduced by increasing the mass velocity of the injected high-temperature water including the air suction force, and the jet-propulsion is performed. organ.

The all-rotating blade steam gas turbine that performs the injection propulsion is characterized in that the injection load is drastically reduced by increasing the mass velocity of the injection high-temperature water and the combustion gas including the air suction force of the spraying principle 91a, thereby performing the injection propulsion. All-blade steam gas turbine combined engine.

The jet-propelled all-blade steam turbine performs jet-propulsion by drastically reducing the fuel loading amount by increasing the mass velocity of the injected high-temperature water including the air suction force of the principle of spraying 91a. Wing steam gas turbine combined engine.

The above-mentioned all-blade steam gas turbine for injection propulsion is required to increase the mass velocity of high-temperature injection water and combustion gas including the air suction force of the spraying principle 91a / 91b, thereby drastically reducing the fuel loading and propulsion. An all-blade steam gas turbine combined engine characterized by the following.

The all-rotating blade steam turbine that performs the injection propulsion is capable of performing the injection propulsion by drastically reducing the fuel load by increasing the mass velocity of the injection high-temperature water and the combustion gas including the air suction force of the spraying principles 91a and 91b. All-blade steam gas turbine combined engine.

The above-described all-rotating blade steam gas turbine is characterized in that the hull is lifted by increasing the mass velocity of the high-temperature water and the combustion gas including the air suction force, thereby drastically reducing the fuel load and performing the fuel injection. All-blade steam gas turbine combined engine.

The all-rotating blade steam turbine for injection propulsion is characterized in that the jet propulsion is performed by raising the hull by increasing the mass velocity of the injected high-temperature water including the air suction force to greatly reduce the fuel loading amount. Wing steam gas turbine combined engine.

The all-rotating blade steam gas turbine that performs the injection propulsion is capable of performing the injection propulsion by drastically reducing the fuel loading amount by increasing the mass velocity of the injection high-temperature water and the combustion gas including the water suction force of the spraying principle 91c and 91d. An all-blade steam gas turbine combined engine characterized by the following.

The injection-propelled all-blade steam turbine is characterized in that the fuel loading is significantly reduced by the increase in the mass velocity of the injected high-temperature water including the water suction force of the spraying principles 91c and 91d, and the fuel is propelled. All blade steam gas turbine combined engine.

The jet-propelled all-blade steam gas turbine is characterized in that the fuel loading is significantly reduced by the increase in the mass velocity of the injected high-temperature water and the combustion gas including the water suction force of the spraying principle 91c, and the fuel is injected and propelled. All-blade steam gas turbine combined engine.

The injection-propelled all-blade steam turbine is characterized in that the fuel loading is drastically reduced by the increase in the mass velocity of the injected high-temperature water and the combustion gas including the water suction force of the spraying principle 91d, and the fuel is injected and propelled. All-blade steam gas turbine combined engine.

The injection-propelled all-blade steam gas turbine is characterized in that the fuel loading is significantly reduced by increasing the mass velocity of the injected high-temperature water and combustion gas including the air suction force, and the fuel is propelled very safely. All-blade steam gas turbine combined engine.

The all-rotating blade steam turbine for injecting and propelling is characterized in that the fuel loading is drastically reduced by increasing the mass velocity of the injected high-temperature water including the air suction force, thereby injecting and propelling very safely. Steam gas turbine combined engine.

The above-described all-blade steam gas turbine for jet propulsion is very safely jet-propelled by increasing the mass velocity of high-temperature water and combustion gas including the air suction force of the atomizing principle 91a to greatly reduce the fuel load. All-blade steam gas turbine combined engine characterized by the following.

The injection-propelled all-blade steam turbine 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 of the spraying principle 91a, and the fuel is propelled very safely. All-blade steam gas turbine combined engine.

The all-wheel steam gas turbine that promotes the injection is very safe by greatly reducing the fuel load by increasing the mass velocity of the injected high-temperature water and combustion gas including the air suction force of the atomizing principle 91a and 91b. An all-blade steam gas turbine combined engine characterized by injection propulsion.

The above-mentioned all-blade steam turbine that promotes the injection is extremely safe in injection by drastically reducing the fuel load by increasing the mass velocity of the injection high-temperature water and the 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.

The above-mentioned jet-propelled all-blade steam gas turbine has a very low fuel load by floating the hull by increasing the mass velocity of the injected high-temperature water and combustion gas, including the air suction force, so that the fuel load is greatly reduced. All-blade steam gas turbine combined engine characterized by the following.

The all-rotating bladed steam turbine that injects and propells is capable of injecting and propelling very safely by increasing the mass velocity of the injected high-temperature water including the air suction force to lift the hull and greatly reduce the fuel load. All-blade steam gas turbine combined engine.

The above-mentioned all-blade steam gas turbine that promotes the injection is very safe by greatly reducing the fuel load by increasing the mass velocity of the injected 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 injection propulsion.

The above-described all-rotating bladed steam turbine is capable of injecting fuel very safely by drastically reducing the fuel load by increasing the mass velocity of injected high-temperature water including the water suction force of the spraying principle 91c and 91d. An all-blade steam gas turbine combined engine characterized by the following.

The jet-propelled all-blade steam gas turbine is very safe in fuel injection by greatly increasing the mass velocity of high-temperature water and combustion gas, including the water suction force of the spraying principle 91c, to greatly reduce the fuel load. An all-blade steam gas turbine combined engine characterized in that:

The injection-propelled all-blade steam turbine performs very safe injection propulsion by increasing the mass velocity of the injected high-temperature water and combustion gas, including the water suction force of the spraying principle 91d, to greatly reduce the fuel load. An all-blade steam gas turbine combined engine, characterized in that:

An all-blade steam gas turbine combined engine, wherein tap water is used as cooling water for the vaporizing latent heat recovery device (66a).

An all-blade steam gas turbine combined engine, wherein tap water is used as cooling water for the vaporizing latent heat recovery device (66a) to store and supply warm heat to a customer.

An all-blade steam gas turbine combined engine, wherein tap water is used as cooling water for the vaporizing latent heat recovery device (66a) to store it and supply a heat near 100 ° C to a customer.

An all-blade steam gas turbine combined engine, wherein tap water is used as cooling water for the vaporizing latent heat recovery device (66a), and hot water of 100 ° C. or less is supplied to a customer.

An all-blade steam gas turbine combined engine, wherein all condensed water of the vaporizing latent heat recovery unit (66a) is supplied to a combustor / heat exchanger (4) to become supercritical pressure high temperature water (5a).

An all-blade steam gas turbine combined engine, wherein all condensed water of the vaporizing latent heat recovery unit (66a) is supplied to a combustor / heat exchanger (4) to produce high-temperature water (5a).

Supplying all of the condensed water from the vaporizing latent heat recovery unit (66a) to the combustor / heat exchanger (4) to reduce the amount of fuel supplied to the vaporizing latent heat to reduce it to supercritical pressure high-temperature water (5a). All-blade steam gas turbine combined engine.

All of the condensed water of the vaporizing latent heat recovery unit (66a) is supplied to the combustor / heat exchanger (4) to reduce the amount of heat supplied to the fuel by approaching the vaporizing latent heat to produce high-temperature water (5a). All blade steam gas turbine combined engine.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water and the like are aggregated with the low-temperature combustion gas as a nucleus and collected as water droplets, and the tap water is cooled and stored. An all-blade steam gas turbine combined engine characterized by completely eliminating the use of commercial and domestic coolers by supplying it to consumers and eliminating global warming by removing Freon.

In the all-blade steam gas turbine combined engine that brings the combustion gas exhaust temperature close to -273 ° C, water and the like are aggregated with the low-temperature combustion gas as a nucleus and collected as water droplets, and the tap water is cooled and stored. An all-blade steam gas turbine combined engine characterized by supplying cooling water to customers and cooling the entire urban area to prevent global warming by removing CFCs.

In an all-blade steam gas turbine united engine that brings the combustion gas exhaust temperature close to -273 ° C, water and the like are aggregated using low-temperature combustion gas as a core and collected as water droplets, and tap water is cooled to around 5 ° C. An all-blade steam gas turbine combined engine characterized by completely eliminating the use of commercial and household coolers by storing and supplying them to consumers, and preventing global warming by removing Freon.

In an all-blade steam gas turbine united engine that brings the combustion gas exhaust temperature close to -273 ° C, water and the like are aggregated using low-temperature combustion gas as a core and collected as water droplets, and tap water is cooled to around 5 ° C. An all-blade steam gas turbine combined engine characterized by storing, storing and supplying it to consumers to cool the entire urban area and prevent global warming by removing Freon.