JP2012207596A - Various energy conservation cycle combined engine - Google Patents
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本発明は理論最良エンジン発明のため色々な実験が必要ですが、既存最良蒸気タービン発電の大気圧同速度同容積仕事率kg重m/秒が、横型全動翼水重力タービン8P発電の1/1700と僅少や、ボイラや原子炉など燃料費や危険が膨大に加えて、蒸気速度を堰止めて仕事皆無静翼を動翼と交互に半分具備して回転出力を0に近付け、発電熱量全部で海水温度を7度上昇海面全部温度上昇して自然現象を不可能にし、上限の無い地震津波の巨大化や、異常気象を増大50年前後海水の豪雨等で人類絶滅に近付く危険や、緑の地球は奇跡の産物で他の星に近付く危険が大きく人類絶滅を阻止する技術として、横型全動翼水重力タービン8P燃料費0発電とし、大気圧同速度同容積仕事率を既存蒸気タービン発電の1700倍水仕事率発電にし、ボイラや原子炉全廃の燃料費0発電として、8P発電電気駆動の1〜複数段熱ポンプ1Gや太陽光加熱器2とし、太陽光加熱の空気を圧縮高温として、1〜複数段圧縮熱回収器2Cで熱回収分割保存供給する熱製造にし、50〜200MPa過熱蒸気50温熱+液体空気28a冷熱に分割保存して、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dとし、船舶や車両や飛行機には液体酸素や液体窒素等て供給して、圧縮仕事率を既存往復機関の1/600に圧縮圧力20倍容易にし、船舶駆動では自然現象高速化2a海水に窒素や酸素やCO2を供給微生物や海草類増大して、食物連鎖等で魚類等人類の食料を大増大し、飛行機や自動車駆動ではCO2排気1/10や燃料費1/10や1/50万経費宇宙到達狙い等、飛行機や船舶は10倍速度狙い等、各種エネルギ保存サイクル合体機関や各種エネルギ保存合体方法の技術に関する。 Although the present invention requires various experiments for the theoretical best engine invention, the existing best steam turbine power generation has the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / sec. In addition to 1700, fuel costs and dangers such as boilers and nuclear reactors are enormous, the steam speed is dammed, the workless blades are alternately half-rotated and the rotating power is brought close to 0, and the total amount of heat generated The sea temperature rises by 7 degrees, making the whole sea surface warm, making natural phenomena impossible, increasing the unprecedented seismic tsunami, increasing abnormal weather, the danger of approaching human extinction due to heavy rains of seawater around 50 years, The Earth's earth is a miracle product and has a great risk of approaching other stars, and as a technology to prevent human extinction, the horizontal full-blade water gravity turbine 8P fuel cost 0 power generation, the atmospheric pressure, the same speed, and the same volumetric power, the existing steam turbine power generation 1700 times water power generation , Boiler and nuclear reactor abolition fuel cost 0 power generation, 8P power generation electric drive 1-multiple stage heat pump 1G and solar heater 2 The heat production is divided and stored and supplied by the vessel 2C, divided into 50 to 200 MPa superheated steam 50 heat + liquid air 28a cold and stored as electricity + liquid air cold + superheated steam heat supply equipment 3D, and used for ships, vehicles and airplanes Is supplied with liquid oxygen, liquid nitrogen, etc., making the compression work rate 1/600 of the existing reciprocating engine, and the compression pressure is 20 times easier. Ship driving increases the natural phenomenon 2a Nitrogen, oxygen and CO2 are supplied to seawater And seaweeds, fish and other human foods are greatly increased in the food chain, etc. Airplanes and ships are driven by planes and automobiles, such as 1/10 CO2 exhaust, 1 / 10th fuel cost and 1 / 500,000 cost, aiming to reach space. Is 1 Double-speed aim, etc., related to technology of various energy conservation cycle union organizations and various energy conservation combined method.
既存世界最多の自動車駆動往復機関は空気圧縮で膨大な燃料消費しており、熱効率無限大の横型全動翼水重力タービン8P真空中水重力加速度発電電気駆動の、電気+液体空気冷熱+過熱蒸気温熱供給設備1Aより、液体酸素室5Kや液体窒素室5Lに液体空気を受給し、液体酸素や液体窒素や水の圧縮にして、圧縮仕事率を1/600や1/1700にして200MPa超高圧圧縮を容易にし、液体酸素室5Kや液体窒素室5Lより高圧高温燃焼ガス室5Mに200MPa等噴射して、同様に燃料噴射着火燃焼を継続200MPa等を維持し、内周や外周過熱蒸気室50の200MPa水や液体窒素を加熱することで燃焼量増大して、燃焼ガス室5M内液体窒素や水噴射でも燃焼量を増大し、圧力機関1B駆動室の燃焼ガス室5Mや水蒸気室50の高圧高温を維持することで、多数の各種ポンプや各種圧縮機を夫々液体酸素超高圧噴射燃料噴射燃焼駆動する、多段圧力機関1B各種例えば多段酸素圧力歯車機関3Z+多段水圧力歯車機関3Nや、多段酸素圧力往復機関3F+多段水圧力往復機関3Mの連動等として、多段酸素圧力機関1B駆動の過程で複数回燃料噴射燃焼液体窒素や水噴射して燃焼温度最適にし、外周や内周の200MPa水蒸気や窒素を加熱多段水圧力機関1B駆動して、多段酸素圧力機関1Bに連動の過程で水噴射や液体窒素噴射で最適圧力温度にし、用途により多段酸素圧力機関1B単独使用も可能して、自動車や耕耘機等各種車両類やプロペラ7Aや回転翼7Bやスクリュウ7C駆動し、排気の過程で各種噴射推進との合体を選択可能として、利益率抜群世界一狙う、各種エネルギ保存サイクル合体機関及び合体方法の技術に関する。 The world's largest automobile-driven reciprocating engine consumes enormous amount of fuel due to air compression, and is a horizontal all-blade water gravity turbine with infinite thermal efficiency. Liquid air is received from the heat supply facility 1A into the liquid oxygen chamber 5K and the liquid nitrogen chamber 5L, and compressed into liquid oxygen, liquid nitrogen, and water, and the compression power is reduced to 1/600 or 1/1700, and the pressure exceeds 200 MPa. Compression is facilitated, and 200 MPa or the like is injected into the high-pressure and high-temperature combustion gas chamber 5M from the liquid oxygen chamber 5K or the liquid nitrogen chamber 5L, and the fuel injection ignition combustion is continuously maintained at 200 MPa or the like. The 200 MPa water or liquid nitrogen is heated to increase the combustion amount, and the combustion amount is increased by the liquid nitrogen or water injection in the combustion gas chamber 5M, and the combustion gas chamber 5M or water vapor in the pressure engine 1B driving chamber is increased. By maintaining the high pressure and high temperature of 50, a variety of multistage pressure engines 1B, such as a multistage oxygen pressure gear engine 3Z + a multistage water pressure gear engine 3N, which drive a number of various pumps and various compressors, respectively, are driven by liquid oxygen ultra-high pressure injection fuel injection combustion As an interlock between the multistage oxygen pressure reciprocating engine 3F and the multistage water pressure reciprocating engine 3M, the combustion temperature is optimized by injecting the fuel liquid combustion nitrogen and water several times in the process of driving the multistage oxygen pressure engine 1B. Steam and nitrogen are heated to drive the multi-stage water pressure engine 1B, and in the process linked to the multi-stage oxygen pressure engine 1B, water injection and liquid nitrogen injection are used to achieve the optimum pressure temperature. Depending on the application, the multi-stage oxygen pressure engine 1B can be used alone. Various vehicles such as automobiles and tillers, propellers 7A, rotor blades 7B and screws 7C can be driven and combined with various injection propulsion can be selected in the exhaust process. Aiming the world, it relates to a technology of various energy conservation cycle combined institutions and coalescence method.
既存ジェット機ガスタービンも蒸気タービンと略同様に、回転出力や噴射圧力を静翼で0側に近付け噴射推進出力を僅少とし、空気抵抗01日に地球を16周等宇宙飛行が不可能なため、宇宙ロケットを遥かに超える液体合体噴射部80噴射推進として、水重力発電電気駆動多数の1〜複数段熱ポンプ1G+太陽光加熱器2熱製造により、50〜200MPa大質量の過熱蒸気温熱50+液体空気冷熱28aに分割保存し、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して例えば過熱蒸気は、永久凍土地下や海底のメタンハイドレートに注入、メタンと高温水に分割メタンは液体窒素冷却液体メタンで回収として、飛行機や車両や船舶も前記自動車と同様に液体空気28a駆動とし、液体酸素室5K+液体窒素室5Lに受給し、高圧高温燃焼ガス室5M内燃焼で内周外周の高圧高温水蒸気室5N水蒸気を加熱して、高圧高温燃焼ガス49や高圧高温水蒸気50を製造し、液体合体噴射部80燃焼ガス制御弁24開放して、複数段燃焼室1Y高圧高温燃焼ガス室5Mに高圧高温燃焼ガス49を供給し、燃料制御弁25b開放して5M内燃料噴射燃焼して、水蒸気制御弁5P開放高圧高温水蒸気室5Nに水蒸気噴射して5Mにより1段加熱し、同様に2段燃焼や複数段燃焼して2段加熱や複数段加熱噴射して、燃焼ガス49や水蒸気50を50〜200MPa噴射前方の空気を吸引噴射し、宇宙到達費用を既存の1/50万狙いにして、燃料費0に近い宇宙飛行で1日に地球を16周する等地球上何処でも日帰り旅行を可能にし、各種宇宙往還飛行機類で利益率抜群世界一狙う、各種エネルギ保存サイクル合体機関及び合体方法の技術に関する。 The existing jet gas turbine is almost the same as the steam turbine, and the rotation output and injection pressure are approached to the zero side with a stationary blade, and the injection propulsion output is made small. As a propulsion propulsion of the liquid merging jet 80 that far exceeds the space rocket, water gravity power generation electric drive many 1 to multi-stage heat pump 1G + solar heater 2 heat production, 50-200MPa large mass superheated steam temperature 50 + liquid air Divided and stored in cold heat 28a, received from electricity + liquid air cold heat + superheated steam temperature supply facility 3D, for example, superheated steam is injected into methane hydrate under permafrost and underwater, split into methane and hot water, methane is liquid nitrogen As recovered by cooling liquid methane, airplanes, vehicles and ships are also driven by liquid air 28a as in the case of the automobile, and received in the liquid oxygen chamber 5K + liquid nitrogen chamber 5L. The high-pressure high-temperature steam chamber 5N on the inner periphery is heated by combustion in the high-pressure high-temperature combustion gas chamber 5M to produce the high-pressure high-temperature combustion gas 49 and the high-pressure high-temperature steam 50, and the liquid coalescence injection unit 80 combustion gas control valve 24 is opened. Then, the high-pressure high-temperature combustion gas 49 is supplied to the multistage combustion chamber 1Y high-pressure high-temperature combustion gas chamber 5M, the fuel control valve 25b is opened and the fuel is injected and burned in 5M, and the water-vapor control valve 5P is opened to the high-pressure high-temperature steam chamber 5N. Inject and heat 1 stage with 5M, and similarly 2-stage combustion and multi-stage combustion, 2-stage heating and multi-stage heat injection, combustion gas 49 and water vapor 50 are injected 50 to 200 MPa in front of the air , Aiming for space arrival costs of 1 / 500,000, and making a day trip anywhere on the earth, such as making 16 orbits of the earth a day with a space flight close to zero fuel cost, and profitability on various space return planes The best in the world Cormorants, relates to a technology of various energy conservation cycle combined institutions and coalescence method.
既存船舶は蒸気タービンやガスタービンや更に低性能エンジンを使用し、回転出力や噴射推進出力を僅少として、低速移動に膨大な燃料を消費しているため、前記自動車駆動と同様に多段圧力機関1B駆動してスクリュウ船舶39D駆動して、前記液体合体噴射部80と略同様に液体ウォータージェット80を駆動し、前方の水や空気を吸引噴射して水を吸引噴射して、吸引空気流複数個所にも燃料噴射燃焼を選択可能にし、既存船舶速度の10倍速度や1/10燃料費狙いとして、スクリュウ推進排気の過程では簡単ウォータージェット80噴射推進追加し、噴射推進の過程で自然現象高速化して海中に酸素や窒素やCO2等を供給して、微生物や植物プランクトンや海草類やサンゴや魚類等を増殖人類の食物を増大し、熱効率利益率抜群世界一狙う、各種エネルギ保存サイクル合体機関及び合体方法の技術に関する。 Existing ships use steam turbines, gas turbines, and even lower performance engines, and have a small amount of rotational output and injection propulsion output, and consume a huge amount of fuel for low-speed movement. Drive the screw ship 39D to drive the liquid water jet 80 in substantially the same manner as the liquid coalescing and jetting unit 80, sucking and jetting water and air in front and sucking and jetting water. In addition, fuel injection combustion can be selected, and a simple water jet 80 injection propulsion is added in the process of screw propulsion and exhaust, and natural phenomena are accelerated in the process of injection propulsion, aiming at 10 times the existing ship speed and 1/10 fuel cost. By supplying oxygen, nitrogen, CO2, etc. into the sea, the microorganisms, phytoplankton, seaweeds, corals, fish, etc. can be increased to increase human food, and the thermal efficiency profit rate is outstanding Field one aim, relates to a technology of various energy conservation cycle combined institutions and coalescence method.
洗脳皆無の小学校理科で考えると、既存最良蒸気タービン発電の大気圧同速度同容積仕事率kg重m/秒が、横型全動翼水重力タービン8P仕事率の1/1700と僅少に加えて、蒸気速度を堰止めて仕事皆無の静翼を動翼と交互に半分具備して、回転出力を0側に近付けており、何故全動翼にしないのか大疑問に加えて、発電熱量全部で海水温度を7度上昇して海面全部を温度上昇自然現象不可能にし、上限の無い異常気象を増大し、50〜100年前後海水の豪雨等で人類が絶滅に近付く危険を増大中です。緑の地球は奇跡の産物で他の星に近付く危険が大きく、発電所側説明では海水温度上昇が7度以下なら環境に影響皆無としておりますが、例えば海水温度が30度の海域で7度上昇を継続すると、台風風速が300m/秒等になり海水の集中豪雨塩の被覆等で人類が絶滅する危険や、海面全部温度上昇して冬場に海面冷却海底に窒素や酸素やCO2等の栄養分を供給していた自然現象を不可能にし、海中微生物や植物プランクトンや海草類を激減魚類等人類の海中食物も限り無く激減しており、中国が10%成長を続けると、海水温度上昇量は10年で現在の2倍20年で4倍と加速度的に増大して、最悪予想では台風や季節風や海上竜巻の風速が100m/秒等となり、海水を上空に吸引海水の集中豪雨として日本の農業や林業や居住地域が0に近付く等、50年前後で人類絶滅が急接近するため、手遅れ前に既存技術最悪部分に対応した技術開発が必要。 Considering the elementary school science without brainwashing, the existing best steam turbine power generation at the same pressure and volumetric capacity kg kg m / sec is a little less than 1/1700 of the horizontal all-blade water gravity turbine 8P power, The steam speed is blocked and half blades with no work are alternately provided with the moving blades, and the rotation output is approaching the 0 side. The temperature rises by 7 degrees, making the whole sea surface temperature rise impossible natural phenomenon, increasing abnormal weather without upper limit, increasing the danger of human beings approaching extinction due to heavy rain of seawater around 50 to 100 years. The green earth is a miracle product and there is a great risk of approaching other stars. According to the explanation of the power station, if the rise in seawater temperature is 7 degrees or less, there is no influence on the environment, but for example, 7 degrees in the sea area where the seawater temperature is 30 degrees If the rise continues, the typhoon wind speed will be 300m / sec, etc., and there will be danger of human beings extinction due to the covering of concentrated rainwater salt in seawater, etc., and the temperature of the whole sea surface will rise and nutrients such as nitrogen, oxygen, CO2 etc The natural phenomenon that has supplied water is made impossible, the number of marine microorganisms, phytoplankton and seagrass is drastically reduced. The number of marine foods such as fish is drastically reduced. If China continues to grow 10%, the rise in seawater temperature will be 10%. The current rate is twice as high as the current rate in 20 years, and the speed of typhoons, seasonal winds and ocean tornadoes is 100m / sec. And forestry and residential areas Such as close to 0, for mankind extinction is approaching rapidly before and after 50 years, need for a technology development that corresponds to the existing technologies worst part before it's too late.
大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービン発電の1700倍水仕事率にして、真空中水重力加速度発電にすると、1/10速度1/10容積仕事率が既存蒸気タービン発電の17倍仕事率発電ですが、高さ500m以上に100台で1700倍発電量等膨大な発電量が予想され、水資源は膨大で深層海洋水を使用すると副産物も多く、燃料費0発電の熱効率無限大発電にし、横型全動翼水重力タービン8P大径プラスチックタービン翼8c撥水コーティングして、一台10mと仮定して500mに50台設けて地球最大の水資源で駆動し、地球最大の重力エネルギで蒸気タービンの170倍仕事率小学校理科発電として、出力1000MW(発電所)×17倍仕事率×50台=85万MW=850発電所分とし、安価大量の水資源による燃料費0発電で安価電気の用途拡大に移行して、太陽光加熱器2により空気を太陽光加熱し、燃料費0発電電気駆動の1〜複数段熱ポンプ1Gで複数回圧縮複数回熱回収して、50〜200MPa過熱蒸気温熱50+液体空気冷熱28aに分割保存し、電気+液体空気冷熱+過熱蒸気温熱供給設備1Aより供給して、液体酸素室5Kや液体窒素室5Lに受給し、液体空気駆動の自動車や飛行機や船舶を1/10燃料費駆動や10倍速度駆動にして、極端に安価な発電の蓄電池駆動や電気駆動や、CO2排気僅少の地球温暖化防止が得られる背景がある。 When the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / second, are set to 1700 times the water power of the existing steam turbine power generation, and the water gravity acceleration power generation in the vacuum, the 1/10 speed 1/10 volumetric power is Turbine power generation is 17 times the work rate power generation, but a huge amount of power generation such as 1700 times power generation is expected with 100 units at a height of 500m or more, water resources are enormous, and if deep sea water is used, there are many by-products and fuel costs are 0 The thermal efficiency of the power generation is set to infinite power generation, and the horizontal all-blade water gravity turbine 8P large-diameter plastic turbine blade 8c is water-repellent coating. As the earth's largest gravitational energy, 170 times the work efficiency of steam turbines, elementary power generation at 1000 MW (power plant) x 17 times the work rate x 50 units = 850,000 MW = 850 power plants Shift to expansion of low-cost electricity usage with zero fuel cost generation by water resources, solar heating the air with solar heater 2, and compression multiple times with 1-stage heat pump 1G with fuel cost zero power generation electric drive The recovered heat is recovered and divided into 50 to 200 MPa superheated steam temperature 50 + liquid air cooling heat 28a, supplied from the electricity + liquid air cooling heat + superheated steam temperature supply facility 1A, and received by the liquid oxygen chamber 5K and the liquid nitrogen chamber 5L. In addition, by driving liquid-air-powered automobiles, airplanes and ships to 1/10 fuel cost driving or 10-times speed driving, it is possible to obtain extremely inexpensive power storage battery driving and electric driving, and to prevent global warming with little CO2 emissions. There is a background.
高校や大学では既存エンジンを理論最良エンジンと説明しており、洗脳皆無の小学校理科に戻って理論最良エンジンを考えると、仕事率の単位がkg重m/秒等重量×速度のため、重い物質を高速度にして回転出力発生が理論最良エンジンですが考えた痕跡が皆無という背景がある。そこで例えば横型全動翼水重力タービン8P発電にすると熱効率が無限大発電になる背景があり、日本近海や永久凍土地下に眠る膨大なメタンハイドレートを加熱する場合を、小学校理科で考えると燃料費0加熱が最良です。そこで燃料費0発電電気駆動太陽光加熱器2にして、太陽光で加熱の空気28aを燃料費0発電電気駆動の、1〜複数段熱ポンプ1G1〜複数段圧縮熱回収器2Cで複数回圧縮複数回熱回収し、冷熱の液体酸素5Kや液体窒素5L+温熱の過熱蒸気50に分割保存して、温熱利用無限大の過程で例えば、永久凍土地下のメタンハイドレートに過熱蒸気50を注入メタンと高温水に分割し、メタンを液体窒素冷却液体メタンで回収して過熱蒸気注入を永遠に継続して、メタン回収囲い内を適温で水滴の多い牧草地放牧とし、人類の食糧増大温熱利用無限大にして、液体空気28a製造量を増大して、液体空気駆動の自動車や船舶や宇宙往還機全盛とし、宇宙到達費用1/50万狙いにして、船舶駆動の過程で自然現象高速化2aすると、微生物や海草類やサンゴ等を増殖食物連鎖等で魚類等人類の食物を増大し、海水の豪雨阻止し、人類絶滅を先送り出来る背景があり。燃料費僅少で10倍速度狙いの船舶革命や飛行機革命となって、運用利益率が既存運用利益率の10倍等膨大となり、世界規模100%独占した製造運用とし、雇用を増大する雇用増大革命に出来る背景がある。 In high school and university, the existing engine is described as the best engine, and when we return to elementary school science without brainwashing and think about the best engine, the unit of work is kg weight m / sec. The engine is the best engine in terms of generating rotational output at a high speed, but there is no trace of thought. Therefore, for example, the horizontal full-blade hydrogravity turbine 8P power generation has the background that the thermal efficiency becomes infinite power generation. When heating a huge methane hydrate sleeping in the sea near Japan or permafrost, fuel costs are considered in elementary school science. Zero heating is the best. Therefore, the fuel cost 0 power generation electric drive solar heater 2 is used, and the solar heating air 28a is compressed a plurality of times by the fuel cost 0 power generation electric drive 1 to multistage heat pump 1G1 to multistage compression heat recovery unit 2C. Heat collected multiple times, divided and stored in cold liquid oxygen 5K and liquid nitrogen 5L + warm superheated steam 50, and injecting superheated steam 50 into methane hydrate under permafrost, for example, in the process of infinite use of heat Divided into high-temperature water, recovered methane with liquid nitrogen cooled liquid methane, continued superheated steam injection forever, made the methane recovery enclosure grazing in a grazing land with appropriate temperature and many water droplets, increasing human food use heat Then, increase the production volume of liquid air 28a, make liquid air driven automobiles and ships and spacecrafts prime, aim for space arrival cost 1 / 500,000, natural phenomenon speeding up 2a in the process of ship driving, Microbe The food of fish such as the human race to increase the seaweed and coral, such as in growth the food chain, etc., sea water and heavy rain prevented, there is a background that can put off the human race extinct. Revolution of employment growth that will increase the employment by making the manufacturing operation monopolized 100% worldwide, with the operating profit rate becoming 10 times larger than the existing operational profit ratio, as the ship revolution and airplane revolution aiming at 10 times speed with low fuel cost There is a background that can be.
既存世界の火力原子力発電所では、発電熱量全部で海水温度摂氏7度上昇海水温度上昇量を100年で1000倍等とし、下降気流や上昇気流を限り無く増大して、異常乾燥山火事や砂漠化や集中豪雨や熱波や寒波等を限り無く増大し、日本近海は20年前後で台風や季節風や竜巻を100m/秒等として、海水を上空に吸引海水の集中豪雨等により陸地に塩の被覆を設けて人類陸上食物減少の危険を増大し、冬場に海面冷却海底に栄養分を供給していた自然現象を不可能として、微生物や植物プランクトンや海草類やサンゴ等を激減、食物連鎖により魚類を1/100等に激減人類の海中食物も限り無く減少し、旱魃や集中豪雨や台風や季節風を100年で10倍等に増大して、例えば台風や季節風を300m/秒等上限の無い異常気象の巨大化とし、海底岩盤膨張地震や津波を巨大化ハイチ超える災害を創造して、人類絶滅の危険を増大のため海水の豪雨等を阻止し、海水温度上昇0等地球温暖化防止して、人類絶滅を先送りする課題がある。又最近の課題は財政赤字国の急増です。最大原因は安価労働コスト国を世界の工場として簡単に利益を得る流行蔓延で、簡単に利益が得られる半面途上国全部が過去の日本のように物真似改良で世界一を競うため、安価優良製品続出して先進国製造設備壊滅財政赤字増大雇用壊滅の危険があり、物真似改良が可能な発明実施は時代遅れと認識し、世界規模100%独占を永遠に続ける発明品の極秘製造極秘運用として、利益率抜群の世界一にする課題がある。 In the existing thermal power plants in the world, the total heat generation is 7 degrees Celsius, and the seawater temperature rise is 1000 times in 100 years, and the downdrafts and updrafts are increased as much as possible. As the number of storms, torrential rains, heat waves, cold waves, etc. increases without limit, typhoons, seasonal winds, tornadoes, etc., around 100 years in the sea near Japan, salt water on the land due to concentrated heavy rains, etc. Covering increases the danger of human land food loss, making it impossible for the natural phenomenon of supplying nutrients to the sea surface cooling seabed in winter, reducing microorganisms, phytoplankton, seaweeds, corals, etc. Decreased to 1/100, etc., the number of underwater foods has been reduced as much as possible, and droughts, torrential rains, typhoons and seasonal winds have increased 10 times in 100 years. For example, typhoons and seasonal winds have no upper limit such as 300m / sec. of Creates a disaster that exceeds Haiti by enlarging submarine rock expansion earthquakes and tsunamis, preventing heavy rains of seawater to increase the danger of human extinction, preventing global warming by raising seawater temperature, etc. There is a challenge to postpone extinction. A recent issue is the rapid increase in countries with deficits. The biggest cause is the epidemic that easily makes profits with low labor cost countries as the world's factories, and all the developing countries that can easily make profits compete for the best in imitation improvement like Japan in the past, so cheap and excellent products Proceeding with the destruction of industrialized equipment in the industrialized countries, there is a danger of increased employment deficit, and the implementation of inventions that can be imitated is recognized as out of date, and profits as a top-secret manufacturing operation of inventions that continue to be a 100% monopoly worldwide forever There is a challenge to be the best in the world.
横型全動翼水重力タービン8P燃料費0熱効率無限大発電にして、太陽光加熱器2+電気駆動1〜複数段熱ポンプ1G+1〜複数段圧縮熱回収器2Cにより熱製造し、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dとして、受給した液体空気噴射燃料噴射燃焼して50〜200MPaの高圧高温燃焼ガス室5Mとし、内周や外周に水噴射して構成した高圧高温水蒸気室5Nを加熱して、最適温度50〜200MPaの高圧高温燃焼ガス室5M+高圧高温水蒸気室5Nとし、圧縮容積を液体圧縮独立で1/600や1/1700にして、同一燃料量既存技術の10倍出力狙いとし、高圧高温燃焼ガス制御弁5a+水蒸気制御弁5P開放して、高圧高温燃焼ガス室5M+高圧高温水蒸気室5Nより、圧力機関1Bや液体ウォータージェット80や液体合体噴射部80に供給し、圧力機関1Bや液体ウォータージェット80や液体合体噴射部80を駆動して、自動車等車両類や船舶類や飛行機類を駆動し、船舶類駆動では自然現象高速化して海中に酸素や窒素やCO2等を供給して、微生物や植物プランクトンや海草類やサンゴや魚類等を増殖人類の食物を増大し、飛行機はCO2排気0に近い宇宙飛行全盛1日に地球を16周する等として、地球上何処でも日帰り旅行や大気中はCO2排気僅少飛行狙いとし、世界規模100%独占して極秘製造極秘運用する発電や船舶や飛行機として、利益率抜群の世界一や新規雇用抜群の世界一にし、旱魃や集中豪雨や台風や季節風や海水の豪雨や地震津波の巨大化を阻止して、地球温暖化防止し人類絶滅を先送りする。 Horizontal full blade water gravity turbine 8P Fuel cost 0 Thermal efficiency infinity power generation, heat production with solar heater 2+ electric drive 1-multistage heat pump 1G + 1-multistage compression heat recovery unit 2C, electricity + liquid air cold heat + As the superheated steam temperature heat supply facility 3D, the received liquid air injection fuel injection combustion is performed to form a high pressure high temperature combustion gas chamber 5M of 50 to 200 MPa, and the high pressure high temperature steam chamber 5N configured by water injection on the inner periphery and outer periphery is heated. The high pressure high temperature combustion gas chamber 5M + high pressure high temperature steam chamber 5N with an optimum temperature of 50 to 200 MPa, the compression volume is 1/600 or 1/1700 independent of liquid compression, and the target of the same fuel amount is 10 times the output of the existing technology, The high pressure high temperature combustion gas control valve 5a + steam control valve 5P is opened, and the pressure engine 1B and liquid water jet 80 are supplied from the high pressure high temperature combustion gas chamber 5M + high pressure high temperature steam chamber 5N. Supplied to the liquid coalescence injection unit 80, drives the pressure engine 1B, the liquid water jet 80, and the liquid coalescence injection unit 80 to drive vehicles such as automobiles, ships and airplanes. By supplying oxygen, nitrogen, CO2, etc. into the sea, the microorganisms, phytoplankton, seaweeds, corals, fishes, etc. are grown to increase human food. As a lap, etc., it is aimed at day trips anywhere on the earth and the CO2 exhaust is a little flight in the atmosphere. Being the best in the world, it will prevent droughts, torrential rains, typhoons, seasonal winds, heavy rains in seawater, and huge earthquakes and tsunamis to prevent global warming and postpone human extinction.
横型全動翼水重力タービン8P熱効率無限大発電にすると、燃料費0でボイラや原子炉が不要で構造が簡単になる効果が大きく、大気圧同速度同容積仕事率を既存蒸気タービン発電の1700倍水重力タービン発電にし、水落差を拡大して既存発電量の1700倍発電量に近付ける効果が大きく、熱効率無限大発電電気製造の電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより、液体酸素室5K+液体窒素室5Lに供給し、超高圧噴射して気化酸素に燃料噴射着火燃焼して気化窒素ガスを加熱して、50〜200MPaの高圧高温燃焼ガス室5M+高圧高温水蒸気室5Nにし、酸素圧力機関や水圧力機関や液体ウォータージェットや液体合体噴射部を駆動して、自動車や船舶や飛行機を燃料費1/10や10倍速度等が狙えるのに加えて、熱効率無限大重力タービン8P発電機一台で85万MW発電狙いに出来る効果が大きく、宇宙到達経費を既存宇宙ロケットの1/50万経費狙いに出来る効果等から、発電機1やスクリュー7Cやプロペラ7Aや回転翼7Bを非常に安価駆動し、酸素圧力機関+水圧力機関排気の過程で液体ウォータージェット80や液体合体噴射部80と合体出来るため、同一燃料量10倍回転出力や10倍噴射推進出力狙いに出来る効果があり、燃料費僅少で既存船舶や飛行機の10倍速度等、世界規模100%独占して製造運用する発電や船舶や飛行機や自動車等とし、先進国用実験最良や利益率抜群の世界一や新規雇用抜群の世界一を狙える効果がある。 Horizontal full-blade hydrogravity turbine 8P thermal efficiency infinite power generation has the effect of simplifying the structure with no fuel cost and no need for boilers or nuclear reactors. Double water gravity turbine power generation, greatly increasing the water drop and bringing it closer to 1700 times the existing power generation amount. Electricity + liquid air cold heat + superheated steam heat supply equipment 3D for infinite thermal efficiency power generation Electricity of liquid oxygen Chamber 5K + liquid nitrogen chamber 5L, super high pressure injection, fuel injection ignition combustion in vaporized oxygen and heating the vaporized nitrogen gas to 50-200 MPa high pressure high temperature combustion gas chamber 5M + high pressure high temperature steam chamber 5N, oxygen In addition to driving a pressure engine, a water pressure engine, a liquid water jet, and a liquid coalesced injection unit, and aiming for a fuel cost of 1/10 or 10 times the speed of an automobile, ship or airplane, The efficiency that can be aimed at 850,000 MW power generation with one infinite efficiency gravity turbine 8P generator, and the effect that the space arrival cost can be aimed at 1 / 500,000 of existing space rockets, generator 1 and screw 7C and propeller 7A and rotor blades 7B are driven at a very low cost and can be combined with the liquid water jet 80 and the liquid combined injection unit 80 in the process of oxygen pressure engine + water pressure engine exhaust. It has the effect of being able to target the output, fuel costs are low, 10 times the speed of existing ships and airplanes, etc. Power generation, ships, airplanes, automobiles, etc. that are 100% monopolized and operated worldwide. It has the effect of aiming for the best in the world and the best in the world for new employment.
緑の地球は奇跡の産物で他の星に近付く危険が大きく、例えば中国が10%成長を100年続けると、火力発電や原子力発電により中国近海の海水温度上昇量が1000倍を超えるため、現在日本のゲリラ豪雨増大が海水の豪雨1000倍等となり、現在の魚類激減が0に近付く等人類絶滅が100年以内に急接近する可能性が強く、海水温度上昇0やCO2排気0や燃料費0発電電気駆動で地球温暖化防止して、熱効率無限大重力発電電気駆動の電気+液体空気冷熱+過熱蒸気温熱供給設備より受給し、液体酸素+液体窒素で自動車や飛行機や船舶を燃料費僅少で駆動して、船舶駆動では自然現象高速化2aし、海中に窒素や酸素やCO2等の栄養分として供給して、水中微生物のCO2等の消化能力を森林の数万倍狙い等に増大する効果が大きく、植物プランクトンや海草類やサンゴ等を増殖し、食物連鎖で魚類等を増殖人類の海中食物を大増大して、砂漠化や旱魃や集中豪雨や台風や季節風や地震津波等の巨大化を阻止し、海水の豪雨等を阻止して、人類で最も重要な人類絶滅を先送りする効果がある。 The green earth is a miracle product and has a high risk of approaching other stars. For example, if China continues to grow 10% for 100 years, the temperature rise in the sea near China will exceed 1000 times due to thermal power generation and nuclear power generation. There is a strong possibility that the extinction of mankind will rapidly approach within 100 years, such as the increase in guerrilla heavy rain in Japan is 1000 times the heavy rain in seawater, the current drastic decrease in fish is close to 0, etc. Power generation electric drive to prevent global warming, thermal efficiency infinite gravity power generation electric drive electricity + liquid air cold heat + superheated steam temperature supply equipment, liquid oxygen + liquid nitrogen fuels cars, airplanes and ships with little fuel costs Driving, speeding up natural phenomena in ship driving, and supplying it as nutrients such as nitrogen, oxygen and CO2 in the sea, increasing the digestive capacity of underwater microorganisms such as CO2 to aim for tens of thousands of times in the forest Large, phytoplankton, seaweeds, corals, etc., propagate fish, etc. in the food chain, greatly increase the human food underwater, prevent desertification, drought, concentrated heavy rain, typhoon, seasonal wind, earthquake tsunami, etc. In addition, it has the effect of preventing the heavy rain of seawater and delaying the most important human race extinction.
飛行機駆動は、熱効率無限大重力発電電気駆動の電気+液体空気冷熱+過熱蒸気温熱供給設備より液体酸素+液体窒素を受給し、高圧高温燃焼ガス室5Mに液体酸素を超高圧噴射気化酸素に燃料噴射着火燃焼して、高圧高温水蒸気室5Nの高圧高温水蒸気5Nを加熱し、50〜200MPa高圧高温燃焼ガス5M+高圧高温水蒸気5Nとして液体合体噴射部80を駆動して、宇宙到達費用を既存宇宙ロケットの1/50万経費狙いにし、同一燃料費10倍噴射推進出力で宇宙利用全盛を狙う効果があり、例えば噴射推進出力を既存ジェット機の100倍圧力10倍熱量噴射短時間1000倍噴射推進出力狙いとして、大気中は燃料費僅少のプロペラ飛行や回転翼飛行や噴射推進狙いにし、水蒸気噴射速度や燃焼ガス噴射速度が真空中で最大のため、既存宇宙ロケット地上大量噴射は最悪と考え、既存航空機最高飛行高度付近より、50〜200MPaの高圧高温燃焼ガス5M+高圧高温水蒸気5Nの噴射量増大にして、1日に地球を16周する等とし、地球上何処でも日帰り旅行が可能な宇宙利用全盛を狙える効果がある。 Airplane drive receives electricity + liquid air cold heat + superheated steam temperature heat supply equipment of thermal efficiency infinite gravity power generation electric drive, liquid oxygen + liquid nitrogen, and fuels liquid oxygen into high pressure high temperature combustion gas chamber 5M as super high pressure injection vaporized oxygen High-temperature high-temperature steam 5N in the high-pressure high-temperature steam chamber 5N is heated by injection ignition combustion, and the liquid coalescence injection unit 80 is driven as 50 to 200 MPa high-pressure high-temperature combustion gas 5M + high-pressure high-temperature steam 5N. Has the effect of aiming for space use with the same fuel cost 10 times injection propulsion output, for example, the injection propulsion output is 100 times the pressure of existing jets 10 times the calorie injection for a short time 1000 times injection propulsion output As for the propeller flight, rotor blade flight and injection propulsion aiming at low fuel costs in the atmosphere, the steam injection speed and the combustion gas injection speed are the largest in vacuum Therefore, the existing space rocket ground mass injection is considered the worst, and from around the highest flight altitude of the existing aircraft, the injection amount of high pressure high temperature combustion gas 5M + high pressure high temperature steam 5N of 50-200MPa is increased 16 times a day, etc. And it has the effect of being able to aim for a prime use of space where you can take a day trip anywhere on the planet.
既存エンジンが洗脳で長期間発明が阻止され、例えば既存最良蒸気タービン発電の大気圧同速度同容積仕事率kg重m/秒を、水仕事率の1/1700と僅少にし、静翼を動翼と交互に設けて堰き止めて回転出力を0に近付け、蒸気タービン発電の駆動熱量全部で海水温度7度上昇魚類激減、海底岩盤を膨張地震や津波を巨大化し、20年前後で日本近海の台風や季節風や海上竜巻の上昇気流を巨大化100m/秒等にして、海水を上空に吸引海水の豪雨が予想される等、50〜100年前後で陸地に塩の被覆を設けて食糧激減人類絶滅が急接近する危険があります。即ち既存技術の致命的欠点多数で発明が膨大になり過ぎるため、発明を符号の説明に記載すると共に、先の出願で再三説明した部分は省略し、竪型全動翼重力タービン以外3種類は横軸全動翼重力タービンで既存タービンに近いため、横型対向全動翼水重力タービン8P実施例で代用説明して、横型対向全動翼水重力タービン8P・横型直列全動翼水重力タービン8P・横型食込全動翼水重力タービン8P・竪型全動翼水重力タービン8Hの代替説明にし、発電用比重大物質は資源量最大の水52a重力加速度加速駆動で代替説明する等、常識を省略した発明の具体化に挑戦します。 The existing engine is brainwashed and the invention is blocked for a long time. For example, the existing best steam turbine power generation has the same atmospheric pressure, same speed, same volumetric power, kg weight m / sec. It is alternately installed and dammed to bring the rotational output close to 0, the seawater temperature rises by 7 degrees with all the heat generated by steam turbine power generation, the fish drastically diminishes, the submarine bedrock expands into earthquakes and tsunamis, and typhoons around Japan around 20 years ago And the rising wind of seasonal winds and tornadoes at sea is increased to 100m / second, and a heavy rain of suction seawater is expected over the seawater. There is a risk of sudden approach. In other words, since the invention is too large due to many fatal defects of the existing technology, the invention is described in the explanation of the reference numerals, and the part that has been repeatedly explained in the previous application is omitted, and there are three types other than the vertical rotor blade gravity turbine. Since the horizontal axis full blade gravity turbine is close to the existing turbine, the horizontal opposed total blade water gravity turbine 8P embodiment will be used as a substitute, and the horizontal opposed full blade water gravity turbine 8P / horizontal series full blade water gravity turbine 8P will be described.・ The common explanation such as the alternative explanation of the horizontal-type bite-type full-blade water gravity turbine 8P and the vertical-type full-blade water gravity turbine 8H and the specific material for power generation is substituted by the water 52a gravity acceleration acceleration drive with the largest amount of resources. We will challenge the embodiment of the omitted invention.
図1実験が必要な横型対向全動翼水重力タービン8P発電は、資源量最大の水3Eを比重大物質上昇装置2Fにより最上部に上昇保存し、比重大物質加速機6W複数〜多数開放水3Eを噴射重力加速度真空加速して、大径ドラムの中心に水平軸16A外周に対向同速度食込み回転可能に、同一形状長大対向のタービン翼8c1台目を駆動して、重力加速部1gで水3E真空中重力加速度加速して2台目タービン8P駆動し、同様に3台目4台目と次々に駆動駆動台数無制限として、既存蒸気タービン発電の1/10速度1/100容積水3E噴射タービン翼8c駆動し、大気圧1/10速度1/100容積水仕事率を既存蒸気タービン発電の1、7倍仕事率発電として、タービン外箱77a内対向に100台等落差使用無制限具備し、1台の発電量1、7倍×100台=170倍発電量発電所等を可能にして、実験最良に移行の過程で既存の2倍直径プラスチックタービン8P撥水コーティングとし、製造単価や重量や回転数を大幅に低減して、振動や騒音を大幅に低減住宅等の併設を可能にし、燃料費0の熱効率無限大発電等原子炉もボイラも不要の簡単発電として、小学校理科計算で安価な電気製造無限大狙い電気の用途開発必要とし、排気の過程の気体専用冷却室11Dに空気抽出器51を設けて、摩擦熱で発生蒸気を水冷却の僅少冷却や、海水発電蒸留水や塩の製造等とし、最高真空水重力加速発電の最大回転出力にして、海水温度上昇0CO2排気0燃料費0で地球温暖化防止し、構造簡単や利益率抜群世界一の発電方法にして、安価な電気製造物無限多や電気駆動無限多にして、各種エネルギ保存サイクル合体機関発電方法にする。 Fig. 1 Horizontal opposed full-blade water gravity turbine 8P power generation, which requires experiments, stores water 3E, which has the largest amount of resources, at the top by means of a specific material lift device 2F, and has a large number of specific material accelerators 6W and many open water. 3E is accelerated by jet gravity acceleration vacuum, and the first turbine blade 8c facing the same shape and length is driven in the center of the large-diameter drum so as to be able to bite and rotate on the outer periphery of the horizontal shaft 16A. 3E vacuum acceleration in 3E to drive the second turbine 8P, similarly, the third and fourth to drive the number of drive units one after the other, 1/10 speed 1/100 volume water 3E injection turbine of existing steam turbine power generation The blade 8c is driven, and the atmospheric pressure 1/10 speed 1/100 volume water power is 1,7 times the power generation of the existing steam turbine power generation. Stand 1. Electricity 1, 7 times x 100 units = 170 times Electricity generation Power plant, etc. is made possible, and the existing best double diameter plastic turbine 8P water-repellent coating is adopted in the course of the transition to the best experiment. Reduces vibration and noise to a great extent, enabling the installation of houses, etc., and thermal efficiency infinite power generation with no fuel cost, etc. It is necessary to develop the application of the target electricity, and an air extractor 51 is provided in the gas cooling chamber 11D in the process of exhaust, and the generated steam is cooled with water by frictional heat, or the production of distilled water or salt for seawater power generation, Highest vacuum water gravity acceleration power generation maximum rotation output, seawater temperature rise 0CO2 exhaust 0 fuel cost 0 to prevent global warming, simple structure and excellent profit rate And electric drive infinity Thus, various energy storage cycle combined engine power generation methods are obtained.
実験が必要ですがタービン翼角度を衝撃に強い角度や水3E最適速度使用として、合成樹脂タービン翼8cにはシリコン樹脂又はフッ素樹脂等で撥水コーティング3Aにし、金属製タービン翼8c使用では撥水鍍金3aとして、水平軸16A又は16A16Aで発電機1を駆動し、横型対向全動翼水重力タービン8P簡単発電として、安価な電気駆動の1〜複数段熱ポンプ1Gで太陽光加熱器2や地熱加熱等の空気を複数回圧縮高温とし、1〜複数段圧縮熱回収器2Cの空気熱交換器2Xで太陽光加熱の別空気28aで熱回収して、圧縮空気28aを製造増大し、2〜複数段熱ポンプ1Gで複数回圧縮して、2〜複数段圧縮熱回収器2Cの水熱交換器2Yで複数回熱回収し、50〜200MPa過熱蒸気50温熱+液体空気28a冷熱に分割保存して、電気+液体空気冷熱+過熱蒸気温熱供給設備3D多数とし、例えばメタンハイドレートに過熱蒸気50を注入メタンを回収液化メタン利用にして、炊飯や暖房を温熱50駆動し冷凍庫や氷製造を液体空気冷熱28a駆動無限製造にし、船舶類や車両類や飛行機類には液体酸素や液体窒素て供給して、限り無く小型簡単や大型簡単船舶類や車両類や飛行機類駆動にし、船舶駆動では自然現象高速化2a海水に窒素や酸素やCO2を供給微生物や海草類増大して、食物連鎖等で魚類等人類の食料を大増大し、飛行機や車両駆動では高速やCO2排気経費僅少にして、宇宙往還機では1/50万経費宇宙到達狙い1日に地球を16周する等、各種エネルギ保存サイクル合体機関や各種エネルギ保存合体方法にする。 Although experiments are required, the turbine blade angle is set to a shock-resistant angle and water 3E optimum speed. The synthetic resin turbine blade 8c is made of water-repellent coating 3A with silicon resin or fluororesin, and when the metal turbine blade 8c is used, it is water-repellent. As the plating 3a, the generator 1 is driven by the horizontal shaft 16A or 16A16A, and the solar heater 2 or the geothermal heat is generated by an inexpensive electric drive 1 to multi-stage heat pump 1G as a simple power generation of the horizontal opposed total moving blade water gravity turbine 8P. The air such as heating is compressed a plurality of times at a high temperature, and heat is recovered with the separate air 28a of solar heating by the air heat exchanger 2X of the 1-stage multi-stage compression heat recovery unit 2C to increase the production of compressed air 28a, Compressed multiple times with multistage heat pump 1G, recovered heat multiple times with hydrothermal exchanger 2Y of 2-stage multistage compression heat recovery unit 2C, divided into 50-200MPa superheated steam 50 warm heat + liquid air 28a cold heat There are 3D electricity + liquid air cold heat + superheated steam temperature supply equipment, for example, superheated steam 50 is injected into methane hydrate, methane is recovered and liquefied methane is used, rice cooking and heating are driven with heat 50, freezer and ice production The liquid air cooling heat 28a drive is infinitely manufactured, and it is supplied with liquid oxygen or liquid nitrogen to ships, vehicles, and airplanes to drive small and simple, large simple ships, vehicles, airplanes, and so on. Then, natural phenomenon speeding up 2a Supply nitrogen, oxygen and CO2 to seawater Increase microorganisms and seaweeds, greatly increase human food such as fish in the food chain, etc. In the space shuttle, the energy conservation cycle coalescence engine and the various energy conservation coalescence methods are used, such as 16 orbits of the earth for 1 / 500,000 expenses per day.
図2の横型対向全動翼水重力タービン8Pには、推力や重量を支える推力軸受80aや軸受80や水3Eを加速する重力加速部1gを設け、水3E最適速度使用とし、大径外周長大プラスチック環状多数組立タービン翼8c撥水コーティング等として、大径ドラムの中心に水平軸16Aを設け、外周環状に同一形状直線長大多数を環状政策組立で安価な軽量化にし、重力球誘導曲面8d具備タービン翼8cを具備し、タービン8Pを対向にタービン外箱77a内垂直に無制限に複数台設け、用途に合わせた台数使用にし、比重大物質上昇装置2Fにより水3Eを最上部に上昇保存して、比重大物質加速機6Wで比重大物質噴射ノズル6E多数噴射又は直線状噴射にし、水重力真空加速して重力加速部1g重力中核加速し対向タービン翼8cに噴射して、横型全動翼水重力タービン8P駆動発電機1を駆動し、海洋深層水52a11〜12℃を駆動水や冷却水として使用努力して、空気抽出器51を気体専用冷却室11Dに具備最高真空にし、水の摩擦熱のみ冷却する僅少冷却として、逆浸透膜や電気透析で海洋深層水濃縮・比重や表面張力の増大凍結温度−21℃等とし、飲料水や乾燥による塩の製造等に参入して、清浄でミネラルが豊富な海洋深層水52a利用の化粧品や飲料や食品製造等とし、海水温度上昇0CO2排気0燃料費0として、構造簡単や利益率を抜群世界一とし、ボイラも原子炉も不要な簡単構造革命の各種エネルギ保存サイクル合体機関発電にする。 2 is provided with a thrust bearing 80a that supports thrust and weight, a gravity acceleration unit 1g that accelerates the bearing 80 and water 3E, and uses an optimum speed of water 3E, and has a large outer diameter and large diameter. As a plastic ring multi-assembly turbine blade 8c, a horizontal shaft 16A is provided at the center of the large-diameter drum as a water-repellent coating, etc. Turbine blades 8c are provided, and an unlimited number of turbines 8P are vertically provided opposite to each other in the turbine outer box 77a. The number of the turbines 8P is adjusted according to the intended use. , The specific critical material accelerator 6W makes multiple specific material injection nozzles 6E multiple injections or linear injection, water gravity vacuum acceleration and gravity acceleration part 1g gravity core acceleration to the opposed turbine blade 8c The horizontal full-blade water gravity turbine 8P drive generator 1 is driven, and the ocean deep water 52a11-12 ° C. is used as drive water or cooling water, and the air extractor 51 is turned into the gas-only cooling chamber 11D. Built-in maximum vacuum, only slight frictional heat of water is cooled, and reverse osmosis membranes and electrodialysis are used to concentrate deep seawater, increase specific gravity and surface tension to freeze temperature -21 ° C, etc., and produce salt by drinking water and drying Etc., making cosmetics, beverages, foods, etc. using clean deep mineral water 52a rich in minerals, seawater temperature rise 0CO2 exhaust 0 fuel cost 0 And energy saving cycle combined engine power generation with a simple structural revolution that requires neither a nuclear reactor nor a nuclear reactor.
横型全動翼水重力タービン8H発電電力駆動、1段熱ポンプ1Gで空気を吸入圧縮20〜100度前後にして、1段圧縮熱回収器2C空気熱交換器2Xで別空気28aを加熱し、20〜100度前後に加熱1段熱ポンプ1Gで100〜500度等に圧縮して、別空気で熱回収圧縮を繰り返す圧縮空気28a質量増大の熱製造にし、2〜複数段熱ポンプ1Gで1〜複数回圧縮空気28aを1〜複数回高温にして、2〜複数段圧縮熱回収器2C空気熱交換器2Xで1〜複数回熱回収低温にし、圧縮空気28a圧力を1〜複数回上昇水熱交換器2Yでは過熱蒸気温熱50製造して、圧縮空気28aや過熱蒸気50の圧力増大で温熱や冷熱需要に対応し、液体空気28a冷熱を液体酸素室5K+液体窒素室5Lに保存して、400度前後50〜200MPa過熱蒸気50温熱を高圧高温水蒸気室5Nに分割保存し、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dにして、例えばメタンハイドレートに温熱50を注入メタン回収し、冷熱28aで冷却液体メタンで利用して、炊飯器や洗濯乾燥機を温熱50で駆動する台所革命にし、暖房や冷房等に温熱50や冷熱28aを使用し、温室栽培や氷製造等無限用途対応の加熱革命や冷却革命にして、液体空気冷熱28aで自動車や飛行機や船舶駆動し、船舶駆動の過程で自然現象高速化2aして、海水に窒素や酸素やCO2を供給微生物や植物プランクトンや海草類増大し、食物連鎖等で魚類や海草類等人類の食料を大増大する。 Horizontal full-blade water gravity turbine 8H drive power generated, 1 stage heat pump 1G sucks and compresses air to around 20-100 degrees, and heats separate air 28a with 1 stage compression heat recovery unit 2C air heat exchanger 2X, Compressed to about 100 ° C to 500 ° C or the like with a heating single-stage heat pump 1G around 20 to 100 ° C, and heat production with compressed air 28a mass increase that repeats heat recovery and compression with separate air, and 1 to 2 with multiple-stage heat pump 1G -Multiple times compressed air 28a is made hot one to several times, 2 to multiple stage compression heat recovery device 2C air heat exchanger 2X is used to make heat recovery low temperature one to several times, and the pressure of compressed air 28a is raised one or more times In the heat exchanger 2Y, the superheated steam temperature 50 is manufactured, the pressure of the compressed air 28a and the superheated steam 50 is increased to meet the demand for heat and cold, and the liquid air 28a is stored in the liquid oxygen chamber 5K + liquid nitrogen chamber 5L. Around 400 degrees 50-200 The Pa superheated steam 50 heat is divided and stored in the high-pressure high-temperature steam chamber 5N, and the electricity + liquid air cold heat + superheated steam heat supply equipment 3D is used. The kitchen revolution that drives rice cookers and washing / drying machines with heat 50 is used, and the heat 50 and cold 28a are used for heating and cooling, etc., and the heating revolution and cooling revolution for infinite applications such as greenhouse cultivation and ice production. Then, driving a car, airplane or ship with liquid air cooling heat 28a, speeding up the natural phenomenon 2a in the process of driving the ship, supplying nitrogen, oxygen or CO2 to seawater, increasing microorganisms, phytoplankton, seaweed, food chain, etc. And greatly increase human food such as fish and seaweed.
図3の電気+液体空気冷熱+過熱蒸気温熱供給設備3Dを説明すると、横型全動翼水重力タービン8P燃料費0発電電気駆動の、太陽光加熱器2で各種水面を利用し、地球最大熱量の太陽光を矩形長レンズ2d複数重ねて直線状に集めて、焦点距離最短の幅最大狙う長レンズ2dで熱吸収材2B温度を上昇して、空気路28A空気28a温度を上昇し、1〜複数段熱ポンプ1Gで熱製造として、既存のレンズ断面を直線状に延長矩形の長レンズ2dとしてレンズ材質全部を使用可能とし、発泡プラスチック等の断熱材2cを半筒形外箱77Bで囲って円筒等の長大な筒を設けて、その中に耐熱材2Aを設けて太陽熱で高温にする板状熱吸収材2Bで空気28aを加熱し、上部に複数重ねの幅広長大な長レンズ2dを継手80A+締付具80Bで密封真空断熱可能に設けて、焦点距離最短幅最大可能に長手方向や直角方向には継手80Aで延長可能複数を直角継手で一纏めにし、熱ポンプ1Gで複数吸入空気路28Aから加熱空気28aを吸入制御可能にして、水上で東から西に180度回転太陽光と直角にする太陽光加熱器2とし、更に傾斜して太陽光に2方向直角維持回転する装置として、空気28aを加熱して横型全動翼水重力タービン8P発電電気駆動の、1〜複数段熱ポンプ1Gで吸入圧縮800〜1200度等とし、太陽光加熱の別空気を加熱圧縮する質量増大や繰返し圧縮して、1〜複数段圧縮熱回収器2Cで繰返し熱回収を繰返し、液体酸素を液体酸素室5Kに分割保存して、液体窒素を液体窒素室5Lに分割保存し、過熱蒸気温熱50を高圧高温水蒸気室5Nに分割保孫して、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dとし、各種温熱利用全盛や各種冷熱利用全盛にする。 Explaining the electricity + liquid air cold heat + superheated steam temperature supply facility 3D in FIG. 3, the maximum heat quantity of the earth is obtained by using various water surfaces in the solar heater 2 of the horizontal full-rotor blade water gravity turbine 8P fuel cost 0 power generation electric drive. Of the rectangular long lens 2d are collected in a straight line, and the heat absorbing material 2B temperature is increased by the long lens 2d aiming at the maximum width of the shortest focal length, and the temperature of the air passage 28A is increased. As a heat production with a multistage heat pump 1G, the entire lens material can be used as a rectangular long lens 2d extending linearly in an existing lens cross section, and a heat insulating material 2c such as foamed plastic is surrounded by a semi-cylindrical outer box 77B. A long cylinder such as a cylinder is provided, heat-resistant material 2A is provided therein, and air 28a is heated by a plate-like heat absorbing material 2B that is heated to high temperature by solar heat. 80A + Fastener 80B Provided in a hermetically sealed vacuum insulation, the focal length can be maximized by the shortest width, and can be extended by a joint 80A in the longitudinal direction and the right angle direction. As a solar heater 2 that can be controlled and rotated from the east to the west by 180 degrees perpendicular to the sunlight on the water, and further inclined and rotated in two directions at right angles to the sunlight, the air 28a is heated to form a horizontal type. Fully bladed water gravity turbine 8P power generation electric drive, 1 to multi-stage heat pump 1G to suction compression 800 to 1200 degrees, etc. Repeated heat recovery with the stage compression heat recovery unit 2C, liquid oxygen is divided and stored in the liquid oxygen chamber 5K, liquid nitrogen is divided and stored in the liquid nitrogen chamber 5L, and the superheated steam temperature 50 is divided into the high-pressure and high-temperature steam chamber 5N. And Homago, and electrical + liquid air cold + superheated steam heat supply facilities. 3D, a variety of thermal utilization prime and various cold use golden.
図4の液体スクリュー船舶39Dの圧力機関1B駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから受給して、液体酸素室5Kに液体酸素を受給保存し、液体窒素室5Lに液体窒素を受給保存して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、例えば高圧高温燃焼ガス制御弁5a開放して、歯車ポンプの吸入路を1段燃焼室1Yとした酸素圧力歯車機関3Zに高圧高温燃焼ガス供給し、燃料噴射燃焼高圧高温として内周や外周の水圧力歯車機関3Nの高圧高温水蒸気5Nを加熱して、多段酸素圧力歯車機関3Z多段燃焼して多段水圧力歯車機関3Nを多段加熱連動し、夫々の回転出力でスクリュー7C駆動して、排気の過程では簡単液体ウォータージェット80を構成し、既存往復機関やガスタービンの気体空気圧縮を液体空気圧縮として、圧縮仕事率を1/600として100倍出力狙いとし、既存船舶の10倍速度狙い自然現象高速化2a推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、中大型スクリュウュー船舶69Dにした、各種エネルギ保存サイクル合体機関及び合体方法にする。 The driving of the pressure engine 1B of the liquid screw ship 39D in FIG. 4 will be described. The liquid oxygen chamber 5K is received from the electricity + liquid air cold heat + superheated steam temperature heat supply facility 3D of the horizontal full-blade water gravity turbine 8P power generation electric manufacturing. The liquid nitrogen is received and stored in the liquid nitrogen chamber 5L, the liquid nitrogen is received and stored in the liquid nitrogen chamber 5L, the superheated steam 50 is received and stored in the high-pressure and high-temperature steam chamber 5N, and the liquid nitrogen injection + liquid oxygen injection + in the high-pressure and high-temperature combustion gas chamber 5M Fuel injection combustion is performed to heat the high-pressure and high-temperature steam 5N on the outer periphery and the inner periphery, and the addition of liquid nitrogen and water injection can be selected for each. The chamber 5N is opened, for example, the high-pressure high-temperature combustion gas control valve 5a is opened, and the high-pressure high-temperature combustion gas is supplied to the oxygen pressure gear engine 3Z in which the intake passage of the gear pump is the first-stage combustion chamber 1Y. The high pressure and high temperature steam 5N of the inner and outer water pressure gear engines 3N is heated as high pressure and high temperature, and the multistage oxygen pressure gear engine 3Z is combusted in multiple stages to link the multistage water pressure gear engine 3N with multistage heating. A simple liquid water jet 80 is constructed in the process of exhaust by driving the screw 7C, the gas air compression of the existing reciprocating engine or gas turbine is liquid air compression, the compression work rate is 1/600, and the target is 100 times output. Combining various energy conservation cycles with medium speed large-sized screw ship 69D aiming at 10 times the speed of a ship and promoting natural phenomenon speedup 2a, aiming at 10 times the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate Institutions and coalescing methods.
図5の液体水吸引ウォータージェット80スクリュー船舶39D駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから受給して、液体酸素室5Kに液体酸素を受給保存し、液体窒素室5Lに液体0窒素を受給保存して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、5M+5Nにより夫々酸素圧力往復機関機関3Fや酸素圧力歯車機関3Zを駆動して、スクリュー7C駆動方向舵40Aで進行方向操舵し、5M+5Nにより液体水吸引ウォータージェット80Xを駆動して、噴射推進の過程で3Fや3Zの排気を80X最適圧力部に合流噴射し、3Fや3Zの回転出力でスクリュー7C駆動排気合流して、液体水吸引ウォータージェット80X合流噴射推進して自然現象高速化2aし、既存往復機関やガスタービンの気体空気圧縮を液体空気圧縮として、圧縮仕事率を1/600として100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、中大型液体水吸引ウォータージェット80スクリュー船舶39Dにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid water suction water jet 80 screw ship 39D drive in FIG. 5 will be described. The horizontal oxygen-operated water gravity turbine 8P power generation / electricity manufacturing of the horizontal type moving blade water gravity turbine 8P receives the electric oxygen + liquid air cold heat + superheated steam temperature supply equipment 3D, the liquid oxygen chamber Liquid oxygen is received and stored in 5K, liquid 0 nitrogen is received and stored in the liquid nitrogen chamber 5L, superheated steam 50 is received and stored in the high-pressure and high-temperature steam chamber 5N, and liquid nitrogen injection + liquid oxygen is supplied to the high-pressure and high-temperature combustion gas chamber 5M. High pressure and high temperature steam 5N on the outer periphery and inner periphery is heated by injection + fuel injection combustion, and addition of liquid nitrogen and water injection can be selected for each, and a high pressure and high temperature combustion gas chamber 5M of about 50 to 200 MPa 500 degrees or high pressure A high-temperature steam chamber 5N is used, and the oxygen pressure reciprocating engine 3F and the oxygen pressure gear engine 3Z are driven by 5M + 5N, respectively, and the traveling direction is steered by the screw 7C driving rudder 40A. The liquid water suction water jet 80X is driven by 5M + 5N, the 3F or 3Z exhaust gas is merged and injected into the 80X optimum pressure part in the process of injection propulsion, and the screw 7C drive exhaust gas is merged with the rotation output of 3F or 3Z. Water suction water jet 80X confluence injection speeds up natural phenomenon 2a, gas air compression of existing reciprocating engines and gas turbines is liquid air compression, compression work rate is 1/600 and the target is 100 times output, Combined with various energy conservation cycles, aiming at 10 times speed injection propulsion, same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate 10 times that of existing ship, medium-sized liquid water suction water jet 80 screw ship 39D Institutions and coalescing methods.
図6の液体水吸引ウォータージェット80船舶38C駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、5M+5Nにより液体水吸引ウォータージェット80Xを駆動して、液体水吸引ウォータージェット80船舶38Cを噴射推進して自然現象高速化2aし、海水中に窒素や酸素やCO2等を供給して、海中の微生物や海草類に食糧や栄養分供給海中資源を増大して、食物連鎖等で魚類やコンブ等人類の食糧を増大し、既存往復機関やガスタービンの気体空気圧縮を液体空気圧縮として、圧縮仕事率を1/600として100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、中大型液体水吸引ウォータージェット80船舶38Cにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid water suction water jet 80 ship 38C drive in FIG. 6 will be described. The high pressure and high temperature steam chamber is received from the electricity + liquid air cold heat + superheated steam temperature / heat supply facility 3D of the horizontal full-blade water gravity turbine 8P power generation electric manufacturing. The superheated steam 50 is received and stored in 5N, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. It is possible to select the addition of injection, and the high pressure high temperature combustion gas chamber 5M and the high pressure high temperature steam chamber 5N of about 50 to 200 MPa 500 degrees are set to 5N + 5N, and the liquid water suction water jet 80X is driven by 5M + 5N, and the liquid water suction water jet 80 ship 38C. To accelerate natural phenomena 2a, supply nitrogen, oxygen, CO2 etc. into seawater to feed microbes and seagrass in the sea for food and nutrition Increase the supply of underwater resources, increase food for humans such as fish and kombu in the food chain, etc., gas air compression of existing reciprocating engines and gas turbines as liquid air compression, compression work rate 1/600, output 100 times The aim is to make the jet propulsion aiming at 10 times the speed of the existing ship, the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate, aiming 10 times that of the existing ship, the medium-sized liquid water suction water jet 80 ship 38C, Various energy storage cycle coalescence engines and coalescence methods are used.
図7の液体空気吸引ウォータージェット80船舶38B駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、5M+5Nにより液体空気吸引ウォータージェット80Zを駆動して、液体空気吸引ウォータージェット80船舶38Bを噴射推進して自然現象高速化2aし、空気を吸引噴射することで海水中に窒素や酸素やCO2等を増大して供給して、海中の微生物や海草類に食糧や栄養分供給海中資源を増大して、食物連鎖等で魚類やコンブ等人類の食糧を増大し、既存往復機関やガスタービンの気体空気圧縮を液体空気圧縮として、圧縮仕事率を1/600として100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、中大型液体空気吸引ウォータージェット80船舶38Bにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid air suction water jet 80 ship 38B drive of FIG. 7 will be described. The high pressure high temperature steam chamber is received from the electricity + liquid air cold heat + superheated steam temperature / heat supply facility 3D of the horizontal all-blade water gravity turbine 8P power generation electric manufacturing. The superheated steam 50 is received and stored in 5N, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. The addition of injection can be selected, and the high-pressure and high-temperature combustion gas chamber 5M and the high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 degrees are set to 5M + 5N to drive the liquid air suction water jet 80Z, and the liquid air suction water jet 80 ship 38B. Speeds up natural phenomena 2a, and sucks and injects air to increase supply of nitrogen, oxygen, CO2, etc. into seawater As a result, the supply of food and nutrients to the microbes and seagrass in the sea is increased, the food of the human chain, such as fish and kombu, is increased in the food chain, etc. Medium-to-large size aiming at 100 times output with a compression work rate of 1/600, aiming at 10 times speed injection of existing ships, aiming at 10 times the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate of existing ships Liquid air suction water jet 80 ship 38B, various energy storage cycle coalescence engine and coalescence method.
図8の液体空気吸引ウォータージェット80スクリュー船舶39E駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから受給して、液体酸素室5Kに液体酸素を受給保存し、液体窒素室5Lに液体0窒素を受給保存して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、5M+5Nにより夫々酸素圧力往復機関機関3Fや酸素圧力歯車機関3Zを駆動して、スクリュー7C駆動方向舵40Aで進行方向操舵し、5M+5Nにより液体空気吸引ウォータージェット80Zを駆動して、噴射推進の過程で3Fや3Zの排気を80Z最適圧力部に合流噴射し、3Fや3Zの回転出力でスクリュー7C駆動排気合流して、液体空気吸引ウォータージェット80Z合流噴射推進して自然現象高速化2aし、既存往復機関やガスタービンの気体空気圧縮を液体空気圧縮として、圧縮仕事率を1/600として100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、中大型液体空気吸引ウォータージェット80スクリュー船舶39Eにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid air suction water jet 80 screw ship 39E drive in FIG. 8 will be described. The liquid oxygen chamber is received from the electricity + liquid air cold heat + superheated steam temperature heat supply facility 3D of the horizontal full-blade water gravity turbine 8P power generation electric manufacturing. Liquid oxygen is received and stored in 5K, liquid 0 nitrogen is received and stored in the liquid nitrogen chamber 5L, superheated steam 50 is received and stored in the high-pressure and high-temperature steam chamber 5N, and liquid nitrogen injection + liquid oxygen is supplied to the high-pressure and high-temperature combustion gas chamber 5M. High pressure and high temperature steam 5N on the outer periphery and inner periphery is heated by injection + fuel injection combustion, and addition of liquid nitrogen and water injection can be selected for each, and a high pressure and high temperature combustion gas chamber 5M of about 50 to 200 MPa 500 degrees or high pressure The high-temperature steam chamber is set to 5N, and the oxygen pressure reciprocating engine 3F and the oxygen pressure gear engine 3Z are driven by 5M + 5N, respectively, and the traveling direction steering is performed by the screw 7C driving direction rudder 40A. Then, the liquid air suction water jet 80Z is driven by 5M + 5N, the 3F or 3Z exhaust gas is merged and injected into the 80Z optimum pressure portion in the course of injection propulsion, and the screw 7C drive exhaust gas is merged with the rotation output of 3F or 3Z. Liquid air suction water jet 80Z merging jet propulsion to speed up natural phenomenon 2a, gas air compression of existing reciprocating engines and gas turbines is liquid air compression, compression work rate is 1/600 and the target is 100 times output. Various energy storage cycles, with medium-to-large liquid air suction water jet 80-screw ship 39E, aiming at 10 times the target speed of injection, aiming at 10 times the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate as existing ship Use a coalescence engine and coalescence method.
図9の液体合体噴射部80飛行機39A駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、5M+5Nにより液体合体噴射部80Fを駆動ロケット噴射して、液体合体噴射部80飛行機39Aを噴射推進し、既存ガスタービンの気体空気圧縮を液体空気圧縮として、圧縮仕事率を1/600燃料燃焼量10倍以上を容易として1000倍出力狙いとし、宇宙上昇時には短時間1000倍出力ロケット噴射宇宙到達確実として、宇宙到達費用を既存の1/50万等僅少にし、液体合体噴射部80飛行機39Aで燃料費0に近い宇宙利用全盛にして、1日に地球を16周する等地球上何処でも日帰り旅行を可能にし、大気中を飛行時には燃料費僅少として、噴射速度が真空で最大のため既存宇宙ロケット地上大量噴射を最悪と考え、既存飛行機最高飛行高度で大出力ロケット推進する方法で宇宙に到達し、地球帰還時には液体合体噴射部80F円筒回転部77Gを180度等回転して、逆噴射減速地球帰還や重力加速度対応や垂直上昇垂直降下を可能にし、宇宙利用やビルの屋上や月面等何処でも飛行場にする方法にして、各種エネルギ保存サイクル合体機関及び合体方法にする。 9 will be described. The high pressure / high temperature steam chamber 5N received from the electricity + liquid air cold / superheated steam temperature / heat supply facility 3D of the horizontal all-blade water gravity turbine 8P power generation / electricity manufacturing will be described. The superheated steam 50 is received and stored in the high-pressure and high-temperature combustion gas chamber 5M, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed to heat the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery, and liquid nitrogen and water injection respectively. The high pressure high temperature combustion gas chamber 5M and the high pressure high temperature steam chamber 5N of about 50 to 200 MPa 500 degrees are made into 5N + 5N, and the liquid combined injection unit 80F is driven rocket-injected by 5M + 5N. Injecting propulsion, gas-air compression of existing gas turbines is liquid-air compression, compression work rate is 1/600, fuel combustion amount is more than 10 times easier, and output is 1000 times In order to make sure that the rocket will reach the space for a short time 1000 times output when the space rises, the space arrival cost will be reduced to 1 / 500,000, etc. It enables day trips anywhere on the earth, such as 16 rounds of the earth per day, fuel costs are minimal when flying in the atmosphere, and the existing jets are considered the worst because the jet speed is the highest in vacuum and the existing space rocket ground injection is the worst. Reach the space by propelling high power rockets at the highest flight altitude, and when returning to the earth, rotate the liquid coalesced injection part 80F cylindrical rotating part 77G by 180 degrees, reverse injection deceleration earth return, gravity acceleration support, vertical ascending vertical descent The energy storage cycle coalescence engine and the coalescence method are made into a method of making the airfield anywhere such as space use, building rooftop or moon surface.
図10の液体合体噴射部80回転飛行機39B駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、5M+5Nにより液体合体噴射部80Fを駆動ロケット噴射して、液体合体噴射部80飛行機39Aを噴射推進し、既存ガスタービンの気体空気圧縮を液体空気圧縮として、圧縮仕事率を1/600燃料燃焼量10倍以上を容易として1000倍出力狙いとし、宇宙上昇時には短時間1000倍出力ロケット噴射宇宙到達確実として、宇宙到達費用を既存の1/50万等僅少にし、液体合体噴射部80飛行機39Aで燃料費0に近い宇宙利用全盛にして、1日に地球を16周する等地球上何処でも日帰り旅行を可能にします。 10 will be described. The high pressure and high temperature steam chamber is received from the electric + liquid air cold heat + superheated steam temperature heat supply equipment 3D of the horizontal all-blade water gravity turbine 8P power generation electric manufacturing. The superheated steam 50 is received and stored in 5N, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. Addition of injection is made selectable, and a high-pressure high-temperature combustion gas chamber 5M or a high-pressure high-temperature steam chamber 5N of about 50 to 200 MPa 500 degrees is formed into a high-pressure high-temperature steam chamber 5N. The gas air compression of the existing gas turbine is liquid air compression, the compression work rate is 1/600, and the fuel combustion amount is 10 times or more easy. When aiming for output, assured that the rocket will reach the universe for 1000 times in a short time when the universe rises, the space arrival cost will be reduced to 1 / 500,000, etc. This makes it possible to make day trips anywhere on the earth, such as 16 rounds of the earth per day.
大気中を飛行時には、5M+5Nにより夫々酸素圧力往復機関機関3Fや酸素圧力歯車機関3Zを駆動して、夫々プロペラ7A駆動方向舵40Aで進行方向操舵し、5M+5Nにより液体合体噴射部80Fを駆動して、噴射推進の過程で3Fや3Zの排気を80F最適圧力部に合流噴射し、3Fや3Zの回転出力でプロペラ7A駆動排気合流して、液体合体噴射部80F合流噴射推進し燃料費僅少とし、噴射速度が真空で最大のため既存宇宙ロケット地上大量噴射を最悪と考え、既存飛行機最高飛行高度で大出力ロケット推進する方法で宇宙に到達し、地球帰還時には液体合体噴射部80F円筒回転部77Gを180度等回転して、逆噴射減速地球帰還や重力加速度対応や垂直上昇垂直降下を可能にし、宇宙利用やビルの屋上や月面等何処でも飛行場にする方法にして、各種エネルギ保存サイクル合体機関及び合体方法にする。 When flying in the atmosphere, the oxygen pressure reciprocating engine 3F and the oxygen pressure gear engine 3Z are driven by 5M + 5N, respectively, the traveling direction steering is driven by the propeller 7A driving direction rudder 40A, and the liquid combined injection unit 80F is driven by 5M + 5N, In the process of injection propulsion, the 3F or 3Z exhaust is combined and injected into the 80F optimum pressure part, and the propeller 7A drive exhaust is combined with the rotation output of 3F or 3Z, and the liquid combined injection part 80F is combined and propelled to reduce fuel cost. Since the speed is the maximum at vacuum, the existing space rocket ground mass injection is considered the worst, and it reaches the space by the method of propelling the high output rocket at the highest flight altitude of the existing airplane. Rotate the same angle to allow reverse injection deceleration earth return, gravitational acceleration response, vertical ascending and vertical descent, anywhere in space use, building rooftop, moon surface etc. In the way to the airport, to a variety of energy storage cycle combined institutions and coalescence method.
図11の酸素圧力往復機関3F駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから受給して、液体酸素室5Kに液体酸素を受給保存し、液体窒素室5Lに液体窒素を受給保存して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、酸素圧力往復機関3Fと同様に外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、高圧高温燃焼ガス制御弁5a開放して、往復圧縮機の吸入路を1段燃焼室1Yとした酸素圧力往復機関3Fに高圧高温燃焼ガス5Mを供給し、燃料噴射ノズル6Xより燃料噴射燃焼高圧高温として往復ピストン3Hを移動駆動して、反対側2段燃焼室1Y排気室5Cの排気弁5Dを開放し、3段燃焼室1Yに高圧高温燃焼ガス5Mを供給3段燃焼や4段燃焼にして、次の酸素圧力往復機関3Fを次次に駆動する構成にし、次次に駆動する過程で内周や外周の水圧力往復機関3Mの高圧高温水蒸気5Nを加熱して、3Fと同様に多段水圧力往復機関3Mを多段加熱連動し、夫々の回転出力を合体してプロペラ7Aや回転翼7Bやスクリュー7C駆動して、排気の過程では簡単液体ウォータージェット80を構成や、簡単液体合体噴射部80を構成や、液体ウォータージェット80や液体合体噴射部80最適圧力部に合流を選択可能にする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The oxygen pressure reciprocating engine 3F drive in FIG. 11 will be described. The oxygen is received from the electric + liquid air cold heat + superheated steam temperature heat supply equipment 3D of the horizontal full-blade water gravity turbine 8P power generation electric manufacture, and the liquid oxygen chamber 5K receives liquid oxygen. Is received and stored, liquid nitrogen is received and stored in the liquid nitrogen chamber 5L, superheated steam 50 is received and stored in the high-pressure and high-temperature steam chamber 5N, and liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is stored in the high-pressure and high-temperature combustion gas chamber 5M. Then, like the oxygen reciprocating engine 3F, the high-pressure high-temperature steam 5N on the outer periphery and the inner periphery is heated, and the addition of liquid nitrogen and water injection can be selected for each, and the high-pressure high-temperature combustion gas chamber of about 50 to 200 MPa 500 degrees 5M or high-pressure high-temperature steam chamber 5N, high-pressure high-temperature combustion gas control valve 5a is opened, and high-pressure high-temperature combustion gas 5M is supplied to oxygen pressure reciprocating engine 3F in which the suction passage of the reciprocating compressor is the first-stage combustion chamber 1Y. The reciprocating piston 3H is moved and driven from the fuel injection nozzle 6X as a fuel injection combustion high pressure and high temperature, the exhaust valve 5D of the opposite side second stage combustion chamber 1Y exhaust chamber 5C is opened, and the high pressure high temperature combustion gas 5M is supplied to the third stage combustion chamber 1Y. In the configuration in which the next oxygen pressure reciprocating engine 3F is driven one after another in the three-stage combustion or the four-stage combustion, the high-pressure and high-temperature steam 5N of the water pressure reciprocating engine 3M on the inner and outer circumferences is driven in the next driving process. In the same way as 3F, the multi-stage water pressure reciprocating engine 3M is interlocked with the multi-stage heating, and the rotation outputs are combined to drive the propeller 7A, the rotor blade 7B, and the screw 7C. Various energy storage cycle coalescence engines and coalescence that make it possible to select the merging in the configuration, the simple liquid coalescence injection unit 80, the liquid water jet 80 or the liquid coalescence injection unit 80 optimum pressure part To the law.
図12の酸素圧力歯車機関3Z駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dから受給して、液体酸素室5Kに液体酸素を受給保存し、液体窒素室5Lに液体窒素を受給保存して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、酸素圧力往復機関3Fと同様に外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、高圧高温燃焼ガス制御弁5a開放して、歯車ポンプの吸入路を1段燃焼室1Yとした酸素圧力歯車機関3Zに高圧高温燃焼ガス5Mを供給し、燃料噴射ノズル6Xより燃料噴射燃焼高圧高温として往復ピストン3Hを移動駆動して、反対側2段燃焼室1Y排気室5Cの排気弁5Dを開放し、3段燃焼室1Yに高圧高温燃焼ガス5Mを供給3段燃焼や4段燃焼にして、次の酸素圧力往復機関3Fを次次に駆動する構成にし、次次に駆動する過程で内周や外周の水圧力歯車機関3Nの高圧高温水蒸気5Nを加熱して、3Zと同様に多段水圧力歯車機関3Nを多段加熱連動し、夫々の回転出力を合体してプロペラ7Aや回転翼7Bやスクリュー7C駆動して、排気の過程では簡単液体ウォータージェット80を構成や、簡単液体合体噴射部80を構成や、液体ウォータージェット80や液体合体噴射部80最適圧力部に合流を選択可能にする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The oxygen pressure gear engine 3Z drive of FIG. 12 will be explained. The oxygen is received from the electric + liquid air cold heat + superheated steam temperature heat supply equipment 3D of the horizontal full-blade water gravity turbine 8P power generation electric manufacture, and the liquid oxygen chamber 5K receives liquid oxygen. Is received and stored, liquid nitrogen is received and stored in the liquid nitrogen chamber 5L, superheated steam 50 is received and stored in the high-pressure and high-temperature steam chamber 5N, and liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is stored in the high-pressure and high-temperature combustion gas chamber 5M. Then, like the oxygen reciprocating engine 3F, the high-pressure high-temperature steam 5N on the outer periphery and the inner periphery is heated, and the addition of liquid nitrogen and water injection can be selected for each, and the high-pressure high-temperature combustion gas chamber of about 50 to 200 MPa 500 degrees 5M or high-pressure high-temperature steam chamber 5N, high-pressure high-temperature combustion gas control valve 5a is opened, and high-pressure high-temperature combustion gas 5M is supplied to oxygen pressure gear engine 3Z in which the suction path of the gear pump is the first-stage combustion chamber 1Y. The reciprocating piston 3H is moved and driven from the fuel injection nozzle 6X as a fuel injection combustion high pressure and high temperature, the exhaust valve 5D of the opposite side second stage combustion chamber 1Y exhaust chamber 5C is opened, and the high pressure high temperature combustion gas 5M is supplied to the third stage combustion chamber 1Y. In the configuration in which the next oxygen pressure reciprocating engine 3F is driven successively by the supply three-stage combustion or the four-stage combustion, the high-pressure high-temperature steam 5N of the inner or outer water-pressure gear engine 3N is supplied in the next driving process. In the same way as 3Z, the multistage water pressure gear engine 3N is interlocked with the multistage heating, and the rotation outputs are combined to drive the propeller 7A, the rotor blade 7B and the screw 7C. Various energy storage cycle coalescence engines and coalescence that make it possible to select the merging in the configuration, the simple liquid coalescence injection unit 80, the liquid water jet 80 or the liquid coalescence injection unit 80 optimum pressure part To the law.
図13の液体水吸引ウォータージェット80U駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段燃料噴射ノズル6Xより燃料噴射2段燃焼して内周の5N水蒸気50Aを加熱して、3段燃料噴射ノズル6Xより燃料噴射3段燃焼して内周外周の水蒸気50Aを加熱し、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射夫々で水52a吸引噴射し、液体水吸引ウォータージェット80Uとして、空気の圧縮仕事率を1/600として超高圧大量燃焼100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、液体水吸引ウォータージェット80Uにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid water suction water jet 80U drive in FIG. 13 will be described. The horizontal full-blade water gravity turbine 8P power generation electric manufacturing receives electricity + liquid air cold heat + superheated steam temperature supply equipment 3D, and enters the high-pressure high-temperature steam chamber 5N. The superheated steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. Addition is made selectable, and a high-pressure and high-temperature combustion gas chamber 5M or a high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 ° C. is supplied to the superheated steam reservoir 95c. The combustion gas 5M is supplied to the first-stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel injection one-stage combustion from the fuel control valve 25b open fuel injection nozzle 6X. Two-stage fuel injection from the two-stage fuel injection nozzle 6X burns the inner peripheral 5N water vapor 50A, three-stage fuel injection from the three-stage fuel injection nozzle 6X three-stage combustion heats the inner peripheral outer circumference water vapor 50A, and the water vapor Steam 50A is injected from the injection nozzle 6Z, combustion gas 49 is injected from the combustion gas injection nozzle 6Y by water 52a, and the liquid water suction water jet 80U is used as a liquid water suction water jet 80U. The target is 100 times the combustion output, the target is 10 times the target jet propulsion, the same speed CO2 exhaust 1/10 fuel cost 1/10 the operating profit ratio is 10 times the existing ship, the liquid water suction water jet 80U, Various energy storage cycle coalescence engines and coalescence methods are used.
図14の液体水吸引ウォータージェット80X駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段燃料噴射ノズル6Xより燃料噴射2段燃焼して内周外周の5N水蒸気50Aを加熱して、3段や4段の燃料噴射ノズル6Xより燃料噴射3段4段燃焼で夫々内周外周の水蒸気50Aを加熱し、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射夫々で水52a吸引噴射し、液体水吸引ウォータージェット80Uとして、空気の圧縮仕事率を1/600として超高圧大量燃焼100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、液体水吸引ウォータージェット80Uにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid water suction water jet 80X driving in FIG. 14 will be described. The horizontal water-blade hydrogravity turbine 8P power generation electric manufacturing receives the electric + liquid air cold heat + superheated steam temperature supply equipment 3D, and enters the high-pressure high-temperature steam chamber 5N. The superheated steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. Addition is made selectable, and a high-pressure and high-temperature combustion gas chamber 5M or a high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 ° C. is supplied to the superheated steam reservoir 95c. The combustion gas 5M is supplied to the first-stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel injection one-stage combustion from the fuel control valve 25b open fuel injection nozzle 6X. Two-stage fuel injection nozzle 6X performs two-stage fuel injection and heats 5N water vapor 50A on the inner and outer circumferences, and three-stage and four-stage fuel injection nozzles 6X perform fuel injection three-stage and four-stage combustion, respectively. Water vapor 50A is heated, water vapor 50A is injected from the water vapor injection nozzle 6Z, and combustion gas 49 is injected from the combustion gas injection nozzle 6Y by water 52a. Liquid water aiming at 1/600 with 100 times the output of ultra high pressure mass combustion, aiming at 10 times speed injection propulsion of the existing ship, the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate 10 times that of the existing ship A suction water jet 80U is used, and various energy storage cycle coalescence engines and coalescence methods are used.
図15の液体空気吸引ウォータージェット80S駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段燃料噴射ノズル6Xより燃料噴射2段燃焼して内周の5N水蒸気50Aを加熱して、3段燃料噴射ノズル6Xより燃料噴射3段燃焼で内周外周の水蒸気50Aを加熱し、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射、夫々で空気28aを吸引噴射で水52a吸引噴射し、液体空気吸引ウォータージェット80Sとして、空気の圧縮仕事率を1/600として超高圧大量燃焼100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、液体空気吸引ウォータージェット80Sにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid air suction water jet 80S drive in FIG. 15 will be described. The horizontal air / water turbine 8P power generation / electricity manufacturing of the horizontal full-blade water gravity turbine 8P receives from the electricity + liquid air cold / superheated steam temperature supply facility 3D, and enters the high pressure / high temperature steam chamber 5N. The superheated steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. Addition is made selectable, and a high-pressure and high-temperature combustion gas chamber 5M or a high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 ° C. is supplied to the superheated steam reservoir 95c. The combustion gas 5M is supplied to the first stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel injection one stage combustion from the fuel control valve 25b open fuel injection nozzle 6X. Two-stage fuel injection from the two-stage fuel injection nozzle 6X burns the inner peripheral 5N water vapor 50A, and the three-stage fuel injection nozzle 6X heats the inner and outer peripheral water vapor 50A by three-stage fuel injection. Water vapor 50A is injected from the injection nozzle 6Z, combustion gas 49 is injected from the combustion gas injection nozzle 6Y, air 28a is sucked and injected into the water 52a, and the liquid air suction water jet 80S is used as the liquid air suction water jet 80S. Liquid air that aims at 1/600, 100 times the output of ultra-high pressure mass combustion, 10% speed target injection propulsion of the existing ship, the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate 10 times that of the existing ship Various energy storage cycle coalescence engines and coalescence methods are used for the suction water jet 80S.
図16の液体空気吸引ウォータージェット80T駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段燃料噴射ノズル6Xより燃料噴射2段燃焼して内周の5N水蒸気50Aを加熱して、3段燃料噴射ノズル6Xより燃料噴射3段燃焼で内周外周の水蒸気50Aを加熱し、外周空気吸引流複数個所に4段燃料噴射ノズル6X燃料噴射燃焼して内周水蒸気50Aを加熱して、水蒸気噴射ノズル6Zより水蒸気50A噴射し、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射して、夫々で空気28aを吸引噴射で水52a吸引噴射し、液体空気吸引ウォータージェット80Sとして、空気の圧縮仕事率を1/600として超高圧大量燃焼100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、液体空気吸引ウォータージェット80Tにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid air suction water jet 80T drive in FIG. 16 will be described. The horizontal air / water turbine 8P power generation / electricity production of the horizontal full-blade water gravity turbine 8P receives from the electricity + liquid air cold / superheated steam temperature supply facility 3D, and enters the high pressure / high temperature steam chamber 5N. The superheated steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. Addition is made selectable, and a high-pressure and high-temperature combustion gas chamber 5M or a high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 ° C. is supplied to the superheated steam reservoir 95c. The combustion gas 5M is supplied to the first-stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel injection one-stage combustion from the fuel control valve 25b open fuel injection nozzle 6X. Two-stage fuel injection from the two-stage fuel injection nozzle 6X burns the inner peripheral 5N water vapor 50A, and the three-stage fuel injection nozzle 6X heats the inner and outer peripheral water vapor 50A by three-stage fuel injection. Four-stage fuel injection nozzle 6X fuel injection combustion in a plurality of locations of the air suction flow to heat the inner circumferential water vapor 50A, inject water vapor 50A from the water vapor injection nozzle 6Z, inject combustion gas 49 from the combustion gas injection nozzle 6Y, In each case, the air 28a is sucked and injected into the water 52a by suction injection, and the liquid air suction water jet 80S is set to aim at 100 times output of ultrahigh-pressure mass combustion with 1/600 of the compression work rate of air, and 10 times speed target injection of the existing ship. Propulsion, the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate Targeting 10 times that of existing ships, liquid air suction water jet 80T, various To Nerugi save cycle combined institutions and coalescence method.
図17の液体空気吸引ウォータージェット80Y駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段燃料噴射ノズル6Xより燃料噴射2段燃焼して内周外周の5N水蒸気50Aを加熱して、同様に3段や4段の燃料噴射ノズル6Xより燃料噴射3段4段燃焼で内周外周の水蒸気50Aを加熱し、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射し、夫々で空気28aを吸引噴射で水52a吸引噴射して、液体空気吸引ウォータージェット80Yとし、空気の圧縮仕事率を1/600や酸素量増大として、超高圧大量燃焼100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、液体空気吸引ウォータージェット80Yにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The driving of the liquid air suction water jet 80Y in FIG. 17 will be described. It is received from the electricity + liquid air cold heat + superheated steam temperature supply facility 3D of the horizontal full-blade water gravity turbine 8P power generation electric manufacture, and is supplied to the high pressure / high temperature steam chamber 5N. The superheated steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. Addition is made selectable, a high-pressure high-temperature combustion gas chamber 5M or a high-pressure high-temperature steam chamber 5N of about 50 to 200 MPa 500 ° C. is supplied, and the steam control valve 5P open steam 50A is supplied to the superheated steam reservoir 95c. The combustion gas 5M is supplied to the first stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel injection one stage combustion from the fuel control valve 25b open fuel injection nozzle 6X. Two-stage fuel injection from the two-stage fuel injection nozzle 6X burns two stages of fuel injection and heats the 5N water vapor 50A on the inner and outer periphery. The water vapor 50A on the outer periphery is heated, the water vapor 50A is injected from the water vapor injection nozzle 6Z, the combustion gas 49 is injected from the combustion gas injection nozzle 6Y, and the air 28a is sucked and injected into the water 52a by suction injection, respectively. Water jet 80Y, air compression work rate of 1/600 and oxygen amount increase, super high pressure mass combustion 100 times output target, 10 times speed target injection propulsion of existing ship, same speed CO2 exhaust 1/10 fuel Cost 1/10 Operational profit ratio A liquid air suction water jet 80Y aimed at 10 times that of an existing ship, combined with various energy storage cycle coalescence engines and coalescence methods.
図18の液体空気吸引ウォータージェット80Z駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段3段4段燃料噴射ノズル6Xより燃料噴射2段3段4段燃焼して内周外周の5N水蒸気50Aを加熱して、外周空気28a吸引流の燃料噴射ノズル6Xより燃料噴射5段燃焼で内周の水蒸気50Aを加熱し、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射し、夫々で空気28aを吸引噴射で水52a吸引噴射して、液体空気吸引ウォータージェット80Zとし、空気の圧縮仕事率を1/600や酸素量増大として、超高圧大量燃焼100倍出力狙いとし、既存船舶の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存船舶の10倍狙う、液体空気吸引ウォータージェット80Zにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The liquid air suction water jet 80Z driving in FIG. 18 will be described. The horizontal air / water blade / gravity turbine 8P power generation / electricity production of electric / liquid air cold / superheated steam / heat supply equipment 3D receives the high pressure / high temperature steam chamber 5N. The superheated steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion is performed in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery is heated. Addition is made selectable, a high-pressure high-temperature combustion gas chamber 5M or a high-pressure high-temperature steam chamber 5N of about 50 to 200 MPa 500 ° C. is supplied, and the steam control valve 5P open steam 50A is supplied to the superheated steam reservoir 95c. The combustion gas 5M is supplied to the first stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel injection one stage combustion from the fuel control valve 25b open fuel injection nozzle 6X. Two-stage, three-stage, and four-stage fuel injection nozzles 6X burn fuel, two-stage, three-stage, and four-stage combustion heat 5N water vapor 50A on the inner and outer circumferences, and fuel injection five-stage from the fuel injection nozzle 6X that sucks the outer peripheral air 28a. The water vapor 50A on the inner circumference is heated by combustion, the water vapor 50A is injected from the water vapor injection nozzle 6Z, the combustion gas 49 is injected from the combustion gas injection nozzle 6Y, and the air 28a is sucked and injected by the water 52a by suction injection, respectively. Liquid air suction water jet 80Z, air compression work rate 1/600, oxygen amount increase, super high pressure mass combustion 100 times output target, 10% speed target injection propulsion of existing ship, same speed CO2 exhaust 1 / 10 Fuel Cost 1/10 Operating Profit Ratio Targeting 10 times that of existing ships, liquid air suction water jet 80Z, various energy storage cycle coalescence engine and coalescence method That.
図19の液体合体噴射部80W駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段燃料噴射ノズル6Xより燃料噴射2段燃焼して内周の5N水蒸気50Aを加熱して、3段燃料噴射ノズル6Xより燃料噴射3段燃焼して内周外周の水蒸気50Aを加熱し、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射夫々で空気28a吸引噴射し、液体合体噴射部80Wとして、空気の圧縮仕事率を1/600や酸素量増大として超高圧大量燃焼100倍出力狙いとし、既存飛行機の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10とし、運用利益率既存飛行機の10倍狙う、液体合体噴射部80Wにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 Referring to FIG. 19, the liquid coalescence injection unit 80W drive is received from the electric + liquid air cold heat + superheated steam temperature supply facility 3D of the horizontal all-blade water gravity turbine 8P power generation electric manufacturing, and the high pressure and high temperature steam chamber 5N is superheated. Steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery are heated, and liquid nitrogen and water injection are added respectively. The high-pressure and high-temperature combustion gas chamber 5M and the high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 degrees are supplied, the steam control valve 5P open steam 50A is supplied to the superheated steam reservoir 95c, and the combustion gas control valve 24 is opened high-pressure and high-temperature combustion. Gas 5M is supplied to the first-stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel-injection one-stage combustion from the fuel control valve 25b open fuel injection nozzle 6X, and two-stage fuel injection is performed. Two-stage fuel injection from the nozzle 6X heats the 5N water vapor 50A on the inner periphery, three-stage fuel injection from the three-stage fuel injection nozzle 6X heats the water vapor 50A on the inner and outer periphery, and from the water vapor injection nozzle 6Z. Steam 50A is injected, combustion gas 49 is injected from the combustion gas injection nozzle 6Y, and air 28a is sucked and injected as a liquid coalescence injection unit 80W. The target is 100 times output, the target is 10 times the speed of the existing airplane, and the same speed CO2 exhaust 1/10 fuel cost is 1/10, and the operating profit ratio is 10 times that of the existing airplane. Various energy storage cycle coalescence engines and coalescence methods are used.
図20の液体合体噴射部80V駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段燃料噴射ノズル6Xより燃料噴射2段燃焼して内周の5N水蒸気50Aを加熱して、3段燃料噴射ノズル6Xより燃料噴射3段燃焼して内周外周の水蒸気50Aを加熱し、外周空気28a吸引流の燃料噴射ノズル6X複数より燃料噴射4段燃焼して、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射夫々で空気28a吸引噴射し、液体合体噴射部80Vとして、空気の圧縮仕事率を1/600や酸素量増大として超高圧大量燃焼100倍出力狙いとし、既存飛行機の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10とし、運用利益率既存飛行機の10倍狙う、液体合体噴射部80Wにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 Referring to FIG. 20, the liquid combined injection unit 80V drive is received from the electricity + liquid air cold heat + superheated steam temperature heat supply facility 3D of the horizontal all-blade water gravity turbine 8P power generation electric manufacturing, and the high pressure / high temperature steam chamber 5N is superheated. Steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery are heated, and liquid nitrogen and water injection are added respectively. The high-pressure and high-temperature combustion gas chamber 5M and the high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 ° C. are supplied, the steam control valve 5P open steam 50A is supplied to the superheated steam reservoir 95c, and the combustion gas control valve 24 is opened high-pressure and high-temperature combustion. Gas 5M is supplied to the first-stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel-injection one-stage combustion from the fuel control valve 25b open fuel injection nozzle 6X, and two-stage fuel injection is performed. Two-stage fuel injection from the nozzle 6X heats the inner peripheral 5N water vapor 50A, three-stage fuel injection from the three-stage fuel injection nozzle 6X heats the inner peripheral outer water vapor 50A, and the outer air 28a suction flow The fuel injection nozzle 6X burns four stages of fuel injection, the steam injection nozzle 6Z injects 50A of steam, the combustion gas 49 injects the combustion gas 49 from the combustion gas injection nozzle 6Y, and the liquid combined injection unit 80V Assuming that the compression work rate of air is 1/600 and the oxygen amount is increased, aiming at 100 times output of ultra-high pressure mass combustion, aiming at 10 times speed target injection propulsion of the existing airplane, the same speed CO2 exhaust 1/10 fuel cost 1/10 The operating profit rate is 10 times that of existing airplanes, and the liquid coalescence injection unit 80W is used, and various energy storage cycle coalescence engines and coalescence methods are used.
図21の液体合体噴射部80E駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段燃料噴射ノズル6Xより燃料噴射2段燃焼して内周外周の5N水蒸気50Aを加熱して、同様に3段や4段の燃料噴射ノズル6Xより燃料噴射3段4段燃焼で内周外周の水蒸気50Aを加熱し、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射し、夫々で前方の空気28aを吸引噴射して、液体合体噴射部80Eとし、空気の圧縮仕事率を1/600や酸素量増大として、超高圧大量燃焼100倍出力狙いとし、既存飛行機の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存飛行機の10倍狙う、液体合体噴射部80Eにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The driving of the liquid coalescence injection unit 80E shown in FIG. 21 will be described. The high pressure / high temperature steam chamber 5N is superheated by receiving it from the electricity + liquid air cold heat + superheated steam temperature heat supply facility 3D of the horizontal full-blade water gravity turbine 8P power generation electric manufacturing. Steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery are heated, and liquid nitrogen and water injection are added respectively. The high-pressure and high-temperature combustion gas chamber 5M and the high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 ° C. are supplied, the steam control valve 5P open steam 50A is supplied to the superheated steam reservoir 95c, and the combustion gas control valve 24 is opened high-pressure and high-temperature combustion. Gas 5M is supplied to the first-stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel-injection one-stage combustion from the fuel control valve 25b open fuel injection nozzle 6X, and two-stage fuel injection is performed. Two-stage fuel injection from the nozzle 6X burns and heats the 5N water vapor 50A on the inner and outer circumferences. Similarly, three-stage and four-stage fuel injection nozzles 6X produce three-stage and four-stage fuel injections to produce the inner and outer water vapor 50A. After heating, 50 A of water vapor is injected from the water vapor injection nozzle 6Z, the combustion gas 49 is injected from the combustion gas injection nozzle 6Y, and the air 28a in front is sucked and injected to form the liquid combined injection unit 80E. The rate is 1/600 and the oxygen amount is increased, aiming at 100 times the output of ultra-high pressure mass combustion, aiming at 10 times the target jet injection of the existing aircraft, the same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate The liquid coalescence injection unit 80E is aimed at 10 times the energy storage cycle coalescence engine and the coalescence method.
図22の液体合体噴射部80F駆動を説明すると、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより受給して、高圧高温水蒸気室5Nに過熱蒸気50を受給保存し、高圧高温燃焼ガス室5Mに液体窒素噴射+液体酸素噴射+燃料噴射燃焼して、外周や内周の高圧高温水蒸気5Nを加熱し、夫々に液体窒素や水噴射の追加を選択可能にして、50〜200MPa500度前後の高圧高温燃焼ガス室5Mや高圧高温水蒸気室5Nにし、水蒸気制御弁5P開放水蒸気50Aを過熱蒸気溜95cに供給、燃焼ガス制御弁24開放高圧高温燃焼ガス5Mを1段燃焼室1Yに供給して、燃料制御弁25b開放燃料噴射ノズル6Xより燃料噴射1段燃焼で外周5Nの水蒸気50Aを加熱し、2段3段4段燃料噴射ノズル6Xより燃料噴射2段3段4段燃焼して内周外周の5N水蒸気50Aを加熱して、外周空気28a吸引流の燃料噴射ノズル6Xより燃料噴射5段燃焼で内周の水蒸気50Aを加熱し、水蒸気噴射ノズル6Zより水蒸気50A噴射して、燃焼ガス噴射ノズル6Yより燃焼ガス49を噴射し、夫々で空気28aを吸引噴射して、液体合体噴射部80Fとし、空気の圧縮仕事率を1/600や酸素量増大として、超高圧大量燃焼100倍出力狙いとし、既存飛行機の10倍速度狙い噴射推進にして、同一速度CO2排気1/10燃料費1/10運用利益率既存飛行機の10倍狙う、液体合体噴射部80Fにする、各種エネルギ保存サイクル合体機関及び合体方法にする。 The driving of the liquid coalescence injection unit 80F shown in FIG. 22 will be described. The horizontal combined rotor water gravity turbine 8P power generation electric manufacturing receives electricity + liquid air cold heat + superheated steam temperature supply equipment 3D, and superheats the high pressure and high temperature steam chamber 5N. Steam 50 is received and stored, liquid nitrogen injection + liquid oxygen injection + fuel injection combustion in the high-pressure and high-temperature combustion gas chamber 5M, and the high-pressure and high-temperature steam 5N on the outer periphery and inner periphery are heated, and liquid nitrogen and water injection are added respectively. The high-pressure and high-temperature combustion gas chamber 5M and the high-pressure and high-temperature steam chamber 5N of about 50 to 200 MPa 500 degrees are supplied, the steam control valve 5P open steam 50A is supplied to the superheated steam reservoir 95c, and the combustion gas control valve 24 is opened high-pressure and high-temperature combustion. Gas 5M is supplied to the first-stage combustion chamber 1Y, and the water vapor 50A on the outer periphery 5N is heated by the fuel injection one-stage combustion from the fuel control valve 25b open fuel injection nozzle 6X, and two stages, three stages, and four stages. The fuel injection nozzle 6X burns the fuel injection in two stages, three stages, and four stages to heat the outer peripheral 5N water vapor 50A, and from the fuel injection nozzle 6X that sucks the outer air 28a, the fuel injection nozzle 6X burns the inner peripheral water vapor 50A. , The steam 50A is jetted from the steam jet nozzle 6Z, the combustion gas 49 is jetted from the combustion gas jet nozzle 6Y, and the air 28a is sucked and jetted to form the liquid combined jet section 80F. Is 1/600 or oxygen increase, super high pressure mass combustion is aimed at 100 times output, and 10 times speed target injection propulsion of existing airplane, same speed CO2 exhaust 1/10 fuel cost 1/10 operating profit rate Various energy storage cycle coalescence engines and coalescence methods are used, aiming at 10 times, to make the liquid coalescence injection unit 80F.
理論最良タービン発電を横型全動翼水重力タービン8P発電として、大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービン発電の1700倍水仕事率発電にし、既存のボイラや原子炉を不要として、構造を非常に簡単にして既存発電量の1700倍発電量を非常に容易し、燃料費0CO2排気0で地球温暖化防止する極端に安価な電気として、電気の用途開発無限大とし、横型全動翼水重力タービン8P発電電気製造の、電気+液体空気冷熱+過熱蒸気温熱供給設備3Dより供給して、例えば永久凍土地下のメタンハイドレートに過熱蒸気温熱を注入し、メタンと高温水に分割メタンは冷却液体メタンで回収して、過熱蒸気注入は永遠に継続メタン回収囲い内を適温として水滴の多い牧草地放牧とし、永久凍土地帯全部を牧草地として放牧全盛にする可能性がある。 Theoretical best turbine power generation is a horizontal full-blade water gravity turbine 8P power generation, the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / sec. , Making the structure very simple, making the power generation 1700 times the existing power generation very easy, and extremely low-cost electricity to prevent global warming with 0 CO2 exhaust 0, and the use of electricity is infinite Supplied from 3D of electricity + liquid air cold heat + superheated steam temperature supply equipment of horizontal all blade hydrogravity turbine 8P power generation electricity production, for example, superheated steam temperature heat is injected into methane hydrate under permafrost, methane and high temperature Split methane into water is recovered with chilled liquid methane, and superheated steam injection is continued forever.The methane recovery enclosure is kept at a suitable temperature for pasture grazing with many water droplets, and the entire permafrost zone is used as pasture. There is a possibility that the grazing flourish.
横型全動翼水重力タービン8P燃料費0発電で海水温度7度上昇を阻止し、地震津波の人為的巨大化を阻止して地震津波を限り無く縮小して、台風や季節風や竜巻等の人為的な上昇気流の巨大化を阻止して下降気流の巨大化を阻止し、旱魃や集中豪雨や異常乾燥山火事や寒波や熱波の巨大化を阻止して、地経温暖化防止する可能性がある。 Horizontal full blade hydrogravity turbine 8P Fuel cost 0 power generation prevents the seawater temperature from rising by 7 degrees, prevents the artificial tsunami from becoming huge, and reduces the earthquake tsunami to an unlimited extent. Potential to prevent global warming by preventing drastic increase in downdraft, preventing drought, torrential rain, abnormal dry forest fire, cold wave and heat wave There is.
既存火力発電+原子力発電により海水温度を7度上昇し、海面冷却海底に酸素等の栄養分を供給の自然現象を不可能して、魚類や海草等人類の海中食糧を限り無く減少し、台風や季節風や竜巻等の人為的巨大化により、自動車の空中吸引より遥かに容易な海水波頭を空中吸引して、海水の豪雨を通常豪雨の10倍100倍1000倍と加速的人為的に巨大化し、山の緑全部を押し流す山津波や塩の被覆により、人類の陸上食物を0にする、人為的な人類絶滅を、海水温度7度上昇を阻止して人類絶滅阻止する可能性がある。 The existing thermal power generation + nuclear power generation will raise the seawater temperature by 7 degrees, making it impossible for the natural phenomenon of supplying nutrients such as oxygen to the sea surface cooling seabed, reducing the number of fish and seaweed underwater foods as much as possible, By artificially enlarging seasonal winds, tornadoes, etc., the seawater wave head that is much easier than the air suction of the car is sucked into the air, and the heavy rain of the seawater becomes 10 times 100 times 1000 times that of the normal heavy rain, and it becomes an artificial maneuver. There is a possibility that anthropogenic mankind extinction, which reduces the land food of mankind to 0 by the mountain tsunami and salt coating that pushes all the greenery of the mountain, prevents the humankind extinction by preventing the sea water temperature from rising by 7 degrees.
横型全動翼水重力タービン8P発電電気製造の液体酸素駆動全盛とし、既存気体空気圧縮を液体空気圧縮や水圧縮として、圧縮仕事率を既存ガスタービンや往復機関のの1/600や1/1700とし、10倍燃料10倍圧力燃焼容易な自動車や船舶や飛行機として、燃料費1/10自動車や10倍速度の船舶や飛行機とし、船舶駆動の過程では自然現象高速化2aして窒素や酸素やCO2を海水に供給、微生物や植物プランクトンや海草等を増殖して、食物連鎖等により魚類やコンブ類等人類の食糧を増大し、飛行機は垂直上昇や垂直降下や逆噴射を可能にして、何処でも飛行場や1日に地球を16周する等宇宙利用全盛にし、地球上何処でも日帰り旅行等にする可能性がある。 The horizontal full-blade water gravity turbine 8P is the liquid oxygen drive prime of the power generation electric production, the existing gas air compression is liquid air compression or water compression, and the compression work rate is 1/600 or 1/1700 of the existing gas turbine or reciprocating engine 10 times fuel 10 times pressure combustion easy car, ship or airplane, fuel cost 1/10 automobile or 10 times speed ship or airplane Supply CO2 to seawater, multiply microorganisms, phytoplankton, seaweed, etc., increase food for humans such as fish and kombu through food chains, etc. However, there is a possibility to make a day trip etc. anywhere on the earth by making the best use of space, such as flying around the earth 16 times a day.
0:各種エネルギ保存サイクル合体機関(各種熱エネルギは空気温度として熱ポンプで圧縮高圧の液体空気冷熱+過熱蒸気温熱に分割保存使用・重力エネルギは上昇保存噴射真空中重力加速度加速使用する各種エネルギ合体エンジン合体手段) 0:各種エネルギ保存サイクル合体機関及び合体方法(各種熱エネルギは太陽熱や地熱で加熱等空気温度として熱ポンプで圧縮高圧の液体空気冷熱+過熱蒸気温熱に分割保存使用・500以下液体金属使用時は保温装置で保温保存使用・衝撃エネルギはタービン翼や小径金属球にシリコン樹脂被覆やフッ素樹脂被覆を設け作用時間の保存延長に使用・重力エネルギは上昇装置により上昇保存使用する各種エネルギ合体エンジン及び各種エネルギ合体手段) 1:発電機、 1B:圧力機関(酸素圧力歯車機関・酸素圧力往復機関・水圧力歯車機関・水圧力往復機関等液体を高圧噴射する各種機関) 1C:アルコール、 1D:燃料噴射ポンプ、 1F:復水ポンプ、 1G:1〜複数段熱ポンプ(温熱50を温熱室3Bに+冷熱28aを冷熱室3Aに分割保存冷熱回収量増大後圧力無限上昇狙う) 1Y:複数段燃焼室(液体酸素と液体窒素を別圧縮50〜200MPa燃焼ガスと窒素ガス別製造し1Yに燃焼ガス噴射燃料噴射燃焼内外の水蒸気加熱を複数回実施して噴射又は排気する) 1b:燃料管(燃料噴射温度が最適温度になるように具備する) 1d:水銀、 1g:重力加速部、 1h:横軸、 2:太陽光加熱器(長レンズで太陽光を直線状に集めて高温部形成吸入空気を加熱) 2a:自然現象高速化(空気中では変化略0の残飯類が近くの川に移動すると一夜で0に近付く膨大な微生物量を人類の食糧増大に利用) 2a:自然現象高速化(発電では海水に冷熱28aを混合自然現象高速化した海水を海底に供給窒素や酸素やCO2等の栄養分を供給微生物増大して魚類やコンブ等食糧大増大する装置) 2a:自然現象高速化(船舶では海中に窒素や酸素やCO2等の栄養分を供給微生物の消化能力を森林の数万倍狙い植物プランクトンや海草等を増殖食物連鎖等により魚類やコンブ類等人類の食糧を増大) 2b:水抵抗僅少(船底に空気+燃焼ガス+過熱蒸気を超高速噴射して水抵抗僅少にする) 2c:断熱材、 2d:長レンズ(凸レンズ断面を直線状に延長矩形とし複数使用で焦点距離最短レンズ幅最大狙う) 2e:水面、 2A:耐熱材、 2B:熱吸収材、 2C:1〜複数段圧縮熱回収器(1〜複数段熱ポンプで複数回圧縮複数回高温として2Cの2X2Y2Zで複数回熱回収の容器で冷熱+温熱の質量圧力無限増大狙う) 2E:比重大物質(合金含む、白金球・金球・タングステン合金粉末焼結球・銀球・銅球・錫球・鉛球・亜鉛球・アルミニウム球・インジウム・カドミウム・ガリウム・タリウム・ビスマス等比重の大きい物質) 2E:比重大物質(製造法は小径程衝撃エネルギが低減するため例えば溶融鋼を大気中に噴射高速衝突粉砕空気冷却水冷却で超小径鋼球等製造) 2E:比重大物質(シリコン樹脂被覆やケイ素樹脂被覆の被覆白金合金球・被覆金合金球・被覆タングステン合金粉末焼結球・被覆銀合金球・被覆ビスマス合金球・被覆銅合金球・被覆錫合金球・被覆鉛合金球・被覆亜鉛合金球・被覆アルミニウム合金球) 2F:比重大物質上昇装置(重力エネルギを上昇保存) 2H:冷熱海水混合器(海水に冷熱を混合自然現象高速化の過程で過熱蒸気気化熱を冷却復水にする装置) 2X:空気熱交換器(空気を熱ポンプで圧縮高温として熱回収圧縮空気質量無限増大や圧力無限上昇狙う) 2Y:水熱交換器(高温空気や燃焼ガスで過熱蒸気製造) 2Z:比重大物質熱交換器(500度以下液体金属の温度管理等で使用) 3a:撥水鍍金、 3A:撥水コーティング、 3B:水圧力往復機関(多段酸素圧力往復機関で水や水蒸気を多段加熱して多段水圧力往復機関を駆動する) 3D:電気+液体空気冷熱+過熱蒸気温熱供給設備(重力発電電気で冷熱+温熱製造し液体酸素や液体窒素を供給自動車や船舶や飛行機を駆動や過熱蒸気で供給メタンハイドレートに注入メタンを回収等電気+冷熱+温熱利用全盛にする) 3E:比重大物質(水銀や水等常温で液体の比重大物質) 3E:比重大物質(低融点合金の500度以下液体で安定高温液体合金) 3F:酸素圧力往復機関(液体酸素と液体窒素と燃料を噴射燃焼50〜200MPa燃焼ガスとし、膨張の過程で燃料噴射多段燃焼して多段酸素圧力往復機関を駆動する) 3H:往復ピストン 3K:外接歯車 3L:複数段燃焼室 3M:水圧力往復機関(3F又は3Zで加熱した高圧高温水蒸気室5Nで駆動3F又は3Zに連動する) 3N:水圧力歯車機関(多段酸素圧力歯車機関で水や水蒸気を多段加熱して多段水圧力歯車機関を駆動する) 3Z:酸素圧力歯車機関(液体酸素と液体窒素と燃料噴射燃焼して50〜200MPa燃焼ガスとし内周外周の水や水蒸気を多段燃焼加熱して多段水圧力歯車機関を連動する) 3a:撥水鍍金、 3b:撥水コーティング、 4X:タービン翼断面(断面積を拡大表面積増大) 5a:高圧高温燃焼ガス制御弁、 5A:給気弁、 5B:冷却ヒレ、 5C:排気室 5D:排気弁 5E:給気室 5F:酸素加熱室 5G:水蒸気加熱室、 5H:水加熱室、 5K:液体酸素、 5K:液体酸素室、 5L:液体窒素、 5L:液体窒素室、 5M:高圧高温燃焼ガス、 5M:高圧高温燃焼ガス室、 5N:高圧高温水蒸気室、 5P:水蒸気制御弁、 6A:過熱蒸気噴射ノズル、 6B:圧縮空気噴射ノズル、 6E:比重大物質噴射ノズル、 6W:比重大物質加速機(液体比重大物質3E圧力と比重差利用して比重大物質3Eや2E混合噴射) 6X:燃料噴射ノズル、 6X:アフターバーナー(吸引空気流に燃料噴射冷熱28a燃焼流6Yに合流燃焼して燃料燃焼量大増大で宇宙上昇) 6Y:燃焼ガス噴射ノズル(冷熱28a燃焼流) 6Z:水蒸気噴射ノズル、 7A:プロペラ、 7B:回転翼、 7C:スクリュー、 8c:タービン翼(実験最良断面や形状に順次移行するドラム缶外周形状環状多数直線長大タービン翼) 8d:重力球誘導曲面(重力球を内部に誘導する曲面を設ける) 8P:横型全動翼タービン(対向全動翼弾み車タービン直列全動翼弾み車タービン食込全動翼弾み車タービン) 8P:横型全動翼タービン(ドラム缶形プラスチックや軽合金で軽量化や超硬合金貼付やシリコン樹脂被覆やフッ素樹脂被覆を選択使用実験最良に移行) 8P:横型全動翼水重力タービン(既存蒸気タービンは静翼で堰き止め出力が0に近付くため全動翼を必須とし仕事率が白金球の1/3.6万等僅少なため比重大物質重力使用必須とし太陽光加熱空気等空気を1〜複数段熱ポンプ+圧縮熱回収器で圧縮熱回収し温熱+冷熱に分割保存タービン駆動+各種用途に使用) 8P:横型全動翼水重力タービン(温熱駆動+冷熱駆動にすると使用落差が限定されるため落差使用を無制限として使用する場合に使用する) 9:段落毎環状ネジ組立、 10:船体、 10A:船室、 10b:操縦室、 10c:制御室、 10d:客室、 10e:貨物室、 16A:水平軸、 11D:気体専用冷却室、 24:燃焼ガス制御弁、 24A:圧縮空気制御弁、 25:過熱蒸気制御弁、 25b:燃料制御弁、 28a:空気、 28a:冷熱(空気28aを熱ポンプで圧縮して圧縮空気熱量の過熱蒸気50温熱+液体酸素や液体窒素を含む圧縮空気28a冷熱に分割保存) 28b:圧縮空気熱量、 28A:吸入空気路、 28B:空気路入口、 38:回転案内具、 38a:飛行胴、 38b:飛行翼、 38c:飛行尾翼、 38d:垂直翼、 38e:翼前縁心、 38g:水上翼、 38h:浮上艇、 38B:空気吸引噴射船舶(79S79T79Y79Z具備) 38C:水吸引噴射船舶(79U79X具備) 39A:太陽熱重力飛行機、 39B:太陽熱重力回転飛行機、 39C:太陽熱重力ヘリコプター、 39D:スクリュー船舶、 39G:太陽熱重力飛行船舶、 40A:方向舵、 49:燃焼ガス、 50:過熱蒸気、 50:過熱蒸気室、 50:温熱(空気28aを熱ポンプで圧縮して圧縮空気熱量の過熱蒸気50温熱+圧縮空気28a冷熱に分割保存) 50A:水蒸気、 51:空気抽出器、 51:合流抽出器(合流するための抽出器) 51A:空気抽出室、 52a:水、 52a:海洋深層水、 52b:高温水、 52d:温熱(50から変化) 52e:冷熱(28aから変化) 55B:変速装置、 60A:内側軸装置(タービン翼具備装置) 60B:外側軸装置(タービン翼具備装置) 60C:内側動翼群(内側と外側が反対回転) 60D:外側動翼群(内側と外側が反対回転) 76:歯車装置(磁気摩擦動力伝達装置を含む) 77B:半筒形外箱、 77F:噴射部外箱、 77G:円筒回転部、 77a:タービン外箱、 78A:合体機関噴射部(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と内周外周から複数回加熱して噴射し、空気吸引噴射する) 78B:合体機関噴射部(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射する) 78V:合体機関噴射部(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と外周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射する) 78W:合体機関噴射部(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と外周と内周外周から複数回加熱して噴射し、空気吸引噴射する) 79S:ウォータージェット(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と外周と内周外周から複数回加熱して噴射し、空気吸引噴射して水を吸引噴射する) 79T:ウォータージェット(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と外周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射して水を吸引噴射する) 79U:ウォータージェット(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と外周と内周外周から複数回加熱して噴射し、水を吸引噴射する) 79X:ウォータージェット(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と内周外周から複数回加熱して噴射し、水を吸引噴射する) 79Y:ウォータージェット(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と内周外周から複数回加熱して噴射し、空気吸引噴射して水を吸引噴射する) 79Z:ウォータージェット(冷熱に複数回燃料噴射燃焼して超高圧噴射した液体を内周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射して水を吸引噴射する) 80:軸受、 80a:推力軸受 80A:継手、 80B:締付具、 80E:液体合体噴射部(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、空気吸引噴射する) 80F:液体合体噴射部(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射する) 80V:液体合体噴射部(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射する) 80W:液体合体噴射部(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、空気吸引噴射する) 80S:液体空気吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、空気吸引噴射して水を吸引噴射する) 80T:液体空気吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温
水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射して水を吸引噴射する) 80U:液体水吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と外周と内周外周から複数回加熱して噴射し、水を吸引噴射する) 80X:液体水吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、水を吸引噴射する) 80Y:液体空気吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、空気吸引噴射して水を吸引噴射する) 80Z:液体空気吸引ウォータージェット(高圧高温燃焼ガス5M高圧高温水蒸気室5Nを受給して5Mに複数回燃料噴射燃焼して5Nを内周と内周外周から複数回加熱して噴射し、空気吸引流複数か所にも燃料噴射燃焼噴射して、空気吸引噴射して水を吸引噴射する) 84:二重反転磁気摩擦装置(固定部具備内側動翼群と外側動翼群を略同速度反対回転にする装置) 84Y:二重反転歯車装置(既存技術で同様にする) 95a:燃焼ガス溜、 95b:圧縮空気溜、 95c:過熱蒸気溜、 103:冷熱回収器、
0: Various energy storage cycle coalescing engine (various heat energy is compressed with a heat pump as air temperature, divided into high-pressure liquid air cold heat + superheated steam heat) Engine uniting means) 0: Various energy storage cycle coalescence engine and coalescence method (various thermal energy is heated by solar heat or geothermal heat, etc., air temperature is compressed and stored by heat pump compressed high pressure liquid air cold + superheated steam temperature, liquid under 500 When using metal, keep it warm with a heat retaining device. Use impact energy for turbine blades and small metal balls with silicone resin coating or fluororesin coating to extend the working time. Combined engine and various energy combining means) 1: Generator, 1B: Pressure engine (oxygen pressure tooth) Engines, oxygen pressure reciprocating engines, water pressure gear engines, water pressure reciprocating engines, etc. that inject high-pressure liquids) 1C: alcohol, 1D: fuel injection pump, 1F: condensate pump, 1G: 1 to multistage heat pump ( 1H: Multistage combustion chamber (liquid oxygen and liquid nitrogen are separately compressed 50 to 200 MPa, combustion gas and nitrogen gas) The heat 50 is divided into the heat chamber 3B and the cold 28a is divided into the cold chamber 3A. 1B: Fuel pipe (provided so that the fuel injection temperature becomes the optimum temperature) 1d: Mercury, 1g: Gravity acceleration unit, 1h: horizontal axis, 2: solar heater (collects sunlight in a straight line with a long lens and heats the high-temperature part forming intake air) 2a: speeds up natural phenomenon (residual rice with almost zero change in air) Kind is near 2a: Acceleration of natural phenomena (In power generation, cold water 28a is mixed with seawater in the power generation to supply seawater with accelerated natural phenomena to the seabed) Nitrogen and oxygen 2a: Speeding up natural phenomena (on ships, supplying nutrients such as nitrogen, oxygen and CO2 into the sea, the digestive capacity of microorganisms in the number of forests) Increase phytoplankton, seaweed, etc. to increase food for humans such as fish and kombu by increasing food chain, etc. 2b: Water resistance is low (Air + combustion gas + superheated steam is jetted to the bottom of the ship to reduce water resistance) 2c: heat insulating material, 2d: long lens (convex lens cross-section extended into a straight line and using a plurality of lenses, aiming at the maximum focal length shortest lens width) 2e: water surface, 2A: heat resistant material, 2B: heat absorbing material, 2C: 1 ~ Several stage compression heat recovery unit (1 to 2 stage 2P2Y2Z with 2C2X2Y2Z as a high temperature, multiple times compression with multiple stage heat pump, aiming at infinite increase in cold / heat mass pressure) 2E: Specific substances (including alloys) , Platinum sphere, gold sphere, tungsten alloy powder sintered sphere, silver sphere, copper sphere, tin sphere, lead sphere, zinc sphere, aluminum sphere, indium, cadmium, gallium, thallium, bismuth, etc. (Manufacturing method reduces impact energy for smaller diameters. For example, molten steel is injected into the atmosphere to produce ultra-small diameter steel balls by high-speed collision pulverization and air cooling water cooling.) 2E: Specific material (silicon resin coating or silicon resin coating) Platinum alloy balls, coated gold alloy balls, coated tungsten alloy powder sintered balls, coated silver alloy balls, coated bismuth alloy balls, coated copper alloy balls, coated tin alloy balls, coated lead alloy balls, coated zinc alloy balls Coated aluminum alloy sphere) 2F: Specific critical substance riser (gravity energy is increased and preserved) 2H: Cold seawater mixer (Cooling seawater is mixed with cold heat to cool the superheated vaporization heat in the process of speeding up the natural phenomenon) 2X: Air heat exchanger (the air is compressed with a heat pump at a high temperature, heat recovery compressed air mass is infinitely increased or the pressure is infinitely increased) 2Y: Water heat exchanger (superheated steam production with high temperature air or combustion gas) 2Z: Specific critical substances Heat exchanger (used for temperature control of liquid metal below 500 degrees) 3a: Water repellent plating, 3A: Water repellent coating, 3B: Water pressure reciprocating engine (Multistage oxygen water reciprocating engine heats water and steam in multiple stages 3D: Electricity + liquid air cold heat + superheated steam hot water supply equipment (cooled heat + thermal production by gravity power generation electricity to supply liquid oxygen and liquid nitrogen, driving automobiles, ships and airplanes and superheated steam 3E: Specific critical substances (specific critical substances that are liquid at normal temperatures such as mercury and water) 3E: Specific critical substances (500 of low melting point alloys) 3F: Oxygen pressure reciprocating engine (liquid oxygen, liquid nitrogen, and fuel are used as injection combustion 50-200 MPa combustion gas, and fuel injection multistage combustion is driven during expansion to drive a multistage oxygen pressure reciprocating engine. 3H: Reciprocating piston 3K: External gear 3L: Multistage combustion chamber 3M: Water pressure reciprocating engine (linked to 3F or 3Z driven by high pressure high temperature steam chamber 5N heated by 3F or 3Z) 3N: Water pressure gear engine ( Multistage oxygen pressure gear engine heats water and water vapor in multiple stages to drive the multistage water pressure gear engine) 3Z: Oxygen pressure gear engine (50 to 20 by fuel injection combustion with liquid oxygen and liquid nitrogen 3a: Water repellent plating, 3b: Water repellent coating, 4X: Turbine blade cross section (enlarged cross-sectional area and increased surface area) 5a: High pressure high temperature combustion gas control valve, 5A: Supply valve, 5B: Cooling fin, 5C: Exhaust chamber 5D: Exhaust valve 5E: Supply chamber 5F: Oxygen heating chamber 5G: Steam heating chamber, 5H: Water heating chamber 5K: Liquid oxygen, 5K: Liquid oxygen chamber, 5L: Liquid nitrogen, 5L: Liquid nitrogen chamber, 5M: High pressure high temperature combustion gas, 5M: High pressure high temperature combustion gas chamber, 5N: High pressure high temperature steam chamber, 5P: Steam control valve 6A: Superheated steam injection nozzle, 6B: Compressed air injection nozzle, 6E: Specific critical material injection nozzle, 6W: Specific critical material accelerator (Liquid specific critical material 3E Pressure specific gravity difference and specific gravity material 3E or 2E mixing 6X: Fuel injection nozzle, 6X: Afterburner (combustion merged with the fuel injection cold heat 28a combustion flow 6Y into the suction air flow and rise in space due to a large increase in fuel combustion amount) 6Y: Combustion gas injection nozzle (cool heat 28a combustion flow) 6Z : Steam injection nozzle, 7A: Propeller, 7B: Rotating blade, 7C: Screw, 8c: Turbine blade (drum can outer peripheral shape circular multiple straight long turbine blades that gradually shift to the experimental best cross section and shape) 8d: Gravity sphere induction curved surface (gravity 8P: Horizontal all-blade turbine (opposite all-blade propeller turbine series all-blade propeller turbine turbine bite all-blade propeller turbine) 8P: Horizontal all-blade turbine (drum-type plastic or Light weight with light alloy, cemented carbide paste, silicon resin coating or fluororesin coating selected Use experiment best transition) 8P: Horizontal full blade weight Power turbines (existing steam turbines are stationary blades and the damming output approaches 0, so all the blades are essential, and the work rate is as small as 1 / 36,000 of platinum balls. Compressed heat is recovered with 1 to multi-stage heat pump + compression heat recovery unit and air is stored separately for heating and cooling and used for various purposes. 8P: Horizontal all-blade hydrogravity turbine (for heating and cooling drive) 9: An annular screw assembly for each paragraph, 10: Hull, 10A: Ship cabin, 10b: Cockpit, 10c: Control room, 10d: Guest room, 10e: cargo compartment, 16A: horizontal axis, 11D: dedicated gas cooling chamber, 24: combustion gas control valve, 24A: compressed air control valve, 25: superheated steam control valve, 25b: fuel control valve, 28a: air, 28a: cold Heat (compressed air 28a is compressed with a heat pump, and is stored in the form of 50 heated superheated steam of compressed air + compressed air 28a cold containing liquid oxygen or liquid nitrogen) 28b: calorie of compressed air, 28A: intake air passage, 28B: air Road entrance, 38: Rotating guide, 38a: Flight trunk, 38b: Flying wing, 38c: Flying wing, 38d: Vertical wing, 38e: Wing leading edge, 38g: Water wing, 38h: Surfing boat, 38B: Air suction Jet ship (with 79S79T79Y79Z) 38C: Water suction jet ship (with 79U79X) 39A: Solar thermal gravity plane, 39B: Solar thermal gravity rotating plane, 39C: Solar thermal gravity helicopter, 39D: Screw ship, 39G: Solar thermal gravity flying ship, 40A: Rudder 49: combustion gas, 50: superheated steam, 50: superheated steam chamber, 50: warm heat (air 28a is heated 50A: water vapor, 51: air extractor, 51: confluence extractor (extractor for confluence) 51A: air extraction chamber, 52a: Water, 52a: Deep sea water, 52b: High temperature water, 52d: Thermal (change from 50) 52e: Cold (change from 28a) 55B: Transmission, 60A: Inner shaft device (turbine blade equipped device) 60B: Outer Shaft device (equipment with turbine blades) 60C: Inner blade group (inside and outside rotating in opposite directions) 60D: Outer blade group (inside and outside rotating in opposite directions) 76: Gear device (including magnetic friction power transmission device) 77B : Semi-cylindrical outer box, 77F: Injection part outer box, 77G: Cylindrical rotating part, 77a: Turbine outer box, 78A: Combined engine injection part 78B: Combined engine injection part (multiple times of fuel injection combustion in cold heat and ultra-high pressure injection from the inner periphery and inner periphery outer periphery multiple times from the inner periphery and inner periphery outer periphery) 78V: Combined engine injection section (inner circumference of super high pressure liquid that has been injected by fuel injection several times into cold heat and injected) 78W: Combined engine injection section (multiple times of fuel injection combustion to cold heat and combustion) 79S: Water jet (injecting the liquid injected into the cold and injecting the fuel multiple times into the cold and spraying it with ultra high pressure) Sprayed by heating multiple times from the circumference, outer circumference, and inner circumference 79T: Water jet (injection of ultra-high pressure fuel by burning multiple times into cold heat and injecting the liquid multiple times from the inner periphery, outer periphery, and inner periphery outer periphery) 79U: Water jet (inner and outer peripheries of liquids injected and burned multiple times into cold air and injected with ultra-high pressure) 79X: Water jet (heated by multiple injections of fuel into the cold and fired multiple times and heated from the inner and outer peripheries multiple times from the inner and outer peripheries) 79Y: Water jet (injection and combustion of the fuel multiple times to the cold heat and injecting the ultra-high pressure spray from the inner periphery and the inner periphery outer periphery multiple times to inject, air suction injection) Water is sucked and jetted) 79Z: Water jet (liquid that has been fuel-injected and burned multiple times into cold heat and injected from the inner circumference and inner and outer circumference multiple times to inject and inject the fuel into the air suction flow at several locations. 80: Bearing, 80a: Thrust bearing 80A: Joint, 80B: Fastener, 80E: Liquid coalescence injection part (High pressure high temperature combustion gas 5M High pressure high temperature steam chamber 5N 5M fuel-injected and burned multiple times, 5N heated and injected multiple times from the inner and outer peripheries, and air sucked and injected) 80F: Liquid coalesced injection part (high pressure high temperature combustion gas 5M receiving high pressure high temperature steam chamber 5N Then, 5N is injected and burned multiple times, and 5N is heated and injected multiple times from the inner and outer peripheries, and the fuel is injected and injected into a plurality of locations of the air suction flow as well. Liquid coalescence injection part (high pressure high temperature combustion Fired gas 5M received high-pressure high-temperature steam chamber 5N, fuel-injected and combusted multiple times to 5M, heated and injected 5N multiple times from the inner circumference, outer circumference, and outer circumference, and fuel-injected into multiple air suction flows 80W: Liquid coalescence injection unit (receives high pressure / high temperature combustion gas 5M high pressure / high temperature steam chamber 5N and injects and burns fuel 5M multiple times to 5M for inner circumference, outer circumference and inner circumference outer circumference 80S: Liquid air suction water jet (receives high-pressure high-temperature combustion gas 5M high-pressure high-temperature steam chamber 5N, and fuel-injects and combusts multiple times 5M to 5N as the inner periphery) 80T: Liquid air suction water jet (receives high pressure high temperature combustion gas 5M, high pressure high temperature steam chamber 5N and multiple to 5M) Fuel 80N is heated and injected from the inner circumference, outer circumference, and inner circumference outer circumference several times and injected, and fuel injection combustion injection is also performed at a plurality of locations of the air suction flow, and air suction injection is performed to suck and inject water. : Liquid water suction water jet (high pressure high temperature combustion gas 5M received high pressure high temperature steam chamber 5N, fuel injected and burned to 5M multiple times, heated 5N multiple times from the inner periphery, outer periphery and inner periphery outer periphery to inject water 80X: Liquid water suction water jet (receives high pressure / high temperature combustion gas 5M, high pressure / high temperature steam chamber 5N, and injects and burns fuel 5M multiple times to heat 5N multiple times from the inner periphery and inner periphery outer periphery) 80Y: Liquid air suction water jet (receives high pressure / high temperature combustion gas 5M, high pressure / high temperature steam chamber 5N, and injects and combusts multiple times to 5M to generate 5N from the inner periphery and inner periphery outer periphery) Heat once 80Z: Liquid air suction water jet (receives the high-pressure high-temperature combustion gas 5M high-pressure high-temperature steam chamber 5N, and injects and burns the fuel several times to 5M, and 5N is the inner circumference. Heating and injecting multiple times from the inner and outer periphery, and fuel injection / combustion injection at a plurality of locations of air suction flow, air suction injection and water suction injection) 84: Counter-rotating magnetic friction device (equipped with a fixed portion) 84Y: Counter-rotating gear device (same for existing technology) 95a: Combustion gas reservoir, 95b: Compressed air reservoir, 95c: Superheated steam Reservoir, 103: Cold energy recovery device,
Claims (214)
体機関。 With a work rate of 1700 times that of the existing steam turbine and a horizontal all-blade hydrogravity turbine (8P) power generation with an annular multiple linear long turbine blade (8c), Manufactured and mounted liquid air cold super high pressure injection Multiple times fuel injection Combustion and super high pressure injection liquid is heated and injected multiple times from the inner circumference, outer circumference and inner circumference outer circumference, and fuel injection combustion is also conducted at multiple locations of air suction flow Various heat energy is jetted and moved as a moving unit that drives the liquid combined jet unit (80V) that sucks and jets air. The heat energy is divided into a high-pressure liquid air cold heat + superheated steam temperature using a heat pump as the air temperature. Various energy conservation cycle coalescing engine and coalescence method for using acceleration acceleration of gravity acceleration in ascending storage jet.
Body engine.
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