JP2011185081A - Various energy conservation cycle combined engine - Google Patents
Various energy conservation cycle combined engine Download PDFInfo
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本発明はスクラムジェットの高速燃焼と蒸気タービンの高圧大膨張速度とロケットを合体し、宇宙で無限大容積の過熱蒸気を500度等に加熱噴射して膨張速度を更に増大する、合体機関噴射部78B太陽熱重力ヘリコプター39Cとし、又熱ポンプで使用電力の3〜10倍の熱エネルギが得られる情報があり、太陽光加熱空気を種に大気圧同速度同容積仕事率を、既存蒸気タービンの2.3万倍前後水銀等仕事率重力タービン駆動熱ポンプで圧縮熱回収して、3〜10倍の温熱と冷熱両方のエネルギを無限回収利用のエネルギ保存サイクルにし、太陽光加熱の空気を吸入圧縮1000度等として、太陽光加熱別空気を加熱吸入圧縮1200度等とし、熱交換過熱蒸気50温熱+圧縮空気28a冷熱を製造する操作を複数回実施して、理論最良の推進剤過熱蒸気50+酸化剤圧縮空気28a無限製造に燃料費0でも挑戦し、合体機関噴射部78B噴射は、燃焼器1Yに圧縮空気供給燃料噴射燃焼1200度等として、外周過熱蒸気50を加熱最高温度燃焼にし、噴射の過程で複数の燃焼ガス噴射ノズル6Y高温高速燃焼内に燃料噴射2段燃焼して、過熱蒸気50を1200度に近付けて、真空0〜大気圧100度に近付く過熱蒸気を800度等に加熱し、過熱蒸気容積を増大して、噴射推進出力と燃焼ガス49の吸引出力を真空部飛行で最大にし、燃焼ガス吸引出力の増大によりスクラムジェットの欠点を解消して、2.3万倍前後水銀等仕事率太陽熱タービン駆動を含めて空気抵抗0CO2排気0の宇宙利用全盛を狙う、合体機関噴射部78B太陽熱重力ヘリコプター39C等の技術に関する。 The present invention combines a rocket with high-speed high-speed combustion of a scramjet and high-pressure high-expansion velocity of a steam turbine, and heats and injects superheated steam of infinite large volume in space etc. in space to further increase the expansion velocity. There is information that thermal energy can be obtained 3 to 10 times the power used by the heat pump with the 78B solar thermal gravity helicopter 39C, and the same atmospheric pressure same speed work rate can be obtained by using solar heated air as a seed. .30,000 times mercury, etc. Power factor gravity turbine driven heat pump recovers compression heat, 3 to 10 times energy of both heat and cold are infinite recovery utilization energy preservation cycle, suction air of solar heating is suctioned and compressed Conduct the operation of producing heat exchange superheated steam 50 temperature + compressed air 28a cold heat several times by setting the heating suction compression 1200 temperature etc. as 1000 degrees etc. Propellant superheated steam 50 + oxidant compressed air 28a Infinite fuel production to even the fuel cost 0 challenge, united engine injection part 78B injection heats the outer peripheral superheated steam 50 as compressed air supply fuel injection combustion 1200 degree etc to the combustor 1Y Maximum temperature combustion, and in the process of injection, two stages of fuel injection into a plurality of combustion gas injection nozzles 6Y high temperature high speed combustion in the process of injection, superheated steam 50 is brought close to 1200 degrees, superheated steam approaching vacuum 0 to atmospheric pressure 100 degrees By heating to 800 ° C., etc., increasing the superheated steam volume, maximizing the injection propulsion output and the suction output of the combustion gas 49 in the vacuum part flight, and eliminating the drawback of the scramjet by increasing the combustion gas suction output, Combined engine injection part 78B solar thermal gravity helicopter 39C etc aiming at space utilization of air resistance 0CO2 exhaust 0 including the power factor solar thermal turbine drive of around 23,000 times mercury etc. Surgery on.
燃料費僅少の太陽熱重力ヘリコプター39C等で燃料費0の宇宙利用全盛を狙うもので、大気中では太陽光で加熱した空気を、竪型金属球水銀重力太陽熱タービン駆動の熱ポンプ1Gで吸入圧縮熱交換熱回収して、必要に応じて圧縮熱交換熱回収複数回の過程で燃料噴射燃焼熱交換過熱蒸気50を製造し、酸化剤の圧縮空気28a冷熱乃至燃焼ガス49冷熱と推進剤の過熱蒸気50を製造して、宇宙では金属球水銀の圧縮空気冷熱加速タービン駆動低圧排気で、密閉吸入空気路28A太陽光加熱熱回収の循環とし、直射太陽光120度Cと長レンズ2dと熱ポンプにより過熱蒸気製造効率を上昇して、宇宙上昇時は圧縮空気28a圧縮熱回収器2Cで過熱蒸気50製造の過程で、複数回燃料噴射燃焼燃焼ガス49にして、24〜400MPa過熱蒸気製造量を増大し、合体機関噴射部78B燃焼器1Yに燃焼ガスを供給その外周に過熱蒸気を供給して、24〜400MPa燃焼ガス49に燃料噴射燃焼外周の過熱蒸気を加熱し、2段燃焼や3段燃焼以後は過熱蒸気を内週や外周から最適時間環状加熱して、蒸気タービンの高圧大膨張速度とスクラムジェットの高速燃焼とロケットを合体し、既存ジェット機の10〜100倍圧力10倍熱量噴射100〜1000倍噴射出力狙い、実験最良エンジンに移行の合体機関噴射部78B技術に関する。 Aim for zero fuel cost space use with solar thermal gravity helicopter 39C etc. with minimal fuel cost. Air heated by solar light in the atmosphere, suction heat of compression with heat pump 1G driven by vertical metal sphere mercury gravity solar thermal turbine Heat exchange heat recovery, and if necessary, compression heat exchange heat recovery Multiple-shot fuel injection combustion heat exchange superheated steam 50 is produced, compressed air 28a cold of oxidant to combustion gas 49 cold overheat and superheated steam of propellant 50 manufactured in space, metal sphere mercury compressed air cold heat accelerated turbine driven low pressure exhaust by mercury, closed intake air path 28A solar heat recovery heat circulation, direct sunlight 120 degrees C, long lens 2d and heat pump Increase the superheated steam production efficiency, and during the ascend to space, in the process of producing superheated steam 50 with compressed air 28a compression heat recovery unit 2C, make the fuel injection combustion combustion gas 49 multiple times, 24 to 400MPa Increase the amount of heat steam production, supply combustion gas to united engine injection part 78B combustor 1Y and supply superheated steam to the outer circumference, heat the superheated steam of fuel injection combustion outer circumference to 24-400MPa combustion gas 49, 2 Stage-stage combustion and after stage 3-stage combustion, superheated steam is annularly heated for an optimal time from the inner week and the outer circumference, and high speed large expansion speed of steam turbine and high speed combustion of scramjet are combined with rocket, 10 to 100 times pressure of existing jet The present invention relates to a combined engine injection section 78B technology for transitioning to a 10 times calorie injection 100 to 1000 times injection power aiming and an experimental best engine.
竪型金属球水銀重力太陽熱タービン8G駆動各種重力タービン併用等として、水銀や液体金属(鉛合金中核500度以下液体金属合金)を衝撃低減材料3Eとし、金属球を(合金を含む白金球・金球・タングステン球・鋼球・モリブデン球・鋳鉄球・銀球・銅球・ニッケル球・コバルト球・クロム球)等として、被覆金属球を金属球に被覆を設けたものとし、液体金属を500度以下で液体の金属として、液体金属の中核を鉛合金とし、資源量に最適対応した太陽熱タービン駆動として、金属球水銀を水銀噴射ポンプ6Zで噴射し、温熱加速や冷熱加速で太陽熱タービン駆動重力加速追加駆動して、タービン翼断面4Xを既存蒸気タービンの2〜26倍にしたタービン翼8cに噴射し、金属球水銀の転がり接触回転出力の増大として、竪型金属球水銀重力太陽熱タービン8G回転にし、長レンズ2d熱吸収材2Bで構成の吸入空気路28A太陽光加熱の空気28aを吸入して、熱ポンプで圧縮900度前後にし、圧縮熱回収器2Cで熱交換太陽光加熱の別空気28aを500度前後に加熱して、吸入圧縮1200度等にし、熱回収を継続して圧縮空気28a温熱冷熱製造を無限継続膨大として、大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービンの2.3万倍前後水銀等仕事率にし、実験最良に移行の竪型金属球水銀重力太陽熱タービン8G技術に関する。 Ball-shaped metal spheres Mercury gravity solar thermal turbine 8G driven Various gravity turbines combined use mercury or liquid metal (lead alloy core 500 degrees or less liquid metal alloy) as impact reduction material 3E, metal spheres (platinum spheres / gold containing alloy) Ball, tungsten ball, steel ball, molybdenum ball, cast iron ball, silver ball, copper ball, nickel ball, cobalt ball, chromium ball), etc., with coated metal spheres coated on metal spheres, 500 liquid metals The core of the liquid metal is a lead alloy as a liquid metal and the core of the liquid metal is a lead alloy, and a solar ball is driven by a mercury jet pump 6Z as a solar heat turbine drive that optimally corresponds to the amount of resources. Accelerating additional drive to inject the turbine blade section 4X into the turbine blade 8c which is 2 to 26 times the size of the existing steam turbine, and increase the rolling contact rotational power of mercury metal A spherical mercury gravity solar heat turbine 8G rotation, suction air path 28A composed of long lens 2d heat absorbing material 2B is drawn in, the air 28a of solar light heating is sucked and compressed by a heat pump to around 900 degrees, heat is reduced by compression heat recovery device 2C Heat exchange air heating separate air 28a to around 500 degrees and make suction compression 1200 degrees etc., heat recovery is continued, and compressed air 28a thermal cold / cold energy production is infinite continuous hugeness, atmospheric pressure same speed same volume work rate It is related to vertical-type metal sphere mercury gravity solar thermal turbine 8G technology of the best transition in the experiment by setting the kg heavy m / s to about 23,000 times the power of mercury etc. of the existing steam turbine.
既存蒸気タービンの大気圧同速度同容積仕事率が、白金球重力太陽熱タービン仕事率の1/3.6万仕事率等無茶苦茶僅少に加えて、仕事をしない半分の静翼で蒸気速度を堰き止めて蒸気速度低減方向変換する等、無茶苦茶過ぎるため人類絶滅狙う宇宙人の陰謀と考えると、火力原子力発電の海面温度7度上昇は環境に影響皆無としておりますが、海面温度が周囲より7度上昇すると蒸発量が爆発的に増大し、異常気象発生は明白で周囲の海水と混合分散すると海面全部が温度上昇するため、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て、魚類や海草類等人類の食糧が激減するため現状と一致し、海面温度7度上昇を100年続け、原子力発電でCO2排出量を低減しても、海水表面温度7度上昇海域が10%成長で1000倍を超える等として、旱魃や豪雨や風速を10倍等の300m/秒台風や季節風とし、海水を上空に吸引海水の集中豪雨等として、陸地全部を塩で被覆して陸と海の食糧が0に近付き、人類が絶滅に近付く背景があります。中国が10%成長を10年続けると海水温度7度上昇量が2倍ですが、沖縄に近付く台風がカトリーナを超える予想が最悪予想で、20年では7度上昇海水量が4倍台風や季節風の最大風速が100m/秒となって、海水の集中豪雨が始まるのではと心配、最悪予想は外れて欲しいのです。 The atmospheric pressure same speed same volume work rate of the existing steam turbine, in addition to a slight amount such as 1 / 3.6 thousand work rate of platinum ball gravity solar heat work rate etc, steam speed with the half vane which does not work Considering the imprisonment of aliens aiming for human extinction because it is too intimidating, such as stopping and changing the steam velocity reducing direction, the sea surface temperature rise of thermal power nuclear power is considered to have no effect on the environment, but the sea surface temperature is If the temperature rises further by 7 ° C, evaporation will increase explosively, abnormal weather occurrence is obvious, and mixing and dispersing with surrounding seawater will raise the temperature of the entire sea surface, so nutrients such as nitrogen, oxygen and CO2 will be added to the sea surface cooling seabed in winter. It is consistent with the present situation because the natural phenomena that have been supplied have become impossible and human food such as fish and seaweeds are drastically reduced. Even if the sea surface temperature rises 7 degrees continuously for 100 years, even if CO2 emissions are reduced by nuclear power generation, Sea water surface temperature 7 degrees As the rising sea area is 10% growth and more than 1000 times, the flood, heavy rain, wind speed is made 10 times 300 m / s typhoon and seasonal wind, seawater is drawn into the sky and concentrated rain of seawater etc., the whole land is covered with salt. Land and sea food are approaching 0, and there is a background that humanity is approaching extinction. If China continues 10% growth for 10 years, the temperature rise by sea temperature doubles, but the typhoon approaching Okinawa is expected to surpass Katrina, and the sea level rise by 7 degrees in 20 years quadruples typhoon and monsoon wind The maximum wind speed of is 100m / s, and I am worried that the torrential rain of seawater will begin, and I want you to get rid of the worst expectation.
高校や大学で既存エンジンを理論最良エンジンと説明しており、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ります。そこで消費燃料僅少の竪型金属球水銀重力太陽熱タービン8G駆動飛行機類や船舶類にして、停止中は熱と電気と冷熱の供給設備で使用可能に地球温暖化防止する等とし、大気圧同速度同容積仕事率kg重m/秒最高を既存蒸気タービンの3.6万倍前後白金球仕事率にして、水銀・液体鉛・液体錫・液体亜鉛等液体金属や金属球や被覆金属球を垂直下方に重力加速度加速にすると、低速で落差を増大する入力より重力加速度加速だけでも出力発生は大幅に増大し、タービンの大型化多数化+落差を1000m以上に増大限り無く出力を増大できる背景があります。地球での最大加速が重力加速度で無限大に近く、海水温度上昇0やCO2排気0や燃料費0の理論最良エンジン重力太陽熱発電として、化石燃料等限りある資源が枯渇するため、限りある資源を子孫に残す手段の温熱や冷熱の回収利用無限大や無限大に近い発電量とし、重力太陽熱発電蓄電池駆動や電気駆動の、各種自動車類全盛や各種船舶類全盛や全面電化住宅全盛や工場電化全盛等、極端に安価な発電の蓄電池駆動や電気駆動の地球温暖化防止が得られる背景があります。 High school or university describes the existing engine as the theoretical best engine, and returns to elementary school science and thinks about the theoretical best engine, the unit of work rate is kg weight m / s equal weight x speed, so heavy material with high speed The rotational power generation is the theoretical best engine, but there is a background that there is no trace considered. Therefore, the consumption of fuel is small, so that it can be used in the supply facilities of heat, electricity and cold heat, etc., while stopping it as a plane-type metal sphere mercury gravity solar heat turbine 8G drive airplanes and ships etc. The same volume work load kg heavy m / s maximum is about 36,000 times the platinum steam work rate of the existing steam turbine, and the liquid metal such as mercury, liquid lead, liquid tin, liquid zinc and metal balls and coated metal balls are vertical When acceleration is accelerated downward, output generation is greatly increased by gravity acceleration alone than input that increases the drop at low speed, and the size increase of the turbine + increase of the drop to 1000 m or more The background can be increased without limit There is. The maximum acceleration on the earth is close to infinity by the gravitational acceleration, and the theoretical best engine gravity solar power of sea water temperature rise 0, CO2 exhaust 0 and fuel cost 0 is exhausted, as limited resources such as fossil fuel are exhausted. Thermal energy and cold energy recovery means to leave to descendants Infinite or almost infinite power generation, Gravity solar thermal power storage battery driven and electric driven, various kinds of cars and ships, various kinds of ships, and full electrification houses and factories electrification Such as, there is a background that can be obtained storage battery drive of extremely cheap power generation and prevention of global warming of the electric drive.
外れて欲しい予想は、中国が10%成長を50年続けると海水温度上昇量が現在の32倍になり、日本の季節風が50〜80m/秒となって国土全部が海水に汚染され、農業と緑が壊滅して餓死者続出が類似世界に拡大する可能性があり、今の雇用不安も小泉総理に再三予想を提供の日本大企業80%前後ゴーストタウン化が始まったのではと心配、危機をチャンスにする知恵が必要です。昭和17〜18年に理論最良エンジンの発明を決意実際は改良から始め、昭和38年岡山地方発明センターの請負で試作を開始して、自分でも試作を続けましたがエンジンの試作は非常に困難です。そこで昭和57年2月より国内大企業等多数にご協力のお願い始めましたが、日本企業等の協力が皆無で、外国唯一お願いしたクリントン大統領の協力がお願いの都度3年3回得られ、1992年米国特許5133305号、1993年米国特許5230307号、1995年米国特許5429078号の駄目発明が判明したのです。既存のエンジンに致命的な欠点が非常に多く改良発明不可能が判明し、急がば回れと1997年ホームページを開設して欠点を1つ改良特許出願して、2008年理論最良エンジンに到達し、元大統領の協力により例えば重力太陽熱発電により燃料費0で発電機及び熱ポンプを駆動して、無限大に近い電気及び温熱と冷熱を極端に安価製造タービン駆動可能とし、500°C以下液体金属発電で、大気圧同速度同容積仕事率を既存蒸気タービン発電の1〜2.3万倍にして、実際に実験して実験最良エンジンに移行したいのです。 It is expected that if China continues to grow at 10% for 50 years, the temperature rise of seawater will be 32 times that of the present, and Japanese monsoon wind will be 50 to 80m / sec, and the whole country will be polluted with seawater. It is feared that the greening of around 80% of Japan's large companies that offer the resumption of the current employment fear to Prime Minister Koizumi may have begun to be around around 80%, as greenery may be destroyed and successive deaths may extend to similar worlds We need wisdom to make Decided to invent the theoretical best engine in 1965. In fact, it began to improve and started trial production at the contract of the Okayama regional invention center in 1955, and continued trial production on its own, but trial production of the engine is very difficult. . Therefore, we started asking for a large number of large domestic companies to cooperate from February 1982. However, there is no cooperation from Japanese companies, etc. The cooperation of President Clinton who only asked foreign countries is obtained three or three times every request. The useless inventions of 1992 US Patent 5133305, 1993 US Patent 5230307 and 1995 US Patent 5429078 have been found. There are many fatal defects in the existing engine, and it turns out that it is impossible to improve the invention, and in a hurry and opens the 1997 home page, one defect patent application is filed and the 2008 theoretical best engine is reached To drive the generator and heat pump at a fuel cost of 0, for example, by gravity solar thermal power generation with the cooperation of the former president, and to enable extremely inexpensive manufacturing turbine drive for near infinite electricity and heat and cold, liquid metal below 500 ° C In power generation, I would like to make an atmospheric pressure same speed same volume work factor 1 to 23,000 times that of existing steam turbine power generation, actually experiment and shift to an experimental best engine.
既存世界の火力原子力発電所では、CO2増大地球温暖化加速や海水表面温度摂氏7度上昇海域を100年で1000倍等とし、大気中のCO2増大地球温暖化加速や海水温度上昇により下降気流や上昇気流を増大して、異常乾燥山火事や旱魃や集中豪雨等を限り無く増大人類の陸上食物を限り無く減少し、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、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、陸地全部に塩の被覆を設ける人類絶滅の危険を増大のため、地球温暖化防止して人類絶滅を先送りする課題が在り、化石燃料を大量に燃焼すると地球が温暖化すると共に資源が枯渇するため、CO2排気0で既存船舶の10倍速度を狙う重力太陽熱船舶類や、空気抵抗0CO2排気0の宇宙利用全盛の重力太陽熱飛行機類にして化石燃料燃焼は必要最少にして、限りある資源を子孫に残すと共に海水温度上昇0CO2排気0の重力発電蓄電池駆動の自動車類や船舶類にし、利益が少ないと協力不可能なため、利益率抜群の世界一の重力太陽熱船舶類や重力太陽熱飛行機類が必要です。 In existing thermal power nuclear power plants in the world, accelerating CO2 global warming and increasing sea surface temperature by 7 degrees centigrade to 1000 times over 100 years in 100 years, increasing CO2 in the atmosphere global warming accelerating and rising seawater temperature Increase the updraft, increase abnormally dry wildfires and droughts and torrential rains as much as possible, and decrease the land food of humanity as much as possible, and the natural phenomenon of supplying nutrients to the sea surface cooling seabed in the winter, impossible, Reduce phytoplankton, seaweeds, corals, etc., reduce fish to 1/100 by food chain, decrease human food in the sea as much as possible and increase flooding, torrential rain, typhoon, and monsoon by 10 times in 100 years. For example, typhoons and monsoon winds are an increase in abnormal weather without an upper limit of 300 m / s, etc., and salt coverage is provided on the entire land to increase the danger of human extinction, thereby curbing global warming and delaying human extinction. There are many issues, and burning a large amount of fossil fuel will cause global warming and exhaustion of resources, so space utilization of gravity solar thermal vessels and air resistance 0CO2 exhaust 0 aiming at 10 times the speed of existing ships with CO2 exhaust 0 Coexistence of limited use of fossil fuels for the generation of solar powered vehicles and ships driven by gravity storage batteries with sea water temperature rise 0CO 2 exhaust 0 with limited use of fossil fuels as a prime mover as a solar solar powered as a prime mover Because it is possible, we need the world's best gravity solar vessels and gravity solar airplanes with excellent profitability.
熱製造の熱ポンプを各種太陽熱重力タービンで駆動すると、温熱(過熱蒸気熱量)と冷熱(圧縮空気質量)を燃料費0で無限製造の挑戦となり、重力太陽熱発電や重力太陽熱船舶や重力太陽熱飛行機により、太陽熱や熱製造装置の熱ポンプにより温熱と冷熱の製造量を無限大に近付け、重力太陽熱発電では燃料費0でCO2を大気と共に吸引海底に供給して、限りある石油資源等は必要最小限の使用とし、子子孫孫まで残すと共に地球温暖化防止して、旱魃や海面上昇や台風や季節風の巨大化を阻止し、重力太陽熱船舶でもCO2を大気と共に吸引海中噴射して、既存船舶の10倍速度狙い噴射推進の過程で自然現象を高速化し、海中に冷熱の酸素や窒素やCO2等の栄養分供給を太陽熱重力発電と協力して、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、既存世界の10倍発電量以上として、各種重力太陽熱発電全盛にし、重力発電蓄電池駆動の各種自動車類全盛や各種船舶類全盛や、電気駆動の全面電化住宅全盛や工場電化全盛や温熱と冷熱利用全盛にして、海水温度上昇0やCO2排気0や燃料費0で発電し、地球温暖化防止の人類絶滅先送りにして、重力太陽熱飛行機類は既存ジェット機の100倍圧力10倍熱量噴射1000倍噴射出力狙いとし、過熱蒸気膨張速度が真空で最大のため既存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より大出力ロケット推進宇宙に到達して、大気中は燃料0飛行狙い+空気抵抗0CO2排気0の宇宙飛行全盛にします。 When the heat pump of heat production is driven by various solar thermal gravity turbines, it becomes a challenge of infinite heat production (thermal heat of superheated steam) and cold heat (compressed air mass) with zero fuel cost, by gravity solar thermal power generation, gravity solar thermal ship or gravity solar thermal airplane , Heat capacity of the solar heat and heat production equipment brings the amount of heat and cold close to infinity, and in gravity solar power generation, the fuel cost is 0 and CO2 is supplied to the suction seabed together with the atmosphere, and the limited oil resources etc. Use as the offspring and descendants as well as to prevent global warming, to prevent flooding, sea level rise and typhoon and the increase of the size of the monsoon wind, and even a gravity solar thermal vessel sucks CO2 together with the atmosphere and sinks it under the sea; In the process of double-speed aiming injection promotion, natural phenomena are accelerated, and nutrients such as cold heat oxygen, nitrogen, and CO2 are supplied to the sea in cooperation with solar thermal gravity power generation to produce phytoplankton, seaweeds and Increase the food of humans and increase the food of human beings and make it 10 times more power than in the existing world, and make various gravity solar thermal power generations full, various vehicles such as gravity power storage battery driven and various ships fullness, all surfaces of electric drive Electrified housing and factory electrification and thermal and cold energy utilization, power generation with seawater temperature rise 0, CO2 exhaust 0 and fuel cost 0, and humanity extinction for global warming prevention, and extinct of gravity solar thermal airplanes existing jet aircraft 100 times pressure 10 times thermal energy injection 1000 times injection power target, and the superheated steam expansion speed is maximum in vacuum, and the existing rocket ground ground injection is regarded as the worst, reaching the high power rocket propulsion space from the existing aircraft highest flight altitude In the atmosphere, fuel 0 flight aim + air resistance 0 CO 2 exhaust 0 space flight to the fullest.
竪型金属球水銀重力太陽熱タービン8G駆動+各種重力タービンと併用駆動可能とし、宇宙では温熱加速と冷熱加速にして大気中では重力追加駆動で使用して、金属球水銀重力太陽熱エンジン回転出力発生にし、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、竪型金属球水銀重力太陽熱タービン8G駆動の各種重力太陽熱エンジンとし、宇宙では太陽光直射部120度Cと日陰部−150度Cという絶好環境を利用して、過熱蒸気タービン駆動や過熱蒸気製造絶好の環境を利用して、吸入空気路28Aを密閉して循環空気路とし、冷熱タービン排気を直射120度太陽光と長レンズ等で回収して、500度等に加熱して熱ポンプにより1200度前後に圧縮し、圧縮熱回収器2Cで熱交換過熱蒸気50製造にして、温熱タービンを駆動その排気を−150度日陰部で冷却して復水にする循環を繰り返し、通常は燃焼ガス使用0合体機関噴射部78Bより過熱蒸気50のみ噴射する噴射推進出力発生にして、燃料量0で既存ジェットエンジンの10倍噴射推進出力狙い理論最良ロケット推進にし、過熱蒸気膨張速度が真空で最大のため既存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大出力ロケット推進して、宇宙到達燃料費を1/100以下等僅少にし、既存世界の各種船舶類や各種飛行機類で宇宙利用全盛を狙う効果と、資源を子孫に残す効果があります。 Vertical-type metal sphere mercury gravity solar thermal turbine 8G drive + various gravity turbines can be used in combination, thermal acceleration and cold thermal acceleration in space and using gravity additional drive in the atmosphere, metal sphere mercury gravity solar thermal engine rotational power generation The injection propulsion output is 100 times the pressure 10 times the amount of heat injection of the existing jet time short term 1000 times injection promotion output aiming at various gravity solar thermal engines driven by vertical metal sphere mercury gravity solar thermal turbine 8G, 120 degrees direct sunlight in space C and shaded area-utilizing the optimum environment of 150 ° C, utilizing the superheated steam turbine drive and the superheated steam production environment, the intake air passage 28A is sealed to form a circulating air passage, and the cold heat turbine exhaust gas is exposed directly Recovered with 120 degree sunlight and long lens etc., heated to 500 degrees etc., compressed by a heat pump to around 1200 degrees, compressed heat recovery unit 2C Production of replacement superheated steam 50 and driving of the thermal turbine is repeated by cooling its exhaust at the -150 degree shade to be condensed, and usually only the superheated steam 50 is injected from the combustion gas use 0 combined engine injection part 78B. As the injection propulsion power generation, the fuel amount is 0 and the existing jet engine is 10 times injection propulsion power aiming theory best rocket propulsion, and the superheated steam expansion speed is maximum in vacuum, so the existing rocket ground mass injection is considered the worst, the existing aircraft maximum Propulsion of high-powered rockets from near the flight altitude, reducing the attainment fuel cost to as low as 1/100 or less, aiming to use the space in various ships and airplanes in the existing world, and leaving resources to descendants There is.
発明の実施の形態や実施例を、図面を参照して説明するが、実施形態や実施例と既説明とその構成が略同じ部分には、同一の名称又は符号を付して、重複説明はできるだけ省略し、特徴的な部分や説明不足部分は、順次追加重複説明する。又非常に難解な脳内理論最良エンジン発明のためと、意図する所及び予想を具体的に明快に説明するため、アイディアを仮説数字で説明するが、正解は実験数字として理論最良エンジンの仮説数字に限定しません。最良と思われるアイディアを多数の用途で重複説明し、用途に合せてアイディアを選択使用して、請求項では多用途に合せて選択使用するため千変万化し、理論最良エンジンから順次噴射推進を含む資源量や需要量に合わせた出力として、例えば無限需要量の発電は水出力や衝撃低減タービン駆動にして軽量大出力が最も重要な飛行機類は水銀出力や衝撃低減タービン駆動とし、軽量大出力が重要な船舶類は鉛合金中核液体金属出力や衝撃低減タービン駆動として、実験最良エンジンに移行実用化します。 The embodiments and examples of the invention will be described with reference to the drawings, but the same names and symbols are given to parts substantially the same as the ones in the embodiments and examples described above. It will be omitted as much as possible, and the characteristic parts and the inexplicable parts will be sequentially added and explained. In addition, although the idea is explained with hypothesized numbers in order to clearly explain the intended purpose and prediction specifically for the extremely difficult brain theory best engine invention, the correct answer is the experimental number of the theoretical best engine as the experimental number. Not limited to The idea that seems to be the best is redundantly explained in many applications, and the idea is selected and used according to the application, and the claim is converted into a variety for selection and use according to the versatility, resources from theoretical best engine to sequential injection promotion As output according to the volume and demand volume, for example, power generation with infinite demand is driven by water output and impact reduction turbine, and light and large output is most important airplanes with mercury output and impact reduction turbine drive, light and large output is important Marine vessels will be put to practical use as the lead engine core liquid metal power and impact reduction turbine drive, etc.
図1の竪型金属球水銀重力温熱タービン8G駆動は、増大球上昇装置2Fを設けて金属球水銀を最上部に上昇保存して、外箱77a内に1〜10段等タービンを垂直に多段に設けて用途に合わせた台数使用にし、1種類使用では温熱タービン8G冷熱タービンの選択使用として、2種類使用は温熱タービン+冷熱タービン使用にし、金属球水銀を水銀噴射ポンプ6Zで噴射して過熱蒸気温熱加速重力加速度加速して、竪型金属球水銀重力温熱タービン8Gを駆動し、タービン間に横軸1hを設けてタービン外箱77a外で、発電機1や熱ポンプ1Gや圧縮熱回収器2Cや水熱交換器2Yや空気熱交換器2Xを駆動して、タービン8Gの回転方向を交互にして振動や騒音を相殺僅少にし、太陽熱を種に熱ポンプ1Gと圧縮熱回収器2Cで無限大に近い温熱(圧縮空気熱量の過熱蒸気)や冷熱(圧縮空気質量)を製造して、例えば500度前後24〜400MPa過熱蒸気温熱+100ヘ200度前後24〜400MPa圧縮空気冷熱に分割保存し、一部と重力で温熱タービン+冷熱タービンを駆動して、大部分で合体機関噴射部78Bを駆動太陽熱重力ヘリコプター39C飛行にし、停止中は熱と電気の供給設備等で使用します。 The vertical ball type metal sphere mercury gravity thermal turbine 8G drive of FIG. 1 is provided with an increase ball elevation device 2F to ascend and store the metal sphere mercury at the uppermost part, and multistage vertically 1 to 10 stages etc. turbines in the outer box 77a. The number of heat pumps used in the number according to the application, and one type of heat turbine is used as a selective use of 8G cold heat turbine, two types of heat heat turbine + cold heat turbine is used, metal ball mercury is injected by mercury jet pump 6Z and overheated Steam thermal acceleration Gravity acceleration is accelerated to drive the vertical metal ball mercury gravity thermal turbine 8G, the horizontal axis 1h is provided between the turbines, and the generator 1, the heat pump 1G, and the compression heat recovery device outside the turbine outer box 77a. Drive 2C, water heat exchanger 2Y and air heat exchanger 2X to alternate the direction of rotation of turbine 8G to offset vibration and noise slightly, and use solar heat as a seed for heat pump 1G and compression heat recovery machine 2C for infinity Big Produce close thermal energy (superheated steam of compressed air heat) and cold energy (compressed air mass), for example, divide and store it into around 500 to 24 to 400 MPa superheated steam thermal + 100 to around 200 to 24 to 400 MPa compressed air cold, And by driving the thermal turbine + cold thermal turbine by gravity and driving the combined engine injection part 78B in most part by the solar thermal gravity helicopter 39C flight, it is used in the supply equipment of heat and electricity while stopped.
温熱タービン8G駆動の過程では、冷熱タービン8Gで冷却した金属球水銀を500度前後過熱蒸気50で加熱温度上昇して、冷熱タービン駆動圧縮空気冷熱容積増大にして回転出力を増大し、冷熱タービン排気を合流抽出器51で吸入圧縮して、最適圧力冷熱にし、合体機関噴射部78Bの最適圧力高速冷熱で吸引して、混合合流酸化剤で使用する循環にし、温熱タービン排気の過熱蒸気も合流抽出器51で吸入圧縮して、合体機関噴射部78Bの最適圧力高速温熱で吸引し、混合合流推進剤で使用する循環にして、内側動翼群60C外側動翼群60Dは大重量を支える油圧浮上追加の推力軸受80aを具備し、全自動加工可能に段落毎同径略同形として嵌合ボルト組立にして、多段動翼群と多段タービンを可能にすると共に組立容易にし、金属球水銀を加速する重力加速部1gには横軸1hや貫通穴を具備して、発電機1や熱ポンプ1G多数等をタービン外箱77aの外で駆動し、太陽熱加熱の空気を圧縮1000度前後にして、空気熱交換器2Xで太陽熱加熱の別空気を600度C等に加熱して圧縮1200度前後にし、繰り返して高圧の圧縮空気28a冷熱と過熱蒸気50温熱の熱製造量を増大して、大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービンの2.3万倍前後水銀仕事率等にし、既存タービン翼断面積の2〜26倍断面積にしたタービン翼断面4Xに噴射して、転がり接触回転出力発生で重力や太陽熱を最大限利用し、熱ポンプ駆動して圧縮空気冷熱製造と温熱(過熱蒸気)を製造する、竪型金属球水銀重力温熱タービン8Gにします。 In the process of thermal turbine 8G drive, the temperature of metal ball mercury cooled by cold heat turbine 8G is raised by heating temperature around 500 degrees by superheated steam 50, cold heat turbine drive compressed air cold heat volume is increased to increase rotational power, cold heat turbine exhaust Are suctioned and compressed by the joint extraction unit 51 to obtain optimum pressure cooling and suctioned by the optimum pressure high-speed cooling of the united engine injection part 78B to be used as a circulation by the mixing and joining oxidant, and the superheated steam of the thermal turbine exhaust is also joined and extracted The inner bucket blade group 60C and the outer bucket blade group 60D support large weight by hydraulic suction by suction and compression by the compressor 51, suction by the optimum pressure high speed thermal of the united engine injection unit 78B, and circulation by using mixing and mixing propellant. It has an additional thrust bearing 80a, and can be fully automated and can be assembled in the same diameter and substantially the same shape for each stage into a mating bolt assembly, enabling multistage blade groups and multistage turbines and facilitating assembly A metallurgical acceleration unit 1g that accelerates metal sphere mercury is equipped with a horizontal axis 1h and a through hole, and drives a large number of generators 1, heat pumps 1G, etc. outside the turbine casing 77a to compress solar heating air 1000 The heat of solar heat is separately heated to 600 ° C and so on with the air heat exchanger 2X and compressed to around 1200 ° C, repeatedly increasing the heat production of high pressure compressed air 28a cold energy and superheated steam 50 temperature A turbine blade with a cross-sectional area of 2 to 26 times that of the existing turbine blade by converting the atmospheric pressure same velocity and volumetric work ratio kg weight m / sec to about 23,000 times the mercury work rate of the existing steam turbine etc. Vertical-type metal sphere mercury gravity thermal turbine 8G which injects to the cross section 4X and makes maximum use of gravity and solar heat by rolling contact rotational power generation and heat pump drive to produce compressed air cold heat and heat (superheated steam) I will.
図2の竪型金属球水銀重力冷熱タービン8G駆動も、外箱77a内に1〜10段等タービンを垂直に多段に設けて、用途に合わせた台数使用にして、温熱タービン駆動で温度上昇した金属球水銀を増大球上昇装置2Fで最上部に上昇保存し、金属球水銀を水銀噴射ポンプ6Zで噴射して圧縮空気28a冷熱加速重力加速度加速して、竪型金属球水銀重力冷熱タービン8Gを金属球水銀の転がり接触で駆動し、駆動の過程で絶対0度に近付く圧縮空気28aを温度上昇した金属球水銀で加熱して、圧縮空気容積速度を増大してタービン出力を増大して金属球水銀を冷却し、冷却した金属球水銀で温熱タービン8G駆動金属球水銀温度を上昇する循環として、温度上昇した冷熱タービン排気空気28aを合流抽出器51で吸入圧縮し、低圧冷熱排気として出力増大にして、合体機関噴射部78Bの最適圧力高速冷熱で吸引し、混合合流酸化剤で使用する循環にして、熱ポンプと共に金属球水銀重力冷熱タービンによる噴射推進出力の上昇にし、圧縮空気28a冷熱の最大限活用にします。 In the vertical metal ball mercury gravity cold heat turbine 8G drive of FIG. 2 as well, the 1-10 stages etc. turbines are vertically provided in the outer case 77a in multiple stages vertically, and the temperature is raised by the thermal turbine drive by using the number according to the application. Metal ball mercury is raised and stored at the top with the ball rising device 2F, metal ball mercury is injected by the mercury jet pump 6Z and compressed air 28a cold thermal acceleration Gravity acceleration is accelerated, and the bowl-shaped metallic ball mercury gravity cold thermal turbine 8G Metal spheres are driven by rolling contact with mercury, and compressed air 28a, which approaches absolute zero in the process of driving, is heated with metal sphere mercury heated to increase compressed air volume velocity and increase turbine output to increase metal spheres. Cooled mercury, and cooled metal ball mercury as thermal gas turbine 8G drive metal ball as circulation to raise the temperature of mercury ball Cooled heat exhaust gas exhaust air 28a with temperature rise was combined and suctioned by extractor 51, low pressure cold heat exhaustion As the power increase, combined engine injection part 78B optimal pressure high speed cold air suctioned, mixed combined oxidant used in circulation, heat pump with metal ball mercury gravity cold heat turbine increased injection propulsion output, compressed air 28a Make the most of cold energy.
タービン間重力加速部1gに貫通穴と横軸1hを設けタービン外箱77a外で、発電機1や熱ポンプ1Gや圧縮熱回収器2Cや水熱交換器2Yや空気熱交換器2X等を駆動して、タービン8Gの回転方向を交互にして振動や騒音を相殺僅少にし、太陽熱を種に熱ポンプ1Gと空気熱交換器2Xで無限大に近い温熱や冷熱を製造して、24〜400MPa過熱蒸気温熱+24〜400MPa圧縮空気冷熱に分割保存使用し、圧縮空気28a冷熱で金属球水銀を加速駆動する、竪型金属球水銀重力冷熱タービン8Gにして、内側動翼群60C外側動翼群60Dには、大重量を支える油圧浮上追加の推力軸受80aを具備して多段タービンを可能にし、太陽熱加熱の空気を圧縮1000度前後にして、空気熱交換器2Xで太陽熱加熱の別空気を500度C等に加熱して圧縮1200度前後にし、繰り返して高圧の圧縮空気28aと過熱蒸気50の製造量を増大するエネルギ保存サイクルにして、大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービンの2.3万倍前後水銀仕事率等にし、既存タービン翼断面積の2〜26倍断面積にしたタービン翼断面4Xに噴射して、転がり接触回転出力発生とし、重力や太陽熱を最大限利用する、竪型金属球水銀重力冷熱タービン8Gにします。 A through hole and horizontal axis 1h are provided in the inter-turbine gravity acceleration unit 1g, and the generator 1, heat pump 1G, compression heat recovery device 2C, water heat exchanger 2Y, air heat exchanger 2X, etc. are driven outside the turbine outer box 77a. Then, the rotational direction of the turbine 8G is alternated to offset the vibration and noise slightly, and the solar heat is used as a heat pump 1G and the air heat exchanger 2X to produce nearly infinite heat and cold, 24 to 400MPa heating Steam thermal +24-400MPa compressed air cold storage divided use, compressed air 28a cold metal accelerated metal ball mercury by acceleration, vertical type metal sphere mercury gravity cold thermal turbine 8G, inner rotor blade group 60C outer rotor blade group 60D Support hydraulic lift and additional thrust bearing 80a to support a large weight, enable multi-stage turbine, compress solar heating air around 1000 degrees, separate solar heating air with air heat exchanger 2X 50 Heat to about 120 ° C and so on to a compression temperature of around 1200 ° C, and repeatedly create an energy storage cycle that increases the production volume of high pressure compressed air 28a and superheated steam 50, atmospheric pressure same speed same volume work power kg weight m / s , 23,000 times the mercury work rate of the existing steam turbine, etc., 2 to 26 times the cross-sectional area of the existing turbine blade injection to the turbine blade cross-section 4X, rolling contact rotational power generation, gravity and solar thermal Make the most of the vertical metal ball mercury gravity cooling turbine 8G.
図3の合体機関噴射部78B太陽熱重力ヘリコプター39C回転出力噴射推進出力発生は、重力使用が限定されるため飛行胴38a船体10を一体として、金属球水銀重力冷熱タービン8G+金属球水銀重力温熱タービン使用で落差を最適にし、空気吸入口28Bより空気28aを吸入の過程で、長レンズ2d熱吸収材2Bで構成の吸入空気路28Aで太陽光加熱の空気28aを吸入して、熱ポンプ1Gで圧縮1000度等にして空気熱交換器2Xで太陽光加熱の別空気28aで熱回収し、熱ポンプ1Gで圧縮1200度等として熱回収を繰り返す圧縮熱製造として、水熱交換器2Yでは過熱蒸気50製造で熱回収を繰り返す熱製造とし、宇宙上昇時には圧縮熱回収器2Cで燃料噴射燃焼限り無く高圧燃焼熱交換冷却燃焼して、繰り返し圧縮1200度等にして水熱交換器2Yで熱回収を繰り返して、過熱蒸気50温熱と燃焼ガス49冷熱を、既存ジェット機噴射圧力の10〜100倍圧力等で合体機関噴射部78Bに供給し、燃焼ガス49に燃料噴射燃焼外周の過熱蒸気50を加熱全部で10倍熱量等を噴射して、噴射推進出力を既存ジェット機の100〜1000倍に短時間近付けて宇宙に到達し、宇宙では超音速マッハ32の地球脱出速度や光の速度に近付けて、各種飛行船舶類や各種航空機類で燃料費0に近い宇宙利用全盛にし、中間圏飛行や成層圏飛行を可能にして、大気中では複数回転翼7Bを夫々の2.3万倍前後水銀等仕事率タービンで回転駆動飛行し、圧縮空気28a酸化剤冷熱と過熱蒸気50推進剤温熱を貯蔵増大し、既存宇宙ロケット地上大量噴射を最悪噴射と考え、既存航空機最高飛行高度付近より大出力ロケット推進して、宇宙到達燃料費を1/100以下等僅少にします。 The combined engine injection part 78B solar thermal gravity helicopter 39C rotational output injection propulsion power generation of FIG. 3 uses the metallic sphere mercury gravity cold thermal turbine 8G + metallic sphere mercury gravity thermal thermal turbine with the flight shell 38a hull 10 integrally because the use of gravity is limited. In the process of suctioning the air 28a from the air suction port 28B, the sun-heated air 28a is suctioned by the suction air passage 28A composed of the long lens 2d heat absorbing material 2B and compressed by the heat pump 1G. Heat is recovered by another air 28a of solar heating with air heat exchanger 2X at 1000 degrees etc., and heat recovery is repeated with heat pump 1G as compression 1200 degrees etc with heat pump 1G. Superheated steam 50 with water heat exchanger 2Y. Heat production is repeated in heat production, and when it goes up in space, compression heat recovery unit 2C performs high pressure combustion heat exchange cooling combustion as much as fuel injection combustion as much as possible, and repeated compression Heat recovery is repeated with the water heat exchanger 2Y at 200 ° C, etc., and the superheated steam 50 thermal energy and the combustion gas 49 cold energy are supplied to the combined engine injection part 78B at a pressure 10 to 100 times the existing jet machine injection pressure, etc. Heat the superheated steam 50 of the fuel injection combustion periphery to the gas 49 and inject a total of 10 times the heat amount etc., and make the injection propulsion output close to 100 to 1000 times of the existing jet for a short time to reach space. Close to the Earth's escape velocity and speed of light, make it possible to use space with a fuel cost close to zero with various types of flight vessels and aircraft, enable mesosphere flight and stratosphere flight, and make multiple rotors 7B in the atmosphere The rotary drive flight of about 23,000 times the power rate turbine around mercury, compressed air 28a oxidizer cold heat and superheated steam 50 store thermal increase, increase the existing space rocket ground massive injection worst injection With the idea, and large output rocket propulsion from the vicinity of the existing aircraft maximum flying altitude, and the universe reaching fuel costs to equal insignificant 1/100 or less.
大気中を飛行時には、竪型金属球水銀重力タービン8G複数駆動の、回転翼7B複数の回転出力により垂直上昇降下海上陸上何処でも着水着陸可能に飛行し、熱ポンプ1G・圧縮熱回収器2C・空気熱交換機2X・水熱交換器2Yを、横並び又は立て並びタービン横軸1h駆動として、用途に合わせた台数を夫々1〜10段に設けて落差を増大し、金属球水銀を水銀噴射ポンプ6Zで噴射して、分割保存した圧縮空気冷熱+圧縮空気温熱で加速し、夫々の竪型金属球水銀重力タービン8Gに噴射して、タービン翼断面4Xを既存蒸気タービンの2〜26倍にし、タービン翼8cに噴射転がり接触駆動で重力や太陽光を最大限利用して、大気圧同速度同容積仕事率kg重m/秒を、既存蒸気タービンの2.3万倍前後水銀等仕事率にし、熱ポンプ多数を重力太陽熱駆動して、24〜400MPa過熱蒸気50温熱と24〜400MPa圧縮空気28a冷熱を限り無く増大し、空気吸引噴射推進する出力の発生は、合体機関噴射部78Bに分割保存した過熱蒸気50温熱と圧縮空気49冷熱を供給して、冷熱に燃料噴射燃焼双方の噴射温度を近付けることで理論最良の噴射とし、既存ジェット機の10〜100倍圧力1/10噴射熱量10倍噴射推進出力大型化等として、船体10の外部に複数設けた、合体機関噴射部78Bを180度以上回転して逆噴射や垂直上昇垂直降下を可能にし、宇宙利用全盛や水上等何処でも着水着陸可能にして、月面着陸等の場合は4脚や6却等を設けて着陸可能にします。 When flying in the atmosphere, the vertical rising descent can be made to land and land anywhere on the ground by the rotary power of multiple rotary blades 7B, driven by vertical-type metal ball mercury gravity turbine 8G multiple drives, heat pump 1G, compression heat recovery device 2C · The number of air heat exchangers 2X · water heat exchangers 2Y are driven side by side or side by side with a horizontal axis or turbine horizontal axis 1h, the number according to the application is provided in 1 to 10 stages respectively to increase the head difference and mercury metal mercury mercury pump Sprayed at 6Z, accelerated by divided and stored compressed air cold + compressed air thermal, injected to each vertical metal ball mercury gravity turbine 8G, and the turbine blade cross section 4X is 2 to 26 times the existing steam turbine, Make maximum use of gravity and sunlight at the turbine blade 8c by injection rolling contact drive, and make the atmospheric pressure same velocity same volume work ratio kg weight m / s to be about 23,000 times mercury such as existing steam turbine , Heat pong Super heat steam driven by gravity solar heat to increase the heat of 50 to 24 to 400MPa superheated steam and 24 to 400MPa compressed air 28a as much as possible by gravity solar heat generation and generating air suction and injection propulsion in split engine jet part 78B 50 thermal energy and compressed air 49 cold energy are supplied, and the injection temperature of both fuel injection and combustion is brought close to cold energy to make it the theoretical best injection, 10 to 100 times the pressure of the existing jet machine As rotation, etc., a plurality of united engine injection units 78B provided outside of the hull 10 are rotated 180 degrees or more to enable reverse injection and vertical ascent and vertical descent, and landing landing on any place, such as space use prime or water, In the case of landing on the moon, etc., landing is possible by providing 4 legs or 6 turns.
宇宙到達時前に回転翼7Bを停止して、竪型金属球水銀重力冷熱タービン8G駆動、空気路入口28Bを密閉冷熱タービン8Gの圧縮空気28a低圧低温排気により、120度直射太陽光の熱量を長レンズ2d熱吸収材2Bの空気28a排気で熱回収し、500度前後排気を温熱タービン駆動と冷熱タービン駆動多数の熱ポンプ1Gで圧縮して、1200度前後にして空気熱交換器2Xで太陽光加熱の別空気28aで熱交換熱回収し、熱ポンプ1Gで圧縮1200度等にして熱回収とタービン駆動を繰り返して、同様に水熱交換器2Yでは過熱蒸気50製造と温熱タービン駆動を繰り返し、宇宙では過熱蒸気50温熱を120度直射太陽光で最も効率良く製造貯蔵して、温熱タービン8Gや冷熱タービン8Gを温熱駆動や冷熱駆動重力0に対応し、宇宙での噴射推進は過熱蒸気50推進剤による噴射推進とし、圧縮空気28aは過熱蒸気50の製造や生命維持物質で使用して、長距離の宇宙旅行を可能にし、地球帰還時には摩擦熱を含む高圧高温空気28aを吸入圧縮熱交換する熱製造にして、圧縮空気28a冷熱で冷熱タービン8Gを駆動し、その排気を合流抽出器51により吸入最適圧力に圧縮して、合体機関噴射部78B酸化剤の高速最適圧力部で吸引混合合流し、燃料噴射着火燃焼噴射推進出力の増大に使用します。 Stop the rotor 7B before reaching the space, drive the vertical metal ball mercury gravity cold-heat turbine 8G, the air passage inlet 28B by compressed air 28a low-pressure low-temperature exhaust of cold air turbine 8G 120 ° C The heat is recovered by the air 28a exhaust of the long lens 2d heat absorbing material 2B, and the exhaust around 500 degrees is compressed by the thermal turbine drive and the large number of heat pumps 1G driven by the cold heat turbines. Heat-exchanged heat is recovered with another air 28a for light heating, and heat recovery and turbine drive are repeated with compression set at 1200 ° C using heat pump 1G, and similarly, superheated steam 50 production and thermal turbine drive are repeated in water heat exchanger 2Y. In the universe, superheated steam 50 thermal energy is produced most efficiently by direct sunlight at 120 ° C, and thermal turbine 8G and cold turbine 8G are used against thermal drive and cold drive gravity 0 In the space, the injection propulsion is by the superheated steam 50 propellant, and the compressed air 28a is used in the production of the superheated steam 50 and life support material to enable long distance space travel, and the frictional heat at the time of earth return The high-pressure high-temperature air 28a including the above is heat-suction-heat-exchanged to produce heat, and the cold-heat turbine 8G is driven by cold air of the compressed air 28a, and the exhaust is compressed to a suction optimum pressure by the merging extractor 51. At high speed optimum pressure section of the oxidant, suction mixing and joining are performed, and it is used to increase the fuel injection ignition combustion injection propulsion output.
図4の合体機関噴射部78B駆動は、過熱蒸気制御弁25を開放分割保存した過熱蒸気50を燃焼器1Y外周の過熱蒸気溜95cの最上流に供給し、宇宙上昇準備の場合は推進剤の過熱蒸気50製造の過程で圧縮空気28aに燃料噴射燃焼して、圧縮熱回収器2Cで複数回圧縮燃料噴射燃焼複数回熱回収し、限り無く高圧の燃焼ガス49酸化剤と過熱蒸気50推進剤を貯蔵限り無く増大して、宇宙上昇時には燃焼ガス制御弁24を開放し、200度前後24〜400MPa燃焼ガス49を燃焼ガス溜95a燃焼器1Yの最上流に供給して、燃料制御弁25b開放燃料噴射ポンプ1Dにより燃料1bを燃料噴射ノズル6Xより噴射し、燃焼器1Y最上流で着火燃焼外周の過熱蒸気50を加熱燃焼温度上昇して、外周長大な過熱蒸気溜95cの400度前後24〜400MPa過熱蒸気50を加熱双方の噴射出力を増大し、燃焼器1Yの複数燃焼ガス噴射ノズル6Yを過熱蒸気溜95c内部環状に具備して、複数1段噴射燃焼流の燃料噴射ノズル6Xより燃料噴射2段燃焼器複数最適距離環状燃焼にし、過熱蒸気50を外周と内周より加熱噴射出力と燃焼ガス吸引出力を増大して、燃焼ガス燃焼流に複数の燃焼ガス噴射ノズル6Yを具備し、夫々の燃料噴射ノズル6Xより燃料噴射3段燃焼器複数最適距離環状燃焼にして、必要に応じて同様に4段燃焼し、過熱蒸気50噴射流を内周と外周から環状加熱して、大気圧では100度Cに近付き真空では0度に近付く過熱蒸気を500度等とし、既存ジェット機の10〜100倍圧力10倍質量噴射の安価な噴射出力狙いにします。 The combined engine injection unit 78B shown in FIG. 4 supplies the superheated steam 50 with the superheated steam control valve 25 opened and divided and stored in the uppermost stream of the superheated steam reservoir 95c on the outer periphery of the combustor 1Y. Fuel is injected into compressed air 28a in the process of producing superheated steam 50, and the heat is recovered multiple times by compressed heat recovery device 2C and compressed fuel injection combustion multiple times, and heat is recovered a number of times, infinitely high pressure combustion gas 49 oxidant and superheated steam 50 propellant As much as possible for storage, open the combustion gas control valve 24 at the time of ascent, and supply combustion gas 49 around 200 degrees to the uppermost stream of the combustion gas reservoir 95a combustor 1Y to open the fuel control valve 25b. The fuel 1b is injected from the fuel injection nozzle 6X by the fuel injection pump 1D, and the overheated steam 50 of the ignition combustion outer periphery is heated and heated to rise at the uppermost stream of the combustor 1Y. The injection output of both heating is increased by heating the superheated steam 50 of around 24 to 400 MPa around 0 degrees, and the multiple combustion gas injection nozzle 6Y of the combustor 1Y is provided in an annular shape inside the superheated steam reservoir 95c, and fuel injection of multiple one-stage injection combustion flow Two-stage fuel injection from the nozzle 6X Multiple optimal distance annular combustion is performed, and the heating injection output and the combustion gas suction output are increased from the outer circumference and the inner circumference of the superheated steam 50 to make the combustion gas combustion flow a plurality of combustion gas injection nozzles 6Y. The fuel injection three-stage combustor multiple optimal distance annular combustion from each fuel injection nozzle 6X, and similarly four-stage combustion as necessary, annularly heating the superheated steam 50 injection flow from the inner circumference and the outer circumference The superheated steam that approaches 100 ° C at atmospheric pressure and approaches 0 ° C at vacuum is set to 500 ° C, etc., aiming for an inexpensive jet output of 10 to 100 times the pressure and 10 times the mass jet of the existing jet.
大気中で更に大幅な噴射推進出力の増大が可能に、空気28a吸入路最適位置に複数の燃料噴射ノズル6Xを具備して、燃料噴射着火燃焼して短時間大幅な燃料燃焼量の増大と噴射推進出力の増大とし、過熱蒸気50の低温噴射大膨張速度と燃焼ガス49の高温噴射とロケットを合体して、夫々の長所を利用最良の組み合わせにした理論最良の合体機関噴射部78Bとし、スクラムジェットの高速燃焼と蒸気タービンの高圧噴射とロケットの真空飛行を合体して、大気中を通常飛行時には3.6万倍仕事率タービン等で圧縮熱回収器2Cの燃焼が不要で、上記燃焼ガス制御弁24開放が圧縮空気制御弁24A開放となり、太陽光加熱の空気28aを圧縮酸化剤製造し、1000度等に圧縮して圧縮熱回収器2Cで熱交換過熱蒸気50の推進剤製造にして、推進剤と酸化剤を保存増大主として過熱蒸気50による噴射推進とし、1段燃焼も2段燃焼も3段燃焼も僅少にする地球温暖化防止推進として、100度に近付く過熱蒸気50を500度等に加熱噴射推進出力を大幅に増大し、過熱蒸気容積の大部分を増大噴射速度を増大燃焼ガス49の吸引力を増大して、最も効率良く過熱蒸気50と燃焼ガス49を混合噴射する合体機関噴射部78Bを駆動し、スクラムジェット高速燃焼+蒸気タービンの高圧噴射大膨張速度+ロケットと合体して、過熱蒸気50や圧縮空気28aの酸化剤や推進剤を保存使用し、円筒回転部77Gを180度以上の回転にして垂直上昇や垂直降下や逆噴射を可能にして、何処でも飛行場や宇宙利用全盛にし、地球上何処でも日帰り旅行等を可能にします。 The fuel injection ignition combustion is performed in a short time with a large increase in the amount of fuel combustion and injection, with a plurality of fuel injection nozzles 6X at the optimum position of the air intake path, allowing a significant increase in the injection propulsion output in the atmosphere. To increase the propulsion output, combine the rocket with the low-temperature injection large expansion rate of the superheated steam 50 and the high-temperature injection of the combustion gas 49, and make the best combination engine injection part 78B of theoretical best using their respective advantages as the scrum Combining high-speed combustion of jets, high-pressure injection of steam turbines and vacuum flight of rockets, there is no need to burn compression heat recovery device 2C with a 36,000 times power ratio turbine etc. during normal flight in the atmosphere, the above combustion gases The control valve 24 is opened and the compressed air control valve 24A is opened. The solar heating air 28a is manufactured as a compressed oxidant, compressed to 1000 ° C., etc. and compressed by the heat recovery device 2C. In order to promote the global warming prevention by promoting injection and promotion mainly by the superheated steam 50, and reducing the one-stage combustion, the two-stage combustion and the three-stage combustion, the superheated steam 50 approaching 100 degrees. The heating injection propulsion output is greatly increased to 500 degrees etc., the superheated steam volume is increased by a large amount, the injection speed is increased, the suction power of the combustion gas 49 is increased, and the superheated steam 50 and the combustion gas 49 are mixed most efficiently. The combined engine injection unit 78B to be injected is driven to combine with the scramjet high speed combustion + high pressure injection high expansion velocity of the steam turbine + rocket to store and use the oxidant and propellant of the superheated steam 50 and the compressed air 28a. The rotation part 77G is rotated by 180 degrees or more to enable vertical ascent, vertical descent and reverse injection, making it possible to fly anywhere in the airfield and space, and to make day trips etc. anywhere on the earth.
理論最良タービンの竪型金属球水銀重力太陽熱タービン8G+各種重力太陽熱タービン選択併用を可能として、太陽光加熱の空気を熱ポンプで吸入圧縮熱回収して24〜400MPa等の温熱+冷熱で保存使用し、タービン駆動合体機関噴射部78B太陽熱重力ヘリコプター39C駆動として、垂直上昇や垂直降下や逆噴射を可能にして、何処でも飛行場や宇宙利用全盛にし、地球上何処でも日帰り旅行等を可能にする可能性があります。 Theoretically the best of the vertical-shaped metal ball mercury gravity solar thermal turbine 8G + various gravity solar thermal turbine selection combined use, air of solar heating is suction heat compression heat recovery with heat pump and stored and used with heat + cold such as 24 to 400MPa As a turbine-driven combined engine injection unit 78B solar thermal gravity helicopter 39C drive, it enables vertical ascent, vertical descent and reverse injection, making it possible to fly anywhere in the airfield or space, and possibly make day trips etc. anywhere on earth there is.
0:真空、 1:発電機、 1A:水銀排気検査室、 1B:酸素量増大手段、 1C:アルコール冷熱、 1D:燃料噴射ポンプ、 1F:復水ポンプ、 1G:熱ポンプ、 1H:揚水ポンプ、 1J:揚水装置、 1Y:燃焼器、 1b:燃料、 1c:比重大物質、 1d:水銀、 1e:被覆鋼球(衝撃低減手段2Gで被覆) 1e:被覆水銀(球形のステンレス等耐久材や衝撃低減手段2Gで被覆) 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傾斜回転して追跡) 2a:水復水器、 2a:復水冷却器、 2b:太陽熱増大吊橋(吊具左右を上下して長レンズ複数段で太陽光を傾斜回転して追跡) 2c:断熱材、 2d:長レンズ、 2e:水面、 2f:吊具左、 2g:吊具右、 2h:海水冷却器、 2z:太陽熱空気加熱器、 2A:耐熱材、 2B:熱吸収材、 2C:圧縮熱回収器、 2D:出力増大手段、 2E:出力増大球(液体鉛や液体錫や液体亜鉛等の液体金属・白金球や被覆白金球や金球や被覆金球や白金合金球や金合金球や鉛合金球や銀合金球や被覆白金合金球や被覆金合金球や被覆鉛球や被覆銀合金球やタングステン合金球や被覆タングステン合金球やタングステン鋼球や被覆タングステン鋼球やタンタル合金球や被覆タンタル合金球やモリブデン鋼球や被覆モリブデン鋼球やモリブデン鋳鉄球や被覆モリブデン鋳鉄球や銀球や被覆銀球等の金属球や被覆金属球) 2F:増大球上昇装置、 2G:衝撃低減手段(小径球・潤滑油類・不燃液体類・ゴム類・プラスチック類等の被覆) 2H:冷熱復水器、 2J:液体金属熱交換器、 2K:潤滑性材料、 2X:空気熱交換器、 2Y:水熱交換器、 2Z:水銀熱交換器、 3:摩擦損失低減手段(撥水作用や加熱高温手段や被覆等最適利用公知技術で摩擦損失を低減) 3A:撥水作用(水との摩擦損失低減手段) 3B:加熱高温手段(電気抵抗や電磁加熱等既存技術で高温にする) 3C:冷熱回収手段、 3E:衝撃低減材料(水銀・液体金属・水) 3G:撥水作用(水銀との摩擦損失低減手段) 4A:タービン翼断面(既存断面) 4B:タービン翼断面(出力面湾曲少断面) 4C:タービン翼断面(出力面直線断面) 4D:タービン翼断面(出力反対面直線断面) 4E:タービン翼断面(出力反対面湾曲少断面) 4F:タービン翼断面(既存の反対断面) 4X:タービン翼断面(4A〜4Fより選択断面) 5C:空気排気室、 6:ノズル、 6a:ノズル噴射部、 6b:ノズル噴射部、 6d:ノズル噴射部、 6z:水噴射ポンプ、 6A:過熱蒸気噴射ノズル、 6B:液体鉛噴射ポンプ、 6C:液体錫噴射ポンプ、 6D:液体ビスマス噴射ポンプ、 6E:液体亜鉛噴射ポンプ、 6F:圧縮空気噴射ノズル、 6H:液体カドミウム噴射ポンプ、 6I:液体インジウム噴射ポンプ、 6J:液体ガリウム噴射ポンプ、 6K:液体タリウム噴射ポンプ、 6L:液体金属噴射ポンプ、 6M:金属噴射ポンプ、 6X:燃料噴射ノズル、 6Y:燃焼ガス噴射ノズル、 6Z:水銀(液体金属)噴射ポンプ、 7:燃料噴射弁、 7A:回転翼7B:回転翼7B、 7C:スクリュー、 7E:回転腕翼、 8a:全動翼弾み車ガスタービン、 8b:全動翼弾み車水タービン、 8c:タービン翼、 8d:側板、 8e:円筒胴、 8E:全動翼弾み車水銀タービン、8F:全動翼弾み車重力タービン、 8G:竪型全動翼金属球重力太陽熱タービン、 8K:金属球水銀重力対向タービン、8K:対向直列全動翼弾み車タービン、 8L:直列全動翼弾み車タービン、 10:船体、 10A:船室、 10a:拡径圧縮室、10b:操縦室、 10c:制御室、 10d:客室、 10e:貨物室、 11A:隔壁、 11B:水室 11C:空気室、 11D:真空室、 16:クランク軸、16A:水平軸、 21:拡径ピストン、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:高温水制御弁、 25a:吸気弁、 25b:燃料制御弁、 28a:空気、 28a:内部空気、 28a:空気管空気、 28b:圧縮空気熱量、 28A:吸入空気路、 28B:空気路入口、 37a:着磁摩擦車、 37b:内着磁摩擦車、 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、 38A:重力飛行機、 38B:空気吸引噴射ウォータージェット船舶、 38C:水吸引噴射船舶、 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、 46:磁石部、 49:燃焼ガス、 49B:煙突燃焼ガス熱量、 49C:工場使用熱量、 50:過熱蒸気、 51:空気抽出器、 51:合流抽出器、 52a:水、 52b:水(太陽光で温度が変る水) 52b:高温水、 52d:温熱、 52d:水温熱、 52d:過熱蒸気温熱、 52e:冷熱、 52e:水冷熱、 52e:圧縮空気冷熱、 52e:アルコール冷熱、 52e:氷冷熱、 55:歯車式同期装置(磁気摩擦同期装置を含む) 55B:磁気摩擦変速装置(歯車式及び送水ポンプ兼用を含む) 55Y:歯車式変速装置(既存変速機から選択) 60A:内側軸装置、 60B:外側軸装置、 60C:内側動翼群、 60D:外側動翼群、 77B:筒形外箱、 77D:ウォータージェット外箱、 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、 78B:合体機関噴射部、 78K:合体機関噴射部、 78S:合体機関噴射部、 78T:合体機関噴射部、 78U:合体機関噴射部、 78V:合体機関噴射部、 78W:合体機関噴射部、 78X:合体機関噴射部(78S78T78U78Bがら選択) 79K:合体機関噴射部、 79M:ウォータージェット、 79S:ウォータージェット、 79T:ウォータージェット、 79U:ウォータージェット(水吸引噴射) 79V:ウォータージェット(79S79Tから選択) 79X:ウォータージェット(水吸引噴射) 79Y:ウォータージェット(空気吸引噴射) 79Z:ウォータージェット(空気吸引噴射) 80:軸受、 80a:推力軸受、 80A:継手、 80B:締付具、 81:支軸、 81a:支点、 84:二重反転磁気摩擦動力伝達装置(歯車式及び送水ポンプ兼用を含む) 84Y:二重反転歯車装置(既存技術) 94:固定外箱、 94A:外箱垂直部、 95:高温水溜、 95a:燃焼ガス溜、 95b:圧縮空気溜、 95c:過熱蒸気溜、 95A:吸水路、 95B:燃料溜、 96A:送水路、 97:逆止弁、103:冷熱回収器、 0: Vacuum, 1: Generator, 1A: Mercury Exhaust Inspection Room, 1B: Means of increasing oxygen level, 1C: Alcohol cold heat, 1D: Fuel injection pump, 1F: Condensate pump, 1G: Heat pump, 1H: Pumping pump, 1J: Water pumping apparatus, 1Y: Combustor, 1b: Fuel, 1c: Specific substance, 1d: Mercury, 1e: Coated steel ball (coated with impact reducing means 2G) 1e: Coated mercury (spherical stainless steel durable material or impact 1g: Gravity acceleration part, 1h: Horizontal axis, 2: Sunlight heater (tilt and rotate sunlight with long lens) 2a: Water condenser, 2a: Condenser cooler, 2b: Solar thermal augmentation suspension bridge (vertically suspended lifting gear left and right to tilt and track sunlight with multiple steps of long lens) 2c: heat insulating material, 2d: long lens, 2e: water surface, 2f: lifting tool left, 2g: hanging Ingredient right, 2h: seawater cooler, z: Solar air heater, 2A: heat resistant material, 2B: heat absorbing material, 2C: compression heat recovery device, 2D: power increase means, 2E: power increase sphere (liquid metal such as liquid lead, liquid tin or liquid zinc, etc. Platinum ball, coated platinum ball, gold ball, coated gold ball, platinum alloy ball, gold alloy ball, lead alloy ball, silver alloy ball, coated platinum alloy ball, coated gold alloy ball, coated lead ball, coated silver alloy ball, tungsten alloy Balls or coated tungsten alloy balls or tungsten steel balls or coated tungsten steel balls or tantalum alloy balls or coated tantalum alloy balls or molybdenum steel balls or coated molybdenum steel balls or molybdenum cast iron balls or coated molybdenum cast iron balls or silver balls or coated silver balls etc Metal spheres and coated metal spheres) 2F: Augmented sphere lifter, 2G: Impact reduction means (coating of small spheres, lubricating oils, incombustible liquids, rubbers, plastics, etc.) 2H: cold heat condenser, 2J: Liquid metal heat exchange Converter, 2K: Lubricant material, 2X: air heat exchanger, 2Y: water heat exchanger, 2Z: mercury heat exchanger, 3: friction loss reduction means (water repellent action, heating high temperature means, coating etc. optimum utilization known Technology to reduce friction loss 3A: Water repellent action (means to reduce friction loss with water) 3B: Heating high temperature means (high temperature with existing technology such as electric resistance and electromagnetic heating) 3C: Cold heat recovery means, 3E: Impact reduction Materials (mercury, liquid metal, water) 3G: Water repellant (means for reducing friction loss with mercury) 4A: Turbine blade cross section (existing cross section) 4B: Turbine blade cross section (small output surface curve cross section) 4C: Turbine blade cross section Output surface straight section) 4D: Turbine blade cross section (output opposite surface straight section) 4E: Turbine blade cross section (output opposite curved surface minor cross section) 4F: Turbine blade cross section (existing opposite section) 4X: Turbine blade cross section (4A to 4F More choice Cross section 5C: air exhaust chamber, 6: nozzle, 6a: nozzle injection part, 6b: nozzle injection part, 6d: nozzle injection part, 6z: water injection pump, 6A: superheated steam injection nozzle, 6B: liquid lead injection pump 6C: Liquid tin injection pump, 6D: Liquid bismuth injection pump, 6E: Liquid zinc injection pump, 6F: Compressed air injection nozzle, 6H: Liquid cadmium injection pump, 6I: Liquid indium injection pump, 6J: Liquid gallium injection pump, 6K: liquid thallium injection pump, 6L: liquid metal injection pump, 6M: metal injection pump, 6X: fuel injection nozzle, 6Y: combustion gas injection nozzle, 6Z: mercury (liquid metal) injection pump, 7: fuel injection valve, 7A : Rotor 7B: Rotor 7B, 7C: Screw, 7E: Rotor arm, 8a: All rotors -Bin, 8b: All moving wing water turbine, 8c: Turbine blade, 8d: Side plate, 8e: Cylindrical cylinder, 8E: All moving wheel bounced wheel mercury turbine, 8F: All moving wheel bounced wheel Gravity turbine, 8G: All wing Metal Ball Gravity Solar Thermal Turbine, 8 K: Metal Ball Mercury Gravity Countered Turbine, 8 K: Counter-Series All-Roller Impact-Brusher Turbine, 8 L: In-Series Total Rotor-Body Impactor Turbine, 10: Hull, 10A: Cabin, 10a: Expanded Compression Chamber, 10b : Flight control room, 10c: Control room, 10d: Guest room, 10e: Cargo room, 11A: Bulkhead, 11B: Water room 11C: Air room, 11D: Vacuum room, 16: Crankshaft, 16A: Horizontal axis, 21: Expansion diameter Piston, 24: combustion gas control valve, 24A: compressed air control valve, 25: overheated steam control valve, 25B: high temperature water control valve, 25a: intake valve, 25b: fuel control , 28a: air, 28a: internal air, 28a: air air, 28b: compressed air heat, 28A: intake air path, 28B: air path inlet, 37a: magnetized friction wheel, 37b: internally magnetized friction wheel, 38a A: flying body, 38b: flying wing, 38c: flying wing, 38d: vertical wing, 38e: wing leading edge, 38g: surface wing, 38h: floating surface, 38A: gravity plane, 38B: air suction jet water jet vessel, 38C: water suction jet vessel, 39A: solar thermal gravity plane, 39B: solar thermal gravity rotary plane, 39C: solar thermal gravity helicopter, 39D: screw ship, 39G: solar thermal gravity airship, 40A: rudder, 46: magnetic part, 49: burning Gas, 49B: chimney combustion gas heat quantity, 49C: factory use heat quantity, 50: superheated steam, 51: air extraction Unit, 51: combined extractor, 52a: water, 52b: water (water whose temperature changes due to sunlight) 52b: high temperature water, 52d: heat, 52d: water temperature heat, 52d: superheated steam heat, 52e: cold heat, 52e: Water-cooled heat, 52e: Compressed-air cold energy, 52e: Alcohol-cooled heat, 52e: Ice-cooled heat, 55: Gear-type synchronizer (including magnetic friction synchronizer) 55B: Magnetic friction transmission (including gear-type and water pump) 55Y Gear transmission (selected from existing transmissions) 60A: inner shaft device, 60B: outer shaft device, 60C: inner blade group, 60D: outer blade group, 77B: cylindrical outer box, 77D: water jet outside Box, 77F: Outer case of injection part, 77G: Cylindrical rotating part, 77a: Outer case of turbine, 78A: Combined engine injection part, 78B: Combined engine injection part, 78K: Combined Seki injection part, 78S: combined engine injection part, 78T: combined engine injection part, 78U: combined engine injection part, 78V: combined engine injection part, 78W: combined engine injection part, 78X: combined engine injection part (78S78T78U78B is selected) 79K: coalesced engine injection unit, 79M: water jet, 79S: water jet, 79T: water jet, 79U: water jet (water suction jet) 79V: water jet (selected from 79S 79T) 79X: water jet (water suction jet) 79Y : Water jet (Air suction jet) 79Z: Water jet (Air suction jet) 80: Bearing, 80a: Thrust bearing, 80A: Joint, 80B: Fastening tool, 81: Support shaft, 81a: Support point, 84: Double reversal Magnetic friction power transmission (gears And 84Y: Double reversing gear device (existing technology) 94: Fixed outer box, 94A: Outer box vertical part, 95: High temperature water reservoir, 95a: Combustion gas reservoir, 95b: Compressed air reservoir, 95c: Overheated steam reservoir, 95A: water absorption path, 95B: fuel reservoir, 96A: water supply channel, 97: check valve, 103: cold heat recovery device,
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JP2003126325A (en) * | 2001-10-24 | 2003-05-07 | Tasuke Nishi | Roller board for sliding |
JP2004254730A (en) * | 2003-02-24 | 2004-09-16 | Masashi Yamaguchi | Skateboard and skateboard truck mounting device |
JP2008521543A (en) * | 2004-12-03 | 2008-06-26 | タセム カンパニー リミテッド | Caster skate equipment |
JP2008545480A (en) * | 2006-04-28 | 2008-12-18 | レイザー ユーエスエイ,リミテッド ライアビリティ カンパニー | Flexible one-piece skateboard |
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Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
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JP2003126325A (en) * | 2001-10-24 | 2003-05-07 | Tasuke Nishi | Roller board for sliding |
JP2004254730A (en) * | 2003-02-24 | 2004-09-16 | Masashi Yamaguchi | Skateboard and skateboard truck mounting device |
JP2008521543A (en) * | 2004-12-03 | 2008-06-26 | タセム カンパニー リミテッド | Caster skate equipment |
JP2008545480A (en) * | 2006-04-28 | 2008-12-18 | レイザー ユーエスエイ,リミテッド ライアビリティ カンパニー | Flexible one-piece skateboard |
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