JP2017223212A - Engine and multi-purpose fan motor turbo - Google Patents

Engine and multi-purpose fan motor turbo Download PDF

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JP2017223212A
JP2017223212A JP2016146762A JP2016146762A JP2017223212A JP 2017223212 A JP2017223212 A JP 2017223212A JP 2016146762 A JP2016146762 A JP 2016146762A JP 2016146762 A JP2016146762 A JP 2016146762A JP 2017223212 A JP2017223212 A JP 2017223212A
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engine
turbine
fan motor
coolant
rotated
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早川　秀樹
Hideki Hayakawa
秀樹 早川
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    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
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    • Y02T10/12—Improving ICE efficiencies

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Abstract

PROBLEM TO BE SOLVED: To provide a high efficiency engine reducing a loss of engine as much as possible and producing its regeneration.SOLUTION: In this invention, a turbine or a rotating shaft is floated under activation of a powerful magnetic action or repelling action of the powerful magnet to decrease mechanical loss, the turbine is rotated under activation of exhaust gas, a fan placed inside of it is rotated to blow air to an intake port, an air feeding port or a coolant tank or a combustion chamber. A power generator is fixed to the turbine and the fan to cause the power generator to be rotated and to produce a regeneration energy. An engine is controlled by a computer and mixture gas is prevented from being entered into the combustion chamber unless an accelerator pedal is stepped on. An electric magnet is operated and a shutting plate cooperating with a valve is lowered and the mixture gas is put into the combustion chamber and then when the valve and the shutting plate are lifted up, a switch is turned on and a spark plug is applied to perform an ignition to cause useless state not to be produced. In addition, since the regeneration is also produced at the running with a motor, it can be expected to have a high effect. Further, it can also be expected that cooling effects against the engine and coolant is applied.SELECTED DRAWING: Figure 1

Description

本発明はエンジンと多目的ファンモーターに関する。The present invention relates to an engine and a multipurpose fan motor.

従来のエンジンは、一般的に出力３０％位排気損失３５％冷却損失２２％機械損失１０％と言われています。Conventional engines are generally said to have an output of around 30%, an exhaust loss of 35%, a cooling loss of 22%, and a mechanical loss of 10%.

特許公報第２５２４１３９号Patent Publication No. 2524139

特開２０１５−９４３５３JP2015-94353 A

排気損失３５％と冷却損失２２％と機械損失１０％できるだけ軽減して出力を上げて発電するエンジンEngine that generates electricity by reducing output as much as possible by reducing exhaust loss 35%, cooling loss 22% and mechanical loss 10%

本発明は、強力磁石の反発作用や強力磁力を活用してタービンと多目的ファンモーターと回転軸を浮かせて重力を軽減して、吸気口及びタービン内部に多目的ファンモーターで、送風して発電力を向上及び冷却効果を出し、クーラントにも冷却効果を出し発電機を回転させ発電をして自動車の場合は、エンジンを停止してバッテリー走行時にも回生発電を実施して低燃費を実現させる。The present invention utilizes the repulsive action and strong magnetic force of a strong magnet to float the turbine, the multi-purpose fan motor, and the rotating shaft to reduce gravity, and the multi-purpose fan motor in the intake and the turbine generates air to generate power. In the case of an automobile, which produces an improvement and cooling effect, and also produces a cooling effect on the coolant and rotates the generator to generate electricity, the engine is stopped and regenerative power generation is performed even during battery running to achieve low fuel consumption.

多目的ファンモーターによる出力アップと排気損失３５％と冷却損失２２％と機械損失１０％をできるだけ軽減して排気ガスで多目的ファンモーターと発電機を回転させ回生して発電をする。
自動車の場合は、モーター走行時も回生をしてできるだけ発電をする。
電力消費はコンピューター制御と点火プラグと吸気バルブと遮断板に使用する電磁弁がメインなだけです。
従来のエンジンより性能が高い見込みです。
多目的ファンモーターを回転させ回転率を上げるとターボ車としても使用できます。普通はエンジンの回転数が上がらないとターボ効果は悪いですが、ターボスィッチを入れるとモータプラス排気ガスでファンを回転させるので低回転から早くターボ効果が出る見込みです。
また、ターボスィッチを切ると燃費の悪化を防止します。Power output by multi-purpose fan motor, exhaust loss 35%, cooling loss 22% and mechanical loss 10% are reduced as much as possible, and the multi-purpose fan motor and generator are rotated and regenerated by exhaust gas to generate electricity.
In the case of an automobile, it generates electricity as much as possible by regenerating even when the motor is running.
The main power consumption is computer control, spark plugs, intake valves, and solenoid valves used for shut-off plates.
Expected to perform better than conventional engines.
It can be used as a turbo car by rotating the multi-purpose fan motor to increase the rotation rate. Normally, if the engine speed does not increase, the turbo effect is bad, but if the turbo switch is turned on, the fan is rotated with motor plus exhaust gas, so the turbo effect is expected to come out quickly from low rotation.
Turning off the turbo switch will prevent fuel consumption from deteriorating.

本発明の上から見た全体図の例Example of overall view from above of the present invention 本発明のカーバを取ったエンジンの部分図の例Example of partial view of engine with carver of the present invention 本発明の横から見たエンジン部分図（断面）Ａ−Ａ、Engine partial view (cross section) AA as seen from the side of the present invention, 本発明の横から見た多目的ファンモーターの部分図Partial view of a multi-purpose fan motor viewed from the side of the present invention 本発明の燃焼室付近の部分図Partial view of the vicinity of the combustion chamber of the present invention 本発明の逆から見た風車（横）Windmill viewed from the opposite side of the present invention (horizontal) 本発明の上から見たクーラント循環用風車Coolant circulation wind turbine viewed from above

本発明は、図１のように配置される。The present invention is arranged as shown in FIG.

混合気を電磁弁を使用して燃焼室に入れる。
その時に同時に遮断板が下がり漏れが発生しないようにする。
バルブと遮断板が上昇したらスィッチが入り点火プラグで点火する。
爆発燃焼エネルギーがタービンを回転させ発電機も回転する。
排気ガスは多目的ファンモーターを回転させ発電機も回転する。
ファンモーターの回転により送風効果でエンジンとクーラントを冷却する。
クーラント循環用風車も回転させクーラントを循環させる。
モーター走行時にも回生をして発電する。The air-fuel mixture is put into the combustion chamber using a solenoid valve.
At the same time, the shield plate is lowered so that no leakage occurs.
When the valve and the shut-off plate rise, the switch enters and ignites with the spark plug.
Explosive combustion energy rotates the turbine and the generator.
The exhaust gas rotates the multipurpose fan motor and the generator.
The engine and coolant are cooled by the ventilation effect by the rotation of the fan motor.
The coolant circulation wind turbine is also rotated to circulate the coolant.
Regenerative power is generated when the motor is running.

１．ミッション
２．風車式クーラント循環装置（ポンプ）
３．クーラントタンク
４．排水管
５．フィルター
６．通風口
７．発電機
８．発電機またはモーター
９．ファンの羽根
１０．ファンの羽根
１１．吸気口
１２．燃料機
１３．発電機兼用モーター
１４．燃焼室
１５．点火プラグ
１６．発電機兼用モーター
１７．タービン
１８．クーラント配管
１９．タービン羽根
２０．タービン主軸
２１．吸気バルブ
２２．排水コック
２３．タービン羽根
２４．多目的ファンモーター固定金具
２５．電磁石装置
２６．点火スィッチ
２７．遮断板
２８．点火プラグ
２９．風車
３０．風車下部循環用羽根
３１．歯車
３２．歯車
３３．強力磁石
３４．強力磁石
３５．強力磁石
３６．主軸
３７．多目的ファンモーターのタービン羽根
注意点 強力磁石を使用しないと問題が発生する場合があります。
発電機やモーターも強力磁石を使用する事
多目的ファンモーターは複雑な構造になっていて排気ガスが漏れないように固定金具があります。
大型の多目的ファンモーターの場合は固定金具を増やして排気ガスが漏れないようにする事
後、図面は一例としていますので、場合によって変更した方が便利です。
大型エンジンの場合はダブルタービンにする事も可能です。
エンジンの燃焼室付近はクーラント配管が図面上は記入がありませんが、理解しがたいため未記入にしました。
あらかじめご理解の方お願い申し上げます。1. Mission 2. Windmill type coolant circulation device (pump)
3. 3. Coolant tank Drain pipe 5. Filter 6. Ventilation opening7. Generator 8. 8. Generator or motor Fan blades10. 10. Fan blades Inlet 12. Fuel machine 13. Generator / motor 14. Combustion chamber 15. Spark plug 16. Generator / motor 17. Turbine 18. Coolant piping 19. Turbine blade 20. Turbine main shaft 21. Intake valve 22. Drain cock 23. Turbine blade 24. Multipurpose fan motor fixing bracket 25. Electromagnet device 26. Ignition switch 27. Shielding plate 28. Spark plug 29. Windmill 30. Windmill lower circulation blade 31. Gear 32. Gear 33. Strong magnet 34. Strong magnet 35. Strong magnet 36. Main shaft 37. Cautions for turbine blades for multi-purpose fan motors If strong magnets are not used, problems may occur.
Generators and motors also use strong magnets Multipurpose fan motors have a complicated structure and have mounting brackets to prevent exhaust gas from leaking.
In the case of a large multi-purpose fan motor, the number of fixing brackets is increased so that the exhaust gas does not leak, and the drawing is an example.
In the case of a large engine, a double turbine can be used.
The coolant piping is not shown on the drawing near the combustion chamber of the engine, but it is left blank because it is difficult to understand.
Thank you in advance for your understanding.

本発明はエンジンと多目的ファンモーターターボに関する。The present invention relates to an engine and a multipurpose fan motor turbo.

ジェットエンジンはテコ作用が小さく騒音も大きい。
バードストライクの問題もあるし、ジェット噴射式なので自動車に使用できない。
ピストン式エンジンもテコ作用は小さく、ロータリーエンジンは高温が発生する為に大型エンジンが実用化できない問題や不完全燃焼が発生する問題があった。Jet engines have little leverage and loud noise.
There is a problem of bird strike, and it cannot be used for cars because it is a jet injection type.
The piston type engine also has a small lever action, and the rotary engine has a problem that a large engine cannot be put into practical use due to high temperature, and incomplete combustion occurs.

特許公報第２５２４１３９号Patent Publication No. 2524139

特開２０１５−９４３５３JP2015-94353 A

従来のエンジンより不完全燃焼を防止してテコ作用をできるだけ出す高性能エンジンと高性能ファンモーターターボです。A high-performance engine and a high-performance fan motor turbo that prevent incomplete combustion and produce the maximum possible leverage compared to conventional engines.

本発明はエンジンに不完全燃焼防止装置を取り付け不完全燃焼を防止して、エンジンに通風口を設けタービンの回転によりエンジンの内部を送風冷却する。
また磁石の反発作用を活用してタービンと軸及び歯車を浮上させる。
調整によりアクセルを踏まないと燃焼室に混合気が入らないようにして燃費の悪化を防止する。
それに多目的ファンモーターターボを使用してエンジン全体及びエンジン内部とクーラントを送風冷却して発電機を回転させる。
排気ガスの効果が悪い場合は、モーターも同時に使用してターボ効果を強化する。
また、多目的ファンモーターターボの送風を利用して風車を回転させクーラントを循環させる。According to the present invention, an incomplete combustion prevention device is attached to an engine to prevent incomplete combustion, an air vent is provided in the engine, and the inside of the engine is blown and cooled by rotation of a turbine.
In addition, the repulsive action of the magnet is used to float the turbine, shaft and gears.
The adjustment prevents the gas mixture from entering the combustion chamber unless the accelerator is stepped on, thereby preventing fuel consumption from deteriorating.
In addition, a multi-purpose fan motor turbo is used to blow and cool the entire engine and the interior of the engine and the coolant to rotate the generator.
If the effect of exhaust gas is poor, use the motor at the same time to enhance the turbo effect.
In addition, the wind turbine is rotated using the air of the multipurpose fan motor turbo to circulate the coolant.

一般的に排気損失３５％冷却損失２２％機械損失１０％と言われていますが、それをできるだけ軽減して、テコ作用をエンジンの構造を活用してできるだけ出し、ロータリーエンジンでは製造実用化できなかった大型エンジンを実用可能にして不完全燃焼を防止して大型エンジンではテコ作用だけでも理論計算上約２０倍の効果を出す。
計算例として、従来のディゼルエンジン２００００ＣＣ８気筒の場合はシリンダー直径１４．２３５２４ｃｍ半径７．１１７６２ｃｍピストンの上下運動３１．４１５９２６５４ｃｍクランクシャフトの円運動３１．４１５９２６５４ｃｍクランクシャフトの円運動の直径は１０ｃｍでテコ作用はクランクシャフトの円運動の半径になるので５ｃｍになります。
私の発明したエンジンの場合は例えば内径直径２ｍ羽根の長さ３ｃｍ羽根の高さ１．５ｃｍのタービンを使用すると（１０３×１０３×π×１．５）−（１００×１００×π×１．５）＝２８６９．８４４８９となり燃焼室の体積をプラスしても２９００ＣＣ位の排気量で騒音も従来より小さい見込みです。
テコ作用は、タービンの内径半径に羽根の長さの約半分をプラスした数値で計算すると１０１．５ｃｍになり従来のエンジンと比較すると２０．３倍です。
燃焼室に入れる混合気の量を従来の２０分の１にすると約２０倍はテコ作用だけで燃費が向上する計算になります。
他には私の発明したエンジンは吸気バルブ１本ですが、８気筒は普通３２バルブ（排気１６バルブ）で排気バルブを押し上げパワーを消費するのと吸気バルブが多い分パワーを消費します。
私の発明したエンジンの場合は吸気バルブ１本と不完全燃焼防止装置に電力は消費しますが、タービンの上に発電機があり発電するので実質は冷却損失がゼロとエアコン●ラジエーター、パワステ、点火プラグ、ライト、カーナビ、不完全燃焼防止装置、燃料機、制動灯に使用する電力より発電する予定です。
また、私の発明したエンジンの場合タービンの回転により空気を取り入れ冷却するのとテコ作用が約２０倍あるので発生する熱量は２０分の１位を冷却するので消費電力は大幅に軽減する見込みです。
それに関して、クーラント使用量も大幅に削減できる見込みです。
燃料タンクも従来２００ｌを１０ｌ位にできる見込みです。
磁石の反発作用でタービンと軸と歯車を浮かせるので推定機械損失は８％位向上が見込めます。
排気損失は従来３５％と言われていますが私の発明したエンジンの場合は、爆発燃焼圧力と排気ガスが、タービンを約半回転して遠心力排気をするので大幅に向上が見込まれます。
エンジンに空気を取り込む事によりタービンに加わる圧力は従来のエンジンより高くなり、不完全燃焼防止装置の効果もあるので燃費はその分、向上する見込みです。
私の発明したエンジンはコスト的には従来のエンジンと同じ位と思っています。
一般的にタービンロスは排気タービンの場合４５％と言われています。
それを私の発明したエンジンに仮定すると５５％になり機械損失が８％向上すると６３％位で一般的エンジン出力３０％の約２倍となりテコ作用が２０倍なので合計は約４０倍従来のエンジンより燃費が向上する見込みです。
多目的ファンモーターターボはエンジンの回転数が低い場合は、モーターも同時に使用して高いターボ効果が期待できます。
従来のターボより送風、発電、モーター効果があり性能は上です。
それに耐熱構造になっています。
しかし、発明したエンジンにパワーがあるので自動車には、多目的ファンモーターターボは使用しない方がいいと思います。It is generally said that the exhaust loss is 35%, the cooling loss is 22%, the mechanical loss is 10%, but this is reduced as much as possible, and the lever action is made as much as possible by utilizing the structure of the engine. The large-sized engine can be put into practical use to prevent incomplete combustion, and in the large-sized engine, the lever action alone is about 20 times as effective in theoretical calculation.
As an example of calculation, in the case of a conventional diesel engine 20000 CC8 cylinder, cylinder diameter 14.23524 cm radius 7.11172 cm piston vertical motion 31.41592654 cm crankshaft circular motion 31.41592654 cm crankshaft circular motion diameter is 10 cm and lever action is It becomes 5cm because it is the radius of the circular motion of the crankshaft.
In the case of the engine invented by the present invention, for example, when a turbine having an inner diameter of 2 m and a length of 3 cm and a height of 1.5 cm is used, (103 × 103 × π × 1.5) − (100 × 100 × π × 1. 5) = 2869.84489, and even if the volume of the combustion chamber is increased, the displacement is about 2900 CC and the noise is expected to be smaller than before.
The lever action is 101.5 cm when calculated by adding approximately half of the blade length to the inner radius of the turbine, which is 20.3 times that of the conventional engine.
If the amount of air-fuel mixture to be put into the combustion chamber is 1/20 of the conventional value, the calculation will improve fuel efficiency by levering only about 20 times.
The other engine I invented is one intake valve, but the 8-cylinder usually consumes power by pushing up the exhaust valve with 32 valves (16 exhaust valves) and more intake valves.
In the case of the engine that I invented, power is consumed by one intake valve and the incomplete combustion prevention device, but since there is a generator on the turbine and power is generated, there is virtually no cooling loss and air conditioning ● Radiator, power steering, Electricity will be generated from electricity used for spark plugs, lights, car navigation systems, incomplete combustion prevention devices, fuel machines, and brake lights.
Also, in the case of the engine invented by me, the cooling effect is about 20 times that of cooling by taking in air by rotating the turbine, so the amount of heat generated is expected to be reduced by about 20th, so the power consumption is expected to be greatly reduced. .
In connection with this, the amount of coolant used is expected to be significantly reduced.
The fuel tank is expected to be 200 liters up to 10 liters.
The estimated mechanical loss can be improved by about 8% because the turbine, shaft, and gears are lifted by the repulsive action of the magnet.
Exhaust loss is said to be 35% in the past, but in the case of the engine that I invented, the explosion combustion pressure and exhaust gas are expected to be greatly improved because the turbine is exhausted by centrifugal force about half a turn.
By taking air into the engine, the pressure applied to the turbine is higher than that of the conventional engine, and the effect of the incomplete combustion prevention device is also expected, so the fuel consumption is expected to improve accordingly.
I think that the engine I invented is about the same as a conventional engine in terms of cost.
Generally, turbine loss is said to be 45% for exhaust turbines.
Assuming that the engine that I invented is 55% and the mechanical loss is improved by 8%, it is about 63%, about twice the general engine output 30% and the lever action is 20 times, so the total is about 40 times the conventional engine Expected to improve fuel efficiency.
When the engine speed is low, the multipurpose fan motor turbo can be used at the same time as the motor to achieve a high turbo effect.
Better performance than the conventional turbo, with air blowing, power generation, and motor effects.
It has a heat resistant structure.
However, because the invented engine has power, it is better not to use a multi-purpose fan motor turbo in the car.

本発明を上から見た全体図の例Example of overall view of the present invention viewed from above 本発明からカバーを取ったエンジンの部分図の例Example of partial view of engine with cover from the present invention 本発明を横から見たエンジン部分図（断面）Ａ−Ａ．Engine partial view (cross section) AA. 本発明を横から見た多目的ファンモーターターボの部分図Partial view of the multipurpose fan motor turbo as seen from the side of the present invention 本発明の燃焼室付近の部分図Partial view of the vicinity of the combustion chamber of the present invention 本発明を逆から見た風車（横）Windmill (side) of the present invention viewed from the reverse 本発明を上から見たクーラント循環用風車Coolant circulation wind turbine viewed from above

発明を実施するための形能Form for carrying out the invention

本発明は、例として図１のように配置される。The present invention is arranged as shown in FIG. 1 as an example.

混合気を電磁弁を使用して燃焼室に入れる。
その時同時に遮断板が下がり混合気が漏れが発生しないようにする。
吸気バルブと遮断板が上昇したらスィッチが入り点火プラグで点火する。
爆発燃焼エネルギーがタービンを回転させ連動で発電機も回転する。
排気ガスは多目的ファンモーターターボを回転させターボ効果及び発電機を回転させ、エンジン全体とエンジン内部送風とクーラント冷却及びクーラント循環用風車を回転させクーラントを循環させる。
ハイブリッドの場合はモーター走行時にも回生をして発電する。
例として、エンジンを軽自動車に使用した場合は、多目的ファンモーターターボはエンジン性能が高い為に使用しない見込みです。
エンジンの内部直径１１０ｃｍ・タービンの内径１０７ｃｍ・羽根の長さ１．５ｃｍ・高さ１．５ｃｍです。
従来の軽自動車のテコ作用は１．９２８２５７８２ｃｍ位で私の発明したエンジンはタービンの半径５３．５ｃｍに羽根の長さ１．５ｃｍ÷２を合計した５４．２５ｃｍがテコ作用になります。
ピストン式エンジンの２８．１３４２０４５８倍になりますので混合気は、従来の約２５分の１位にした方がいいと思います。（最大に混合気を入れた場合）アクセルを踏まないと混合気が燃焼室に入らないように調整する事。
パワステは別に電動モーターを使用してください。（エンジンを停止する場合がある為です。）
タービンの上に発電機があるので性能がいい発電機を使用すればバッテリーがなくなる事はない見込みです。
ファンモーターターボを使用しない場合は、ファンモーターを取り付けてください。
風力でクーラントが循環するようにしてください。
サーモスタットは必要ありません。（クーラント循環用）
燃費がいいので燃料タンクは５ｌ位でいいと思います。
点火プラグは１本だけで排気は排気バルブはなく遠心力排気システムです。
エンジンの組立は磁石の反発作用でタービンを浮かせた後にエンジンの外カバーを取り付けてその後発電機を取り付けてください。
磁石はサビに強い磁石を使用した方がよく、磁石付近は水分が高くならないようにカバーを取り付けてください。
単純計算では約４０倍燃費がいいため発生する熱量も少量になりますのでクーラント使用量は２ｌ位でいいと思います。
エンジンの燃焼室は図面に書いていませんがクーラントを循環するようにしてください。
また、エンジンの固定が悪いと思う場合は、軸受けを取り付けてください。
タービンの上下には図面には書いていませんが、５ｍｍ位の板を取り付けて爆発圧力が逃げないようにしてください。
多目的ファンモーターターボは複雑な構造になっていて排気ガスが漏れないように固定金具があります。（設置には注意して問題がないようにしてください。）後、図面は一例としていますので場合によって変更した方が便利です。
超大型エンジンの場合はダブルタービンにする事も可能です。The air-fuel mixture is put into the combustion chamber using a solenoid valve.
At the same time, the barrier plate is lowered so that the air-fuel mixture does not leak.
When the intake valve and shut-off plate rise, the switch enters and ignites with the spark plug.
Explosive combustion energy rotates the turbine and interlocks with the generator.
The exhaust gas rotates the multi-purpose fan motor turbo, rotates the turbo effect and the generator, and rotates the entire engine, the engine internal air blow, the coolant cooling and coolant circulation wind turbine, and circulates the coolant.
In the case of a hybrid, power is generated by regeneration even when the motor is running.
As an example, when the engine is used in a light vehicle, the multi-purpose fan motor turbo is not expected to be used due to its high engine performance.
The engine has an internal diameter of 110 cm, a turbine internal diameter of 107 cm, a blade length of 1.5 cm, and a height of 1.5 cm.
The lever action of a conventional light vehicle is about 1.92582578cm, and the engine that I invented has a lever radius of 54.25cm, which is a total of the radius of the turbine 53.5cm and the blade length 1.5cm / 2.
Since it is 28.13420458 times that of a piston type engine, I think that the air-fuel mixture should be about 1 / 25th of the conventional one. (When the air-fuel mixture is maximum) Adjust so that the air-fuel mixture does not enter the combustion chamber unless the accelerator is stepped on.
Use an electric motor separately for power steering. (Because the engine may be stopped.)
Since there is a generator on the turbine, it is expected that the battery will not run out if a generator with good performance is used.
When not using the fan motor turbo, install the fan motor.
Make sure the coolant circulates with wind power.
A thermostat is not required. (For coolant circulation)
I think the fuel tank should be about 5 liters because the fuel consumption is good.
There is only one spark plug and exhaust is a centrifugal exhaust system without an exhaust valve.
When assembling the engine, lift the turbine by the repulsive action of the magnet, attach the outer cover of the engine, and then install the generator.
It is better to use a magnet resistant to rust, and attach a cover so that moisture does not become high near the magnet.
In simple calculation, the amount of heat generated is small because the fuel consumption is about 40 times better, so the amount of coolant used should be about 2 liters.
The engine combustion chamber is not shown in the drawing, but please circulate the coolant.
If you think that the engine is not fixed properly, install a bearing.
Although there are no drawings on the top and bottom of the turbine, install a 5mm plate to prevent the explosion pressure from escaping.
The multi-purpose fan motor turbo has a complicated structure and has fixing brackets to prevent the exhaust gas from leaking. (Please be careful about the installation so that there is no problem.) After that, the drawing is an example, so it is more convenient to change it depending on the case.
In the case of a super-large engine, a double turbine can be used.

１、ミッション
２、風車式クーラント循環装置（ポンプ）
３、クーラントタンク
４、排水管
５、フィルター
６、通風口
７、発電機
８、発電機またはモーター
９、ファンの羽根
１０、ファンの羽根
１１、吸気口
１２、燃料機
１３、発電機兼用モーター
１４、燃焼室
１５、点火プラグ
１６、発電機兼用モーター
１７、タービン
１８、クーラント配管
１９、タービン羽根
２０、タービン主軸
２１、吸気バルブ
２２、排水コック
２３、タービン羽根
２４、多目的ファンモーターターボ固定金具
２５、電磁石装置
２６、点火スィッチ
２７、遮断板
２８、点火プラグ
２９、風車
３０、風車下部循環用羽根
３１、歯車
３２、歯車
３３、強力磁石
３４、強力磁石
３５、強力磁石
３６、主軸
３７、多目的ファンモーターターボのタービンの羽根1, mission 2, windmill coolant circulation system (pump)
3, coolant tank 4, drain pipe 5, filter 6, vent 7, generator 8, generator or motor 9, fan blade 10, fan blade 11, air inlet 12, fuel machine 13, generator / motor 14 , Combustion chamber 15, spark plug 16, generator / motor 17, turbine 18, coolant pipe 19, turbine blade 20, turbine main shaft 21, intake valve 22, drain cock 23, turbine blade 24, multipurpose fan motor turbo fixing bracket 25, Electromagnet device 26, ignition switch 27, shield plate 28, spark plug 29, windmill 30, windmill lower circulation blade 31, gear 32, gear 33, strong magnet 34, strong magnet 35, strong magnet 36, main shaft 37, multipurpose fan motor Turbo turbine blades

Claims (3)

回転軸を磁気浮上させたファンモーターを排気ガスと場合によってモーターで回転させクーラントの冷却とエンジンの冷却と吸気口と通風口に送風して発電する多目的ファンモーターA multi-purpose fan motor that generates electricity by rotating a fan motor with a rotating shaft magnetically levitated into the exhaust gas and, depending on the case, the motor, cooling the coolant, cooling the engine, and blowing air to the intake and vents 磁石の反発作用を活用して磁気浮上させたタービンを爆発燃焼エネルギーで回転させて、動力を発生させ発電機で発電をして、タービンの回転力でエンジン内部に送風冷却するエンジンでモーター走行も可能なエンジンThe turbine that has been magnetically levitated by utilizing the repulsive action of the magnet is rotated with explosion combustion energy, power is generated, and power is generated by the generator. Possible engine 磁石の反発作用を活用して磁気浮上させたタービンを爆発燃焼エネルギーで回転させ動力を発生させ発電機で発電して、排気ガスとモーターで多目的ファンモーターを回転させ発電とエンジン内部に送風とクーラント冷却循環と吸気口に強力な送風をする多目的ファンモータータービンエンジンで場合によってモータースィッチを切り燃費の悪化を防止するエンジンA turbine that has been magnetically levitated by utilizing the repulsive action of magnets is rotated by explosion combustion energy to generate power, and power is generated by a generator. A multi-purpose fan motor is rotated by exhaust gas and motors to generate power and coolant inside the engine. An engine that prevents the deterioration of fuel consumption by turning off the motor switch in some cases with a multi-purpose fan motor turbine engine that cools and circulates power to the air intake.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2023177190A (en) * 2022-06-01 2023-12-13 秀樹 早川 engine

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55121922U (en) * 1979-02-22 1980-08-29
JPS5738645A (en) * 1980-07-02 1982-03-03 Gen Electric Propulsion reinforcing turbo fan engine
JPS6193258A (en) * 1984-10-09 1986-05-12 ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン Gas turbine engine for airplane and its operation
JPS61294131A (en) * 1985-06-20 1986-12-24 Sanden Corp Twin turboengine
JPS6251729A (en) * 1985-08-30 1987-03-06 Isuzu Motors Ltd Turbocharger control device for internal combustion engine
JPS63130630U (en) * 1987-02-20 1988-08-26
JPH01500605A (en) * 1986-08-21 1989-03-01 ワン，リン・シュー Internal combustion engine and its operating method
JPH01104913A (en) * 1987-10-16 1989-04-21 Isuzu Motors Ltd Cooling system for thermally insulated engine
JPH0650176A (en) * 1992-03-23 1994-02-22 General Electric Co <Ge> Cooling device for gas turbine engine
JP2003174742A (en) * 2001-12-06 2003-06-20 Ishikawajima Harima Heavy Ind Co Ltd Rotary machine and assembling method thereof
JP2008144752A (en) * 2006-10-19 2008-06-26 General Electric Co <Ge> Gas turbine engine heat exchanger and gas turbine engine
JP2008304052A (en) * 2007-03-08 2008-12-18 General Electric Co <Ge> Vacuum stator assembly and its manufacturing process
JP2009516793A (en) * 2005-11-09 2009-04-23 プラット アンド ホイットニー カナダ コーポレイション Aircraft taxing method and apparatus
JP2014501871A (en) * 2010-11-22 2014-01-23 ゼネラル・エレクトリック・カンパニイ Integrated variable shape flow restrictor and heat exchanger

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55121922U (en) * 1979-02-22 1980-08-29
JPS5738645A (en) * 1980-07-02 1982-03-03 Gen Electric Propulsion reinforcing turbo fan engine
JPS6193258A (en) * 1984-10-09 1986-05-12 ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン Gas turbine engine for airplane and its operation
JPS61294131A (en) * 1985-06-20 1986-12-24 Sanden Corp Twin turboengine
JPS6251729A (en) * 1985-08-30 1987-03-06 Isuzu Motors Ltd Turbocharger control device for internal combustion engine
JPH01500605A (en) * 1986-08-21 1989-03-01 ワン，リン・シュー Internal combustion engine and its operating method
JPS63130630U (en) * 1987-02-20 1988-08-26
JPH01104913A (en) * 1987-10-16 1989-04-21 Isuzu Motors Ltd Cooling system for thermally insulated engine
JPH0650176A (en) * 1992-03-23 1994-02-22 General Electric Co <Ge> Cooling device for gas turbine engine
JP2003174742A (en) * 2001-12-06 2003-06-20 Ishikawajima Harima Heavy Ind Co Ltd Rotary machine and assembling method thereof
JP2009516793A (en) * 2005-11-09 2009-04-23 プラット アンド ホイットニー カナダ コーポレイション Aircraft taxing method and apparatus
JP2008144752A (en) * 2006-10-19 2008-06-26 General Electric Co <Ge> Gas turbine engine heat exchanger and gas turbine engine
JP2008304052A (en) * 2007-03-08 2008-12-18 General Electric Co <Ge> Vacuum stator assembly and its manufacturing process
JP2014501871A (en) * 2010-11-22 2014-01-23 ゼネラル・エレクトリック・カンパニイ Integrated variable shape flow restrictor and heat exchanger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2023177190A (en) * 2022-06-01 2023-12-13 秀樹 早川 engine

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