WO2020217304A1 - Sclosed circulation vertical rising system - Google Patents
Sclosed circulation vertical rising system Download PDFInfo
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- WO2020217304A1 WO2020217304A1 PCT/JP2019/017189 JP2019017189W WO2020217304A1 WO 2020217304 A1 WO2020217304 A1 WO 2020217304A1 JP 2019017189 W JP2019017189 W JP 2019017189W WO 2020217304 A1 WO2020217304 A1 WO 2020217304A1
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- lift
- vertical
- circulation
- air
- circulation path
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Definitions
- a substance such as air is circulated in a closed circulation path by a fan or the like, and the fluid substance is applied to a lift body provided in the middle to generate lift.
- Efficient use of mass transfer energy saves energy, and the circulation type makes it possible to create airtightness, which makes it possible to generate lift even in a vacuum state. Therefore, the lift generated by this system allows vertical ascent, and vertical ascent, vertical descent, and dwelling to the sky, which is a dilute air layer, or to outer space, which is a vacuum.
- it is a lift system that does not rely on the injection of a jet engine, and it uses less energy due to its circulation type, and because it does not rely on explosive energy, it can create a simple and lightweight aircraft.
- the present invention is lift by an air flow or the like that circulates in an internally sealed circulation cylinder or the like. An air flow is generated from a power unit such as a propeller installed inside the sealed and circulated at high speed in the closed circulation path, and a plurality of sheets are installed in the internal circulation path.
- Mechanism / shape Select the optimum wing shape according to the properties and speed of the fluid material used.
- the circulation path has a flat or gently uneven surface on the upper surface to reduce the resistance of the fluid and maintain a smooth air flow and a relatively low air pressure.
- the lower surface maintains a relatively high air pressure while causing turbulent swirls due to the lift body, vortex, bellows and unevenness on the half surface of the wing.
- the turbulent flow generated on the lower side of the circulation path is a high-pressure spiral, which draws in the outer peripheral part like a low pressure system in a weather map, so that it attracts the lower surface of the circulation path. Then, the low pressure is flowed upward by the following fluid while attracting the lower surface.
- the vortex is gradually decomposed and joins the air flow on the upper surface of the circulation path or collides with the lower surface of the blade of the path, so that a large lift is generated as a whole. Further, since the airflow and the like circulated by the blade having a large angle of attack adopted above are collected on the lower side, the fluid is strongly passed under the circulation path, and the airflow hits the lift body to generate lift. It produces a strong circulatory lift, which becomes a large lift along with the lift generated on the wing.
- Shape Cylindrical circulation cylinders are arranged in parallel, with a combination of both horizontal and vertical arrangements of triangular circulation paths, and a combination of both horizontal and vertical arrangements of square circulation paths, horizontal and vertical.
- a combination of polygonal circulation paths such as pentagons, both horizontal and vertical arrangements, and a circular circulation path such as a floating ring and its combination, both horizontal and vertical arrangements.
- Left and right double propellers Floating ring type Propeller power units are attached to the left and right of the circulation path to lift. Ascending power. It becomes higher at the part where the air pressure is applied.
- the air circulation for intake of the power unit moves air above the outside or inside. There is an increase in lift due to the repulsive pressure between energy units, and a propulsive force is generated due to the pressure difference between the upper and lower surfaces.
- Power unit The power unit circulates the airflow as power, and the propeller itself generates lift, so that lift is used.
- the propeller In order to increase the lift in the vertical ascending direction, the propeller with the air blowing direction facing downward, also downward. It also includes a circulation type in which the jet turbine blades generate lift upward in the facing jet injection type.
- Barrel-type helicopter type The wings of a multi-layered helicopter generate lift, but the circulation type improves energy efficiency and enables multi-pole use due to airtightness.
- a helicopter wing is installed in the inner barrel inside the double barrel to generate lift, and the airflow generated at that time is circulated upward in the outer barrel to recirculate it. It also includes internal and external reverse circulation.
- Helicopter wings include those with multiple layers to increase lift and those with a rectifying louver between the helicopter wings.
- the barrel type also includes those with an inner barrel that can be opened and closed. In the area with air, the helicopter fan of the energy unit in the inner barrel raises vertically, and when the air becomes thin, close the inner barrel and switch to the circulation type to efficiently raise vertically.
- the substance to be circulated is usually air, but it also includes substances that have been compressed to increase the density in order to increase the lift generated, and circulation by gases other than air, water, and other substances.
- the lower surface of the circulation path has a waveform that generates turbulence, and the upper surface has a flat or gentle waveform to prevent large turbulence and accelerate the flow velocity.
- the blades are not in the circulation path, and a large number of waveforms that generate turbulent flow on the lower surface of the circulation path and a circulation path having a flat surface on the upper surface are laminated to circulate wind and water.
- a rectifying louver or the like rectifies the flow of air or the like in order to efficiently generate lift by circulating air or the like, and the louver also has a curve that generates lift. Or, there are no wings, and the continuous installation of the lift louver, the continuous installation of the lift louver, and the one with only the corrugated circulation path are included.
- Power unit, airflow generation power includes multiple or repositioned ones Although it is mainly for vertical ascent, it can also be used for propulsion in all directions.
- the present invention also includes a combined type equipped with an externally installed wing, an externally installed propeller, and a jet such as an ordinary airplane.
- the lift for levitation is lifted by this system, and if the propulsion to proceed is performed by a jet or propeller, the wings need to be small, so the propulsion resistance is reduced, and the moving energy of air generated by the jet or propeller is reduced.
- the air is once passed through the internal circulation engine to generate lift, and then the external jet is injected, released and propelled.
- the wing and lift body are blown to generate lift in the spiral through the circulation path, and then the jet is injected downward.
- the jet engine turbine is interlocked with the circulation type propeller to circulate the air in the circulation path, and the ascending force is increased by the circulation type lift.
- Various shapes can be used for the wings to be installed.
- the pick-up angle is changed depending on the speed of the fluid, but since the system functions effectively even at an angle where the angle is large and turbulence occurs and the system peels off or stalls, the present invention also adopts an extremely large pick-up angle. And.
- the specific angle cannot be increased because it depends on the shape of the wing, the medium of the fluid, and the flow velocity, but the angle of the wing is usually such that the airplane will peel off or stall. Due to this large lift angle, a large lift can be obtained even if the fluid velocity is low.
- a suction port is attached to the front of the wing shape to lower the air pressure on the upper surface of the wing
- a perforated horizontal plate is attached to the lower surface to increase resistance and increase the air pressure to increase the lift of the wing itself.
- the strong flow that blows onto the lower surface of the circulation path hits the angular wave surface on the lower surface, creating turbulence and attracting the lower surface upward.
- the wind hits the lower side of the next wing again and the lift lift of 1 becomes stronger, and the fluid also flows strongly on the lift body wave surface of the lower surface of 3. It becomes a virtuous cycle that the lift generation becomes stronger.
- Lift on the underside of the circulation path Lift is generated when the wave surface is hit by wind or the like.
- the mechanism is as follows. The wind bent on the curved surface is stretched according to the length of the surface. Then, the air pressure becomes low and lift is generated.
- the present invention also relates to a soft outer shell that can be folded and carried and inflated when necessary.
Abstract
In a system which uses jets to rise vertically, or a system which travels forward and hovers by means of air striking wings or a propeller and generating lift, as in a standard airplane or a helicopter, energy in the generated airflow is lost to the air in conjunction with forward travel, and therefore such systems suffer a large amount of energy loss. Moreover, rockets and jet engines mainly use explosion energy and therefore are heavy in order to be durable. The present invention uses a fan, etc., to circulate a substance such as air in a closed circulation path, and generates lift by providing a lift body therein which is struck by said flowing substance.
Description
当発明はファンなどにより空気などの物質を密閉循環路に循環させ、途中に設けた揚力体にその流動物質を当てて揚力を発生させるものである。
物質移動エネルギーを効率的に使い、エネルギー節約をするとともに、循環式という特徴により密閉性も作ることが可能になるため、真空状態でも揚力を発生させることが可能となる。よって当システムの発生揚力により垂直上昇ができ、さらに希薄な空気層である上空または真空である宇宙空間まで垂直上昇、垂直下降、滞空することができる。
またジェットエンジンの噴射に頼らない揚力システムであり、その仕組みである循環形式により使用エネルギーが少なく、また爆発エネルギーに頼らないので構造が簡易かつ軽量な飛行体ができる。
具体的なイメージとしてはUFOのような宇宙まで垂直上昇飛行ができる飛行体であり、宇宙船、宇宙進行飛行機などや、ロープに頼らない宇宙エレーベーターなどを実現することができる。またスクリュー、ジェット、タイヤなどによる外界との接触摩擦がなく推進できるので音が外に漏れない静音タイプの宇宙船、飛行機、ヘリコプター、船、潜水艦、地上車、列車などの推進エンジンとして利用ができる。
また機密式でジェト噴射やフロペラによる風が外部に影響しないので、噴煙の撒き散らしや、砂、チリの巻揚などがなくなる。
従来よりジェットによる垂直上昇、また通常の飛行機やヘリコプターのように外気を翼やプロペラにあてて揚力を発生させ進行、浮揚するシステムはあった、しかし通常一般的にあるロケット、ジェット機、プロペラ機、ヘリコプター共に発生した気流のエネルギーは進行とともに空に捨てていくので大きなエネルギーロスがあるのである。またロケットやジェットエンジンは爆発エネルギーをメインとするので耐久性を持たせるために重いものとなる。
当発明は内部密閉した循環筒等に循環させる気流等による揚力であり、密閉した内部に設置したプロペラなどのパワーユニットから気流を発生させて密閉循環路に高速循環させ、内部循環路に複数枚設置した翼や揚力体に気流を当てることにより発生した揚力で上昇し、また気流のエネルギーを無駄なくローテーションさせてさらに再循環させるので、摩擦抵抗で損失するエネルギー以外の気流エネルギー損失を無くなるのである。
また上記のように循環による外気不要のシステムであるので気体が希薄または真空である上空、宇宙空間での揚力発生を可能とする。
In the present invention, a substance such as air is circulated in a closed circulation path by a fan or the like, and the fluid substance is applied to a lift body provided in the middle to generate lift.
Efficient use of mass transfer energy saves energy, and the circulation type makes it possible to create airtightness, which makes it possible to generate lift even in a vacuum state. Therefore, the lift generated by this system allows vertical ascent, and vertical ascent, vertical descent, and dwelling to the sky, which is a dilute air layer, or to outer space, which is a vacuum.
In addition, it is a lift system that does not rely on the injection of a jet engine, and it uses less energy due to its circulation type, and because it does not rely on explosive energy, it can create a simple and lightweight aircraft.
As a concrete image, it is an air vehicle that can fly vertically up to space like a UFO, and it can realize spacecraft, space traveling airplanes, space elevators that do not rely on ropes, and so on. In addition, since it can be propelled without contact friction with the outside world due to screws, jets, tires, etc., it can be used as a propulsion engine for silent type spacecraft, airplanes, helicopters, ships, submarines, ground vehicles, trains, etc. ..
In addition, since it is a confidential type and the wind from jet injection and flopera does not affect the outside, there is no need to scatter the plume or wind up sand or dust.
Traditionally, there have been systems for vertical ascent by jets, and for moving and floating by applying outside air to wings and propellers to generate lift like ordinary airplanes and helicopters, but usually rockets, jets, propellers, Since the energy of the airflow generated by the helicopter is thrown into the sky as it progresses, there is a large energy loss. In addition, rockets and jet engines are mainly explosive energy, so they are heavy in order to have durability.
The present invention is lift by an air flow or the like that circulates in an internally sealed circulation cylinder or the like. An air flow is generated from a power unit such as a propeller installed inside the sealed and circulated at high speed in the closed circulation path, and a plurality of sheets are installed in the internal circulation path. It rises due to the lift generated by applying the airflow to the wing and lift body, and the energy of the airflow is rotated without waste and further recirculated, so that the airflow energy loss other than the energy lost due to frictional resistance is eliminated.
Further, as described above, since the system does not require outside air by circulation, it is possible to generate lift in the sky or outer space where the gas is lean or vacuum.
物質移動エネルギーを効率的に使い、エネルギー節約をするとともに、循環式という特徴により密閉性も作ることが可能になるため、真空状態でも揚力を発生させることが可能となる。よって当システムの発生揚力により垂直上昇ができ、さらに希薄な空気層である上空または真空である宇宙空間まで垂直上昇、垂直下降、滞空することができる。
またジェットエンジンの噴射に頼らない揚力システムであり、その仕組みである循環形式により使用エネルギーが少なく、また爆発エネルギーに頼らないので構造が簡易かつ軽量な飛行体ができる。
具体的なイメージとしてはUFOのような宇宙まで垂直上昇飛行ができる飛行体であり、宇宙船、宇宙進行飛行機などや、ロープに頼らない宇宙エレーベーターなどを実現することができる。またスクリュー、ジェット、タイヤなどによる外界との接触摩擦がなく推進できるので音が外に漏れない静音タイプの宇宙船、飛行機、ヘリコプター、船、潜水艦、地上車、列車などの推進エンジンとして利用ができる。
また機密式でジェト噴射やフロペラによる風が外部に影響しないので、噴煙の撒き散らしや、砂、チリの巻揚などがなくなる。
従来よりジェットによる垂直上昇、また通常の飛行機やヘリコプターのように外気を翼やプロペラにあてて揚力を発生させ進行、浮揚するシステムはあった、しかし通常一般的にあるロケット、ジェット機、プロペラ機、ヘリコプター共に発生した気流のエネルギーは進行とともに空に捨てていくので大きなエネルギーロスがあるのである。またロケットやジェットエンジンは爆発エネルギーをメインとするので耐久性を持たせるために重いものとなる。
当発明は内部密閉した循環筒等に循環させる気流等による揚力であり、密閉した内部に設置したプロペラなどのパワーユニットから気流を発生させて密閉循環路に高速循環させ、内部循環路に複数枚設置した翼や揚力体に気流を当てることにより発生した揚力で上昇し、また気流のエネルギーを無駄なくローテーションさせてさらに再循環させるので、摩擦抵抗で損失するエネルギー以外の気流エネルギー損失を無くなるのである。
また上記のように循環による外気不要のシステムであるので気体が希薄または真空である上空、宇宙空間での揚力発生を可能とする。
In the present invention, a substance such as air is circulated in a closed circulation path by a fan or the like, and the fluid substance is applied to a lift body provided in the middle to generate lift.
Efficient use of mass transfer energy saves energy, and the circulation type makes it possible to create airtightness, which makes it possible to generate lift even in a vacuum state. Therefore, the lift generated by this system allows vertical ascent, and vertical ascent, vertical descent, and dwelling to the sky, which is a dilute air layer, or to outer space, which is a vacuum.
In addition, it is a lift system that does not rely on the injection of a jet engine, and it uses less energy due to its circulation type, and because it does not rely on explosive energy, it can create a simple and lightweight aircraft.
As a concrete image, it is an air vehicle that can fly vertically up to space like a UFO, and it can realize spacecraft, space traveling airplanes, space elevators that do not rely on ropes, and so on. In addition, since it can be propelled without contact friction with the outside world due to screws, jets, tires, etc., it can be used as a propulsion engine for silent type spacecraft, airplanes, helicopters, ships, submarines, ground vehicles, trains, etc. ..
In addition, since it is a confidential type and the wind from jet injection and flopera does not affect the outside, there is no need to scatter the plume or wind up sand or dust.
Traditionally, there have been systems for vertical ascent by jets, and for moving and floating by applying outside air to wings and propellers to generate lift like ordinary airplanes and helicopters, but usually rockets, jets, propellers, Since the energy of the airflow generated by the helicopter is thrown into the sky as it progresses, there is a large energy loss. In addition, rockets and jet engines are mainly explosive energy, so they are heavy in order to have durability.
The present invention is lift by an air flow or the like that circulates in an internally sealed circulation cylinder or the like. An air flow is generated from a power unit such as a propeller installed inside the sealed and circulated at high speed in the closed circulation path, and a plurality of sheets are installed in the internal circulation path. It rises due to the lift generated by applying the airflow to the wing and lift body, and the energy of the airflow is rotated without waste and further recirculated, so that the airflow energy loss other than the energy lost due to frictional resistance is eliminated.
Further, as described above, since the system does not require outside air by circulation, it is possible to generate lift in the sky or outer space where the gas is lean or vacuum.
仕組み・形状
翼の形状は使用する流体物質の性質や速度により最適なものを選ぶ。
また循環路は上面はフラット又はなだらかな凹凸面で流動体の抵抗を減らして、スムーズな気流と比較的低い気圧を保つ。また下面は翼半面の揚力体やボルテックス、蛇腹や凹凸で乱流渦巻を起こしながら比較的高い気圧を保つ。
循環路下側に発生する乱流は高圧の渦巻であり、天気図の低気圧の様に外周部を引きこむので循環路の下面を引きつける。そしてその低気圧は下面を引きつけながら後続の流動体により上方に流される。そして徐々に渦巻は分解され循環路上面部の気流に合流するか又は経路の翼の下面に衝突するので全体的に大きな揚力が発生する。
また上記採用した迎え角の大きい翼が循環する気流等を下側に集めるので、循環路の下側に強く流動体を通すこととなり、上記の揚力体に気流があたり揚力を発生する。それは循環路揚力が強く発生し、翼に発生する揚力とともに大きな揚力になるのである。循環路下面の揚力は大きいので翼の角度を水平に近く変えた時はルーバー等により循環路下側に気流を集めて循環路下側の蛇腹等に多く気流等があたるようにする。また翼も効率よく気流等によく当たるように下側に移動させる。
形状
円筒の循環筒を並列に並べたもので、水平・垂直の並びの両方の形
三角の循環路の組み合わせで、水平・垂直の並びの両方の形
四角の循環路の組み合わせで、水平・垂直の並びの両方の形
五角などの多角の循環路の組み合わせで、水平・垂直の並びの両方の形
浮き輪のような円形循環路とその組み合わせで、水平・垂直の並びの両方の形
円形渦巻の循環路の組み合わせで、水平・垂直の並びの両方の形、それをずらして合わせたもの
上記の多重積層複層化したもの
左右ダブルプロペラ浮き輪型
循環路の左右にプロペラパワーユニットつけて揚力、上昇力とする。空気圧がした部分で高くなる。パワーユニットの吸気のための空気循環は外側又は内側より上部に空気を移動させる。エネルギーユニット同士の反発圧力による揚力増加、上面、下面の気圧差による推進力発生がある。
楕円横直線ありにして直線部分に羽を沢山設ける。
ファンの上昇揚力と反対側立ち上がり部分の穴開き半球揚力体のバランスを取る。
パワーユニット
パワーユニットは、動力として気流を循環させるとともに、プロペラ自体が揚力発生させているのでその揚力を利用、垂直上昇方向に揚力をプラスさせるために下方向に送風方向が向いたプロペラ、同じく下方向に向いたジェット噴射式でジェットタービン羽が上向きに揚力発生する循環式も含む。
Mechanism / shape Select the optimum wing shape according to the properties and speed of the fluid material used.
In addition, the circulation path has a flat or gently uneven surface on the upper surface to reduce the resistance of the fluid and maintain a smooth air flow and a relatively low air pressure. In addition, the lower surface maintains a relatively high air pressure while causing turbulent swirls due to the lift body, vortex, bellows and unevenness on the half surface of the wing.
The turbulent flow generated on the lower side of the circulation path is a high-pressure spiral, which draws in the outer peripheral part like a low pressure system in a weather map, so that it attracts the lower surface of the circulation path. Then, the low pressure is flowed upward by the following fluid while attracting the lower surface. Then, the vortex is gradually decomposed and joins the air flow on the upper surface of the circulation path or collides with the lower surface of the blade of the path, so that a large lift is generated as a whole.
Further, since the airflow and the like circulated by the blade having a large angle of attack adopted above are collected on the lower side, the fluid is strongly passed under the circulation path, and the airflow hits the lift body to generate lift. It produces a strong circulatory lift, which becomes a large lift along with the lift generated on the wing. Since the lift on the lower surface of the circulation path is large, when the angle of the wing is changed to be close to horizontal, the airflow is collected under the circulation path by a louver or the like so that a large amount of airflow or the like hits the bellows or the like under the circulation path. Also, move the wings downward so that they can hit the airflow efficiently.
Shape Cylindrical circulation cylinders are arranged in parallel, with a combination of both horizontal and vertical arrangements of triangular circulation paths, and a combination of both horizontal and vertical arrangements of square circulation paths, horizontal and vertical. A combination of polygonal circulation paths such as pentagons, both horizontal and vertical arrangements, and a circular circulation path such as a floating ring and its combination, both horizontal and vertical arrangements. A combination of two circulation paths, both horizontal and vertical arrangements, which are combined by shifting them. The above-mentioned multi-layered multi-layered one. Left and right double propellers Floating ring type Propeller power units are attached to the left and right of the circulation path to lift. Ascending power. It becomes higher at the part where the air pressure is applied. The air circulation for intake of the power unit moves air above the outside or inside. There is an increase in lift due to the repulsive pressure between energy units, and a propulsive force is generated due to the pressure difference between the upper and lower surfaces.
Make an elliptical horizontal straight line and provide a lot of wings on the straight line.
Balance the lift of the fan with the perforated hemispherical lift on the opposite side of the rise.
Power unit The power unit circulates the airflow as power, and the propeller itself generates lift, so that lift is used. In order to increase the lift in the vertical ascending direction, the propeller with the air blowing direction facing downward, also downward. It also includes a circulation type in which the jet turbine blades generate lift upward in the facing jet injection type.
翼の形状は使用する流体物質の性質や速度により最適なものを選ぶ。
また循環路は上面はフラット又はなだらかな凹凸面で流動体の抵抗を減らして、スムーズな気流と比較的低い気圧を保つ。また下面は翼半面の揚力体やボルテックス、蛇腹や凹凸で乱流渦巻を起こしながら比較的高い気圧を保つ。
循環路下側に発生する乱流は高圧の渦巻であり、天気図の低気圧の様に外周部を引きこむので循環路の下面を引きつける。そしてその低気圧は下面を引きつけながら後続の流動体により上方に流される。そして徐々に渦巻は分解され循環路上面部の気流に合流するか又は経路の翼の下面に衝突するので全体的に大きな揚力が発生する。
また上記採用した迎え角の大きい翼が循環する気流等を下側に集めるので、循環路の下側に強く流動体を通すこととなり、上記の揚力体に気流があたり揚力を発生する。それは循環路揚力が強く発生し、翼に発生する揚力とともに大きな揚力になるのである。循環路下面の揚力は大きいので翼の角度を水平に近く変えた時はルーバー等により循環路下側に気流を集めて循環路下側の蛇腹等に多く気流等があたるようにする。また翼も効率よく気流等によく当たるように下側に移動させる。
形状
円筒の循環筒を並列に並べたもので、水平・垂直の並びの両方の形
三角の循環路の組み合わせで、水平・垂直の並びの両方の形
四角の循環路の組み合わせで、水平・垂直の並びの両方の形
五角などの多角の循環路の組み合わせで、水平・垂直の並びの両方の形
浮き輪のような円形循環路とその組み合わせで、水平・垂直の並びの両方の形
円形渦巻の循環路の組み合わせで、水平・垂直の並びの両方の形、それをずらして合わせたもの
上記の多重積層複層化したもの
左右ダブルプロペラ浮き輪型
循環路の左右にプロペラパワーユニットつけて揚力、上昇力とする。空気圧がした部分で高くなる。パワーユニットの吸気のための空気循環は外側又は内側より上部に空気を移動させる。エネルギーユニット同士の反発圧力による揚力増加、上面、下面の気圧差による推進力発生がある。
楕円横直線ありにして直線部分に羽を沢山設ける。
ファンの上昇揚力と反対側立ち上がり部分の穴開き半球揚力体のバランスを取る。
パワーユニット
パワーユニットは、動力として気流を循環させるとともに、プロペラ自体が揚力発生させているのでその揚力を利用、垂直上昇方向に揚力をプラスさせるために下方向に送風方向が向いたプロペラ、同じく下方向に向いたジェット噴射式でジェットタービン羽が上向きに揚力発生する循環式も含む。
Mechanism / shape Select the optimum wing shape according to the properties and speed of the fluid material used.
In addition, the circulation path has a flat or gently uneven surface on the upper surface to reduce the resistance of the fluid and maintain a smooth air flow and a relatively low air pressure. In addition, the lower surface maintains a relatively high air pressure while causing turbulent swirls due to the lift body, vortex, bellows and unevenness on the half surface of the wing.
The turbulent flow generated on the lower side of the circulation path is a high-pressure spiral, which draws in the outer peripheral part like a low pressure system in a weather map, so that it attracts the lower surface of the circulation path. Then, the low pressure is flowed upward by the following fluid while attracting the lower surface. Then, the vortex is gradually decomposed and joins the air flow on the upper surface of the circulation path or collides with the lower surface of the blade of the path, so that a large lift is generated as a whole.
Further, since the airflow and the like circulated by the blade having a large angle of attack adopted above are collected on the lower side, the fluid is strongly passed under the circulation path, and the airflow hits the lift body to generate lift. It produces a strong circulatory lift, which becomes a large lift along with the lift generated on the wing. Since the lift on the lower surface of the circulation path is large, when the angle of the wing is changed to be close to horizontal, the airflow is collected under the circulation path by a louver or the like so that a large amount of airflow or the like hits the bellows or the like under the circulation path. Also, move the wings downward so that they can hit the airflow efficiently.
Shape Cylindrical circulation cylinders are arranged in parallel, with a combination of both horizontal and vertical arrangements of triangular circulation paths, and a combination of both horizontal and vertical arrangements of square circulation paths, horizontal and vertical. A combination of polygonal circulation paths such as pentagons, both horizontal and vertical arrangements, and a circular circulation path such as a floating ring and its combination, both horizontal and vertical arrangements. A combination of two circulation paths, both horizontal and vertical arrangements, which are combined by shifting them. The above-mentioned multi-layered multi-layered one. Left and right double propellers Floating ring type Propeller power units are attached to the left and right of the circulation path to lift. Ascending power. It becomes higher at the part where the air pressure is applied. The air circulation for intake of the power unit moves air above the outside or inside. There is an increase in lift due to the repulsive pressure between energy units, and a propulsive force is generated due to the pressure difference between the upper and lower surfaces.
Make an elliptical horizontal straight line and provide a lot of wings on the straight line.
Balance the lift of the fan with the perforated hemispherical lift on the opposite side of the rise.
Power unit The power unit circulates the airflow as power, and the propeller itself generates lift, so that lift is used. In order to increase the lift in the vertical ascending direction, the propeller with the air blowing direction facing downward, also downward. It also includes a circulation type in which the jet turbine blades generate lift upward in the facing jet injection type.
その他の要件
下記の形態の場合も当発明と同等のものとする。
樽型ヘリコプター型
多重にしたヘリコプターの羽で揚力を発生させるが、循環式にしてエネルギー効率UPとと密閉性による多極使用を可能とする。
二重の樽の中の内側の樽のなかにヘリコプター羽を設置、揚力を発生させ、その時に発生する気流を外側樽にて上へ循環させての再循環させていくもの。また内外逆循環も含む。
ヘリコプターの羽は多重にして揚力を強くするものや、ヘリコプターの羽と羽の間に整流ルーバーつける物含む。
樽型は内樽が開閉式になっているものも含む。空気があるエリアは内樽にあるエネルギーユニットのヘリコプターファンが垂直上昇させ、空気が薄くなったところで内樽を閉めて循環式に切り替えると効率よく垂直上昇出来る。
ジェットエンジのタービン翼を上向きの揚力が発生するような角度をつけるタイプ
下記の要件も当発明と同等のものとする。
循環させる物質は通常空気であるが、発生揚力を上げるために、圧縮して密度を上げたものや、空気以外の気体、水やその他の物質による循環も含む。
循環路下面は乱流発生させる波形にし、上面は平面やなだらかな波形にして大きな乱流を防ぎ流速を速める。
また翼が循環路になく、循環路下面に乱流発生させる波形と上面に平面もつ循環路を重ねたものを沢山積層させて風や水などを循環させるものも含む。
循環空気等により効率よく揚力発生させるために整流ルーバー等で空気等の流れを整流するが、そのルーバーにも揚力が発生するようなカーブをつける。
または翼はなくその揚力ルーバーの連続設置、揚力ルーバーの連続設置と波形の循環路のみのものも含む。
パワーユニット、気流発生動力は複数或いは位置を変えたものも含む
垂直上昇を主とした物であるがあらゆる方向への推進としても使えるとする。
循環式垂直上昇システムに加え、通常飛行機等みたいな外部設置の羽、外部設置のプロペラ、ジェットを備えた併用タイプでも当発明とする。その場合浮揚のための揚力は当システムで浮揚させ、進行するための推進はジェットやプロペラで行うと翼が小さくて済むので推進抵抗が少なくなる、またジェットやプロペラで発生した空気等の移動エネルギーを一度内部の循環機関で揚力発生のために通して、その後外部ジェット噴射、放出して推進させるタイプも含むとする。また密閉循環を基礎とするが一部外部流動体との出入りをすることも可能とする。ジェット直噴でなく循環路の渦巻通し渦巻内のに羽や揚力体に風あてて揚力を発生させ、その後下向きに噴射する。
また、ジェットエンジンタービンを循環式のプロペラに連動して循環路の空気を循環させて循環式揚力により上昇力を大きくする。
設置する翼は様々な形を使用できる。また迎え角度については流体の速度により変えるが、角度が大きめで乱流が起きて剥離したり失速するような角度でも当システムでは有効に機能するのでその極端に大きい迎え角度の採用についても当発明とする。具体的な角度は翼の形状、流動物の媒体、流動速度によるので上げられないが、通常その角度の翼であると飛行機が剥離したり失速するような角度である。この大きい迎え角度により流体の速度が低くても大きな揚力を得ることができるのである。
また翼の形の先頭に吸い取り口を付け、翼上面の気圧を下げ、下面には穴開き横板をつけて抵抗を増し気圧を高めことにより翼自体の揚力高める方式も含める。
当システムの大きな迎え角に対する有効性は次のとおりである。
極端に大きい迎え角がつくる力
1 翼下面に対する押し上げ揚力
2 翼上面に起きる引き延ばしによる流動高速化揚力と、上面後部に起きる乱流による翼に対する乱流の引きつけ揚力
3 そして下に押し曲げられた流動物質の循環路の下側に対する強い流れである。そして循環路下面に吹き付ける強い流れは下面の角のある波面にあたり乱流を作り、下面を上に引きつける。また循環路下面に流動体の流れが集中する為、再び次の翼の下側に強く風が当たって1の押し上げ揚力が強くなり、3の下面の揚力体波面にも流動体が強く流れるので揚力発生が強くなるとういう好循環になるのである。
循環路下面の揚力体波面はその面に風等が当たると揚力が発生する。その仕組みは次のとおりである。
湾曲面に曲げられた風が面の長さに合わせて引き伸ばされる。すると気圧が低くなるので揚力が発生する。さらに風が渦巻くために天気図で言うところの低気圧に似たものが発生してその小さな低気圧帯の外周部が引き込み要素になりその部分の気圧が下がるのである。渦巻は風を中心部に強く押し込むので中心部は気圧が高くなるが、外周部は引き込みがあり伸びるので逆に気圧が低くなる。そこで外周部との接点部分は気圧が低くなり揚力を発生させるのである。
また外殻を柔らかいものにして折りたたみ携帯して必要時に膨らませて使用するものも当発明とする。
Other requirements The following forms are also equivalent to the present invention.
Barrel-type helicopter type The wings of a multi-layered helicopter generate lift, but the circulation type improves energy efficiency and enables multi-pole use due to airtightness.
A helicopter wing is installed in the inner barrel inside the double barrel to generate lift, and the airflow generated at that time is circulated upward in the outer barrel to recirculate it. It also includes internal and external reverse circulation.
Helicopter wings include those with multiple layers to increase lift and those with a rectifying louver between the helicopter wings.
The barrel type also includes those with an inner barrel that can be opened and closed. In the area with air, the helicopter fan of the energy unit in the inner barrel raises vertically, and when the air becomes thin, close the inner barrel and switch to the circulation type to efficiently raise vertically.
A type in which the turbine blades of a jet engine are angled so as to generate upward lift.
The following requirements are also equivalent to those of the present invention.
The substance to be circulated is usually air, but it also includes substances that have been compressed to increase the density in order to increase the lift generated, and circulation by gases other than air, water, and other substances.
The lower surface of the circulation path has a waveform that generates turbulence, and the upper surface has a flat or gentle waveform to prevent large turbulence and accelerate the flow velocity.
In addition, there are also those in which the blades are not in the circulation path, and a large number of waveforms that generate turbulent flow on the lower surface of the circulation path and a circulation path having a flat surface on the upper surface are laminated to circulate wind and water.
A rectifying louver or the like rectifies the flow of air or the like in order to efficiently generate lift by circulating air or the like, and the louver also has a curve that generates lift.
Or, there are no wings, and the continuous installation of the lift louver, the continuous installation of the lift louver, and the one with only the corrugated circulation path are included.
Power unit, airflow generation power includes multiple or repositioned ones
Although it is mainly for vertical ascent, it can also be used for propulsion in all directions.
In addition to the circulation type vertical climbing system, the present invention also includes a combined type equipped with an externally installed wing, an externally installed propeller, and a jet such as an ordinary airplane. In that case, the lift for levitation is lifted by this system, and if the propulsion to proceed is performed by a jet or propeller, the wings need to be small, so the propulsion resistance is reduced, and the moving energy of air generated by the jet or propeller is reduced. Is also included in the type in which the air is once passed through the internal circulation engine to generate lift, and then the external jet is injected, released and propelled. In addition, although it is based on closed circulation, it is also possible to enter and exit some external fluids. Instead of direct jet injection, the wing and lift body are blown to generate lift in the spiral through the circulation path, and then the jet is injected downward.
In addition, the jet engine turbine is interlocked with the circulation type propeller to circulate the air in the circulation path, and the ascending force is increased by the circulation type lift.
Various shapes can be used for the wings to be installed. In addition, the pick-up angle is changed depending on the speed of the fluid, but since the system functions effectively even at an angle where the angle is large and turbulence occurs and the system peels off or stalls, the present invention also adopts an extremely large pick-up angle. And. The specific angle cannot be increased because it depends on the shape of the wing, the medium of the fluid, and the flow velocity, but the angle of the wing is usually such that the airplane will peel off or stall. Due to this large lift angle, a large lift can be obtained even if the fluid velocity is low.
In addition, a suction port is attached to the front of the wing shape to lower the air pressure on the upper surface of the wing, and a perforated horizontal plate is attached to the lower surface to increase resistance and increase the air pressure to increase the lift of the wing itself.
The effectiveness of this system for large angles of attack is as follows.
The power created by an extremely large angle of attack
1 Push-up lift on the underside of the wing
2 Lifting force for speeding up flow due to stretching on the upper surface of the wing and lift for attracting turbulent flow to the wing due to turbulence occurring on the rear of the upper surface
3 And it is a strong flow of the fluid material pushed down to the lower side of the circulation path. The strong flow that blows onto the lower surface of the circulation path hits the angular wave surface on the lower surface, creating turbulence and attracting the lower surface upward. In addition, since the flow of fluid is concentrated on the lower surface of the circulation path, the wind hits the lower side of the next wing again and the lift lift of 1 becomes stronger, and the fluid also flows strongly on the lift body wave surface of the lower surface of 3. It becomes a virtuous cycle that the lift generation becomes stronger.
Lift on the underside of the circulation path Lift is generated when the wave surface is hit by wind or the like. The mechanism is as follows.
The wind bent on the curved surface is stretched according to the length of the surface. Then, the air pressure becomes low and lift is generated. Furthermore, because the wind swirls, something similar to a low pressure system in the weather chart is generated, and the outer peripheral part of the small low pressure zone becomes a pull-in element, and the atmospheric pressure in that part drops. Since the swirl pushes the wind strongly into the central part, the air pressure rises in the central part, but the outer peripheral part draws in and stretches, so that the air pressure decreases. Therefore, the air pressure at the contact portion with the outer peripheral portion becomes low and lift is generated.
The present invention also relates to a soft outer shell that can be folded and carried and inflated when necessary.
下記の形態の場合も当発明と同等のものとする。
樽型ヘリコプター型
多重にしたヘリコプターの羽で揚力を発生させるが、循環式にしてエネルギー効率UPとと密閉性による多極使用を可能とする。
二重の樽の中の内側の樽のなかにヘリコプター羽を設置、揚力を発生させ、その時に発生する気流を外側樽にて上へ循環させての再循環させていくもの。また内外逆循環も含む。
ヘリコプターの羽は多重にして揚力を強くするものや、ヘリコプターの羽と羽の間に整流ルーバーつける物含む。
樽型は内樽が開閉式になっているものも含む。空気があるエリアは内樽にあるエネルギーユニットのヘリコプターファンが垂直上昇させ、空気が薄くなったところで内樽を閉めて循環式に切り替えると効率よく垂直上昇出来る。
ジェットエンジのタービン翼を上向きの揚力が発生するような角度をつけるタイプ
下記の要件も当発明と同等のものとする。
循環させる物質は通常空気であるが、発生揚力を上げるために、圧縮して密度を上げたものや、空気以外の気体、水やその他の物質による循環も含む。
循環路下面は乱流発生させる波形にし、上面は平面やなだらかな波形にして大きな乱流を防ぎ流速を速める。
また翼が循環路になく、循環路下面に乱流発生させる波形と上面に平面もつ循環路を重ねたものを沢山積層させて風や水などを循環させるものも含む。
循環空気等により効率よく揚力発生させるために整流ルーバー等で空気等の流れを整流するが、そのルーバーにも揚力が発生するようなカーブをつける。
または翼はなくその揚力ルーバーの連続設置、揚力ルーバーの連続設置と波形の循環路のみのものも含む。
パワーユニット、気流発生動力は複数或いは位置を変えたものも含む
垂直上昇を主とした物であるがあらゆる方向への推進としても使えるとする。
循環式垂直上昇システムに加え、通常飛行機等みたいな外部設置の羽、外部設置のプロペラ、ジェットを備えた併用タイプでも当発明とする。その場合浮揚のための揚力は当システムで浮揚させ、進行するための推進はジェットやプロペラで行うと翼が小さくて済むので推進抵抗が少なくなる、またジェットやプロペラで発生した空気等の移動エネルギーを一度内部の循環機関で揚力発生のために通して、その後外部ジェット噴射、放出して推進させるタイプも含むとする。また密閉循環を基礎とするが一部外部流動体との出入りをすることも可能とする。ジェット直噴でなく循環路の渦巻通し渦巻内のに羽や揚力体に風あてて揚力を発生させ、その後下向きに噴射する。
また、ジェットエンジンタービンを循環式のプロペラに連動して循環路の空気を循環させて循環式揚力により上昇力を大きくする。
設置する翼は様々な形を使用できる。また迎え角度については流体の速度により変えるが、角度が大きめで乱流が起きて剥離したり失速するような角度でも当システムでは有効に機能するのでその極端に大きい迎え角度の採用についても当発明とする。具体的な角度は翼の形状、流動物の媒体、流動速度によるので上げられないが、通常その角度の翼であると飛行機が剥離したり失速するような角度である。この大きい迎え角度により流体の速度が低くても大きな揚力を得ることができるのである。
また翼の形の先頭に吸い取り口を付け、翼上面の気圧を下げ、下面には穴開き横板をつけて抵抗を増し気圧を高めことにより翼自体の揚力高める方式も含める。
当システムの大きな迎え角に対する有効性は次のとおりである。
極端に大きい迎え角がつくる力
1 翼下面に対する押し上げ揚力
2 翼上面に起きる引き延ばしによる流動高速化揚力と、上面後部に起きる乱流による翼に対する乱流の引きつけ揚力
3 そして下に押し曲げられた流動物質の循環路の下側に対する強い流れである。そして循環路下面に吹き付ける強い流れは下面の角のある波面にあたり乱流を作り、下面を上に引きつける。また循環路下面に流動体の流れが集中する為、再び次の翼の下側に強く風が当たって1の押し上げ揚力が強くなり、3の下面の揚力体波面にも流動体が強く流れるので揚力発生が強くなるとういう好循環になるのである。
循環路下面の揚力体波面はその面に風等が当たると揚力が発生する。その仕組みは次のとおりである。
湾曲面に曲げられた風が面の長さに合わせて引き伸ばされる。すると気圧が低くなるので揚力が発生する。さらに風が渦巻くために天気図で言うところの低気圧に似たものが発生してその小さな低気圧帯の外周部が引き込み要素になりその部分の気圧が下がるのである。渦巻は風を中心部に強く押し込むので中心部は気圧が高くなるが、外周部は引き込みがあり伸びるので逆に気圧が低くなる。そこで外周部との接点部分は気圧が低くなり揚力を発生させるのである。
また外殻を柔らかいものにして折りたたみ携帯して必要時に膨らませて使用するものも当発明とする。
Other requirements The following forms are also equivalent to the present invention.
Barrel-type helicopter type The wings of a multi-layered helicopter generate lift, but the circulation type improves energy efficiency and enables multi-pole use due to airtightness.
A helicopter wing is installed in the inner barrel inside the double barrel to generate lift, and the airflow generated at that time is circulated upward in the outer barrel to recirculate it. It also includes internal and external reverse circulation.
Helicopter wings include those with multiple layers to increase lift and those with a rectifying louver between the helicopter wings.
The barrel type also includes those with an inner barrel that can be opened and closed. In the area with air, the helicopter fan of the energy unit in the inner barrel raises vertically, and when the air becomes thin, close the inner barrel and switch to the circulation type to efficiently raise vertically.
A type in which the turbine blades of a jet engine are angled so as to generate upward lift.
The following requirements are also equivalent to those of the present invention.
The substance to be circulated is usually air, but it also includes substances that have been compressed to increase the density in order to increase the lift generated, and circulation by gases other than air, water, and other substances.
The lower surface of the circulation path has a waveform that generates turbulence, and the upper surface has a flat or gentle waveform to prevent large turbulence and accelerate the flow velocity.
In addition, there are also those in which the blades are not in the circulation path, and a large number of waveforms that generate turbulent flow on the lower surface of the circulation path and a circulation path having a flat surface on the upper surface are laminated to circulate wind and water.
A rectifying louver or the like rectifies the flow of air or the like in order to efficiently generate lift by circulating air or the like, and the louver also has a curve that generates lift.
Or, there are no wings, and the continuous installation of the lift louver, the continuous installation of the lift louver, and the one with only the corrugated circulation path are included.
Power unit, airflow generation power includes multiple or repositioned ones
Although it is mainly for vertical ascent, it can also be used for propulsion in all directions.
In addition to the circulation type vertical climbing system, the present invention also includes a combined type equipped with an externally installed wing, an externally installed propeller, and a jet such as an ordinary airplane. In that case, the lift for levitation is lifted by this system, and if the propulsion to proceed is performed by a jet or propeller, the wings need to be small, so the propulsion resistance is reduced, and the moving energy of air generated by the jet or propeller is reduced. Is also included in the type in which the air is once passed through the internal circulation engine to generate lift, and then the external jet is injected, released and propelled. In addition, although it is based on closed circulation, it is also possible to enter and exit some external fluids. Instead of direct jet injection, the wing and lift body are blown to generate lift in the spiral through the circulation path, and then the jet is injected downward.
In addition, the jet engine turbine is interlocked with the circulation type propeller to circulate the air in the circulation path, and the ascending force is increased by the circulation type lift.
Various shapes can be used for the wings to be installed. In addition, the pick-up angle is changed depending on the speed of the fluid, but since the system functions effectively even at an angle where the angle is large and turbulence occurs and the system peels off or stalls, the present invention also adopts an extremely large pick-up angle. And. The specific angle cannot be increased because it depends on the shape of the wing, the medium of the fluid, and the flow velocity, but the angle of the wing is usually such that the airplane will peel off or stall. Due to this large lift angle, a large lift can be obtained even if the fluid velocity is low.
In addition, a suction port is attached to the front of the wing shape to lower the air pressure on the upper surface of the wing, and a perforated horizontal plate is attached to the lower surface to increase resistance and increase the air pressure to increase the lift of the wing itself.
The effectiveness of this system for large angles of attack is as follows.
The power created by an extremely large angle of attack
1 Push-up lift on the underside of the wing
2 Lifting force for speeding up flow due to stretching on the upper surface of the wing and lift for attracting turbulent flow to the wing due to turbulence occurring on the rear of the upper surface
3 And it is a strong flow of the fluid material pushed down to the lower side of the circulation path. The strong flow that blows onto the lower surface of the circulation path hits the angular wave surface on the lower surface, creating turbulence and attracting the lower surface upward. In addition, since the flow of fluid is concentrated on the lower surface of the circulation path, the wind hits the lower side of the next wing again and the lift lift of 1 becomes stronger, and the fluid also flows strongly on the lift body wave surface of the lower surface of 3. It becomes a virtuous cycle that the lift generation becomes stronger.
Lift on the underside of the circulation path Lift is generated when the wave surface is hit by wind or the like. The mechanism is as follows.
The wind bent on the curved surface is stretched according to the length of the surface. Then, the air pressure becomes low and lift is generated. Furthermore, because the wind swirls, something similar to a low pressure system in the weather chart is generated, and the outer peripheral part of the small low pressure zone becomes a pull-in element, and the atmospheric pressure in that part drops. Since the swirl pushes the wind strongly into the central part, the air pressure rises in the central part, but the outer peripheral part draws in and stretches, so that the air pressure decreases. Therefore, the air pressure at the contact portion with the outer peripheral portion becomes low and lift is generated.
The present invention also relates to a soft outer shell that can be folded and carried and inflated when necessary.
Claims (16)
- プロペラ、ジェットなどの動力により発生させた気流などの流動体の流れを循環させて気流エネルギーの効率利用する。 Efficient use of airflow energy by circulating the flow of fluid such as airflow generated by the power of propellers and jets.
- 循環経路を気密化して外部流動体との接触を断ち、外界概況に作用されない安定した揚力発生を可能とさせる。 It makes the circulation path airtight and cuts off contact with the external fluid, enabling stable lift generation that is not affected by the external conditions.
- 気密化した安定したユニットであるので宇宙や海中など様々な空間での静音かつ安定した動力を可能とし、周りの環境を気流等で乱さない。 Since it is an airtight and stable unit, it enables quiet and stable power in various spaces such as space and underwater, and does not disturb the surrounding environment with air currents.
- 循環経路に揚力発生させる為、循環路下面に抵抗の増える波状の板を設けて乱流を起こし、循環路上面には平面や緩やかな波面で抵抗のない流速を高めるゾーンにする。流速の差異による揚力発生と乱流の持つ揚力により全体揚力の向上をする。またそれはホールやディンプル、半面にした翼を組み合わせたりしたものに流動体を当てて揚力を発生させることも含む。 In order to generate lift in the circulation path, a wavy plate with increased resistance is provided on the lower surface of the circulation path to cause turbulence, and the upper surface of the circulation path is provided with a flat or gentle wave surface to create a zone for increasing the flow velocity without resistance. The overall lift is improved by the lift generated by the difference in flow velocity and the lift of the turbulent flow. It also includes applying a fluid to a combination of holes, dimples, and half-faced wings to generate lift.
- 大きな迎え角も大きな揚力を発生させるものとして使える。 A large angle of attack can also be used to generate a large lift.
- 樽内ヘリコプター型、図面のように二重の樽の中の内側にプロペラを、外側を循環通路にするもの、また内外逆のものも含む。 Includes in-barrel helicopter type, one with a propeller inside the double barrel as shown in the drawing, and one with the outside as a circulation passage, and the inside and outside reverse.
- ジェットエンジンの噴出気流に揚力発生する翼を設けるタイプ。 A type that has wings that generate lift in the jet airflow of a jet engine.
- 動力ユニットのプロペラの揚力を上向きに向けて揚力利用するもの。 The lift of the propeller of the power unit is used upward.
- 外殻を柔らかいものにして折りたたみ携帯して必要時に膨らませて使用するものも当発明とする。 It is also the present invention to make the outer shell soft, fold it, carry it, and inflate it when necessary.
- 循環空気等により効率よく揚力発生させるために整流ルーバー等で空気等の流れを整流する。またそのルーバーにも揚力が発生するようなカーブをつける。また揚力体波形と平面を重ねたものをペアとして、それを沢山重ねたものに風などを循環させるものも含む。 The flow of air is rectified with a rectifying louver or the like in order to efficiently generate lift by circulating air or the like. Also, make a curve on the louver so that lift is generated. It also includes a pair of lift body waveforms and planes, and a lot of them that circulate wind.
- 気流発生動力は複数或いは位置を変えたものも含む Airflow generation power includes multiple or repositioned powers
- 垂直上昇を主とした物であるがあらゆる方向への推進としても使える。 It is mainly for vertical climbing, but it can also be used for propulsion in all directions.
- 循環式垂直上昇システムに加え、通常の航空システムである外部の外気にあたる羽、プロペラ、ジェットを備えた併用タイプでも当発明とする。 In addition to the circulation type vertical climbing system, the present invention also includes a combined type equipped with wings, a propeller, and a jet that correspond to the outside air, which is a normal aviation system.
- 形状は図面2〜7の通りである。
円筒の水平・垂直
三角の水平・垂直
四角の水平・垂直
五角などの多角の水平・垂直
浮き輪のような円形
円形渦巻の水平・垂直
上記の積層複層
上記の縦型及び縦型の合わせ型 The shape is as shown in Drawing 2 〜 7.
Cylindrical horizontal / vertical Triangular horizontal / vertical Square horizontal / vertical pentagonal polygon horizontal / vertical Floating ring-like circular circular spiral horizontal / vertical The above laminated multi-layer The above vertical and vertical combined type - また密閉循環を基礎とするが一部外部流動体との出入りをすることも可能とする。 In addition, although it is based on closed circulation, it is also possible to enter and exit some external fluids.
- 循環させる物質は水やその他の物質によるもの、空気等を圧縮したものの循環も含む
The substances to be circulated include those caused by water and other substances, and the circulation of compressed air, etc.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/JP2019/017189 WO2020217304A1 (en) | 2019-04-23 | 2019-04-23 | Sclosed circulation vertical rising system |
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| Application Number | Priority Date | Filing Date | Title |
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| PCT/JP2019/017189 WO2020217304A1 (en) | 2019-04-23 | 2019-04-23 | Sclosed circulation vertical rising system |
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| Publication Number | Publication Date |
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| WO2020217304A1 true WO2020217304A1 (en) | 2020-10-29 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN115432836A (en) * | 2022-09-09 | 2022-12-06 | 长江生态环保集团有限公司 | Uniform aeration robot and trajectory planning method |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019035718A (en) * | 2017-08-21 | 2019-03-07 | 三菱重工機械システム株式会社 | Wind tunnel device |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| JP2019035718A (en) * | 2017-08-21 | 2019-03-07 | 三菱重工機械システム株式会社 | Wind tunnel device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115432836A (en) * | 2022-09-09 | 2022-12-06 | 长江生态环保集团有限公司 | Uniform aeration robot and trajectory planning method |
| CN115432836B (en) * | 2022-09-09 | 2023-09-29 | 长江生态环保集团有限公司 | Uniform aeration robot and track planning method |
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