JP2016017520A - Engine with no-reactive driving force - Google Patents
Engine with no-reactive driving force Download PDFInfo
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- JP2016017520A JP2016017520A JP2014152356A JP2014152356A JP2016017520A JP 2016017520 A JP2016017520 A JP 2016017520A JP 2014152356 A JP2014152356 A JP 2014152356A JP 2014152356 A JP2014152356 A JP 2014152356A JP 2016017520 A JP2016017520 A JP 2016017520A
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- fluid
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この発明は密閉した容器の中で流体を循環させそれと同時に図示(図1)するごとき円盤(片側の面に羽根をつけた)を高速で回転させ、円盤に無反動推進力を発生する機関である。This invention is an engine that circulates fluid in a sealed container and simultaneously rotates a disk (with a blade on one side) as shown in the figure (FIG. 1) at high speed to generate a reactionless propulsion force on the disk. is there.
現在推進力と言われるものはすべて反動力である。
流体(液体・水・空気またはガス)を噴射または後方へ移動させる時の反動力で推進している。All that is currently called propulsion is reaction.
It is propelled by the reaction force when fluid (liquid, water, air or gas) is jetted or moved backward.
反動力は次のような欠点がある。
(イ) ジェット機・ヘリコプターなどで分かるように大きな騒音と振動を発生する。
(ロ) ジェット機・ヘリコプターなどで分かるように機体の推進・揚力のためにエネルギーの大半が流体を動かす動力に消費される。
(ハ) ジェット機・ヘリコプターなどで分かるようにエンジンや回転翼のそばに人は近づけない。
(ニ) ジェット機・ヘリコプターなどで分かるように上述(イ)(ハ)の理由で住宅・人家の近くなどに近付けない。
本発明は以上のような欠点をなくすためになされたものである。The reaction force has the following drawbacks.
(B) Generates loud noise and vibration, as can be seen with jets and helicopters.
(B) As can be seen from jet aircraft and helicopters, most of the energy is consumed by the power that moves the fluid for propulsion and lift of the aircraft.
(C) As you can see with jets and helicopters, keep people away from the engine and rotor blades.
(D) As you can see from jet planes and helicopters, keep away from the vicinity of houses and houses due to the reasons described in (a) and (c) above.
The present invention has been made to eliminate the above drawbacks.
(イ) この機関は密閉した容器の中で流体(液体・ガス体)を再循環させながら、その途中に図1.のごとき円盤を高速で回転させる構造である。
(ロ) 回転する円盤は片側の面は滑らかな面(図3に示すごとく中心部に流体が流れる穴がある)・他方は多数の羽根(図2.に示するごとく中心から外周方向へ一定間隔でつけた真直ぐなもの)をつけたもの。
(ハ) 羽根の付いた円盤が回転しない場合はただ内部の流体が循環するだけである。
(ニ) 密閉容器の中の流体が再循環している状態で、羽根の付いた円盤と滑らかな面を持った円盤が同時に回転すると、そのそれぞれの表面において流速の違いが生じて圧力(静圧力)の差が発生する。
(ホ) その流速の違いは図4.,図5.に示す如く中心から外周方向へ同じ時間に同じ距離(中心から外周方向への)(L)動く場合、直線より曲線の方が道のりが長くそれだけ曲線の方が早く移動しなければならないことになる。
(ヘ) これはベルヌーイの定理に従ったものである。
図6に示すような流路の大きさが広いところから狭いところに流体が流れる状態。
図7に示すような流速圧力の関係が定理として成り立つ。
(ト) 密閉容器の中の流体を比重が大きい液体にしたり、ガス体の場合圧力を大きくすることで小型のもので大きな力を発生することができる。(A) This engine recirculates fluid (liquid / gas) in a sealed container, while FIG. This is a structure that rotates the disk at high speed.
(B) A rotating disk has a smooth surface on one side (as shown in Fig. 3 there is a hole through which fluid flows in the center), and the other is a large number of blades (as shown in Fig. 2. constant from the center to the outer circumference) Straight ones attached at intervals).
(C) If the disk with blades does not rotate, the internal fluid just circulates.
(D) If the bladed disk and the disk with a smooth surface rotate at the same time while the fluid in the sealed container is recirculating, a difference in flow velocity occurs on each surface, causing pressure (static Pressure) difference occurs.
(E) The difference in flow velocity is shown in Fig. 4. FIG. When the same distance (from the center to the outer circumference) (L) moves from the center to the outer circumference at the same time, the curve has a longer path than the straight line, and the curve has to move faster. .
(F) This is in accordance with Bernoulli's theorem.
A state in which the fluid flows from a wide area to a narrow area as shown in FIG.
The relationship between flow velocity and pressure as shown in FIG.
(G) A large force can be generated with a small size by changing the fluid in the sealed container to a liquid having a large specific gravity or increasing the pressure in the case of a gas body.
(イ) 大きな騒音と振動を発生することなく、推進力を発生することができる。
(ロ) 推進力・揚力を高いエネルギー効率で発生できる。
(ハ) 回転部が密閉容器の中にあるため、人がそばに近づける。
(ニ) 密閉容器の中の流体の密度を高めたり、圧力を高くすることで小型で大きな力をつくることが出来る。
(ホ) この推進力は飛行機・自動車・船などすべての乗り物・移動手段に使える。
(ヘ) この推進力は乗り物以外にも使える。(A) Propulsive force can be generated without generating large noise and vibration.
(B) Propulsion and lift can be generated with high energy efficiency.
(C) Because the rotating part is in an airtight container, a person approaches it.
(D) A large force can be created in a small size by increasing the density of the fluid in the sealed container or increasing the pressure.
(E) This propulsive force can be used for all vehicles and transportation means such as airplanes, automobiles and ships.
(F) This propulsive force can be used for other than vehicles.
以下、本発明を実施するための形態について説明する。
(イ) 本発明の原理を説明するにあたり、現在輸送手段として空を飛んでいる飛飛行機の翼を考えると図8に示すように翼の上側の面と下側の面上を流れる空気の流速(対面上の)には差がある。
(ロ) 翼の上側の面はより速く下側の面上はより遅く流れるためベルヌーイの定理に従い上側が圧力(静圧力)は低く下側は圧力(静圧力)が高くなる。
(ハ) 本発明を実施するための形態は図10に示すような断面構造で密閉容器の中の流体を動かすプロペラ(8)と狭い流路の途中にある回転する円盤(片側の面に羽根がついた)(2)(3)(4)およびそれぞれを回転させる動力(モーターまたはエンジン)(6)(7)で構成される。
(ニ) 密閉容器の中の流体は液体・ガス体および圧力の高さなど適切な条件を選定し決定する。
(ホ) 流体を再循環させる流量、回転する円盤の回転速度および回転する羽根のついた円盤の構造などは効率の高い条件を選定する。
(ヘ) 図9で流体の中の円柱(12)が回転する時揚力が発生するが、回転しない時は揚力が発生ない。
(ト) 本発明を実施するための形態は図10に示すような構造で流体を再循環させるプロペラ(8)と狭い流路の途中にある回転する円盤(片側の面に羽根がついた)(2)(3)(4)が同時に回転する時に推進力が発生する。
(チ) 流体を再循環させるプロペラ(8)または狭い流路の途中にある円盤(片側の面に羽根がついた)(2)(3)(4)が同時に回転しない場合は推進力は発生しない。
(リ) 流体が流れる方向は図4、図5、図10のように中心から外側へ流れる場合および逆に外周から中心へ流れる場合(図11)も推進力は発生する。
(ヌ) 本発明を実施するための形態は図10,11に示すような断面構造の密閉容器のみに限定されず、図12のように容器が一部開放されていても狭い流路を流体が流れる状態で回転する円盤(片側の面に羽根がついて、他方は滑らかな面をした)およびそれぞれを回転させる動力があれば推進力は発生する。
(ル) ただし(ヌ)の場合は密閉容器の時に比べ効率・能力が低下する。Hereinafter, modes for carrying out the present invention will be described.
(A) In explaining the principle of the present invention, when considering a wing of a flying plane currently flying in the sky as a transportation means, the flow velocity of air flowing on the upper surface and the lower surface of the wing as shown in FIG. There is a difference (on face to face).
(B) Since the upper surface of the wing flows faster and slower on the lower surface, the pressure (static pressure) is lower on the upper side and the pressure (static pressure) is higher on the lower side according to Bernoulli's theorem.
(C) A mode for carrying out the present invention is a cross-sectional structure as shown in FIG. 10 and a propeller (8) for moving fluid in a sealed container and a rotating disk in the middle of a narrow channel (blade on one side) (2) (3) (4) and power (motor or engine) (6) (7) for rotating each of them.
(D) The fluid in the sealed container is determined by selecting appropriate conditions such as liquid / gas body and pressure level.
(E) Select highly efficient conditions such as the flow rate for recirculating fluid, the rotating speed of the rotating disk, and the structure of the disk with rotating blades.
(F) In FIG. 9, lift occurs when the cylinder (12) in the fluid rotates, but no lift occurs when it does not rotate.
(G) A form for carrying out the present invention is a propeller (8) for recirculating a fluid with a structure as shown in FIG. 10 and a rotating disk in the middle of a narrow channel (blade on one side) (2) Propulsive force is generated when (3) and (4) rotate simultaneously.
(H) Propeller that recirculates fluid (8) or a disk in the middle of a narrow flow path (with blades on one side) (2) (3) (4) if propulsion is not generated simultaneously do not do.
(I) Propulsive force is generated when the fluid flows from the center to the outside as shown in FIGS. 4, 5, and 10 and conversely from the outer periphery to the center (FIG. 11).
(Nu) The form for carrying out the present invention is not limited to a closed container having a cross-sectional structure as shown in FIGS. 10 and 11, and even if the container is partially opened as shown in FIG. Propulsion is generated if there is a disk that rotates in a flowing state (with a blade on one side and a smooth surface on the other) and the power to rotate each.
(Le) However, in the case of (N), efficiency and capacity are reduced compared to the case of an airtight container.
1 羽根が付いた円盤を回転させる回転軸
2 羽根が付いた円盤
3 羽根が付いていない円盤
4 羽根
5 再循環する流体が通るための穴部
6 円盤を回転させる動力
7 流体を再循環させる動力
8 流体を再循環させるプロペラ
9 密閉容器の外側の板
10 流体の流れる状態・方向
11 流体を再循環させるプロペラの回転軸
12 円柱1 Rotating shaft for rotating a disk with
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JP2014152356A JP2016017520A (en) | 2014-07-08 | 2014-07-08 | Engine with no-reactive driving force |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106642644A (en) * | 2016-11-16 | 2017-05-10 | 上海贵鸣新能源科技有限公司 | Multi-energy-source constant-temperature water supply system |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4882242A (en) * | 1972-02-07 | 1973-11-02 | ||
JPS51106990A (en) * | 1975-03-15 | 1976-09-22 | Masatada Naito | MUHANDOSUISHINKIKAN |
EP0042453A1 (en) * | 1980-06-24 | 1981-12-30 | Erich Pröschel | Gravitation-force motor |
JPS58214681A (en) * | 1982-06-07 | 1983-12-13 | Yukutada Naito | Reaction-less propelling engine |
EP0545280A1 (en) * | 1991-12-02 | 1993-06-09 | Willi Maurer | Drive mechanism |
WO2008044967A1 (en) * | 2006-10-09 | 2008-04-17 | Lev Nikolaevich Khomyakov | Method for producing additional power by the multiple conversion thereof in a closed circuit for circulating a working body and a device for carrying g out said method |
US20130156566A1 (en) * | 2009-12-31 | 2013-06-20 | Gilbert LY | High-efficiency thruster independentof the outside environment |
-
2014
- 2014-07-08 JP JP2014152356A patent/JP2016017520A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4882242A (en) * | 1972-02-07 | 1973-11-02 | ||
JPS51106990A (en) * | 1975-03-15 | 1976-09-22 | Masatada Naito | MUHANDOSUISHINKIKAN |
EP0042453A1 (en) * | 1980-06-24 | 1981-12-30 | Erich Pröschel | Gravitation-force motor |
JPS58214681A (en) * | 1982-06-07 | 1983-12-13 | Yukutada Naito | Reaction-less propelling engine |
EP0545280A1 (en) * | 1991-12-02 | 1993-06-09 | Willi Maurer | Drive mechanism |
WO2008044967A1 (en) * | 2006-10-09 | 2008-04-17 | Lev Nikolaevich Khomyakov | Method for producing additional power by the multiple conversion thereof in a closed circuit for circulating a working body and a device for carrying g out said method |
US20130156566A1 (en) * | 2009-12-31 | 2013-06-20 | Gilbert LY | High-efficiency thruster independentof the outside environment |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106642644A (en) * | 2016-11-16 | 2017-05-10 | 上海贵鸣新能源科技有限公司 | Multi-energy-source constant-temperature water supply system |
CN106642644B (en) * | 2016-11-16 | 2022-02-18 | 康贵明 | Multi-energy constant-temperature water supply system |
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