JP2007218240A - Thrust force and buoyancy increasing machine - Google Patents

Thrust force and buoyancy increasing machine Download PDF

Info

Publication number
JP2007218240A
JP2007218240A JP2006075587A JP2006075587A JP2007218240A JP 2007218240 A JP2007218240 A JP 2007218240A JP 2006075587 A JP2006075587 A JP 2006075587A JP 2006075587 A JP2006075587 A JP 2006075587A JP 2007218240 A JP2007218240 A JP 2007218240A
Authority
JP
Japan
Prior art keywords
fan
cylinder
rotating shaft
edge
air
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2006075587A
Other languages
Japanese (ja)
Inventor
Yoshioki Tomoyasu
良興 友安
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP2006075587A priority Critical patent/JP2007218240A/en
Publication of JP2007218240A publication Critical patent/JP2007218240A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To efficiently improve rotational power of a fan installed on a rotating shaft. <P>SOLUTION: A truncated cylindrical cover with the edge turning outward is attached on a motor and an engine to generate a differential pressure by attracting force. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

従来、モーターやエンジンは出力の効率が悪く、その為、排ガスが多く、又、燃費が悪い為それらを適用した自動車が環境汚染を起し環境破壊が進んでいる。Conventionally, motors and engines have poor output efficiency, and therefore have a lot of exhaust gas, and fuel consumption is poor, so automobiles to which they are applied have caused environmental pollution and environmental destruction has progressed.

当該技術The technology

当該技術は、モーターやエンジンに円錐台形のシリンダーの覆いをつけて気流の差圧でファンの回転運動を加速させて省エネと排ガス低減させる推力及び浮力増大器で面積の広いシリンダーの出口の縁を外側に突出させてその裏側の壁を反らせてシリンダーの壁に沿って流れる気流を迂回させて、シリンダーの境界付近に差圧を低下させない仕組と複数のファンを設置して加速力を増大させる仕組。In this technology, a motor or engine is covered with a frustoconical cylinder, and the rotational movement of the fan is accelerated by the differential pressure of the air flow to save energy and reduce exhaust gas. A mechanism that protrudes outward and deflects the back wall to bypass the airflow that flows along the cylinder wall, and a mechanism that does not reduce the differential pressure near the cylinder boundary and a mechanism that increases the acceleration force by installing multiple fans .

当該推力及び浮力増大器は、地上と空中での出力を増大させることを可能にする為、ヘリコプターより遥かに簡便な空中車と又、スカイクレーン車を実現化可能な為橋や高速道ひいては港湾設備等の社会施設を必要としなくなります。Since the thrust and buoyancy increaser can increase the output on the ground and in the air, the aerial vehicle that is much simpler than the helicopter and the sky crane vehicle can be realized. No need for social facilities such as equipment.

当該推力及び浮力増大器を導入したモーターの断面図の一例An example of a sectional view of a motor with the thrust and buoyancy increaser introduced

符号の説明Explanation of symbols

1.円錐台形シリンダー 2.No.1プロペラー 3.No,2プロペラー
4.縁 5.出口 6.固定子
7.回転子 8.流体 9.回転軸
1. Frustoconical cylinder 1. No. 1 propeller No, 2 propeller4. Edge 5. Exit 6. Stator 7 Rotor 8. Fluid 9 Axis of rotation

Claims (5)

モーター又はエンジンの出力を増大させる補助装置として回転軸に元々設置されているかその延長上に新たにファンを設置して、そのファンを円筒台形で且つ直径の大きい方の末端の縁が外側に反っているシリンダーで囲むことによって発生するシリンダーの内と外の気圧差による引力で、ファンの回転運動を促進するように作用して動力負荷を削減させ省エネと駆動力を増大させる方法。As a supplementary device to increase the output of the motor or engine, it is originally installed on the rotating shaft or a new fan is installed on the extension, and the fan has a cylindrical trapezoidal shape and the edge of the larger end warps outward. A method of reducing energy consumption and driving power by reducing the power load by acting to promote the rotational movement of the fan by the attractive force due to the pressure difference between the inside and outside of the cylinder generated by surrounding the cylinder. 上記(請求項1)に於いて、シリンダーの末端の縁を外側に反らせることによりシリンダーの外側の壁に沿って流れる気流がシリンダー外部の薄い気圧の層に流れ込んで上記ファンの回転運動を促進する引力を上記縁の裏側で気流の方向を迂回させ引力を弱めない構造。In the above (Claim 1), the air flow flowing along the outer wall of the cylinder flows into the thin air pressure layer outside the cylinder by bending the edge of the end of the cylinder outward to promote the rotational movement of the fan. A structure that does not weaken the attractive force by bypassing the direction of airflow at the back of the edge. 上記請求項の1及び2を適用したモーター又はエンジンを自動車に適用して出力を高め省エネをはかり且つ、排ガスを低減させる他、電気自動車を実用化に利用する。The motor or engine to which the above claims 1 and 2 are applied is applied to an automobile to increase the output, save energy, reduce exhaust gas, and use an electric automobile for practical use. 上記請求項1及び2及び3において、回転軸に複数のファンを取付け、そのうちのファンの回転を逆向きに回転させて、直ぐ前のファンの回転力の反作用を果たす空気層を作成する。又、動力に連動する回転軸の前方に別のファンを設置して、空気層の希薄化を一層促進することによって引力を強めて、更に、高出力化と省エネ化を促進する方法。In the first, second, and third aspects, a plurality of fans are attached to the rotating shaft, and the rotation of the fans is rotated in the opposite direction, thereby creating an air layer that counteracts the rotational force of the immediately preceding fan. In addition, another fan is installed in front of the rotating shaft linked to the power to further increase the attractive force by further promoting the dilution of the air layer, and further increase the output and save energy. 上記請求項のファン又はプロペラを自動車の屋根上に縦に設置して同じく上記シリンダーで囲うことにより高出力化し、ヘリコプターを小型簡素化にすることによって垂直離発着可能な空中車と尚且つ空中でクレイン作業を可能にすスカイクレインの製作可能にする推力及び浮力増大器。By installing the fan or propeller of the above claim vertically on the roof of an automobile and enclosing it with the cylinder, the power can be increased, and the helicopter can be reduced in size and simplified so that it can be separated from an aerial vehicle capable of vertical takeoff and landing, and still is a crane in the air. Thrust and buoyancy increaser that enables the production of sky cranes that enable work.
JP2006075587A 2006-02-20 2006-02-20 Thrust force and buoyancy increasing machine Pending JP2007218240A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2006075587A JP2007218240A (en) 2006-02-20 2006-02-20 Thrust force and buoyancy increasing machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2006075587A JP2007218240A (en) 2006-02-20 2006-02-20 Thrust force and buoyancy increasing machine

Publications (1)

Publication Number Publication Date
JP2007218240A true JP2007218240A (en) 2007-08-30

Family

ID=38495787

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006075587A Pending JP2007218240A (en) 2006-02-20 2006-02-20 Thrust force and buoyancy increasing machine

Country Status (1)

Country Link
JP (1) JP2007218240A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020118505A (en) * 2019-01-22 2020-08-06 エスペック株式会社 Environment formation device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2020118505A (en) * 2019-01-22 2020-08-06 エスペック株式会社 Environment formation device
JP7246942B2 (en) 2019-01-22 2023-03-28 エスペック株式会社 Environment forming device

Similar Documents

Publication Publication Date Title
CN109279002B (en) VTOL vehicles with fan blades outside of the exhaust flow path
JP6715884B2 (en) Aircraft propulsion system
EP3964438B1 (en) Hybrid aircraft propulsion system
CN109204842B (en) Propulsion system for an aircraft
US8562284B2 (en) Propulsive fan system
JP4115902B2 (en) Electric auxiliary auxiliary and emergency drive
JP2019031271A (en) Hybrid-electric propulsion system for aircraft
US11448189B2 (en) Power generation and propulsion architecture using fluid flow
JP2016135671A (en) Gas-electric propulsion system for aircraft
JP2019048616A (en) Propulsion system for aircraft
CN109071030A (en) Propelling motor for aircraft
BR112015007799B1 (en) UNPLUGGED PUSH PRODUCTION SYSTEM
JP2017072136A (en) Engine having variable pitch outlet guide vanes
CN109110135A (en) Propulsion system for aircraft
JP4305518B2 (en) Chip turbine drive fan
EP3569857B1 (en) Electric ducted fan
CA3008406A1 (en) Propulsion system for an aircraft
US9181900B1 (en) Fully advanced superconducting segmented turbo-electric rotormachine (fasster)
EP2939929B1 (en) Multi-axis accessory gearboxes of mechanical drive systems and gas turbine engines including the same
CN112930436A (en) Turbine with unducted twin propeller
JP2007522997A (en) Auxiliary drive by changing the direction of fluid flow
CN106357051A (en) Wheel hub motor driving system with internal and external circulating airway cooling structure
US8794902B1 (en) System and method to improve the exhaust pressure across a RAM air turbine through secondary flow mixing
JP2007218240A (en) Thrust force and buoyancy increasing machine
WO2015191017A1 (en) Propeller with super conductive electrical motor for air vehicles