WO2003008801A1 - Systeme de turbine a ailettes bidimentionnelles a portance - Google Patents

Systeme de turbine a ailettes bidimentionnelles a portance Download PDF

Info

Publication number
WO2003008801A1
WO2003008801A1 PCT/JP2001/006159 JP0106159W WO03008801A1 WO 2003008801 A1 WO2003008801 A1 WO 2003008801A1 JP 0106159 W JP0106159 W JP 0106159W WO 03008801 A1 WO03008801 A1 WO 03008801A1
Authority
WO
WIPO (PCT)
Prior art keywords
lift
dimensional
wing
blade
turbine
Prior art date
Application number
PCT/JP2001/006159
Other languages
English (en)
Japanese (ja)
Inventor
Kosuke Ota
Original Assignee
Kosuke Ota
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 Kosuke Ota filed Critical Kosuke Ota
Priority to PCT/JP2001/006159 priority Critical patent/WO2003008801A1/fr
Publication of WO2003008801A1 publication Critical patent/WO2003008801A1/fr

Links

Classifications

    • 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
    • F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/40—Use of a multiplicity of similar components
    • 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
    • Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction

Definitions

  • the present invention relates to a lift turbine system that generates aerodynamic lift using a blade and converts the generated lift into a rotational force to turn a generator, and more particularly to a lift turbine system using a wide wing span of a two-dimensional blade.
  • the inventor has filed a lift energy system with PCT application date, May 12, 2000, PCT application number PCTZ JP 00/03047.
  • One energy source of this lift energy system is a lift tarpin system that drives an automatic rotor to advance in the atmosphere and causes autorotation with lift that acts on the wing, and turns the generator with the resulting torque.
  • This lift turbine has many advantages such as 10,000 times the capacity of a wind turbine, and the ability to simultaneously produce and supply clean power, and is expected for early commercialization.
  • fixed wings are also widely used, and the main wing of an aircraft is a fixed wing.
  • the advantage of fixed wings is that a wide wing, a large wing area, and high-speed motion generate a large amount of lift.
  • the wing of an airplane is a lifting device that lifts the airframe and heavy objects, so the wing is used horizontally to generate upward lift, but when using the wing as a lift generating device other than for flight purposes, lift is It is possible to generate in the horizontal direction and convert the generated lift into a rotational force.
  • the present invention aims to provide a fixed blade utilization lift turbine system focusing on the lift mass generation capability of an aircraft wing, and to provide it as an energy source of a lift energy system together with a rotary blade utilization lift turbine of the prior application. Disclosure of the invention
  • the fixed wing of the wing of a fixed wing aircraft is vertically erected, and the upper and lower sides of the wing are fixed to the ceiling and floor of the wind tunnel to form a two-dimensional wing,
  • Two-dimensional bladed turbines having a two-dimensional design, and a number of cyclical Gottingen type wind tunnels including a turbine blade and a fan in a wind tunnel, an annular wind tunnel arranged in an annular shape, a lifting turbine and a ring wind tunnel are suspended and fixed.
  • It consists of a rotating frame that rotates horizontally around the central axis, a gear mechanism, a generator mechanism, and an operation control mechanism, and it circulates with a strong wind with a blower and blows a strong wind at the wing leading edge. It is a two-dimensional wing lift turbine system characterized by generating lift in the same tangential direction, rotating a bin, rotating the generator with the torque obtained, and generating electricity.
  • Two-dimensional wings are used in the present invention. Two-dimensional wings with infinitely long wings do not exist in reality, but in a wind tunnel, they can create conditions close to that. This wing is called a two-dimensional wing, and the wing of an airplane with a finite wing width is called a three-dimensional wing. Comparing the two-dimensional and three-dimensional wings, there is no essential difference in achieving the lift coefficient, but there is a critical difference in terms of airflow turbulence and drag. In two-dimensional wings, theoretically there is no induced drag due to trailing vortices and lifting forces due to tip vortices that can not be avoided with three-dimensional wings.
  • the lift force divided by the drag force ie, the lift-to-drag ratio
  • the lift-drag ratio of this two-dimensional wing is much larger than that of a three-dimensional wing, and it is only a wing that does not have an airframe or tail wing that increases resistance, so the lift-drag ratio is even larger.
  • the absence of turbulence in the air flow around the wing of the two-dimensional wing can reduce the cross-sectional area of the wind tunnel, and the air flow rate is inversely proportional to the cross-sectional area.
  • the lift force L acting on the fixed wing can be obtained by the following equation.
  • Airspeed is the air velocity created by the blower and the speed increasing device, and corresponds to the flight speed of the aircraft.
  • the plane In order to fly, the plane must be propelled by a jet engine or propeller, but in the present invention, the wind created by the blower is that, and the input is the horsepower of an electric or hydraulic motor.
  • the torque obtained by this two-dimensional wing lifting power bin is the product of the lift generated on each wing and the arm length of the couple, and the product of the number of wings. Also, the power factor is the product of torque and angular velocity.
  • the amount of lift generated on the turbine blades is large compared to the total amount of output when dozens of airplanes are simultaneously operating, and because the couple arm of the turbine is long, the torque obtained is very large.
  • Fig. 1 shows the entire configuration, in which 11A is a longitudinal sectional view and 11B is a transverse sectional view.
  • Fig. 1 _A 1 1 B is the rotating frame 2 that rotates horizontally around the fixed central axis 1
  • An annular wind tunnel 3 is suspended, and a two-dimensional wing is fixedly installed in the straight wind path of the wind tunnel, and it is shown that a tarpin is formed in an annular shape.
  • the Göttingen-type wind tunnel 3 is a circulating system consisting of a straight air path and a curved air path, and a two-dimensional wing 4 and a speed increasing device 5 in the straight air path, and a blower 6 and a blower 6 in the curved air path. It has a guide vane 7 and built-in.
  • the straight air paths are all radially directed to the central axis, and the air flow is also radial.
  • the blower 6 illustrates the case where the axial fan is taken in the longitudinal direction, and the longitudinal air path is divided by several horizontal walls.
  • the two-dimensional wing 4 is turned to the left and right as shown in Fig. 1B, because the circulating flow is always received at the wing leading edge to generate lift in the same tangential direction. Both wings are located at equal distances from the center of pressure.
  • Fig. 1B shows the case where one wing is placed in the straight air path, but it can be increased to two or three.
  • the mechanisms that make up this system are all made of lightweight materials and are made extremely lightweight.
  • the gear mechanism 8 and the power generation mechanism 9 which are heavy objects are fixed near the central axis, and the operation control mechanism 10 is installed on the ground.
  • the present invention generates a large amount of lift using a large number of two-dimensional blades, converts the generated lift into a rotational force and turns the generator, and generates power without combustion, clean, no fuel, and very low cost. It can be mass-produced and supplied, and it can be used to protect the global environment and solve energy problems.

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

L'invention concerne un système de turbine à ailettes bidimentionnelles à portance utilisant une portance capable de produire une portance aérodynamique à l'aide d'ailettes et de convertir la portance générée en force de rotation afin de faire tourner un générateur pour obtenir de l'énergie. Ledit système de turbine comprend une pluralité d'ailettes bidirectionnelles disposées en anneau, chacune d'elles étant formée par placement vertical d'une ailette fixe de taille égale à celle d'une aile d'aéronef et par fixation des côtés supérieur et inférieur de ladite ailette au plafond et au plancher d'une soufflerie de façon à utiliser l'aptitude de l'aile d'aéronef à produire une portance élevée; et une soufflerie annulaire formée par placement annulaire d'un certain nombre de souffleries du type Göttingen associées les unes aux autres afin de produire simultanément une grande quantité d'énergie électrique. Cette énergie propre peut être produite partout, à tout moment et en quantité quelconque sans utiliser de combustible. Elle est également produite et fournie directement à des sites d'utilisateurs finaux, de manière stable et à faible taux de consommation.
PCT/JP2001/006159 2001-07-17 2001-07-17 Systeme de turbine a ailettes bidimentionnelles a portance WO2003008801A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/JP2001/006159 WO2003008801A1 (fr) 2001-07-17 2001-07-17 Systeme de turbine a ailettes bidimentionnelles a portance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2001/006159 WO2003008801A1 (fr) 2001-07-17 2001-07-17 Systeme de turbine a ailettes bidimentionnelles a portance

Publications (1)

Publication Number Publication Date
WO2003008801A1 true WO2003008801A1 (fr) 2003-01-30

Family

ID=11737554

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2001/006159 WO2003008801A1 (fr) 2001-07-17 2001-07-17 Systeme de turbine a ailettes bidimentionnelles a portance

Country Status (1)

Country Link
WO (1) WO2003008801A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8215659B2 (en) 2007-06-28 2012-07-10 Kaestle Gmbh Ski

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5648701B2 (fr) * 1977-07-07 1981-11-17
JPH0129990B2 (fr) * 1980-06-27 1989-06-15 Mitsubishi Electric Corp

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5648701B2 (fr) * 1977-07-07 1981-11-17
JPH0129990B2 (fr) * 1980-06-27 1989-06-15 Mitsubishi Electric Corp

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8215659B2 (en) 2007-06-28 2012-07-10 Kaestle Gmbh Ski

Similar Documents

Publication Publication Date Title
US4936748A (en) Auxiliary power source in an unducted fan gas turbine engine
CN104755703B (zh) 无涵道的推力产生系统
US4917332A (en) Wingtip vortex turbine
US9409643B2 (en) Helicopter with cross-flow fan
US8461713B2 (en) Adaptive control ducted compound wind turbine
EP3964438B1 (fr) Système de propulsion d'aéronef hybride
US4045144A (en) Wind energy concentrators
CN107672802B (zh) 开槽涵道式卷流旋翼飞行器
KR20130014452A (ko) 전환식 항공기
KR20130014453A (ko) 전환식 항공기
US11939060B2 (en) Lift nacelle
CA3060758C (fr) Aeronef a soufflante canalisee rotative
KR101067017B1 (ko) 끝단의 후퇴각을 능동적으로 변동시킬 수 있는 회전익항공기용 회전익
Murugan et al. Concept study for adaptive gas turbine rotor blade
WO2003008801A1 (fr) Systeme de turbine a ailettes bidimentionnelles a portance
US6457671B1 (en) Funneled rotary foil
US6602054B1 (en) Fluid motor apparatus for amplifying thrust
CN205445823U (zh) 一种涵道流体推进装置
CN117842349A (zh) 一种产生升力的结构及方法
BG113193A (bg) Устройство за създаване на подемна и теглителна сила, на принципа на симетричното обтичане на махаща пластина във въздушен поток, при летателните апарати с вертикално излитане и кацане и за генериране на електрическа мощност при вятърните и водни генератори
CN117284475A (zh) 一种垂直风车式直升机
CN113320687A (zh) 一种旋翼螺旋桨装置
KR20190032034A (ko) 보조 블레이드를 갖는 수평축 풍력발전기 및 이의 작동 방법
GB2264679A (en) Vtol aircraft.
Karna et al. Ducted Fan Flyer-Design Overview and Roll Moment Control

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NO NZ PL PT RO RU SD SE SG SI SK SL TJ TM TR TT TZ UA UG US UZ VN YU ZA ZW

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG US

Kind code of ref document: A1

Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
REG Reference to national code

Ref country code: DE

Ref legal event code: 8642

122 Ep: pct application non-entry in european phase
NENP Non-entry into the national phase

Ref country code: JP