FR1496152A - Tuyère pour aile d'avion ou pale d'hélicoptère soufflée - Google Patents

Tuyère pour aile d'avion ou pale d'hélicoptère soufflée

Info

Publication number
FR1496152A
FR1496152A FR66167A FR66167A FR1496152A FR 1496152 A FR1496152 A FR 1496152A FR 66167 A FR66167 A FR 66167A FR 66167 A FR66167 A FR 66167A FR 1496152 A FR1496152 A FR 1496152A
Authority
FR
France
Prior art keywords
jet
flap
flaps
vary
axis
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.)
Expired
Application number
FR66167A
Other languages
English (en)
Inventor
Pierre Rene Leon Bernar Dorand
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 FR66167A priority Critical patent/FR1496152A/fr
Priority to DE19671506591 priority patent/DE1506591B1/de
Priority to GB27652/67A priority patent/GB1174496A/en
Priority to US647509A priority patent/US3456904A/en
Application granted granted Critical
Publication of FR1496152A publication Critical patent/FR1496152A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/325—Circulation-control rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/08—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/16—Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/28—Boundary layer controls at propeller or rotor blades
    • 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
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Turbines (AREA)
  • Air-Flow Control Members (AREA)
FR66167A 1966-06-20 1966-06-20 Tuyère pour aile d'avion ou pale d'hélicoptère soufflée Expired FR1496152A (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR66167A FR1496152A (fr) 1966-06-20 1966-06-20 Tuyère pour aile d'avion ou pale d'hélicoptère soufflée
DE19671506591 DE1506591B1 (de) 1966-06-20 1967-06-14 Schlitzduese,insbesondere fuer die Hinterkante von Flugzeugtragflaechen und Drehfluegeln
GB27652/67A GB1174496A (en) 1966-06-20 1967-06-15 Jet Flap Control.
US647509A US3456904A (en) 1966-06-20 1967-06-20 Jet flap control

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR66167A FR1496152A (fr) 1966-06-20 1966-06-20 Tuyère pour aile d'avion ou pale d'hélicoptère soufflée

Publications (1)

Publication Number Publication Date
FR1496152A true FR1496152A (fr) 1967-09-29

Family

ID=8611345

Family Applications (1)

Application Number Title Priority Date Filing Date
FR66167A Expired FR1496152A (fr) 1966-06-20 1966-06-20 Tuyère pour aile d'avion ou pale d'hélicoptère soufflée

Country Status (4)

Country Link
US (1) US3456904A (fr)
DE (1) DE1506591B1 (fr)
FR (1) FR1496152A (fr)
GB (1) GB1174496A (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3940092A (en) * 1974-11-07 1976-02-24 The Boeing Company Jet flow deflector for aircraft
US6079672A (en) * 1997-12-18 2000-06-27 Lam; Lawrence Y. Aileron for fixed wing aircraft
RU2220072C1 (ru) * 2002-06-07 2003-12-27 Дябин Николай Васильевич Самолет с плоским хвостовым оперением
US7837141B2 (en) * 2006-03-22 2010-11-23 The Boeing Company Reaction drive rotor/wing variable area nozzle
DE102007009060A1 (de) * 2007-02-23 2008-08-28 Airbus Deutschland Gmbh Spoiler für eine aerodynamisch wirksame Fläche eines Luftfahrzeugs
FR2948628B1 (fr) * 2009-08-03 2012-02-03 Airbus Operations Sas Avion a controle en lacet par trainee differentielle
CN102745329A (zh) * 2012-08-08 2012-10-24 南昌航空大学 涡流旋翼式飞行器
US9464532B2 (en) * 2013-03-05 2016-10-11 Bell Helicopter Textron Inc. System and method for reducing rotor blade noise
US9243622B2 (en) * 2013-05-22 2016-01-26 The Boeing Company Bellows synthetic jet

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2617487A (en) * 1948-09-30 1952-11-11 Edward A Stalker Wing for helicopters and other aircraft
US3102704A (en) * 1955-10-05 1963-09-03 Ii Roger W Griswold Airfoil jet reaction control means

Also Published As

Publication number Publication date
US3456904A (en) 1969-07-22
GB1174496A (en) 1969-12-17
DE1506591B1 (de) 1970-01-22

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