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특허 상세정보

Aircraft aerodynamic surface with trailing edge deflector

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50    B64C-021/00   
미국특허분류(USC) 244/215; 244/075.A; 244/212
출원번호 US-0958356 (2002-03-27)
우선권정보 FR-0004777 (1999-04-16)
국제출원번호 PCT/FR00/00864 (2000-04-06)
국제공개번호 WO00/63071 (2000-10-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Stevens, Davis, Miller & Mosher, LLP
인용정보 피인용 횟수 : 22  인용 특허 : 2
초록

An aerodynamic surface, such as a wing, empennage, angle of drift, nacelle pylon and the like for an aircraft includes at least one lightening hole pertaining to the trailing edge of the underwing, at least one hinged baffle that can be mounted in the lightening hole of the underwing, whereby the chord thereof is equal to a several hundredths of the chord of the aerodynamic surfacer and an actuator for the moveable baffle so that it can rotate around the hinge line.

대표
청구항

1. An aircraft aerodynamic surface comprising a reduced-pressure face and a pressure face which are connected together, at the front, by a leading edge and, at the rear, by a trailing edge, and at least one moving deflector articulated via its front part about an axis at least essentially parallel to said trailing edge so as to be able to pivot about said axis of articulation under the action of actuating means, wherein: a chord of said at least one deflector is equal to a few hundredths of a chord of said aerodynamic surface; said at least one movin...

이 특허를 인용한 특허 피인용횟수: 22

  1. Brewer, Paul R.; Shorcoll, Steven; Raval, Reg R.. Active gurney flap. USP2013128616504.
  2. Brewer, Paul R.; Shorcott, Steven; Raval, Reg R.. Active gurney flap. USP2014068757557.
  3. Brewer, Paul R.; Shorcott, Steven; Raval, Reg R.. Active gurney flap. USP2014048695926.
  4. Reckzeh, Daniel; Schlipf, Bernhard; Andreani, Luc; Sutcliffe, Mark. Advanced trailing edge control surface on the wing of an aircraft. USP2012128336829.
  5. Friedel, Hendrik; Zapf, Bodo. Aerodynamic body with an ancillary flap. USP2015018925869.
  6. Gessler, Andreas; Hansen, Heinz; Havar, Tamas; Horoschenkoff, Alexander. Aerodynamic profile with an adjustable flap. USP2005036863245.
  7. Mahmoudi, Amirhossein; Alizadeh Salimi, Firouz. Flap device. USP2011027891612.
  8. Subramaniyan, Moorthi; Chengappa, Manjunath Bangalore; Patel, Pradeep. Gas turbine diffuser strut including a trailing edge flap and methods of assembling the same. USP20181210151325.
  9. Prince, Troy S.; Kolacinski, Richard; Patel, Mehul. Hierarchical closed-loop control system for aircraft, missiles and munitions. USP2012058190305.
  10. Butler, Clark M.; Gilchrist, Ian J.. Inverted airfoil pylon for an aircraft. USP2010087770841.
  11. Butler, Clark M.; Gilchrist, Ian J.. Inverted airfoil pylon for an aircraft. USP2014018632032.
  12. Butler, Clark M.; Gilchrist, Ian J.. Inverted airfoil pylon for an aircraft. USP2012018091824.
  13. Berthereau, Mathieu; Mazet, Michel. Method and device for an aircraft buffet reduction. USP2012068191832.
  14. Burgunder, Samuel; Guering, Bernard. Method and device for fitting out an aircraft nose compartment in an avionics bay. USP2018019878790.
  15. Hoeffler, James P.; Fernandez, Joseph M.; Nasoff, Marc S.. Microarray and uses therefor. USP2010097794946.
  16. Hoeffler, James P.; Fernandez, Joseph M.; Nasoff, Marc S.. Microarrays and uses therefor. USP2014018637264.
  17. Hoeffler, James; Fernandez, Joseph; Nasoff, Marc. Microarrays and uses therefor. USP2011098012703.
  18. Lee,Hak Tae; Bieniawski,Stefan R.; Kroo,Ilan M.. Miniature trailing edge effector for aerodynamic control. USP2008087410133.
  19. Jamison, Flint M.; Amorosi, Stephen R.; Klein, Michael K.. Slidable divergent trailing edge device. USP2016109463869.
  20. Vassberg, John Charles; Gregg, III, Robert D.. Variable trailing edge geometry and spanload control. USP2005016843452.
  21. Schroeder, Karsten. Wing arrangement comprising an adjustable flap and fairing element for covering a flap adjustment mechanism of a wing. USP2013078474763.
  22. Irving,Jan; Davies,Robert. Wing tip device. USP2007107275722.