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특허 상세정보

Aircraft wing flaps

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/34    B64C-023/06   
미국특허분류(USC) 244/199 ; 244/203 ; 244/213
출원번호 US-0856844 (1997-05-15)
발명자 / 주소
대리인 / 주소
인용정보 피인용 횟수 : 16  인용 특허 : 7

A wing assembly has a wing and at least one slender delta shaped flap with sharp leading edges pointing into the flow direction and deployable above the upper wing surface close to the quarter line of the wing for providing significantly enhanced lift and maneuverability to an aircraft. In normal flight the delta flaps are retracted into the wing such that the upper surface of the delta flaps become part of the upper surface of the wing. If higher lift is required or the wing has stalled, the delta flaps are deployed at an angle of attack into the high e...


[ Having thus set forth the nature of the invention, what is claimed herein is:] [1.] A flight lifting surface assembly for aircraft comprising in combination, a wing including upper and lower surfaces extending lengthwise intermediate a leading edge and a trailing edge and at least one flap, said flap having a delta shaped configuration including an apex extending into the flow, a pair of leading edges extending from the apex and terminating at a trailing edge, said flap having upper and lower surfaces converging at a small angle to define sharp leading...

이 특허를 인용한 특허 피인용횟수: 16

  1. Glezer, Ari; DeSalvo, Michael Edward. Airfoil performance modification using synthetic jet actuators. USP2010117823839.
  2. Thombi Layukallo JP. Control of flow separation and related phenomena on aerodynamic surfaces. USP2002116484971.
  3. Craig L. Streett ; John C. Lin. Device and method for reducing aircraft noise. USP2002106471157.
  4. Bernhardt, Roger D.. Flow control structure and associated method for controlling attachment with a control surface. USP2015119193436.
  5. Norman Sherman. Funneled rotary foil. USP2002106457671.
  6. Hamilton, Terry Wayne. Hamilton H.N2 laminar flow diskette wing. USP2013028382040.
  7. Batcho Paul F.. Method and apparatus for mitigating junction flows. USP2001026186445.
  8. Huenecke, Klaus. Method and apparatus for reducing trailing vortices in the wake of an aircraft. USP2003026513761.
  9. Ingo Borchers DE; Roger Drobietz DE; Michael Gruenewald DE; Knut Mau DE; Johann Reichenberger DE. Noise reducing vortex generators on aircraft wing control surfaces. USP2002126491260.
  10. Lang, James D.. Reducing runway requirement for aircraft. USP2011087997528.
  11. Mangalam Sivaramakrishman M.. Self-actuated flow control system. USP2000096123296.
  12. Lang Renee M. ; Blaisdell George L.. Self-aligning vortex snow fence. USP2000046053479.
  13. Gionta, Matthew; Karkow, Jon; Roncz, John; Koehler, Dieter; Lednicer, David. Spin resistant aircraft configuration. USP2018039926071.
  14. Gionta, Matthew; Karkow, Jon; Roncz, John; Koehler, Dieter; Lednicer, David. Spin resistant aircraft configuration. USP2016059327828.
  15. Janardan, Bangalore Ananthamurthy; Brausch, John Francis. Stub airfoil exhaust nozzle. USP2003016502383.
  16. Emunds, Rolf. Wing comprising a flow fence, and aircraft having such wings. USP2014128910910.