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특허 상세정보

Moveable leading edge device for a wing

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/214; 244/216; 244/217
출원번호 US-0505065 (2009-07-17)
등록번호 US-8534611 (2013-09-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Yee & Associates, P.C.
인용정보 피인용 횟수 : 6  인용 특허 : 22
초록

A method and apparatus for managing a flight control surface system. A leading edge section on a wing of an aircraft is extended into a deployed position. A deformable section connects the leading edge section to a trailing section. The deformable section changes from a deformed shape to an original shape when the leading edge section is moved into the deployed position. The leading edge section on the wing is moved from the deployed position to an undeployed position. The deformable section changes to the deformed shape inside of the wing.

대표
청구항

1. An apparatus comprising: a leading edge section;a trailing section, the trailing section comprising an upper skin and a lower skin, the leading edge section and the upper skin being discontinuous, the leading edge section and the lower skin being discontinuous; anda deformable section connecting the leading edge section to the trailing section, the deformable section comprising an upper deformable section and a lower deformable section, the upper deformable section positioned between the leading edge section and the upper skin, the lower deformable se...

이 특허에 인용된 특허 (22)

  1. Broadbent, Michael Craig. Contiguous variable camber device. USP2004016682023.
  2. Rao Dhanvada M. (Yorktown VA). Control configured vortex flaps. USP1992035094411.
  3. Larssen, Jon V.; Calkins, Frederick T.. Deployable flap edge fence. USP2010077753316.
  4. Broadbent, Michael Craig. Deployment system for a moveable wing surface. USP2005126974112.
  5. Bliesner Wayne T.. Leading edge slat/wing combination. USP1998115839699.
  6. Bliesner Wayne T. (Snohomish WA). Leading edge slat/wing combination. USP1996085544847.
  7. Joyce Michael A. (Balderstone GB3) Thompson William (Bury GB3). Manufacture of aircraft track-cans and the like. USP1993065222653.
  8. Gleine, Wolfgang; Mau, Knut; Carl, Udo. Pressure control system for a pressure-expandable displacement element. USP2003036536714.
  9. Wood, Jeffrey H.; Dunne, James P.. Shape changing airfoil system. USP2012098256719.
  10. Ingram Richard B. (Ithaca NY) Gerardi Joseph J. (Dryden NY). Shape memory alloy de-icing technology. USP1997115686003.
  11. Ellmers Wilfried (Achim DEX) Martens Wilhelm (Delmenhorst DEX). Slat actuation and steering. USP1990044915327.
  12. Dizdarevic Faruk. Slot forming segments and slot changing spoilers. USP2001126328265.
  13. Lorkowski, Thomas; Grohmann, Boris. System for reducing aerodynamic noise at a supplementary wing of an aircraft. USP2010087766281.
  14. Wayne T. Bliesner. Tailored wing assembly for an aircraft moveable slat system. USP2002086435458.
  15. Zimmer Herbert (Friedrichshafen DEX). Transverse force-connected body with variable profiling, particularly an airplane wing. USP1981024252287.
  16. Roglin Robert L. (Duluth GA) Hanagud Sathyanaraya (Atlanta GA). Variable camber control of airfoil. USP1992095150864.
  17. Zapel Edwin J. (Box 433 Maple Valley WA 98038). Variable camber leading edge for airfoil. USP1979104171787.
  18. Rudolph Peter K. C. (Seattle WA). Vortex leading edge flap assembly for supersonic airplanes. USP1997105681013.
  19. Cole James B. (Mercer Island WA). Wind edge movable airfoil having variable camber. USP1987034650140.
  20. Hinkleman Michael J.. Wing leading edge flap and method therefor. USP1999075927656.
  21. Evans Arthur (Seattle WA). Wing leading edge slat. USP1983084399970.
  22. Grohmann, Boris; Reichenberger, Johann; Lorkowski, Thomas. Wing of an aircraft. USP2012068191835.