• 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Method and apparatus for a leading edge slat on a wing of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/214; 244/215
출원번호 US-0505061 (2009-07-17)
등록번호 US-8534610 (2013-09-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Yee & Associates, P.C.
인용정보 피인용 횟수 : 2  인용 특허 : 22

A method and apparatus for managing a flight control surface system. A leading edge device is moved on a leading edge from an undeployed position to a deployed position. The leading edge device has an outer surface, an inner surface, and a deformable fairing attached to the leading edge device such that the deformable fairing covers at least a portion of the inner surface. The deformable fairing changes from a deformed shape to an original shape when the leading edge device is moved to the deployed position. The leading edge device is then moved from the...


1. An apparatus comprising: a leading edge device having an outer surface and an inner surface, the outer surface being farther from, and the inner surface being nearer to, a structure connected to an actuator, the actuator configured to deploy the leading edge device away from the structure and to remove a mechanical load from a fairing when the leading edge device is in a deployed position; andthe fairing, attached to the leading edge device such that the fairing is configured to cover at least a portion of the inner surface, the fairing configured in ...

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.