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특허 상세정보

Slat support funk plate

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/214; 244/213; 244/215; 244/035R
출원번호 US-0246816 (2008-10-07)
등록번호 US-8181913 (2012-05-22)
우선권정보 GB-0722425.6 (2007-11-15)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lowe, Hauptman, Ham & Berner, LLP
인용정보 피인용 횟수 : 4  인용 특허 : 24
초록

An aircraft wing high lift assembly comprising a movable element and a load receiving element including a body portion having a first load receiving region arranged to receive loads from the movable element in a first direction during normal operation of the high lift assembly and including at least one restraining arm projecting from the body portion, the or each restraining arm having a second load receiving region arranged to receive loads from the movable element in a second direction in the event of a failure within the high lift assembly.

대표
청구항

1. An aircraft wing high lift assembly comprising a movable element and a fixed load receiving element including a body portion having a first load receiving region arranged to receive lateral loads from the movable element and to be in sliding contact with the movable element during normal operation of the high lift assembly and including at least one restraining arm projecting from the body portion, said at least one restraining arm having a second load receiving region spaced away from the movable element during normal operation and arranged to suppor...

이 특허에 인용된 특허 (24)

  1. Portier Serge (Clichy FR). Actuating system for wing leading-edge slats. USP1976043949957.
  2. Werner Dobrzynski DE; Burkhard Gehlhar DE. Auxiliary airfoil for aircraft main wings. USP2002106457680.
  3. Caferro Joseph S. (Seattle WA) Tomassi Hector V. (Renton WA). Auxiliary airfoil lost motion detector and actuator. USP1997055628477.
  4. Cole James B. (King County WA). Biased leading edge slat apparatus. USP1988064753402.
  5. Pace James W. (Mercer Island WA). Closing device for an airfoil. USP1987024640477.
  6. Jaggard Philip R.,GBX. Deployment mechanisms for aircraft auxiliary airfoils. USP2000116149105.
  7. Day Roger A. (Bristol GB2). Device for closing and opening in the leading edge of a wing. USP1989114880189.
  8. Cole James B. (Mercer Island WA). Extendible airfoil track assembly. USP1984094471928.
  9. Cabriere Jean (Vaucresson FR). Flap or wing droop arrangement for an aircraft wing. USP1976023940093.
  10. Narramore Jimmy C. (Bedford TX). Flaperon system for tilt rotor wings. USP1992035094412.
  11. Williams Anthony J. (Filton GBX). Flexible closing device for a wing leading edge. USP1991095044580.
  12. Bliesner Wayne T.. Leading edge slat/wing combination. USP1998115839699.
  13. Bliesner Wayne T. (Snohomish WA). Leading edge slat/wing combination. USP1996085544847.
  14. Shaffer James R. (Costa Mesa CA) Kramer Louis T. (Long Beach CA). Locking, redundant slat drive mechanism. USP1984094470569.
  15. Williams George H. (Bristol GBX). Mechanism for supporting and extending a high lift device for aircraft wings. USP1989064838503.
  16. Sakurai Seiya (Seattle WA). Three-position variable camber Krueger leading edge flap. USP1992105158252.
  17. Cole James B. (Mercer Island WA). Variable camber leading edge assembly for an airfoil. USP1984104475702.
  18. Cole James B. (Mercer Island WA). Variable camber leading edge assembly for an airfoil. USP1987114706913.
  19. Rudolph Peter K. C. (Seattle WA). Vortex leading edge flap assembly for supersonic airplanes. USP1997105681013.
  20. Cole James B. (Mercer Island WA). Wind edge movable airfoil having variable camber. USP1987034650140.
  21. Hinkleman Michael J.. Wing leading edge flap and method therefor. USP1999075927656.
  22. Brown Robert B. (Kent WA). Wing leading edge slat. USP1982114360176.
  23. Evans Arthur (Seattle WA). Wing leading edge slat. USP1983084399970.
  24. Knowler John C. (Renton WA). Wing slat anti-ice air duct system. USP1986104615499.