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특허 상세정보

Leading edge variable camber system and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50    B64C-009/24    B64C-013/50    B64C-013/00    B64C-013/16   
출원번호 US-0034987 (2013-09-24)
등록번호 US-9180962 (2015-11-10)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 17
초록

A system for varying a wing camber of an aircraft wing may include a leading edge device coupled to the wing. The leading edge device may be configured to be actuated in an upward direction and a downward direction relative to a retracted position of the leading edge device.

대표
청구항

1. A system for varying a wing camber, comprising: a flight control computer configured to compute an optimum slat setting based on aircraft state data;a control system communicatively coupled to the flight control computer, the control system including a control device moveable to any one of a plurality of control device positions including a designated control device position selected by the control device for selecting any one of a plurality of corresponding standard flap settings;a leading edge device coupled to a wing of the aircraft;a slat actuatio...

이 특허에 인용된 특허 (17)

  1. Yamasaki, Koichi. Aerodynamic coefficient estimation device and control surface failure/damage detection device. USP2015028954208.
  2. Borzachillo Angelo (San Marcos CA). Aeroelastic control flap. USP1988034729528.
  3. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  4. Lee, Howard; Morgenstern, John M.; Aminpour, Hossein. Aircraft with active center of gravity control. USP2005076913228.
  5. Bliesner Wayne T. (Snohomish WA) Wang Timothy (Bellevue WA) Stoner Ronald C. (Bellevue WA). Apparatus and method for aircraft wing stall control. USP1991105056741.
  6. Johnson, Andrew T.; Hanlon, Casey; Potter, Calvin C.. Distributed flight control surface actuation system. USP2009077556224.
  7. Onu, Dan; Winter, John D.; Carr, Candy L.; Vijgen, Paul M.; Emch, Gary A.; Renzelmann, Michael E.. Dynamic adjustment of wing surfaces for variable camber. USP2010017641152.
  8. Spitzer ; Robert E. ; May ; III ; Fred W.. Engine out control system for STOL aircraft. USP1978084106730.
  9. Bliesner Wayne T.. Leading edge slat/wing combination. USP1998115839699.
  10. Muller Dietmar,DEX. Lift body having a variable camber. USP2000116152405.
  11. Shmilovich, Arvin; Yadlin, Yoram. Low noise wing slat system with rigid cove-filled slat. USP2013048424810.
  12. Gangsaas Dagfinn (Bellevue WA) Norman Daniel C. (Renton WA). Maneuver enchancement and gust alleviation system. USP1989044821981.
  13. Williams George H. (Bristol GBX). Mechanism for supporting and extending a high lift device for aircraft wings. USP1989064838503.
  14. Edward Emaci ; Scott Wilkinson ; William Leden. Method and apparatus for sensing skews and disconnects of adjacent movable components. USP2002116483436.
  15. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael. Systems and methods for providing differential motion to wing high lift device. USP2010067726610.
  16. Garthaffner, Joseph M.. Winder for rectangular cross-section wire. USP2013018356766.
  17. Krafka Herfried (Toulouse FRX) Jendrian Henry (Tournefeuille FRX). Wing with extendable flap and variable camber. USP1988024725026.