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특허 상세정보

Leading and trailing edge device deflections during descent of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-013/00    B64C-013/16    B64C-009/32    B64C-019/02    G05D-001/06   
출원번호 US-0035001 (2013-09-24)
등록번호 US-9327827 (2016-05-03)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 1  인용 특허 : 17
초록

An system for increasing the descent rate of an aircraft may include a flight control computer, an edge control system, and a speedbrake control device. The flight control computer may be configured to compute a first setting for a leading edge device and/or a trailing edge device of an aircraft wing. The edge control system may be communicatively coupled to the flight control computer and may include an edge control device having a plurality of control device positions including a cruise position. The speedbrake control device may include a plurality of...

대표
청구항

1. A system for increasing a descent rate of an aircraft, the system comprising: a flight control computer configured to compute a first setting for a leading edge device and/or a trailing edge device of an aircraft wing having one or more spoilers:an edge control system communicatively coupled to the flight control computer and including an edge control device having a plurality of control device positions including a cruise position;a speedbrake control device having a plurality of speedbrake detents includinga down detent and a flight detent, the down...

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. Fox, III, Angus C.. Autopilot for aircraft having automatic descent function in the event of cabin depressurization. USP2003016507776.
  7. Johnson, Andrew T.; Hanlon, Casey; Potter, Calvin C.. Distributed flight control surface actuation system. USP2009077556224.
  8. 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.
  9. Aimar, Jeffrey L.. Emergency descent system. USP2010097792615.
  10. Bliesner Wayne T.. Leading edge slat/wing combination. USP1998115839699.
  11. Muller Dietmar,DEX. Lift body having a variable camber. USP2000116152405.
  12. Shmilovich, Arvin; Yadlin, Yoram. Low noise wing slat system with rigid cove-filled slat. USP2013048424810.
  13. Gangsaas Dagfinn (Bellevue WA) Norman Daniel C. (Renton WA). Maneuver enchancement and gust alleviation system. USP1989044821981.
  14. Williams George H. (Bristol GBX). Mechanism for supporting and extending a high lift device for aircraft wings. USP1989064838503.
  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.