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특허 상세정보

System and method for reducing the stopping distance of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-025/42    G05D-001/00   
출원번호 US-0035030 (2013-09-24)
등록번호 US-9296475 (2016-03-29)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 14

A system for reducing a stopping distance of an aircraft may include an edge control system configured to control a leading edge device mounted to a wing of an aircraft. The edge control system may be configured to automatically command extension of the leading edge device from a first position to a second position in response to deployment of a spoiler if a ground speed of the aircraft is greater than a threshold ground speed.


1. A system for reducing a stopping distance of an aircraft, comprising: an edge control system configured to control a leading edge device deployable from a leading edge of a wing of an aircraft on the ground;a thrust control system including a thrust lever positionable in at least an idle position corresponding to an idle thrust setting and a non-idle position corresponding to a thrust setting different than the idle thrust setting;a speedbrake control system automatically commanding deployment of a spoiler at least partially responsive to movement of ...

이 특허에 인용된 특허 (14)

  1. Borzachillo Angelo (San Marcos CA). Aeroelastic control flap. USP1988034729528.
  2. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael. Aircraft wing systems for providing differential motion to deployable lift devices. USP2009027494094.
  3. Johnson, Andrew T.; Hanlon, Casey; Potter, Calvin C.. Distributed flight control surface actuation system. USP2009077556224.
  4. 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.
  5. Bliesner Wayne T.. Leading edge slat/wing combination. USP1998115839699.
  6. Muller Dietmar,DEX. Lift body having a variable camber. USP2000116152405.
  7. Shmilovich, Arvin; Yadlin, Yoram. Low noise wing slat system with rigid cove-filled slat. USP2013048424810.
  8. Gangsaas Dagfinn (Bellevue WA) Norman Daniel C. (Renton WA). Maneuver enchancement and gust alleviation system. USP1989044821981.
  9. Williams George H. (Bristol GBX). Mechanism for supporting and extending a high lift device for aircraft wings. USP1989064838503.
  10. Goodman, William L.; Peck, Andrew J.; Imrich, Thomas. Method, system, and computer program product for performance monitored aircraft rejected takeoff braking. USP2010057720579.
  11. Denniston James L. (Columbus OH). Selectively actuated flight simulation system for trainer aircraft. USP1983024372507.
  12. 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.
  13. Garthaffner, Joseph M.. Winder for rectangular cross-section wire. USP2013018356766.
  14. Krafka Herfried (Toulouse FRX) Jendrian Henry (Tournefeuille FRX). Wing with extendable flap and variable camber. USP1988024725026.