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특허 상세정보

Leading edge system and method for approach noise reduction

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/16    B64C-009/20    B64C-009/22    B64C-009/24    B64C-013/28   
출원번호 US-0035011 (2013-09-24)
등록번호 US-9771141 (2017-09-26)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 14
초록

A slat control system for an aircraft may include a flight control computer configured to generate a gap command in response to an occurrence of a gap-command condition. The slat control system may further include an edge control system including an edge control device having a plurality of control device positions including at least one designated control device position. The slat control system may additionally include a device actuation system configured to move a leading edge device of an aircraft. The edge control system may be configured to automat...

대표
청구항

1. A slat control system for an aircraft, comprising: a flight control computer configured to generate a gap command in response to an occurrence of a gap-command condition;an edge control system including an edge control device selectable into any one of a plurality of control device positions including at least one of an approach flaps position and a landing flaps position, the control device positions corresponding to settings for leading edge devices and trailing edge devices of an aircraft;a device actuation system configured to move a leading edge ...

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. Bliesner Wayne T. (Snohomish WA) Wang Timothy (Bellevue WA) Stoner Ronald C. (Bellevue WA). Apparatus and method for aircraft wing stall control. USP1991105056741.
  4. Gast Mark E.. Autopilot/flight director stall protection system. USP1998095803408.
  5. 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.
  6. Bliesner Wayne T.. Leading edge slat/wing combination. USP1998115839699.
  7. Muller Dietmar,DEX. Lift body having a variable camber. USP2000116152405.
  8. Shmilovich, Arvin; Yadlin, Yoram. Low noise wing slat system with rigid cove-filled slat. USP2013048424810.
  9. Gangsaas Dagfinn (Bellevue WA) Norman Daniel C. (Renton WA). Maneuver enchancement and gust alleviation system. USP1989044821981.
  10. Williams George H. (Bristol GBX). Mechanism for supporting and extending a high lift device for aircraft wings. USP1989064838503.
  11. 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.
  12. Garthaffner, Joseph M.. Winder for rectangular cross-section wire. USP2013018356766.
  13. Hinkleman Michael J.. Wing leading edge flap and method therefor. USP1999075927656.
  14. Krafka Herfried (Toulouse FRX) Jendrian Henry (Tournefeuille FRX). Wing with extendable flap and variable camber. USP1988024725026.