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특허 상세정보

Variable camber flap system and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50    B64C-013/34    B64C-009/14    B64C-013/26   
출원번호 US-0034940 (2013-09-24)
등록번호 US-9193440 (2015-11-24)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 1  인용 특허 : 13
초록

A variable camber system for an aircraft may include a variable camber trim unit (VCTU) positioned between an inboard device and an outboard device. The inboard device and the outboard device may be mounted to at least one of a leading edge and a trailing edge of a wing. The VCTU may include a speed sum gearbox having an inboard shaft coupled to the inboard device and an outboard shaft coupled to the outboard device. The VCTU may additionally include a VCTU electric motor engaged to the speed sum gearbox. The VCTU electric motor may be selectively operab...

대표
청구항

1. A variable camber system for an aircraft, comprising: a variable camber trim unit (VCTU) positioned between an inboard device and an outboard device mounted to at least one of a leading edge and a trailing edge of a wing, and including: a speed sum gearbox including: a sun gear coupled to an inboard shaft and surrounded by a plurality of planet gears, the planet gear supported on a carrier coupled to an outboard shaft, the planet gears engaged to an internal side of a ring gear, an external side of the ring gear engaged to a motor shaft, the inboard s...

이 특허에 인용된 특허 (13)

  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. 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. Spitzer ; Robert E. ; May ; III ; Fred W.. Engine out control system for STOL aircraft. USP1978084106730.
  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. Krafka Herfried (Toulouse FRX) Jendrian Henry (Tournefeuille FRX). Wing with extendable flap and variable camber. USP1988024725026.