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특허 상세정보

Thrust reversers including support members for inhibiting deflection

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02    F02K-003/00   
미국특허분류(USC) 060/226.2; 239/265.31; 244/110.B
출원번호 UP-0252444 (2005-10-18)
등록번호 US-7600371 (2009-10-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 14  인용 특허 : 59

Aircraft systems having thrust reversers with support members are disclosed herein. In one embodiment, an aircraft system includes a thrust reverser having a nozzle inner wall, a nozzle outer wall radially outward of the inner wall, and a blocker door carried by the outer wall. The blocker door is movable between a deployed position and a stowed position. The thrust reverser further includes a support member extending between a forward section of a nozzle inner wall and a forward section of the nozzle outer wall. The support member is positioned such tha...


I claim: 1. An aircraft system, comprising a thrust reverser including: a nozzle inner wall; a nozzle outer wall radially outward of the nozzle inner wall, the nozzle outer wall including a blocker door movable between a deployed position and a stowed position; a fixed structure positioned radially outward of the nozzle outer wall; a link having a first end portion pivotally coupled to the fixed structure and a second end portion spaced apart from the first end portion; and a support member extending between the nozzle inner wall and the nozzle outer wa...

이 특허에 인용된 특허 (59)

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이 특허를 인용한 특허 피인용횟수: 14

  1. Burak, Dariusz; Choy, John; Grannen, Kevin J.; Zou, Qiang. Acoustic resonator comprising collar and acoustic reflector with temperature compensating layer. USP2016119490418.
  2. Burak, Dariusz; Choy, John; Shirakawa, Alexandre; Nikkel, Phil. Acoustic resonator comprising collar and frame. USP2016119490771.
  3. Gormley, Timothy. Blocker door lock mechanism of a thrust reverser for a turbofan engine. USP2017049611808.
  4. James, Norman J.. Dual actuation system for cascade and thrust reverser panel for an integral cascade variable area fan nozzle. USP20180910077739.
  5. Mercier, Claude; Cloft, Thomas G.. Nacelle electrical locking system for leading edge of openable panel. USP2016019239030.
  6. Sawyers-Abbott, Nigel David; Foster, Joseph P.. Nacelle mounted latching system. USP20180910066510.
  7. Kopecek, Joseph Thomas; Walker, Peter William. System and method for operating a thrust reverser for a turbofan propulsion system. USP2014058713911.
  8. Peyron, Vincent. Thrust reverser device. USP2015099127623.
  9. Gormley, Timothy. Thrust reverser for a turbofan engine. USP2018049938929.
  10. Gormley, Timothy. Thrust reverser for a turbofan engine. USP2018059976516.
  11. Gormley, Timothy. Thrust reverser for a turbofan engine. USP2017089739235.
  12. Niergarth, Daniel Alan; Prentice, Ian Francis; Kroger, Christopher James. Variable pitch fan blade retention system. USP20181010100653.
  13. Miller, Brandon Wayne; Prentice, Ian Francis; Niergarth, Daniel Alan. Variable pitch fan for gas turbine engine and method of assembling the same. USP20180910072510.
  14. Niergarth, Daniel Alan; Miller, Brandon Wayne; Bradley, Donald Albert. Variable-pitch rotor with remote counterweights. USP2018019869190.