发明授权
- 专利标题: Turbojet engine nacelle having a variable nozzle
- 专利标题(中): 具有可变喷嘴的涡轮喷气发动机舱
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申请号: US14173484申请日: 2014-02-05
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公开(公告)号: US09587583B2公开(公告)日: 2017-03-07
- 发明人: Pierre Caruel , Patrick Gonidec , Patrick Boileau
- 申请人: AIRCELLE
- 申请人地址: FR Gontreville L'Orcher
- 专利权人: AIRCELLE
- 当前专利权人: AIRCELLE
- 当前专利权人地址: FR Gontreville L'Orcher
- 代理机构: Burris Law, PLLC
- 优先权: FR1157174 20110805
- 主分类号: F02K1/76
- IPC分类号: F02K1/76 ; F02K1/62 ; F02K1/06 ; F02K1/12 ; F02K1/30 ; F02K1/72
摘要:
A turbojet engine nacelle has a thrust reverser device and an actuating system for said thrust reverser device, and the thrust reverser device includes a moving cowl mounted translatably alternating between a closed position and an open position, and a jet nozzle section for gases that extends the moving cowl. In particular, the jet nozzle section includes a nozzle flap mounted movable between a closed position and an open position in which the nozzle flap opens a leakage passage toward the outside of the nozzle section. The actuating system has an actuator shared with the moving cowl and the nozzle flap to activate the translational movement of the moving cowl and to pivot the nozzle flap between three following positions: an idle position, an open position of the nozzle flap and an open position of the moving cowl.
公开/授权文献
- US20150354499A1 TURBOJET ENGINE NACELLE HAVING A VARIABLE NOZZLE 公开/授权日:2015-12-10
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