Invention Grant
US08833055B2 Locking/unlocking device for a thrust reverser with a sliding cover and adaptive nozzle for aircraft engine nacelle
有权
用于具有滑动盖的推力反向器的锁定/解锁装置和用于飞机发动机机舱的自适应喷嘴
- Patent Title: Locking/unlocking device for a thrust reverser with a sliding cover and adaptive nozzle for aircraft engine nacelle
- Patent Title (中): 用于具有滑动盖的推力反向器的锁定/解锁装置和用于飞机发动机机舱的自适应喷嘴
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Application No.: US13801813Application Date: 2013-03-13
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Publication No.: US08833055B2Publication Date: 2014-09-16
- Inventor: Patrick Gonidec , Philippe Avenel , Pierre Moradell-Casallas
- Applicant: Aircelle
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: Aircelle
- Current Assignee: Aircelle
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Brinks Gilson & Lione
- Priority: FR1057240 20100913
- Main IPC: F02K1/09
- IPC: F02K1/09 ; F02K1/76 ; F02K1/72
Abstract:
A locking/unlocking device for a thrust reverser with sliding cover and adaptive nozzle is provided that includes a fixed pin secured to a fixed structure of the reverser, a first sleeve secured to the sliding cover and able to accommodate the pin, a second sleeve slidably mounted on the first sleeve, a third sleeve secured to the adaptive nozzle and slidably mounted on the second sleeve, first locking means able to lock the first sleeve with respect to the pin, second locking means able to lock the second sleeve with respect to the first sleeve, and third locking means able to lock the third sleeve with respect to the second sleeve.
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