Invention Grant
US09476383B2 Aircraft turbojet engine thrust reverser with a reduced number of latches
有权
飞机涡轮喷气发动机推力反向器具有减少的锁存数量
- Patent Title: Aircraft turbojet engine thrust reverser with a reduced number of latches
- Patent Title (中): 飞机涡轮喷气发动机推力反向器具有减少的锁存数量
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Application No.: US13944187Application Date: 2013-07-17
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Publication No.: US09476383B2Publication Date: 2016-10-25
- Inventor: Pierre Caruel
- Applicant: AIRCELLE
- Applicant Address: unknown Gonfreville l'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: unknown Gonfreville l'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1150342 20110117
- Main IPC: F02K1/54
- IPC: F02K1/54 ; B64D33/04 ; F02K1/72 ; F02K1/76

Abstract:
A thrust reverser with grids includes a jet engine pylon, a one piece cowl either directly or indirectly slidably mounted on the jet engine pylon between a direct jet position and a reverse jet position, and a system for locking this cowl on a beam. The system has a single tertiary lock, which is positioned on one side of the jet engine pylon being capable of locking a corresponding upper edge of the cowl. In addition, the tertiary lock includes a locker to lock the cowl, a blocker for blocking the locker, and a position detector in order to detect the position of the locker. The system further includes another detector to detect proper closing of the other upper edge of the cowl.
Public/Granted literature
- US20140131515A1 AIRCRAFT TURBOJET ENGINE THRUST REVERSER WITH A REDUCED NUMBER OF LATCHES Public/Granted day:2014-05-15
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