发明名称 AIRCRAFT TURBOJET ENGINE THRUST REVERSER WITH A REDUCED NUMBER OF LATCHES
摘要 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.
申请公布号 EP2665911(A1) 申请公布日期 2013.11.27
申请号 EP20120705332 申请日期 2012.01.13
申请人 AIRCELLE 发明人 CARUEL, PIERRE
分类号 F02K1/72;F02K1/76 主分类号 F02K1/72
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