Locking system on a cascade thrust reverser

Details Locking system on a cascade thrust reverser Locking system on a cascade thrust reverser

2006-03-07

2006-03-07

Rodriguez, William H. (Department: 3746)

Power plants

Reaction motor

Interrelated reaction motors

C239S265290, C060S230000

Reexamination Certificate

active

07007454

ABSTRACT:
The invention provides a locking system on a cascade thrust reverser for a bypass turbojet, the reverser (20) comprising guide means (60) for the movable parts (50), and the guide means (60) comprising rails (64) attached to the movable parts (50) and tracks (62) attached to the longitudinal members (36).According to the invention, the locking system (80) comprises locks (82) located at the end (62a) of each track (62) in the opening direction (52), each lock comprising a bolt (110) capable of preventing the rail (64) moving in the opening direction (52).

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