A thrust reverser actuation system (10), comprising: a first cowl actuation system (62A) for translating a first cowl (60A) of a thrust reverser; a second, separate cowl actuation system (62B) for translating a second cowl (60B) of the thrust reverser; a device (100) operatively connected between the first cowl actuation system (62A) and the second cowl actuation system (62B), and configured to transmit drive from one of the first and second cowl actuation systems (62A,62B) to the other of the first and second cowl actuation systems (62A,62B) in the event of a failure of the other of the first and second cowl actuation systems (62A,62B).
THRUST REVERSER ACTUATION SYSTEM
SYSTEME D'ACTIONNEMENT D'INVERSEUR DE POUSSEE
2019-11-25
Patent
Elektronische Ressource
Englisch
Boeing 777 thrust reverser actuation system
Online Contents | 1998
|Electric Thrust Reverser Actuation Systems
SAE Technical Papers | 2002
|Boeing 777 thrust reverser actuation system
Emerald Group Publishing | 1998
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