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).


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    Title :

    THRUST REVERSER ACTUATION SYSTEM


    Additional title:

    SYSTEME D'ACTIONNEMENT D'INVERSEUR DE POUSSEE


    Contributors:

    Publication date :

    2019-11-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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