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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    Titel :

    THRUST REVERSER ACTUATION SYSTEM


    Weitere Titelangaben:

    SYSTEME D'ACTIONNEMENT D'INVERSEUR DE POUSSEE


    Beteiligte:
    MORGAN ANTONY (Autor:in)

    Erscheinungsdatum :

    2019-11-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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