A system architecture for a backup thrust reverser actuation system control is provided. The system architecture includes an AC power supply (101, 201) of an aircraft, a power supply (102, 202) and a motor control (103, 203) adapted to control an electric motor (M) of a thrust reverser actuation system. The system architecture further includes a backup power supply (105, 212) adapted to provide power to the electric motor in the event that the power supply fails


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    Title :

    BACK-UP THRUST REVERSER ACTUATION SYSTEM CONTROL


    Additional title:

    COMMANDE DE SYSTEME D'ACTIONNEUR DU RENVERSEUR DE POUSSEE DE SECOURS


    Contributors:

    Publication date :

    2023-05-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge



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