An aircraft actuator assembly includes a failsafe holding device, comprising a body that extends between a lug 503 configured to hingedly connect the holding device to a actuator support body 423 and an attachment flange 501 configured to fixedly attach the holding device to a landing provided by a main body 507 of an actuator, wherein the holding device is configured to prevent movement of the actuator 507 from a normal working position relative to the actuator support body 423 in the event of structural failure of a connection body 407 of the actuator.


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    Title :

    Holding device for an aircraft actuator


    Contributors:

    Publication date :

    2019-01-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



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