Systems and methods are disclosed herein for an aircraft seat with a decoupled linear actuator. The linear actuator may activate a first adjustable feature by moving in a first direction. The linear actuator may include a decoupling mechanism. The decoupling mechanism may decouple the first adjustable feature from the linear actuator in response to loss of power to the linear actuator.


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    Title :

    Decoupled aircraft seat actuator


    Contributors:

    Publication date :

    2016-03-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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