A pitch trimmer assembly for an aircraft landing gear having a damping element arranged to be connected between a first and a second element of an aircraft landing gear and arranged to exert a first damping force when in a first state and a second damping force in a second state, the damping element being switchable between the first and second states in dependence on the relative positions of the first and second landing gear elements.


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    Title :

    РЕГУЛИРУЮЩИЙ ПРИВОД С ИЗМЕНЯЕМОЙ СТЕПЕНЬЮ ДЕМПФИРОВАНИЯ


    Publication date :

    2017-03-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge