The invention relates to an actuator. More specifically, but not exclusively, an aircraft pitch damper which comprises an actuator. The actuator comprises a first chamber charged with gas and a second chamber charged with gas. An intermediate chamber containing liquid is located between the first chamber and second chamber. A piston rod extends towards the first chamber through the second chamber and intermediate chamber. A first piston head is associated with and partially defines the first chamber, and a second piston head is associated with and partially defines the second chamber. The piston rod is arranged to abut and move with the first piston head in a first direction, the piston rod further arranged to abut and move with the second piston head in a second direction.


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    Title :

    Aircraft actuator


    Contributors:

    Publication date :

    2019-07-23


    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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