Description of hydraulic actuator units operating control surfaces of British Aircraft Corp/Sud Aviation Concorde Supersonic transport airliner; control system comprises eight power units for operating elevons and upper and lower rudder sections; three hydraulic relay control units identified as pitch, roll and yaw relays are described; each power control unit is fed from three hydraulic supplies provided by engine driven pump systems operating at 4000 psi.


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    Title :

    Concorde power controls


    Additional title:

    Fluid Power Int


    Published in:

    Publication date :

    1967


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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