The patent application describes a steering and braking system for aircraft while ground borne with remote and pilot-override control modes. In the remote mode, a single command controller operates both rudder and differential brakes of the main landing gear. The rudder is provided with a fast-response electro-hydraulic actuator for right, neutral and left positions while the brakes are provided with slow-response pulsating hydraulic actuators for right, left and unison braking. Above a predetermined air speed, the brake control is inactivated. In the pilot-override control mode, the rudder and differential brakes are independently controlled.


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    Titel :

    Aircraft Steering and Braking System


    Beteiligte:
    A. Berg (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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