Single integral unit includes motor, gearbox, and clutch. Device has two-speed capability, fits within aerodynamic contours of aircraft, operates with onboard power source, does not interfere with normal landing gear functions, reduces use of regular brakes in congested areas, and provides locomotion and supplementary braking capability.


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    Titel :

    Powered wheel for aircraft


    Beteiligte:
    Long, M. J. (Autor:in) / Irick, S. C. (Autor:in) / Van Ausdal, R. K. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1977-01-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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