Consideration of airplane wheel brakes and indication of probable improvements; at least half of increased weight of braked undercarriage is directly due to heavier structure required for transmitting torque loads; essential requirements of braked under-carriages; separate control to each wheel; writer does not think that any servo-motor carried apart from wheel should be considered; particulars of Bendix self-energizing brake unit; points to watch in wheel mounting.


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    Title :

    Wheel brake equipment for aircraft


    Additional title:

    Aeroplane


    Contributors:
    Dowty, G.H. (author)

    Published in:

    Aeroplane ; 35 , n 9


    Publication date :

    1928


    Size :

    2 pages


    Remarks:

    5 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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