Descriptive analysis and diagammatic view of pitch control gear for propeller of BMW 801 A airplane engine; mechanism comprises two separate devices, one for regular use, and other for emergency use and to stop engine that has become disabled in flight by feathering its propeller; mechanism includes speed governor, and electric hydraulic pitch changing control by which power from stationary pitch control mechanism is transmitted to pitch changing gear.


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    Title :

    VDM propeller pitch changing mechanism


    Additional title:

    Automotive Aviation Industries


    Published in:

    Publication date :

    1943


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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