The A-C electric power generation system components for the VFW-614 aircraft are described. It consists of 2 main engine/constant speed drive driven channels and 1 auxiliary power unit (gas turbune) driven channel. Each channel consists of a generator, generator control unit, a differential protection current transformer assembly and a control assembly.


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    Title :

    Electrical system


    Additional title:

    Elektrisches System


    Published in:

    Aircraft Engineering ; 46 , 6 ; 24-26


    Publication date :

    1974


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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