An electrical system composed of an integral main engine electrical starter/generator and a power management and distribution system for a high performance more electric airplane is presented. The paper emphasizes the fault tolerance and high reliability requirements and discusses the necessary architecture to satisfy them. A number of critical technical issues associated with the more electric airplane, such as severe EMI environment, regenerative power, and system integration and stability are discussed.


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    Titel :

    A Candidate Electrical Power System for Next Generation Military Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Ferreira, Caio A. (Autor:in) / Leonard, Charles (Autor:in) / Said, Waleed (Autor:in)

    Kongress:

    Aerospace Atlantic Conference & Exposition ; 1995



    Erscheinungsdatum :

    01.05.1995




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch