A gas turbine powered aircraft auxiliary power system is described. The system is capable of efficiently supplying all aircraft auxiliary services both in flight and on the ground. It is capable also of operating independently of the aircraft main engines. The system employs multiple gas turbine compressor stages, and utilizes the aircraft cabin as a plenum chamber between the first and second compressor stages, thereby accomplishing cabin pressurization, ventilation and heating.


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    Titel :

    Independent Power Generator


    Beteiligte:
    R. N. Young (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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