A unique bleed air environmental system has been developed for the Turbo Commander. This system utilizes air-to-air jet pumps as “flow multipliers” to reduce engine bleed flow requirements. Bleed power extraction is reduced from an unacceptably high 12% to a more reasonable 6%. The system is integrated with the original air cycle cooling system and heating is by compression heat. The jet pumps furnish a solution to the problem of high bleed power extraction common to turboprops, at a modest increase in cost and weight and at practically no decrease in reliability or maintainability.


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    Titel :

    The Turbo Commander Bleed Air Environmental System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1969



    Erscheinungsdatum :

    01.02.1969




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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