Adaptation of fixed shaft turboprop engines to business and utility aircraft requires drastic simplification of the control system as compared to transport turboprops. The AiResearch TPE331 engine incorporates a variable low pitch stop controlled thru mechanical linkage to achieve both simplified control and also reverse thrust. Control of the system utilizes a cam cut to match airplane-engine-propeller flight characteristics. Flight testing in aircraft varying from a converted B-26 test bed to slow STOL aircraft was used to verify calculations and develop control system, negative torque system and general engine development.


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    Titel :

    Development and Flight Testing a Simplified Fixed Shaft Turboprop Flight Control System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Baker, J. R. (Autor:in) / Massey, J. W. (Autor:in) / Johnson, Vern (Autor:in)

    Kongress:

    2nd Annual Business Aircraft Conference ; 1966



    Erscheinungsdatum :

    01.02.1966




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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