Adaptation of fixed shaft turboprop engines to business aircraft requires drastic simplification of control system as compared to transport turboprops; AiResearch TPE331 engine incorporates variable low pitch stop controlled through mechanical linkage to achieve simplified control and also reverse thrust; control of system uses cam cut to match airplane-engine-propeller flight characteristics; flight testing in aircraft varying from 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 simplified fixed shaft turboprop flight control system


    Weitere Titelangaben:

    SAE -- Paper


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

    Kongress:

    SAE Meeting ; 1966



    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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

    Baker, J. R. / Massey, J. W. / Johnson, Vern | SAE Technical Papers | 1966


    Flight testing wright typhoon turboprop

    Templeton, R.R. / Cervino, M.P. | Engineering Index Backfile | 1949



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