The overall problem of achieving dynamic compatibility in helicopter propulsion system can be conveniently divided into four major areas: engine vibration limits; design of the engine/airframe interface; whirling and vibration of power transmission shafting, gearboxes, and bearings; and torsional stability of the engine and drive train with closed-loop fuel controls. These four areas are discussed each with a review of the state of the art and recommendations for future research and development. (Author)


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    Titel :

    Dynamic Compatibility of Helicopter Propulsion Systems


    Beteiligte:
    J. M. Vance (Autor:in) / J. Gomez (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch