Concepts are discussed that project turbine engine cost savings through use of geometrically constrained components designed for low rotational speeds and low stress to permit manufacturing economies. Aerodynamic development of geometrically constrained components is recommended to maximize component efficiency. Conceptual engines, airplane applications, airplane performance, engine cost, and engine-related life cycle costs are presented. The powerplants proposed offer encouragement with respect to fuel efficiency and life cycle costs, and make possible remarkable airplane performance gains.


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    Titel :

    Advanced General Aviation Turbine Engine (GATE) Concepts


    Beteiligte:
    E. J. Lays (Autor:in) / G. L. Murray (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    189 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    General aviation turbine engine /GATE/ concepts

    Lays, E. J. / Murray, D. L. | NTRS | 1979


    General aviation turbine engine /GATE/ concepts

    LAYS, E. / MURRAY, D. | AIAA | 1979


    General Aviation Turbine Engine (GATE) Study

    C. F. Baerst / D. G. Furst | NTIS | 1979


    General Aviation Turbine Engine (GATE) study

    Baerst, C. F. / Furst, D. G. | NTRS | 1979


    Advanced non-turbine engines for general aviation

    Willis, E.A. | Tema Archiv | 1978