Background and development of lift fan propulsion system by General Electric for U S Army research Aircraft XV-5A; significant features of propulsion arrangement include dual inlet scrolls at each fan for engine-out light safety; pitch fan -- 36 in. aerodynamic scale of wing fan developing lift/weight ratio of 18; hover and low speed aircraft control derived from spoiling and vectoring fan thrusts; opposite rotation of wing fans; J85-5B engines modified for dry operation; fast convertibility, and 500-600-hr fan static and wind tunnel experience including 50-hr flightworthiness qualification; propulsion performance.


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    Titel :

    Initial flight experience with lift fan propulsion


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Beeler, E.F. (Autor:in) / Russell, H.O. (Autor:in)

    Kongress:

    SAE Meeting ; 1964



    Erscheinungsdatum :

    1964


    Format / Umfang :

    29 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Barber, T. J. / Cowley, R. T. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2002