Problems which must be solved by airframe propulsion designer to obtain high thrust-to-weight ratio lift engine installation include starting, air induction, exhaust, fire protection, and VTO control; thrust-to-weight ratio degradation from bare engine to final installation is shown for typical example; some installation requirements which must also be considered, are noted.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Considerations of lift engine installations in VTOL aircraft from viewpoint of airframe designer


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Bagby, C.L. (Autor:in)

    Kongress:

    SAE Meeting ; 1963 VTOL-STOL



    Erscheinungsdatum :

    1963


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    ANNULAR LIFT FAN VTOL AIRCRAFT

    JIANG YUN | Europäisches Patentamt | 2018

    Freier Zugriff

    Lift/cruise fan VTOL aircraft

    Quigley, H. C. / Franklin, J. A. | NTRS | 1977


    VTOL AIRCRAFT LIFT INCREASING DEVICE

    KIRIAKIDI SERGEJ KONSTANTINOVICH / ANOKHIN IVAN MIKHALOVICH / KOTOV IVAN ALEKSEEVICH | Europäisches Patentamt | 2015

    Freier Zugriff

    Annular ducted lift fan VTOL aircraft

    JIANG YUN | Europäisches Patentamt | 2016

    Freier Zugriff