New airplane wing tilts 90 degrees, leading edge up, to feather into rotor downwash during hovering, takeoff, or landing. After hovering or takeoff, rotors tilted forward slightly to accelerate airplane into forward flight. As airplane accelerates, wings start to tilt forward. At speeds of 20 to 40 knots (10.3 to 20.6 m/s), wings are in horizontal orientation. In this speed range, rotor power requirements decreased sufficiently to allow wings to assume normal orientation. Tiltable wings movable independently of tiltable rotors. Tilted at whatever pitch schedule yields greatest efficiency.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Tiltable-Wing, Tiltable-Rotor Aircraft


    Beteiligte:
    Stroub, R. H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.01.1986



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Tiltable rotor wing aircraft

    ZHANG SHIDONG | Europäisches Patentamt | 2020

    Freier Zugriff

    Tiltable hybrid rotor-wing aircraft

    YAO LONGJIANG | Europäisches Patentamt | 2015

    Freier Zugriff

    Tandem tiltable rotor aircraft

    YANG SHOULI | Europäisches Patentamt | 2020

    Freier Zugriff

    Fixed-wing aircraft with tiltable duct

    SHEN LIANG / YANG CHANGFA / LENG ZHIHUI et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Tiltable power module wing

    XU XING / LI ZHIHONG / BING FUQIANG | Europäisches Patentamt | 2023

    Freier Zugriff