The geared flap control system provides a means for controlling a tiltwing V/STOL aircraft in hover and transition flight without the use of auxiliary systems such as cyclic propeller pitch or tail jets/rotors. The system is based on using the flap as an aerodynamic servo to position the wing relative to the fuselage. Although the system is mechanically simple, the control characteristics are difficult to visualize because of the coupled body dynamics involved. Therefore, a comprehensive analytical and model testing program was performed to evaluate the system. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Evaluation of Geared Flap Control System for Tiltwing V/STOL Aircraft


    Beteiligte:

    Erscheinungsdatum :

    1970


    Format / Umfang :

    108 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Tiltwing aircraft

    ALBER MARK R / PARKHURST JEFFREY / GAYAGOY CHARLES | Europäisches Patentamt | 2019

    Freier Zugriff

    TILTWING AIRCRAFT

    ALBER MARK R / PARKHURST JEFFERY / GAYAGOY CHARLES | Europäisches Patentamt | 2017

    Freier Zugriff

    X-tiltwing aircraft

    GRONINGA KIRK LANDON / ROBERTSON DANIEL BRYAN | Europäisches Patentamt | 2019

    Freier Zugriff

    X-Tiltwing Aircraft

    GRONINGA KIRK LANDON / ROBERTSON DANIEL BRYAN | Europäisches Patentamt | 2018

    Freier Zugriff