An afterbody for a rotor blade of a rotorcraft is unitarily formed of a single material of construction. The afterbody includes an upper surface disposed from a lower surface, a concave leading edge connected to the upper surface and the lower surface, and a trailing edge formed at an intersection of the upper surface with the lower surface.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotor blade afterbody


    Beteiligte:

    Erscheinungsdatum :

    2020-07-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    ROTOR BLADE AFTERBODY

    MCINTYRE JOEL J / BURNETT MICHAEL CHRISTOPHER | Europäisches Patentamt | 2019

    Freier Zugriff




    Lobed nozzle afterbody research

    Russell, W.D. | Tema Archiv | 1987