A tilt rotor system, comprising: a pylon portion that includes: an upper protrusion that is configured to be in contact with an upper surface of a wing and a lower protrusion that is configured to be in contact with a lower surface of the wing; and a rotor portion that includes a rotor, wherein the rotor portion is able to move between: (1) a first position that is associated with a vertical flight mode and (2) a second position that is associated with a forward flight mode. The pylon portion further includes an air intake vent, a horizontal surface, a rotor controller, and a heat sink.


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    Titel :

    Pylon mounted tilt rotor


    Beteiligte:
    MCLAREN CAMPBELL (Autor:in) / SINHA PRANAY (Autor:in)

    Erscheinungsdatum :

    15.02.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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