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 when the tilt rotor system and the wing are coupled; and a lower protrusion that is configured to be in contact with a lower surface of the wing when the tilt rotor system and the wing are coupled; and a rotor portion that includes a rotor, wherein the rotor portion is moveably coupled to the pylon portion such that the rotor portion is able to move between: (1) a first position that is associated with a vertical flight mode of a vehicle that includes the tilt rotor system and the wing and (2) a second position that is associated with a forward flight mode of the vehicle that includes the tilt rotor system and the wing.


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    Titel :

    PYLON MOUNTED TILT ROTOR


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

    Erscheinungsdatum :

    16.12.2021


    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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