A rotor assembly for an aircraft is operable to generate a variable thrust vector. The rotor assembly includes a mast that is rotatable about a mast axis. A ball joint is positioned about and non rotatable with the mast. A tilt control assembly is positioned on and has a tilting degree of freedom relative to the ball joint. The tilt control assembly is non rotatable with the mast. A rotor hub is rotatably coupled to the tilt control assembly. The rotor hub is rotatable with the mast in a rotational plane and tiltable with the tilt control assembly. The rotor hub includes a plurality of grips each coupled to a rotor blade. Actuation of the tilt control assembly changes the rotational plane of the rotor hub relative to the mast axis, thereby generating the variable thrust vector.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotor assembly having a ball joint for thrust vectoring capabilities


    Beteiligte:

    Erscheinungsdatum :

    2020-04-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotor Assembly having Thrust Vectoring Capabilities

    MCCULLOUGH JOHN RICHARD / OLDROYD PAUL K / WIINIKKA MARK ADAM et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    ROTOR ASSEMBLY HAVING THRUST VECTORING CAPABILITIES

    OLDROYD PAUL K / MCCULLOUGH JOHN RICHARD | Europäisches Patentamt | 2021

    Freier Zugriff

    Fixed rotor thrust vectoring

    SEBESTA KENNETH D | Europäisches Patentamt | 2017

    Freier Zugriff

    FIXED ROTOR THRUST VECTORING

    SEBESTA KENNETH D | Europäisches Patentamt | 2015

    Freier Zugriff

    FIXED ROTOR THRUST VECTORING

    SEBESTA KENNETH D | Europäisches Patentamt | 2018

    Freier Zugriff