The present disclosure is directed to rotor assemblies for scissoring rotors, aircraft including the same, and associated methods. In one example, a hub assembly comprises: a first hub subassembly configured to rotate a first blade assembly about an axis of rotation in a first plane, a second hub subassembly configured to rotate a second blade assembly about the axis of rotation in a second plane, and a rotary guide configured to control an axial position of the second hub subassembly relative to the first hub subassembly about the axis of rotation. The rotary guide is configured to adjust the axial position as a function of a lifting force generated by the first blade assembly or the second blade assembly.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotor Assemblies for Scissoring Propeller


    Beteiligte:

    Erscheinungsdatum :

    14.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotor assemblies for scissoring propeller

    JORDAN JEFFREY SCOTT | Europäisches Patentamt | 2023

    Freier Zugriff

    SCISSORING PROPELLER WITH CENTRIPETALLY ACTUATED CENTERING LEVER LOCK

    ENSSLIN OLIVER DANIEL | Europäisches Patentamt | 2021

    Freier Zugriff

    Scissoring propeller with centripetally actuated centering lever lock

    ENSSLIN OLIVER DANIEL | Europäisches Patentamt | 2023

    Freier Zugriff

    Railcar ant-scissoring system

    BALKE RODNEY W | Europäisches Patentamt | 2023

    Freier Zugriff

    SCISSORING FOLD ARRANGEMENT FOR DUAL PLANE FOUR BLADED ROTOR HUBS

    THOMPSON TERRY / STAMPS FRANK B | Europäisches Patentamt | 2016

    Freier Zugriff