A tail sitter aircraft includes a fuselage having a forward portion and an aft portion. The forward portion of the fuselage includes first and second rotor stations. A first rotor assembly is positioned proximate the first rotor station. A second rotor assembly is positioned proximate the second rotor station. A tailboom assembly extends from the aft portion of the fuselage. The tailboom assembly includes a plurality of landing members. In a vertical takeoff and landing mode of the aircraft, the first and second rotor assemblies rotate about the fuselage to provide vertical thrust. In a forward flight mode of the aircraft, the first rotor assembly rotates about the fuselage to provide forward thrust and the second rotor assembly is non-rotatable about the fuselage forming wings to provide lift.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft having Rotor-to-Wing Conversion Capabilities


    Beteiligte:

    Erscheinungsdatum :

    2018-03-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft having rotor-to-wing conversion capabilities

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / STAMPS FRANK BRADLEY | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT HAVING ROTOR-TO-WING CONVERSION CAPABILITIES

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / STAMPS FRANK BRADLEY | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft having Dual Rotor-to-Wing Conversion Capabilities

    GRONINGA KIRK LANDON / ROBERTSON DANIEL BRYAN / STAMPS FRANK BRADLEY | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft having dual rotor-to-wing conversion capabilities

    GRONINGA KIRK LANDON / ROBERTSON DANIEL BRYAN / STAMPS FRANK BRADLEY | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT HAVING DUAL ROTOR-TO-WING CONVERSION CAPABILITIES

    GRONINGA KIRK LANDON / ROBERTSON DANIEL BRYAN / STAMPS FRANK BRADLEY | Europäisches Patentamt | 2019

    Freier Zugriff