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 and includes a plurality of landing members. A pusher propeller extends from the tailboom assembly. In a vertical takeoff and landing mode, the first and second rotor assemblies rotate about the fuselage to provide vertical thrust. In a forward flight mode, rotation of the pusher propeller provides forward thrust and the first and second rotor assemblies are non-rotatable about the fuselage forming a dual wing configuration to provide lift.


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    Title :

    Aircraft having Dual Rotor-to-Wing Conversion Capabilities



    Publication date :

    2018-03-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Aircraft having dual rotor-to-wing conversion capabilities

    GRONINGA KIRK LANDON / ROBERTSON DANIEL BRYAN / STAMPS FRANK BRADLEY | European Patent Office | 2019

    Free access

    AIRCRAFT HAVING DUAL ROTOR-TO-WING CONVERSION CAPABILITIES

    GRONINGA KIRK LANDON / ROBERTSON DANIEL BRYAN / STAMPS FRANK BRADLEY | European Patent Office | 2019

    Free access

    AIRCRAFT HAVING ROTOR-TO-WING CONVERSION CAPABILITIES

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / STAMPS FRANK BRADLEY | European Patent Office | 2018

    Free access

    Aircraft having Rotor-to-Wing Conversion Capabilities

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / STAMPS FRANK BRADLEY | European Patent Office | 2018

    Free access

    Aircraft having rotor-to-wing conversion capabilities

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / STAMPS FRANK BRADLEY | European Patent Office | 2019

    Free access