This disclosure is directed to an unmanned aerial vehicle (“UAV”) that transitions in-flight between vertical flight configuration and horizontal flight configuration by changing an orientation of the UAV by approximately ninety degrees. The UAV may include propulsion units that are coupled to a fuselage or wing. The UAV may include a tail and/or a swing arm that is rotatably coupled to the fuselage and that rotate between different positions. The swing arm may be selectively coupled to cargo. The wing may include wing segments rotatably coupled together by pivots that rotate to position the propulsion units around a center of mass of the UAV when the fuselage is oriented perpendicular with the horizon.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    In-flight reconfigurable hybrid unmanned aerial vehicle


    Beteiligte:

    Erscheinungsdatum :

    27.08.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    In-flight reconfigurable hybrid unmanned aerial vehicle

    ERDOZAIN JR JACK / OZTURK BERK / ROBERTS NICHOLAS HAMPEL et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    In-flight reconfigurable hybrid unmanned aerial vehicle

    ERDOZAIN JR JACK / OZTURK BERK / ROBERTS NICHOLAS HAMPEL et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    In-flight reconfigurable hybrid unmanned aerial vehicle

    ERDOZAIN JR JACK / OZTURK BERK / ROBERTS NICHOLAS HAMPEL et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Reconfigurable unmanned aerial vehicle

    YANG PENGQIAN / NI JUN / JIN ZIHAN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Stable flight performance Hybrid Unmanned Aerial Vehicle

    KANG BEOM SOO / YOON JUN SEOK / JEONG JIN SEOK | Europäisches Patentamt | 2018

    Freier Zugriff