An aircraft has a propulsion unit and a fuselage unit. The propulsion unit has a first rotor for providing a propulsion force on the aircraft. The fuselage unit extends along a rotation axis of the first rotor and has a rotationally symmetrical shape with respect to the rotation axis of the first rotor. The fuselage unit has a suspension at a first end by which the fuselage unit is coupled to the first rotor so that the fuselage unit is spaced apart from the first rotor along the rotation axis. A detection unit for the detection of environmental information is provided in the area of a second end of the fuselage unit. The propulsion unit is designed to keep the aircraft in a hovering flight condition so that a relative position of the aircraft with respect to a reference point on the Earth's surface remains unchanged.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft Capable Of Hovering


    Contributors:

    Publication date :

    2020-08-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



    AIRCRAFT CAPABLE OF HOVERING

    BRAGHIROLI MARCO / CANTA ENRICO | European Patent Office | 2021

    Free access

    AIRCRAFT CAPABLE OF HOVERING

    PODDA DANIELE / GABRIELLI ANDREA / MONTAGNA FEDERICO et al. | European Patent Office | 2024

    Free access

    AIRCRAFT CAPABLE OF HOVERING

    BRAGHIROLI MARCO / CANTA ENRICO | European Patent Office | 2023

    Free access

    Aircraft capable of hovering

    BRAGHIROLI MARCO / CANTA ENRICO | European Patent Office | 2022

    Free access

    AIRCRAFT CAPABLE OF HOVERING

    BRAGHIROLI MARCO / CANTA ENRICO | European Patent Office | 2021

    Free access