A vertical takeoff and landing aircraft includes a starboard wing, a port wing, first and second tilt rotors coupled to the port and starboard wings respectively, and first and second batteries. A pair of control surfaces are arranged on a first side of the mid-sagittal plane of the aircraft, the pair comprising a first and a second control surface. A first flight actuator is electrically connected to the first battery and a second flight actuator is electrically connected to the second battery. The first and second flight actuators are mechanically connected to the first and second control surfaces respectively.


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    Titel :

    FAULT-TOLERANT VTOL AIRCRAFT WITH REDUNDANT CONTROL SURFACES AND ACTUATORS


    Beteiligte:
    BEVIRT JOEBEN (Autor:in) / STOLL ALEX (Autor:in) / VAN DER GEEST MARTIN (Autor:in) / MACAFEE SCOTT (Autor:in) / RYAN JASON (Autor:in)

    Erscheinungsdatum :

    12.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64C AEROPLANES , Flugzeuge



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