A hover-capable aircraft includes a body including a tubular strut, a first rotor assembly rotatably coupled to the body and positioned about the strut, wherein the first rotor assembly includes a first plurality of circumferentially-spaced blades, a first actuation assembly including a first plurality of electronically controlled actuators coupled to a first swashplate and configured to control the movement of the first swashplate relative to the body, and a control system coupled to the body and configured to control the first plurality of actuators, wherein the control system includes a cable extending through a passage formed in the tubular strut and in signal communication with the first plurality of actuators.


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    Titel :

    Hover-capable aircraft


    Beteiligte:
    BENEDICT MOBLE (Autor:in) / COLEMAN DAVID (Autor:in) / HALDER ATANU (Autor:in) / LEE BOCHAN (Autor:in) / RIHA ANDREW (Autor:in) / SAEMI FARID (Autor:in) / RUNCO CARL (Autor:in) / SUBRAMANIAN VISHAAL (Autor:in) / GREENWOOD ERIC (Autor:in) / LAKSHMINARAYAN VINOD (Autor:in)

    Erscheinungsdatum :

    08.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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