A hybrid electric aircraft equipped with gyroscopic stabilization control is provided. In one aspect, a hybrid electric aircraft includes a turbo-generator having a gas turbine engine and an electric generator operatively coupled thereto for generating electrical power. The turbo-generator defines a rotation axis. The aircraft also includes one or more electrically-driven propulsors for producing thrust for the aircraft. In addition, the aircraft includes a pivot mount operatively coupled with the turbo-generator. To provide gyroscopic stabilization control of the aircraft, the pivot mount is controlled to adjust the rotation axis of the turbo-generator relative to a prime stability axis of the aircraft. Additionally or alternatively, a rotational speed of the turbo-generator can be changed to provide gyroscopic stabilization control of the aircraft.


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    Titel :

    HYBRID ELECTRIC AIRCRAFT WITH GYROSCOPIC STABILIZATION CONTROL


    Beteiligte:

    Erscheinungsdatum :

    2023-02-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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    Freier Zugriff

    HYBRID ELECTRIC AIRCRAFT WITH GYROSCOPIC STABILIZATION CONTROL

    BALADI MEHDI MILANI / VONDRELL RANDY M | Europäisches Patentamt | 2023

    Freier Zugriff

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