The present invention relates to a body (2) provided at air vehicles: at least one rotor (3) extending longitudinally out of the body (2) and rotating around an axis along which it extends: at least one blade (4) connected to the rotor (3), which, upon triggering of the rotor (3), rotates around the axis along which the rotor (3) extends, thus creating an aerodynamic lifting force required for the body (2) to take-off: a blade tip (5) which is located on the blade (4), at the end of a direction along which the blade (4) extends: and at least one plate (6) made of a piezo-electric material, which is located on the blade (4) and enables energy conversion.


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    Titel :

    AN ELECTRICITY GENERATION SYSTEM


    Weitere Titelangaben:

    STROMERZEUGUNGSSYSTEM
    SYSTÈME DE PRODUCTION D'ÉLECTRICITÉ


    Beteiligte:
    SAHIN BURHAN (Autor:in) / GUNEL MURAT (Autor:in)

    Erscheinungsdatum :

    26.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02N Elektrische Maschinen, soweit nicht anderweitig vorgesehen , ELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR / B64C AEROPLANES , Flugzeuge



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