A rotor for an aircraft is described, comprising an input shaft rotatable around a first axis; an output member rotatable around a second axis; a coupling element functionally interposed between the input shaft and the output member and adapted to transmit the motion from the input shaft to the output member; the coupling element is configured to allow, in use, a fixed or variable inclination between the respective first and second axes; the coupling element comprises at least a first corrugated element made of an elastically deformable material; the first corrugated element allows the inclination through elastic deformation.


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    Titel :

    ROTOR FOR AN AIRCRAFT CAPABLE OF HOVERING


    Beteiligte:
    BOTTASSO LUIGI (Autor:in) / POGGI STEFANO (Autor:in) / WOODY PHIL (Autor:in) / LOSI FABRIZIO (Autor:in) / NAVA ALESSANDRO (Autor:in) / SARTORI SERGIO (Autor:in) / SIMONETTA ROBERTO (Autor:in) / AIROLDI ALESSANDRO (Autor:in) / BOIOCCHI MATTEO (Autor:in)

    Erscheinungsdatum :

    2023-07-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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