A hover-capable aircraft (1) is described that comprises a drive unit (10), a rotor (3, 4) and a transmission (5) interposed between the drive unit (10) and the rotor (3, 4); the transmission (5) comprises a gear (9a, 9b, 9c, 9d, 9e); the gear (9a, 9b, 9c, 9d, 9e), in turn, comprises a main body (40) rotatable about a first axis (B) and a plurality of first teeth (13) projecting in a cantilever fashion from the main body (40); the gear (40) comprises a first pair of first rings (50, 51) axially opposite to each other and cooperating with the gear (9a, 9b, 9c, 9d, 9e) so as to exert a radial force on the gear (9a, 9b, 9c, 9d, 9e).


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    Title :

    HOVER-CAPABLE AIRCRAFT


    Additional title:

    GLEITFÄHIGES FLUGZEUG
    AÉRONEF APTE À EFFECTUER UN VOL STATIONNAIRE


    Contributors:

    Publication date :

    2020-12-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge



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