An aircraft (1) capable of hovering is described, comprising a motor member (10); a rotor (5) connected to the motor member (10); a transmission shaft (11) rotatable around a first axis (B) and adapted to drive the rotor (5); and a transmission (9) interposed between the motor member (10) and the rotor (5) and comprising a planetary gear (21AXES) formed by a sun (7) rotatable around a second axis (D); a crown (17) that is angularly fixed; and two satellites (19) meshing, each, with the crown (17) and the sun (15), and rotatable around respective third axes (I), which are, in turn, rotatable around the second axis (D); and a satellite carrier (30) rotatable around the second axis (D) and comprising two first pins (32) with respect to which the satellites (19) are rotatable around the respective third axes (E); the transmission (9) comprises an interface (50), angularly integral with the satellite carrier (30) around the second axis (D) and said transmission shaft (11) around the first axis (B); the interface (50) being coupled to said satellite carriers (30) and the transmission shaft (11) so as to allow an angular misalignment between the second axis (B) and a portion (55) of the interface (50).


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    Title :

    AIRCRAFT CAPABLE OF HOVERING


    Additional title:

    SCHWEBEFLUG-FÄHIGES LUFTFAHRZEUG
    UN AÉRONEF CAPABLE DE FAIRE DU VOL STATIONNAIRE


    Contributors:

    Publication date :

    2023-05-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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