A power transmission system having at least one inlet speed-reducing gear and a main speed-reducing gear, each inlet speed-reducing gear comprising an inlet pinion meshing with an inlet gearwheel. The inlet gearwheel is constrained to rotate with a main pinion of the main speed-reducing gear, the main pinion meshing with a main gearwheel. At least one inlet gearwheel is secured to reversible connection means in order to be capable of driving a first additional drivetrain connected to an additional rotor.


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    Title :

    SYSTEME DE TRANSMISSION DE PUISSANCE ET AERONEF AYANT UNE VOILURE TOURNANTE


    Additional title:

    POWER TRANSMISSION SYSTEM AND ROTARY-WING AIRCRAFT
    ANTRIEBSSYSTEM UND DREHFLÜGELFLUGZEUG


    Contributors:

    Publication date :

    2019-07-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



    SYSTEME DE TRANSMISSION DE PUISSANCE ET AERONEF AYANT UNE VOITURE TOURNANTE

    DE MEERSCHMAN OLIVIER / BARAIS OLIVIER | European Patent Office | 2017

    Free access




    AERONEF A VOILURE TOURNANTE

    CABARBAYE AURELIEN / CABARBAYE ADRIEN / CABARBAYE ANDRE | European Patent Office | 2019

    Free access