According to the invention, the assembly comprises a first inlet shaft (10a) configured to receive torque from a first engine (10), an outlet shaft (60a) configured to transmit torque to a torque receiver (60), a first transmission member (20) having at least two degrees of freedom and comprising first, second, and third movable portions, a first reversible electrical regulator machine (30), and a first reversible electrical balancing machine (40), wherein the inlet shaft (10a) is coupled to the first movable portion, the outlet shaft (60a) is coupled to the second movable portion, the first electrical regulator machine (30) is coupled to the third movable portion, and the first electrical balancing machine (40) is coupled in series with the inlet shaft or the outlet shaft (60a).


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    Title :

    ENSEMBLE DE TRANSMISSION POUR AERONEF ET HELICOPTERE


    Contributors:

    Publication date :

    2017-09-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge



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