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).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ENSEMBLE DE TRANSMISSION POUR AERONEF ET HELICOPTERE


    Beteiligte:

    Erscheinungsdatum :

    2017-09-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge



    ENSEMBLE DE TRANSMISSION POUR AERONEF ET HELICOPTERE

    BEDDOK STÉPHANE / BAZET JEAN-MICHEL | Europäisches Patentamt | 2015

    Freier Zugriff

    ENSEMBLE DE TRANSMISSION POUR AERONEF ET HELICOPTERE

    BEDDOK STEPHANE / BAZET JEAN-MICHEL | Europäisches Patentamt | 2022

    Freier Zugriff

    ENSEMBLE DE TRANSMISSION POUR AERONEF ET HELICOPTERE

    BEDDOK STÉPHANE / BAZET JEAN-MICHEL | Europäisches Patentamt | 2018

    Freier Zugriff

    DISPOSITIF DE MANUTENTION POUR AERONEF, NOTAMMENT POUR HELICOPTERE

    RASPIC PIERRE / BAURY ALEXANDRE / BOSCH FABRICE | Europäisches Patentamt | 2021

    Freier Zugriff

    ANTICOUPLE D'URGENCE POUR HELICOPTERE

    JARRY GILLES | Europäisches Patentamt | 2015

    Freier Zugriff