A gear transmission for aeronautical applications comprising an input shaft rotating about an axis, an output shaft rotating about said axis, and a transfer group for transferring the torque from the input shaft to the output shaft; the transfer group comprises a first torque splitting stage, receiving the torque entered from the input shaft, and a second torque splitting stage, receiving the torque entered from the first stage; the first stage presents at least one first rotating member and the second stage presents at least one second rotating member; the input shaft and the first rotating member cooperate with one another at respective interaction surfaces coupled frontally and extending transversely to the first axis; the rotating members cooperate with one another at respective friction surfaces coupled frontally and extending transversely to said axis; one of the interaction surfaces comprises first engagement elements, and another of the interaction surfaces comprises second engagement elements complementary to the first engagement elements, and said engagement elements are clutch coupled to one another.


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    Title :

    GEAR TRANSMISSION FOR AERONAUTICAL APPLICATIONS


    Contributors:

    Publication date :

    2019-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60K Anordnung oder Einbau von Antriebseinheiten oder von Kraft- bzw. Drehmomentübertragungen in Fahrzeugen , ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES / F16H Getriebe , GEARING



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