A gas turbine engine for an aircraft with an engine shaft which is in operative connection with auxiliary units. The operative connection includes interengaging gear wheels. At least one gear wheel of the operative connection is configured as a beveloid gear wheel.


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    Title :

    GAS TURBINE ENGINE FOR AN AIRCRAFT WITH AN ENGINE SHAFT


    Contributors:

    Publication date :

    2020-03-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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