Turbine engine, comprising two structural annular casings (16, 22) which are interconnected by connecting rods (54), characterized in that the turbine engine further has at least one accessory gearbox (40) which is fixed to a first of the casings (16) and which is connected by the connecting rods to the other of the casings (22).


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    Title :

    ГАЗОТУРБИННАЯ УСТАНОВКА, ОБОРУДОВАННАЯ СРЕДСТВАМИ ПЕРЕДАЧИ УСИЛИЙ ТЯГИ ЕЕ ДВИГАТЕЛЯ


    Publication date :

    2017-12-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

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