A turbine engine assembly (16) is provided. The assembly includes a stationary component (52), a drive shaft (32), and a gearbox (50) coupled along the drive shaft (32), and coupled to the stationary component (52). The assembly also includes a vibration-reducing mechanism (62) coupled between the stationary component (52) and the gearbox (50). The vibration-reducing mechanism (62) is configured to isolate a vibratory response of the gearbox (50) from the stationary component (52).

    Un ensemble de moteur de turbine (16) est décrit. Lensemble comprend un composant stationnaire (52), un arbre dentraînement (32) et une boîte dengrenages (50) couplée le long de larbre dentraînement (32) et couplée au composant stationnaire (52). Lensemble comprend également un mécanisme de réduction des vibrations (62) couplé entre le composant stationnaire (52) et la boîte dengrenages (50). Le mécanisme de réduction des vibrations (62) est conçu pour isoler une réponse vibratoire de la boîte dengrenages (50) du composant stationnaire (52).


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    Title :

    TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF


    Additional title:

    ENSEMBLE DE MOTEUR DE TURBINE ET METHODE DE FABRICATION ASSOCIEE



    Publication date :

    2017-12-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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