PROBLEM TO BE SOLVED: To provide systems and methods of reducing vibratory responses induced into at least one of an engine and an airframe from a gearbox assembly.SOLUTION: A turbine engine 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, and configured to isolate a vibratory response of the gearbox 50 from the stationary component 52.SELECTED DRAWING: Figure 2

    【課題】ギヤボックス組立体からエンジン及び機体の少なくとも一方に誘発される振動応答を低減するシステム及び方法を提供すること。【解決手段】タービンエンジン組立体は、静止構成要素52と、駆動シャフト32と、駆動シャフト32に沿って結合されると共に静止構成要素52に結合されたギヤボックス50とを含む。また、この組立体は、静止構成要素52とギヤボックス50との間に結合され、ギヤボックス50の振動応答を静止構成要素52から遮断するように構成された振動低減機構62を含む。【選択図】図2


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    Title :

    TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THE SAME


    Additional title:

    タービンエンジン組立体及びその製造方法



    Publication date :

    2016-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    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 / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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