An assembly for mounting a turbine engine to a pylon includes a mounting beam, a plurality of fasteners, a first mounting linkage and a second mounting linkage. The mounting beam includes a mount beam fitting that extends axially between a first mount beam end and a second mount beam end, and a mount beam flange that extends radially out from the mount beam fitting at the first mount beam end. A first fastener aperture extends radially through the mount beam fitting, and a second fastener aperture extends axially through the mount beam flange. The fasteners connect the mounting beam to the pylon. A first of the fasteners is mated with the first fastener aperture, and a second of the fasteners is mated with the second fastener aperture. The first mounting linkage connects the first mount beam end to a first engine attachment. The second mounting linkage connects the second mount beam end to second engine attachments.


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    Titel :

    ASSEMBLY FOR MOUNTING A TURBINE ENGINE TO A PYLON


    Weitere Titelangaben:

    ANORDNUNG ZUR BEFESTIGUNG EINES TURBINENTRIEBWERKS AN EINEM PYLON
    ENSEMBLE DE MONTAGE D'UN MOTEUR À TURBINE SUR UN PYLÔNE


    Beteiligte:
    SANDY DAVID F (Autor:in) / ZHENG ZHIJUN (Autor:in) / DAILEY STEPHEN P (Autor:in) / FOSTER JOSEPH P (Autor:in)

    Erscheinungsdatum :

    05.06.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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