A connection for mounting an aircraft engine (20) to an aircraft pylon (62) has a plate (102) to be bolted to a portion (60) of an aircraft engine (20), and a body (104) extending rearwardly from the plate (102). The body (104) has a main pivot attachment (106) to a balance beam (108), which has thrust links (110) pivotally attached to the balance beam (108). A back-up connection (112) is included between the balance beam (108) and the body (104) such that the back-up connection (112) allows normal pivoting movement of the balance beam (108) relative to the body (104) without contact at the back-up connection (112).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATH


    Weitere Titelangaben:

    GASTURBINENMOTORMONTAGESTRUKTUR MIT SEKUNDÄREM LASTPFAD
    STRUCTURE DE MONTAGE DE MOTEUR À TURBINE À GAZ AVEC TRAJET DE CHARGE SECONDAIRE


    Beteiligte:
    SANDY DAVID F (Autor:in) / ZHENG ZHIJUN (Autor:in)

    Erscheinungsdatum :

    2018-07-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Gas turbine engine mounting structure with secondary load path

    SANDY DAVID F / ZHENG ZHIJUN | Europäisches Patentamt | 2017

    Freier Zugriff

    GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATHS

    ZHENG ZHIJUN / SANDY DAVID F | Europäisches Patentamt | 2016

    Freier Zugriff

    Secondary load path for gas turbine engine

    ZHENG ZHIJUN / SANDY DAVID F | Europäisches Patentamt | 2016

    Freier Zugriff

    SECONDARY LOAD PATH FOR GAS TURBINE ENGINE

    ZHENG ZHIJUN / SANDY DAVID F | Europäisches Patentamt | 2017

    Freier Zugriff

    GAS TURBINE ENGINE MOUNTING RING

    ELEFTHERIOU ANDREAS / LECLAIR DENIS / DENIS DAVID et al. | Europäisches Patentamt | 2021

    Freier Zugriff