A waiting link to support an engine on an aircraft includes a body portion including a first body portion opening, a second body portion opening, and a space therebetween. A first bearing is received in the first body portion opening and moveable in a generally vertical direction. A second bearing is received in the second body portion opening. The first and second bearings include a first and second bearing opening, respectively, that receives a first and second attachment member, respectively, that secures the body portion to a first and second structure, respectively. A cam is located in the space. The cam is pivotable between a first position and a second position. The waiting link does not provide a load path when the cam is in the first position, and when a primary load path fails, the waiting link provides the load path when the cam is in the second position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Secondary load path for gas turbine engine


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

    Erscheinungsdatum :

    2016-01-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    SECONDARY LOAD PATH FOR GAS TURBINE ENGINE

    ZHENG ZHIJUN / SANDY DAVID F | Europäisches Patentamt | 2017

    Freier Zugriff

    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 PATH

    SANDY DAVID F / ZHENG ZHIJUN | Europäisches Patentamt | 2018

    Freier Zugriff

    GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATHS

    ZHENG ZHIJUN / SANDY DAVID F | Europäisches Patentamt | 2016

    Freier Zugriff

    Secondary load path detection

    TEYSSIER GHISLAIN / PERSOUYRE FRÉDÉRIC | Europäisches Patentamt | 2020

    Freier Zugriff