Disclosed is a linkage assembly for a gas turbine engine having a link having a first end, a second end, and a rod extending therebetween, the first end having a first sliding bearing disposed within a first sliding bearing housing, a fastener comprising a first flange and a second flange, a pin extending between the first flange and the second flange, wherein the first sliding bearing is pivotally connected to the pin; and a biasing member secured between the first flange and the sliding bearing housing, the biasing member contacting the sliding bearing housing and biasing the link against rotation about a center axis for the rod of the link.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LINKAGE ASSEMBLY


    Beteiligte:

    Erscheinungsdatum :

    14.03.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Linkage assembly

    KOLLATH MICHAEL D / BERING CHRISTOPHER A / HUDSON SCOTT A et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    LINKAGE ASSEMBLY

    SIMPSON ALEX J / KNOWLTON ROBERT T | Europäisches Patentamt | 2021

    Freier Zugriff

    LINKAGE ASSEMBLY

    KOLLATH MICHAEL D / BERING CHRISTOPHER A / HUDSON SCOTT A et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    LINKAGE ASSEMBLY

    SIMPSON ALEX J / KNOWLTON ROBERT T | Europäisches Patentamt | 2020

    Freier Zugriff

    SWAYBAR LINKAGE ASSEMBLY

    PARKER GLEN C / SCHRIEBER DUSTIN / AUQUIER ANDREW LOUIS et al. | Europäisches Patentamt | 2021

    Freier Zugriff