The present disclosure relates to a thrust reverser device for a turbo jet engine nacelle including a fixed thrust reverser support structure having a longitudinal support half beam able to support a thrust reverser half-cowl, and the thrust reverser half-cowl mounted such that it can slide on the fixed structure in a direction substantially parallel to a longitudinal axis of the device via a guidance assembly, between a direct-jet position and a reverse-thrust position. In particular, the fixed structure includes a structure for offsetting the guidance assembly that guides the half-cowl circumferentially in a plane radial to the longitudinal axis between its various positions with respect to the half-beam on which the half-cowl is mounted.


    Access

    Download


    Export, share and cite



    Title :

    Fixed structure of a thrust reverser device


    Contributors:

    Publication date :

    2020-01-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    FIXED STRUCTURE OF A THRUST REVERSER DEVICE

    BUNEL SERGE / BELLANGER ALEXANDRE | European Patent Office | 2016

    Free access

    Thrust reverser-integrated track beam and inner fixed structure

    SORIA CHRISTIAN / CHIOU SONG / LAYLAND MICHAEL J et al. | European Patent Office | 2018

    Free access

    THRUST REVERSER

    HIGGINS ROGER | European Patent Office | 2017

    Free access

    THRUST REVERSER ACTUATING

    KOPECEK JOSEPH THOMAS / SWEET JULIAN | European Patent Office | 2017

    Free access

    THRUST REVERSER SYSTEM

    BOL ERIC D | European Patent Office | 2017

    Free access