A thrust reverser with grids includes a jet engine pylon, a one piece cowl either directly or indirectly slidably mounted on the jet engine pylon between a direct jet position and a reverse jet position, and a system for locking this cowl on a beam. The system has a single tertiary lock, which is positioned on one side of the jet engine pylon being capable of locking a corresponding upper edge of the cowl. In addition, the tertiary lock includes a locker to lock the cowl, a blocker for blocking the locker, and a position detector in order to detect the position of the locker. The system further includes another detector to detect proper closing of the other upper edge of the cowl.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft turbojet engine thrust reverser with a reduced number of latches


    Contributors:

    Publication date :

    2016-10-25


    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



    Aircraft turbojet engine comprising two thrust reverser modules

    LESCOUP JÉRÔME | European Patent Office | 2023

    Free access

    Grid-type thrust reverser for turbojet engine

    GRALL LOÏC / HEAU ALEXIS / BREBION BENJAMIN et al. | European Patent Office | 2022

    Free access

    Thrust reverser for a nacelle of an aircraft turbojet engine

    MORADELL-CASELLAS PIERRE | European Patent Office | 2019

    Free access

    Aircraft engine thrust reverser

    Emerald Group Publishing | 1998


    Automatic deflection limiting latches for a thrust reverser

    PRETTY MICHAEL SEAN / MOULE JOHN / ZECCA JOSEPH C | European Patent Office | 2017

    Free access