An aircraft rear engine attachment connecting a primary structure of a pylon and an engine of an aircraft. The rear engine attachment includes first and second rods, each of them including at least two parts, a first part including at least one support orifice, accommodating a support link bar, configured to connect the rod directly or indirectly to the primary structure, at least one second part including at least one engine orifice, accommodating an engine link bar, configured to connect the rod directly or indirectly to the engine, and also detachable link elements for connecting the first and second parts oriented parallel to the direction of the rod.


    Access

    Download


    Export, share and cite



    Title :

    Rear engine attachment of an aircraft having two-part rods and aircraft comprising at least one such rear engine attachment


    Contributors:

    Publication date :

    2022-12-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen




    REAR ENGINE ATTACHMENT FOR AN AIRCRAFT ENGINE

    COMBES STÉPHANE / GELIOT JEAN / DEFORET THOMAS et al. | European Patent Office | 2019

    Free access

    REAR ENGINE ATTACHMENT FOR AN AIRCRAFT ENGINE

    VAYSSIERES MANON / BERJOT MICHAEL | European Patent Office | 2020

    Free access

    Rear engine attachment for an aircraft engine

    VAYSSIERES MANON / BERJOT MICHAEL | European Patent Office | 2022

    Free access

    Rear engine attachment for an aircraft engine

    COMBES STÉPHANE / GELIOT JEAN / DEFORET THOMAS et al. | European Patent Office | 2020

    Free access