An engine support truss assembly for aircraft includes a mounting plate having a front side and a back side opposite the front side, a truss structure mechanically coupled to the front side of the mounting plate, and a backup structure mechanically coupled to the back side of the mounting plate. The truss structure includes a plurality of structural members each including precipitation-hardened stainless steel. The backup structure is configured to provide mechanical support to the truss structure.


    Access

    Download


    Export, share and cite



    Title :

    Engine Truss for Aircraft



    Publication date :

    2023-06-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Engine truss for aircraft

    MATSON ZACHARY RICHARD / MILLER CLARK RAY / DOGGETT SHAWN DURWIN et al. | European Patent Office | 2024

    Free access

    Truss rib connecting rod and aircraft

    MA ZHIYANG / GUO JIN / HE TIREN et al. | European Patent Office | 2023

    Free access

    Truss type engine mounting structure

    LIANG LI / CHEN XIFENG / WANG FACUN et al. | European Patent Office | 2024

    Free access

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR

    ACKS JAMES | European Patent Office | 2024

    Free access

    Articulating truss configuration for aircraft landing gear

    ACKS JAMES | European Patent Office | 2024

    Free access