A method of making a thin-skin support member, comprising: forging a mounting interface (608); forging a mid-body support (504) having a cylinder (606) extending from the mid-body support; and welding sheet metal (700, 702, 704, 706) to the mid-body support and the mounting interface


    Access

    Download


    Export, share and cite



    Title :

    AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE


    Additional title:

    VERRINGERUNG VON AERODYNAMISCHEM LÄRM DURCH DÜNNWANDIGE FAHRWERKSTRUKTUR
    RÉDUCTION DU BRUIT AÉRODYNAMIQUE D'UNE STRUCTURE DE TRAIN D'ATTERRISSAGE À FINE PELLICULE


    Contributors:

    Publication date :

    2021-05-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE

    HIMMELMANN RICHARD A | European Patent Office | 2017

    Free access

    Aerodynamic noise reducing thin-skin landing gear structure

    HIMMELMANN RICHARD A | European Patent Office | 2021

    Free access

    AERODYNAMIC NOISE REDUCING THIN-SKIN LANDING GEAR STRUCTURE

    HIMMELMANN RICHARD A | European Patent Office | 2019

    Free access

    Aerodynamic noise reducing thin-skin landing gear structure

    HIMMELMANN RICHARD A | European Patent Office | 2019

    Free access

    AERODYNAMIC NOISE REDUCTION THIN-SKIN LANDING GEAR STRUCTURE

    HIMMELMANN RICHARD A | European Patent Office | 2024

    Free access