A landing gear system (102, 202) for an aircraft (104, 200) is presented. The landing gear system (102, 202) includes a composite flex beam (106, 204, 500, 702, 802, 902) having through-thickness stitching (108, 906, 1002) and a curvature (110, 206) having a radius (112, 208) greater than 5 inches (12.7 centimeters) and a trunnion (114, 402, 404, 506, 508, 808) connected to the composite flex beam (106, 204, 500, 702, 802, 902) and offset (116, 410, 412, 810) from a neutral plane (118) of the composite flex beam (106, 204, 500, 702, 802, 902).


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    Title :

    Система шасси с композитной упругой балкой


    Publication date :

    2021-09-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge