A system (101) for use with a landing gear (100) of an aircraft (10) includes a drag brace assembly (102) having an upper end (108) configured to be rotatably coupled to the aircraft and a lower end (110) configured to be rotatably coupled to a shock strut of the landing gear. The system further includes a jury linkage (114) having a brace portion (116) configured to be pivotally coupled to the drag brace assembly and a strut portion (118) pivotally coupled to the brace portion and configured to be rotatably coupled to the shock strut.


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    Title :

    SIDE FOLDING AND REFORMING LINKAGE FOR LANDING GEAR


    Additional title:

    SEITENFALT- UND -UMFORMUNGSGELENK FÜR FAHRWERK
    LIAISON DE PLIAGE ET DE REFORMAGE LATÉRAL POUR TRAIN D'ATTERRISSAGE


    Contributors:

    Publication date :

    2021-05-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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