An aircraft landing gear includes a strut leg, a bottom portion carrying at least one wheel and mounted to slide in the strut leg, and a plurality of elements such as power electric cables, signal-carrying electric cables, and hydraulic pipes extending toward the bottom portion along the strut leg and terminating at the bottom portion, all of the elements being flexible between a bottom end of the strut leg and the bottom portion of the landing gear. The landing gear includes a first movable support having a proximal end hinged to the bottom end of the strut leg, and a distal end carrying a rack for receiving and guiding the flexible elements. The landing gear also includes a second movable support having a distal end hinged to the bottom portion of the landing gear and a proximal end carrying a rack for receiving and guiding the flexible elements.


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    Title :

    ATTERRISSEUR D'AERONEF MUNI DE MOYENS DE ROUTAGE DE CABLES ET TUYAUX


    Additional title:

    AIRCRAFT LANDING GEAR PROVIDED WITH A MEANS FOR ROUTING CABLES AND PIPES
    FAHRWERK EINES LUFTFAHRZEUGS, DAS MIT ROUTING-MITTELN FÜR KABEL UND LEITUNGEN AUSGESTATTET IST


    Contributors:

    Publication date :

    2022-09-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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