An aircraft landing gear (10) includes an axle (18b) on which wheel and brake assemblies (20b, 22b) are mounted. An adaptor member (30) is mounted on the axle and arranged to define a brake rod connection point (26b) that is distinct from a conventional brake rod connection point (26b') defined by the brake assembly. The adaptor member is coupled to the brake assembly via an adaptor linkage (32) that is arranged to react brake torque but arranged to permit relative movement between the adaptor member and the brake assembly in degrees of freedom which are not required to react brake torque.

    Un train datterrissage daéronef (10) comprend un essieu (18b) sur lequel sont montés des ensembles roue et frein (20b, 22b). Un élément adaptateur (30) est monté sur lessieu et agencé pour définir un point de raccordement de tige de frein (26b) qui est distinct dun point de connexion de tige de frein classique (26b) défini par lensemble frein. Lélément adaptateur est couplé à lensemble frein par lintermédiaire dune liaison dadaptateur (32) qui est conçue pour faire réagir un couple de freinage, mais agencée pour permettre un mouvement relatif entre lélément adaptateur et lensemble frein dans des degrés de liberté qui ne sont pas nécessaires pour faire réagir le couple de freinage.


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    Title :

    AIRCRAFT LANDING GEAR ASSEMBLY


    Additional title:

    MECANISME DE TRAIN D'ATTERRISSAGE D'AERONEF


    Contributors:

    Publication date :

    2021-03-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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