A landing gear (100A, 100B) including an outer cylinder (110) rotatably coupled to a frame of an aircraft (1000) about a trunnion axis of rotation, a shock strut assembly (120) movably coupled to the outer cylinder (110) so as to reciprocate along a longitudinal axis (115) of the outer cylinder, and a shrink mechanism (130A, 130B) including a first shrink link member (140) pivotally coupled to the outer cylinder, a second shrink link member (150) coupling the first shrink link member to the shock strut assembly (120), a crank member (160) pivotally coupled to the outer cylinder (110), a drive member (170) coupling the crank member (160) to a walking beam (210) of a landing gear retract mechanism (200), and a driven member (180) coupling the crank member (160) to the first shrink link member (140).


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    Title :

    LANDING GEAR SHRINK LINK MECHANISM


    Additional title:

    SCHRUMPFVERBINDUNGSMECHANISMUS FÜR FAHRWERK
    MÉCANISME DE LIAISON RÉTRACTABLE DE TRAIN D'ATTERRISSAGE



    Publication date :

    2021-06-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR SHRINK LINK MECHANISM

    ALLEY CHRISTOPHER M / CAMPBELL LEANNE M / DEFRANCISCI GABRIELA K et al. | European Patent Office | 2021

    Free access

    LANDING GEAR SHRINK LINK MECHANISM

    ALLEY CHRISTOPHER M / CAMPBELL LEANNE M / DEFRANCISCI GABRIELA K et al. | European Patent Office | 2023

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    Landing gear shrink link mechanism

    ALLEY CHRISTOPHER M / CAMPBELL LEANNE M / DEFRANCISCI GABRIELA K et al. | European Patent Office | 2023

    Free access

    LANDING GEAR SHRINK LINK MECHANISM

    CHRISTOPHER M ALLEY / LEANNE M CAMPBELL / GABRIELA K DEFRANCISCI et al. | European Patent Office | 2020

    Free access

    LANDING GEAR SHRINK LINK MECHANISM

    ALLEY CHRISTOPHER M / CAMPBELL LEANNE M / DEFRANCISCI GABRIELA K et al. | European Patent Office | 2020

    Free access