A landing gear arrangement may comprise a shock strut, a retraction actuator, and a shrink actuator. The retraction actuator may move the shock strut between a stowed position and a deployed position. The shrink actuator may move between a shrink position and an unshrink position in response to the shock strut moving between the stowed position and the deployed position.


    Access

    Download


    Export, share and cite



    Title :

    LANDING GEAR ARRANGEMENT WITH PASSIVE SHOCK STRUT SHRINK ACTUATOR


    Contributors:

    Publication date :

    2018-03-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



    LANDING GEAR ARRANGEMENT WITH PASSIVE SHOCK STRUT SHRINK ACTUATOR

    LUCE WILLIAM E | European Patent Office | 2020

    Free access

    Landing gear arrangement with passive shock strut shrink actuator

    LUCE WILLIAM E | European Patent Office | 2019

    Free access

    LANDING GEAR ARRANGEMENT WITH PASSIVE SHOCK STRUT SHRINK ACTUATOR

    LUCE WILLIAM E | European Patent Office | 2018

    Free access


    Shrink strut landing gear system

    LUCE WILLIAM E | European Patent Office | 2019

    Free access