A landing gear (0) for an aircraft comprising a wheel (R), a system (1) for rotationally driving the wheel that is mobile between a clutched position and a safety position by passing through a declutched position, and a manoeuvring system (3) to displace the driving system (1) between its declutched and clutched positions. The gear comprises an elastic return (4) for returning the driving system (1) to its safety position and first and second abutments (51a, 52a) that are separated as long as the driving system (1) is away from its safety position and in contact with one another when the driving system (1) is in safety position. The first and second abutments (51a, 52a) oppose the passing of the driving system (1) from its safety position to its declutched position when the abutments are in contact with one another.


    Access

    Download


    Export, share and cite



    Title :

    LOCKABLE WHEEL ACTUATOR DISENGAGEMENT SYSTEM ON AN AIRCRAFT LANDING GEAR


    Contributors:

    Publication date :

    2017-09-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



    Lockable wheel actuator disengagement system on an aircraft landing gear

    BELLENGER VINCENT | European Patent Office | 2020

    Free access

    AIRCRAFT LANDING GEAR ACTUATOR

    COLLINS ANDREW JOHN | European Patent Office | 2015

    Free access

    Aircraft landing gear aircraft wheel synchronizer

    YANG AO | European Patent Office | 2020

    Free access

    Aircraft landing gear unlock actuator

    COLLINS ANDREW JOHN | European Patent Office | 2018

    Free access

    AIRCRAFT LANDING GEAR WHEEL-DRIVE SYSTEM

    LO CHARLES / STEVES ALLAN | European Patent Office | 2017

    Free access