A lockable actuator has lock segments that move into recesses inside a piston to enable the piston to move. The lock segments may also move radially outwardly from the recesses in the piston to engage a bevel edge of a cylinder housing assembly to lock the piston. Lock rams having ramps force the lock segments radially outwardly into engagement with the bevel edge of the cylinder housing assembly.


    Access

    Download


    Export, share and cite



    Title :

    Dual locking hydraulic actuator for structural brace


    Contributors:

    Publication date :

    2018-04-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / B64C AEROPLANES , Flugzeuge



    DUAL LOCKING HYDRAULIC ACTUATOR FOR STRUCTURAL BRACE

    LEE V-BOND / COLANTONIO DAVID | European Patent Office | 2017

    Free access

    DUAL LOCKING HYDRAULIC ACTUATOR FOR STRUCTURAL BRACE

    LEE V-BOND / COLANTONIO DAVID | European Patent Office | 2016

    Free access

    LANDING GEAR FOLDING BRACE WITH LOCKING ACTUATOR

    ACKS JAMES / REBER KOREY MICHAEL | European Patent Office | 2018

    Free access

    Landing gear folding brace with locking actuator

    ACKS JAMES / REBER KOREY MICHAEL | European Patent Office | 2019

    Free access

    LANDING GEAR FOLDING BRACE WITH LOCKING ACTUATOR

    ACKS JAMES / REBER KOREY MICHAEL | European Patent Office | 2020

    Free access