An integrated asymmetric brake system for an aircraft includes a housing and a control surface actuator arranged in the housing. The control surface actuator includes a torque limiter output member and is operable to selectively deploy and retract a control surface. An asymmetry brake system is arranged in the housing and is operably connected to the control surface actuator and the torque limiter output member. The asymmetry brake system is selectively operable to prevent deployment of the control surface by activating the torque limiter output member upon detecting an asymmetry event. An asymmetry brake test monitor switch is mounted in the housing and operably coupled to the asymmetry brake system. The asymmetry brake test monitor switch is monitored to confirm functionality of the asymmetry brake system prior to flight.


    Access

    Download


    Export, share and cite



    Title :

    Integrated assymmetry brake mechanism


    Contributors:

    Publication date :

    2023-10-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    INTEGRATED ASSYMETRY BRAKE MECHANISM

    BARGER VICTOR | European Patent Office | 2022

    Free access

    INTEGRATED ASSYMETRY BRAKE MECHANISM

    BARGER VICTOR | European Patent Office | 2024

    Free access

    INTEGRATED ASSYMETRY BRAKE MECHANISM

    BARGER VICTOR | European Patent Office | 2022

    Free access

    PARKING BRAKE MECHANISM INTEGRATED WITH PNEUMATIC TRAILER BRAKE

    CENGIZ CAGAN / YETKIN EMRE / KARS HAKAN et al. | European Patent Office | 2016

    Free access

    DRIVING AXLE ASSEMBLY AND SERVICE BRAKE AND PARKING BRAKE INTEGRATED MECHANISM THEREOF

    DONG HONGPENG / XU DELIANG / LUO HONGPING et al. | European Patent Office | 2025

    Free access