A system for cooling the brakes of a brake system of a landing gear of an aircraft, including: a compressor configured to generate a pressurized airflow, the compressor including at least one air outlet, and an air jet pump including: a pump tube including a first end connected to the air outlet and a second end, the pump tube being designed to carry the pressurized airflow between the first and second ends, and a plurality of injectors connected to the second end of the pump tube, and configured to inject the pressurized airflow.


    Access

    Download


    Export, share and cite



    Title :

    System and method for cooling the brakes of landing gear of an aircraft


    Contributors:

    Publication date :

    2024-07-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF



    Active cooling system for landing gear brakes

    KIRKBRIDE DAVID W | European Patent Office | 2022

    Free access

    Active Cooling System for Landing Gear Brakes

    KIRKBRIDE DAVID W | European Patent Office | 2021

    Free access

    SYSTEM AND METHOD FOR COOLING THE BRAKES OF LANDING GEAR OF AN AIRCRAFT

    FONTALBAT THIERRY / CHALLAS FLORENT / ORLANDINI FABIEN | European Patent Office | 2021

    Free access

    LANDING GEAR OF AN AIRCRAFT AND METHOD FOR COOLING AN ELECTRIC TAXIING MOTOR AND BRAKES OF SUCH A LANDING GEAR

    FONTALBAT THIERRY / BLANCO LOIC / CASSAGNET CHRISTOPHE et al. | European Patent Office | 2022

    Free access

    LANDING GEAR OF AN AIRCRAFT AND METHOD FOR COOLING AN ELECTRIC TAXIING MOTOR AND BRAKES OF SUCH A LANDING GEAR

    FONTALBAT THIERRY / BLANCO LOIC / CASSAGNET CHRISTOPHE et al. | European Patent Office | 2020

    Free access