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.
System and method for cooling the brakes of landing gear of an aircraft
2024-07-02
Patent
Electronic Resource
English
SYSTEM AND METHOD FOR COOLING THE BRAKES OF LANDING GEAR OF AN AIRCRAFT
European Patent Office | 2021
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