This invention relates to a body (2) located on the aircraft, at least one tank (T) located on the body (2) and allows fuel accumulation, at least one valve (3) that allows the water accumulated in the tank (T) to be discharged out of the body (2), at least one fastener (4) that enables the valve (3) to be mounted on the body (2), and a shell(S) located on the air-contacting surface of the body (2).
FLUID DISCHARGE SYSTEM
2025-02-20
Patent
Electronic Resource
English