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US 2025/0060047 A1Published application
Fluid discharge system
AssigneeTusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi
InventorBerke ALP MIRZA
Life of this patent
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Abstract
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).
Claims14
A fluid discharge system comprising a body located on the aircraft, at least one tank (T) that is located on the body and allows fuel to be accumulated in it;
- at least one valve that allows the water accumulated in the tank (T) to be discharged out of the body;
- at least one fastener that enables the valve to be mounted on the body;
- and a shell(S) located on the air-contacting surface of the body, wherein a reservoir that is removably installed between the tank (T) and the shell(S) and protects the valve by surrounding it;
- and an apparatus that is located between the reservoir and the shell(S) and allows the reservoir to be removed from the shell(S) by the user.
1 more element
Dependencies are inferred from the claim text.