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US 2025/0051027 A1Published application
Coolant wing surface heat exchanger
AssigneeGoodrich Corporation
InventorGrzegorz KRUCZEK
Life of this patent
Estimating the term…
Abstract
An aircraft wing incorporating a coolant loop through which a coolant flows. The coolant loop is a closed loop and a part of the closed loop is formed within a body of the aircraft wing. Aircraft and other systems are also disclosed as well a parts that can be cooled.
Claims14
A method of removing heat from a coolant in a closed coolant loop, the method comprising:
- integrating part of the closed coolant loop in the body of an aircraft wing;
- and
- passing the coolant, as part of the coolant loop, through the body of the aircraft wing.
An aircraft wing comprising:
- a coolant loop through which a coolant flows, wherein the coolant loop is a closed loop, and wherein a part of the closed loop is formed within a body of the aircraft wing.
The aircraft wing of 3, wherein the coolant loop is formed by spars along the aircraft wing.
Dependencies are inferred from the claim text.