Thermal control systems for aircraft landing gear wheel wells and related methods
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United States of America Patent
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Mar 5, 2024
Grant Date -
Nov 18, 2021
app pub date -
May 15, 2020
filing date -
May 15, 2020
priority date (Note) -
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Abstract
Thermal control system for aircraft main landing gear wheel wells and related methods are disclosed. An example thermal control system includes a conduit defining a fluid passageway between an inlet and an outlet. The inlet of the conduit positioned in fluid communication with a landing gear wheel well and the outlet of the conduit positioned in fluid communication with the atmosphere. The conduit generates a pressure differential through the fluid passageway between the inlet and the outlet to exhaust heat from the landing gear wheel well to the atmosphere.
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