Cooling system for power cables in a gas turbine engine
A cooling system for a plurality of conductive cables in a gas turbine engine includes a cooling source and an electric motor disposed in a tail cone. The cooling source may comprise an electric fan or an oil pump. The cooling source may be configured for active cooling of the plurality of conductiv...
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Main Author | |
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Format | Patent |
Language | English |
Published |
23.07.2024
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Subjects | |
Online Access | Get full text |
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Summary: | A cooling system for a plurality of conductive cables in a gas turbine engine includes a cooling source and an electric motor disposed in a tail cone. The cooling source may comprise an electric fan or an oil pump. The cooling source may be configured for active cooling of the plurality of conductive cables. The electric fan may be in fluid communication with ambient air during operation of the gas turbine engine. |
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Bibliography: | Application Number: US202318333443 |