Bleed air driven vapor cycle system
AssigneeRolls-Royce North American Technologies Inc.
InventorsTimothy Unton, Eric S. Donovan
Life of this patent
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AssigneeRolls-Royce North American Technologies Inc.
InventorsTimothy Unton, Eric S. Donovan
Estimating the term…
A cooling system may comprise a vapor cycle system. The cooling system may comprise a gas turbine engine. The vapor cycle system may include a compressor, a heat exchanger downstream from the compressor, and a heat load downstream from the heat exchanger and upstream of the compressor. The cooling system may comprise a bleed air conduit. The bleed air conduit may be configured to receive bleed air from the gas turbine engine. The cooling system may comprise a bleed turbine driven by the bleed air supplied from the bleed air conduit. The bleed turbine may be configured to drive the compressor of the vapor cycle system. The compressor may be connected to a bleed turbine via a shaft. The cooling system may comprise a throttle valve to control a flow of the bleed air through the bleed air conduit.
A cooling system comprising:
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A method of cooling a heat load, the method comprising:
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A system comprising:
Dependencies are inferred from the claim text.