GAS TURBINE ENGINE COMPRESSOR IMPELLER COOLING AIR SINKS
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Sep 13, 2016
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Sep 8, 2016
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Abstract
A gas turbine engine includes devices, systems, and methods for providing bleed air from the compressor impeller to the turbine for cooling and/or other use. The bleed air may include compressor cooling air that is routed through the diffuser and external to an outer bypass duct and/or internally to a forward wheel cavity of the turbine.
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