INTEGRATED AUXILIARY COMPRESSORS FOR COOLING IN GAS TURBINE ENGINES

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20250043725A1
SERIAL NO

18228649

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Abstract

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A gas turbine engine including an auxiliary compressor for pressuring cooling air delivered to turbine section components is disclosed. The auxiliary compressor is configured to increase the pressure of compressed air received from a primary compressor prior to movement of the compressed air to cooling air passageways of the turbine system.

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Humes, Ryan C Indianapolis, US 28 46
Unton, Timothy Indianapolis, US 29 39

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