Centrifical compressor assembly for a gas turbine engine

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United States of America Patent

PATENT NO 11578654
SERIAL NO

17360653

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Importance

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Abstract

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A compressor adapted for use in a gas turbine engine includes an impeller, a diffuser, and a deswirler. The impeller is arranged circumferentially about an axis and configured to rotate about the axis. The diffuser is arranged circumferentially around the impeller to receive the air from the impeller. The deswirler is configured to receive the air from the diffuser and to conduct the air into a combustion chamber.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INCINDIANAPOLIS IN

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Eifert, Andrew J Indianapolis, US 23 78
Humes, Ryan C Indianapolis, US 28 46

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