Modular multistage compressor system for gas turbine engines

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United States of America Patent

PATENT NO 11655757
APP PUB NO 20230032126A1
SERIAL NO

17390836

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A method of assembling a gas turbine engine is disclosed herein. The method comprises providing a set of standard axial compressor stages. Each axial compressor stage included in the set of standard axial compressor stages includes a rotor having a plurality of blades configured to rotate about an axis and a stator having a plurality of stator vanes.

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Patent Owner(s)

  • ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC.

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Iwrey, Benjamin M Indianapolis, US 6 14

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