Gas turbine engine front section

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12247493
APP PUB NO 20230042974A1
SERIAL NO

17969179

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Importance

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Abstract

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A gas turbine engine includes, among other things, a propulsor section including a propulsor hub, the hub including a hub diameter supporting a plurality of propulsor blades. A compressor section includes a first compressor and a second compressor. A turbine section includes a first turbine and a second turbine. A geared architecture interconnects the first turbine and the propulsor hub. The geared architecture includes a gear volume. A compressor inlet passage is disposed annularly about the geared architecture.

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Patent Owner(s)

  • RTX CORPORATION

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Schwarz, Frederick M Glastonbury, US 446 5139
Sheridan, William G Southington, US 276 6115

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