Gas turbine engine with power density range

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 11970984
APP PUB NO 20230383699A1
SERIAL NO

18107126

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Abstract

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A gas turbine engine includes a propulsor section including a propulsor, a compressor section including a first compressor and a second compressor, a geared architecture, a turbine section including a first turbine and a drive turbine, and a power density of greater than or equal to 4.75 and less than or equal to 5.5 lbf/in3, wherein the power density is a ratio of a thrust provided by the engine to a volume of the turbine section.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Kupratis, Daniel Bernard Wallingford, US 197 1812
Schwarz, Frederick M Glastonbury, US 446 5139

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