Turbomachinery engines with high-speed low-pressure turbines

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12152537
APP PUB NO 20240280057A1
SERIAL NO

18430317

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Abstract

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A turbomachinery engine includes a fan assembly, a low-pressure turbine, and a gearbox. The fan assembly includes a plurality of fan blades. The low-pressure turbine includes 3-5 rotating stages. The low-pressure turbine includes an area ratio equal to the annular exit area of an aft-most rotating stage of the low-pressure turbine divided by the annular exit area of a forward-most rotating stage of the low-pressure turbine. In some instances, the area ratio is within a range of 3.1-5.1.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC COMPANY1 RIVER ROAD SCHENECTADY NY 12345

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Clements, Jeffrey D Evendale, US 20 38
Kamat, Pranav R Bengaluru, IN 9 35
Mondal, Bhaskar Nanda Bengaluru, IN 60 299

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