Turbomachine and turbine blade therefor

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United States of America Patent

PATENT NO 9957805
APP PUB NO 20170175530A1
SERIAL NO

14973894

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Abstract

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A blade has an airfoil, and the blade is configured for use with a turbomachine. The airfoil has a throat distribution measured at a narrowest region in a pathway between adjacent blades, at which adjacent blades extend across the pathway between opposing walls to aerodynamically interact with fluid flow. The airfoil defines the throat distribution, and the throat distribution reduces aerodynamic loss and improves aerodynamic loading on the airfoil. The airfoil has a linear trailing edge profile.

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Patent Owner(s)

Patent OwnerAddress
GE INFRASTRUCTURE TECHNOLOGY LLC300 GARLINGTON ROAD GREENVILLE SC 29615

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Chouhan, Rohit Karnataka, IN 52 278
Gustafson, Ross James York, US 11 115
Neville, Jason Adam Greenville, US 10 59
Soni, Sumeet Karnataka, IN 11 93

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