Tapered part-span shroud

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9546555
APP PUB NO 20140169974A1
SERIAL NO

13717265

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A rotatable blade for use in a turbomachine includes an airfoil portion having a leading edge, a trailing edge a radially-inner end and a radially-outer end; a root section at to the radially-inner end of the airfoil portion, and a part-span shroud located on the airfoil portion between the root section and the radially-outer end. The part-span shroud decreases in width and thickness from decreasing in width and thickness from the airfoil portion to a contact surface adapted to engage a mating contact surface on a part-span shroud of an adjacent blade.

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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
Davis, Holly Renae Greenville, US 4 63
Valliappan, Lakshmanan Karnataka, IN 11 32

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