Airfoil with leading edge reinforcement

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 9470097
APP PUB NO 20150044056A1
SERIAL NO

14094313

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A leading edge member for a composite vane of a gas turbine engine. The leading edge member includes a first leg and a second leg. The first leg includes a proximal end joined to a proximal end of the second leg.

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Patent Owner(s)

  • ROLLS-ROYCE CORPORATION

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hodgson, Benedict N Indianapolis, US 12 47
Rivers, Jonathan M Indianapolis, US 13 48

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