Composite filled gas turbine engine blade with gas film damper

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United States of America Patent

PATENT NO 7278830
APP PUB NO 20060263222A1
SERIAL NO

11131570

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A gas turbine engine blade comprises a housing, a composite core located within the housing, and a gas damper located within the housing for damping vibration of the blade.

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Patent Owner(s)

Patent OwnerAddress
ALLISON ADVANCED DEVELOPMENT COMPANY INCP O BOX 7162 INDIANAPOLIS IN 46206-7162

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Vetters, Daniel K Indianapolis, IN 94 1006

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