Separable blade platform

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 7284958
APP PUB NO 20070189901A1
SERIAL NO

10799223

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A gas turbine engine blade platform including a par of platform retention members. The pair of platform retention members are configured to be located on opposite sides of a disk lug. The retention members interact with the disk lug to restrain radial movement of the platform during rotation of a disk.

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Patent Owner(s)

Patent OwnerAddress
ALLISON ADVANCED DEVELOPMENT COMPANYP O BOX 7162 INDIANAPOLIS IN 46206

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dundas, Jason E Post Falls, ID 2 57
Freeman, Ted J Avon, IN 191 1843

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