Vane assembly for a gas turbine engine

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United States of America Patent

PATENT NO 8834109
APP PUB NO 20130034434A1
SERIAL NO

13196969

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Abstract

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A vane assembly for a gas turbine engine includes a first vane and a second vane. The first vane and the second vane include an inner platform, an outer platform and an airfoil that extends between the inner platform and the outer platform. The first vane and the second vane are attached at least at one of their inner platforms or their outer platforms with a first attachment mechanism and a second attachment mechanism.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Propheter-Hinckley, Tracy A Manchester, US 240 1816

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