Nozzle and nozzle assembly for gas turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10161266
APP PUB NO 20170082062A1
SERIAL NO

14862330

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A nozzle for a gas turbine engine, including an airfoil having an exterior surface, flange and radially compressive contact face. Also included is an airfoil support frame having a mating face positioned in engagement with the contact face. A non-orthogonal engagement angle is provided in order to transmit a compressive force to the airfoil.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC COMPANY1 NEUMANN WAY MAIL DROP F16 EVENDALE OH 45215-6301

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Albrecht,, Jr Richard William Fairfield, US 10 80
Ruthemeyer, Michael Anthony Cincinnati, US 11 130
Senile, Darrell Glenn Oxford, US 43 451

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