Cooling passages for gas turbine engine component

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 10526897
APP PUB NO 20170089204A1
SERIAL NO

14870175

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A gas turbine engine component includes a wall portion that includes a first side and a second opposite side. A plurality of passages extends between the first side of the wall portion and the second side of the wall portion and includes a plurality of inlets located on the first side of the wall portion. A plurality of outlets are located on a second side of the wall portion. The plurality of outlets include a first plurality of outlets located on a first side of the plurality of inlets and a second plurality of outlets located on a second side of the plurality of inlets.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Lutjen, Paul M Kennebunkport, US 137 1116
Swift, Anthony B North Waterboro, US 13 78

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