Gas turbine engine components with film cooling holes having cylindrical to multi-lobe configurations

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United States of America Patent

PATENT NO 9650900
APP PUB NO 20130294889A1
SERIAL NO

13465647

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Abstract

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An engine component includes a body; and a plurality of cooling holes formed in the body, at least one of the cooling holes having a multi-lobed shape with at least a first lobe, a second lobe, and a third lobe.

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Patent Owner(s)

  • HONEYWELL INTERNATIONAL INC.

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Chou, David Phoenix, US 42 747
Liu, Jong Scottsdale, US 8 147
Malak, Malak Fouad Tempe, US 21 273
Rana, Rajiv Tempe, US 9 108
Tapia, Luis Maricopa, US 13 170

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