Method for fabricating dilution holes in ceramic matrix composite combustor panels

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United States of America Patent

PATENT NO 11149684
APP PUB NO 20200102907A1
SERIAL NO

16146818

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Abstract

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A heat shield panel for use in a combustor of a gas turbine engine is disclosed. In various embodiments, the heat shield panel includes an inner base layer, an outer base layer, and a grommet having a flange disposed between the inner base layer and the outer base layer.

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Patent Owner(s)

Patent OwnerAddress
RTX CORPORATION10 FARM SPRINGS ROAD FARMINGTON CT 06032

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dillard, Gary J Gainesville, US 18 60

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