Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor

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United States of America Patent

PATENT NO 10655853
APP PUB NO 20180231250A1
SERIAL NO

15348639

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Abstract

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A combustor for a gas turbine engine including a forward liner panel mounted to a support shell via a multiple of studs, the forward liner panel including an aft non-linear circumferential edge and an aft liner panel mounted to the support shell via a multiple of studs, the aft liner panel including a forward non-linear circumferential edge that is complementary to the aft non-linear circumferential edge.

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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
Burd, Steven W Cheshire, US 76 841

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