Non-planar combustor liner panel for a gas turbine engine combustor

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United States of America Patent

PATENT NO 10935235
APP PUB NO 20180231248A1
SERIAL NO

15348568

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Abstract

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A combustor for a gas turbine engine including a liner panel mounted to a support shell via a multiple of studs, the liner panel including a forward section and an aft section that defines an angle therebetween in the axial profile between the forward section and the aft section.

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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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