Thermally free liner retention mechanism

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United States of America Patent

PATENT NO 9897317
SERIAL NO

14038038

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Abstract

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The present invention discloses a novel and improved device and method for securing a combustion liner within a gas turbine combustor. The improved configuration comprises a plurality of equally spaced support tab assemblies secured about the combustion liner and positioned radially outward of the combustion zone. The support tab assemblies comprise parallel liner tabs which provide increased flexibility, greater structural support, and lower operating stresses.

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Patent Owner(s)

Patent OwnerAddress
H2 IP UK LIMITED27 OLD GLOUCESTER STREET LONDON WC1N 3AX

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Jorgensen, Stephen Palm City, US 9 95
Rizkalla, Hany Stuart, US 32 535
Stuttaford, Peter John Jupiter, US 27 228

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