Transition Duct Exit Holder and Inlet Ring Support Arrangement

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United States of America Patent

APP PUB NO 20180017259A1
SERIAL NO

15208265

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A gas turbine engine has a transition duct supporter that is able to support and accommodate the operation of the gas turbine engine. The transition duct supporter is located between a metallic integrated exit piece and a transition duct that is made of ceramic matrix composites.

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Patent Owner(s)

Patent OwnerAddress
SIEMENS ENERGY INC4400 ALAFAYA TRAIL ORLANDO FL 32826

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Schiavo, Anthony L Oviedo, US 26 768

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