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Transition Duct Support Arrangement for a Gas Turbine Engine

United States Patent Application

20180016922
A1
View the Complete Application at the US Patent & Trademark Office
A gas turbine engine has a crown locking device and a seal portion. The crown locking device and seal portion connect a transition duct to an inlet extension piece. The crown locking device and seal portion is located between a metallic integrated exit piece and a transition duct that is made of ceramic matrix composites.
Schiavo, Anthony L. (Oviedo, FL)
15/ 208,219
July 12, 2016
STATEMENT REGARDING FEDERALLY SPONSORED DEVELOPMENT [0001] This invention was made with government support under Program DE-FE0023955, awarded by the United States Department of Energy. The government has certain rights in the invention.