Transition Duct Support Arrangement for a Gas Turbine Engine
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Jul 12, 2016
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Jul 12, 2016
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Abstract
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.
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