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High temperature turbine engine structureA high temperature turbine engine includes a hybrid ceramic/metallic rotor member having ceramic/metal joint structure. The disclosed joint is able to endure higher temperatures than previously possible, and aids in controlling heat transfer in the rotor member.
Document ID
20080008761
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Boyd, Gary L.
Date Acquired
August 24, 2013
Publication Date
June 19, 1990
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-280761
Patent Number: US-Patent-4,934,138
Funding Number(s)
CONTRACT_GRANT: DEN3-167
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-4,934,138
Patent Application
US-Patent-Appl-SN-280761

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