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High temperature turbine engine structureA hybrid ceramic/metallic fastener (bolt) includes a headed ceramic shank carrying a metallic end termination fitting. A conventional cap screw threadably engages the termination fitting to apply tensile force to the fastener.
Document ID
20080004416
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Boyd, Gary L.
Date Acquired
August 24, 2013
Publication Date
April 30, 1991
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-PATENT-5,011,353
Patent Application Number: US-PATENT-APPL-SN-280760
Funding Number(s)
CONTRACT_GRANT: DEN3-167
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,011,353
Patent Application
US-PATENT-APPL-SN-280760

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