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Thermal-Stress Reducer For Metal/Composite JointSimple insert called "thermal link" reduces stresses caused by mismatches between thermal expansions of metal part and nonmetallic part made of fiber/matrix composite material. Link conceived for use in casing of advanced jet engine.
Document ID
19930000591
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Glinski, Robert L. (United Technologies Corp.)
Date Acquired
August 16, 2013
Publication Date
September 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 9
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-15232
Accession Number
93B10591
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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