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Composite wall concept for high temperature turbine shrouds: Survey of low modulus strain isolator materialsPlasma sprayed yttria stabilized zirconium oxide turbine seal specimens, incorporating various low modulus porous metal strain isolator pads between the zirconium oxide and a dense metal substrate, were subjected to cyclic thermal shock testing. Specimens that had a low modulus pad composed of sintered FeNiCrAlY fibermetal survived 1000 thermal shock cycles without spalling of the ceramic. A figure of merit for the low modulus pad materials taking into consideration the elastic modulus, thermal conductivity, strength, and oxidation resistance of the pad was proposed, and showed reasonable agreement with the thermal shock results. A potential surface distress problem on the zirconium oxide, associated with nonuniform temperature distribution and rapid stress relaxation was identified. One approach to solving the surface distress problem through application of laser surface fusion of the zirconium oxide layer showed some promise, but improvements in the laser surface fusion process are necessary to prevent process associated damage to the ceramic.
Document ID
19800011914
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bill, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Allen, G. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Wisander, D. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1980
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA-TM-81443
E-363
AVRADCOM-TR-80-C-7
Report Number: NASA-TM-81443
Report Number: E-363
Report Number: AVRADCOM-TR-80-C-7
Meeting Information
Meeting: Ann. Intern. Gas Turbine Conf.
Location: New Orleans
Start Date: March 9, 1980
End Date: March 13, 1980
Sponsors: ASME
Accession Number
80N20398
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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