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NiAl-based Polyphase in situ Composites in the NiAl-Ta-X (X = Cr, Mo, or V) SystemsPolyphase in situ composites were generated by directional solidification of ternary eutectics. This work was performed to discover if a balance of properties could be produced by combining the NiAl-Laves phase and the NiAl-refractory metal phase eutectics. The systems investigated were the Ni-Al-Ta-X (X = Cr, Mo, or V) alloys. Ternary eutectics were found in each of these systems and the eutectic composition, temperature, and morphology were determined. The ternary eutectic systems examined were the NiAl-NiAlTa-(Mo, Ta), NiAl-(Cr, Al) NiTa-Cr, and the NiAl-NiAlTa-V systems. Each eutectic consists of NiAl, a C14 Laves phase, and a refractory metal phase. Directional solidification was performed by containerless processing techniques in a levitation zone refiner to minimize alloy contamination. Room temperature fracture toughness of these materials was determined by a four-point bend test. Preliminary creep behavior was determined by compression tests at elevated temperatures, 1100-l400 K. Of the ternary eutectics, the one in the NiAl-Ta-Cr system was found to be the most promising. The fracture toughness of the NiAl-(Cr, Al)NiTa-Cr eutectic was intermediate between the values of the NiAl-NiAlTa eutectic and the NiAl-Cr eutectic. The creep strength of this ternary eutectic was similar to or greater than that of the NiAl-Cr eutectic.
Document ID
19970003570
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Johnson, D. R.
(Tennessee Univ. Knoxville, TN United States)
Oliver, B. F.
(Tennessee Univ. Knoxville, TN United States)
Noebe, R. D.
(NASA Lewis Research Center Cleveland,OH United States)
Whittenberger, J. D.
(NASA Lewis Research Center Cleveland,OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: Intermetallics
Publisher: Elsevier Science Ltd.
Volume: 3
ISSN: 0966-9795
Subject Category
Metallic Materials
Report/Patent Number
NASA-TM-111737
NAS 1.15:111737
Report Number: NASA-TM-111737
ISSN: 0966-9795
Report Number: NAS 1.15:111737
Accession Number
97N12265
Distribution Limits
Public
Copyright
Public Use Permitted.
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