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Hot hardness of nickel-rich nickel-chromium-aluminum alloysRockwell A hardness of cast nickel-chromium-aluminum (NiCrAl) alloys was examined from ambient to 1150 K and compared to cast NiAl and IN-100. Alloy constitution was either gamma, gamma prime + gamma or gamma + beta + alpha + gamma prime. Below 1000 K beta containing NiCrAl alloys have hardnesses comparable to IN-100; above 1000 K they soften faster than IN-100. At 1150 K the hardness of beta-containing NiCrAl alloys decreases with increasing beta-content. The beta-containing NiCrAl alloys were harder than beta-NiAl. The ultimate tensile strengths of the NiCrAl alloys were estimated. The effects of NiCrAl coatings on strength and fatigue life of cooled turbine components were deduced.
Document ID
19770004212
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Levine, S. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1976
Subject Category
Metallic Materials
Report/Patent Number
NASA-TM-X-3429
E-8750
Accession Number
77N11155
Funding Number(s)
PROJECT: RTOP 505-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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