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Coatings for directional eutecticsCoating compositions were evaluated for oxidation protection of directionally solidified composite alloy NiTaC-13. These coatings included three NiCrAlY compositions (30-5-1, 25-10-1 and 20-15-1), two FeCrAlY compositions (30-5-1 and 25-10-1), a CoCrAlY composition (25-10-1), and one duplex coating, Ni-35Cr + Al. Duplicate pin samples of each composition were evaluated using two cyclic furnace oxidation tests of 100 hours at 871 C and 500 hours at 1093 C. The two best coatings were Ni-20Cr-15Al-lY and Ni-35Cr + Al. The two preferred coatings were deposited on pins and were evaluated in detail in .05 Mach cyclic burner rig oxidation to 1093 C. The NiCrAlY coating was protective after 830 hours of cycling, while the duplex coating withstood 630 hours. Test bars were coated and cycled for up to 500 hours. Tensile tests indicated no effect of coatings on strength. In 871 C air stress rupture, a degradation was observed for coated relative to bare material. The cycled NiCrAlY coating offered excellent protection with properties superior to the bare cycled NiTaC-13 in 1093 C air stress rupture.
Document ID
19740023904
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jackson, M. R.
(General Electric Co. Schenectady, NY, United States)
Rairden, J. R.
(General Electric Co. Schenectady, NY, United States)
Hampton, L. V.
(General Electric Co. Schenectady, NY, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Materials, Nonmetallic
Report/Patent Number
SRD-74-047
NASA-CR-134665
Report Number: SRD-74-047
Report Number: NASA-CR-134665
Accession Number
74N32017
Funding Number(s)
CONTRACT_GRANT: NAS3-16793
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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