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Thermal fatigue and oxidation data of oxide dispersion-strengthened alloysThermal fatigue and oxidation data were obtained 24 specimens representing 9 discrete oxide dispersion-strengthened alloy compositions or fabricating techniques. Double edge wedge specimens, both bare metal and coated for each systems, were cycled between fluidized beds maintained at 1130 C with a three minute immersion in each bed. The systems included alloys identified as 262 in hardness of HRC 38; 264 in hardness of HRC 38, 40 and 43; 265 HRC 39, 266 of HRC 37 and 40; 754; and 956. Specimens in the bare condition of 265 HRC 39 and 266 HRC 37 survived 6000 cycles without cracking on the small radius of the double edge wedge specimen. A coated specimen of 262 HRC 38, 266 HRC 37 and 266 HRC40 also survived 6000 cycles without cracking. A duplicate coated specimen of 262 HRC 38 alloy survived 5250 cycles before cracks appeared. All the alloys showed little weight change compared compared to alloys tested in prior programs.
Document ID
19800016919
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hofer, K. E.
(IIT Research Inst. Chicago, IL, United States)
Hill, V. L.
(IIT Research Inst. Chicago, IL, United States)
Humphreys, V. E.
(IIT Research Inst. Chicago, IL, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1980
Subject Category
Metallic Materials
Report/Patent Number
IITRI-M6001-82
NASA-CR-159842
Report Number: IITRI-M6001-82
Report Number: NASA-CR-159842
Accession Number
80N25415
Funding Number(s)
CONTRACT_GRANT: NAS3-17787
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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