NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Thermal fatigue and oxidation data of TAZ-8A and M22 alloys and variationsThermal fatigue and oxidation data were obtained on 36 specimens, representing 18 distinct variations (including the base systems) of TAZ-8A and M22 alloys. Double-edge wedge specimens for these systems were cycled between fluidized beds maintained at 1088 C and 316 C with a 180 s immersion in each bed. The systems included alloys TAZ-8A, M22, and 16 variations of these alloys. Each alloy variation consisted of a unique composition with an alternation in the percentage of carbon (C1 and C2), molydenum (M1 and M2), tungsten (W1 and W2), columbium (CB1, CB2, and CB3), tantalium (T1, T2, and T3), or boron (B1, B2, and B3) present. All of the alloys showed little weight change due to oxidation compared with other alloys previously tested in fluidized beds. Only both C1 alloy variation specimens survived 3500 cycles without cracking in the small radius, although substantial cracks were present, emanating from the end notches which were used for holding the specimens.
Document ID
19820002320
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hofer, K. E.
(IIT Research Inst. Chicago, IL, United States)
Humphreys, V. E.
(IIT Research Inst. Chicago, IL, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Subject Category
Metallic Materials
Report/Patent Number
NASA-CR-165407
IITRI-M06001-89
Accession Number
82N10193
Funding Number(s)
CONTRACT_GRANT: NAS3-17787
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available