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Development of improved low-strain creep strength in Cabot alloy R-41 sheetThe feasibility of improving the low-strain creep properties of a thin gauge nickel base sheet alloy through modified heat treatment or through development of a preferred crystal-lographic texture was investigated. The basic approach taken to improve the creep strength of the material by heat treatment was to increase grain size by raising the solution treatment temperature for the alloy to the range of 1420 K to 1475 K (2100 F to 2200 F). The key technical issue involved was maintenance of adequate tensile ductility following the solutioning of M6C primary carbides during the higher temperature solution treatment. The approach to improve creep properties by developing a sheet texture involved varying both annealing temperatures and the amount of prior cold work. Results identified a heat treatment for alloy R-14 sheet which yields a substantial creep-life advantage at temperatures above 1090 K (1500 F) when compared with material given the standard heat treatment. At the same time, this treatment provides reasonable tensile ductility over the entire temperature range of interest. The mechanical properties of the material given the new heat treatment are compared with those for material given the standard heat treatment. Attempts to improve creep strength by developing a sheet texture were unsuccessful.
Document ID
19840023276
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rothman, M. F.
(Cabot Corp. Kokomo, IN, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Metallic Materials
Report/Patent Number
REPT-11816
NAS 1.26:172392
NASA-CR-172392
Report Number: REPT-11816
Report Number: NAS 1.26:172392
Report Number: NASA-CR-172392
Accession Number
84N31346
Funding Number(s)
CONTRACT_GRANT: NAS1-15975
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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