Hostname: page-component-7479d7b7d-m9pkr Total loading time: 0 Render date: 2024-07-12T00:31:18.781Z Has data issue: false hasContentIssue false

Effects of Processing and Prolonged High Temperature Exposure on the Microstructure of Nb-1Zr-C Sheet

Published online by Cambridge University Press:  25 February 2011

Mehmet Uz
Affiliation:
Chemical Engineering Department, Lafayette College, Easton, PA 18042
R. H. Titran
Affiliation:
NASA Lewis Research Center, MS 49-1, Cleveland, OH 44135
Get access

Abstract

High temperature stability of the microstructure of Nb-lZr sheet containing 0.1 and 0.06 wt.%C was studied as affected by processing and prolonged 1350-K exposure with and without applied stress. Sheets were fabricated by cold rolling bars that were single-, double- or triple-extruded at 1900 K. Creep samples were double-annealed (1 h @ 1755 K + 2 h @ 1475 K) prior to testing at 1350 K for 10,000 - 34,500 h. The microstructures of the as-cast, extruded, rolled, DA and crept samples were characterized using various metallographic and analytical methods. The precipitates were rather coarse Nb2C initially, but transformed to finer (≤1 µm) carbides of (Zr,Nb)C with each subsequent high temperature process. The grain size, and the relative amount and morphology of (Zr,Nb)C were found to be affected by the number of extrusions and to some extent by C-content. However, the microstructures of all the crept samples were similar with (Zr,Nb)C distributed throughout the matrix indicating that prolonged exposure to 1350 K gave rise to complete transformation of Nb2 C to (Zr,Nb)C regardless of the processing history. These and other observations are presented with the emphasis on the correlation between processing, microstructure and creep properties.

Type
Research Article
Copyright
Copyright © Materials Research Society 1994

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Cooper, R.H. Jr., in Refractory Alloy Technology for Space Nuclear Power Applications, edited by Cooper, R. H. and Hoffman, E. E., (Technical Information Center, US Department of Energy, Oak Ridge, TN 1984) pp. 1417.Google Scholar
2. Titran, R. H., Advanced Materials and Processes 142(5), 3441(1992).Google Scholar
3. Kruger, G. C., Vaidyanathan, S., Deane, N., Protsik, R., Murata, R.E., in SP-100 Reactor Design, (22nd Intersociety Energy Conversion Engineering Conference Proc. 1, AIAA, New York, 1989) pp. 419423.Google Scholar
4. DelGrosso, E.J., and, C.E. Carlson Kaminsky, J.J., JLCM 12, 173201(1967).Google Scholar
5. Dokko, W., JPL Report No. JPL D-1948, Jet Propulsion Lab., Pasadena, CA, 1984.Google Scholar
6. Bryhan, A. J. and Chan, R. C., JOM 45(6), 5053(1993).CrossRefGoogle Scholar
7. Titran, R.H., NASA TM-100142, NASA LeRC, Cleveland, OH, 1986.Google Scholar
8. Titran, R.H., Moore, T.J. and Grobstein, T.L., NASA TM-89834, NASA LeRC, Cleveland, OH, 1987.Google Scholar
9. Titran, R.H., NASA TM-102390, NASA LeRC, Cleveland, OH, 1990.Google Scholar
10. Uz, Mehmet and Titran, R.H., NASA TM-106319, NASA LeRC, Cleveland, OH, 1993.Google Scholar
11. Norton, J.T. and Mowry, A.L., J. Metals 1(2), 133136(1949).Google Scholar