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Reaction Zone Growth in Ti-Base/SiC Composites

Published online by Cambridge University Press:  21 February 2011

Ann M. Ritter
Affiliation:
GE Corporate Research & Development, P.O. Box 8, Schenectady, NY 12301
Ernest L. Hall
Affiliation:
GE Corporate Research & Development, P.O. Box 8, Schenectady, NY 12301
Nathan Lewis
Affiliation:
GE Corporate Research & Development, P.O. Box 8, Schenectady, NY 12301
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Abstract

Reaction zone phases and kinetics over a temperature range of 650-1200°C have been characterized for Ti-14Al-21Nb/SiC and Ti-6Al-2Sn-4Zr-2Mo/SiC fibrous composites. The matrix of the Ti-1421/SiC materials was α2 with varying amounts of beta phase and transformed beta phase, and the Ti-6242 matrix consisted of alpha plus beta. The reaction zone in the as-HIP Ti-1421/SiC contained fine-grained TiC, a region of coarser-grained TiC, a carbide layer containing Ti, Al and Nb, and a region of(Ti, Nb)5(Si, Al)3. The matrix adjacent to the reaction zone was α2-Ti3Al with no beta phase. In the as-HIP Ti-6242/SiC composites, the reaction zone contained TiC near the fiber, and a layer of (Ti,Zr)5Si3 adjacent to the matrix. In heat-treated samples, the reaction zone thicknesses varied in a linear fashion with the square-root of aging time, indicating diffusion-controlled growth. Incubation periods for reaction zone growth were observed in Ti-1421/SiC samples aged at 760-1000°C. The overall kinetics for the two matrix alloys were approximately the same, and the activation energy was measured as 63-73 kcal/mole for Ti-1421/SiC and 73kcal/mole for Ti-6242/SiC.

Type
Research Article
Copyright
Copyright © Materials Research Society 1990

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References

1. Brindley, P.A., Bartolatta, P.A. and Klima, S.J., NASA Technical Memorandum 100956 (NASA Lewis Research Center, Cleveland, OH, 1988).Google Scholar
2. Baumann, S.F. and Brindley, P.K., presented at the Fall TMS Meeting, Chicago, IL, 1988 (unpublished).Google Scholar
3. Smith, P.R., Froes, F.H. and Cammett, J.T., in Mechanical Behavior of Composite Materials, edited by Hack, J.E. and Amateau, M.F. (TMS, Warrendale, 1982), p. 143.Google Scholar
4. Rhodes, C.G., Ghosh, A.K. and Spurling, R.A., Metall. Trans. 18A, 2151 (1987).Google Scholar
5. Smith, P.R., Revelos, W.C., and Rhodes, C.G., presented at the Annual TMS Meeting, Anaheim, CA, 1990 (unpublished).Google Scholar
6. Siemers, P.A. and Rutkowski, S.F., GE Corporate Research & Development, Report No. 90CRD022 (1990).Google Scholar
7. Amato, R.A., GE Aircraft Engine Report No. 86-AEB-234 (1986).Google Scholar
8. Amato, R.A., GE Aircraft Engine Report No. R88-AEB-374 (1988).Google Scholar
9. Metcalfe, A.G. and Klein, M.J., in Interfaces in Metal Matrix Composites, Vol.1, edited by Metcalfe, A.G. (Academic Press, New York, 1974), p. 125.Google Scholar
10. Lancin, M., Bour, J.S. and Thibault-Desseaux, J., in High Temperature/High Performance Composites, edited by Lemky, F.D., Fishman, S.G., Evans, A.G. and Strife, J.R. (Mater. Res. Soc. Proc. 120, Pittsburgh, PA 1988), p.351.Google Scholar
11. Yang, J.M. and Jeng, S.M., Scripta Met. 23, 1559 (1989).Google Scholar
12. Banerjee, D., Gogia, A.K., Nandi, T.K., and Joshi, V.A., Acta Metall. 36, 871 (1988).Google Scholar
13. Ritter, A.M., Siemers, P.A., Clark, F.W., and Rutkowski, S.F., to be presented at the Fall TMS Meeting, Detroit, MI, 1990 (unpublished).Google Scholar
14. Schuster, J.C., Nowotny, H., and Vaccaro, C., J. Sol. State Chem. 32, 213 (1980).Google Scholar
15. Smith, P.R. and Revelos, W.C., to be presented at Fatigue ‘90, Honolulu, Hawaii, 1990 (unpublished).Google Scholar