Effects of Long-Time Aging on Fatigue Crack Propagation Behaviors of a Hardworking Ni-Based Superalloy

Article Preview

Abstract:

Fatigue crack propagation behaviors coupled with the microstructure evolution of a hardworking Ni-based superalloy after long-time aging at 1023K were studied, to provide fundamental data for the fatigue life prediction of the superalloy. The results show that the microstructures remarkably change and the fatigue crack propagation resistance decreases with the aging time prolongs. It is found that the precipitation and the growth of topologically close packed (TCP) phases as well as the coarsening of γ' phase and carbides on grain boundaries can significantly affect the fatigue crack growth rate. On one hand, coarsened γ' phase and carbides at grain boundaries block dislocation movements near the crack tip, thus the fatigue crack propagation is hindered in near-threshold region and Paris region. On the other hand, the stress concentration accumulates continually with carbides precipitation increases, so that the grain boundaries become the main fatigue crack propagation rout. As well as, the effect of the TCP phases on the fatigue crack propagation behavior ascribes to the size and the distribution of TCP phases. Very small quantity of TCP phases contribute to pinning dislocation and enlarging fatigue crack propagation absorption energy, but high quantity of TCP phases with short rod shape changed to the needle, which gradually precipitate uniformly within the grain after 1000h besides on grain boundaries in the earlier aging, leads to much higher stress concentration degree. Those discussed above are the most important reasons why the fatigue crack growth rate increases after long-time aging.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 891-892)

Pages:

1657-1662

Citation:

Online since:

March 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] J. J. Moverare, S. Johansson, R. C. Reed, Deformation and damage mechanisms during thermal-mechanical fatigue of a single-crystal superalloy, Acta Mater. 57 (2009) 2266-2276.

DOI: 10.1016/j.actamat.2009.01.027

Google Scholar

[2] W. Betteridge, S. W. Shaw, Development of superalloys, Mater. Sci. Technol. 3 (1987) 682-694.

Google Scholar

[3] C. Bruni, A. Forcellese, F. Gabrielli, Hot workability and models for flow stress of Nimonic 115 Ni-base superalloy, J. Mater. Process Tech. 125-126(2002) 242-247.

DOI: 10.1016/s0924-0136(02)00302-3

Google Scholar

[4] D. L. Davidson, Gas turbine disk-blade attachment crack, J. Fail Anal Prevent, 5 (2005) 55-71.

DOI: 10.1361/15477020522104

Google Scholar

[5] K. Prasad, N. C. Babu, V. Kumar, Effect of frequency and orientation on fatigue crack growth behavior of forged turbine disc of IN 718 superalloy, Mater. Sci. Eng. A. 544 (2012) 83-87.

DOI: 10.1016/j.msea.2012.02.088

Google Scholar

[6] R.J.H. Wanhill, Significance of dwell cracking for IN718 turbine discs, International Journal of Fatigue. 24 (2002) 545-555.

DOI: 10.1016/s0142-1123(01)00109-8

Google Scholar

[7] H. T. Pang, P.A.S. Reed, Microstructure effects on high temperature fatigue crack initiation and short crack growth in turbine disc nickel-base superalloy Udimet 720Li, Mater. Sci. Eng. A. 448 (2007) 67-79.

DOI: 10.1016/j.msea.2006.11.016

Google Scholar

[8] C. M. F. Rae, M. S. Hook, R. C. Reed, The effect of TCP morphology on the development of aluminide coated superalloys, Mater. Sci. Eng. A. 396 (2005) 231-239.

DOI: 10.1016/j.msea.2005.01.005

Google Scholar

[9] S. S. Xie, T. L. Wang, J. Y. Lu, Effects of Zr on Microstructure and short-term strength in GH586, J. Mater. Sci. Technol. 15 (1999) 415-418.

Google Scholar

[10] M. Nganbe, M. Heilmaier, Modelling of particle strengthening in the γ' and oxide dispersion strengthened nickel-base superalloy PM3030, Mater. Sci. Eng. A. 387-389 (2004) 609-612.

DOI: 10.1016/j.msea.2004.01.109

Google Scholar