Affiliation:
1. Lanzhou University of Technology
Abstract
Based on the fatigue crack propagation experiments did by A.-L. Gloanec et al., the fatigue crack propagation rates of TiAl alloy of two processing routes, namely casting and PM, and stress ratios had been tested, in order to find out the effects of microstructure and stress ratio. An improved fatigue crack propagation formula for region Ⅱ (the expansion region) was derived according to Paris formula. The specific values of the constants in the formula were calculated. Fatigue crack propagation resistance of nearly fully lamellar microstructure is superior to that of equiaxed γ grain. The experimental results present that both microstructure and stress ratio has a significant influence on fatigue crack growth rate.
Publisher
Trans Tech Publications, Ltd.
Reference10 articles.
1. Y.W. Kim, Overview: Ordered Intermetallic Alloys 3. Gamma-Titanium Aluminides, Jom-J. Min. Metals Mater. Soc., 46(7)(1994) 30-39.
2. S.C. Huang and J.C. Chesnutt, Gamma TiAl and its Alloys, in J.H. Westbrook and R.L. Fleisher (eds. ), Intermetallic Compounds: Vol. 2, Practice, Wiley, New York, 1994, pp.73-90.
3. G. Hénaff, B. Bittar, C. Mabru, J. Petit, P. Bowen. fatigue crack propagation resistance of a Ti-48Al-2Mn-2Nb alloy in the as-cast condition. Materials Science and Engineering A219 (1996) 212-220.
4. Gilbert Hénaff, Anne-Lise Gloanec. Fatigue properties of TiAl alloys. Intermetalics 13(2005) 543-558.
5. A.H. Rosenberger. effect of environment on the fatigue crack growth of gamma titanium aluminide alloys at ambient temperatures. Scripta mater. 44 (2001) 2653-2659.
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2 articles.
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