Abstract
Low-cycle fatigue (LCF) behavior of Ti-2Al-2.5Zr was investigated at 298 and 673K. Cyclic stress response curves showed that initial cyclic hardening was followed by cyclic softening at 298 and 673K, while secondary cyclic hardening appeared when testing temperature increased to 673K. Ti-2Al-2.5Zr displayed higher LCF lives at 673K than those at 298K. Microstructural characterization with transmission electron microscopy (TEM) revealed that 1̄1 0 1̄ 0; prismatic slip was primary plastic deformation mode in Ti-2Al-2.5Zr fatigued at 298K. 1̄1 2̄ 1 1; pyramidal slip could be activated at high cyclic strain amplitude. Whereas, multiple slips were simultaneously operated on 1̄1 0 1̄ 0; prismatic and 1̄1 2̄ 1 1; pyramidal planes in the range of tested cyclic strain amplitudes at 673K. Plastic deformation mode changed from planar slip to wavy slip as testing temperature increased from 298 to 673K. The improvement of LCF life of Ti-2Al-2.5Zr could be attributed to the increase of plastic deformation homogeneity due to activating multiple slips at 673K.
| Original language | English |
|---|---|
| Pages (from-to) | 3493-3500 |
| Number of pages | 8 |
| Journal | Materials Science and Engineering: A |
| Volume | 527 |
| Issue number | 15 |
| DOIs | |
| State | Published - Jun 2010 |
Keywords
- Cyclic deformation behavior
- Dislocation
- Low-cycle fatigue
- Secondary cyclic hardening
- Ti-2Al-2.5Zr
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