Abstract
The effect of carbon addition on the high-temperature tensile properties and microstructure of Ti-43Al-6Nb-1Mo-1Cr alloys has been studied in this paper. 0.5 at.% C could increase both the ultimate tensile strength(UTS) and elongation of the alloys, as 643.85 ± 13.06 MPa and 7.07 ± 1.02% at 800 °C, 540.02 ± 4.29 MPa and 23.55 ± 0.58% at 850 °C, 389.82 ± 10.24 MPa and 40.5 ± 0.41% at 900 °C. With carbon content increasing from 0.5 at.% to 1.0 at.%, the UTS were increased while the elongations were reduced dramatically at high temperatures. 1.0 at.% carbon addition could also stabilize the UTS in the range of 600–800 MPa at 800–900 °C. Additionally, three types of strengthening mechanism and two types of toughening mechanism caused by carbon addition are discussed and concluded.
| Original language | English |
|---|---|
| Pages (from-to) | 441-448 |
| Number of pages | 8 |
| Journal | Journal of Alloys and Compounds |
| Volume | 775 |
| DOIs | |
| State | Published - 15 Feb 2019 |
Keywords
- Carbon addition
- Dislocation
- High-temperature tensile properties
- Strengthening and toughening mechanism
- TiAl alloys
- TiAlC
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