Abstract
The manufacturing method for producing high-strength Ti-10V-2Fe-3Al alloy forgings with suitable ductility/toughness combinations has been established. The achievable property combinations at high strengths depend critically on the billet chemistry-homogeneity, the forge heat-treat variables, and the section thickness of the forgings. The manufacturing capability developed in this program has made this alloy an attractive potential for high-strength forging applications on Boeing's future aircraft.
| Original language | English |
|---|---|
| Pages (from-to) | 33-39 |
| Number of pages | 7 |
| Journal | Journal of Metals |
| Volume | 31 |
| Issue number | 7 |
| Publication status | Published - 1 Jan 1979 |