VT8-1
Heat resistant alloy
For disks and compressor blades of aircraft engines
Heat resistant alloy
For disks and compressor blades of aircraft engines
Standard | Fe, % | Si, % | Sn, % | Ti, % | Zr, % | Al, % | C, % | O, % | Mo, % | N, % | H, % |
---|---|---|---|---|---|---|---|---|---|---|---|
Standard | Fe, % | Si, % | Sn, % | Ti, % | Zr, % | Al, % | C, % | O, % | Mo, % | N, % | H, % |
OST 1-90013-81 | < 0.2 | 0.1–0.25 | 0.4–1.5 | 85.37–90.1 | 0.5–1.5 | 5.8–6.8 | < 0.08 | < 0.15 | 2.8–3.8 | < 0.03 | < 0.015 |
Standard | Description |
---|---|
Standard | Description |
OST 1-90013-81 |