Custom Ti6Al-4V Titanium Disk
Custom Ti6Al-4V titanium disk The specific strength (strength-to-weight ratio) of titanium and its alloys is very high in metal structural materials. When aircraft, missiles, and rockets fly at high speeds, their engines and surface temperatures are quite high. The comprehensive excellent properties of light weight and strong heat resistance can not only prolong the service life of the aircraft, but also reduce its weight when it is used to replace other metals in aircraft
Custom Ti6Al-4V titanium disk
The specific strength (strength-to-weight ratio) of titanium and its alloys is very high in metal structural materials. When aircraft, missiles, and rockets fly at high speeds, their engines and surface temperatures are quite high. The comprehensive excellent properties of light weight and strong heat resistance can not only prolong the service life of the aircraft, but also reduce its weight when it is used to replace other metals in aircraft manufacturing, thereby greatly improving its flight performance.
| Chemical requirements | |||||||||||
| N | C | H | Fe | O | Al | V | Pd | Mo | Ni | Ti | |
| Gr1 | 0.03 | 0.08 | 0.015 | 0.20 | 0.18 | / | / | / | / | / | bal |
| Gr2 | 0.03 | 0.08 | 0.015 | 0.30 | 0.25 | / | / | / | / | / | bal |
| Gr5 | 0.05 | 0.08 | 0.015 | 0.40 | 0.20 | 5.5~6.75 | 3.5~4.5 | / | / | / | bal |
| Gr7 | 0.03 | 0.08 | 0.015 | 0.30 | 0.25 | / | / | 0.12~0.25 | / | / | bal |
| Gr12 | 0.03 | 0.08 | 0.015 | 0.30 | 0.25 | / | / | / | 0.2~0.4 | 0.6~0.9 | bal |
| Tensile requirements | |||||
| Grade | Tensile srength(min) | Yeild strength(mm) | Elongation(%) | ||
| KSI | MPa | Ksi | MPa | ||
| 1 | 35 | 240 | 20 | 138 | 24 |
| 2 | 50 | 345 | 40 | 275 | 20 |
| 5 | 130 | 895 | 120 | 828 | 10 |
| 7 | 50 | 345 | 40 | 275 | 20 |
| 12 | 70 | 438 | 50 | 345 | 18 |
Product picture:
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