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Ti Gr.9
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1.) Annealing: plates and plate parts: 660-710°C, 15-60min, air cooling or slower cooling; bars, forgings and pipes: 740-790°C, 1-2h, air cooling.
2.) Stress relief annealing, 545-585°C, 0.5-6h, air cooling or furnace cooling.
Gr.9(TC2) alloy has relatively satisfactory process plasticity, weldability and thermal stability. The long-term working temperature can reach 350°C, and the short-term working temperature is 750°C.
The plasticity of the process is good in the hot state, and complex parts can be made by hot stamping.
Application:
- Aviation industry
- Stamping
- Aircraft parts (accessories, engines, aircraft wings, etc.)
- Weldment
- Manufacturing
- Plate structural parts
- Catheter
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