Technical Specifications
Download DatasheetTi (Balance), Al 5.5–7.1, V 0.8–2.5, Zr 1.5–2.5, Mo 0.5–2.0, Si ≤ 0.15, Fe ≤ 0.25, O ≤ 0.15 (GB/T 3620.1-2016)
15–53 µm (GB/T 19077-2016)
~ 4.5 g/cm³ (GB/T 3850-2015)
> 99.9% (GB/T 3850-2015)
≥ 6 µm (GB/T 40389-2021)
1,050 ± 50 MPa (GB/T 228.1-2015)
1,230 ± 50 MPa (GB/T 228.1-2015)
7 ± 3 % (GB/T 228.1-2015)
38 ± 2 HRC (GB/T 230.1-2018)
980 ± 50 MPa (GB/T 228.1-2015)
1,080 ± 50 MPa (GB/T 228.1-2015)
13 ± 3 % (GB/T 228.1-2015)
35 ± 2 HRC (GB/T 230.1-2018)
2 Hours at 850 °C, Furnace Cooling
Yield 560 ± 30 MPa; Tensile 700 ± 30 MPa; Elongation 14 ± 3 % (GB/T 228.2-2015)
HBD 150, HBD 200, HBD 200Pro, HBD 400, HBD 500, HBD 600, HBD 800, HBD 1600
Besides the listed systems, the material can also be used with third-party systems that meet its requirements. Parameters must be developed separately.
Key Features and Applications
Key Features
- Provides high-temperature strength up to 500 °C.
- Delivers lightweight structures through high specific strength.
- Is developed for aerospace structural parts.
Applications
- Aerospace structural components.
- Engine-area parts operating at high temperature.
