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Product Introduction
Product Introduction
Ti2AlNb alloy belongs to the Ti–Al intermetallic compound family and, compared with conventional near-α high‑temperature titanium alloys, exhibits outstanding properties such as high strength, excellent creep resistance, a high specific strength at elevated temperatures, and superior oxidation resistance. It can operate continuously at 650–750°C and, for short durations, at 800–900°C, making it an ideal lightweight structural material for high‑temperature applications.
| Chemical composition |
Ti |
Al |
Note |
Mo |
Zr |
Fe |
O |
H |
| Bal. |
9:50-11:50 |
38.00-45.00 |
0.50-1.50 |
0.50-1.50 |
≤0.15 |
≤0.10 |
≤0.010 |
| Physical properties |
D10(μm) |
D50(μm) |
D90(μm) |
Loose packing density (g/cm³) |
Tap density (g/cm³) |
Flowability (s/50g) |
| ≥15.63 |
33.24 |
59.91 |
2.79 |
3.64 |
28.30 |
Application areas
Aerospace
1. Aero Gas Turbine Engine
- High-pressure compressor rear section: rear casing, support ring, blade outer shroud, and guide vanes.
- Combustion Chamber Section: combustion chamber outer casing, inlet support plate, thermal insulation sleeve, cooling structure
- Nozzle system: nozzle control vanes, sealing rings, and afterburner barrel supports.
2. Space Rockets and Satellites
- Liquid- and solid-propellant rocket engines: nozzle support structures, high-temperature thrust chamber liners, and medium-temperature casings for turbopumps.
- Satellite thermal control system: medium- and high-temperature support frames, heat pipe connectors, and heat-resistant structures for deep-space probes.
Ti2AlNb titanium alloy powder
Category:
Brand: Asia Materials
Category: Titanium Alloy Powder
Product Name: Ti2AlNb Titanium Alloy Powder
European and American grades: /
Specifications and model numbers: 0–20 μm, 15–45 μm, 15–53 μm, 45–105 μm, 53–150 μm
Reference standard: /
Appearance: Spherical
Oxygen content: ≤1300 ppm
For more product details, please contact our product experts. We look forward to your call.
Product Introduction
Product Introduction
Ti2AlNb alloy belongs to the Ti–Al intermetallic compound family and, compared with conventional near-α high‑temperature titanium alloys, exhibits outstanding properties such as high strength, excellent creep resistance, a high specific strength at elevated temperatures, and superior oxidation resistance. It can operate continuously at 650–750°C and, for short durations, at 800–900°C, making it an ideal lightweight structural material for high‑temperature applications.
| Chemical composition |
Ti |
Al |
Note |
Mo |
Zr |
Fe |
O |
H |
| Bal. |
9:50-11:50 |
38.00-45.00 |
0.50-1.50 |
0.50-1.50 |
≤0.15 |
≤0.10 |
≤0.010 |
| Physical properties |
D10(μm) |
D50(μm) |
D90(μm) |
Loose packing density (g/cm³) |
Tap density (g/cm³) |
Flowability (s/50g) |
| ≥15.63 |
33.24 |
59.91 |
2.79 |
3.64 |
28.30 |
Application areas
Aerospace
1. Aero Gas Turbine Engine
- High-pressure compressor rear section: rear casing, support ring, blade outer shroud, and guide vanes.
- Combustion Chamber Section: combustion chamber outer casing, inlet support plate, thermal insulation sleeve, cooling structure
- Nozzle system: nozzle control vanes, sealing rings, and afterburner barrel supports.
2. Space Rockets and Satellites
- Liquid- and solid-propellant rocket engines: nozzle support structures, high-temperature thrust chamber liners, and medium-temperature casings for turbopumps.
- Satellite thermal control system: medium- and high-temperature support frames, heat pipe connectors, and heat-resistant structures for deep-space probes.
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