| Item | Description |
|---|---|
| Material | Inconel 718 Nickel-Based Superalloy Powder |
| Characteristics | Excellent high-temperature strength, corrosion resistance, oxidation resistance, and creep resistance |
| Performance | Maintains mechanical properties under extreme temperature conditions |
| Manufacturing Process | LPBF / SLM Additive Manufacturing |
| Industry | Applications |
|---|---|
| Aerospace | Turbine blades, engine components, high-temperature structural parts |
| Aviation | Aircraft engine parts and heat-resistant components |
| Energy Industry | Gas turbine components, power generation equipment |
| Industrial Manufacturing | High-temperature molds, precision mechanical parts |
| Automotive | Turbocharger components and heat-resistant parts |
| Element | Content |
|---|---|
| Nickel (Ni) | 50.0 – 55.0% |
| Chromium (Cr) | 17.0 – 21.0% |
| Niobium (Nb) | 4.75 – 5.50% |
| Molybdenum (Mo) | 2.8 – 3.3% |
| Oxygen (O) | ≤0.10% |
| Iron (Fe) | Balance |
| Parameter | Specification |
|---|---|
| Powder Particle Size | 15–53 μm |
| D10 | 10–25 μm |
| D50 | 25–40 μm |
| D90 | 40–60 μm |
| Flowability | ≤20 s / 50 g |
| Apparent Density | ≥4.0 g/cm³ |
| Tap Density | ≥4.6 g/cm³ |
| Sphericity | ≥90% |
| Property | Value |
|---|---|
| Tensile Strength | ≥1240 MPa |
| Yield Strength | ≥1030 MPa |
| Elongation | ≥10% |
| Hardness | 48–52 HRC |
| Feature | Description |
|---|---|
| High Temperature Performance | Excellent strength retention at elevated temperatures |
| Corrosion Resistance | Outstanding resistance to oxidation and harsh environments |
| High Strength | Superior tensile and yield strength |
| Powder Quality | High sphericity and excellent flowability |
| Additive Manufacturing | Suitable for complex aerospace and industrial components |
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