MOQ: | 100KG |
Price: | Price is negotiated based on the required specifications and quantity |
Standard Packaging: | Standard export packaging, or packaging as required |
Delivery Period: | 5-8 working days, depending on the parameters required for negotiation |
Payment Method: | Payment Terms: Mainly T/T.. L/C, D/A, D/P, |
Supply Capacity: | 5000 tons per month |
Attribute | Value |
---|---|
Density | ~8.9g/cm³ (0.321 lb/in³) |
Melting Point | ~1350-1450°C (2460-2640°F) |
Tensile Strength | ~900 MPa (130 ksi) |
Yield Strength | ~750 MPa (109 ksi) |
Elongation | ~15% |
Thermal Conductivity | ~14 W/m·K (10 BTU·in/hr·ft²·°F) |
Modulus of Elasticity | ~210 GPa (30 x 10³ ksi) |
Corrosion Resistance | Good resistance to oxidation and corrosion at high temperatures |
Applications | Aerospace components, gas turbines, high-temperature industrial parts |
GH39 Alloy is a high-performance nickel-based superalloy engineered for exceptional strength and oxidation resistance at elevated temperatures. It is specifically designed to perform reliably in extreme environments, making it ideal for aerospace and industrial applications where high thermal and mechanical stress is common.
GH39 Alloy's combination of high strength, excellent oxidation resistance, and thermal stability makes it a preferred material for critical applications where reliability and durability are paramount.
Element | Composition Range (%) |
---|---|
Nickel (Ni) | 60.0 - 65.0 |
Chromium (Cr) | 15.0 - 20.0 |
Cobalt (Co) | 5.0 - 10.0 |
Molybdenum (Mo) | 3.0 - 5.0 |
Iron (Fe) | ≤ 6.0 |
Titanium (Ti) | 1.0 - 2.0 |
Aluminum (Al) | 1.0 - 2.0 |
Carbon (C) | ≤ 0.10 |
Manganese (Mn) | ≤ 0.5 |
Silicon (Si) | ≤ 0.5 |
Sulfur (S) | ≤ 0.01 |
These values are general guidelines. For precise specifications or detailed applications, consult specific standards or suppliers.