Alloy Grades | % | Copper (Cu) | Iron (Fe) | Nickel (Ni) | Chromium (Cr) | Carbon (C) | Silicon (Si) | Manganese (Mn) | Phosphorus (P) | Sulfur (S) | Titanium (Ti) | Molybdenum (Mo) | Vanadium (V) | Aluminum (Al) | Cobalt (Co) | Boron (B) | Zirconium (Zr) | Lead (Pb) | Bismuth (Bi) | Silver (Ag) | Tungsten (W) | Cerium (Ce) | Niobium (Nb) |
A-286 | Min. | Rest | 24 | 13.5 | 1.9 | 1 | 0.1 | 0.001 | |||||||||||||||
Max. | 27 | 16 | 0.08 | 1 | 2 | 0.04 | 0.03 | 2.35 | 1.5 | 0.5 | 0.35 | 0.01 | |||||||||||
80A | Min. | Rest | 18 | 1.8 | 1 | ||||||||||||||||||
Max. | 3 | 21 | 0.1 | 1 | 1 | 0.02 | 0.015 | 2.7 | 1.8 | 2 | 0.008 | 0.15 | |||||||||||
Nimonic 90 | Min. | 18 | 2 | 1 | 15 | ||||||||||||||||||
Max. | 0.2 | 1.5 | Rest | 21 | 0.13 | 1 | 1 | 0.015 | 3 | 2 | 21 | 0.02 | 0.15 | 0.002 | 0.0001 | 0.0005 | |||||||
GH1140 | Rest | 35.0-40.0 | 20.0-23.0 | 0.06-0.12 | ≤0.80 | ≤0.07 | ≤0.025 | ≤0.015 | 0.70-1.20 | 2.00-2.50 | 0.20-0.60 | 1.40~1.80 | ≤0.05 | ||||||||||
GH3625 | ≤0.5 | Rest | 20-23 | ≤0.1 | 3.15-4.15 | ≤0.4 | 8-10 | ≤0.4 | ≤1.0 | ||||||||||||||
GH3536 | Rest | 20.5-23 | 0.05-0.15 | ≤0.15 | 8-10 | ≤0.5 | 0.5~2.5 | 0.2~1 | |||||||||||||||
GH4169 | ≤0.3 | Rest | 50-55 | 17-21 | ≤0.08 | ≤0.35 | ≤0.35 | ≤0.01 | 0.7-1.15 | 2.8-3.3 | 0.2-0.8 | ≤1.0 | 4.75~5.5 |
Alloy Grades | Density (g/cm³) | Melting Point (°C) | Electrical Resistivity (μΩ·m) | Coefficient of Lines Expansion (α×10⁻⁶/20~1000ºC) | Tensile Strength (Rm N/mm²) | Yield Strength (Rp 0.2N/mm²) | Elongation at Break A5 (%) | Brinell Hardness (HBS) | Thermal Conductivity λ (W/m·℃) | Specific Heat (J/kg·°C) | Modulus of Elasticity (GPa) | Shear Modulus (GPa) | Poisson's Ratio |
A-286 | 7.99 | 1364-1424℃ | 0.914 | 15.7 | |||||||||
80A | 8.19 | 1320-1365 | 930 | 620 | 20 | ||||||||
Nimonic 90 | 8.20 | 1400 | |||||||||||
GH1140 | |||||||||||||
GH3625 | 8.44 | 1290-1350 | 1.28 | 12.3 | 830 | 410 | 30 | ≤290 | 12.1(100℃) | 430 | 205 | 79 | |
GH3536 | |||||||||||||
GH4169 | 8.24 | 1260-1320 | 11.8 | 930 | 620 | 20 | ≥363 | 14.7(100℃) | 435 | 199.9 | 77.2 | 0.3 |
Steps | DZX Do | Time |
Confirmation of product parameters and application | We confirm the product according to the demand | Immediate |
Sample customization | In stock or confirm OEM/ODM customization | Immediate |
Production and processing | Confirmation of production as well as product testing | 7-15 days |
Packaging and Transportation | Using carton + preservative film + pallet | According to the national |
Consider your application’s temperature, stress, and environmental conditions, and consult with us to match alloy properties to your needs.
Costs depend on alloy composition, processing complexity, and market demand for specific elements like nickel or titanium.
They are designed to resist deformation and fatigue, ensuring stability in applications like turbines or engines under constant stress.
Aerospace, energy, automotive, and industrial manufacturing rely on these alloys for parts exposed to high temperatures and stress.
Yes, many high temperature alloys are designed to resist oxidation and corrosion, even in harsh environments like chemical plants or jet engines.
They maintain strength and resist corrosion or deformation in extreme heat, unlike standard metals, making them ideal for demanding environments.
High temperature alloys are used in industries like aerospace, power generation, and petrochemicals for components such as turbine blades, exhaust systems, and heat exchangers that operate under extreme heat.
dlx-group@dlx-alloy.com | |
Phone | 0086-1990 6119 641 |
Address | NO.32 West Taihu Road, Xinbei District, Changzhou, Jiangsu,China |