Inconel 625 Turbine wheel
Density: 8.28 g/cm3
Melting point: 1295-1381℃
Magnetic: no
Linear expansion coefficient: 12.1-16.1 Hardness: 150-220 (HB)
Inconel 625 is a nickel-based alloy that is commonly used in the construction of turbine components due to its excellent combination of high-temperature strength, corrosion resistance, and overall mechanical properties. Here's an introduction to Inconel 625 turbines:
UNS N06625/W.NR.2.4856/alloy625
It has excellent corrosion resistance and oxidation resistance, has good tensile properties and fatigue properties from low temperature to 980 °C, and is resistant to stress corrosion in salt spray atmosphere. Therefore, it can be widely used in the manufacture of aero-engine parts, aerospace structural parts and chemical equipment and occasions exposed to seawater and subjected to high mechanical stress.
Similar Grades
United States: UNS N06625
France: NC 22DNb
United Kingdom: NA21
Germany: W.Nr.2.4856, NiCr22Mo9Nb
Technical Standard
ASTM B446, ASTM B564
ASM 5666
Typical values(Weight %)
|
Cr |
Ni |
Mo |
C |
Si |
P |
S |
Nb |
|
≤ |
|||||||
|
20.0-23.0 |
Remain |
8.0-10.0 |
0.10 |
0.50 |
0.015 |
0.015 |
3.15-4.15 |
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