GH2132 Nickel Alloy
GH2132（UNS S66286）It has excellent high-temperature strength, oxidation resistance and corrosion resistance, and is widely used in aerospace, energy, chemical industry and other fields.
Chemical Composition
|
|
V |
Ni |
C |
Si |
Mn |
Mo |
Cr |
Fe |
Ti |
P |
Cu |
Al |
B |
|
Min |
0.1 |
24 |
- |
- |
1 |
1 |
13.5 |
Rem |
1.75 |
- |
0.5 |
- |
0.001 |
|
Max |
0.5 |
27 |
0.08 |
1 |
2 |
1.5 |
16 |
Rem |
2.35 |
0.03 |
1.5 |
0.4 |
0.01 |
Material Properties
|
Density |
Melting Point |
Minimum Mechanical Properties of the Alloy at Room Temperature |
||
|
Tensile Strength |
Yield Strength |
Elongation |
||
|
g/cm3 |
℃ |
Rm N/mm2 |
Rp0.2 N/mm2 |
A5% |
|
7.93 |
1364-1424 |
900 |
590 |
15 |
Standards
ASTM B511 ASTM B512
Feature
High-temperature high-strength alloy: High yield/rupture/creep strength (≤650°C), good processability/weldability
Applications
GH2132 alloy for:
• Aero-engine blades
• Nuclear steam generators
• Petrochemical reactors
• Automotive turbochargers
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