GH2132 alloy is Fe-25Ni-15Cr-based high-temperature alloy, which is comprehensively strengthened by adding molybdenum, titanium, aluminum, vanadium and trace boron. It has high yield strength and lasting and creep strength below 650ºC, and has good processing plasticity and satisfactory welding performance. It is suitable for manufacturing high-temperature bearing components of aero-engines, such as turbine disks, compressor disks, rotor blades and fasteners, which work for a long time below 650ºC.

GH2132 (GH132) high temperature alloy

Overview of GH2132 features and application areas:

Similar grades of GH2132:
A-286 P.Q.A286 UNSS666286 (U.S.), ZbNCT25 (France)

GH2132 chemical composition: (GB/T14992-2005)

alloy Grade%
                                        Ni       Cr      Fe         B         Mo    V     C      Mn    Si       S        P       Cu    Al      Ti
GH2132  minimum        24.0   13.5   margin  0.003   1.0    0.1                                                                    1.90
               maximum        27.0  16.0                 0.010   1.5   0.5   0.08  0.35  0.35  0.002  0.015  0.3  0.35   2.35 

GH2132 physical properties:
density  g/cm3                                                    7.99
Melting point °C                                          1364 - 1424
Thermal conductivity  λ/(W/m·ºC)               14.2(100ºC)
Resistivity  μΩ·m                                            0.914
Linear expansion coefficient  a/10-6ºC-1    15.7(20~100ºC)

Mechanical properties of GH2132: (Detect the minimum value of mechanical properties at 20ºC)
Heat treatment method:   Solution treatment
tensile strength  σb/MPa:     930
Yield Strength  σp0.2/MPa:   590
Elongation   σ5 /%:     15
Brinell hardness  HBS:  ≤341