GH2132 Material introduction
GH2132 alloy is a Fe-25Ni-15Cr based superalloy, which is comprehensively strengthened by adding molybdenum, titanium, aluminum, vanadium and trace boron. It has high yield strength, endurance and creep strength below 650 ℃, and has good processing plasticity and satisfactory welding performance. It is suitable for manufacturing high-temperature load-bearing components of aeroengines that work for a long time below 650 ℃, such as turbine disks, compressor disks, rotor blades and fasteners.
GH2132 chemical composition
element | C | Cr | Ni | Mo | Al | Ti | Fe |
mass fraction/% | ≤0.08 | 13.5-16.0 | 24.0-27.0 | 1.0-1.5 | ≤0.4 | 1.75-2.35 | 余 |
element | B | V | Mn | Si | P | S | Cu |
mass fraction/% | 0.001-0.01 | 0.10-0.50 | 1.0-2.0 | ≤1.0 | ≤0.03 | ≤0.02 | ≤0.25 |
GH2132 Physical and mechanical properties
density | melting point |
7.93g/cm3 | 1364-1424℃ |
varieties | Heat treatment method | σb/MPa | σp0.2/MPa | δ5/% | Ψ/%
| HBS
|
Rolled bar and forged bar | Solution+aging | 930 | - | 20 | 40 | 255-321 |
Cold drawn rod | Solution+aging | 900 | 590 | 15 | 20 | 248-341 |
GH2132 Heat treatment system
Hot rolled and forged bars, forgings, cold drawn bars,990℃±10℃×(l-2)h/OQ or AC+(700-720)℃×16h/AC;
Hot rolled plate, weldment,(980-1000)℃/AC+(700-720)℃×(12-16) h/AC,Including solution heat preservation time,δ≤3mm:15min-20min;δ3 mm-5mm:20min-25min;
Silk material,(980-1000)℃/WQ or OQ +(700-720)℃×16h/AC,Including solution heat preservation time,d ≤3mm:15min-20min;d3mm-5mm;20min-5min。