GH2132
Beschreibung
Lieferumfang für Aviation Group
Schmiedestücke, Rundstangen, Stahlplatten, Ringe, nahtlose Rohre, Stahlplatten/Stahlbänder, Drahtschweißmaterial, bitte fragen Sie uns an!
1. Introduction to GH2132 Materials
GH2132 alloy is a Fe-25Ni-15Cr-based high-temperature alloy, and is strengthened with molybdenum, titanium, aluminum, vanadium and trace boron. Below 650°C, it has high yield strength, long-lasting, creep strength, and has good processing plasticity and satisfactory welding properties. Suitable for manufacturing high-temperature bearing components for aircraft engines that work under 650°C for a long time, such as turbine discs, compressor discs, rotor blades and fasteners.
2. GH2132 physical properties
| Legierung | % | Unter | Cr | Fe | B | Mo | V | C | Mn | Und | S | P | Cu | Al | von |
| Gh2132 | Minimaler Wert | 24 | 13.5 | Marge | 0.003 | 1 | 0.1 | – | – | – | – | – | – | – | 1.9 |
| Maximaler Wert | 27 | 16 | 0.01 | 1.5 | 0.5 | 0.08 | 0.35 | 0.35 | 0.002 | 0.015 | 0.3 | 0.35 | 2.35 |
3. GH2132 physical properties
| Dichte | Schmelzpunkt | Wärmeleitfähigkeit | Spezifische Wärmekapazität | Elastizitätsmodul | Shear modulus | Widerstandsfähigkeit | Koeffizient der linearen Ausdehnung |
| g / cm3 | ℃ | λ/(W/m·℃) | J/kg·℃ | GPa | GPa | μΩ·m | a/10-6℃-1 |
| 7.99 | 1364-1424 | 14.2(100℃) | 0.914 | 15.7(20~100℃) |
GH2132 mechanical properties: (Minimum value of mechanical properties detected at 20℃)
| Status der Legierung | Zugfestigkeit Rm N/mm |
Ausbeute der Ausbeute
RP0.2 N/mm |
Dehnung
A5 % |
Brinell-Härte HB |
| Fester Lösungszustand | 930 | 590 | 15 | ≤341 |
Heat treatment requirements
| Material variety | Heat treatment system |
| Bars, round cakes | 980~1000℃, 1~2h, oil-cooled +700~720℃, 12~16h, air-cooled |
| Hot rolled plate, cold rolled plate | 980~1000℃, air-cooled +700~720℃, 16h, air-cooled |
| Cold pull rod | 980~1000℃, 1~2h, oil-cooled +700~720℃, 16h, air-cooled |
| Ring blank | 980~990℃, 1~2h, oil-cooled +700~720℃, 15h, air-cooled |
| Cold drawing for cold heading | 980~1000℃, 1~2h, water-cooled or oil-cooled +700~720℃, 16h, air-cooled |
4. GH2132 production implementation standards:
| Standard | Chemical composition | Stick | Schmiedeteile | Platte | Silk material | Rohrleitung | Schmiedeteile |
| National Standards | GB/T14992 | GB/T14994
GB/T14993 |
GB/T14997GB/T14998 | GB/T14995
GB/T14996 |
GB/T15062 | ||
| Aviation industry standards | HB5189 | ||||||
| National Military Standards | Gjb2611
GJB3165 |
GJB3317 | GJB2612
GJB3167 |
GJB3020
GJB3782 |
V. GH2132 application fields
Application Overview and Special Requirements In aviation, it is mainly used for engine compressor discs, turbine discs, load bearing rings, receivers, shafts, fasteners, and plate welded bearing parts that work below 650°C. in the country, this alloy has been widely used in aviation.
