GH132 superalloy is introduced in detail
Grade:gh132
National Standards:uns s66286, werkstoff 1.4980, en 1.4980, ams: 5525, 5804, 5732, 5737 ge b50t1181, ge b50t12, ge b50t8 gh2132(gh132) incoloya-286
Cooperative manufacturers:Outokumpu (Outokumpu), *ESTA (Avista), Hastelloy (USA), SMC (USA), ATI (USA), ThyssenKrupp VDM, MANNEX, German Nickel, Sandvik (Sweden), Metallurgical (Japan), Nippon Steel and other well-known brands.
w.nr.1.4890 Nickel Alloy (GH132) Chemical Composition:
Nickel (Ni): 24-27%.
Chromium (CR): 135-16%
Molybdenum (Mo): 10-1.5%
Boron (b): 0001-0.01%
Iron (Fe): Margin.
Aluminum (AL): 040%
Titanium (Ti): 175-2.35%
Carbon (c): 008%
Manganese (mn): 10-2.0%
Silicon (Si): 10%
Vanadium (v): 010-0.50%
Sulfur (s): 002%
w.nr.1.Physical properties of 4890:
Density: 793 g/cm3
Melting Point: 1364-1424
w.nr.1.The minimum value of the mechanical properties of the alloy at room temperature of 4890:
Tensile strength rm n mm2: 950
Yield strength rp02n/mm2：680
Elongation a5 %: 28
Key features:
gh132（w.nr.1.4890) is an alloy material with high high temperature strength and high temperature oxidation resistance.
It is widely used in the manufacture of parts and components on aero engines and industrial gas turbines, such as turbine blades, afterburners, fasteners, etc.
It is also widely used in automobile engines.
Areas of application and examples:
It is used to manufacture high-temperature load-bearing parts of aero engines that work for a long time below 650°C, such as turbine discs.
In aerospace and industrial applications, especially where high temperatures, high strength and corrosion resistance are required, GH132 demonstrates excellent performance and ensures reliable operation under extreme conditions.