GH4133 (GH33) high-temperature alloy is an age-hardened nickel-based high-temperature alloy composed of elements such as nickel, molybdenum, and aluminum, with a nickel content of about 68%. GH4043 high-temperature alloy has good hot and cold working properties, further alloyed based on GH4033, and exhibits good overall performance. Compared to GH4033, it has uniformly fine grains, a yield strength of (80-100) MPa, and provides creep and fatigue performance. It has good hot working properties and is easy to shape.

The GH4145 (GH145) alloy is a nickel-based superalloy that is strengthened by aging with the γ′ [Ni3(Al, Ti, Nb)] phase. It exhibits good corrosion resistance and oxidation resistance below 980°C, high strength below 800°C, and good relaxation resistance below 540°C. Additionally, it has excellent formability and weldability. This alloy is primarily used to manufacture ring parts, structural components, and bolts that operate below 800°C and require high strength and corrosion resistance, as well as flat springs and helical springs that operate below 540°C with moderate or lower stress and require relaxation resistance. It can also be used to manufacture parts such as gas turbine blades. Available forms include plates, strips, bars, forgings, rings, wires, and tubes.

GH1015 high-temperature alloy is a solid solution strengthened iron-based high-temperature alloy composed of elements such as nickel, molybdenum, and niobium, with a nickel content of about 38%. GH1015 high-temperature alloy has good hot and cold working properties, exhibiting a good combination of strength and plasticity at various temperatures, along with high thermal strength, good thermal fatigue resistance, and oxidation resistance; its stamping, welding, and other process performances are also good. There may be aging phenomena during long-term use.

GH1016 high-temperature alloy is a solid solution strengthened iron-based high-temperature alloy composed of elements such as nickel, molybdenum, and niobium, with a nickel content of about 35%. GH1016 high-temperature alloy has good hot and cold working properties, exhibiting a favorable combination of strength and plasticity at various temperatures, along with high thermal strength, good thermal fatigue resistance, and oxidation resistance; its stamping and welding process performance is also good. There may be aging phenomena during long-term use.

GH1035 high-temperature alloy is a solid solution strengthened iron-based high-temperature alloy composed of elements such as nickel, chromium, niobium, and nitrogen, with a nickel content of about 38%. GH1035 high-temperature alloy has good hot and cold working properties, as well as excellent oxidation resistance, plasticity, and impact performance. It is used in the combustion chambers of turbo engines, afterburners, and other sheet metal components. It is also suitable for use at temperatures ranging from 550 to 1000°C, for manufacturing general load-bearing components in aerospace, aviation, gas turbines, and other industrial applications (excluding turbine blades), and for components such as combustion chambers and afterburners in turbo engines operating below 950°C.

GH1040 iron-based high-temperature alloy is a solid solution strengthened iron-based high-temperature alloy composed of elements such as nickel, molybdenum, chromium, and nitrogen, with a nickel content of about 26%. The GH1040 high-temperature alloy has good hot and cold working properties, and can achieve sufficiently high instantaneous strength for short-term use at temperatures between 990-1000°C; it also has good plasticity during hot processing.

GH1131 is a high-performance iron-based superalloy strengthened by solid solution of elements such as tungsten, molybdenum, niobium, and nitrogen, with a nickel content of about 28%. However, its thermal strength level is comparable to that of the GH3044 alloy. The alloy exhibits good hot workability and performance in welding and cold forming processes. The main products include cold-rolled thin plates, hot-rolled medium plates, bars, flat steel, and wires. It can be used to manufacture high-temperature components for rocket engines operating for short periods at 700 to 1000°C and for aircraft engines operating for long periods at 700 to 750°C.

GH1140 high-temperature alloy is a solid solution strengthened iron-nickel-based high-temperature alloy. In addition to containing a large amount of chromium, it is also reinforced with a small amount of tungsten, molybdenum, aluminum, and titanium. The alloy has moderate thermal strength, high plasticity, good thermal fatigue resistance, structural stability, and welding process performance. It is suitable for manufacturing sheet structural components and other high-temperature parts for aircraft engines and gas turbine combustion chambers operating at temperatures below 850°C. Various deformed products such as plates, rods, pipes, wires, strips, and forgings can be supplied.

GH2018 high-temperature alloy is a type of aging-hardened iron-based high-temperature alloy composed of elements such as tungsten, molybdenum, and nickel, with a nickel content of about 43%. GH2018 high-temperature alloy has good hot and cold working properties, and exhibits good processability in the solution-treated state; after complete heat treatment, it has high high-temperature strength.

GH2036 (GH36) high-temperature alloy is a type of iron-based high-temperature alloy that is age-hardened and composed of elements such as chromium, molybdenum, and nickel, with a nickel content of about 8%. GH2036 (GH36) high-temperature alloy has good hot and cold working properties, a simple alloy composition, stable microstructure, and exhibits good physical and mechanical properties at 600-650°C, along with excellent machinability. The alloy has a large coefficient of expansion.

GH2038 high-temperature alloy is a type of aging-hardened iron-based high-temperature alloy composed of elements such as chromium, nickel, and titanium, with a nickel content of about 20%. The GH2038 high-temperature alloy has good hot and cold working properties, sufficient thermal strength for use below 700°C, and exhibits good machinability and weldability.

GH2130 high-temperature alloy is a type of aging-hardened iron-based high-temperature alloy composed of elements such as chromium, nickel, and tungsten, with a nickel content of about 38%. GH2130 high-temperature alloy has good hot and cold working properties, excellent plasticity, and its structure and performance remain stable during long-term use below 800°C. Its high-temperature strength is comparable to that of GH4037.

IncoloyA-286 Nickel-Based Alloy Overview: It has high yield strength, durability and creep strength below 650°C, and has good processing plasticity and satisfactory welding function. It is suitable for the manufacture of high-temperature load-bearing parts of aero engines that work for a long time below 650°C, such as turbine discs, press discs, rotor blades and fasteners. The alloy can produce deformed products of various shapes, such as coils, forgings, plates, rods, wires and rings, etc. IncoloyA-286 nickel-based alloy improves alloy purity, restricts gas content, controls low melting point element content, and adjusts heat treatment guidelines, so that the thermal strength and long-term use function of the alloy are improved.

Monel K-500 (N055000) is a type of Monel alloy that is widely used and has excellent overall performance as a corrosion-resistant alloy. This alloy exhibits outstanding corrosion resistance in hydrofluoric acid and fluorine gas environments, as well as good corrosion resistance in hot concentrated alkaline solutions. The chemical composition of Monel K-500 (N055000) mainly consists of 30% Cu and 63% Ni, with a small amount of Fe (1%-2%). Compared to Monel 400, it also contains aluminum and titanium.