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00Cr25Ni7Mo4WCuN (S32760) is a super duplex stainless steel, also known as F55 or Zeron 100. It features high strength and excellent corrosion resistance, and is widely used in the petroleum, chemical, and other strongly corrosive environments.
NiFe25Cr20NbTi is a nickel-based superalloy with excellent high-temperature strength, oxidation resistance, and corrosion resistance. It is widely used in aerospace, petrochemical, and other fields.
Alloy 602CA is a nickel-chromium-iron based high-temperature alloy with excellent high-temperature and corrosion resistance properties, widely used in industrial furnaces, petrochemicals and other fields.
Alloy 901 is an iron-nickel-chromium based austenitic age-hardenable alloy. Foreign standards include AMS 5660 and AMS 5661; the domestic equivalent is GH2901.
D6AC is a high-strength alloy steel with excellent comprehensive performance, widely used in aerospace and military industries.
Monel K500 is an age-hardenable nickel-copper alloy widely used in aerospace, chemical, marine, and other fields.
N05500 typically refers to Monel alloy K-500, a precipitation-hardenable nickel-copper alloy. It can be produced in various specifications of seamless tubes, plates, bars, forgings, flanges, rings, welded pipes, strips, wires and matching welding materials.
N04400 is a nickel-copper alloy, commonly known as Monel Alloy. It is mainly composed of nickel (Ni) and copper (Cu), with nickel content ranging from 63% to 70% and copper content ranging from 28% to 34%. In addition, it contains small amounts of other elements such as iron (Fe), manganese (Mn), silicon (Si), carbon (C), and sulfur (S).
2.4668 is a Fe-Ni-Cr based precipitation hardening deformable high-temperature alloy, corresponding to UNS N07718 in the US and GH4169 in China. Nickel-based alloy is a high-performance material widely used in various engineering projects in extreme environments.
2.4668 is a Fe-Ni-Cr based precipitation hardening deformed high-temperature alloy, corresponding to UNS N07718 in the US and GH4169 in China.
2.4858 is a fully austenitic nickel-iron-chromium alloy, corresponding to grade NCF825 and UNS number N08825 in the US. It is widely used in various industrial fields due to its excellent corrosion resistance and mechanical properties.
N08810 is a high-performance nickel-iron-chromium alloy, specifically designed for high-temperature environments, and possesses excellent oxidation, carburization, and sulfidation resistance.
N06600 is a nickel-based alloy with excellent corrosion resistance, high-temperature performance, and mechanical properties. It is widely used in the chemical and energy industries.
N06455 is a high-performance austenitic low-carbon nickel-molybdenum-chromium alloy, also known as Hastelloy C-4, widely used in chemical, petroleum, natural gas, power, aerospace and other industrial fields. It is often used to manufacture flue gas desulfurization systems, acid pickling and acid regeneration plant equipment, acetic acid and agricultural chemical production equipment, titanium dioxide production (chlorine method) equipment, electrolytic plating equipment, etc.
Inconel 718 is a precipitation-hardening nickel-chromium-iron alloy containing niobium and molybdenum. It has excellent comprehensive performance and is widely used in aerospace, petrochemical and other fields.
NCF690 is a high-performance nickel-based alloy with excellent corrosion resistance and high-temperature performance, widely used in aerospace, chemical and other fields.
NCF825 is a high-performance nickel-iron-chromium-based alloy, also known as Incoloy 825 or UNS N08825. It features excellent corrosion resistance and high-temperature strength, and is widely used in various fields.
NCF800 is a high-performance nickel-based alloy, also known as Incoloy 800 or N08800. High-temperature oxidation resistance: A dense oxide film forms in high-temperature environments (such as below 1000°C), effectively resisting oxidation and carburization.
The alloy is a corrosion-resistant, oxidation-resistant, and high-strength precipitation-hardening alloy. It is mainly a nickel-based superalloy that is age-hardened by the γ'' phase. Its operating temperature is below 800℃. The alloy exhibits good corrosion and oxidation resistance below 980℃, high strength below 800℃, good creep resistance below 700℃, and good stress-rupture resistance below 540℃. It also possesses good formability and weldability. In the solution-treated state, the alloy has a pure austenitic structure.
Aerospace: Used in manufacturing key components such as engine turbine disks and blades that operate at 650℃-700℃. Petroleum and Chemical Industry: Can be used to manufacture catalysts and reactors operating at high temperatures. Power Energy Sector: For example, in the manufacture of components in equipment such as gas turbines.
N06035, also known as Hastelloy G-35, is a nickel-based, solid-solution-strengthened corrosion-resistant alloy
Haynes 718 is a nickel-based precipitation-hardening superalloy with excellent comprehensive performance, widely used in aerospace, energy and other fields.
Hastelloy C-276 is a nickel-chromium-molybdenum-tungsten alloy with excellent corrosion resistance and high-temperature performance.
N08800 is an iron-nickel-based alloy, also known as Incoloy 800, with good high-temperature performance and corrosion resistance
Incoloy 825 is a nickel-iron-chromium alloy with additions of molybdenum, copper and titanium, exhibiting excellent corrosion resistance and good mechanical properties.
Inconel 800 is a Fe-Ni-Cr based solid solution strengthened, deformable, high-temperature corrosion-resistant alloy.
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