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Cobalt based alloys are a type of alloy mainly composed of cobalt, containing a considerable amount of nickel, chromium, tungsten, and small amounts of alloying elements such as molybdenum, niobium, tantalum, titanium,La, and occasionally iron. Its products have good mechanical properties, stable chemical properties, and strong corrosion resistance, and are widely used in daily life and medical fields.

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TiAl titanium alloy has low density, good mechanical properties, and excellent corrosion resistance, and is widely used in aerospace, shipbuilding, military and other fields. TiAl titanium alloy powder solves a series of problems in additive manufacturing processes, and can achieve high-strength, large-sized, and lightweight components through additive manufacturing processes rapid prototyping manufacturing.

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Spherical vanadium powder is manufactured using RF plasma spheroidization technology, which has the characteristics of high purity, low oxygen content, high sphericity, smooth surface, no satellites, uniform particle size distribution, excellent flowability, high loose density and tap density.

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The tantalum implant formed by 3D printing has the closest elastic modulus to human cartilage tissue, making it the most ideal orthopedic implant material. Spherical tantalum powder is suitable for processes such as laser/electron beam additive manufacturing, hot isostatic pressing, laser cladding, and hot/cold spraying.

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GH5188 is a solid solution strengthened cobalt based high-temperature alloy, which is strengthened by adding 14% tungsten to give the alloy excellent high-temperature thermal strength. At the same time, adding a high content of chromium and trace amounts of La gives the alloy good high-temperature oxidation resistance. Compared to nickel based high-temperature alloys, GH5188 has more good creep resistance, thermal corrosion resistance, fatigue resistance, and high temperature strength. GH5188 has excellent formability, welding and other process properties, making it suitable for manufacturing parts for aircraft engines that require high strength below 980 ℃ and anti-oxidation below 1000 ℃. In the 1980s, GH5188 alloy was applied to components such as vortex plates and flame deflectors in turboshaft eight aircraft engines. Currently, some aircraft engines use GH5188 alloy sheets to prepare high-temperature components such as combustion chamber walls, outer walls, and sealing plates.

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GH4169 is an aging precipitation strengthened alloy with γ~Ni as the matrix, γ ” phase (Ni3Nb) as the main phase, and weak strengthening phase γ ‘[Ni3 (Al, Ti)] with a face centered cubic structure. It has excellent high-temperature strength, oxidation resistance, corrosion resistance, fatigue resistance, and good high-temperature creep strength. It is commonly used in the manufacture of hot end structural components and is widely used in aerospace, energy, military and other fields.

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TC4 titanium alloy has excellent mechanical properties, corrosion resistance, light specific gravity, and good biocompatibility. Such characteristics are applied in many high-performance engineering applications, such as aerospace and medical implants other fields.