Incoloy028 Chemical Composition: Alloy % Nickel, Chromium, Molybdenum, Niobium, Tantalum, Iron, Aluminum, Titanium, Carbon, Manganese, Silicon, Copper, Phosphorus, Sulfur Incoloy028 product size range: diameter 6-500mm, length 0.5-30m; Incoloy028 product size range: thickness 0.5-80mm, length 1-6m, width 0.5-3m Incoloy028 product size range: outer diameter 6-530mm, wall thickness 0.5-50mm, length 1-12m; Incoloy028 product shape: forgings, bars, plates, strips, rings, wires, flanges, etc. can be produced according to customer requirements

Alloy 800 is in the single austenite region after high temperature and fast cooling, so the use state is a single austenite structure. The alloy has a high chromium content and sufficient nickel content, so it has high temperature corrosion resistance, and is widely used in industry. In chloride, low concentration of NaOH aqueous solution and high temperature and high pressure water, it has excellent resistance to stress corrosion cracking, so it is used to manufacture resistance force corrosion cracked equipment

Incoloy 825 is a fully austenitic nickel-iron-chromium alloy stabilized with titanium stabilized and copper and molybdenum added. Incoloy 825 It is a general-purpose engineering alloy that is resistant to acid and alkali metal corrosion in both oxidizing and reducing environments.

INCOLOY800H/HT is an austenitic heat-resistant alloy widely used in high-temperature pressure-bearing structural parts.The high strength of 800H/HT is mainly due to the addition carbon, aluminum, titanium and annealed at temperatures as low as 1149°C to achieve grain size ASTM5 grade or better.

Incoloy 800HT is an all-austenitic low-carbon nickel-iron-chromium alloy of the same series as Incoloy 800 The cobalt content in it can be strictly controlled below 0.01%.

The Cr content in Incoloy 925 (N08925) nickel-based alloy is typically 19.5-23.50% and 42.0-26.0% nickel. Incoloy 925 (N08925) alloy is a nickel-based alloy containing molybdenum and copper with good hot and cold working properties.

Incoloy926 alloy is a nickel-based alloy containing titanium and aluminum, containing enough chromium to form and maintain a sufficient scale of chromium oxide to protect it at high temperatures, and its oxidation resistance is no less than that of higher grades of alloys that can be used at temperatures up to 1900 degrees Fahrenheit (1038°C).

N08825 is a fully austenitic nickel-iron-chromium alloy that is titanium stabilized and contains copper and molybdenum. Incoloy 825 is a versatile engineering alloy that exhibits resistance to acid and alkaline metal corrosion in both oxidizing and reducing environments.

The 800 alloy is in the austenite single-phase region after rapid cooling from high temperatures, thus it exists in a single austenitic structure. The alloy has a high chromium content and sufficient nickel content, which provides excellent high-temperature corrosion resistance, making it widely used in industry. It exhibits excellent stress corrosion cracking resistance in chloride environments, low concentration NaOH solutions, and high-temperature high-pressure water, making it suitable for manufacturing equipment that requires resistance to stress corrosion cracking.

NS312 (N06600, 2.4816) alloy is an early nickel-chromium-iron-based solution strengthened alloy, which has good high temperature corrosion resistance and oxidation resistance, excellent cold and hot working and welding process performance, and satisfactory thermal strength and high plasticity below 700 °C. The alloy can be strengthened by cold working, or it can be connected by resistance welding, fusion welding or brazing, and can be supplied with cold-rolled sheets, hot-rolled thick plates, strips, wires, bars, round cakes, ring blanks, ring forgings, etc., and is suitable for making oxidation resistant parts with low loads below 1100 °C.

NS322 (Hastelloy B2, N10665) alloy is a corrosion-resistant, solid-solution nickel-molybdenum alloy. The NS322 has the following features: (1) Control the minimum content of iron and chromium to prevent the formation of β phase Ni4Mo. (2) Excellent corrosion resistance to the reducing environment. (3) Excellent resistance to moderate concentration of sulfuric acid and many non-oxidizing acids. (4) Very good resistance to chloride ion reduction stress corrosion cracking (SCC). (5) Excellent resistance to various organic acids

GH4098 is a nickel-based precipitation hardening high-temperature alloy, specifically designed to withstand extreme high-temperature environments. Its main application areas include high-temperature critical components in aerospace and missile engines. The chemical composition of the GH4098 alloy mainly includes elements such as nickel (Ni), chromium (Cr), cobalt (Co), molybdenum (Mo), tungsten (W), aluminum (Al), titanium (Ti), and niobium (Nb). The combination of these elements endows the alloy with excellent high-temperature strength, oxidation resistance, and thermal corrosion resistance.

GH4093 is a nickel-chromium-cobalt-based precipitation hardening high-temperature alloy, widely used in aerospace, chemical, and nuclear energy fields due to its excellent performance in high-temperature environments. It has good hot workability, allowing for a deformation amount of 80% without cracking in the temperature range of 1050 to 1150°C. - It has good welding performance, and plates can be connected using argon arc welding. After welding in the solution-treated state, stress relief and aging treatment should be performed. - The average grain size is closely related to the degree of deformation of the forged piece and the final forging temperature. - The cutting performance in the solution-treated state is better than that in the aged state.

GH4137 (SG37A) is a Ni-Cr based precipitation hardening deformation high-temperature alloy, suitable for use at temperatures below 700°C. It has high strength and excellent high-temperature oxidation resistance. It exhibits good creep resistance, allowing for long-term use at high temperatures without deformation. It also has good elastic modulus, wear resistance, hot workability, welding, and cold forming process performance.

GH4098 is a Ni-Cr based precipitation hardening deformation high-temperature alloy, which exhibits excellent performance in high-temperature environments, with a long-term operating temperature of up to 1000°C. Due to its outstanding comprehensive properties, this alloy has been widely used in aerospace, petrochemical, and nuclear industries.