Haynes 230 Alloy Suppliers and Manufacturers

Haynes 230 is a nickel-based superalloy that is known for its high strength, excellent resistance to oxidation and corrosion, and good thermal stability. It was developed by Haynes International, Inc., and is commonly used in high-temperature applications, such as gas turbine engines, aerospace, and chemical processing industries. Chemical Composition: Haynes 230 is composed of a range of elements, including nickel (Ni), chromium (Cr), molybdenum (Mo), iron (Fe), cobalt (Co), manganese (Mn), silicon (Si), carbon (C), and aluminum (Al). The chemical composition of Haynes 230 can be adjusted within certain ranges to meet specific application requirements. Mechanical Properties: Haynes 230 has excellent mechanical properties, including high strength, good ductility, and toughness. Its yield strength is 685 MPa and its tensile strength is 1025 MPa. It also has a 42% elongation rate. Thermal Properties: Haynes 230 exhibits good thermal stability, making it an excellent choice for high-temperature applications. Its melting point is 1305�°C (2381�°F), and it has a thermal expansion coefficient of 13.7 �µm/m�·K (7.6 �µin/in�·�°F). Corrosion and Oxidation Resistance: Haynes 230 has excellent resistance to oxidation and corrosion in high-temperature and high-stress environments. It has a good resistance to sulfur-bearing gases, such as hydrogen sulfide (H2S) and sulfur dioxide (SO2), and can withstand harsh chemical environments. Weldability: Haynes 230 can be welded using a variety of methods, including gas tungsten arc welding (GTAW), gas metal arc welding (GMAW), and resistance welding. However, special precautions need to be taken during welding to avoid cracking and other defects. Here are the country standards for Haynes 230 alloy: USA: AMS 5878, AMS 5879, AMS 5962, AMS 5963, AMS 5964, AMS 5965, AMS 5966, AMS 5967, AMS 5968, AMS 5969, AMS 5970, AMS 5971, AMS 5972, AMS 5973, AMS 5974, AMS 5975, AMS 5976, AMS 5977, AMS 5978, AMS 5979, AMS 5980, AMS 5981, AMS 5998, AMS 5999, AMS 5877, ASTM B366, ASTM B435, ASTM B572, ASTM B619, ASTM B622, ASTM B626, ASTM B366, UNS N06230 Europe: EN 2.4733 Germany: DIN 17742, VdT�?V 546 UK: BS HR 201 Japan: JIS NW 6230 We can provide the following the form:Haynes 230 coil; Haynes230 strip;Haynes 230 plate; Haynes 230 sheets; Haynes 230 tube; Haynes 230 pipe;Haynes 230 flat; Haynes 230 bar GB/JIS:NW 6230/UNS:R06230/W.Nr:2.4733 Haynes 230 is widely used in high-temperature applications, such as gas turbine engines, aerospace, and chemical processing industries. It is also used in heat exchangers, industrial furnaces, and in the production of petroleum and natural gas. Its excellent mechanical properties, corrosion and oxidation resistance, and good weldability make it a popular choice for a wide range of applications.

Haynes 242 is a nickel-chromium-molybdenum alloy with excellent high-temperature strength, good oxidation resistance, and resistance to hot corrosion and thermal fatigue. It is typically used in gas turbine engine components, such as turbine blades, vanes, and combustor liners, as well as in industrial furnace applications. Haynes 242 offers excellent high-temperature strength, with a minimum yield strength of 880 MPa and a minimum tensile strength of 1100 MPa. It also has good ductility, with a minimum elongation of 12%. In addition, it has good thermal stability and resistance to thermal fatigue, making it suitable for use in high-temperature applications. Haynes 242 also has good resistance to oxidation and hot corrosion, which makes it suitable for use in gas turbine engine components that are exposed to high-temperature and corrosive environments. It has a maximum HB hardness of 300 and excellent fatigue strength at high temperatures. Haynes 242 is typically available in the form of sheet, plate, bar, and wire. It can be machined using conventional methods and is weldable using standard welding techniques. Overall, Haynes 242 is a high-strength, high-temperature alloy with excellent resistance to oxidation and hot corrosion, making it ideal for use in gas turbine engine components and industrial furnace applications. Here are the national standards for Haynes 242 alloy: United States: AMS 5708, AMS 5776, AMS 5777, AMS 5853, AMS 5854, AMS 5857, AMS 5858, AMS 5895, AMS 5896, AMS 5897, AMS 5898, AMS 5965, AMS 5966, AMS 5967, AMS 5968, AMS 5969, AMS 5970, AMS 5971, AMS 5972, AMS 5973, AMS 5974, AMS 5975, AMS 5976, AMS 5977, AMS 5978, AMS 5979, AMS 5980, AMS 5981, ASTM B435, ASTM B572, UNS R30556 Europe: EN 2.4683 Germany: DIN 17743, VdTÃ??V 435 United Kingdom: BS HR 202, BS HR 501, BS HR 502 Japan: JIS NW 6242 We can provide the following the form:Haynes 242 coil; Haynes242 strip;Haynes 242 plate; Haynes 242 sheets; Haynes 242 tube; Haynes 242 pipe;Haynes 242 flat; Haynes 242 bar GB/JIS:NW 625/UNS:N10242/W.Nr:2.4683 Haynes 242 is typically used in gas turbine engine components, such as turbine blades, vanes, and combustor liners. It is also used in industrial furnace applications, including muffles, retorts, and heat treating fixtures. The high-temperature strength and excellent resistance to oxidation and hot corrosion make Haynes 242 an ideal material for use in high-temperature and corrosive environments. It is commonly used in aerospace, power generation, and industrial applications where high-temperature and corrosive conditions are present.

Haynes 188 is a high-temperature, high-strength, and high-corrosion-resistant superalloy developed and produced by Haynes International in the United States. It is typically used in high-temperature, high-pressure, and corrosive environments. Haynes 188 alloy is renowned for its outstanding high-temperature strength and excellent corrosion resistance. The main components of Haynes 188 alloy include nickel, chromium, molybdenum, iron, titanium, aluminum, and tantalum. The combination of these elements gives Haynes 188 extremely high heat resistance and corrosion resistance. It can be used at temperatures as high as 1095 and has excellent oxidation and thermal corrosion resistance. Additionally, Haynes 188 has good machinability, weldability, and castability, making it suitable for manufacturing components of various shapes and sizes. The following are the international standards for Haynes 188 alloy: United States: AMS 5608, AMS 5772, AMS 5801, AMS 5796, AMS 5797, AMS 5800, AMS 5879, AMS 6925, AMS 5803, AMS 5596, AMS 5708, AMS 5804, AMS 5806, AMS 5799, AMS 5836, AMS 5875, AMS 5954, ASTM B574, ASTM B574M, ASTM B435, ASTM B582, UNS R30188 Europe: EN 2.4683, EN 2.4684, EN 2.4694 Germany: DIN 17743 France: AFNOR Z 20 CNDT 35.20, AIR 9165 United Kingdom: BS HR 203, BS HR 504, BS HR 505 Japan: JIS NW 5886 We can provide the following the form:Haynes 188 coil; Haynes 188 strip;Haynes 188 plate; Haynes 188 sheets; Haynes 188 tube; Haynes 188 pipe;Haynes 188 flat; Haynes 188 bar GB:GH5188/JIS:NW 6190/UNS:R30188/W.Nr:2.4683 Haynes 188 is primarily used in aerospace, petrochemical, chemical, energy, and marine fields. In aerospace, Haynes 188 is commonly used to manufacture components such as turbine blades, combustors, and nozzles in turbine engines. In petrochemical, chemical, and energy fields, Haynes 188 is often used to manufacture petrochemical reactors, catalyst carriers, high-temperature pipelines, corrosion-resistant coatings, and oil extraction equipment. In the marine industry, Haynes 188 is commonly used to manufacture components in marine environments such as propellers and bearings. Overall, Haynes 188 alloy has excellent high-temperature, high-strength, and high-corrosion resistance properties and is widely used in various industrial fields. It is an important superalloy material.

Haynes HR120 is a nickel-based alloy with excellent high-temperature strength, good resistance to oxidation and thermal fatigue, and excellent creep resistance. It is typically used in gas turbine engine components, such as turbine blades and vanes, as well as in industrial furnace applications. Haynes HR120 offers excellent high-temperature strength, with a minimum yield strength of 830 MPa and a minimum tensile strength of 980 MPa. It also has good ductility, with a minimum elongation of 14%. In addition, it has excellent creep resistance, with a rupture life of up to 20,000 hours at 760�°C. Haynes HR120 also has good resistance to oxidation and thermal fatigue, which makes it suitable for use in gas turbine engine components that are exposed to high-temperature and corrosive environments. It has a maximum HB hardness of 290 and excellent fatigue strength at high temperatures. Haynes HR120 is typically available in the form of sheet, plate, bar, and wire. It can be machined using conventional methods and is weldable using standard welding techniques. Overall, Haynes HR120 is a high-strength, high-temperature alloy with excellent resistance to oxidation and thermal fatigue, making it ideal for use in gas turbine engine components and industrial furnace applications where high-temperature and corrosive conditions are present. Here are the international standards for Haynes HR120 alloy: USA: AMS 5538, AMS 5794, AMS 5795, AMS 5798, AMS 5859, AMS 5860, AMS 5936, AMS 5937, AMS 5960, AMS 5961, AMS 5977, AMS 5978, AMS 5979, AMS 5980, AMS 5981, AMS 5990, AMS 5991, ASTM B435, ASTM B582, UNS N08120 Europe: EN 2.4869 Germany: DIN 17742 UK: BS HR 206 Japan: JIS NW 6888 We can provide the following the form:Haynes HR120 coil; HaynesHR120 strip;Haynes HR120 plate; Haynes HR120 sheets; Haynes HR120 tube; Haynes HR120 pipe;Haynes HR120 flat; Haynes HR120 bar GB/JIS/UNS:N08120/W.Nr Haynes HR120 is a high-strength, high-temperature alloy that is commonly used in gas turbine engine components and industrial furnace applications where high-temperature and corrosive environments are present. It offers excellent high-temperature strength, good ductility, and excellent creep resistance. The following are some of the specific applications of Haynes HR120: Gas turbine engine components: Haynes HR120 is often used in the manufacture of turbine blades, vanes, and other components in gas turbine engines. Its high-temperature strength, excellent creep resistance, and resistance to thermal fatigue make it ideal for use in this application.

Raw melting material - aluminum scraps, cans, engine waste etc. Output capacity - 5-30 tons/h, customized Automation - Full automatic/ half automatic (based on output requirement and investment budget Ingot type - ADC12 (7.5kg/ 10kg / customized) 1. After cleaning the oil and grease of waste aluminum, manually put it into the furnace with a forklift; 2. Ignition for melting furnace .Heat up to 680C, and input appropriate proportion of alloy elements. Heat up to 800C, melt and stir evenly, then fetch samples to the spectrometer for testing. Every lot of production need to do testing . 3. Put A tool that attracts iron into the furnace by forklift, to suck away the iron in the aluminum water. 4. Put the slag agent into Alu liquid to remove the slag. After slag removed , put the slags into Aluminum ash separation machine , and let the aluminum water and ash separate. The proportion of slag agent and aluminum liquid is 1:500 5.Open the drain valve and the aluminum water flows automatically to the ingot production line After the ingot casting is completed, the ingot stacking robot will stack the ingots, which means the production is completed.

Haynes 625 is a nickel-chromium-molybdenum alloy with niobium/tantalum added to enhance its corrosion resistance and strength at elevated temperatures. It is one of the most widely used superalloys due to its exceptional mechanical properties, high corrosion resistance, and ease of fabrication. Haynes 625 has excellent resistance to pitting, crevice corrosion, and stress corrosion cracking in chloride-containing environments, making it suitable for use in marine and chemical processing applications. It also exhibits high resistance to oxidation and scaling at elevated temperatures up to 1000â??, making it suitable for use in high-temperature applications such as gas turbines, furnace components, and heat exchangers. Haynes 625 can be easily fabricated by various methods including welding, forging, and machining. It can be used in both as-welded and annealed conditions. It is available in various forms such as plates, sheets, bars, and tubes, and is widely used in industries such as aerospace, chemical processing, oil and gas, and nuclear power. US standards: AMS 5599: Specifies the standard specifications for Haynes 625 plate, sheet, and strip; AMS 5666: Specifies the standard specifications for Haynes 625 bars, wire, profiles, and forgings; AMS 5837: Specifies the standard specifications for Haynes 625 seamless or welded tubes; ASME SB 443: Specifies the standard specifications for Haynes 625 plate, sheet, and strip; ASME SB 446: Specifies the standard specifications for Haynes 625 bars and forgings; ASME SB 444: Specifies the standard specifications for Haynes 625 seamless and welded tubes. European standards: EN 2.4856: Specifies the standard specifications for Haynes 625 plate, sheet, strip, bars, and wire; EN 10216-5: Specifies the standard specifications for Haynes 625 seamless steel tubes. Japanese standards: JIS NW 625: Specifies the standard specifications for Haynes 625 plate, sheet, strip, bars, and seamless tubes; JIS NW 6692: Specifies the standard specifications for Haynes 625 welded tubes. Chinese standards: GB/T 14992: Specifies the standard specifications for Haynes 625 plate, sheet, and strip; GB/T 14994: Specifies the standard specifications for Haynes 625 welded seamless steel tubes; GB/T 15008: Specifies the standard specifications for Haynes 625 bars and forgings; GB/T 15010: Specifies the standard specifications for Haynes 625 seamless and welded tubes. We can provide the following the products:Haynes 625 alloy coil; Haynes 625 alloy strip;Haynes 625 alloy plate; Haynes 625 alloy sheets; Haynes 625 alloy tube; Haynes 625 alloy pipe;Haynes 625 alloy flat; Haynes 625 alloy bar GB/JIS:G4903/UNS:N06625/W.Nr:2.4856

Haynes 617 is a nickel-chromium-cobalt-molybdenum alloy with excellent high-temperature strength, good oxidation resistance, and excellent resistance to carburization and sulfidation. It is commonly used in gas turbine engine components, industrial furnace applications, and other high-temperature applications. Haynes 617 has a nominal composition of 44.5% nickel, 20-24% chromium, 8-10% molybdenum, 0.5% maximum copper, 0.15% maximum carbon, 1.0% maximum cobalt, 0.5% maximum silicon, 1.0% maximum manganese, 0.015% maximum sulfur, 0.015% maximum phosphorus, and the balance iron. Haynes 617 offers excellent mechanical properties at high temperatures, making it ideal for use in gas turbine engine components such as combustion liners, transition ducts, and exhaust systems. Its high-temperature strength and resistance to carburization and sulfidation make it suitable for use in industrial furnace applications such as radiant tubes, muffles, and retorts. In addition to its high-temperature strength and resistance to oxidation and carburization, Haynes 617 also offers good resistance to thermal shock and thermal fatigue. This makes it ideal for use in applications that require resistance to cyclic heating and cooling, such as gas turbine engine components and industrial furnace applications. Overall, Haynes 617 is a versatile high-temperature alloy that offers excellent mechanical properties and resistance to corrosion and oxidation in high-temperature environments. Its use in gas turbine engine components and industrial furnace applications has been well-established, and it continues to be an important material in these industries. US standards: AMS 5887: Standard specification for Haynes 617 plate, sheet, and strip; AMS 5888: Standard specification for Haynes 617 rod, wire, and bar; AMS 5889: Standard specification for Haynes 617 seamless or welded pipe; ASME SB 166: Standard specification for Haynes 617 rod, wire, and bar; ASME SB 167: Standard specification for Haynes 617 seamless pipe; ASME SB 168: Standard specification for Haynes 617 plate, sheet, and strip; ASME SB 564: Standard specification for Haynes 617 forgings. We can provide the following the products:Haynes 617 alloy coil; Haynes 617 alloy strip;Haynes 617 alloy plate; Haynes 617 alloy sheets; Haynes 617 alloy tube; Haynes 617 alloy pipe;Haynes 617 alloy flat; Haynes 617 alloy bar GB/JIS:NW 6617/UNS:N06617/W.Nr:2.4663

Haynes 718 Alloy is a high-temperature, high-strength nickel-based alloy developed by Haynes International. It has excellent oxidation resistance, corrosion resistance, and high-temperature strength, and is widely used in high-temperature and high-pressure environments in aerospace, energy, chemical, petroleum, and natural gas industries. The chemical composition of Haynes 718 Alloy includes approximately 52% nickel, 19% chromium, 3% titanium, 5% aluminum, about 0.9% iron, and trace amounts of carbon, sulfur, phosphorus, copper, and tantalum. This combination of elements gives Haynes 718 Alloy its excellent high-temperature performance. In addition, Haynes 718 Alloy uses advanced heat treatment processes, which can further improve its high-temperature strength and oxidation resistance. Haynes 718 Alloy can be made into various shapes of products, such as sheets, rods, pipes, forgings, castings, and welding materials, etc. Its mechanical properties improve with increasing temperature, and it can maintain high strength and toughness at high temperatures ranging from 600�°C to 980�°C. In addition, Haynes 718 Alloy has excellent oxidation resistance and can withstand high-temperature oxidation environments for a long time. Haynes 718 alloy is an important nickel-based superalloy used in high-temperature applications such as gas turbine engines. Below are the standards for Haynes 718 alloy in various countries: United States: AMS 5596, AMS 5662, AMS 5663, AMS 5664, AMS 5832, AMS 5962, AMS 5665, AMS 5666, AMS 5667, AMS 5668, AMS 5669, AMS 5670, AMS 5671, AMS 5758, AMS 5759, AMS 5660, AMS 5661, AMS 5677, AMS 5909, AMS 5927, AMS 5947, AMS 5950, AMS 5963, AMS 5964, AMS 5966, AMS 5967, AMS 5968, AMS 5969, AMS 5970, AMS 5971, AMS 5972, AMS 5973, AMS 5974, AMS 5975, AMS 5976, AMS 5977, AMS 5978, AMS 5979, AMS 5980, AMS 5981, ASTM B637, ASTM B670, UNS N07718 Europe: EN 2.4668 Germany: DIN 17744, VdT�?V 718 France: AFNOR NC 19 Fe Nb United Kingdom: BS HR 201, BS HR 401, BS HR 501 Japan: JIS NW 0771 We can provide the following the form:Haynes 718 Alloy coil; Haynes 718 Alloy strip;Haynes 718 Alloy plate; Haynes 718 Alloy sheets; Haynes 718 Alloy tube; Haynes 718 Alloy pipe;Haynes 718 Alloy flat; Haynes 718 Alloy bar BS:HR 201/JIS:NC19FeNb/UNS:N07718/W.Nr:2.4669 Haynes 718 is a nickel-chromium alloy that is known for its high strength and excellent corrosion resistance. It is commonly used in a wide range of applications, including: Aerospace industry: Haynes 718 is widely used in the aerospace industry due to its high strength, excellent fatigue resistance, and good weldability. It is used for components such as gas turbine engine parts, thrust reversers, and exhaust systems.

Haynes 718 alloy is a precipitation-hardening nickel-chromium alloy that offers high strength, toughness, and resistance to corrosion and high-temperature environments. It was developed in the 1950s for use in gas turbine engine components, and has since found a wide range of applications in other high-stress industries such as aerospace, nuclear, and chemical processing. The alloy is characterized by its excellent mechanical properties, including high tensile and yield strength, good ductility and toughness, and resistance to fatigue, creep, and stress-corrosion cracking. These properties are achieved through a combination of precipitation hardening and solid-solution strengthening, which involve heat treatment processes that cause the formation of fine, uniform precipitates within the metal matrix. Haynes 718 alloy also has good resistance to oxidation and other forms of corrosion, particularly in high-temperature environments. It is capable of maintaining its properties at temperatures up to around 1300�°F (700�°C), making it suitable for use in hot sections of gas turbine engines, nuclear reactor components, and other high-temperature applications. In addition to its mechanical and corrosion resistance properties, Haynes 718 alloy also has good weldability and machinability. It can be readily welded using a range of methods, and can be easily machined using standard metalworking techniques. Overall, Haynes 718 alloy is a versatile and reliable material that has proven itself in a wide range of demanding applications. Its combination of high strength, toughness, and resistance to corrosion and high-temperature environments make it an ideal choice for use in critical components where reliability and performance are paramount. Haynes 718 alloy standards vary by country. Here are some of the common ones: United States Standards: AMS 5596: Standard Specification for Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate, Haynes 718 AMS 5662: Standard Specification for Nickel Alloy, Bars, Forgings, and Rings, Haynes 718 AMS 5663: Standard Specification for Nickel Alloy, Bars, Forgings, and Rings, Haynes 718 (UNS N07718) AMS 5664: Standard Specification for Nickel Alloy, Bars, Forgings, and Rings, Haynes 718 (UNS N07718) AMS 5832: Standard Specification for Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire, Haynes 718 AMS 5962: Standard Specification for Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, Haynes 718 AMS 5838: Standard Specification for Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire, Haynes 718SPF We can provide the following the prodcuts:Haynes 718 alloy coil; Haynes 718 alloy strip;Haynes 718 alloy plate; Haynes 718 alloy sheets; Haynes 718 alloy tube; Haynes 718 alloy pipe;Haynes 718 alloy flat; Haynes 718 alloy bar GB/JIS:NW7718/UNS:NW7718/W.Nr:2.4668

Inconel nickel alloy It is a solid-solution strengthened nickel-based deformed superalloy with molybdenum and niobium as the main strengthening elements. It has excellent corrosion resistance and oxidation resistance. It has good tensile properties and fatigue properties from low temperature to 980 �° C, and is resistant to salt spray. Stress corrosion in atmosphere. Therefore, it can be widely used in the manufacture of aero-engine parts, aerospace structural parts and chemical equipment. The alloy has good processing and welding properties, and can supply a variety of plates, bars, pipes, wires, strips and forgings

Incoloy is a nickel-chromium-iron alloy, which is a nickel-iron-chromium iron-nickel-based corrosion-resistant alloy designed for anti-oxidation and carbonization when the temperature rises. This alloy is used in high-temperature water vapor, including steam-air-CO2 In mixed gas, it has good corrosion resistance. In some high-temperature and high-pressure water media, its stress corrosion resistance is significantly better than 18-8 stainless steel and Inconel600; it also has good corrosion resistance in H2+H2S media. In the alkaline medium containing NaOH, its stress corrosion resistance is better than high-nickel alloys such as Inconel600.

Name of product : Cobalt Concentrate 10-20% and Cobalt Hydroxide 24-26% and grade 8-10%. Price of product : LME Cobalt x Co% x payable % on dry basis ex-warehouse Zambia. Exact payable % to be determined for quality required. Product origin : Zambia Key Specifications/Special Features Harmonization System (HS) Code : Minimum Order Size : 500 mt, but up to 2000 MT per month Packaging details : Big bags

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Monel 404 is a copper-nickel alloy that has high strength and toughness over a wide temperature range and excellent resistance to many corrosive environments. The alloy also has low permeability and good brazing properties, low magnetic induction, and high strength. Application fields: Monel 404 is mainly used in chemical and petrochemical and marine development and other fields. It can be used to manufacture various heat exchange equipment, boiler feed water heaters, petroleum and chemical pipelines, containers, towers, tanks, valves, pumps, reactors, shafts, etc. We can provide the following the form:Monel alloy404 coil; Monel alloy 404 strip;Monel alloy 404 plate; Monel alloy 404 sheets; Monel alloy 404 tube; Monel alloy 404 pipe;Monel alloy 404 flat; Monel alloy 404 bar UNS:N04404

Monel 401 has excellent strength and plasticity, and has good pressure processing performance in both cold and hot states. It is a corrosion-resistant alloy with large dosage, wide application and excellent comprehensive performance. The alloy has excellent corrosion resistance in HF and F2 media, and is one of the few important materials that can withstand hydrofluoric acid. An important feature of this alloy is that it generally does not produce stress corrosion cracks and has good cutting performance. A kind of Monel alloy, its alloy structure is a high-strength single-phase solid solution, 3 a nickel-based alloy similar to Monel 400, and the corrosion resistance of the metal is fundamentally obtained by hindering the migration of charged particles through the discharge process of hydrogen ions. Obtained, the addition of 30% Cu by mass fraction minimizes the corrosion rate of TH, Ni in F, Cl and other halogen element ionic media, and the higher the Cu content, the better the resistance to sulfuric acid and phosphoric acid. Adding mass fraction to Monel 401 55% Cu improves the corrosion resistance of the alloy in reducing acids. Application fields: Wirewound Resistors bimetal contact Electrical and Electronic Applications Marine Engineering Chemical and Hydrocarbon Processing Equipment petrol and fresh water tanks Distiller degas heater Boiler feed water heaters and other heat exchangers Valves, pumps, shafts, fittings and fasteners Industrial heat exchanger Chlorinated solvents Crude distillation tower We can provide the following the form:Monel alloy401 coil; Monel alloy 401 strip;Monel alloy 401 plate; Monel alloy 401 sheets; Monel alloy 401 tube; Monel alloy 401 pipe;Monel alloy 401 flat; Monel alloy 401 bar UNS:N04401

Incoloy alloy 800, also known as UNS N08800, is a nickel-iron-chromium alloy with high strength and excellent resistance to oxidation and carburization at high temperatures. It has a high level of resistance to corrosion in many environments, including acids, alkalis, and seawater. Incoloy alloy 800 has a chemical composition of approximately 32% nickel, 21% chromium, and 46% iron, with small amounts of carbon, aluminum, and titanium. It has good mechanical properties and can be easily formed, machined, and welded.The alloy's excellent high-temperature strength and oxidation resistance make it suitable for use in heat-treating equipment such as baskets, trays, and fixtures. Incoloy alloy 800H is a high-temperature nickel-iron-chromium alloy, also known as UNS N08810. Some international standards and specifications for Incoloy alloy 800H include: American standards: ASTM B407, ASTM B163, ASTM B515, ASTM B514, ASTM B407, ASTM B408, ASTM B409, ASTM B564, ASME SB-407, ASME SB-163, ASME SB-515, ASME SB-514, ASME SB-407, ASME SB-408, ASME SB-409, ASME SB-564 European standards: EN 1.4958, EN 1.4959, EN 10216-5, EN 10217-7, EN 10222-5, EN 10269, EN 10272, EN 10296-2, EN 10028-7, EN 10095, EN 10204-3.1 Japanese standards: JIS G3456, JIS G3459, JIS G3463, JIS G3448 Chinese standards: GB/T 14992, GB/T 14994, GB/T 15001, GB/T 15003, GB/T 15007, GB/T 15009, GB/T 15011, GB/T 15013, GB/T 15014, GB/T 15021, GB/T 15023, GB/T 15025, GB/T 15027, GB/T 15029, GB/T 15031, GB/T 15033, GB/T 15037, GB/T 15039, GB/T 15041, GB/T 15043, GB/T 15045, GB/T 15047, GB/T 15049, GB/T 15051, GB/T 15053, GB/T 15055, GB/T 15057, GB/T 15059, GB/T 15061, GB/T 15063, GB/T 15065, GB/T 15067, GB/T 15069, GB/T 15071, GB/T 15073, GB/T 15075, GB/T 15077, GB/T 15079, GB/T 15081, GB/T 15083, GB/T 15085, GB/T 15087, GB/T 15089, GB/T 15091, GB/T 15093, GB/T 15095, GB/T 15097, GB/T 15099, GB/T 15101, GB/T 15103, GB/T 15105, GB/T 15107, GB/T 15109, GB/T 15111, GB/T 15113, GB/T 15115, GB/T 15117, GB/T 15119, GB/T 15121. GB/JISï¼?NCF800H/UNSï¼?N08810/W.Nrï¼?1.4958 We can provide the following the form:Incoloy alloy800H coil; Incoloy alloy 800H strip;Incoloy alloy 800H plate; Incoloy alloy 800H sheets; Incoloy alloy 800H tube; Incoloy alloy 800H pipe; Incoloy alloy 800H flat; Incoloy alloy 800H bar