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.
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 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.
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Maraging (Vascomax) specification abstracts Maraging 250 (AMS 6512/MIL-S-46850) Maraging 300 (AMS 6514/MIL-S-46850) Maraging 350 (MIL-S-46850) Maraging ( Vascomax) in Aerospace Maraging (Vascomax) is stronger than most standard steel yet still malleable. It can be flow formed over mandrels as a thinner rocket or missile skin at any length. Thinner means more room for payloads and fuel. Maraging for the Military Our armed forces rely on weapons that perform reliably over long periods in harsh environments. Maraging (Vascomax) retains its strength and has minimum distortion and deterioration, even after heat and pressure. It is a key material in the manufacture of all types of firing pins and breech blocks. Maraging in Transportation Maragings superior strength and ductility make it the preferred material for critical parts such as landing gear in all types of civilian and military aircraft. Temperature changes and sudden or constant applications of pressure, impact or torque, have little effect on parts made from Maraging. It is the ideal material for high performance internal engine components such as shafts, gears and fasteners. Maraging in Manufacturing Maragings ability to expand without cracking make it the material of choice for drill chucks. Its uniform machinability and durability make it ideal for producing gears in sophisticated robotic arms in assembly lines, and its high strength and wear resistance make it perfect for grippers in automation lines. Other Maraging (Vascomax) benefits for the manufacturing arena include excellent polishability and weldability with pre- or post heating. Maraging in Tool & Die Making Maraging (Vascomax) has a significant cost advantage over other alloys. Uniform predictable shrinkage during heat treatment means Maraging does not require excessive reworking. It is easily machined. Its hardness and strength allow it to withstand the repeated pressures of compression molding for longer tool life with a very good surface finish.
