ALLOY C276Technical Parameter List
Alloy C276 (UNS N10276) exhibits outstanding resistance in a wide range of chemical environments, including highly oxidizing, reducing media, and chloride-containing environments. Its composition is specifically designed to minimize the risk of intergranular corrosion and has excellent resistance to stress corrosion cracking, making it an ideal material choice for extreme corrosive conditions. Alloy C276 is typically used in its annealed state to ensure optimal corrosion resistance and toughness.
I. Unified Specifications for Brand Names
| American Standard (UNS): N10276 |
| National Standard (GB): NS3304 |
| European standard (EN): 2.4819 |
| Standard (JIS): NW 0276 |
II. Chemical Composition (Reference Standard: ASTM B575)
| Element | Content range (%) |
| Nickel (Ni) | Margin |
| Molybdenum (Mo) | 15.0 – 17.0 |
| Chromium (Cr) | 14.5 – 16.5 |
| Iron (Fe) | ≤4.0–7.0 |
| Tungsten (W) | 3.0 – 4.5 |
| Cobalt (Co) | ≤2.5 |
| Manganese (Mn) | ≤1.0 |
| Silicon (Si) | ≤0.08 |
| Carbon (C) | ≤0.01 |
| Phosphorus (P) | ≤0.04 |
| Sulfur (S) | ≤0.03 |
| Vanadium (V) | ≤0.35 |
III. Physical Properties
IV. Mechanical Properties (ASTM B574)
| Performance indicators | Condition / State | Typical value | Organization |
| Tensile Strength | Solution Annealed | ≥690 | MPa |
| Yield Strength, 0.2% | Solution Annealed | ≥283 | MPa |
| Elongation | Solution Annealed | ≥40 | % |
V. Typical Application Scenarios
| Core application fields |
| 1.The sulfuric acid and hydrochloric acid industries |
| 2.Petroleum and chemical industry and natural gas |
| 3.Ocean Engineering and Ships |
| 4.Pharmaceuticals and Food Processing |
| 5.Support customization for high-demand scenarios such as aerospace, nuclear power, and chemical engineering. |
VI.Material form and standard specifications
| Form | Standard |
| Round rod | ASTM A574 |
| Seamless pipe | ASTM B622 |
| Plastic sheet | ASTM A575 |
ALLOY 22Technical Parameter List
Alloy 22 (UNS N06022) exhibits outstanding corrosion resistance and performs exceptionally well in various extreme corrosive environments. It contains a high content of chromium and molybdenum, providing excellent oxidation resistance and resistance to pitting and crevice corrosion, as well as good resistance to chloride stress corrosion cracking. The composition of this alloy is well balanced, enabling it to maintain excellent stability and corrosion resistance even in the annealed state. It is one of the important representatives of high-performance corrosion-resistant materials.
I. Unified Specifications for Brand Names
| American Standard (UNS): N0602 |
| National Standard (GB): NS3308 |
| European standard (EN): 2.4602 |
| Standard (JIS): NCF 62 |
II. Chemical Composition (Reference Standard: ASTM B574)
| Element | Content range (%) |
| Nickel (Ni) | Margin |
| Chromium (Cr) | 20.0 – 22.5 |
| Molybdenum (Mo) | 12.5 – 14.5 |
| Iron (Fe) | 2.0 – 6.0 |
| Tungsten (W) | 2.5 – 3.5 |
| Cobalt (Co) | ≤2.5 |
| Manganese (Mn) | ≤0.5 |
| Silicon (Si) | ≤0.08 |
| Carbon (C) | ≤0.015 |
| Phosphorus (P) | ≤0.02 |
| Sulfur (S) | ≤0.02 |
| Vanadium (V) | ≤0.35 |
III. Physical Properties
IV. Mechanical Properties (ASTM B574)
| Performance indicators | Condition / State | Typical value | Organization |
| Tensile strength | Solution Annealed | ≥690 | MPa |
| Yield Strength, 0.2% | Solution Annealed | ≥310 | MPa |
| Elongation | Solution Annealed | ≥45 | % |
V. Typical Application Scenarios
| Core application fields |
| 1. Chemical and Petrochemical Industry |
| 2. Marine Engineering |
| 3. Pharmaceutical Manufacturing and Food Processing |
| 4. Nuclear Energy and Environmental Protection |
| 5. Supports customization for high-demand scenarios such as aerospace, nuclear power, and chemical industries. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM A574 |
| Seamless pipe | ASTM B622 |
| Plastic sheet | ASTM A575 |
ALLOY 20Technical Parameter List
Alloy 20 (UNS N08020) contains molybdenum and copper and has excellent corrosion resistance, particularly showing outstanding stability in medium-concentration sulfuric acid environments. This alloy achieves this by adding niobium to stabilize the carbide structure and reduce the tendency of intergranular corrosion. In the annealed state, it possesses good toughness and weldability. Its comprehensive performance makes it one of the commonly used corrosion-resistant materials in the chemical industry.
I. Unified Specifications for Brand Names
| American Standard (UNS): N08020 |
| National Standard (GB): NS0808 |
II. Chemical Composition (Reference Standard: ASTM B473)
| Element | Content range (%) |
| Nickel (Ni) | 32.0 – 38.0 |
| Iron (Fe) | Margin |
| Chromium (Cr) | 19.0 – 21.0 |
| Molybdenum (Mo) | 2.0 – 3.0 |
| Copper (Cu) | 3.0 – 4.0 |
| Manganese (Mn) | ≤2.0 |
| Silicon (Si) | ≤1.0 |
| Carbon (C) | ≤0.07 |
| Phosphorus (P) | ≤0.045 |
| Sulfur (S) | ≤0.035 |
| Columbium(Nb)+Tantalum | 8 x carbon-1.00 |
III. Physical Properties
IV. Mechanical Properties (Referencing Standard ASTM B473)
| Performance indicators | Condition / State | Typical value | Organization |
| Tensile Strength | Annealed | ≥551 | MPa |
| Yield Strength, 0.2% | Annealed | ≥241 | MPa |
| Elongation | Annealed | ≥30 | % |
| Reduction of area | Annealed | ≥50 | % |
V. Typical Application Scenarios
| Core application fields |
| 1.The sulfuric acid and phosphoric acid industries |
| 2.Petroleum and chemical industry and natural gas |
| 3.Pharmaceuticals and Food Processing |
| 4.Ocean Engineering |
| 5.Support customization for high-demand scenarios such as aerospace, nuclear power, and chemical engineering. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM A473 |
| Seamless pipe | ASTM B729 |
| Plastic sheet | ASTM A575 |
ALLOY B2Technical Parameter List
Alloy B-2 (UNS N10665) has an extremely high molybdenum content, which endows it with outstanding resistance to reducing acid corrosion, especially excellent resistance to hydrochloric acid and sulfuric acid. This alloy enhances its corrosion resistance and weldability by controlling the content of impurity elements such as iron, silicon, and carbon, while reducing the risk of intergranular corrosion. When used in the annealed state, Alloy B-2 can provide excellent corrosion resistance and good toughness.
I. Unified Specifications for Brand Names
| American Standard (UNS): N10665 |
| National Standard (GB): NS3202 |
| European standard (EN): 2.4617 |
II. Chemical Composition (Reference Standard: ASTM SB564)
| Element | Content range (%) |
| Nickel (Ni) | Margin |
| Molybdenum (Mo) | 26.0 – 30.0 |
| Iron (Fe) | ≤2.0 |
| Chromium (Cr) | ≤1.0 |
| Cobalt (Co) | ≤1.0 |
| Manganese (Mn) | ≤1.0 |
| Silicon (Si) | ≤0.10 |
| Carbon (C) | ≤0.02 |
| Phosphorus (P) | ≤0.04 |
| Sulfur (S) | ≤0.03 |
III. Physical Properties
IV. Mechanical Properties (Referencing Standard ASTM SB564)
| Performance indicators | Typical value | Organization |
|
| Tensile Strength | Solution Annealed | ≥760 | MPa |
| Yield Strength, 0.2% | Solution Annealed | ≥350 | Mpa |
| Elongation | Solution Annealed | ≥40 | % |
V. Typical Application Scenarios
| Core application fields |
| 1.Chemical and Petrochemical Industry |
| 2.Petroleum and chemical industry and natural gas |
| 3.Pharmaceuticals and Food Processing |
| 4.Ocean Engineering |
| 5.Support customization for high-demand scenarios such as aerospace, nuclear power, and chemical engineering. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM SB564 |
| Seamless pipe | ASTM B622 |
| Plastic sheet | ASTM A333 |
ALLOY B3Technical Parameter List
Alloy B-3 (UNS N10675) is a nickel-molybdenum alloy, an improved version of Alloy B-2. It has a higher molybdenum content and a lower carbon content, thereby providing superior resistance to reducing acid corrosion, especially in terms of its corrosion resistance to hydrochloric acid. By further reducing the content of impurity elements such as carbon and silicon, Alloy B-3 enhances its resistance to intergranular corrosion and improves the stability of the material during welding and manufacturing processes. Compared to B-2, it maintains excellent corrosion resistance while also improving processing characteristics and long-term thermal stability.
I. Unified Specifications for Brand Names
| American Standard (UNS): N10675 |
| National Standard (GB): NS3203 |
| European standard (EN): 2.4675 |
II. Chemical Composition (Reference Standard: ASTM SB564)
| Element | Content range (%) |
| Nickel (Ni) | ≥65 |
| Molybdenum (Mo) | 27.0 – 32.0 |
| Iron (Fe) | 1.0 – 3.0 |
| Cobalt (Co) | ≤3.0 |
| Manganese (Mn) | ≤3.0 |
| Chromium (Cr) | 1.0 – 3.0 |
| Aluminum (Al) | ≤0.50 |
| Copper (Cu) | ≤0.20 |
| Titanium (Ti) | ≤0.20 |
| Silicon (Si) | ≤0.10 |
| Carbon (C) | ≤0.01 |
| Phosphorus (P) | ≤0.03 |
| Sulfur (S) | ≤0.01 |
| Tungsten (W) | ≤3.0 |
| Vanadium (V) | ≤0.20 |
| Ni+Mo | 94.0-98.0 |
| Nb | ≤0.20 |
| Ta | ≤0.20 |
| Zr | ≤0.10 |
III. Physical Properties
IV. Mechanical Properties (ASTM SB564)
| Performance indicators | Typical value | Organization / Company / Institution |
|
| Tensile Strength | Solution Annealed | ≥760 | MPa |
| Yield Strength, 0.2% | Solution Annealed | ≥350 | Mpa |
| Elongation | Solution Annealed | ≥40 | % |
V. Typical Application Scenarios
| Core application fields |
| 1. High-temperature chemical and petrochemical industries |
| 2. Petrochemicals and Natural Gas |
| 3. Pharmaceutical Manufacturing and Food Processing |
| 4. Marine Engineering |
| 5. Supports customization for high-demand scenarios such as aerospace, nuclear power, and chemical industries. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM SB564 |
| Seamless pipe | ASTM B622 |
| Plastic sheet | ASTM A333 |
ALLOY 400Technical Parameter List
Alloy 400 (UNS N04400) is a nickel-copper alloy with excellent corrosion resistance, capable of maintaining stability in various media such as seawater, hydrofluoric acid, and other non-oxidizing acids. This alloy ensures good mechanical properties and corrosion resistance by adjusting the ratio of nickel and copper. It also contains small amounts of iron, manganese, and other elements to enhance its processing performance. Alloy 400 performs exceptionally well over a wide temperature range, not only being resistant to corrosion but also having good cold workability and weldability, enabling it to maintain excellent toughness and stability even in extreme conditions.
I. Unified Specifications for Brand Names
| American Standard (UNS): N0440 |
| European standard (EN): 2.4360 |
II. Chemical Composition (in accordance with ASTM SB564 standard)
| Element | Content range (%) |
| Nickel (Ni) | ≥63.0 |
| Copper (Cu) | 28.0 – 34.0 |
| Iron (Fe) | ≤2.5 |
| Manganese (Mn) | ≤2.0 |
| Carbon (C) | ≤0.30 |
| Silicon (Si) | ≤0.50 |
| Sulfur (S) | ≤0.024 |
III. Physical Properties
IV. Mechanical Properties (ASTM SB564)
| Performance indicators | Condition / State | Typical value (annealed state) | Organization |
| Tensile Strength | Annealed | ≥483 | MPa |
| Yield Strength, 0.2% | Annealed | ≥172 | MPa |
| Elongation | Annealed | ≥35 | % |
V. Typical Application Scenarios
| Core application areas |
| 1. Marine Engineering |
| 2. Chemical and Petrochemical Industry |
| 3. Pharmaceutical Manufacturing and Food Processing |
| 4. Valve and pump body assembly |
| 5. Supports customization for high-demand scenarios such as aerospace, nuclear power, and chemical industries. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM SB564 |
| Seamless pipe | ASTM B165 |
| Plastic sheet | ASTM A127 |
ALLOY K500Technical Parameter List
Alloy K500 (UNS N05500) is a precipitation-hardening alloy based on Alloy 400 (a nickel-copper alloy) with the addition of aluminum and titanium. This combination not only retains the excellent corrosion resistance of the nickel-copper alloy but also forms the γ' phase (Ni₃(Al,Ti)) in the alloy through aging treatment, thereby significantly enhancing the strength and hardness of the material. Therefore, Alloy K500 has outstanding mechanical properties, such as enhanced tensile strength and wear resistance, while maintaining good toughness. Its composition design aims to improve the overall performance of the material, enabling it to exhibit excellent corrosion resistance and mechanical properties in harsh environments.
I. Unified Specifications for Brand Names
| American Standard (UNS): N0550 |
| European standard (EN): 2.4375 |
II. Chemical Composition (in accordance with ASTM B865 standard)
| Element | Content range (%) |
| Nickel (Ni) | ≥63.0 |
| Copper (Cu) | 27.0 – 33.0 |
| Aluminum (Al) | 2.3 – 3.15 |
| Titanium (Ti) | 0.35 – 0.85 |
| Iron (Fe) | ≤2.0 |
| Manganese (Mn) | ≤1.5 |
| Carbon (C) | ≤0.20 |
| Silicon (Si) | ≤0.50 |
| Sulfur (S) | ≤0.010 |
III. Physical Properties
IV. Mechanical Properties (in accordance with ASTM B865 standard)
| Form | Condition | Maximum Section Thickness, in. (mm) | Tensile Strength, min. ksi (MPa) | Yield Strength¹, min. ksi (MPa) | Elongation² in 2 in. or 4D, min. % |
| Rounds⁴ hexagons, squares, rectangles, and forgings⁵ | Hot-worked and age-hardened | All sizes | 140 (965) | 100 (690) | 20 |
| Rounds | Cold-worked and age-hardened | over ¼ (6.4) to 1 (25.4), incl | 145 (1000) | 110 (760) | 15 |
|
| over 1 (25.4) to 3 (76.2), incl | 140 (965) | 100 (690) | 17 |
|
| over 3 (76.2) to 4 (101.6), incl | 135 (930) | 96 (655) | 20 |
| Hexagons | Cold-worked and age-hardened | ¼ (6.4) to 2 (50.8), incl | 140 (965) | 100 (690) | 15 |
| Rounds, hexagons, squares, rectangles, and forgings | Annealed and age-hardened⁶ | Up to 1 (25.4) | 130 (895) | 90 (620) | 20 |
|
| 1 (25.4) and over | 130 (895) | 85 (585) | 20 |
V. Typical Application Scenarios
| Core application areas |
| 1. Marine Engineering and Ships |
| 2. Petrochemicals and Natural Gas |
| 3. Aerospace and Nuclear Energy |
| 4. Valve and pump body assembly |
| 5. Supports customization for high-demand scenarios such as aerospace, nuclear power, and chemical engineering. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM B865 |
ALLOY 625Technical Parameter List
Alloy 625 (UNS N06625) is a nickel-chromium-molybdenum alloy that contains a significant proportion of chromium and molybdenum, as well as a small amount of niobium and tantalum. These elements give it outstanding corrosion resistance and high-temperature strength. This alloy enhances its resistance to pitting and crevice corrosion in chloride ion environments by forming a stable oxide film. It also has excellent resistance to oxidation and reduction media. Alloy 625 maintains good mechanical properties at high temperatures and its composition design ensures excellent weldability and machinability, making it exhibit excellent stability and reliability in extreme environments. Additionally, its performance can be further enhanced through solid solution strengthening or precipitation hardening.
I. Unified Specifications for Brand Names
| American Standard (UNS): N06625 |
| European standard (EN): 2.4856 |
II. Chemical Composition (in accordance with ASTM B446 standard)
| Element | Content range (%) |
| Nickel (Ni) | ≥58.0 |
| Chromium (Cr) | 20.0 – 23.0 |
| Molybdenum (Mo) | 8.0 – 10.0 |
| (Cb) + Tantalum (Ta) | 3.15 – 4.15 |
| Iron (Fe) | ≤5.0 |
| Cobalt (Co) | ≤1.0 |
| Manganese (Mn) | ≤0.5 |
| Silicon (Si) | ≤0.5 |
| Aluminum (Al) | ≤0.4 |
| Titanium (Ti) | ≤0.4 |
| Carbon (C) | ≤0.10 |
| Phosphorus (P) | ≤0.015 |
| Sulfur (S) | ≤0.015 |
III. Physical Properties
IV. Mechanical Properties (ASTM B446)
| Performance indicators | Condition / State | Typical value (annealed state) | Organization |
|
| Tensile strength (Tensile Strength) | Annealing (Annealed) | ≥120 | ksi | Outer diameter ≤ 4 inches |
| Yield Strength (0.2%) | Annealing (Annealed) | ≥60 | ksi | Outer diameter ≤ 4 inches |
| Elongation | Annealed | ≥30 | % | Outer diameter ≤ 4 inches |
| Tensile Strength | Annealed | ≥110 | ksi | Outer diameter > 4 inches |
| Yield Strength, 0.2% | Annealed | ≥50 | ksi | Outer diameter > 4 inches |
| Elongation | Annealed | ≥25 | % | Outer diameter > 4 inches |
| Tensile Strength | Solution Annealed | ≥100 | ksi | all sizes |
| Yield Strength, 0.2% | Solution Annealed | ≥40 | ksi | all sizes |
| Elongation | Solution Annealed | ≥30 | % | all sizes |
V. Typical Application Scenarios
| Core application fields |
| 1. Aerospace and Nuclear Energy |
| 2. Marine Engineering and Ships |
| 3. Petrochemical Industry and Natural Gas |
| 4. Valve and pump body assembly |
| 5. Supports customization for high-demand scenarios such as aerospace, nuclear power, and chemical engineering. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM B446 |
| Seamless pipe | ASTM B444 |
| Plastic sheet | ASTM A443 |
ALLOY 718Technical Parameter List
Alloy 718 (UNS N07718) is a precipitation-hardening type nickel-chromium-iron alloy that contains a significant proportion of chromium, molybdenum, niobium, and titanium. Alloy 718 not only possesses excellent mechanical properties, such as high strength and good toughness, but also remains stable over a wide temperature range. Its composition is specially designed to reduce the carbon content to avoid embrittlement, and elements such as aluminum and titanium are added to promote the formation of strengthening phases, making this material exhibit outstanding creep resistance and stability in extreme environments. Additionally, it also has good weldability and machinability.
I. Unified Specifications for Brand Names
| American Standard (UNS): N07718 |
| National Standard (GB): GH4169 |
| European standard (EN): 2.4668 |
II. Chemical Composition (in accordance with ASTM B637 standard)
| Element | Content range (%) |
| Nickel (Ni) | 50.0 – 55.0 |
| Chromium (Cr) | 17.0 – 21.0 |
| Iron (Fe) | Margin |
| Molybdenum (Mo) | 2.8 – 3.3 |
| Cobalt (Co) | 4.75 – 5.50 |
| Copper (Cu) | ≤0.30 |
| Aluminum (Al) | 0.2 – 0.8 |
| Titanium (Ti) | 0.65 – 1.15 |
| Manganese (Mn) | ≤0.35 |
| Silicon (Si) | ≤0.35 |
| Carbon (C) | ≤0.08 |
| Phosphorus (P) | ≤0.015 |
| Sulfur (S) | ≤0.015 |
| Boron | ≤0.006 |
III. Physical Properties
IV. Mechanical Properties (ASTM B637)
| Performance indicators | Condition / State | Typical value (present tense) | Organization |
| Tensile strength (Tensile Strength) | Timely processing (solution+precipitation Harden) | ≥1275 | MPa |
| Yield Strength, 0.2% | solution+precipitation Harden | ≥1034 | MPa |
| Elongation | solution+precipitation Harden | ≥12 | % |
| Reduction of area | solution+precipitation Harden | ≥15 | % |
V. Typical Application Scenarios
| Core application fields |
| 1. Aerospace and Rocket Engines |
| 2. Nuclear Energy and Petrochemical Industry |
| 3. Marine Engineering and Ships |
| 4. Valve and pump body assembly |
| 5. Supports customization for high-demand scenarios such as aerospace, nuclear power, and chemical engineering. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM B637 |
| Plastic sheet | ASTM A670 |
TITANIUM GRADE2Technical Parameter List
Titanium Grade 2 (UNS R50400) is an industrial pure titanium known for its outstanding comprehensive properties, including excellent corrosion resistance, excellent formability and weldability. It contains a small amount of impurity elements such as oxygen, nitrogen, carbon and iron. These components help enhance the material's strength while maintaining high ductility and toughness. Titanium Grade 2 performs well over a wide temperature range, not only resisting the erosion of various corrosive media but also having a relatively low density and good mechanical properties, making it an ideal choice for applications requiring high corrosion resistance and good machinability. This grade of titanium is usually in a annealed state to ensure the best corrosion resistance and operational performance.
I. Unified Specifications for Brand Names
| ASTM standard: Titanium Grade 2 |
| National Standard (GB): TA2 |
| European standard (EN): 3.7035 |
II. Chemical Composition (in accordance with ASTM B348 standard)
| Element | Content range (%) |
| Titanium (Ti) | Margin |
| Oxygen (O) | ≤0.25 |
| Nitrogen (N) | ≤0.03 |
| Carbon (C) | ≤0.08 |
| Hydrogen (H) | ≤0.015 |
| Iron (Fe) | ≤0.30 |
| Other elements | 0.1-0.4 |
III. Physical Properties
IV. Mechanical Properties (ASTM B348)
| Performance indicators | Condition / State | Typical value (annealed state) | Organization |
| Tensile Strength | Annealed | ≥345 | MPa |
| Yield Strength, 0.2% | Annealed | ≥275 | MPa |
| Elongation | Annealed | ≥20 | % |
| Reduction of area | Annealed | ≥30 | % |
V. Typical Application Scenarios
| Core application fields |
| 1. Chemical Engineering and Marine Engineering |
| 2. Aerospace and Medical Devices |
| 3. Petrochemicals and Valve Components |
| 4. Shipbuilding and Automotive Industry |
| 5. Supports customization for high-demand scenarios such as aerospace, nuclear power, and chemical engineering. |
VI. Material Form and Standards/Specifications
| Form | Standard |
| Round rod | ASTM B348 |
| Seamless pipe | ASTM B337 |
| Plastic sheet | ASTM A265 |