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)

ElementContent 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

Density: 8.87 g/cm³

IV. Mechanical Properties (ASTM B574)

Performance indicatorsCondition / StateTypical valueOrganization
Tensile StrengthSolution Annealed≥690 MPa
Yield Strength, 0.2%Solution Annealed≥283 MPa
ElongationSolution 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

FormStandard
Round rodASTM A574
Seamless pipeASTM B622
Plastic sheetASTM 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)

ElementContent 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

Density: 8.69 g/cm³

IV. Mechanical Properties (ASTM B574)

Performance indicatorsCondition / StateTypical valueOrganization
Tensile strengthSolution Annealed≥690 MPa
Yield Strength, 0.2%Solution Annealed≥310 MPa
ElongationSolution 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

FormStandard
Round rodASTM A574
Seamless pipeASTM B622
Plastic sheetASTM 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)

ElementContent 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)+Tantalum8 x carbon-1.00

III. Physical Properties

Density: 8.0 g/cm³

IV. Mechanical Properties (Referencing Standard ASTM B473)

Performance indicatorsCondition / StateTypical valueOrganization
Tensile StrengthAnnealed≥551 MPa
Yield Strength, 0.2%Annealed≥241 MPa
ElongationAnnealed≥30 %
Reduction of areaAnnealed≥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

FormStandard
Round rodASTM A473
Seamless pipeASTM B729
Plastic sheetASTM 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)

ElementContent 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

Density: 9.2 g/cm³

IV. Mechanical Properties (Referencing Standard ASTM SB564)

Performance indicatorsTypical valueOrganization
Tensile StrengthSolution Annealed≥760 MPa
Yield Strength, 0.2%Solution Annealed≥350 Mpa
ElongationSolution 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

FormStandard
Round rodASTM SB564
Seamless pipeASTM B622
Plastic sheetASTM 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)

ElementContent 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+Mo94.0-98.0
Nb≤0.20
Ta≤0.20
Zr≤0.10

III. Physical Properties

Density: 9.3 g/cm³

IV. Mechanical Properties (ASTM SB564)

Performance indicatorsTypical valueOrganization / Company / Institution
Tensile StrengthSolution Annealed≥760 MPa
Yield Strength, 0.2%Solution Annealed≥350 Mpa
ElongationSolution 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

FormStandard
Round rodASTM SB564
Seamless pipeASTM B622
Plastic sheetASTM 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)

ElementContent 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

Density: 8.89 g/cm³

IV. Mechanical Properties (ASTM SB564)

Performance indicatorsCondition / StateTypical value (annealed state)Organization
Tensile StrengthAnnealed≥483 MPa
Yield Strength, 0.2%Annealed≥172 MPa
ElongationAnnealed≥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

FormStandard
Round rodASTM SB564
Seamless pipeASTM B165
Plastic sheetASTM 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)

ElementContent 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

Density: 8.44 g/cm³

IV. Mechanical Properties (in accordance with ASTM B865 standard)

FormConditionMaximum 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 forgings⁵Hot-worked and age-hardenedAll sizes140 (965)100 (690)20
RoundsCold-worked and age-hardenedover ¼ (6.4) to 1 (25.4), incl145 (1000)110 (760)15


over 1 (25.4) to 3 (76.2), incl140 (965)100 (690)17


over 3 (76.2) to 4 (101.6), incl135 (930)96 (655)20
HexagonsCold-worked and age-hardened¼ (6.4) to 2 (50.8), incl140 (965)100 (690)15
Rounds, hexagons, squares, rectangles, and forgingsAnnealed and age-hardened⁶Up to 1 (25.4)130 (895)90 (620)20


1 (25.4) and over130 (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

FormStandard
Round rodASTM 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)

ElementContent 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

Density: 8.44 g/cm³

IV. Mechanical Properties (ASTM B446)

Performance indicatorsCondition / StateTypical value (annealed state)Organization
Tensile strength (Tensile Strength)Annealing (Annealed)≥120 ksiOuter diameter ≤ 4 inches
Yield Strength (0.2%)Annealing (Annealed)≥60 ksiOuter diameter ≤ 4 inches
ElongationAnnealed≥30 %Outer diameter ≤ 4 inches
Tensile StrengthAnnealed≥110 ksiOuter diameter > 4 inches
Yield Strength, 0.2%Annealed≥50 ksiOuter diameter > 4 inches
ElongationAnnealed≥25 %Outer diameter > 4 inches
Tensile StrengthSolution Annealed≥100 ksiall sizes
Yield Strength, 0.2%Solution Annealed≥40 ksiall sizes
ElongationSolution 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

FormStandard
Round rodASTM B446
Seamless pipeASTM B444
Plastic sheetASTM 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)

ElementContent 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

Density: 8.2 g/cm³

IV. Mechanical Properties (ASTM B637)

Performance indicatorsCondition / StateTypical value (present tense)Organization
Tensile strength (Tensile Strength)Timely processing (solution+precipitation Harden)≥1275 MPa
Yield Strength, 0.2%solution+precipitation Harden≥1034 MPa
Elongationsolution+precipitation Harden≥12 %
Reduction of areasolution+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

FormStandard
Round rodASTM B637
Plastic sheetASTM 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)

ElementContent 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 elements0.1-0.4

III. Physical Properties

Density: 4.51 g/cm³

IV. Mechanical Properties (ASTM B348)

Performance indicatorsCondition / StateTypical value (annealed state)Organization
Tensile StrengthAnnealed≥345 MPa
Yield Strength, 0.2%Annealed≥275 MPa
ElongationAnnealed≥20 %
Reduction of areaAnnealed≥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 rodASTM B348
Seamless pipeASTM B337
Plastic sheetASTM A265
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