Inconel 601
General Description
Like Inconel 600, Inconel 601 has resistance to various forms of corrosion at high temperature and oxidization. However Inconel 601 has an addition of aluminum which give it high mechanical properties even in extremely hot environments.
Inconel 601 is used for industrial furnaces, radiant tubes, themocouple tubes, heat treatment equipments, baskets, petrochemical process equipments and aircraft components.
Chemical Composition
Specifications
Physical Properties
Mechanical Properties
Our Production Standard
Size Range
Inconel 601 wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Like Inconel 600, Inconel 601 has resistance to various forms of corrosion at high temperature and oxidization. However Inconel 601 has an addition of aluminum which give it high mechanical properties even in extremely hot environments.
Inconel 601 is used for industrial furnaces, radiant tubes, themocouple tubes, heat treatment equipments, baskets, petrochemical process equipments and aircraft components.
Chemical Composition
| Grade | Ni% | Mn% | Fe% | Si% | Cr% | C% | Cu% | Al% |
|---|---|---|---|---|---|---|---|---|
| Inconel 601 | 58-63 | Max 1.5 | Bal. | Max 0.50 | 21-25 | Max 0.10 | Max 1.00 | 1.0-1.7 |
| Grade | Werkstoff Nr. | UNS |
|---|---|---|
| Inconel 601 | 2.4851 | N06601 |
| Grade | Density | Melting Point |
|---|---|---|
| Inconel 601 | 8.1 g/cm3 | 1320°C-1411 °C |
| Alloy State | Tensile Strength | Yield Strength | Elongation | Brinell Hardness (HB) |
|---|---|---|---|---|
| Annealing Treatment | 650 N/mm² | 300 N/mm² | 30% | - |
| Solution Treatment | 600 N/mm² | 240 N/mm² | 30% | ≤220 |
| Bar | Forging | Pipe | Sheet/Strip | Wire | |
|---|---|---|---|---|---|
| Standard | ASTM B166 | ASTM B166 | ASTM B167/B751/B755 | AMS B168 | ASTM B166 |
Inconel 601 wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Inconel 718
General Description
Inconel 718 is a age-hardenable alloy that is highly corrosion resistant. Its high strength, corrosion resistance, and ease of weld fabrication have made alloy 718 the most popular superalloy used in industry.
Inconel 718 has good to excellent resistance to organic acids, alkalies and salts, and seawater. Fair resistance to sulfuric, hydrochloric, hydrofluoric, phosphoric, and nitric acids. Good to excellent resistance to oxidation, carburization, nitridation, and molten salts. Fair resistance to sulfidation.
Age-hardenable Inconel 718 combines high-temperature strength up to 700 °C (1300 °F) with corrosion resistance and excellent fabricability. Its welding characteristics, especially its resistance to postweld cracking, are outstanding. Because of these attributes, Inconel 718 is used for parts for aircraft turbine engines; high-speed airframe parts, such as wheels, buckets, and spacers; high-temperature bolts and fasteners, cryogenic tankage, and components for oil and gas extraction and nuclear engineering.
Chemical Composition
Specifications
Physical Properties
Mechanical Properties
Our Production Specification
Size Range
Inconel 718 wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Check here: Inconel 718 used in oil and gas service
Inconel 718 is a age-hardenable alloy that is highly corrosion resistant. Its high strength, corrosion resistance, and ease of weld fabrication have made alloy 718 the most popular superalloy used in industry.
Inconel 718 has good to excellent resistance to organic acids, alkalies and salts, and seawater. Fair resistance to sulfuric, hydrochloric, hydrofluoric, phosphoric, and nitric acids. Good to excellent resistance to oxidation, carburization, nitridation, and molten salts. Fair resistance to sulfidation.
Age-hardenable Inconel 718 combines high-temperature strength up to 700 °C (1300 °F) with corrosion resistance and excellent fabricability. Its welding characteristics, especially its resistance to postweld cracking, are outstanding. Because of these attributes, Inconel 718 is used for parts for aircraft turbine engines; high-speed airframe parts, such as wheels, buckets, and spacers; high-temperature bolts and fasteners, cryogenic tankage, and components for oil and gas extraction and nuclear engineering.
Chemical Composition
| Grade | Ni% | Cr% | Mo% | Nb% | Fe% | Al% | Ti% | C% | Mn% | Si% | Cu% | S% | P% | Co% |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Inconel 718 | 50-55 | 17-21 | 2.8-3.3 | 4.75-5.5 | Bal. | 0.2-0.8 | 0.7-0.15 | Max 0.08 | Max 0.35 | Max 0.35 | Max 0.3 | Max 0.01 | Max 0.015 | Max 1.0 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Inconel 718 | N07718 | 2.4668 |
| Grade | Density | Melting Point |
|---|---|---|
| Inconel 718 | 8.2g/cm3 | 1260°C-1340 °C |
| Inconel 718 | Tensile Strength | Yield Strength | Elongation | Brinell Hardness (HB) |
|---|---|---|---|---|
| Solution Treatment | 965 N/mm² | 550 N/mm² | 30% | ≤363 |
| Bar | Forging | Pipe/Tube | Sheet/Strip | Wire | |
|---|---|---|---|---|---|
| Standard | ASTM B637 AMS 5662 AMS 5664 |
ASTM B637 | AMS 5589/5590 | ASTM B670 | AMS 5832 |
Inconel 718 wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Check here: Inconel 718 used in oil and gas service
Inconel 718 NACE
General Description
Inconel 718 NACE has an adjusted composition which allows the material to have a different range of characteristics. Inconel 718 NACE has a tighter element content range in addition to adjusted annealing and aging temperatures which produces a product with lower mechanicals, larger grain and increase toughness. The tensile and yield are lower as well as the hardness which is lower than that of the AMS specification.
Physical Properties
Mechanical Properties
Size Range
Inconel 718 NACE Bar: Dia. 12mm-300mm
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Inconel 718 NACE has an adjusted composition which allows the material to have a different range of characteristics. Inconel 718 NACE has a tighter element content range in addition to adjusted annealing and aging temperatures which produces a product with lower mechanicals, larger grain and increase toughness. The tensile and yield are lower as well as the hardness which is lower than that of the AMS specification.
Inconel 718 NACE is commonly used in oil and gas industry for various applications. These severe environment wells have significant concentrations of H2S, CO2, chlorides and high bottom hole temperatures. The largest use is for downhole tools such as subsurface safety valves, packers, flow control devices and other tools. These alloys are also used for wellhead components and valve bodies.
Chemical Composition| Grade | Ni% | Cr% | Nb+Ta% | Mo% | Ti% | Al% | C% | Co% | Mn% | Si% |
|---|---|---|---|---|---|---|---|---|---|---|
Inconel 718 NACE
|
50-55 | 17-21 | 4.87-5.2 | 2.8-3.3 | 0.8-1.15 | 0.4-0.6 | Max 0.045 | Max 1.0 | Max 0.35 | Max 0.35 |
| P% | S% | B% | Cu% | Pb% | Se% | Bi% | Ca% | Mg% | Fe% | |
| Max 0.01 | Max 0.01 | Max 0.006 | Max 0.23 | Max 0.001 | Max 0.0005 | Max 0.00005 | Max 0.003 | Max 0.006 | Bal. |
Double vacuum melted Inconel 718 is specified to keep the residual elements, carbides, nitrides and oxides at low levels. Specifying low levels of these residual elements allowed control of the microstructure and phase morphologies. Specifically, carbon was specified to .045% max, and P, S, Pb, Se, and Bi were specified to ppb levels. Ti, Al and Nb levels were tightly controlled as well.
Specifications| Grade | NACE | API |
|---|---|---|
| Inconel 718 NACE | MR0175 MR0103 | 6A718 |
| Grade | Density | Melting Point |
|---|---|---|
| Inconel 718 NACE | 8.2g/cm3 | 1180°C-1340 °C |
| Inconel 718 NACE | Tensile Strength | 0.2% Yield Strength | Elongation | Hardness |
|---|---|---|---|---|
| Solution&Aging Treatment | 1034 N/mm² | 827 N/mm² | 20% | <40 HRC |
Inconel 718 NACE Bar: Dia. 12mm-300mm
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Inconel X750
General Description
Inconel X750 is a nickel-chromium alloy similar to Inconel 600 but made precipitation-hardenable by additions of aluminum and titanium. It has good resistance to corrosion and oxidation along with high tensile and creep-rupture properties at temperatures to 1300°F (700°C).
Its excellent relaxation resistance is useful for high-temperature springs and bolts. Used in gas turbines, rocket engines, nuclear reactors, pressure vessels, tooling, and aircraft structures.
Chemical Composition
Specifications
Physical Properties
Mechanical Properties
Our Production Standard
Size Range
Inconel X750 is available as wire, strip, sheet, rod and bar. In the wire form, this grade is covered by specification AMS 5698 for No.1 Temper and AMS 5699 for spring temper grade. No.1 Temper has a higher service temperature than Spring temper, but lower tensile strength.
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Inconel X750 is a nickel-chromium alloy similar to Inconel 600 but made precipitation-hardenable by additions of aluminum and titanium. It has good resistance to corrosion and oxidation along with high tensile and creep-rupture properties at temperatures to 1300°F (700°C).
Its excellent relaxation resistance is useful for high-temperature springs and bolts. Used in gas turbines, rocket engines, nuclear reactors, pressure vessels, tooling, and aircraft structures.
Chemical Composition
| Grade | Ni% | Cr% | Nb% | Fe% | Al% | Ti% | C% | Mn% | Si% | Cu% | S% | Co% |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Inconel X750 | Max 70 | 14-17 | 0.7-1.2 | 5.0-9.0 | 0.4-1.0 | 2.25-2.75 | Max 0.08 | Max 1.00 | Max 0.50 | Max 0.5 | Max 0.01 | Max 1.0 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Inconel X750 | N07750 | 2.4669 |
| Grade | Density | Melting Point |
|---|---|---|
| Inconel X750 | 8.28 g/cm3 | 1390°C-1420 °C |
| Inconel X750 | Tensile Strength | Yield Strength | Elongation | Brinell Hardness (HB) |
|---|---|---|---|---|
| Solution Treatment | 1267 N/mm² | 868 N/mm² | 25% | ≤400 |
| Bar | Forging | Pipe | Sheet/Strip | Wire | |
|---|---|---|---|---|---|
| Standard | ASTM B637 | ASTM B637 | AMS 5582 | AMS 5542 AMS 5598 |
AMS 5698 AMS 5699 |
Inconel X750 is available as wire, strip, sheet, rod and bar. In the wire form, this grade is covered by specification AMS 5698 for No.1 Temper and AMS 5699 for spring temper grade. No.1 Temper has a higher service temperature than Spring temper, but lower tensile strength.
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Nimonic 75
General Description
Nimonic 75 (UNS N06075/2.4951) is a creep-resistant nickel chromium 80/20 alloy with controlled additions of titanium and carbon. Under 800℃, Nimonic 75 has excellet resistance to oxidising atmospheres, used in gas turbine engineering and also for industrial thermal processing, furnace components and heat-treatment equipments.
Chemical Composition
Specifications
Physical Properties
Thermal Conduction
Coefficient of Linear Expansion
Size Range
Nimonic 75 Wire: ￠0.1mm-￠9mm
Nimonic 75 Bar: ￠11mm-￠200mm
Nimonic 75 Strip: 75-110mm*0.15-22mm
Seamless and welded tubes also availabla per request.
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Nimonic 75 (UNS N06075/2.4951) is a creep-resistant nickel chromium 80/20 alloy with controlled additions of titanium and carbon. Under 800℃, Nimonic 75 has excellet resistance to oxidising atmospheres, used in gas turbine engineering and also for industrial thermal processing, furnace components and heat-treatment equipments.
Chemical Composition
| Grade | Ni% | Cr% | Fe% | P% | Cu% | Al% | Ti% | C% | Mn% | Si% | S% |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Nimonic 75 | Bal. | 19-22 | Max 1.0 | Max 0.015 | Max 0.2 | Max 0.15 | 0.15-0.35 | Max 0.12 | Max 0.70 | Max 0.80 | Max 0.02 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Nimonic 75 | N06075 | 2.4951 |
| Grade | Density | Melting Point |
|---|---|---|
| Nimonic 75 | 8.4 g/cm3 | 1374°C-1420 °C |
| θ/℃ | 100 | 200 | 300 | 400 | 500 | 600 | 700 | 800 | 900 |
|---|---|---|---|---|---|---|---|---|---|
| λ/(W/(m·C)) | 15.1 | 16.3 | 18.0 | 19.3 | 20.9 | 22.2 | 23.4 | 25.1 | 26.4 |
| θ/℃ | 20-100 | 20-200 | 20-300 | 20-400 | 20-500 | 20-600 | 20-700 | 20-800 | 20-900 |
|---|---|---|---|---|---|---|---|---|---|
| α/10-6C-1 | 12.8 | 13.5 | 18.0 | 19.3 | 20.9 | 22.2 | 23.4 | 25.1 | 26.4 |
Nimonic 75 Wire: ￠0.1mm-￠9mm
Nimonic 75 Bar: ￠11mm-￠200mm
Nimonic 75 Strip: 75-110mm*0.15-22mm
Seamless and welded tubes also availabla per request.
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Nimonic 80A
General Description
Nimonic 80A (UNS N07080/W. Nr. 2.4952) is a nickel chromium alloy similar to Alloy 75 but made precipitation hardenable by additions of aluminium and titanium. Alloy 80a has good corrosion and oxidation resistance and high tensile and creep rupture properties at temperatures up to 1500 deg F.
Chemical Composition
Specifications
Physical Properties
Mechanical Properties
Our Production Standard
Size Range
Nimonic 80A Wire: ￠0.1mm-￠9mm
Nimonic 80A Bar: ￠11mm-￠200mm
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Nimonic 80A (UNS N07080/W. Nr. 2.4952) is a nickel chromium alloy similar to Alloy 75 but made precipitation hardenable by additions of aluminium and titanium. Alloy 80a has good corrosion and oxidation resistance and high tensile and creep rupture properties at temperatures up to 1500 deg F.
Chemical Composition
| Grade | Ni% | Cr% | Fe% | Mn% | Si% | P% | S% | Al% | Ti% | C% | Co% | B% | Zr% | Cu% |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Nimonic 80A | Bal. | 18-21 | Max 3.0 | Max 1.0 | Max 1.0 | Max 0.02 | Max 0.015 | 1.0-1.8 | 1.8-2.7 | Max 0.1 | Max 2.0 | Max 0.008 | Max 0.15 | Max 0.2 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Nimonic 80A | N07080 | 2.4952 |
| Grade | Density | Melting Point |
|---|---|---|
| Nimonic 80A | 8.19g/cm3 | 1320°C-1365 °C |
| Nimonic 80A | Tensile Strength | Yield Strength σp0.2/MPa | Elongation σ5 /% |
Hardness |
|---|---|---|---|---|
| Heat Treatment (Min) | 930 N/mm² | 620 N/mm² | 20% | 300 HV |
| Nimonic 80A | Bar/Wire | Forging Parts |
|---|---|---|
| ASTM | ASTM B637 | ASTM B637 |
Nimonic 80A Wire: ￠0.1mm-￠9mm
Nimonic 80A Bar: ￠11mm-￠200mm
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Nimonic 90
General Description
Specifications
Physical Properties
Mechanical Properties (20°C Min )
Size Range
Nimonic 90 Wire: ￠0.1mm-￠9mm
Nimonic 90 Bar: ￠11mm-￠200mm
Strip&Sheet also available per request.
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Nimonic 90 (UNS N07090/W. Nr. 2.4632) is a precipitation hardenable nickel-chromium-cobalt alloy strengthened by the addition of titanium and aluminium. Nimonic 90 has a high stress rupture strength and creep-resistant at temperatures to about 920°C. Nimonic 90 is better suited for extremely high temperatures than Inconel X 750 (or Inconel 718).
Chemical Composition| Grade | Ni% | Cr% | Co% | C% | Si% | Cu% | Fe% | Mn% | Ti% | Al% | B% | S% | Zr% |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Nimonic 90 | Rem. | 18-21 | 15-21 | Max 0.13 | Max 1.0 | Max 0.2 | Max 1.5 | Max 1.0 | 2.0-3.0 | 1.0-2.0 | Max 0.02 | Max 0.015 | Max 0.15 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Nimonic 90 | N07090 | 2.4632 |
| Grade | Density | Melting Point | Thermal Conductio | Linear Expansibility |
|---|---|---|---|---|
| Nimonic 90 | 8.2 g/cm3 | 1400 °C | 21.76(100℃) λ/(W/m•℃) | 12.7(20~100℃) a/10-6℃-1 |
| Condition | Tensile Strength | Yield Strength σp0.2/MPa |
|---|---|---|
| Solution Treatment | 820 Mpa | 590 Mpa |
Nimonic 90 Wire: ￠0.1mm-￠9mm
Nimonic 90 Bar: ￠11mm-￠200mm
Strip&Sheet also available per request.
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Incoloy 800
General Description
Incoloy 800 is a nickel-iron-chromium alloy with good strength and excellent resistance to oxidation and carburization in high-temperature atmospheres.
A high chromium content gives Incoloy 800 good resistance to oxidation. It also resists many aqueous media and is relatively free from stress-corrosion cracking. Incoloy 800 has excellent resistance to nitric acid at concentrations up to approximately 70% and at temperatures up to the boiling point. It also has good resistance to organic acids, such as formic, acetic, and propionic. It resists a variety of oxidizing and nonoxidizing salts, but not halide salts.
Typical applications are heat treating equipment, petrochemical pyrolysis tubing and piping systems, sheathing for electrical heating elements, food processing equipment.
Chemical Composition
Specifications
Physical Properties
Mechanical Properties
Welding of Incoloy 800
Any traditional welding procedures can be used to weld Incoloy 800 to similar alloys or other metals, such as gas tungsten arc welding(GTAW), plasma arc welding (PAW), metal inertia gas welding (MIG) and so on. Before welding, remove scale, grease, mark and imprint.
Recommend filler wire regarding welding Incoloy 800: ERNiCrMo-3
Size Range
Incoloy 800 wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Incoloy 800 is a nickel-iron-chromium alloy with good strength and excellent resistance to oxidation and carburization in high-temperature atmospheres.
A high chromium content gives Incoloy 800 good resistance to oxidation. It also resists many aqueous media and is relatively free from stress-corrosion cracking. Incoloy 800 has excellent resistance to nitric acid at concentrations up to approximately 70% and at temperatures up to the boiling point. It also has good resistance to organic acids, such as formic, acetic, and propionic. It resists a variety of oxidizing and nonoxidizing salts, but not halide salts.
Typical applications are heat treating equipment, petrochemical pyrolysis tubing and piping systems, sheathing for electrical heating elements, food processing equipment.
Chemical Composition
| Grade | Ni% | Cr% | Fe% | C% | Mn% | S% | Si% | Cu% | Al% | Ti% |
|---|---|---|---|---|---|---|---|---|---|---|
| Incoloy 800 | 30.0-35.0 | 19.0-23.0 | Min 39.5 | Max 0.10 | Max 1.50 | Max 0.015 | Max 1.0 | Max 0.75 | 0.15-0.60 | 0.15-0.60 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Incoloy 800 | N08800 | 1.4876 |
| Grade | Density | Melting Point |
|---|---|---|
| Incoloy 800 | 8.0 g/cm3 | 1350°C-1400 °C |
| Grade | Tensile Strength | Yield Strength | Elongation |
|---|---|---|---|
| Incoloy 800 | 520 N/mm² | 205 N/mm² | 30% |
Any traditional welding procedures can be used to weld Incoloy 800 to similar alloys or other metals, such as gas tungsten arc welding(GTAW), plasma arc welding (PAW), metal inertia gas welding (MIG) and so on. Before welding, remove scale, grease, mark and imprint.
Recommend filler wire regarding welding Incoloy 800: ERNiCrMo-3
Size Range
Incoloy 800 wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Incoloy 800H/HT
General Description
Incoloy 800H is similar to alloy 800 but with improved creep and stress-rupture properties for applications above 650 °C (1200 °F). Resistant to high-temperature oxidation, carburization, and nitridation, it is widely used in petrochemical and thermal processing.
Incoloy 800HT is similar to alloy 800H but with even more precisely controlled composition.
Alloys 800H and 800HT are the standard materials for intermediate temperatures (620–925 °C, or 1150–1700 °F). These alloys combine corrosion resistance with strength and metallurgical stability. Major applications include hydrogen reformer manifolds and pigtail piping, ethylene dichloride furnace tubing, transfer piping, and high-temperature pressure vessels.
Chemical Composition
Specifications
Physical Properties
Mechanical Properties
Our Production Standard
Size Range
Incoloy 800H and Incoloy 800HT wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Incoloy 800H is similar to alloy 800 but with improved creep and stress-rupture properties for applications above 650 °C (1200 °F). Resistant to high-temperature oxidation, carburization, and nitridation, it is widely used in petrochemical and thermal processing.
Incoloy 800HT is similar to alloy 800H but with even more precisely controlled composition.
Alloys 800H and 800HT are the standard materials for intermediate temperatures (620–925 °C, or 1150–1700 °F). These alloys combine corrosion resistance with strength and metallurgical stability. Major applications include hydrogen reformer manifolds and pigtail piping, ethylene dichloride furnace tubing, transfer piping, and high-temperature pressure vessels.
Chemical Composition
| Grade | Ni% | Cr% | Fe% | C% | Mn% | Si% | Cu% | S% | AL% | Ti% | Al+Ti% |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Incoloy 800H | 30.5-35.0 | 19.0-23.0 | Bal. | 0.05-0.10 | Max 1.5 | Max 1.0 | Max 0.75 | Max 0.015 | 0.15-0.60 | 0.15-0.60 | 0.30-1.20 |
| Incoloy 800HT | 30.0-35.0 | 19.0-23.0 | Bal. | 0.06-0.10 | Max 1.5 | Max 1.0 | Max 0.75 | Max 0.015 | 0.25-0.60 | 0.25-0.60 | 0.85-1.20 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Incoloy 800H | N08810 | 1.4958 |
| Incoloy 800HT | N08811 | 1.4959 |
| Grade | Density | Melting Point |
|---|---|---|
| Incoloy 800H/800HT | 8.0 g/cm3 | 1370°C-1400 °C |
| Alloy | Tensile Strength | Yield Strength | Elongation |
|---|---|---|---|
| Incoloy 800H/800HT | 450 N/mm² | 170 N/mm² | 35% |
| Bar | Forging | Sheet/Strip | Wire | |
|---|---|---|---|---|
| Standard | ASTM B408 | ASTM B564 | ASTM B409 |
Incoloy 800H and Incoloy 800HT wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Incoloy A286
General Description
Incoloy A286 is a Fe-25Ni-15Cr based high temperature alloy, adding titanium, molybdenum, aluminum, boron and vanadium. It is precipitation hardenable for high mechanical properties. The alloy maintains good strength and oxidation resistance at temperatures up to about 1300°F (700°C). The alloy’s high strength and excellent fabrication characteristics make it useful for various components of aircraft and industrial gas turbines.
Applications include blades, vanes, shafts, tail cones, afterburners, springs, and fasteners.
Chemical Composition
Specifications
Physical Properties
Thermal Conduction
Coefficient of Linear Expansion
Our Production Standard
Size Range
Incoloy A286 Wire: ￠0.1mm-￠9mm
Incoloy A286 Bar: ￠11mm-￠200mm
Incoloy A286 Strip: 75-110mm*0.15-22mm
Incoloy A286 screws, bolts are also available per request.
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Incoloy A286 is a Fe-25Ni-15Cr based high temperature alloy, adding titanium, molybdenum, aluminum, boron and vanadium. It is precipitation hardenable for high mechanical properties. The alloy maintains good strength and oxidation resistance at temperatures up to about 1300°F (700°C). The alloy’s high strength and excellent fabrication characteristics make it useful for various components of aircraft and industrial gas turbines.
Applications include blades, vanes, shafts, tail cones, afterburners, springs, and fasteners.
Chemical Composition
| Grade | C% | Cr% | Ni% | Mo% | Ti% | Fe% | V% | B% | Mn% | Al% | P% | S% | Si% |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Incoloy A286 | Max 0.08 | 13.5-16.0 | 24.0-27.0 | 1.00-1.50 | 1.75-2.30 | Bal. | 0.10-0.50 | 0.001-0.010 | 1.00-2.00 | Max 0.40 | Max 0.030 | Max 0.020 | Max 1.00 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Incoloy A286 | S66286 | 1.4980 |
| Grade | Density | Melting Point |
|---|---|---|
| Incoloy A286 | 7.95 g/cm3 | 1370°C-1420 °C |
| θ/℃ | 100 | 200 | 300 | 400 | 500 | 600 | 700 | 800 | 900 |
|---|---|---|---|---|---|---|---|---|---|
| λ/(W/(m·C)) | 14.2 | 15.9 | 17.2 | 18.8 | 20.5 | 22.2 | 23.9 | 25.5 | 27.6 |
| θ/℃ | 20-100 | 20-200 | 20-300 | 20-400 | 20-500 | 20-600 | 20-700 | 20-800 | 20-900 |
|---|---|---|---|---|---|---|---|---|---|
| α/10-6C-1 | 15.37 | 16.09 | 16.31 | 16.84 | 17.58 | 18.06 | 18.74 | 19.62 | 20.45 |
| Bar | Forging Parts | Sheet/Strip | Wire | |
|---|---|---|---|---|
| Standard | ASTM A638 | ASTM B564 | ASTM B670 |
Incoloy A286 Wire: ￠0.1mm-￠9mm
Incoloy A286 Bar: ￠11mm-￠200mm
Incoloy A286 Strip: 75-110mm*0.15-22mm
Incoloy A286 screws, bolts are also available per request.
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Hastelloy X
General Description
Hastelloy X is a nickel-chromium-iron-molybdenum alloy containing approximately 22% chromium for outstanding resistance to oxidation at high temperatures up to 1200°C.
Hastelloy X has good high temperature and stress rupture properties above 790°C (1450°F) and can be used for applications up to 1200°C (2200°F). With the high levels of chromium, nickel and molybdenum in the material, Hastelloy X exhibits levels of corrosion resistance similar to high nickel alloys more customarily used in corrosion applications.
Hastelloy X can be used in many industrial furnace applications because of its resistance to oxidizing, neutral and carburizing atmospheres; widely used for aircraft parts, such as jet engine tailpipes, afterburners, turbine blades, and vanes.
Chemical Composition
Specifications
Physical Properties
Mechanical Properties
Our Production Standard
Size Range
Hastelloy X wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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Hastelloy X is a nickel-chromium-iron-molybdenum alloy containing approximately 22% chromium for outstanding resistance to oxidation at high temperatures up to 1200°C.
Hastelloy X has good high temperature and stress rupture properties above 790°C (1450°F) and can be used for applications up to 1200°C (2200°F). With the high levels of chromium, nickel and molybdenum in the material, Hastelloy X exhibits levels of corrosion resistance similar to high nickel alloys more customarily used in corrosion applications.
Hastelloy X can be used in many industrial furnace applications because of its resistance to oxidizing, neutral and carburizing atmospheres; widely used for aircraft parts, such as jet engine tailpipes, afterburners, turbine blades, and vanes.
Chemical Composition
| Grade | Ni% | Cr% | Fe% | Mo% | C% | Mn% | Si% | Co% | Al% | W% | B% | S% | P% |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Hastelloy X | Bal. | 20.5-23.5 | 17.0-20.0 | 8.0-10.0 | 0.05-0.15 | Max 1.0 | Max 1.0 | 0.5-2.5 | Max 0.1 | 0.2-1.0 | Max 0.005 | Max 0.01 | Max 0.015 |
| Grade | UNS | Werkstoff Nr. |
|---|---|---|
| Hastelloy X | N06002 | 2.4665 |
| Grade | Density | Melting Point |
|---|---|---|
| Hastelloy X | 8.3g/cm3 | 1260°C-1355°C |
| Solution Treatment | Size (mm) | Tensile Strength | Yield Strength 0.2% | Elongation |
|---|---|---|---|---|
| Strip | T<4.75 | 725 N/mm² | 310 N/mm² | 30% |
| Sheet | T>4.75 | 690 N/mm² | 275 N/mm² | - |
| Bar | ø<100 | 660 N/mm² | 240 N/mm² | - |
| Bar | Forging Parts | Welded Tube | Seamless Tube | Sheet/Strip | Wire | |
|---|---|---|---|---|---|---|
| Standard | ASTM B572 | AMS 5754 | ASTM B619/B626 | ASTM B622 | ASTM B435 | AMS 5798 |
Hastelloy X wire, bar, rod, strip, forging, plate, sheet, tube, fastener and other standard forms are available.
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