Kanakratna Steelage Private Limited
KHETWADI, Mumbai, Maharashtra
GST No. 27AAECK9442R1ZP
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- Incoloy Alloy A 286
Incoloy® alloy A-286 (UNS S66286) is an iron-nickel-chromium alloy with additions of molybdenum and titanium. It is age hardenable for high mechanical properties. The alloy maintains good strength and oxidation resistance at temperatures up to about 1300°F (700°C). The limiting chemical composition is given in Table 1. The alloy is austenitic in all metallurgical conditions. The high strength and excellent fabrication characteristics of Incoloy alloy A-286 make the alloy useful for various components of aircraft and industrial gas turbines. It is also used for fastener applications in automotive engine and manifold components subject to high levels of heat and stress and in the offshore oil and gas industry.
In the age-hardened condition, Incoloy alloy A-286 has high strength at room temperature and retains high levels of strength at temperatures to about 1300°F (700°C). Incoloy alloy A-286 has good creep-rupture strength during extended high-temperature exposure. . Stress levels to produce creep rates of 1%/100 h and 1%/1000 h are shown in Figure 3. Mechanical properties reported here are for material given the following heat treatment: solution treatment at 1800°F (980°C) plus age hardening at 1325°F (720°C)/16 h and air cooling.
Corrosion Resistance The nickel and chromium contents of Incoloy alloy A-286 provide resistance to corrosion and oxidation. The alloy has excellent resistance to oxidation at service temperatures up to about 1300°F.
Fabrication Incoloy alloy A-286 is readily fabricated by standard procedures for stainless steels and nickel alloys. Cold forming should be done on material in the solution-treated condition. Procedures, forces, and work hardening rates are similar to those for Inconel alloy 600 and Incoloy alloy 800. For hot forming, the metal should be heated to 2100°F (1150°C). Any final reductions at under 1800°F (980°C) should be greater than 10% to avoid formation of large grains during later solution treatment. No forming should be done below 1700°F (930°C). Heat treatment of Incoloy alloy A-286 consists of solution treatment at either 1800°F (980°C) or 1650°F (900°C) and rapid cooling followed by age hardening at 1325°F (720°C) for 16 hours and air cooling.
| Minimum Order Quantity | 10 kgs |
| Shape | Round |
| Steel Grade | Inconel |
| Nominal Size | 3/4 inch, 1 inch, 1/2 inch |
| Material Grade | Inconel 286 |
| Material | Alloy 660A |
| Usage/Application | Chemical Handling |
| Size/Diameter | >4 inch |
| Length | 3m, 6m |
| Technique | ERW |
Alloy A 286 Pipe & Tubes offered come in precision constructed finish and find use in different industry sectors.
Features:
| Size | Standrad |
| Usage | Manufacturing |
| Single Piece Length | 3 meter |
| Material | Steel |
Inconel 286 (660A) is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 925 composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This super alloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
Characteristics of Inconel 660A
Good mechanical properties – tensile, fatigue and creep-rupture
Yield tensile strength, creep, and rupture strength properties are exceedingly high
Highly resistant to chloride and sulfide stress corrosion cracking
Resistant to aqueous corrosion and chloride ion stress corrosion cracking
High temperature resistant
Age-hardenable with a unique property of slow aging response that permits heating and cooling during annealing without the danger of cracking.
Excellent welding characteristics, resistant to postweld age cracking
Chemical Composition, %
Ni | Fe | Cr | Cu | Mo | Nb | C | Mn |
|---|---|---|---|---|---|---|---|
50.00-55.00 | Remainder | 17.00-21.00 | .30 max | 2.80-3.30 | 4.75-5.50 | .08 max | .35 max |
Applications
Chemical processing
Aerospace
Liquid fuel rocket motor components
Pollution-control equipment
Nuclear reactors
Cryogenic storage tanks
Valves, fasteners, springs, mandrels, tubing hangers
Well head completion equipment and blow out presenters (BOP’s)
Gas turbine engine parts
| Color | Silver |
| Size | Customized |
| Application | Industrial |
| Material | Steel |
Inconel 660A is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 660A composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This super alloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
characteristics of Inconel 660A
Good mechanical properties – tensile, fatigue and creep-rupture
Yield tensile strength, creep, and rupture strength properties are exceedingly high
Highly resistant to chloride and sulfide stress corrosion cracking
Resistant to aqueous corrosion and chloride ion stress corrosion cracking
High temperature resistant
Age-hardenable with a unique property of slow aging response that permits heating and cooling during annealing without the danger of cracking.
Excellent welding characteristics, resistant to postweld age cracking
Chemical Composition, %
Ni | Fe | Cr | Cu | Mo | Nb | C | Mn |
|---|---|---|---|---|---|---|---|
50.00-55.00 | Remainder | 17.00-21.00 | .30 max | 2.80-3.30 | 4.75-5.50 | .08 max | .35 max |
Applications
Chemical processing
Aerospace
Liquid fuel rocket motor components
Pollution-control equipment
Nuclear reactors
Cryogenic storage tanks
Valves, fasteners, springs, mandrels, tubing hangers
Well head completion equipment and blow out preventers (BOP’s)
Gas turbine engine parts
ASTM Specifications
Sheet/Plate--
B670
*Your information is safe with us.
| Minimum Order Quantity | 10 Kilogram |
| Usage | Manufacturing, Construction |
We are a leading Exporter & Supplier of Inconel 660 Rod such as Alloy A 286 Bolt, Alloy A 286 Fasteners, Inconel 660 Alloy A 286 Bolt, Alloy A286 Round Bar, Inconel Rods, Inconel 660 Fasteners .
A-286 alloy is an age-hardenable iron base superalloy for applications requiring high strength from -320°F up to 1000°F long time, 1300-1500°F short time. Oxidation resistance is high for continuous service to 1500°F, intermittent to 1800°F. Aqueous corrosion resistance is comparable to 316/316L stainless. Heat treatment according to AMS 5525 requires a solution anneal at 1800°F, air cool. Age at 1325°F for 16 hours and then air cool.
| Cr | Ni | Mo | Co | Va | Al | Ti | B | C | Fe | Mn | Si | Ph | S | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MIN | 13.5 | 24.0 | 1.0 | - | 0.1 | - | 1.9 | 0.003 | - | - | - | - | - | - |
| MAX | 16.0 | 27.0 | 1.5 | 1.0 | 0.5 | 0.35 | 2.35 | 0.01 | 0.08 | Balance | 2.0 | 1.0 | 0.025 | 0.025 |
| Length | Standard |
| Color | Silver |
| Application | Industrial |
| Material | Steel |
Inconel 660A is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 660A composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This super alloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
characteristics of Inconel 660A
Good mechanical properties – tensile, fatigue and creep-rupture
Yield tensile strength, creep, and rupture strength properties are exceedingly high
Highly resistant to chloride and sulfide stress corrosion cracking
Resistant to aqueous corrosion and chloride ion stress corrosion cracking
High temperature resistant
Age-hardenable with a unique property of slow aging response that permits heating and cooling during annealing without the danger of cracking.
Excellent welding characteristics, resistant to postweld age cracking
Chemical Composition, %
Ni | Fe | Cr | Cu | Mo | Nb | C | Mn |
|---|---|---|---|---|---|---|---|
50.00-55.00 | Remainder | 17.00-21.00 | .30 max | 2.80-3.30 | 4.75-5.50 | .08 max | .35 max |
Applications
Chemical processing
Aerospace
Liquid fuel rocket motor components
Pollution-control equipment
Nuclear reactors
Cryogenic storage tanks
Valves, fasteners, springs, mandrels, tubing hangers
Well head completion equipment and blow out preventers (BOP’s)
Gas turbine engine parts
| Brand | Kanakranta Steelage |
An alloy that 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. This alloy is also used for automotive applications.
*Your information is safe with us.
| Application | Gas Pipe, Structure Pipe |
| Size | 1/2 inch, 3/4 inch, 1 inch |
| Thread Size | Standard |
Inconel 660Ais a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 660A composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This super alloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
characteristics of Inconel 660A
Good mechanical properties – tensile, fatigue and creep-rupture
Yield tensile strength, creep, and rupture strength properties are exceedingly high
Highly resistant to chloride and sulfide stress corrosion cracking
Resistant to aqueous corrosion and chloride ion stress corrosion cracking
High temperature resistant
Age-hardenable with a unique property of slow aging response that permits heating and cooling during annealing without the danger of cracking.
Excellent welding characteristics, resistant to postweld age cracking
Chemical Composition, %
Ni | Fe | Cr | Cu | Mo | Nb | C | Mn |
|---|---|---|---|---|---|---|---|
50.00-55.00 | Remainder | 17.00-21.00 | .30 max | 2.80-3.30 | 4.75-5.50 | .08 max | .35 max |
Applications
Chemical processing
Aerospace
Liquid fuel rocket motor components
Pollution-control equipment
Nuclear reactors
Cryogenic storage tanks
Valves, fasteners, springs, mandrels, tubing hangers
Well head completion equipment and blow out preventers (BOP’s)
Gas turbine engine parts
| Size | Standard |
| Design | Standard |
| Brand | Alloy |