Inconel
INCONEL ALLOYS
We supply a variety of Inconel sheets, Inconel plates, Inconel bars and Inconel round bars, Inconel tubing and Inconel pipes in various sizes. They include Inconel 600 Round Bar, Inconel 625 Round Bar, Incoloy 800 Round Bar, among others. Inconel material is also referred to as nickel alloy plate, sheets, bars, round, tubing and pipes. We are a certified distributor of high temperature pipes & high temperature alloy pipes, high temperature alloy plates, high temperature alloy sheets, and high temperature alloy tubing. They have superior mechanical properties along with good workability and high strength. These products are offered in various specifications.
Inconel 718 - Sheet, Plate, Bar, Forged Bar
UNS N07718, AMS 5662, AMS 5596, AMS 5589
* All Trademarks and/or Trade names are the properties of their respective owners.
Inconel 718 Specifications: AMS 5662, AMS 5596, AMS 5589
UNS N07718 Werkstoff Nr 2.4668, AMS 5596 Sheet, Strip and Plate, AMS 5597 Sheet, Strip and Plate, AMS 5589 Seamless Tube, AMS 5590 Seamless Tube, AMS 5662 Bars, Forgings and Rings, AMS 5663 Bars, Forgings and Rings, AMS 5664 Bars, Forgings and Rings, AMS 5832 Welding Wire, ASTM B637 Forgings, ASTM B670 Plate, Sheet and Strip, AFNOR NC 19 Fe Nb , MSRR 7115 and MSRR 7116
Inconel 718 Available Forms: 718 Alloy Sheet, 718 Alloy Plate, 718 Alloy Bar, 718 Alloy Forged Bar
Inconel 718 Applications: Inconel 718 has been used for jet engine and high-speed airframe parts such as wheels, buckets, spacers, and high temperature bolts and fasteners.
Description
Inconel 718 is a precipitation hardenable nickel-based alloy designed to display exceptionally high yield, tensile and creep-rupture properties at temperatures up to 1300 Degrees F. The sluggish age-hardening response of Inconel 718 permits annealing and welding without spontaneous hardening during heating and cooling. Inconel 718 has excellent weldability when compared to the nickel-base superalloys hardened by aluminum and titanium.
Composition
Alloy 718 is made up primarily of nickel (52%). Alloying elements include Iron (19%), Chromium (18%), Columbium+ Tantalum (5%), Molybdenum (3%), Titanium (0.9%), Aluminum (0.5%) with the addition of other elements in trace amounts such as Baron, Cobalt, Copper, Manganese and Silicon.
Physical Properties
718 features a melting point of 2300°c and possesses impressive tensile strength that lends itself well to the wide variety of industrial applications. The alloy has excellent performance in properties such as weldability and creep-rupture.
Heat Treatment
Heat treatment schedules for wrought Inconel 718 are based primarily on considerations of solution and re-precipitation reactions of the gamma-prime and gamma-double-prime phases for strengthening and of delta phase for grain size control. The heat treatments generally involve a high temperature anneal for solutioning of these second phases followed by one or two lower temperature aging treatments to re-precipitate the strengthening phases in the desired distributions.Some strengthening precipitate generally forms on cooling from the solution annealing temperature. The first aging treatment coarsens this precipitate as well as forming additional precipitate. The second lower temperature aging treatment promotes additional fine precipitate for improved tensile strength and creep rupture life.
Standard heat treatment for most specifications includes a solution heat treatment in the range of 1750F to 1800F, followed by a duplex precipitation heat treatment of 1325F/8 hours with a ~100F/hour cool down to 1150F, and holding an additional 8 hours at 1150F, for a total precipitation heat treat time of 18 hours, then AC. A second heat treat procedure involves slightly higher solutioning and aging temperatures. It is used for optimum ductility and low temperature toughness in heavy sections, although it can also produce notch brittleness in creep rupture and is not recommended for applications operating above 1000F. This heat treatment involves solution annealing above the delta solvus temperature, as follows: Solution heat treat at 1950F, one-half to one hour, AC or faster; duplex precipitation heat treat at 1400F.
Corrosion Resistance
Inconel 718 possesses excellent corrosion and oxidation resistance. It also has good sea water corrosion resistance and it is attractive for marine applications.
Royal Emperor Metals & Supply is a leading supplier of quality Inconel 718 Sheet, Inconel 718 Plate, Inconel 718 Bar, Inconel 718 Forged Bar.
All of our Inconel 718 is ordered to specific thickness. We supply Inconel 718 and are capable of fulfilling your required lengths and widths. Royal Emperor Metals & Supply Inc. also has a stocking program to support long term contract for your Inconel 718 needs.
Inconel 600 - Sheet, Plate, Bar, Forged Bar
UNS N06600, AMS 5540, AMS 5580, AMS 5665
* All Trademarks and/or Trade names are the properties of their respective owners.
Inconel 600 Specifications: AMS 5540, AMS 5580, AMS 5665
Inconel Alloy 600, Alloy 600, UNS N06600, Ni 72.0, Cr 15.5, Fe 8.0 Mn 1.0 C 0.15 Cu 0.5 Si 0.5 S 0.015, Werkstoff 2.4816, EN 2.4816
Inconel 600 Available Forms:
600 Nickel Alloy Sheet, 600 Nickel Alloy Plate, 600 Nickel Alloy Bar, 600 Nickel Alloy Forged Bar
Inconel 600 Applications: Inconel Alloy 600 is used in the aerospace, heat treating industries, pulp and paper as well as the chemical process, food process and nuclear industries.
Description
Inconel Alloy 600 is a solid solution strengthened alloy used for corrosion and high temperature resistance up to 2000 Degrees F. It is also nonmagnetic, possessing an excellent combination of high strength, both hot and cold workability and resistance to ordinary forms of corrosion. A600 also shows high levels of resistance to stress-corrosion cracking, atmospheric corrosion, corrosion by high purity water, halogen, exhaust gases and most organic acids and inorganic acids.
Royal Emperor Metals & Supply is a leading supplier of quality Inconel 600 Sheet, Inconel 600 Plate, Inconel 600 Steel Bar, Inconel 600 Forged Bar.
All of our Inconel 600 is ordered to specific thickness. We supply Inconel 600 and are capable of fulfilling your required lengths and widths. Royal Emperor Metals & Supply Inc. also has a stocking program to support long term contract for your Inconel 600 needs.
Inconel 625 - Sheet, Plate, Bar, Forged Bar
UNS N06625, AMS 5599, AMS 5581, AMS 5666
* All Trademarks and/or Trade names are the properties of their respective owners.
Inconel 625 Specifications: AMS 5599, AMS 5581, AMS 5666
Alloy 625, Nickel 625, 625 Inconel Alloy, A625, UNS N06625, Ni 58.0, Cr 21.5 Mo 9.0,Mn 0.50 C0.10 Si 0.50 Fe 5.
Inconel 625 Available Forms: 625 Nickel Alloy Sheet, 625 Nickel Alloy Plate, 625 Nickel Alloy Bar, 625 Nickel Alloy Forged Bar
Inconel 625 Applications: Alloy 625 is used in the chemical process industry, marine engineering, pollution control equipment and nuclear industries.
Description
Inconel 718 is a precipitation hardenable nickel-based alloy designed to display exceptionally high yield, tensile and creep-rupture properties at temperatures up to 1300 Degrees F. The sluggish age-hardening response of Inconel 718 permits annealing and welding without spontaneous hardening during heating and cooling. Inconel 718 has excellent weldability when compared to the nickel-base superalloys hardened by aluminum and titanium.
Composition
Alloy 718 is made up primarily of nickel (52%). Alloying elements include Iron (19%), Chromium (18%), Columbium+ Tantalum (5%), Molybdenum (3%), Titanium (0.9%), Aluminum (0.5%) with the addition of other elements in trace amounts such as Baron, Cobalt, Copper, Manganese and Silicon.
Physical Properties
718 features a melting point of 2300°c and possesses impressive tensile strength that lends itself well to the wide variety of industrial applications. The alloy has excellent performance in properties such as weldability and creep-rupture.
Heat Treatment
Heat treatment schedules for wrought Inconel 718 are based primarily on considerations of solution and re-precipitation reactions of the gamma-prime and gamma-double-prime phases for strengthening and of delta phase for grain size control. The heat treatments generally involve a high temperature anneal for solutioning of these second phases followed by one or two lower temperature aging treatments to re-precipitate the strengthening phases in the desired distributions.Some strengthening precipitate generally forms on cooling from the solution annealing temperature. The first aging treatment coarsens this precipitate as well as forming additional precipitate. The second lower temperature aging treatment promotes additional fine precipitate for improved tensile strength and creep rupture life.
Standard heat treatment for most specifications includes a solution heat treatment in the range of 1750F to 1800F, followed by a duplex precipitation heat treatment of 1325F/8 hours with a ~100F/hour cool down to 1150F, and holding an additional 8 hours at 1150F, for a total precipitation heat treat time of 18 hours, then AC. A second heat treat procedure involves slightly higher solutioning and aging temperatures. It is used for optimum ductility and low temperature toughness in heavy sections, although it can also produce notch brittleness in creep rupture and is not recommended for applications operating above 1000F. This heat treatment involves solution annealing above the delta solvus temperature, as follows: Solution heat treat at 1950F, one-half to one hour, AC or faster; duplex precipitation heat treat at 1400F.
Corrosion Resistance
Inconel 718 possesses excellent corrosion and oxidation resistance. It also has good sea water corrosion resistance and it is attractive for marine applications.
Royal Emperor Metals & Supply is a leading supplier of quality Inconel 718 Sheet, Inconel 718 Plate, Inconel 718 Bar, Inconel 718 Forged Bar.
All of our Inconel 718 is ordered to specific thickness. We supply Inconel 718 and are capable of fulfilling your required lengths and widths. Royal Emperor Metals & Supply Inc. also has a stocking program to support long term contract for your Inconel 718 needs.