Inconel Alloy 718 Coil
Inconel Alloy 718 Coil Supplier In China
As the professional nickel alloy coils supplier in China, we manufactures and produces customized thickness and width inconel alloy 718 coils.
Inconel alloy 718 is a high-strength, corrosion-resistant nickel chromium material used at -423° to 1300°F. The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding.
Inconel 718 coil is a nickel alloy raw material manufactured by rolling up a Inconel 718 sheet/plate.
According to different production processes, Inconel 718 coils are divided into Inconel 718 hot rolled coils and Inconel 718 cold rolled coils. After they are flattened, they can be made into plate and sheet.
The default surface finish of Inconel 718 cold rolled coil is 2B finish and the default finish of Inconel 718 hot rolled coil is No.1 finish. If you need other finish, please confirm with our expert team to customize.
Inconel Alloy 718 Coil Specifications
| Product Name | Inconel alloy 718 coil |
| Grades | Alloy 718 |
| Standards | ASTM/DIN/JIS/GB/T |
| Thickness | 0.10mm-5.0mm |
| Width | 5mm-1200mm |
| Edge | Slit/Round |
| Quantity Tolerance | ±10% |
| Paper Core Internal Diameter | Ø 150mm,Ø300mm, Ø400mm, Ø500mm paper core, special internal diameter core and without paper core on special request |
| Surface Finish | Mill/Bright/TR/Polishing/Annealing |
| Applications | Nickel alloys coils are ideally suited for a wide range of industries that require high-performance materials, including aerospace, marine, chemical processing, nuclear power generation and oil&gas production |
| Packaging | Wooden pallet/Wooden case |
| Payment Terms | 30% TT deposit and 70% balance before shipment, 100% LC at sight |
| Delivery Time | 7-10 working days |
| MOQ | 2,000 Kgs |
| Shipping Port | Shanghai/Ningbo port |
| Sample | The sample of nickel alloy coil is available |
| Remark | Nickel alloy coil can be customized |
Inconel Alloy 718 Coil Chemical Compositions
| Grade | Standard | C | Si | Mn | P | S | Cr | Ni | Ti |
| Inconel 718 | ASTM B 670 | ≤0.08 | ≤0.35 | ≤0.35 | ≤0.015 | ≤0.015 | 17.00-21.00 | 50.0-55.0 | 0.65-1.15 |
Inconel Alloy 718 Coil Mechanical Properties
| Element | Yield Strength (0.2%Offset) | Melting Point | Density | Tensile Strength | Elongation |
| Inconel 718 | MPa – 550 | 1390 °C (2540 °F) | 8.19 g/cm3 | MPa – 910 | Min 25 % |
Inconel Alloy 718 Coil Equivalent Grades
| STANDARD | 718 |
| WERKSTOFF NR. | 2.4668 |
| UNS | N07718 |
Inconel Alloy 718 Coil: The Ultimate Guide
When you choose to buy quality Inconel Alloy 718 Coil, there have some important points we need to know before we get started.
What are Inconel Alloy 718 Coils?
Inconel alloy 718 is a high-strength, corrosion-resistant nickel chromium material used at -423° to 1300°F. The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding.
Inconel 718 coil is a nickel alloy raw material manufactured by rolling up a Inconel 718 sheet/plate.
According to different production processes, Inconel 718 coils are divided into Inconel 718 hot rolled coils and Inconel 718 cold rolled coils. After they are flattened, they can be made into plate and sheet.
The default surface finish of Inconel 718 cold rolled coil is 2B finish and the default finish of Inconel 718 hot rolled coil is No.1 finish. If you need other finish, please confirm with our expert team to customize.
Inconel Alloy 718 Coil applications
For most applications, INCONEL alloy 718 is specified as: solution annealed and precipitation hardened (precipitation hardening, age hardening, and precipitation heat treatment are synonymous terms). Alloy 718 is hardened by the precipitation of secondary phases (e.g. gamma prime and gamma double-prime) into the metal matrix. The precipitation of these nickel- (aluminum, titanium, niobium) phases is induced by heat treating in the temperature range of 1100 to 1500°F. For this metallurgical reaction to properly take place, the aging constituents (aluminum, titanium, niobium) must be in solution (dissolved in the matrix); if they are precipitated as some other phase or are combined in some other form, they will not precipitate correctly and the full strength of the alloy with not be realized. To perform this function, the material must first be solution heat treated (solution annealed is a synonymous term).
