| Type: | Stainless Steel Sheets |
|---|---|
| Standard: | ASTM, AISI |
| Grade: | Duplex Steel |
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Inconel 718 is a Gamma Prime strengthened alloy with excellent mechanical properties at elevated temperatures, as well as cryogenic temperatures. Suitable for temperatures upto around 1300 F. Can be readily worked and age hardened.
Excellent strength from -423 degrees F to 1300 degrees F (-253 degrees C to 705 degrees C). Age hardenable and may be welded in fully aged condition, Excellent oxidation resistance up to 1800 degrees F (980 degrees C). Typically sold in the solution annealed temper, but can be ordered aged, cold worked, or cold worked & aged.
Inconel 718 Plate is supplied to AMS 5596/5597 and has a UNS designation N07718. Alloy 718 Plate is a nickel-chromium alloy has an addition of aluminum. This addition allows it to demonstrate high mechanical properties even in extremely hot environments. Inconel 718 Sheet is typically used for Jet engine & Gas turbine operations. Inconel 718 Coil is also resistant to caustic corrosion and corrosion caused by high purity water. Cutting of Inconel 718 Clad Plate & Inconel 718 Strip is often done with a waterjet cutter. Internal threads can also be cut by single point method on lathe, or by threadmilling on a machining center. Inconel 718 Shim & Inconel 718 Flat Sheet is commonly used for cryogenic storage tanks, downhole shafts and wellhead parts. Inconel Alloy 718 Plate is used in applications that require high strength such as parts for high temperature Cryogenic tanks, jet engines and high speed airframe parts such as wheels, buckets, spacers. 718 Inconel Sheet can be cold formed by standards methods.
Produc Forms : Sheet, plate , Coil , Strip .wire , Pipe, Tube ,Bar , Profile, Round, Flat, Square, Hexagonal
Specifications
| Form | Standard |
| Metal Type | UNS N07718 |
| Bar | ASTM B637 AMS 5662 AMS 5663 AMS 5664 PWA 1009 PWA 1010 GE B50TF15 |
| Wire | AMS 5832 |
| Sheet | ASTM B670 AMS 5596 AMS 5597 PWA 1033 GE B50TF14 ASTM B670 ASTM B637 |
| Plate | ASTM B670 AMS 5596 AMS 5597 PWA 1033 GE B50TF15 ASTM B670 ASTM B637 |
|
Tube
|
AMS 5589 AMS 5590
|
|
Pipe
|
AMS 5589 AMS 5590
|
| Fitting | |
| Forging | ASTM B637 AMS 5562 AMS 5663 AMS 5664 PWA 1009 PWA 1010 GE B50TF15 |
| Weld Wire | A5.14 ERNiFeCr-2 |
|
Weld Electrode
|
|
| Din | 2.4668 |
|
|
ASTM | JIS | AISI | EN |
| Grade | S30100 | SUS301 | 301 | 1.431 |
| S30400 | SUS304 | 304 | 1.4301 | |
| S30403 | - | 304L | 1.4307 | |
| S31008 | SUS310S | 310S | 1.4845 | |
| S31603 | - | 316L | 1.4404 | |
| S32100 | SUS321 | 321 | 1.4541 | |
| S41008 | SUS410S | 410S | - | |
| S43000 | SUS430 | 430 | 1.4016 | |
| S43932 | - | - | 1.451 | |
| S44400 | SUS444 | 444 | 1.4521 | |
| S44500 | SUS430J1L | - | - |
Width: 600mm~2030 mm
Thickness: 0.1~120.0 mm
Length: 300~6000 mm , Max 18000 mm
Surface Finish: No.1, 2B, BA, No.3, No.4, No.5, No.8, HL, Etching, SB, Ti-coating,color-coating ,embossing .
Uses for Inconel 718 tend to be in the field of gas turbine components and cryogenic storage tanks. Jet engines, pump bodies and parts, rocket motors and thrust reversers, nuclear fuel element spacers, hot extrusion tooling. Other popular uses are high strength bolting, and down hole shafting.
Inconel® 625 super alloys are also available in plate, bar, forgings and tubing. Contact Xinzheng to Enquiry.
UNS N07718
DIN NiCr19NbMo
EN NiCr19NbMo
Typical chemical analysis of Inconel 718.
|
Element
|
Percentage |
| Carbon | 0.08 max |
| Manganese | 0.35 max |
| Phosphorus | 0.015 max |
| Sulfur | 0.015 max |
| Silicon | 0.35 max |
| Chromium | 17-21 |
| Nickel | 50-55 |
| Molybdenum | 2.80-3.30 |
| Columbium | 4.75-5.50 |
| Titanium | 0.65-1.15 |
| Aluminum | 0.20-0.80 |
| Cobalt | 1.00 max |
| Boron | 0.006 max |
| Copper | 0.30 max |
| Tantalum | 0.05 max |
| Iron | Balance |
Inconel 718 has good resistance to oxidation and corrosion at temperatures in the alloy's useful strength range in atmospheres encountered in jet engines and gas turbine operations.
Typical physical properties of Inconel 718 are summarized in the table below.
| Solution Treated | Solution Treated and Aged | |
| Density | 0.296 lb/in3 (8.192 g/cm3) | 0.297 lb/in3 (8.22 g/cm3) |
| Specific Gravity | 8.19 | 8.22 |
| Melting Range | 2500-2600°F | 1370-1430°C |
The thermal conductivity at various temperatures for Inconel 718 are given in the following table.
| Temperature Range | Co-Efficients | ||
| °C | °F | W/m.K | Btu.ft/ft2.hr.°F |
| 0-100 | 532-212 | 6.5 | 11.2 |
The room temperature strength of the Inconel 718 alloy is substantially increased by precipitation heat treatment as
the following data indicate. These values are properties specified for sheet, strip and plate in AMS 5596 and AMS 5597.
| Yield Strength Min (0.2% offset) |
Ultimate Tensile Strength Min |
Elongation (% in 2") |
|
| Sheet and strip | 80,000 psi (550 MPa) | 140,000 psi (965 MPa) | 30 (min) |
| Plate | 105,000 psi (725 MPa) | 150,000 psi (1,035 MPa) | 30 (min) |
Solution trated plus precipitation heat treated.
| Yield Strength Min (0.2% offset) |
Ultimate Tensile Strength Min |
Elongation (% in 2") |
| 150,000 (1,035 MPa) | 180,000 psi (1,240 MPa) | 12 (min) |
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