All Products
-
Stainless Steel Strip
-
Stainless Steel Sheet
-
Stainless Steel Plate
-
Stainless Steel Pipe
-
Stainless Steel Bar
-
Galvanized Steel Coil
-
Steel Plate
-
Steel Round Bar
-
Nickel Alloy
-
Seamless Steel Pipe
-
Stainless Steel Beam
-
Copper Plate Sheet
-
Copper Round Bar
-
stainless steel round bar
-
stainless steel channel bar
-
stainless steel angle bar
-
stainless steel coil strip
-
stainless steel flat bar
-
stainless steel circle
-
Pipe Fitting
-
Water Ripple Stainless Steel Sheet
-
Nickel Alloy and Super Alloy
-
cold rolled steel coil
-
copper
-
Nickel Base Alloy Products
-
Others
-
Raian IonescuMaterial quality very good. we have cooperate more than 10 Years. They trade lots kinds of steel material. All material quality good. They duty for all material quality. We are planing continue cooperate with them in the future
Inconel 718 Nickel Alloy Sheet ASTM B670 AMS 5596 High Temperature Resistant Super Alloy Sheet
Product Details
| Model Number | Inconel 718 | Shape | Round |
|---|---|---|---|
| Technique | Hot Rolled | Surface Treatment | Pickling |
| Specification | 1220*2440, 1500*3000, 1500*6000, 2000*6000mm | Production Capacity | 50000kgs |
| Temperature Range | -423°F To 1300°F (-253°C To 705°C) | Oxidation Resistance | Up To 1800°F (980°C) |
| Width Range | 600mm~2030mm | Thickness Range | 0.1~120.0mm |
| Length Range | 300~6000mm, Max 18000mm | Density | 8.192 G/cm3 (Solution Treated), 8.22 G/cm3 (Solution Treated And Aged) |
| Melting Range | 2500-2600°F (1370-1430°C) | Yield Strength | 80,000 Psi (550 MPa) Min (Sheet And Strip), 105,000 Psi (725 MPa) Min (Plate) |
| Ultimate Tensile Strength | 140,000 Psi (965 MPa) Min (Sheet And Strip), 150,000 Psi (1,035 MPa) Min (Plate) | ||
| Highlight | High Temperature Resistant Inconel 718 Sheet,ASTM B670 Nickel Alloy Sheet,AMS 5596 Super Alloy Sheet |
||
Product Description
Inconel 718 Nickel Alloy Sheets Overview
Inconel 718 is a Gamma Prime strengthened alloy with exceptional mechanical properties at both elevated and cryogenic temperatures, suitable for applications up to approximately 1300°F. This versatile alloy can be readily worked and age hardened, offering excellent strength from -423°F to 1300°F (-253°C to 705°C).
The material is age hardenable and can be welded in fully aged condition, with excellent oxidation resistance up to 1800°F (980°C). Typically supplied in solution annealed temper, Inconel 718 can also be ordered in aged, cold worked, or cold worked and aged conditions.
Inconel 718 Plate conforms to AMS 5596/5597 standards with UNS designation N07718. This nickel-chromium alloy, enhanced with aluminum addition, demonstrates high mechanical properties in extremely hot environments. Common applications include jet engine and gas turbine operations, cryogenic storage tanks, downhole shafts, and wellhead parts.
Available Forms: Sheet, plate, coil, strip, wire, pipe, tube, bar, profile, round, flat, square, hexagonal
Specifications and Standards
| 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 |
| Forging | ASTM B637 AMS 5562 AMS 5663 AMS 5664 PWA 1009 PWA 1010 GE B50TF15 |
| Weld Wire | A5.14 ERNiFeCr-2 |
| DIN | 2.4668 |
Common Trade Names
Alloy 718, Inconel® 718, Nickel 718
Dimension Ranges
Width: 600mm ~ 2030 mm
Thickness: 0.1 ~ 120.0 mm
Length: 300 ~ 6000 mm, Maximum 18000 mm
Thickness: 0.1 ~ 120.0 mm
Length: 300 ~ 6000 mm, Maximum 18000 mm
Surface Finish: No.1, 2B, BA, No.3, No.4, No.5, No.8, HL, Etching, SB, Ti-coating, color-coating, embossing
Applications
- Gas turbine components and cryogenic storage tanks
- Jet engines, pump bodies and parts, rocket motors and thrust reversers
- Nuclear fuel element spacers and hot extrusion tooling
- High strength bolting and down hole shafting
Material Equivalents
UNS N07718
DIN NiCr19NbMo
EN NiCr19NbMo
DIN NiCr19NbMo
EN NiCr19NbMo
Chemical Composition
| 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 |
Corrosion and Oxidation Resistance
Inconel 718 provides excellent resistance to oxidation and corrosion at temperatures within the alloy's useful strength range, particularly in atmospheres encountered in jet engines and gas turbine operations.
Physical Properties
| Property | 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 |
Thermal Conductivity
| Temperature Range | Co-Efficients | ||
|---|---|---|---|
| °C | °F | W/m.K | Btu.ft/ft².hr.°F |
| 0-100 | 32-212 | 6.5 | 11.2 |
Mechanical Properties
Sheet and Strip (AMS 5596)
| Yield Strength Min (0.2% offset) | Ultimate Tensile Strength Min | Elongation (% in 2") |
|---|---|---|
| 80,000 psi (550 MPa) | 140,000 psi (965 MPa) | 30 (min) |
Plate (AMS 5597)
| Yield Strength Min (0.2% offset) | Ultimate Tensile Strength Min | Elongation (% in 2") |
|---|---|---|
| 105,000 psi (725 MPa) | 150,000 psi (1,035 MPa) | 30 (min) |
Solution Treated Plus Precipitation Heat Treated
| Yield Strength Min (0.2% offset) | Ultimate Tensile Strength Min | Elongation (% in 2") |
|---|---|---|
| 150,000 psi (1,035 MPa) | 180,000 psi (1,240 MPa) | 12 (min) |
Recommended Products