Inconel 718 Nickel Alloy Sheet ASTM B670 AMS 5596 High Temperature Resistant Super Alloy Sheet

Price Negotiable
Price: 16.55
MOQ: 50
Delivery Time: Negotiable
Product Description
Inconel 718 Nickel Alloy Sheets Overview
Inconel 718 is a Gamma Prime strengthened alloy with excellent mechanical properties at elevated temperatures, as well as cryogenic temperatures. Suitable for temperatures up to around 1300°F (705°C), this alloy can be readily worked and age hardened.
This high-performance alloy demonstrates excellent strength from -423°F to 1300°F (-253°C to 705°C), is age hardenable, and can be welded in fully aged condition. It offers excellent oxidation resistance up to 1800°F (980°C) and is 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 with UNS designation N07718. This nickel-chromium alloy contains aluminum, which enables it to demonstrate high mechanical properties even in extremely hot environments. Common applications include jet engine and gas turbine operations, cryogenic storage tanks, downhole shafts, and wellhead parts.
Available Product 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
Plate ASTM B670, AMS 5596, AMS 5597, PWA 1033, GE B50TF15
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 - 2030mm
Thickness: 0.1mm - 120.0mm
Length: 300mm - 6000mm (Maximum 18000mm)
Surface Finish Options
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
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 has good 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) 2500-2600°F (1370-1430°C)
Thermal Conductivity
Temperature Range Thermal Conductivity
0-100°C (32-212°F) 6.5 W/m·K (11.2 Btu·ft/ft²·hr·°F)
Mechanical Properties
Sheet and Strip (AMS 5596/5597)
Property Minimum Value
Yield Strength (0.2% offset) 80,000 psi (550 MPa)
Ultimate Tensile Strength 140,000 psi (965 MPa)
Elongation (2") 30% minimum
Plate (Solution Treated + Precipitation Heat Treated)
Property Minimum Value
Yield Strength (0.2% offset) 150,000 psi (1,035 MPa)
Ultimate Tensile Strength 180,000 psi (1,240 MPa)
Elongation (2") 12% minimum
Inconel 718 Nickel Alloy Sheets and Plates

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Company TSING SHAN STEEL INDUSTRIAL LIMITED
Location NO.288,Youyi Road Xi Shan Dristrict , Wuxi, Jiangsu, China
Contact Person Gao Ben

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