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

Zertifizierung	ISO, AISI
Min Bestellmenge	50 kg
Preis	US $16.55-20.45 / k

Produktdetails

Modellnummer	inconel 718	Form	Runden
Technik	Warmgewalzt	Oberflächenbehandlung	In Essig einlegen
Spezifikation	12202440, 15003000, 15006000, 20006000 mm	Produktionskapazität	50000 kg
Temperaturbereich	-253 °C bis 705 °C (-423 °F bis 1300 °F)	Oxidationsbeständigkeit	Bis zu 1800 °F (980 °C)
Breitenbereich	600 mm ~ 2030 mm	Dickenbereich	0,1 ~ 120,0 mm
Längenbereich	300~6000 mm, maximal 18000 mm	Dichte	8,192 g/cm3 (lösungsbehandelt), 8,22 g/cm3 (lösungsbehandelt und gealtert)
Schmelzbereich	1370–1430 °C (2500–2600 °F)	Streckgrenze	80.000 psi (550 MPa) min (Blech und Streifen), 105.000 psi (725 MPa) min (Platte)
Bruchfestigkeit	140.000 psi (965 MPa) min (Blech und Streifen), 150.000 psi (1.035 MPa) min (Platte)
Hervorheben	High Temperature Resistant Inconel 718 Sheet , ASTM B670 Nickel Alloy Sheet , AMS 5596 Super Alloy Sheet

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Produkt-Beschreibung

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

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

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)

Umbauten:

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

High Temperature Resistant Inconel 718 Sheet

ASTM B670 Nickel Alloy Sheet

AMS 5596 Super Alloy Sheet