Item # I718-2750, Inconel® 718 Plate On Continental Steel & Tube Co.

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	Item # I718-2750, Inconel® 718 Plate

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Inconel 718 is a precipitation-harden able, nickel-chromium alloy containing also-significant amounts of iron, niobium and molybdenum, along with lesser amounts of aluminum and titanium. It combines corrosion resistance and high strength with outstanding weld ability, including resistance to post weld cracking. Inconel 718 has excellent creep-rupture strength at temperatures to 1300°F (700°C). Inconel 718 is used in gas turbines, rocket motors, space-craft, nuclear reactors, pumps and tooling. Standard product forms are round, flats, extruded section, pipe, tube, forging stock, plate, sheet, strip and wire.

Unit of Measure: Imperial

Specifications · Nickel Alloy Compositions · Typical Mechanical Properties

Specifications

Material		Inconel®

Shapeform		Plates

Thickness		2 3/4 inches

Thickness		2.75 inches

Plate Weight per Unit Area		0.838 lbs/in²

Nickel Alloy Compositions

Alloy		Inconel® 718

Basic Composition		18.0% Chrominum 18.5% Iron 3.0% Molybdenum 5.0% Niobium 54.0% Nickel

Density		0.296 lbs/in³

ASTM Specification		ASTM B670 SAE 5597 UNS N07718

Typical Mechanical Properties

Melting Temperature Range		2300 to 2437 ºF 1260 to 1336 ºC

Rupture Strength (1000 h at 1100°F/595°C)		110000 psi 760 MPa

Rupture Strength (1000 h at 1200°F/650°C)		86000 psi 590 MPa

Rupture Strength (1000 h at 1300°F/705°C)		53000 psi 370 MPa

Rupture Strength (1000 h at 1400°F/760°C)		24000 psi 170 MPa

DOWNLOADS


		Terminology Sheet

		Nickel Alloys Comparison Chart

		Inconel® Datasheet

		Inconel® Reference Guide

Item # I718-2750, Inconel® 718 Plate

Material

Shapeform

Thickness

Thickness

Plate Weight per Unit Area

Alloy

Basic Composition

Density

ASTM Specification

Melting Temperature Range

Rupture Strength (1000 h at 1100°F/595°C)

Rupture Strength (1000 h at 1200°F/650°C)

Rupture Strength (1000 h at 1300°F/705°C)

Rupture Strength (1000 h at 1400°F/760°C)