MONEL
INCONEL
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AEETHER

INCOLOY
HASTELLOY
UNS N07718

Inconel Alloy
718

W.Nr. 2.4668
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Learn about Inconel 718
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Introduction
Main Standards
Chemical Composition
Data Sheet
Applications
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Inconel 718 Introduction

logo of precipitation strengthened alloy

Precipitation
Strengthened Alloy

Nickel
Chromium
Iron
Niobium
Corrosion
Resistance
79
Mechanical
Behavior
90
Purity
94

Overview

As a leading supplier & manufacturer in China, AEETHER supply cost-effective Inconel 718 Products.

INCONEL® alloy 718 (UNS N07718 / W.Nr. 2.4668) is a high-strength, corrosion-resistant nickel chromium material used at -423° to 1300°F.

The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding.

The ease and economy with which INCONEL alloy 718 can be fabricated, combined with good tensile, fatigue, creep, and rupture strength, have resulted in its use in a wide range of applications. Examples of these are components for liquid fueled rockets, rings, casings and various formed sheet metal parts for aircraft and land-based gas turbine engines, and cryogenic tankage. It is also used for fasteners and instrumentation parts.

Mechanical Properties

For most applications, INCONEL alloy 718 is specified as: solution annealed and precipitation hardened (precipitation hardening, age hardening, and precipitation heat treatment are synonymous terms). Alloy 718 is hardened by the precipitation of secondary phases (e.g. gamma prime and gamma double-prime) into the metal matrix. The precipitation of these nickel- (aluminum, titanium, niobium) phases is induced by heat treating in the temperature range of 1100 to 1500°F. For this metallurgical reaction to properly take place, the aging constituents (aluminum, titanium, niobium) must be in solution (dissolved in the matrix); if they are precipitated as some other phase or are combined in some other form, they will not precipitate correctly and the full strength of the alloy with not be realized. To perform this function, the material must first be solution heat treated (solution annealed is a synonymous term).

Corrosion Resistance

INCONEL alloy 718 has excellent corrosion resistance to many media. This resistance, which is similar to that of other nickel-chromium alloys, is a function of its composition. Nickel contributes to corrosion resistance in many inorganic and organic, other than strongly oxidizing, compounds throughout wide ranges of acidity and alkalinity. It also is useful in combating chloride-ion stress-corrosion cracking. Chromium imparts an ability to withstand attack by oxidizing media and sulfur compounds. Molybdenum is known to contribute to resistance to pitting in many media.

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Inconel 718 Standards

ASTM B983
Seamless Pipe & Tube
ASTM B637
Bar and Forging
ASTM B670
Plate, Sheet and Strip
ASTM B906
Plate, Sheet and Strip
SAE AMS 5662
Bar and Forging
SAE AMS 5663
Bar and Forging
SAE AMS 5664
Bar and Forging
SAE AMS 5832
Welding Wire
SAE AMS 5962
Round Bar and Wire
SAE AMS 5596
Plate, Sheet and Strip
SAE AMS 5597
Plate, Sheet and Strip
SAE AMS 5950
Plate, Sheet and Strip
SAE AMS 5589
Seamless Tube
SAE AMS 5590
Seamless Tube
AWS A5.14 ERNiFeCr-2
Filler Metal

Inconel 718 Chemical Composition

Data Sheet

Physical Properties

Density g/cm3 8.19
lb/in.3 0.296
Melting Range °F 2300 - 2437
°C 1260 - 1336
Specific Heat (21°C) Btu/lb-°F 0.104
J/kg-°C 435
Permeability at 200 oersted 15.9 kA/m 1.0006
Curie Temperature Annealed Material °F < -320
°C -196
Annealed and Aged Material °F -170
°C -112
Permeability at 200 oersted and 70°F Annealed Material 1.0013
Annealed and Aged Material 1.0011

Mechanical Properties

Condition Diameter,
in.(mm)
Tensile
Strength, ksi
(Kg/cm2)
min.
Yield Strength
(0.2% Offset),
ksi (Kg/cm2)
Elongation in
2 in. (50.8
mm) or 4D%
minimum
Reduction of
Area, %
minimum
Impact
Strength,
ft•lb (Kg•m)
min. aver.
Hardness, Rockwell C
minimum maximum minimum maximum
Cold worked,
solution
annealed &
aged
0.5 (12.7) to
3 (76.2),
inclusive
150 (10,545) 120 (8436) 140 (9842) 20 25 40 (5.55) 30 40
Hot worked,
solution
annealed &
aged
0.5 (12.7) to
8 (203.2),
inclusive
150 (10,545) 120 (8436) 140 (9842) 20 25 40 (5.55) 30 40
Hot worked,
solution
annealed &
aged
8 (203.2) to
10 (254),
inclusive
150 (10,545) 120 (8436) 140 (9842) 20 25 40 (5.55) 30 40
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Inconel 718 Applications

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