Inconel Alloy
718
Inconel 718 Introduction
Precipitation
Strengthened Alloy
Resistance
Behavior
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.
Inconel 718 Standards
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 |
Inconel 718 Applications
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