Inconel 718 UNS N07718 2.4668 Heat-Resisting Superalloy Bars and plates

It exhibits excellent comprehensive properties in the temperature range of -253°C to 700°C, with its yield strength below 650°C ranking first among wrought superalloys. It also features good fatigue resistance, radiation resistance, oxidation resistance and corrosion resistance, as well as favorable formability and weldability, yet the cost of its machining is relatively high.

Applications of Inconel 718

It can be fabricated into various components with complex geometries and is widely used in aerospace, nuclear energy, petroleum industries and extrusion dies. It is applicable for manufacturing various stationary and rotating parts in aerospace engines, such as disks, ring forging parts, blades, shafts, fasteners, sealing elements and welded structures. Additionally, it can be used to produce various elastic components for nuclear industry applications.

Equivalent Grades and Commonly Used Specifications of Inconel 718

Steel Grade Specification Specification Name
GH4169 /

GH169 /

H41690

GB/T 14992 Superalloys and intermetallic compounds-Designation and chemical composition
GB/T 14994 Superalloy Cold Drawn Bars
GJB 713A Specification for superalloy bars for aerospace
GB/T 30566  Cold-rolled heat-resisting superalloy sheets
UNS N07718 /

Inconel 718

ASTM B637 Standard Specification for Precipitation-Hardening and Cold Worked Nickel Alloy Bars, Forgings, and Forging Stock for Moderate or High Temperature Service
ASTM B670 Precipitation-Hardening Nickel Alloy Plate, Sheet, and Strip for High-Temperature Service
ASTM B983 tandard Specification for Precipitation Hardened or Cold Worked, Seamless Nickel Alloy Pipe and Tube
AMS 5662 Nickel Alloy, Bars, Forgings, and Rings, Solution Treated (Inconel 718)
AMS 5663 Nickel Alloy, Bars, Forgings, and Rings, Solution Treated and Precipitation Hardened (Inconel 718)
AMS 5596 Nickel Alloy, Plate, Sheet, and Strip, Solution Treated (Inconel 718)
AMS 5597 Nickel Alloy, Plate, Sheet, and Strip, Solution Treated and Precipitation Hardened (Inconel 718)
Products produced as per other specifications or technical agreements (if need) are available.

Typical Chemical Composition of Inconel 718

Elements C Si Mn P S Ni Cr Co Mo Ti Al B Cu Nb+Ta
Contents% ≤0.08 ≤0.35 ≤0.35 ≤0.015 ≤0.015 50.00~55.00 17.00~21.00 ≤1.00 2.80~3.30 0.65~1.15 0.20~0.80 ≤0.006 ≤0.30 4.75~5.50
Products produced as per other specifications or technical agreements (if need) are available.

Typical Chemical Composition of Inconel 718

Delivery Condition

Mechanical Properties and Hardness of Heat-Treated Specimens
Rp0.2/(N/mm2) Rm/(N/mm2) A/% Zb/% Aku2d/J HBW

HRC

Solution Treated(924℃-1010℃, hold 1/2h at least, air)

≥1034 ≥1275 ≥6 ≥8 / ≥331

≥36

Precipitation Hardening(718℃±14℃, 8h, furnace cool to 621℃, ±14℃, hold until total time has reached 18h, air)

Products produced as per other specifications or technical agreements (if need) are available.

Product Forms and Size Range of Inconel 718

Product forms

Size range

Bars

Diameter or side length: 5.0mm~1000mm

Flats

thickness: 4.0mm~1000mm

width: 300mm~2200mm

Produce as other form and size according to technical requirements are available.
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