Inconel 718
UNS N07718
Supplier of Nickel Alloys and Specialist METALS
Inconel 718
Trade Names
Inconel® 718
UNS Ref:
N07718
Applications
Aircraft ducting and engine plumbing, gas turbines, rocket motors, spacecraft, nuclear reactors, pumps, and tooling.
Standards
ASTM B-670 AMS 5596 AMS 5597
Available Forms & Sizes
Range From
Range To

Round Bar
9.53mm
267mm

Sheet & Coil
0.25mm
101.6mm





Inconel 718 is a high-strength, corrosion-resistant nickel-chromium alloy that is known for its excellent mechanical properties and good fabricability. It belongs to the family of superalloys, which are designed to operate in high-temperature and high-stress environments, making them suitable for a variety of demanding applications. The composition of Inconel 718 includes:
Characteristics
Key characteristics of Inconel 625 include:
- High Temperature Strength: Inconel 718 maintains its mechanical properties at high temperatures, making it suitable for use in applications involving extreme heat. It has good tensile, fatigue, and creep-rupture strength at elevated temperatures.
- Corrosion Resistance: The alloy exhibits excellent corrosion resistance in a variety of environments, including aqueous corrosion, pitting, and crevice corrosion. This corrosion resistance makes it suitable for use in harsh and corrosive chemical environments.
- High Yield and Tensile Strength: Inconel 718 has high yield and tensile strengths, making it capable of withstanding significant mechanical loads. This property is particularly important in applications where strength and reliability are critical.
- Good Fatigue Resistance: The alloy has good fatigue resistance, making it suitable for applications involving cyclic loading, such as turbine engine components.
- Weldability: Inconel 718 is weldable using common welding techniques. However, post-weld heat treatment is often required to restore the material’s properties and eliminate any potential welding-induced issues.
- Excellent Formability: The alloy is known for its good formability, allowing it to be easily fabricated into various shapes. This property is advantageous in manufacturing processes.
- Gamma Prime Strengthening: Inconel 718 gains its high strength through a precipitation-hardening process involving the formation of a gamma prime phase (Ni3Nb) within the alloy matrix. This contributes to the material’s high-temperature strength.
- Oxidation Resistance: The alloy exhibits good oxidation resistance at high temperatures, which is crucial for applications in environments with elevated heat.
- Machinability: Inconel 718 can be machined, but due to its high strength and work-hardening characteristics, machining may be challenging. Proper tools and machining techniques are essential for achieving desired results.
- Applications: Common applications for Inconel 718 include components in gas turbines, aircraft engines, nuclear reactors, chemical processing equipment, and other high-temperature and corrosive environments.
Applications
It’s important to note that while Inconel 718 offers excellent performance in demanding conditions, its cost is relatively high compared to some other materials, and its use is often reserved for applications where its unique combination of properties is essential.
