Inconel 718 Round Bar Inconel 718 round bar is a high-strength, nickel-based superalloy used in demanding engineering applications that require excellent mechanical properties, corrosion resistance and performance at elevated temperatures. Also known as Alloy 718, it is identified by UNS N07718 and is widely used in aerospace, oil and gas, power generation and specialised industrial manufacturing.
Unlike conventional stainless steels and many other nickel alloys, Inconel 718 is strengthened through precipitation hardening. This gives it a combination of high tensile strength, good fatigue resistance and useful performance under demanding service conditions.
For engineers, manufacturers and procurement professionals, selecting the correct Inconel 718 round bar requires attention to its grade, dimensions, heat-treatment condition, applicable standards and material documentation.
This guide explains the important properties, specifications, applications and purchasing considerations associated with Inconel 718 round bars.
Table of Contents
ToggleInconel 718 is a precipitation-hardenable nickel-chromium alloy containing iron, niobium, molybdenum and other alloying elements.
It is designed for applications where high mechanical strength and resistance to demanding operating environments are important.
Important material identifiers include:
The alloy is particularly recognised for its ability to achieve high strength through controlled heat treatment.
The chemical composition of Inconel 718 contributes to its strength, corrosion resistance and high-temperature characteristics.
The following table provides commonly specified composition limits for Alloy 718. The exact requirements should always be verified against the applicable material specification and material test certificate.
| Element | Typical specification range or limit |
|---|---|
| Nickel (Ni) | 50.0–55.0% |
| Chromium (Cr) | 17.0–21.0% |
| Iron (Fe) | Balance |
| Niobium + Tantalum (Nb + Ta) | 4.75–5.50% |
| Molybdenum (Mo) | 2.80–3.30% |
| Titanium (Ti) | 0.65–1.15% |
| Aluminium (Al) | 0.20–0.80% |
| Cobalt (Co) | 1.0% maximum |
| Carbon (C) | 0.08% maximum |
| Manganese (Mn) | 0.35% maximum |
| Silicon (Si) | 0.35% maximum |
| Phosphorus (P) | 0.015% maximum |
| Sulphur (S) | 0.015% maximum |
These are general reference limits. The applicable product specification should be checked for the complete chemistry requirements and any additional restrictions.
Inconel 718 is selected for applications requiring a combination of high strength, fatigue resistance and corrosion performance.
One of the most important characteristics of Inconel 718 is its high mechanical strength after suitable precipitation-hardening treatment.
Its strength makes it suitable for selected components exposed to significant mechanical loads.
Inconel 718 develops its high strength through a controlled heat-treatment process.
Niobium, titanium and aluminium contribute to the precipitation-strengthening mechanism. The final properties depend on the heat-treatment cycle and material condition.
The nickel and chromium content contributes to resistance against several corrosive environments.
The alloy is used in selected applications where corrosion resistance and mechanical strength are both important. However, its suitability must be checked against the actual chemical environment and operating conditions.
Inconel 718 is used in components exposed to repeated mechanical loading. Its fatigue performance depends on the material condition, component geometry, surface finish, manufacturing process and operating environment.
Inconel 718 is used in selected elevated-temperature applications, particularly in aerospace and power-generation engineering.
Its allowable service temperature depends on the design, stress level, exposure duration and applicable engineering requirements.
Heat treatment is an important part of achieving the required mechanical properties of Inconel 718.
The alloy is commonly supplied in a solution-treated condition before precipitation hardening, depending on the product specification and intended application.
Solution treatment is used to establish a suitable metallurgical condition before subsequent ageing.
Ageing treatments allow strengthening precipitates to form within the alloy’s microstructure.
The commonly used strengthening phases include gamma double-prime and gamma-prime.
The heat-treatment condition affects:
Buyers should specify the required condition and mechanical-property limits rather than assuming that every Inconel 718 round bar has identical properties.
Heat treatment should follow the applicable material specification and qualified processing procedure.
The applicable material standard depends on the product form and project requirements.
| Standard | Product form |
|---|---|
| ASTM B637 | Precipitation-hardening nickel alloy bars, forgings and related product forms covered by the specification |
| AMS 5662 | Nickel alloy bars, forgings and rings in a specified condition |
| AMS 5663 | Nickel alloy bars, forgings and rings in a precipitation-hardened condition |
These are commonly referenced specifications associated with Alloy 718. Confirm the current edition, exact product form, material condition and supplementary requirements before procurement.
Do not assume that every specification applies to every Inconel 718 product.
Inconel 718 is used across industries where mechanical strength, fatigue resistance and performance under demanding operating conditions are important.
Selected aerospace applications include:
Potential applications include:
The suitability of the alloy for sour-service applications must be checked against the relevant standards and project requirements.
Inconel 718 is used in selected power-generation components where high mechanical strength and elevated-temperature performance are required.
The alloy is also used in specialised machinery and equipment where conventional materials may not provide the required mechanical performance.
Before purchasing Inconel 718 round bars, procurement teams should verify the following:
A clear purchase specification helps prevent material mismatches and supports reliable procurement.
Manan Steel & Metals deals in specialty metals and alloys for industrial and engineering requirements.
Buyers looking for Inconel 718 can share their required grade, dimensions, quantity, applicable specification and material condition.
Providing the technical details at the enquiry stage helps identify the correct material requirements.
Explore the Manan Steel & Metals website or submit your requirement through the Contact Us page.
You can also refer to the round bar product page for additional product information.
The UNS designation of Inconel 718 is N07718.
The Werkstoff number commonly associated with Inconel 718 is 2.4668.
Yes. Inconel 718 is a precipitation-hardenable nickel-based alloy. Controlled heat treatment develops its high mechanical strength.
Inconel 718 is a nickel-based precipitation-hardenable superalloy designed for demanding mechanical and temperature conditions. Stainless steel grades have different compositions, strengthening mechanisms and application limits.
It is used in selected aerospace, oil and gas, power-generation and specialised industrial engineering applications.
ASTM B637 is a commonly referenced specification for precipitation-hardening nickel alloy bars and other covered product forms. Specific AMS specifications may also apply depending on the application and material condition.
Inconel 718 round bar is an important material for specialised engineering applications requiring high mechanical strength, fatigue resistance and dependable performance under demanding conditions.
Its precipitation-hardening capability distinguishes it from many conventional nickel alloys. However, selecting the correct product requires careful verification of grade, material condition, dimensions, applicable standards and material documentation.
For Inconel 718 and other specialty alloy requirements, contact Manan Steel & Metals with your technical specifications.
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