Case

Featured Products

Nickel 200/Ni 200/UNS N02200/W.Nr. 2.4066/Alloy 20...

Nickel 200 bar, designated as UNS N02200 and material number W.Nr. 2.4066, is a commercially pure wrought nickel alloy (≥99.0% Ni) known for its exc...
Learn More

Nickel 201/Ni 201/UNS N02201/W.Nr. 2.4068/Alloy 20...

Nickel 201/200 bar, designated as UNS N02200 (200) and N02201 (201), with material number W.Nr. 2.4066/2.4068, is a commercially pure wrought nickel a...
Learn More

Nimonic 263/UNS N07263/W. Nr. 2.4650/Alloy 263 bar

Nimonic 263 bar, designated as UNS N07263 and material number W.Nr. 2.4650, is a nickel-chromium-cobalt-molybdenum superalloy strengthened by precipit...
Learn More

Nimonic 90/UNS N07090/W. Nr. 2.4632/Alloy 90 bar

Nimonic 90 bar, designated as UNS N07090 and material number W.Nr. 2.4632, is a precipitation-hardenable nickel-chromium-cobalt superalloy strengthene...
Learn More

Nimonic 80A/UNS N07080/W.Nr. 2.4952,2.4631/Alloy 8...

Nimonic 80A bar, designated as UNS N07080 and material numbers W.Nr. 2.4952 / 2.4631, is a precipitation-hardenable nickel-chromium superalloy strengt...
Learn More

Nimonic 75/UNS N06075/Alloy 75 bar

Nimonic 75 bar, designated as UNS N06075 and commonly known as Alloy 75, is a nickel-chromium solid-solution strengthened alloy with additions of tita...
Learn More

Nimonic 80A Bar vs Inconel 718: Key Differences & Applications

2026-04-13

In our factory’s daily inquiry handling, Nimonic 80A Bar and Inconel 718 are two nickel-based superalloys that customers frequently compare side by side. Both are suitable for high-temperature and high-load applications, but when it comes to actual material selection, machining, lead time, and total cost, the differences become quite significant. Below, we explain these differences based on the most common issues encountered in real procurement and manufacturing scenarios.

Nimonic 80A

Material Overview

Nimonic 80A Bar is essentially a nickel-chromium-based superalloy strengthened by titanium and aluminum precipitation. It has long been used in hot-section components of aircraft engines and gas turbines. When supplied in bar form, customers typically focus on its high-temperature strength, oxidation resistance, and long-term stability around 700°C. Based on our factory’s shipment experience, 80A is more commonly used in applications requiring clear creep resistance and long-term high-temperature performance.

Inconel 718 follows a different technical route. It is also a nickel-based superalloy, but its strengthening mechanism mainly relies on the γ” phase formed by niobium, supplemented by γ’ strengthening. This gives it outstanding overall strength from room temperature to intermediate-high temperatures. The key practical advantage of 718 is its balance between strength, weldability, machinability, and industrial availability, making it widely used in aerospace, energy, and oil & gas industries.

Simply put: Nimonic 80A is more focused on long-term high-temperature service, while Inconel 718 is more oriented toward high-strength, all-around structural performance. Both are excellent, but their strengths lie in different areas.

Chemical Composition Comparison

Although both belong to the nickel-based system, their alloying strategies differ significantly. 80A primarily consists of Ni, Cr, Ti, Al, and often Co, while 718 relies more on Ni, Cr, Fe, Nb, and Mo, with Nb being a key strengthening element.

Grade Main Alloying Elements Strengthening Mechanism
Nimonic 80A Ni-Cr-Co-Ti-Al Mainly γ’ precipitation strengthening
Inconel 718 Ni-Cr-Fe-Nb-Mo-Ti-Al γ” + γ’ precipitation strengthening

In 80A, Ti and Al are critical for high-temperature precipitation strengthening, helping maintain microstructural stability at elevated temperatures. The addition of Co further enhances high-temperature strength but also increases material cost.

In Inconel 718, Nb plays a dominant role by promoting the formation of the γ” phase, significantly improving yield and tensile strength after aging. Mo contributes to solid-solution strengthening and enhances mechanical performance over a range of temperatures. In practice, 718 is designed for “maximum strength + industrial controllability.”

Mechanical Properties Comparison

At room temperature, Inconel 718 generally exhibits significantly higher strength than Nimonic 80A. This is critical for applications such as fasteners, load-bearing connectors, flanges, or high-strength shafts. In our bar supply experience, once high yield strength becomes a requirement, customers usually lean toward 718.

Grade Yield Strength (Approx.) Tensile Strength (Approx.)
Nimonic 80A ~600–800 MPa ~900–1100 MPa
Inconel 718 >1000 MPa ~1200–1400 MPa

However, at elevated temperatures, room-temperature data alone is not sufficient. Above 650°C, 80A demonstrates superior strength retention and microstructural stability, especially in creep and stress rupture conditions. It is not a lower-grade substitute, but a material optimized for different performance priorities.

Temperature Resistance & Stability

In terms of maximum service temperature, 80A generally has an advantage. It is commonly used around 700°C or higher for long-term applications, while 718 is typically applied below this range. Both are heat-resistant, but their long-term high-temperature stability differs.

Fabrication & Machinability

From a manufacturing perspective, neither material is easy to machine. Nickel-based alloys are prone to work hardening, have low thermal conductivity, and cause rapid tool wear. In actual quotations, material cost is only one part—machining time, tool consumption, heat treatment, and scrap risks all contribute to total cost.

Typical Applications Comparison

80A is mainly used in high-temperature applications such as turbine blades, hot-section components, and exhaust valves. In such cases, materials must maintain strength continuously at high temperatures.

718 has a much broader application range, including high-strength fasteners, turbine disks, aerospace structures, and oilfield tools, where strength, corrosion resistance, and manufacturability must all be balanced.

Nimonic 80A

Cost & Availability

In terms of cost, both materials are relatively expensive, but their pricing logic differs. 80A cost is influenced by cobalt content, while 718 is affected by niobium, molybdenum, and market demand. Generally, 718 has better market availability and price transparency, while 80A may face supply constraints in certain specifications.

Grade Reference Price (Bar) Supply Characteristics
Nimonic 80A Approx. $39–$58/kg (for reference only) Some sizes require production scheduling
Inconel 718 Approx. $36–$52/kg (for reference only) More widely available in the market

From our factory’s experience, 718 is generally easier to source in standard sizes and specifications, while 80A relies more on specialized supply chains, especially for strict quality or performance requirements.

When to Choose Nimonic 80A vs Inconel 718

If the application involves long-term service above 650°C with strict requirements for creep resistance and thermal stability, Nimonic 80A is usually the better choice.

If the project requires high-strength structural components, welding, and scalable manufacturing, Inconel 718 is often the more practical option due to its balanced performance and industrial maturity.

Key Differences at a Glance

Comparison Nimonic 80A Inconel 718
Main Advantage High-temperature stability & creep resistance High strength, fatigue resistance & manufacturability
Typical Use Hot-section, long-term service Structural and high-strength components

FAQ

Which is more expensive, Nimonic 80A Bar or Inconel 718?

It depends on specifications, order volume, heat treatment condition, and raw material market trends. Both materials have overlapping price ranges. 80A is influenced by cobalt, while 718 is affected by niobium, molybdenum, and demand. For standard sizes, 718 pricing is usually more transparent, while customized 80A orders may result in higher total procurement costs.

Why is Inconel 718 often in stock while Nimonic 80A requires lead time?

This is mainly due to market demand. 718 is widely used and commonly stocked, while 80A is more specialized, with less inventory coverage and more frequent need for production scheduling.

What technical requirements should be confirmed when purchasing bars?

At minimum: material grade, standard, size tolerance, delivery condition, heat treatment, ultrasonic testing, surface requirements, and whether high-temperature performance data is needed. For high-temperature applications, service temperature and design life must also be clearly defined to avoid mismatch between supplied material and actual service conditions.

Latest Articles

More from this category

Home Tel Mail Inquiry