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 75 bar chemical composition

2026-05-28
Table of Contents Hide

Nimonic 75 bar is a nickel-chromium heat-resistant alloy bar mainly composed of nickel and chromium, with controlled additions of titanium and carbon. It is commonly identified as UNS N06075, W.Nr. 2.4951, W.Nr. 2.4630, and NiCr20Ti. The chemical composition of Nimonic 75 bar is designed to provide strong oxidation resistance, scaling resistance, good thermal stability, and useful high-temperature strength in low-stress hot-service applications. Unlike Nimonic 80A, Nimonic 75 is not mainly selected as an age-hardenable high-strength alloy. It is more often used where resistance to heat, oxidation, hot gas exposure, and scaling is required, such as furnace parts, gas turbine sheet and bar components, heat treatment fixtures, exhaust-related parts, and industrial high-temperature hardware.

Nimonic 75 Bar Chemical Composition Overview

Nimonic 75 bar belongs to the nickel-chromium alloy family. Its composition is relatively simple compared with age-hardenable superalloys such as Nimonic 80A, Nimonic 90, or Nimonic 263. The alloy is mainly based on nickel and chromium. Nickel provides the base matrix and high-temperature stability, while chromium provides oxidation and scaling resistance. Titanium and carbon are controlled additions that support strength and metallurgical stability.

For buyers and engineers, Nimonic 75 bar chemical composition should be checked carefully because material names alone are not enough. Nimonic 75, Nimonic 80A, Nimonic 90, Inconel 600, and other nickel alloy bars may look similar before machining, but their chemical composition and final performance are different. A correct Nimonic 75 bar order should clearly state the grade, UNS number, standard, bar size, surface condition, heat number, and MTC requirement.

Nimonic 75 bar

Basic Composition Identity

Item Nimonic 75 Bar Information
Common Name Nimonic 75 / Alloy 75
UNS Designation UNS N06075
Werkstoff Number 2.4951 / 2.4630
EN-style Designation NiCr20Ti
Main Alloy System Nickel-Chromium-Titanium
Main Composition Feature Nickel base with about 20% chromium and controlled titanium and carbon

Why Composition Matters

Nimonic 75 bar is selected mainly for heat resistance and oxidation resistance. If chromium is too low, oxidation resistance may be affected. If titanium, carbon, sulfur, or other controlled elements are outside specification, hot workability, weldability, mechanical stability, or surface quality may be affected. This is why the MTC should be reviewed before accepting Nimonic 75 bar for high-temperature service.

Nimonic 75 UNS N06075 Grade Identification

UNS N06075 is the unified designation for Nimonic 75. In international purchasing, this UNS number helps identify the correct nickel alloy grade across different naming systems, supplier catalogs, and material certificates. When a buyer requests Nimonic 75 bar, the MTC should show UNS N06075 or an equivalent recognized designation.

This is especially important because Nimonic grades are easy to confuse. Nimonic 75 is different from Nimonic 80A, Nimonic 90, and Nimonic 263. Nimonic 75 is a nickel-chromium alloy with controlled titanium and carbon, while Nimonic 80A is an age-hardenable nickel-chromium alloy strengthened by titanium, aluminum, and carbon. Nimonic 90 contains significant cobalt and is used for higher-strength hot-service applications.

Grade Identification Table

Identification Item Nimonic 75 Bar
Common Name Nimonic 75 / Alloy 75
UNS Number UNS N06075
Material Family Nickel-chromium heat-resistant alloy
Main Performance Oxidation resistance, scaling resistance, heat resistance, good fabrication
Typical Use Direction Gas turbine parts, furnace components, heat treatment equipment, hot gas parts

How to Avoid Grade Mix-Up

Before accepting Nimonic 75 bar, buyers should check the MTC, bar marking, product label, and packing list. The grade should be shown as Nimonic 75, Alloy 75, UNS N06075, W.Nr. 2.4951, W.Nr. 2.4630, or NiCr20Ti. If the document only says “Nimonic bar” or “nickel alloy bar,” it is not enough for reliable material identification.

Nimonic 75 W.Nr. 2.4951 / 2.4630 and NiCr20Ti Designations

Nimonic 75 is also commonly associated with W.Nr. 2.4951, W.Nr. 2.4630, and NiCr20Ti. These designations are often seen in European material documents, supplier stock lists, and technical drawings. For buyers sourcing from different countries, understanding these equivalent names helps reduce confusion during quotation and inspection.

Equivalent Designation Table

Designation Meaning Buying Note
Nimonic 75 Common trade-name style alloy name Widely used in technical and commercial documents
Alloy 75 Generic alloy name Often used by suppliers and distributors
UNS N06075 Unified material designation Useful for international grade confirmation
W.Nr. 2.4951 European Werkstoff number Common in European material documents
W.Nr. 2.4630 Alternative Werkstoff reference May appear in data sheets and older specifications
NiCr20Ti Nickel-chromium-titanium designation Describes the alloy by main elements

What NiCr20Ti Means

NiCr20Ti means the alloy is nickel-based, contains around 20% chromium, and has titanium addition. This designation helps explain the material type, but it should not replace full MTC verification. Buyers should still check chemical composition, heat number, standard, and inspection documents before accepting the bar.

Nickel Content in Nimonic 75 Bar

Nickel is the base element in Nimonic 75 bar. The alloy is often described as an 80/20 nickel-chromium alloy, meaning it is primarily nickel with about 20% chromium. Nickel provides the matrix structure, high-temperature stability, ductility, and general corrosion resistance.

Role of Nickel Matrix

The nickel matrix allows Nimonic 75 to maintain stable behavior at elevated temperature. Nickel-based alloys are commonly used in heat-resistant applications because nickel can retain useful strength and stability where many steels lose performance. In Nimonic 75, nickel also supports good fabrication and forming behavior compared with some more heavily strengthened superalloys.

Nickel and Hot-Service Stability

Nickel helps the alloy resist structural degradation during thermal exposure. This is important for furnace fixtures, turbine sheet and bar components, hot gas parts, and industrial heat treatment equipment. However, nickel alone is not enough for oxidation resistance; chromium plays the main role in protecting the surface from scaling.

Nickel and Cost

Because Nimonic 75 contains a high nickel content, its price is strongly affected by nickel market movement. It is usually more expensive than common stainless steel and many iron-based heat-resistant alloys. Buyers choose Nimonic 75 when the temperature and oxidation environment justify the use of a nickel-based alloy.

Chromium Content and Oxidation Resistance

Chromium is the most important element for oxidation resistance in Nimonic 75 bar. The chromium content is commonly around 18.0% to 21.0%. This chromium level helps form a protective oxide scale on the alloy surface when exposed to high-temperature air or hot gas environments.

How Chromium Improves Oxidation Resistance

At elevated temperature, chromium helps develop a stable oxide layer that slows further oxidation. This is why Nimonic 75 is often selected for components exposed to hot air, combustion products, furnace atmospheres, and gas turbine environments. Without enough chromium, the alloy would be less resistant to scaling and surface degradation.

Scaling Resistance

Scaling resistance is the ability of a material to resist surface oxide growth and flaking at high temperature. Nimonic 75 has strong scaling resistance in oxidizing atmospheres. Some public material data also describes NiCr20Ti / Alloy 75 as scaling resistant up to approximately 1100–1150°C in air, although the actual application limit depends on stress, atmosphere, and component design. :contentReference[oaicite:1]{index=1}

Chromium and Service Environment

Chromium is very useful in oxidizing atmospheres, but Nimonic 75 should still be evaluated carefully in carburizing, sulfur-bearing, or highly contaminated furnace atmospheres. Hot corrosion depends not only on chromium content, but also on temperature, deposits, gas chemistry, thermal cycling, and exposure time.

Element Typical Content Main Function
Chromium 18.0% – 21.0% Oxidation resistance, scaling resistance, hot gas performance

Titanium and Carbon Controlled Additions

Titanium and carbon are controlled additions in Nimonic 75 bar. They are present in much smaller amounts than nickel and chromium, but they are still important for material behavior. Titanium contributes to strengthening and metallurgical stability, while carbon can influence carbide formation and high-temperature strength.

Titanium in Nimonic 75

Titanium is usually controlled at a low level. It helps improve strength and supports the alloy’s high-temperature behavior. Unlike Nimonic 80A, Nimonic 75 does not rely on a strong titanium-aluminum precipitation-hardening system. This is one of the important differences between the two alloys.

Carbon in Nimonic 75

Carbon is also controlled. It can contribute to carbide formation and support high-temperature strength, but excessive carbon may affect ductility, fabrication, and welding behavior. For hot-service bar applications, carbon should remain within the specified range shown on the MTC.

Why Controlled Additions Matter

Small elements can have large effects in high-temperature alloys. If titanium or carbon is outside the required range, the bar may not show the expected balance of oxidation resistance, strength, ductility, and fabrication behavior. This is why buyers should not focus only on nickel and chromium when checking Nimonic 75 chemical composition.

Element Typical Role Practical Meaning
Titanium Controlled strengthening addition Supports high-temperature performance and alloy stability
Carbon Controlled carbide-forming element Affects high-temperature strength and metallurgical behavior

Iron, Cobalt, Copper, Manganese, Silicon, Sulfur, and Phosphorus Limits

Besides nickel, chromium, titanium, and carbon, Nimonic 75 bar also has controlled limits for iron, cobalt, copper, manganese, silicon, sulfur, phosphorus, and other residual elements. These elements are not the main performance source of the alloy, but they affect quality, hot workability, weldability, and standard compliance.

Iron Limit

Iron may be present as a controlled element. It should remain within the required limit because excessive iron may change the alloy balance and affect performance. Nimonic 75 should not be confused with Inconel 600, which has a higher iron content and different composition balance.

Cobalt and Copper Limits

Cobalt and copper are normally controlled at limited levels. Nimonic 75 is not a cobalt-strengthened alloy like Nimonic 90, and it is not a nickel-copper alloy like Monel 400. If cobalt or copper is unusually high, the buyer should check whether the material grade is correct.

Manganese and Silicon Limits

Manganese and silicon may appear as processing-related or residual elements. They should remain within specification to maintain predictable hot workability and material quality.

Sulfur and Phosphorus Limits

Sulfur and phosphorus are important impurity elements. They should be kept low because excessive sulfur or phosphorus can reduce hot workability, weldability, ductility, and surface quality. For bar products that will be forged, rolled, machined, or welded, low impurity control is important.

Element Why It Is Controlled Possible Concern if Too High
Iron Maintains alloy balance May affect heat-resistant alloy behavior
Cobalt Controlled residual or minor element High value may indicate a different Nimonic grade
Copper Controlled residual element Should not behave like a nickel-copper alloy
Manganese Processing and metallurgical control May affect material consistency if excessive
Silicon Controlled residual and deoxidation-related element May affect oxidation and processing behavior if uncontrolled
Sulfur Kept low for hot workability May increase cracking and reduce surface quality
Phosphorus Controlled impurity May affect ductility and hot workability

Nimonic 75 Bar Chemical Composition Table

The following table gives a practical reference for Nimonic 75 bar chemical composition. Actual acceptance should always follow the required standard, customer specification, and MTC. Different standards and suppliers may show slight differences in element limits, so the purchase order requirement is the final basis for acceptance.

Nimonic 75 bar

Typical Nimonic 75 Chemical Composition

Element Typical Range / Limit Main Function
Nickel (Ni) Balance Base matrix for heat resistance, ductility, and stability
Chromium (Cr) 18.0% – 21.0% Oxidation resistance and scaling resistance
Iron (Fe) About 5.0% max, depending on specification Controlled element in alloy balance
Titanium (Ti) About 0.20% – 0.60% Controlled strengthening and stability addition
Carbon (C) About 0.08% – 0.15% Carbide behavior and high-temperature strength support
Manganese (Mn) 1.00% max Controlled minor element
Silicon (Si) 1.00% max Controlled residual and processing-related element
Copper (Cu) 0.50% max Controlled residual element
Cobalt (Co) About 5.00% max, depending on specification Controlled minor or residual element
Sulfur (S) 0.015% max Kept low for hot workability and quality
Phosphorus (P) 0.020% max Controlled impurity

This table should be used as a technical reference, not as a replacement for the material standard. For formal procurement, buyers should check whether the required standard uses the same limits and whether the actual heat analysis on the MTC meets those limits.

How Composition Supports Heat and Scaling Resistance

Nimonic 75 bar is mainly selected for heat and scaling resistance. Its nickel-chromium composition gives the alloy strong stability in oxidizing hot atmospheres. Nickel provides the high-temperature matrix, while chromium forms a protective oxide scale. This is the main reason Nimonic 75 can be used in furnace parts, hot gas components, heat treatment fixtures, and low-stress turbine-related applications.

Nickel Matrix Stability

Nickel maintains a stable matrix at high temperature. It helps the alloy resist structural degradation and retain useful ductility in hot service. This is important for parts exposed to repeated heating and cooling.

Chromium Oxide Protection

Chromium forms a protective oxide layer that slows down oxidation and scaling. This protective layer is especially useful in air, combustion gas, and oxidizing furnace atmospheres. If the atmosphere contains sulfur, carburizing gas, or aggressive deposits, actual performance should be reviewed carefully.

Titanium and Carbon Support

Titanium and carbon help the alloy maintain useful strength and metallurgical stability. They are not present at the same strengthening level as Nimonic 80A, but they still contribute to the overall heat-resistant behavior of Nimonic 75.

Composition Factor Heat / Scaling Resistance Effect
Nickel Base Supports high-temperature stability and ductility
Chromium Content Improves oxidation resistance and scaling resistance
Titanium Addition Supports strength and alloy stability
Carbon Control Influences carbide behavior and hot strength
Low Sulfur and Phosphorus Improves hot workability and fabrication quality

Chemical Composition and High-Temperature Strength

Nimonic 75 bar provides useful high-temperature strength, but it should not be treated as the same strength class as Nimonic 80A or Nimonic 90. Its chemical composition is designed more for heat resistance, oxidation resistance, and stable low-stress performance than for maximum precipitation-hardened strength.

Solution-Strengthened Behavior

Nimonic 75 is commonly described as a solution-strengthened nickel-chromium alloy with controlled additions of titanium and carbon. This means it does not rely on a strong aging response like Nimonic 80A. Its strength comes from the nickel-chromium matrix, controlled carbon and titanium, and proper processing condition.

Low-Stress High-Temperature Applications

Nimonic 75 is commonly used in low-stress high-temperature applications, especially where oxidation and scaling resistance are more important than very high creep strength. Virgamet describes Alloy N75 as used in low-stress gas turbine and industrial applications up to 650°C. :contentReference[oaicite:2]{index=2}

When Higher Strength Is Needed

If the application requires stronger age-hardened strength, better creep resistance, or high load-bearing capability at elevated temperature, Nimonic 80A, Nimonic 90, Nimonic 263, Inconel X-750, or another superalloy may be more suitable. The correct choice depends on stress, temperature, atmosphere, life requirement, and fabrication method.

Nimonic 75 Chemical Composition Compared with Nimonic 80A

Nimonic 75 and Nimonic 80A are both nickel-chromium alloys, but they are not the same material. The most important difference is that Nimonic 80A contains higher titanium and aluminum for age hardening, while Nimonic 75 has controlled titanium and carbon but is not primarily used as an age-hardenable high-strength alloy.

Main Composition Difference

Comparison Item Nimonic 75 Bar Nimonic 80A Bar
UNS Number UNS N06075 UNS N07080
Main Alloy System Ni-Cr-Ti-C Ni-Cr-Ti-Al-C
Chromium About 18.0% – 21.0% About 18.0% – 21.0%
Titanium Lower controlled addition Higher strengthening addition
Aluminum Not a main age-hardening addition Important age-hardening element
Strengthening Type Mainly solution-strengthened heat-resistant alloy Age-hardenable high-temperature alloy
Primary Selection Reason Heat and scaling resistance in lower-stress service Higher strength, creep resistance, and age-hardened performance

Practical Selection Difference

Choose Nimonic 75 when the project mainly needs oxidation resistance, scaling resistance, and stable hot-service performance in lower-stress applications. Choose Nimonic 80A when higher mechanical strength, age-hardened properties, stress relaxation resistance, or creep resistance is required. Nimonic 80A is developed for service up to about 815°C in suitable applications, while Nimonic 75 is more often used where oxidation resistance and lower-stress hot service are the main concerns. :contentReference[oaicite:3]{index=3}

Nimonic 75 Chemical Composition Compared with Inconel 600

Nimonic 75 and Inconel 600 are both nickel-chromium alloys, and both are used in heat-resistant and corrosion-resistant environments. However, their chemical compositions and design purposes are different. Nimonic 75 is an approximately 80/20 nickel-chromium alloy with controlled titanium and carbon additions. Inconel 600 is a nickel-chromium-iron alloy identified as UNS N06600 and W.Nr. 2.4816. :contentReference[oaicite:4]{index=4}

Main Composition Difference

Comparison Item Nimonic 75 Bar Inconel 600 Bar
UNS Number UNS N06075 UNS N06600
Main Alloy System Nickel-Chromium-Titanium Nickel-Chromium-Iron
Nickel Nickel base, often described as about 80/20 Ni-Cr type Nickel base with significant iron content
Chromium About 18.0% – 21.0% Chromium-bearing nickel alloy for oxidation and corrosion resistance
Titanium Controlled addition Not a main composition feature
Iron Controlled lower level Important alloy component
Main Use Direction Heat and scaling resistance, gas turbine and industrial hot parts Corrosion resistance and heat resistance in wider chemical and thermal environments

Can Inconel 600 Replace Nimonic 75?

Inconel 600 should not be treated as a direct substitute for Nimonic 75 without engineering approval. It may be suitable for some heat-resistant or corrosion-resistant applications, but its iron content, mechanical behavior, and grade specification are different. If a drawing specifies Nimonic 75 / UNS N06075, the buyer should not substitute Inconel 600 / UNS N06600 unless the design authority approves the change.

Nimonic 75 bar

Common Standards for Nimonic 75 Bar Composition

Nimonic 75 bar composition may be supplied according to different standards, customer specifications, or supplier data sheets. The correct standard depends on product form, application, country, and customer requirement. Buyers should always state the required specification before ordering.

Common Designations and Specification References

Reference Meaning for Nimonic 75 Bar
UNS N06075 Unified designation for Nimonic 75 / Alloy 75
W.Nr. 2.4951 European Werkstoff material number reference
W.Nr. 2.4630 Alternative European material number reference
NiCr20Ti European-style material designation based on main alloying elements
Customer Specification May include special composition, heat treatment, testing, marking, or document requirements

Why Standards Should Be Confirmed

Different applications may require different levels of inspection and documentation. A furnace fixture order may need standard MTC and size inspection, while a turbine-related order may require stricter traceability, original mill certificate, PMI, ultrasonic testing, or third-party inspection. A clear standard avoids misunderstanding between buyer and supplier.

How to Check Nimonic 75 Bar Chemical Composition in MTC

MTC means Material Test Certificate. For Nimonic 75 bar, the MTC is the main document used to confirm chemical composition, heat number, grade identity, standard, mechanical properties, and delivery condition. Since Nimonic 75 is used in high-temperature environments, the MTC should be reviewed carefully before machining or installation.

Check Grade Name and UNS Number

The MTC should clearly show Nimonic 75, Alloy 75, or UNS N06075. If the MTC shows UNS N07080, the material is Nimonic 80A, not Nimonic 75. If it shows UNS N06600, the material is Inconel 600, not Nimonic 75.

Check Nickel and Chromium

Nickel should appear as the balance element, and chromium should normally fall within the required range, commonly around 18.0% to 21.0%. These two elements are the foundation of Nimonic 75 heat and scaling resistance.

Check Titanium and Carbon

Titanium and carbon should be checked because they are controlled additions. They affect strength, carbide behavior, and high-temperature stability. If titanium or carbon values are missing, the buyer should request a complete chemical analysis.

Check Residual and Impurity Elements

Iron, cobalt, copper, manganese, silicon, sulfur, and phosphorus should remain within specification. Sulfur and phosphorus are especially important impurity elements because they can affect hot workability and fabrication quality.

Check Heat Number Traceability

The heat number on the MTC should match the bar marking, product label, and packing list. Heat number traceability connects the physical bar to the tested chemical analysis. For high-temperature or critical parts, this traceability is essential.

MTC Check Item What to Confirm Why It Matters
Grade Nimonic 75 / Alloy 75 Confirms material name
UNS Number UNS N06075 Confirms exact alloy designation
Equivalent Designation W.Nr. 2.4951 / 2.4630 / NiCr20Ti Helps match European drawings and specifications
Major Elements Ni balance, Cr 18.0% – 21.0% Confirms nickel-chromium heat-resistant alloy identity
Controlled Additions Ti and C within required range Affects high-temperature strength and stability
Impurities S and P within low limits Supports hot workability and quality
Traceability Heat number matches bar, label, and MTC Prevents material mix-up and supports acceptance

PMI and Full Chemical Analysis

PMI can help verify major elements such as nickel and chromium and reduce material mix-up risk. However, PMI may not accurately measure light or trace elements such as carbon, sulfur, and phosphorus. For Nimonic 75 bar chemical composition verification, PMI should support but not replace the MTC or laboratory chemical analysis when full compliance is required.

Nimonic 75 Bar Chemical Composition Related Questions

What is the composition of Nimonic 75?

Nimonic 75 is a nickel-chromium alloy with nickel as the balance element and chromium commonly around 18.0% to 21.0%. It also contains controlled additions of titanium and carbon, with limits for iron, cobalt, copper, manganese, silicon, sulfur, phosphorus, and other residual elements. The exact composition should be checked according to the required standard and the material test certificate.

Is Nimonic 75 the same as Nimonic 80A?

No, Nimonic 75 is not the same as Nimonic 80A. Nimonic 75 is mainly a nickel-chromium alloy with controlled titanium and carbon, used for heat and scaling resistance in lower-stress high-temperature service. Nimonic 80A is an age-hardenable nickel-chromium alloy strengthened by titanium, aluminum, and carbon, and is usually selected when higher strength and creep resistance are required.

What is Nimonic 75 used for?

Nimonic 75 is used for high-temperature parts requiring oxidation resistance, scaling resistance, and stable hot-service behavior. Common applications include gas turbine components, furnace parts, heat treatment fixtures, hot gas components, industrial heating equipment, sheet metal fabrications, and low-stress high-temperature hardware. Final use should be confirmed according to temperature, stress, atmosphere, and required material standard.

Latest Articles

More from this category

Home Tel Mail Inquiry