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Inconel X-750 bar manufacturer and supplier price depends on nickel and chromium raw material cost, titanium and aluminum strengthening elements, bar ...
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 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.

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

| 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.
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 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 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 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 |
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.
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.
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}
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 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.
| 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 |
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 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}
| 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 |
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 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.
| 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 |
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.
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.
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.
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.
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.
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.
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 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.
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.
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