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Nimonic 75 (UNS N06075) is a nickel-chromium-based solid solution strengthened superalloy designed for high-temperature oxidation resistance and stable mechanical performance in continuous service environments up to approximately 800°C (1472°F).
It is widely used in aerospace engineering, thermal processing equipment, and industrial furnace components where resistance to oxidation, scaling, and thermal fatigue is critical.
Compared with precipitation-hardened alloys, Nimonic 75 offers:
Excellent oxidation resistance
Stable mechanical strength at elevated temperature
Good fabrication and welding properties
Reliable performance under cyclic thermal stress
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NIMONIC 75 Alloy
NIMONIC alloy 75 (UNS N06075/W.Nr. 2.4951 & 2.4630) is an 80/20 nickel-chromium alloy with controlled additions of titanium and carbon. First introduced in the 1940s for turbine blades in the prototype Whittle jet engines, it is now mostly used for sheet applications calling for oxidation and scaling resistance coupled with medium strength at high operating temperatures. It is still used in gas turbine engineering and also for industrial thermal processing, furnace components and heat-treatment equipment. It is readily fabricated and welded.
NIMONIC 75 is prized for the following combination of properties:
Excellent High-Temperature Strength: It retains a significant portion of its strength and hardness at temperatures up to approximately 815°C (1500°F). Its primary strength mechanism is solid-solution strengthening.
Outstanding Oxidation Resistance: The high chromium content (18-21%) forms a dense, adherent, and protective layer of chromium oxide (Cr₂O₃) on the surface, which prevents further oxidation and scaling at high temperatures.
Good Corrosion Resistance: Resists a wide variety of corrosive environments, including many acids and alkalis.
Good Fabricability: It can be readily forged, hot and cold worked, machined, and joined by welding and brazing.
NIMONIC 75 Alloy Chemical Composition, %:
Carbon ........................................................................0.08-0.15
Chromium....................................................................18.0-21.0
Copper..........................................................................0.5 max.
Iron................................................................................5.0 max.
Manganese ...................................................................1.0 max.
Silicon ...........................................................................1.0 max.
Titanium...........................................................................0.2-0.6
Nickel............................................................................Balance
Mechanical & Thermal Properties
| Property | Value |
|---|---|
| Density | 8.37 g/cm³ |
| Melting Range | 1340 – 1380°C |
| Max Service Temperature | ~800°C |
| Tensile Strength | 750–950 MPa |
| Hardness | ~200–250 HV |
| Oxidation Resistance | Excellent |
Heat-Treatment
For bar 30-60 minutes at 1050°C (1920°F) followed by air cooling.
For sheet 5-10 minutes at 1050°C (1920°F) followed by air cooling or, before welding, 5-10 min/1050°C (1920°F)/AC + an optional 10 min/1050°C (1920°F)/AC.
Hot Working
NIMONIC alloy 75 can be hot worked in the range 1220- 950°C (2230-1740°F).
Cold Working
The good ductility and malleability of annealed NIMONIC alloy 75 make it amenable to many methods of cold deformation. The alloy is subject to rapid strain hardening. Because of this increased strength, large reductions can be made without rupture.
Available Products and Specifications
NIMONIC alloy 75 is designated as UNS N06075 and Werkstoff Numbers 2.4951 and 2.4630. Other designations include AFNOR NC20T, AICMA Ni-P91HT and DIN NiCr20Ti. Alloy 75 is available as sheet, strip, plate, round bar, forging stock, wire, tube and extruded section.
Rod, Bar, Wire and Forging Stock - BS HR 5, BS HR 504, DIN 17752, AECMA PrEN2306, AECMA PrEN2307, AECMA PrEN2402, ISO 9723-25
Plate, Sheet and Strip - BS HR 203, DIN 17750, AECMA PrEN2293, AECMA PrEN2302, AECMA PrEN2411, ISO 6208
Pipe and Tube - BS HR 403, DIN 17751, AECMA PrEN2294, ISO 6207
Other Product Forms - DIN 17742, AECMA PrEN2308
Applications
NIMONIC 75's properties make it ideal for high-stress, high-temperature components, particularly in the aerospace and power generation industries.
Aerospace & Gas Turbines:
Turbine Blades and Vanes (in early jet engines)
Combustion Chambers and Liners
Exhaust Systems
Afterburner components
Turbine Disks
Power Generation:
Gas turbine components
Heat treatment fixtures and baskets
Nuclear engineering components
Other Industrial Applications:
Fasteners and bolts for high-temperature service
Springs (when high-temperature performance is needed)
Hot-working tools and dies
Chemical processing equipment
Nimonic 75 vs Other High-Temperature Alloys
| Property / Alloy | Nimonic 75 | Nimonic 80A | Inconel 600 | Hastelloy X |
|---|---|---|---|---|
| Base System | Ni-Cr | Ni-Cr-Ti-Al | Ni-Cr-Fe | Ni-Cr-Fe-Mo |
| Strength at 800°C | Medium | High | Medium | High |
| Oxidation Resistance | High | Very High | High | Very High |
| Creep Resistance | Medium | High | Medium | High |
| Weldability | Good | Moderate | Excellent | Good |
| Cost Level | Medium | High | Medium | High |
| Main Advantage | Stability + oxidation resistance | Highest strength | General-purpose | Extreme high-temp resistance |
Nimonic 75 → best for stable oxidation resistance applications
Nimonic 80A → better for load-bearing turbine parts
Inconel 600 → best for general corrosion + fabrication
Hastelloy X → best for extreme high-temperature aerospace use
👉 This makes Nimonic 75 a balanced cost-performance solution for industrial furnace and aerospace secondary components.
Advantages of Nimonic 75 Alloy
Excellent oxidation resistance up to 800°C
Stable mechanical properties under thermal cycling
Good weldability and machinability
Reliable long-term service performance
Cost-effective compared to higher-grade superalloys
Fabrication & Processing Guide
Welding
TIG welding recommended
Pre-cleaning required to avoid oxidation
Post-weld stress relief recommended
Heat Treatment
Solution treatment improves stability
Controlled cooling prevents grain boundary oxidation
Machining
Requires carbide tooling
Low cutting speed recommended
Coolant essential to avoid work hardening
FAQ
Q1: What is Nimonic 75 alloy used for?
Nimonic 75 is mainly used in aerospace gas turbines, industrial furnace components, heat treatment fixtures, and high-temperature mechanical parts where oxidation resistance is required.
Q2: What is the maximum service temperature of Nimonic 75?
Nimonic 75 can operate continuously at temperatures up to approximately 800°C (1472°F) while maintaining stable mechanical properties.
Q3: Is Nimonic 75 resistant to oxidation?
Yes. Due to its high chromium content, Nimonic 75 offers excellent resistance to oxidation and scaling in high-temperature environments.
Q4: How does Nimonic 75 compare with Inconel 600?
Nimonic 75 provides better high-temperature stability and oxidation resistance, while Inconel 600 offers better general corrosion resistance and easier fabrication.
Q5: Can Nimonic 75 be welded?
Yes, it has good weldability. TIG welding is commonly recommended with proper surface cleaning and post-weld treatment.
Q6: What industries use Nimonic 75 most?
It is widely used in:
Aerospace engineering
Power generation turbines
Heat treatment industry
Industrial furnace manufacturing
Q7: What are the key advantages of Nimonic 75?
High-temperature oxidation resistance
Stable mechanical strength at elevated temperature
Good fabrication and welding performance
Reliable long-term service life
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