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The nickel-chromium alloy Nimonic is offered in a couple of different grades at Kanakratna Steelage. Kanakratna has a reputation for providing their clients with hard-to-find specialty metals, so if you don’t see it on their website, that doesn’t mean they can’t get it for you.
Due to its ability to withstand very high temperatures, Nimonic is ideal for use in aircraft parts and gas turbine components. It is commonly found in the exhaust nozzles on jet engines, for instance, where the pressure and heat are extreme. It is available atKanakratnain different grades including Nimonic 75 (which is used in parts like aerospace fasteners), Nimonic 80A, andNimonic 90.
As leaders in the specialty steel supply industry,Kanakratnais a great source for hard-to-find metals such as Nimonic 90. Not only do they carry Nimonic 90 (and other grades of Nimonic) in theirextensive product inventory, but they also offer it in both pre-cut and custom forged shapes and sizes. The ability to fill even the most specialized order is a big part of what sets Kanakratna Steelage a cut above the competition.
Nimonic 90 is a super alloy of nickel-chromium-cobalt, known for both its strength and its ability to withstand extremely high temperatures. Typically used in temperatures ranging from 100 degrees Celsius to +650 degrees Celsius, Nimonic 90 is a popular alloy in the aerospace and aircraft industries. It is widely used in such applications as valves in turbo motors and blades and discs in gas turbines.
Because they have both a steel service center and a custom forging company,Kanakratnacan supply their clients with virtually any form of Nimonic 90 they need. The steel service center offersNimonic 90 in pre-cut shapes such as hollow bar, round, and square, while the forging company can produce Nimonic 90 in Smls rolled rings, mandrel rings, open die, and discs, among other shapes. TheKanakratnaTeamis happy to assist with special orders that require shapes not listed on the website.
Minimum Order Quantity: 10 Kg
Product Brochure
| Thickness/Diameter | 20mm & above |
| Single Piece Length | 6 meter, 3 meter |
| Usage | Manufacturing, Construction |
| Size | 10mm to 250mm |
| Usage/Application | Manufacturing |
| Finish | Bright or Black |
| Surface Finish | Bright |
| Material | Nimonic 80A |
| Test Certificates | Available |
| Form | Round, Square, Hex (A/F), Rectangle, Billet, Ingot, Forging Etc. |
| Grade | Nimonic 80A (UNS No. N07080) Round Bars 2.4631 |
| Delivery Details | Immediately |
| Shape | Round ,Square ,Hex |
| Standard | Our Nimonic Alloy 80A Round Bars conforms to NACE MR0175/ISO 15156 |
| Tensile Strength | 145 KSI |
| CONDITION | Solution Annealed & Precipatation Treated (aged) |
| MATERIAL TESTING | - Hardness test - Hydrostatic test - Ultrasonic test - Intergranular corrosion test - Positive mater |
| Single Piece Lengh | 6 meter |
| Unit Length | 3 m |
Nimonic 80A is a nickel-chromium-based superalloy strengthened by titanium and aluminum additions. It belongs to the family of high-temperature alloys originally developed by Henry Wiggin & Co. in the UK for use in gas turbines and aerospace applications.
As a round bar product, Nimonic 80A is widely used in fasteners, turbine blades, exhaust valves, and springs where high strength, creep resistance, and oxidation resistance are required at temperatures up to 815 °C (1500 °F).
Its excellent high-temperature performance, combined with good corrosion resistance in oxidizing environments, makes Nimonic 80A a preferred alloy in jet engines, gas turbines, nuclear power, and motorsport racing applications.
Chemical Composition of Nimonic 80A
| Element | Percentage (%) |
|---|---|
| Nickel (Ni) | Balance (≥ 69%) |
| Chromium (Cr) | 18 – 21 |
| Titanium (Ti) | 1.8 – 2.7 |
| Aluminum (Al) | 1.0 – 1.8 |
| Iron (Fe) | ≤ 3.0 |
| Cobalt (Co) | ≤ 2.0 |
| Copper (Cu) | ≤ 0.2 |
| Manganese (Mn) | ≤ 1.0 |
| Silicon (Si) | ≤ 1.0 |
| Carbon (C) | 0.06 – 0.15 |
| Boron (B) | 0.001 – 0.008 |
| Zirconium (Zr) | ≤ 0.15 |
| Sulfur (S) | ≤ 0.015 |
| Property | Value (Annealed Condition) |
|---|---|
| Tensile Strength | 965 – 1250 MPa |
| Yield Strength (0.2% offset) | 600 – 850 MPa |
| Elongation | 15 – 25% |
| Hardness | 250 – 350 HB |
| Density | 8.19 g/cm³ |
| Modulus of Elasticity | ~220 GPa |
Density: 8.19 g/cm³
Melting Range: 1320 – 1365 °C
Thermal Conductivity: 11.2 W/m·K (at 100 °C)
Electrical Resistivity: 1.25 µΩ·m
Specific Heat Capacity: 460 J/kg·K
Magnetic Properties: Essentially non-magnetic
Nimonic 80A derives its strength through precipitation hardening:
Solution Treatment: 1080 °C for 8 hours, air cooling.
Aging Treatment: 700 °C for 16 hours, furnace cooling.
This results in gamma-prime (γ') precipitate formation (Ni3(Al,Ti)), which imparts creep strength and hardness.
Testing & Inspection
Mechanical Testing – Tensile, yield, elongation, hardness.
Corrosion Testing – Oxidation and SCC resistance.
Non-Destructive Testing (NDT):
Ultrasonic Testing (UT)
Radiographic Testing (RT)
Eddy Current Testing (ECT)
Metallographic Analysis – Grain size, precipitate distribution.
Chemical Analysis – Spectrographic verification.
Hydrostatic Testing – For rods used in pressurized components.
Additional Information:
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Minimum Order Quantity: 10 Piece
Product Brochure
| Size/Diameter | 0.5 inch |
| Fitting Type | Elbow |
| End Connection Type | Buttweld |
Nimonic alloys are a family of nickel-chromium-based superalloys strengthened by titanium and aluminum additions, developed originally by Henry Wiggin & Co. in the UK in the 1940s for aerospace gas turbines. These alloys, such as Nimonic 75, 80A, 90, 105, 263, are known for their ability to withstand extreme temperatures (up to 1000 °C), retain creep strength, and resist oxidation.
When manufactured into fittings—such as elbows, tees, reducers, couplings, unions, end caps, and crosses—Nimonic alloys serve as critical connectors in aerospace engines, nuclear reactors, gas turbines, chemical plants, and high-performance automotive systems.
Nimonic alloy fittings combine strength, durability, heat resistance, and corrosion resistance, making them ideal for industries where failure is not an option.
Chemical Composition (Example: Nimonic 90)| Element | % Composition |
|---|---|
| Nickel (Ni) | Balance (≥ 53%) |
| Chromium (Cr) | 18 – 21 |
| Cobalt (Co) | 15 – 21 |
| Titanium (Ti) | 2.0 – 3.0 |
| Aluminum (Al) | 1.0 – 2.0 |
| Iron (Fe) | ≤ 3.0 |
| Carbon (C) | 0.08 – 0.15 |
| Manganese (Mn) | ≤ 1.0 |
| Silicon (Si) | ≤ 1.0 |
| Copper (Cu) | ≤ 0.2 |
| Boron (B) | 0.001 – 0.02 |
| Property | Value |
|---|---|
| Tensile Strength | 1250 MPa |
| Yield Strength | 880 MPa |
| Elongation | 15 – 20% |
| Hardness | 300 HB |
| Density | 8.18 g/cm³ |
| Modulus of Elasticity | 220 GPa |
Density: ~8.2 g/cm³
Melting Range: 1320 – 1380 °C
Thermal Conductivity: 11 W/m·K
Specific Heat Capacity: 460 J/kg·K
Magnetic: Essentially non-magnetic
Solution Treatment: ~1080 °C, air cooling.
Aging: ~700–750 °C for 16 hours.
Result: Precipitation of γ’ (Ni₃(Al,Ti)) phase → creep resistance.
Additional Information:
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