

Nimonic 90 bar, designated as UNS N07090 and material number W.Nr. 2.4632, is a precipitation-hardenable nickel-chromium-cobalt superalloy strengthene…
Nimonic 90 bar, designated as UNS N07090 and material number W.Nr. 2.4632, is a precipitation-hardenable nickel-chromium-cobalt superalloy strengthened by aluminum and titanium. It is an enhanced version of Nimonic 80A, with the addition of cobalt to improve high-temperature strength and creep resistance. This bar stock form is designed for demanding service at temperatures up to approximately 920°C (1690°F) and is a critical material for machining and forging high-stress components such as turbine blades, vanes, discs, and fasteners in aerospace and industrial gas turbines.

Nimonic 90 represents an advancement in the Nimonic alloy series, offering superior high-temperature capabilities compared to Nimonic 80A. The addition of cobalt provides significant solid-solution strengthening and improves the alloy’s structural stability under prolonged thermal exposure. The bar stock achieves an excellent balance of high tensile and creep-rupture strength, good fatigue resistance, and oxidation resistance. It is a premier choice for rotating and static parts in the hot sections of gas turbine engines where reliability under extreme conditions is paramount.
The enhanced properties of Nimonic 90 bar are a result of its optimized composition, which includes cobalt for elevated temperature performance. Supplied by Shanghai NC Metal Materials Co., Ltd., the bar stock meets exacting aerospace specifications.
| Element | Percentage (%) – Typical Range | Primary Function in the Alloy |
|---|---|---|
| Nickel (Ni) | Balance (≥ 55.0) | Base element; forms the austenitic matrix and supports γ’ precipitation. |
| Chromium (Cr) | 18.0 – 21.0 | Provides excellent resistance to oxidation and hot corrosion. |
| Cobalt (Co) | 15.0 – 21.0 | Key addition; provides potent solid-solution strengthening, enhances high-temperature creep resistance, and improves microstructural stability. |
| Titanium (Ti) | 2.0 – 3.0 | Primary hardening element; combines with aluminum to form the strengthening gamma prime (γ’) phase Ni3(Al,Ti). |
| Aluminum (Al) | 1.0 – 2.0 | Co-primary hardening element; essential for γ’ formation. |
| Iron (Fe) | 3.0 max | Residual element; kept low. |
| Carbon (C) | 0.13 max | Controlled to form beneficial grain boundary carbides. |
| Manganese (Mn) | 1.0 max | Residual element. |
| Silicon (Si) | 1.0 max | Residual element. |
| Copper (Cu) | 0.2 max | Residual element. |
| Boron (B) | 0.010 max | Trace addition to strengthen grain boundaries. |
| Zirconium (Zr) | 0.15 max | Trace addition to improve creep rupture ductility. |
The mechanical properties of Nimonic 90 bar are developed through solution treatment and aging, resulting in high strength suitable for the most demanding turbine components.
Typical Value (Aged Condition)
| Mechanical Property | Typical Value (Solution Annealed) | Relevant Specification (e.g., AMS) | |
|---|---|---|---|
| Tensile Strength | ≥ 690 MPa (100 ksi) | ≥ 1000 MPa (145 ksi) | AMS 5667 (Bar), AMS 5705 (Forgings) |
| Yield Strength (0.2% Offset) | ≥ 275 MPa (40 ksi) | ≥ 620 MPa (90 ksi) | – |
| Elongation in 2 inches (50mm) | ≥ 30% | ≥ 15% | – |
| Hardness (Rockwell) | ≤ 100 HRB | 28 – 38 HRC | – |
| Creep Rupture Strength (1000h) | N/A | ≈ 200 MPa (29 ksi) at 815°C (1500°F) | – |
The physical properties of Alloy 90 are consistent with high-performance nickel-based superalloys.
Notes / Condition
| Physical Property | Value at Room Temperature (20°C / 68°F) | |
|---|---|---|
| Density | 8.19 g/cm³ (0.296 lb/in³) | – |
| Melting Range | 1320 – 1360°C (2410 – 2480°F) | – |
| Specific Heat | ≈ 460 J/kg·°C (0.110 BTU/lb·°F) | At 100°C |
| Thermal Conductivity | 11.7 W/m·K (81.1 BTU·in/hr·ft²·°F) | At 100°C |
| Mean Coefficient of Thermal Expansion | 12.8 μm/m·°C (7.1 μin/in·°F) | 20-100°C (68-212°F) |
| Electrical Resistivity | 1.25 μΩ·m (49.2 μΩ·in) | At 20°C |
| Modulus of Elasticity (Tensile) | 206 GPa (29.9 x 10^6 psi) | At 20°C |
Shanghai NC Metal Materials Co., Ltd. supplies Nimonic 90 bar primarily as forging billet and bar for high-integrity aerospace components.
| Product Form | Standard Size Range | Key Standard Specifications | Common Supply Conditions |
|---|---|---|---|
| Forging Billet / Bar Stock | 75mm (3″) to 350mm (14″) Diameter | AMS 5705 (Forgings), AMS 5667 (Bar, UNS N07090), BS HR 506, DIN 17752 (W.Nr. 2.4632) | Solution Treated (Condition A), Forged & Solution Treated |
| Round Bar (for machining) | 20mm to 150mm Diameter | AMS 5667 | Solution Treated & Aged (ready for machining) |
| Hexagonal Bar (for fasteners) | 10mm to 50mm Across Flats | AMS 5667, BS HR 506 | Solution Treated & Aged |
Machined or forged components from Nimonic 90 bar are essential in the hottest and most highly stressed parts of turbines: Aerospace Gas Turbines: High-pressure turbine blades, vanes, discs, and seals in both military and commercial jet engines. Industrial Gas Turbines: Turbine blades, discs, and bolting for land-based power generation units. High-Temperature Fasteners: Bolts, studs, and nuts used in turbine assembly and other high-temperature structures. Automotive & Racing: Turbocharger turbine wheels and components for extreme performance applications.
Nimonic 90 requires a precise heat treatment to develop its optimal high-temperature properties: Solution Treatment: Typically performed at 1080°C (1975°F), holding, followed by rapid cooling (air quench). This dissolves the γ’ forming elements and homogenizes the structure. Aging Treatment: A two-stage aging process is often used for optimal properties, e.g., 700°C for 16 hours, then air cool. This precipitates a fine, uniform dispersion of the strengthening gamma prime (γ’) phase. Bar and billet are often supplied in the solution-treated condition for subsequent forging or machining, with aging as the final step.
Machining Nimonic 90 bar is challenging and is best performed in the solution-annealed condition before final aging. It is a tough, strong alloy with a high work-hardening rate. Successful machining requires: extremely rigid machine tools; premium-grade carbide or ceramic cutting tools; low to moderate cutting speeds; consistent feed rates; and high-pressure coolant to control heat and work hardening. Machining in the fully aged condition is significantly more difficult. The alloy is forgeable within a specific temperature range (1050-1150°C) but requires careful control.
Nimonic 90 has limited weldability. Like other precipitation-hardened superalloys, it is susceptible to strain-age cracking and liquation cracking in the heat-affected zone (HAZ). Welding, if absolutely necessary, should be performed in the solution-annealed condition using matching filler metals and with strict control over heat input and interpass temperature. A full post-weld heat treatment (solution treat + age) is mandatory to restore properties, but this is often impractical. For critical rotating components like turbine blades, welding is generally avoided in favor of integral machining or casting.
The price of Nimonic 90 bar from Shanghai NC Metal Materials Co., Ltd. is significantly influenced by its high cobalt content, placing it in a higher cost category than cobalt-free grades like Nimonic 80A.
| Pricing Factor | Impact on Reference Price | Procurement Guidance |
|---|---|---|
| High Cobalt Content | The cobalt content (15-21%) is the single largest cost driver, as cobalt is a strategic and expensive metal. Price volatility in the cobalt market directly impacts the cost of Nimonic 90. | Nimonic 90 is specified where its superior high-temperature strength over 80A is required. The cost premium over 80A must be justified by performance gains in the application. |
| Aerospace Manufacturing & Certification | Material for flight-critical rotating parts (AMS 5705) involves extensive processing (VIM/VAR melting, controlled forging), 100% non-destructive testing (ultrasonic), and rigorous mechanical property validation, adding substantial cost. | Procurement is part of a qualified aerospace supply chain. Specifications, testing, and documentation requirements are fixed and non-negotiable. |
| Heat Treatment Condition | Bar supplied in the solution-treated and aged condition is more expensive due to the additional thermal processing steps. | For forging billets, the solution-treated condition is standard. For machined bar, the aged condition may be specified to save on in-house heat treating. |
| Form and Quantity | Large diameter, high-integrity forging billets are premium products. Orders are typically project-specific with long lead times and high minimum order values. | This is not a standard stock item. Engage with Shanghai NC Metal Materials Co., Ltd. early in the design and procurement cycle for critical components. |
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