Nimonic 80A is a precipitation-hardened nickel-chromium alloy strengthened with titanium and aluminum, engineered for use in high-temperature environments where exceptional mechanical strength, creep resistance, and oxidation resistance are critical. It offers improved high-temperature strength over Nimonic 75 and maintains structural integrity in continuous service up to 815°C and intermittent exposure beyond 1000°C.
Its excellent thermal fatigue and corrosion resistance make it a preferred material for aerospace turbines, nuclear valves, high-pressure springs, and automotive turbocharger components. Components made from Nimonic 80A are frequently manufactured by forging or casting and precision-finished through CNC machining for tight-tolerance performance-critical applications.
Nimonic 80A (UNS N07080 / W.Nr. 2.4952 / ASTM B637, B408) is a gamma-prime (γ') strengthened alloy designed for high-temperature strength, oxidation resistance, and structural reliability in creep and fatigue-prone environments.
Element | Composition Range (wt.%) | Key Role |
---|---|---|
Nickel (Ni) | Balance (≥69.0) | Matrix providing oxidation resistance and thermal strength |
Chromium (Cr) | 18.0–21.0 | Forms a protective oxide scale; enhances corrosion resistance |
Titanium (Ti) | 1.8–2.7 | Precipitation hardening through γ'-Ni₃(Al,Ti) formation |
Aluminum (Al) | 1.0–1.8 | Strengthens the alloy via gamma-prime phase |
Iron (Fe) | ≤3.0 | Residual element |
Carbon (C) | ≤0.10 | Controls carbide precipitation and creep behavior |
Manganese (Mn) | ≤1.0 | Improves hot workability |
Silicon (Si) | ≤1.0 | Enhances oxidation resistance and casting properties |
Copper (Cu) | ≤0.2 | Limited to minimize hot shortness |
Sulfur (S) | ≤0.015 | Controlled to reduce hot cracking in welding |
Property | Value (Typical) | Test Standard/Condition |
---|---|---|
Density | 8.19 g/cm³ | ASTM B311 |
Melting Range | 1320–1380°C | ASTM E1268 |
Thermal Conductivity | 11.4 W/m·K at 100°C | ASTM E1225 |
Electrical Resistivity | 1.08 µΩ·m at 20°C | ASTM B193 |
Thermal Expansion | 13.3 µm/m·°C (20–1000°C) | ASTM E228 |
Specific Heat Capacity | 435 J/kg·K at 20°C | ASTM E1269 |
Elastic Modulus | 200 GPa at 20°C | ASTM E111 |
Property | Value (Typical) | Test Standard |
---|---|---|
Tensile Strength | 965–1080 MPa | ASTM E8/E8M |
Yield Strength (0.2%) | 690–760 MPa | ASTM E8/E8M |
Elongation | ≥20% | ASTM E8/E8M |
Hardness | 200–230 HB | ASTM E10 |
Creep Rupture Strength | 180 MPa at 750°C (1000h) | ASTM E139 |
Fatigue Resistance | Excellent | ASTM E466 |
High-Temperature Strength: Precipitation of Ni₃(Al,Ti) phase allows high tensile and creep strength up to 815°C in continuous service.
Oxidation Resistance: Retains mechanical properties in oxidizing environments, even with intermittent exposure above 1000°C.
Excellent Fatigue and Thermal Shock Resistance: Suitable for turbine and spring applications under cyclic thermal and mechanical stress.
Enhanced Creep and Rupture Life: Particularly suitable for bolting, valve guides, and pressure-sealing parts in turbines and reactors.
Precipitation-hardened structure increases surface hardness rapidly, causing premature tool wear and potential tolerance issues.
High-temperature strength and abrasion from intermetallic phases like γ'-Ni₃(Al,Ti) cause flank wear and crater formation in carbide tools.
Limited thermal conductivity leads to poor heat dissipation, increasing the likelihood of thermal cracking and edge deformation.
Parameter | Recommendation | Rationale |
---|---|---|
Tool Material | Fine-grain carbide (K20–K30), or CBN for finishing | High wear resistance under thermal stress |
Coating | AlTiN or TiSiN (3–5 µm PVD) | Improves tool life by resisting oxidation and adhesion |
Geometry | Positive rake, sharp cutting edge, 0.05 mm edge hone | Reduces cutting forces and prevents edge chipping |
Operation | Speed (m/min) | Feed (mm/rev) | Depth of Cut (mm) | Coolant Pressure (bar) |
---|---|---|---|---|
Roughing | 12–20 | 0.15–0.20 | 1.5–2.5 | 100–120 |
Finishing | 30–45 | 0.05–0.10 | 0.2–1.0 | 120–150 |
HIP enhances fatigue life and dimensional stability by eliminating internal porosity in cast or AM components.
Heat Treatment stabilizes the gamma-prime phase and optimizes mechanical properties for high-stress, high-temperature conditions.
Superalloy Welding using matching filler material ensures integrity in pressure-bound joints or assemblies.
TBC Coating provides protection for turbine and exhaust parts operating above 900°C.
EDM achieves sub-10 µm tolerances on heat-treated surfaces without introducing residual stresses.
Deep Hole Drilling for manufacturing internal features in bolts, springs, and fuel lines with L/D > 20:1.
Material Testing includes tensile testing, creep life, microstructure validation, and ultrasonic or penetrant inspection.
Turbine blades, combustion components, seals, and nozzle vanes operating in thermal cycling environments.
Valve spindles, control rods, and guide sleeves in reactors requiring long-term mechanical and creep stability.
Springs, brackets, and housings subjected to fluctuating thermal and mechanical loads.
Retorts, hangers, and grates exposed to oxidizing or carburizing atmospheres up to 1000°C.
What cutting tool materials and coatings are most effective for CNC machining Nimonic 80A?
How does Nimonic 80A compare to Nimonic 75 in creep resistance and tensile strength?
Can EDM be used to produce precision features in hardened Nimonic 80A components?
What are the ideal heat treatment conditions for enhancing Nimonic 80A’s gamma-prime phase?
What industries most commonly demand CNC-machined components from Nimonic 80A?