Monel K500 is a high-strength, precipitation-hardenable nickel-copper alloy that offers the same outstanding corrosion resistance as Monel 400, but with significantly enhanced mechanical properties. The addition of aluminum and titanium enables age hardening, increasing tensile and yield strength while maintaining resistance to chloride stress corrosion cracking and seawater environments.
Monel K500 is especially valued in CNC machining for critical parts in aerospace, marine, petroleum, and chemical processing industries. Its ability to retain strength and ductility across temperatures ranging from cryogenic to 650°C makes it a top choice for fasteners, pump shafts, and non-magnetic components operating under high stress or flow conditions.
Monel K500 (UNS N05500 / ASTM B865 / AMS 4676) is a wrought, nickel-copper-aluminum alloy strengthened through precipitation of γ′ (Ni₃(Al,Ti)) phases during aging. It is available in solution-annealed, aged, and hot-worked conditions.
Element | Composition Range (wt.%) | Key Role |
---|---|---|
Nickel (Ni) | ≥63.0 | Base element; provides corrosion resistance |
Copper (Cu) | 27.0–33.0 | Improves seawater and acid resistance |
Aluminum (Al) | 2.30–3.15 | Enables precipitation strengthening (γ′ phase) |
Titanium (Ti) | 0.35–0.85 | Enhances aging response and strength |
Iron (Fe) | ≤2.0 | Maintains toughness and cost efficiency |
Manganese (Mn) | ≤1.5 | Improves hot workability |
Silicon (Si) | ≤0.5 | Enhances oxidation resistance |
Carbon (C) | ≤0.25 | Controlled to prevent carbide precipitation |
Sulfur (S) | ≤0.01 | Reduced to avoid hot cracking and inclusion defects |
Property | Value (Typical) | Test Standard/Condition |
---|---|---|
Density | 8.44 g/cm³ | ASTM B311 |
Melting Range | 1315–1350°C | ASTM E1268 |
Thermal Conductivity | 17.0 W/m·K at 100°C | ASTM E1225 |
Electrical Resistivity | 0.43 µΩ·m at 20°C | ASTM B193 |
Thermal Expansion | 13.8 µm/m·°C (20–300°C) | ASTM E228 |
Specific Heat Capacity | 410 J/kg·K at 20°C | ASTM E1269 |
Elastic Modulus | 179 GPa at 20°C | ASTM E111 |
Property | Value (Typical) | Test Standard |
---|---|---|
Tensile Strength | 960–1100 MPa | ASTM E8/E8M |
Yield Strength (0.2%) | 690–860 MPa | ASTM E8/E8M |
Elongation | ≥20% (25mm gauge) | ASTM E8/E8M |
Hardness | 28–35 HRC | ASTM E18 |
Impact Toughness | ≥100 J at -150°C | ASTM E23 |
High Strength via Aging: Compared to Monel 400, tensile strength increases by 2× to 3× due to γ′ phase precipitation, reaching values up to 1100 MPa.
Excellent Corrosion Resistance: Maintains low corrosion rates (e.g., <0.05 mm/year) in 3.5% NaCl at 25°C and hydrofluoric acid solutions, even under flow conditions exceeding 15 m/s.
Seawater Resistance: Resists cavitation and erosion in high-velocity brine environments, ideal for marine pump impellers and shafts.
Non-Magnetic Stability: Remains essentially non-magnetic in solution-annealed condition; may show slight magnetism after aging, acceptable for most non-magnetic assemblies.
Thermal Range: Operational stability from cryogenic temperatures up to 650°C; minimal creep deformation below 0.5% strain at 450°C over 10,000 hours.
Hardness values up to 35 HRC cause flank wear and edge chipping in conventional tools, requiring premium-grade carbide inserts.
Increases local hardness by 20–30% under shallow cuts, risking tool deflection and poor surface finish if tool geometry is not optimized.
Produces continuous, adhesive chips that raise cutting zone temperatures above 600°C, especially in dry conditions, reducing tool life.
Parameter | Recommendation | Rationale |
---|---|---|
Tool Material | PVD-coated carbide (K10–K20 grade) or ceramic inserts | Maintains wear resistance at elevated temperatures |
Coating | AlTiN, TiAlN, or AlCrN (2–4 µm) | Reduces friction and thermal loading |
Geometry | Positive rake (10–12°), honed edge (~0.02 mm radius) | Reduces cutting force and chip adhesion |
Operation | Speed (m/min) | Feed (mm/rev) | DOC (mm) | Coolant Pressure (bar) |
---|---|---|---|---|
Roughing | 15–25 | 0.20–0.30 | 2.0–3.0 | 100–120 |
Finishing | 30–50 | 0.05–0.10 | 0.5–1.0 | 120–150 |
HIP eliminates internal porosity and increases fatigue strength (>20%) for high-pressure service components.
Heat Treatment includes solution annealing at 980°C ±10°C for 2 hours and aging at 595°C for 8–16 hours to achieve full precipitation hardening.
Superalloy Welding uses controlled heat input and post-weld aging to recover mechanical properties, especially for pressure-retaining parts.
TBC Coating applies up to 200 µm of YSZ ceramic for gas turbine applications, enabling service up to 1000°C on exhaust components.
EDM allows for micro-slotting and feature detailing on hardened K500 with ±0.005 mm tolerance control.
Deep Hole Drilling creates coolant or oil channels up to 50× diameter in pump shafts or marine rotors.
Material Testing includes hardness mapping, X-ray diffraction (XRD) for phase analysis, corrosion testing (ASTM G28), and tensile testing (ASTM E8).
Pump shafts, valve stems, and underwater fasteners.
Corrosion rate in seawater: <0.02 mm/year at 25°C with flow rates >10 m/s.
Non-magnetic drill collars, completion tools, and wellhead hardware.
Meets NACE MR0175 standards for H₂S service with tensile strength >960 MPa.
Actuator parts, landing gear bushings, fastening systems.
Withstands cyclic loads and vibration fatigue up to 10⁷ cycles without failure.
Corrosion-resistant seals, impellers, and HF acid-handling parts.
Maintains mechanical integrity in pH 1–13 environments at up to 150°C.
What distinguishes Monel K500 from Monel 400 in high-strength applications?
How does age hardening affect CNC machining behavior of Monel K500?
What is the typical hardness range of precipitation-hardened Monel K500?
Can Monel K500 be HIP-processed or EDM-machined without degrading properties?
What testing standards validate Monel K500 parts for offshore or aerospace use?