Nimonic PE16 is a high-performance nickel-based superalloy that is designed for exceptional strength and oxidation resistance at elevated temperatures. It is primarily used in demanding aerospace, gas turbine, and power generation applications where components are subjected to extreme thermal and mechanical stresses. Nimonic PE16 provides excellent creep resistance, fatigue strength, and weldability, making it suitable for use in critical engine and turbine components.
Due to the precision required in manufacturing high-stress components, CNC machining services are used to produce tight-tolerance parts from Nimonic PE16. CNC machining allows manufacturers to achieve complex geometries and meet the strict performance criteria demanded by aerospace and power generation industries.
Nimonic PE16 (UNS N07016 / W.Nr. 2.4955) is designed to offer outstanding strength and oxidation resistance in high-temperature environments, with a balanced composition that provides both strength and formability.
Element | Composition Range (wt.%) | Key Role |
---|---|---|
Nickel (Ni) | 45.0–50.0 | Base matrix; provides corrosion resistance and stability at high temperatures |
Chromium (Cr) | 13.0–15.0 | Forms a stable Cr₂O₃ oxide layer to enhance oxidation resistance |
Cobalt (Co) | 10.0–12.0 | Enhances strength and thermal fatigue resistance |
Molybdenum (Mo) | 2.5–3.5 | Strengthens via solid solution hardening and increases creep resistance |
Titanium (Ti) | 3.0–4.0 | Promotes the formation of the γ′ phase, improving precipitation hardening |
Aluminum (Al) | 1.0–2.0 | Increases strength by contributing to the formation of γ′ phase |
Iron (Fe) | ≤2.0 | Residual element |
Carbon (C) | ≤0.08 | Forms carbides that enhance high-temperature strength and wear resistance |
Manganese (Mn) | ≤1.0 | Improves hot workability |
Silicon (Si) | ≤0.5 | Enhances oxidation resistance at high temperatures |
Boron (B) | ≤0.005 | Strengthens grain boundaries for improved creep resistance |
Zirconium (Zr) | ≤0.05 | Improves creep rupture strength at elevated temperatures |
Property | Value (Typical) | Test Standard/Condition |
---|---|---|
Density | 8.3 g/cm³ | ASTM B311 |
Melting Range | 1330–1370°C | ASTM E1268 |
Thermal Conductivity | 14.0 W/m·K at 100°C | ASTM E1225 |
Electrical Resistivity | 1.1 µΩ·m at 20°C | ASTM B193 |
Thermal Expansion | 13.8 µm/m·°C (20–1000°C) | ASTM E228 |
Specific Heat Capacity | 450 J/kg·K at 20°C | ASTM E1269 |
Elastic Modulus | 210 GPa at 20°C | ASTM E111 |
Property | Value (Typical) | Test Standard |
---|---|---|
Tensile Strength | 1000–1100 MPa | ASTM E8/E8M |
Yield Strength (0.2%) | 700–850 MPa | ASTM E8/E8M |
Elongation | ≥20% | ASTM E8/E8M |
Hardness | 220–250 HB | ASTM E10 |
Creep Rupture Strength | 200 MPa at 800°C (1000h) | ASTM E139 |
Fatigue Resistance | Excellent | ASTM E466 |
High-Temperature Strength Nimonic PE16 retains tensile strength above 1000 MPa at temperatures up to 800°C, making it suitable for critical components exposed to high thermal loads.
Oxidation and Corrosion Resistance Chromium and aluminum enhance the alloy’s ability to form a protective oxide layer, providing excellent oxidation resistance up to 1050°C.
Precipitation Hardening The γ′ phase formed during heat treatment increases the alloy’s strength and creep resistance, particularly under high-stress conditions.
Thermal Fatigue Resistance Nimonic PE16 maintains its structural integrity through thermal cycling, resisting cracking and deformation under fluctuating temperatures.
Weldability Its ability to be welded without significant strength loss makes Nimonic PE16 ideal for applications requiring complex shapes and repair capabilities.
High hardness and the presence of solid solution strengthening phases cause rapid tool wear and edge chipping.
Poor heat conductivity in Nimonic PE16 leads to high cutting zone temperatures, increasing the risk of thermal distortion and surface degradation.
The material’s moderate work hardening characteristics make it prone to surface hardening during machining, requiring careful tool management.
Parameter | Recommendation | Rationale |
---|---|---|
Tool Material | Carbide (K20–K30), CBN inserts for finishing | Maintains hardness at high cutting temperatures |
Coating | AlTiN or TiSiN PVD (3–5 µm) | Reduces friction and heat buildup at tool interface |
Geometry | Positive rake (6–8°), honed cutting edge (~0.05 mm) | Minimizes cutting forces and surface work hardening |
Operation | Speed (m/min) | Feed (mm/rev) | Depth of Cut (mm) | Coolant Pressure (bar) |
---|---|---|---|---|
Roughing | 12–20 | 0.10–0.20 | 2.0–3.0 | 100–120 |
Finishing | 25–35 | 0.05–0.10 | 0.3–0.8 | 120–150 |
HIP eliminates internal porosity and increases the fatigue strength of Nimonic PE16 by >25%, particularly beneficial for turbine components.
Heat Treatment involves solution treatment at ~1050°C, followed by aging at 800°C to ensure optimal γ′ phase formation for enhanced creep resistance.
Superalloy Welding offers strong, crack-free joints with minimal loss of mechanical properties in heat-affected zones, using matching composition filler materials.
TBC Coating enhances performance in turbine blades by reducing surface temperatures by up to 200°C, extending component life under high thermal loads.
EDM offers high precision in producing cooling channels and micro-features, with tolerances as tight as ±0.005 mm.
Deep Hole Drilling is essential for creating deep, high-precision cooling passages with a straightness deviation of less than 0.3 mm/m.
Material Testing includes creep, fatigue, tensile, and X-ray diffraction (XRD) testing to confirm material performance against industry standards.
Aerospace Engines: High-performance turbine blades, compressor discs, and combustion liners exposed to cyclic thermal and mechanical stresses.
Power Generation: Gas turbine blades, nozzles, and vanes in both land-based and marine power plants.
Nuclear Reactors: Critical components for pressure vessels and heat exchangers exposed to high radiation and thermal stress.
Automotive Racing Engines: Turbocharger components, exhaust systems, and heat-resistant seals in high-performance vehicles.
Industrial Heat Treatment Equipment: High-temperature furnace parts and fixtures, including expansion bellows and seals.
What is the optimal tool selection for machining Nimonic PE16, considering its thermal and work hardening properties?
How can the fatigue resistance of Nimonic PE16 parts be enhanced through post-machining treatments?
What surface modifications are recommended for Nimonic PE16 to improve its thermal cycling resistance in turbine components?
How does the machinability of Nimonic PE16 compare to other nickel alloys in terms of tool wear and cutting efficiency?
What are the recommended material testing procedures for validating the performance of Nimonic PE16 components in aerospace and energy applications?