Inconel 617 is a solid-solution strengthened nickel-chromium-cobalt-molybdenum alloy engineered for high-temperature applications that demand exceptional creep resistance, thermal stability, and corrosion resistance. With operating capabilities exceeding 1000°C (1832°F), this alloy is ideal for extreme service environments such as gas turbines, petrochemical reactors, and heat exchangers in nuclear plants.
Composed primarily of Ni (44–62%), Cr (20–24%), Co (10–15%), and Mo (8–10%), Inconel 617 achieves outstanding resistance to oxidation, carburization, and various corrosive gases. Its excellent creep rupture strength and weldability make it a leading material choice for components exposed to prolonged thermal stress.
Inconel 617 (UNS N06617 / W.Nr. 2.4663) is defined under ASTM B166, B167, and B168. Its properties allow use in advanced energy and aerospace systems.
Element | Composition Range (wt.%) | Key Role |
|---|---|---|
Nickel (Ni) | 44.5 min. | Base element for corrosion resistance and strength |
Chromium (Cr) | 20.0–24.0 | Provides oxidation and corrosion resistance |
Cobalt (Co) | 10.0–15.0 | Enhances strength at elevated temperatures |
Molybdenum (Mo) | 8.0–10.0 | Increases creep strength and corrosion resistance |
Aluminum (Al) | 0.8–1.5 | Improves oxidation resistance |
Carbon (C) | 0.05–0.15 | Enhances creep rupture strength |
Iron (Fe) | ≤3.0 | Minor strengthening and cost control |
Silicon (Si) | ≤1.0 | Improves oxidation behavior |
Manganese (Mn) | ≤1.0 | Enhances hot workability |
Sulfur (S) | ≤0.015 | Controlled to prevent hot cracking |
Property | Value (Typical) | Test Standard/Condition |
|---|---|---|
Density | 8.36 g/cm³ | ASTM B311 |
Melting Range | 1330–1380°C | ASTM E1268 (DTA) |
Thermal Conductivity | 11.2 W/m·K at 100°C | ASTM E1225 |
Electrical Resistivity | 1.13 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 | 215 GPa at 20°C | ASTM E111 |
Property | Value | Test Standard |
|---|---|---|
Tensile Strength | 540–755 MPa | ASTM E8/E8M |
Yield Strength (0.2%) | 275–365 MPa | ASTM E8/E8M |
Elongation | ≥30% (50mm gauge) | ASTM E8/E8M |
Hardness | 170–210 HB | ASTM E10 |
High-Temperature Strength: Maintains tensile strength above 540 MPa at 800°C and 320 MPa at 1000°C—ideal for long-term exposure in gas turbine engines and energy reactors.
Exceptional Oxidation Resistance: Forms a stable oxide film due to the synergy of Cr, Al, and Co—withstanding temperatures up to 1100°C in air without flaking or spalling.
Creep Resistance: Withstand stresses of up to 80 MPa for 10,000 hours at 900°C, outperforming Inconel 625 and 800H in stress-rupture testing.
Corrosion Resistance: Excellent resistance to chloride pitting, carburizing gases, and reducing/oxidizing environments. Corrosion rate under 0.05 mm/year in boiling 65% HNO₃.
Strain hardening exponent ~0.4 causes rapid surface hardening.
Reduces carbide tool life to 10–20 minutes in conventional roughing.
Generates cutting temperatures exceeding 950–1050°C.
Leads to microcracking and dimensional instability.
Generates tough, continuous chips; high tool load and poor chip evacuation.
Parameter | Recommendation | Rationale |
|---|---|---|
Tool Material | PVD-coated carbide (e.g., GC4325) or ceramic | Withstands high cutting temp |
Coating | TiAlN or AlCrN (2–4µm) | Minimizes thermal and abrasive wear |
Geometry | Positive rake (6°–10°), honed edge | Lowers cutting forces |
Operation | Speed (m/min) | Feed (mm/rev) | DOC (mm) | Coolant Pressure (bar) |
|---|---|---|---|---|
Roughing | 15–25 | 0.15–0.25 | 2–3 | 80–120 |
Finishing | 30–45 | 0.05–0.10 | 0.5–1.0 | 100–150 |
TiAlN/AlCrN coatings enhance wear resistance for components operating above 900°C.
Hardness up to 3000 HV, reduces friction and diffusion wear.
Removes iron contamination after machining, improving corrosion resistance.
Critical for marine, petrochemical, and nuclear applications.
Deposits Inconel 625 or cobalt-based alloys for surface reinforcement.
Ideal for repairing wear-critical parts like turbine disks or transition ducts.
Achieves mirror-finish Ra < 0.3 µm.
Removes machining-induced microdefects for fatigue-sensitive parts.
Combustor liners, transition ducts, and turbine casings.
Withstands thermal gradients and high-cycle fatigue.
Heat exchanger tubes and superheater coils.
Tolerates radiation, steam, and high-pressure corrosive gases.
Afterburner liners, nozzle guide vanes.
Combines light weight with extreme thermal durability.