Inconel 625 is a solid-solution strengthened nickel-based superalloy known for its outstanding resistance to pitting, crevice corrosion, stress corrosion cracking, and high-temperature oxidation. With its superior strength and corrosion resistance across a wide range of extreme environments—from seawater to acidic chemical processing—the alloy performs reliably from cryogenic temperatures up to 980°C (1800°F).
The alloy’s exceptional performance comes from its carefully balanced chemistry: nickel (58% min.), chromium (20–23%), molybdenum (8–10%), and niobium (3.15–4.15%). Inconel 625 is a go-to material in aerospace, marine, chemical processing, and nuclear industries due to its unique ability to combine mechanical strength, corrosion resistance, and thermal fatigue stability.
Inconel 625 (UNS N06625 / W.Nr. 2.4856) conforms to specifications such as ASTM B443, B446, and B564 and is widely used in corrosive and high-strength industrial environments.
Element | Composition Range (wt.%) | Key Role |
---|---|---|
Nickel (Ni) | 58.0 min. | Base metal; corrosion resistance and thermal stability |
Chromium (Cr) | 20.0–23.0 | Improves oxidation and corrosion resistance |
Molybdenum (Mo) | 8.0–10.0 | Increases pitting resistance and mechanical strength |
Niobium (Nb + Ta) | 3.15–4.15 | Enhances creep and fatigue strength |
Iron (Fe) | ≤5.0 | Balance element |
Cobalt (Co) | ≤1.0 | Residual element |
Carbon (C) | ≤0.10 | Controlled to prevent carbide precipitation |
Manganese (Mn) | ≤0.50 | Improves hot workability |
Silicon (Si) | ≤0.50 | Enhances oxidation resistance |
Sulfur (S) | ≤0.015 | Minimizes cracking risk |
Property | Value (Typical) | Test Standard/Condition |
---|---|---|
Density | 8.44 g/cm³ | ASTM B311 |
Melting Range | 1290–1350°C | ASTM E1268 (DTA) |
Thermal Conductivity | 9.8 W/m·K at 100°C | ASTM E1225 |
Electrical Resistivity | 1.30 µΩ·m at 20°C | ASTM B193 |
Thermal Expansion | 12.8 µm/m·°C (20–1000°C) | ASTM E228 |
Specific Heat Capacity | 427 J/kg·K at 20°C | ASTM E1269 |
Elastic Modulus | 207 GPa at 20°C | ASTM E111 |
Property | Value | Test Standard |
---|---|---|
Tensile Strength | 827–960 MPa | ASTM E8/E8M |
Yield Strength (0.2%) | 414–517 MPa | ASTM E8/E8M |
Elongation | ≥30% (50mm gauge) | ASTM E8/E8M |
Hardness | 200–240 HB | ASTM E10 |
High-Strength Retention: Maintains tensile strength above 600 MPa at 800°C and good creep resistance up to 980°C, outperforming most stainless steels and Incoloy alloys under thermal load.
Versatile Corrosion Resistance: Resists chloride pitting (CPT > 85°C in 6% FeCl₃), sulfuric acid attack, and seawater corrosion (corrosion rate < 0.025 mm/year in ASTM G31 tests).
Oxidation Resistance: Stable oxide formation up to 1000°C in air and marine gas turbine environments, proven through cyclic oxidation per ASTM G54.
Weldability and Fabrication: Does not require post-weld heat treatment, allowing use in fabricated pressure vessels and complex assemblies.
High strain hardening index (~0.45) leads to a hardened surface layer during machining.
Increases cutting forces and tool wear if not properly managed.
Poor heat dissipation results in localized tool tip temperatures exceeding 900°C, causing thermal fatigue and crater wear.
Generates long, continuous chips with high shear strength, leading to poor chip control and potential surface galling.
Parameter | Recommendation | Rationale |
---|---|---|
Tool Material | Carbide with AlTiN or TiAlN coating | Withstands high heat and abrasion |
Coating | Thickness 2–5 µm, PVD applied | Reduces wear and thermal cracking |
Geometry | Positive rake (10°), sharp edge, honed flank | Minimizes deformation and improves finish |
Operation | Speed (m/min) | Feed (mm/rev) | DOC (mm) | Coolant Pressure (bar) |
---|---|---|---|---|
Roughing | 20–30 | 0.20–0.30 | 2.0–3.0 | 80–120 |
Finishing | 40–55 | 0.05–0.10 | 0.5–1.0 | 100–150 |
Removes free iron particles after machining and enhances pitting resistance in marine or acid environments.
Immersion in nitric acid (20–50%) or citric acid solution at 40–60°C for 30–60 minutes.
Reduces surface roughness (from Ra 1.6 µm to Ra 0.3 µm), essential for fatigue-sensitive and cleanroom-grade applications.
Adds TiN or AlCrN layer for wear-critical parts, such as turbine rings or valve components operating at 600–800°C.
Increases surface compressive strength and fatigue life, especially in dynamic stress environments such as marine propulsion.
Subsea connectors, risers, and pump shafts.
Resistant to biofouling, corrosion, and cyclic loading in seawater.
Jet engine exhaust components, heat shields, and bellows.
Performs under cyclic heating and oxidation stress.
Reactor core fasteners, steam-line bellows, and heat exchanger tubes.
Reliable under radiation and corrosive coolant flow.
Reactor vessels, expansion joints, and scrubber components.
Tolerant to mixed acid environments and chloride attack.
What are the most effective machining parameters for reducing tool wear on Inconel 625?
How does Inconel 625 resist corrosion in seawater and acidic environments?
What post-processing is recommended after CNC machining Inconel 625?
Can Inconel 625 be used in weld-intensive applications without post-weld heat treatment?
What quality control methods are used to validate Inconel 625 parts for aerospace or nuclear service?