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Inconel Alloy

Inconel 718

Inconel 718 (UNS N07718)Inconel 718 (also specified as UNS N07718 / Werkstoff No. 2.4668 / NCF 718) is a precipitation-hardening nickel-iron-chromium superalloy strengthened by niobium and molybd

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Inconel 718

Inconel 718 (UNS N07718)Inconel 718 (also specified as UNS N07718 / Werkstoff No. 2.4668 / NCF 718) is a precipitation-hardening nickel-iron-chromium superalloy strengthened by niobium and molybd

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Inconel 718 (UNS N07718)

Inconel 718 (also specified as UNS N07718 / Werkstoff No. 2.4668 / NCF 718) is a precipitation-hardening nickel-iron-chromium superalloy strengthened by niobium and molybdenum. It combines very high yield, tensile and creep-rupture strength up to about 650 °C with excellent weldability (including resistance to post-weld strain-age cracking) and good corrosion resistance, making it one of the most widely used aerospace and power-generation superalloys.

Overview

  • Category: Precipitation-hardening (PH) nickel-based superalloy (Ni-Fe-Cr-Nb-Mo)
  • Standards: ASTM B637, AMS 5662, AMS 5663, AMS 5664, UNS N07718, DIN/EN 2.4668, JIS NCF 718
  • Available forms: Round bar / rod, plate, sheet, pipe & tube, wire, forgings, and custom profiles to order

Chemical Composition (wt%)

ElementNiCrFeNb+TaMoTiAlCMnSiBPS
Content 50.0–55.017.0–21.0Bal.4.75–5.50 2.8–3.30.65–1.150.20–0.80≤ 0.08 ≤ 0.35≤ 0.35≤ 0.006≤ 0.015≤ 0.015

Physical Properties

PropertyTypical Value
Densityapprox. 8.24 g/cm³
Melting range1260–1340 °C
Thermal conductivity11.4–13.8 W/(m·K) (21–982 °C)
Coefficient of thermal expansion12.3 ×10-6 /°C (21–982 °C)
Magnetic propertiesNon-magnetic

Mechanical Properties (typical, double-aged)

PropertyTypical Value
Tensile strength (room temperature)≥ 1290 MPa
Yield strength (Rp0.2, room temperature)≥ 1035 MPa
Elongation (room temperature)≥ 12 %
Hardness (after ageing)HRC 38–44
Tensile strength at 650 °C> 1000 MPa, with good creep resistance

Fabrication & Welding

  • Hot working: 980–1160 °C, followed by suitable heat treatment to relieve stresses and refine microstructure.
  • Cold working: Good cold-formability (cold forming, cold drawing), but with a relatively strong work-hardening tendency.
  • Welding: Good weldability by GTAW (TIG), electron-beam welding and laser welding. Clean the surface before welding; post-weld ageing heat treatment is recommended.

Heat Treatment

  • Solution treatment: Heat to 950–1050 °C and cool rapidly, to fully dissolve alloying elements into the matrix and obtain a uniform austenitic structure.
  • Double-ageing: Hold at 720 °C for 8 hours, furnace-cool to 620 °C, hold for a further 8 hours, then air-cool. Precipitation of gamma-prime / double-gamma-prime strengthening phases delivers final high strength and hardness.

Key Features

  • High strength below 650 °C, with excellent yield strength, tensile strength and fatigue performance;
  • Good corrosion resistance in a wide range of environments;
  • Good high-temperature oxidation resistance;
  • Readily fabricated by hot working, cold working and welding into complex components;
  • Welds retain high strength and corrosion resistance.

Corrosion Resistance

  • Good resistance to atmospheric, fresh-water and marine environments;
  • Resists a range of chemical media including nitric, sulfuric and hydrochloric acids to a limited extent;
  • Particularly good performance in neutral and mildly alkaline conditions;
  • Good resistance to pitting and crevice corrosion.

Typical Applications

  • Aerospace: high-temperature engine components such as turbine discs, blades and combustors;
  • Power generation: gas-turbine components and nuclear-reactor internals;
  • Automotive: critical components of high-performance engines;
  • Petrochemical: piping, valves and reaction vessels for high-temperature, high-pressure, corrosive service.

For detailed datasheets, mill certificates (EN 10204 3.1) or inquiries on specific sizes and tolerances, please contact our sales & engineering team.

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