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Nickel-Chromium Precipitation Hardening AlloyUNS N07718W.Nr 2.4668

Inconel 718 (UNS N07718) Seamless Pipes & Tubes

Alloy 718 (Inconel 718, UNS N07718) is a precipitation-hardenable nickel-chromium alloy containing significant amounts of niobium and molybdenum. It possesses exceptionally high yield, tensile, and creep-rupture properties at temperatures up to 704C. Its unique age-hardening response allows it to be welded and annealed without spontaneous hardening during heating and cooling.

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Size Range

1/4" NPS to 10" NPS (6.35mm to 273.1mm OD)

Wall Thickness

SCH 5S to SCH 80S

Standards

5 specs

Chemical Composition (% by weight)

Ni50.0-55.0
Cr17.0-21.0
Nb+Ta4.75-5.50
Mo2.80-3.30
Ti0.65-1.15
Al0.20-0.80
FeRemainder
Co1.0 max
C0.08 max
Mn0.35 max
Si0.35 max

Mechanical Properties (Minimum at Room Temperature)

Tensile Strength1241 MPa min (age hardened)
Yield Strength1034 MPa min (age hardened)
Elongation12% min
Hardness36 HRC max (solution annealed)

Physical Properties - Alloy 718

Density8.19 g/cm3
Melting Range1260-1336 C
Thermal Conductivity11.4 W/m-K
Electrical Resistivity1250 nOhm-m
Specific Heat435 J/kg-K
Coeff. of Thermal Expansion13.0 um/m-C

Corrosion Resistance - Alloy 718

PropertyValue
Pitting Resistance (PREN)N/A (precipitation hardened)
Max Service Temp (Oxidizing)704 C (age-hardened service)
Intergranular CorrosionGood when properly heat treated
Stress Corrosion CrackingGood resistance
General Corrosion RateGood in mild environments
Seawater ResistanceGood

Equivalent International Grades

ASTMN07718
TradeInconel 718
AMS5662/5663
API6A718

Alloy 718 vs Comparable Grades

GradeTensileYield
Alloy 625Nickel-Chromium-Molybdenum Alloy827 MPa min414 MPa min
Alloy C-276Nickel-Molybdenum-Chromium Alloy690 MPa min283 MPa min
Alloy 825Nickel-Iron-Chromium-Molybdenum Alloy586 MPa min241 MPa min
VS
Alloy 718 vs Alloy 625: 718 has much higher strength (precipitation hardened); 625 has better corrosion resistance.
VS
Alloy 718 vs Alloy C-276: C-276 for extreme corrosion; 718 for extreme mechanical strength.
VS
Alloy 718 vs Alloy 825: 718 for high-strength high-temp; 825 for corrosion in acids.

Applicable Standards

ASTM B637 / ASME SB637ASTM B670AMS 5662 / AMS 5663API 6A718DIN 17751

Applications

Gas turbine and jet engine components
Oil & gas downhole tools and wellhead equipment
Cryogenic storage tanks
Nuclear reactor components
Aerospace fasteners and structural parts
High-strength subsea equipment

Key Advantages of Alloy 718

Highest strength of all common nickel alloys (1241 MPa tensile)
Excellent weldability for a precipitation-hardened alloy
Outstanding mechanical properties at cryogenic to 704C
Slow age-hardening response simplifies welding and fabrication
API 6A718 approved for critical oil & gas wellhead equipment
Excellent fatigue and creep-rupture properties

Alloy 718 Applications by Region

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Middle East (UAE, Saudi Arabia, Qatar, Oman, Kuwait)

Used in critical oil & gas wellhead equipment, subsea tools, and downhole components across UAE, Saudi Arabia, Qatar, and Oman.

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Europe (Germany, UK, Norway, Netherlands, Italy)

Aerospace-standard alloy in UK, France, and Germany. Also used in North Sea oil & gas wellhead equipment.

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United States

Primary alloy for aerospace engine components, oil & gas downhole tools, and nuclear applications.

Frequently Asked Questions about Alloy 718 Seamless Pipes

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Stancor is India's leading manufacturer of Alloy 718 seamless pipes, exporting to UAE, Saudi Arabia, Qatar, Germany, UK, and USA. Contact our sales team for competitive pricing, fast delivery, and full material certification.

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