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Inconel 718 B670 Plates

Inconel 718 B670 Plates
Material Grade: Inconel 718 (UNS N07718)
Standard Specification: ASTM B670 / ASME SB670
Hardening Type: Precipitation Hardenable (Age Hardening)
High-Temp Performance: High Creep-Rupture Strength up to 704°C
Metallurgical Edge: Niobium-Modified for Excellent Weldability
Corrosion Resistance: Outstanding in High-Pressure & Acidic Media
Thickness Range: 0.5 mm to 50 mm
Core Industries: Aerospace, Gas Turbines, & Cryogenic Tanks
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Inconel 718 (UNS N07718) Plates, produced under the high-precision ASTM B670 specification, represent the pinnacle of high-strength superalloys. This precipitation-hardenable nickel-chromium alloy is uniquely formulated with significant levels of iron, columbium (niobium), and molybdenum, along with lesser amounts of aluminum and titanium. Unlike many high-temperature alloys that lose their mechanical integrity under thermal stress, Inconel 718 is engineered to maintain exceptionally high yield, tensile, and creep-rupture properties at temperatures as high as 704°C (1300°F). Its metallurgy is specifically designed to allow for age-hardening without the risk of post-weld cracking, making it a reliable choice for complex structural fabrications.

The technical dominance of ASTM B670 Inconel 718 is most evident in the aerospace and energy sectors, where it serves as the backbone for gas turbine engine components, liquid-fueled rocket motors, and high-strength fasteners. Beyond its thermal capabilities, it offers excellent corrosion resistance across a broad spectrum of aggressive media, including organic and inorganic acids. It is also a preferred material for cryogenic storage tanks, as it remains ductile and prevents brittle fracture at sub-zero temperatures. Whether utilized in nuclear fuel element spacers or high-pressure pump bodies, Inconel 718 provides an unmatched combination of weldability, fabrication ease, and extreme environmental endurance.



Inconel 718 B670 Plates Features

  • » Extreme High-Temperature Strength: Designed to maintain exceptional yield and tensile strength at temperatures up to 704°C (1300°F), outperforming standard nickel alloys in thermal stress environments.
  • » Superior Creep-Rupture Properties: Engineered to resist slow deformation (creep) over long periods under high heat and pressure, a critical requirement for turbine and engine components.
  • » Unique Weldability: Niobium modification allows the alloy to be welded in the annealed or age-hardened condition without the risk of "strain-age cracking" during heating and cooling.
  • » High Fatigue Resistance: Demonstrates outstanding endurance under cyclic loading, making it ideal for rotating machinery and high-vibration aerospace applications.
  • » Cryogenic Versatility: Unlike many high-strength materials, it retains its ductility and toughness at cryogenic temperatures, preventing brittle failure in liquid gas storage.
  • » Corrosion & Oxidation Shield: Provides excellent resistance to a wide range of corrosive media and resists oxidation even under extreme thermal cycling.
  • » Age-Hardening Capability: Can be precision-hardened through heat treatment to achieve specific mechanical properties tailored to the demands of the project.
  • » Reliable Stress-Corrosion Resistance: Virtually immune to chloride-ion stress corrosion cracking, ensuring safety in high-pressure oil and gas extraction tools.

Inconel 718 B670 Plates Specification

Standards

  • ASTM Standard: B670
  • ASME Standard: SB670
  • UNS Number: N07718
  • WNR Number: 2.4668

Chemistry

  • Nickel (Ni): 50.0% – 55.0%
  • Chromium (Cr): 17.0% – 21.0%
  • Columbium (Nb): 4.75% – 5.50%
  • Molybdenum (Mo): 2.80% – 3.30%

Mechanical Data

  • Yield Strength: 1034 MPa (Min)
  • Tensile Strength: 1241 MPa (Min)
  • Elongation: 12% (Min)
  • Hardness: 36 - 44 HRC (Aged)

Physical Info

  • Max Service: 704°C (1300°F)
  • Density: 8.19 g/cm³
  • Melting Range: 1260 - 1336°C
  • Specific Heat: 435 J/kg·K

Size Range

  • Thickness: 0.5 mm to 50 mm
  • Width: Up to 2000 mm
  • Length: Up to 6000 mm
  • Condition: Solution Annealed / Aged

Quality Control

  • MTC: EN 10204 3.1
  • Testing: Creep-Rupture / Stress
  • Compliance: AMS 5596 / 5597
  • Finish: Descaled / Bright Annealed

Inconel 718 B670 Plates Detailed Specifications

Property Specification
Specification ASTM B670 / ASME SB670
Width 1000mm - 3000mm
Thickness 3mm - 100mm
Length 2000mm - 12000mm
Supply Condition Hot-Rolled, Cold-Rolled, Annealed, and as per customer requirements.
Impact Tested -196°C
Process of Manufacturing Hot-Rolled, Cold-Rolled, Annealing, Pickling, and Passivation

Inconel 718 B670 Plates Chemical Composition

Element Composition %
Nickel (Ni) 50.0 - 55.0
Chromium (Cr) 17.0 - 21.0
Iron (Fe) Balance
Niobium (Nb) + Tantalum (Ta) 4.75 - 5.50
Molybdenum (Mo) 2.80 - 3.30
Titanium (Ti) 0.65 - 1.15
Aluminum (Al) 0.20 - 0.80
Cobalt (Co) 1.0 max
Manganese (Mn) 0.35 max
Silicon (Si) 0.35 max
Carbon (C) 0.08 max
Phosphorus (P) 0.015 max
Sulfur (S) 0.015 max
Boron (B) 0.006 max

Inconel 718 B670 Plates Mechanical Properties

Property Value
Tensile Strength 135,000 psi (930 MPa) min
Yield Strength 75,000 psi (517 MPa) min
Elongation 12% (in 2 inches / 50 mm)
Hardness Rockwell C: ≤ 40
Modulus of Elasticity 200 GPa (29 x 10⁶ psi)
Poisson's Ratio 0.29
Shear Modulus 77 GPa (11.2 x 10⁶ psi)

Inconel 718 B670 Plates Equivalent Grades

Standard ASTM B670 ASME SB670 EN UNS Werkstoff Nr. ISO
Equivalent Grade Inconel 718 Inconel 718 NiCr19NbMo N07718 2.4668 NC19FeNb

Industrial Locations & Keywords

Industrial Locations & Keywords
Riyadh Industrial Cities (1st, 2nd, 3rd & Sudair)
Jeddah Industrial Cities (1st, 2nd & 3rd)
Dammam Industrial Areas (1st, 2nd & 3rd)
Jubail Industrial City
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Rabigh Industrial City
Al Khobar Industrial Area
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Madinah Industrial City
Makkah Industrial City
Taif Industrial City
Tabuk Industrial City
Jazan Industrial City
Industrial supplier in Saudi Arabia
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Flange and valve supplier Saudi Arabia
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