• Huona (Shanghai) New Material Co., Ltd.
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Contact Person : Roy
Phone Number : +86 18930254719
WhatsAPP : +8618930254719

Inconel 718 UNS N07718 Nickel Alloy Sheet Plate AMS 5596 for Aerospace Gas Turbine Engine Components

Place of Origin Shanghai, China
Brand Name Huona
Certification ISO 9001:2015
Model Number GH4169
Minimum Order Quantity 100 Kilograms
Price negotiation
Packaging Details Export-grade wooden pallet with waterproof wrapping and anti-rust protection
Delivery Time 5 working days for stock, 15-25 days for production
Payment Terms T/T
Supply Ability 50000 Kilograms per Month
Product Details
Material Grade Inconel 718 / UNS N07718 / GH4169 Standard AMS 5596, ASTM B670
Heat Treatment Solution Treated Per AMS 5662 Density 8.19 G/cm³
Melting Point 1260-1336°C Size Customization
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Nickel Alloy Sheet AMS 5596

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Inconel 718 Plate Factory Supply

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GH4169 Cold Rolled Sheet MTC

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Product Description

Inconel 718 (UNS N07718 / GH4169) Nickel Alloy Sheet & Plate

We supply premium Inconel 718 nickel-chromium superalloy sheet and plate in full compliance with AMS 5596 and ASTM B670 standards. Our products undergo strict solution heat treatment per AMS 5662, ensuring excellent mechanical properties and structural integrity for demanding aerospace and high-temperature applications.


1.Chemical Composition


Ni

50.0-55.0

Cr

17.0-21.0

Fe

Bal

Nb

4.75-5.5

Mo

2.8-3.3



2. Technical  Specifications


Parameter

Specification

Max continuous Operating Temperature(℃)

650

Resisivity(Ω/cmf,20℃)

1.25

Density(g/m³)

8.19~8.24

Thermal Conductivity(KJ/m·h·℃)

40.3

Tensile strength(N/m㎡)

1240

Melting point(℃)

1260-1320

Hardness(Hv)

350-450

Elongation(%)

≥12


3. Product Features

  • Excellent High Temperature Strength: Maintains mechanical properties up to 700°C (1300°F), making it ideal for gas turbine and jet engine components.
  • Outstanding Oxidation & Corrosion Resistance: Performs reliably in harsh oxidizing and reducing environments, including chemical processing and marine applications.
  • Precipitation Hardenable: Achieves high strength through gamma prime and gamma double prime phase strengthening without pre-heat treatment distortion.
  • Weldable & Fabrication Friendly: Good weldability with both manual and automated welding processes, allowing complex part fabrication.
  • Mill Test Certificate (MTC): Every shipment includes full traceability documentation per EN 10204 3.1 or 3.2 requirements.


4. Typical Applications

  • Aerospace compressor blades, turbine discs, and structural components
  • Gas turbine hot-section parts (combustors, casings, afterburners)
  • Oil & gas downhole tools, hangers, and wellhead components
  • Nuclear reactor core components and cryogenic storage tanks
  • High-temperature fasteners, springs, and bolting for industrial furnaces


5. Why Choose Us

  • 20+ years specializing in nickel-based superalloys
  • In-house spectrographic and mechanical testing laboratory
  • Flexible order quantities: from trial samples to container loads
  • Fast global shipping via DHL, FedEx, sea freight, or air freight

Inconel 718 UNS N07718 Nickel Alloy Sheet Plate AMS 5596 for Aerospace Gas Turbine Engine Components 0Inconel 718 UNS N07718 Nickel Alloy Sheet Plate AMS 5596 for Aerospace Gas Turbine Engine Components 1Inconel 718 UNS N07718 Nickel Alloy Sheet Plate AMS 5596 for Aerospace Gas Turbine Engine Components 2

Inconel 718 UNS N07718 Nickel Alloy Sheet Plate AMS 5596 for Aerospace Gas Turbine Engine Components 3


Contact us today for a competitive quote or to discuss your specific Inconel 718 sheet and plate requirements. Our engineering team is ready to support your material selection process.