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

Luogo di origine Shangai, Cina
Marca Huona
Certificazione ISO 9001:2015
Numero di modello GH4169
Quantità di ordine minimo 100 chilogrammi
Prezzo Negoziabile
Imballaggi particolari Pallet in legno per esportazione con rivestimento impermeabile e protezione antiruggine
Tempi di consegna 5 giorni lavorativi per stock, 15-25 giorni per produzione
Termini di pagamento T/T
Capacità di alimentazione 50000 chilogrammi al mese
Dettagli
Grado materiale Inconel 718/UNS N07718/GH4169 Standard AMS 5596, ASTM B670
Trattamento termico Soluzione trattata secondo AMS 5662 Densità 8.19 g/cm3
Punto di fusione 1260-1336°C Misurare Personalizzazione
Evidenziare

Nickel Alloy Sheet AMS 5596

,

Inconel 718 Plate Factory Supply

,

GH4169 Cold Rolled Sheet MTC

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Descrizione di prodotto

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.