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Incoloy A-286 Uns S66286 W. Nr. 1.4980 (GH2132) Rod Incoloy A286 Round Bar

Place of Origin CHINA
Nombre de la marca HUONA
Certificación ISO9001
Model Number Incoloy A-286
Minimum Order Quantity 10
Precio DISCUSS
Packaging Details Carton or Wooden Case
Delivery Time 7-21 DAYS
Payment Terms L/C,T/T,Western Union,MoneyGram
Supply Ability 1000kg Per Week

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Datos del producto
Electrical Resistivity 0.8 μΩm Grade Incoloy A-286
Corrosion Resistance Excellent Melting Process Vim + ESR Melting Techniques
Coefficient Of Expansion 5.0 × 10⁻⁶ /°C (30–400°C~) Customized Service Support
Product Usage Heating element for furnace Density 8.1 g/cm3
Resaltar

Incoloy A286 round bar

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Incoloy A286 rod

,

Inconel alloy A286 bar

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Descripción de producto
Incoloy A-286 Uns S66286 W. Nr. 1.4980 (GH2132) Rod Incoloy A286 Round Bar
Product Attributes
Attribute Value
Electrical Resistivity 0.8 μΩm
Grade Incoloy A-286
Corrosion Resistance Excellent
Melting Process Vim + ESR Melting Techniques
Coefficient Of Expansion 5.0 × 10⁻⁶ /°C (30–400°C~)
Customized Service Support
Product Usage Heating element for furnace
Density 8.1 g/cm3
Product Description

Super alloy A-286 (UNS S66286, W. Nr.1.4980, GH2132) is an iron-based high temperature and high strength alloy. A-286 is designed for applications requiring high strength and good corrosion resistance at temperatures up to 1300 °F (704 °C). This alloy offers high ductility in notched sections. In fact, the notched rupture strength of alloy A-286 is superior to many other commercial alloys with comparable high temperature properties.

An advantage of this alloy is that it can be precipitation hardened and strengthened by heat treatments. This makes possible a high degree of uniformity in developing maximum strength, which can be duplicated application after application.

Super alloy A-286 is used in gas turbine forgings, fasteners, superchargers, cryogenic equipment, missile components, corrosive deep well hardware and jet engines.

Limiting Chemical Composition (%)

Iron: Balance, Nickel: 24.00-27.00, Chromium: 13.50-16.00, Titanium: 1.90-2.30, Molybdenum: 1.00-1.75, Manganese: 2.00 max., Silicon: 1.00 max., Vanadium: 0.10-0.50, Aluminum: 0.35 max., Carbon: 0.08 max, Phosphorous: 0.015 max., Sulfur: 0.002 max., Boron: 0.003-0.01

Physical Properties:
  • Density: 7.94g/cm³
  • Melting Point: 1370ºC-1430ºC
  • Specific Heat: 419 J/kg K
  • Electrical Resistivity: 91 J/kg K
  • Can be produced by AOD refining or vacuum induction melting
  • Iron-base superalloy
  • High strength and corrosion resistance up to 1300°F (704°C)
Application:
  • Aircraft and industrial gas turbine components
  • Fasteners
  • Springs
  • After Burner Parts
  • Industrial Gas Turbines
  • Moderate Corrosion Applications in Aqueous Solutions
  • Non-Magnetic Cryogenic Equipment
Typical Mechanical Properties
Material TempºC Yield Strength 0.2% min. (mpa) Tensile Strength min. (mpa) Elongation % min.
Forging Bar RT 680 950 28