Changzhou Victory Technology Co., Ltd victory@dlx-alloy.com 86-199-06119641
Product Details
Place of Origin: China
Brand Name: Victory
Certification: ISO 9001
Model Number: A-286
Document: Product Brochure PDF
Payment & Shipping Terms
Minimum Order Quantity: 15
Packaging Details: Spool package with Carton box, Coil package with polybag
Delivery Time: 5-21 days
Payment Terms: L/C, T/T, Western Union, MoneyGram
Supply Ability: 300 tons per month
Product Name: |
A-286 |
Material: |
Nickel Chromium |
Density: |
0.287 Lb/in3, (7.94 G/cm3) |
Modulus Of Elasticity (E):: |
At 70°F (20°C): 28.8 X 103 Ksi (199 GPa) |
Modulus Of Rigidity (G):: |
At 70°F (20°C): 11.2 X 103 Ksi (77.0 GPa) |
Electrical Resistivity: |
35.8 µΩ.in, (91 µΩ.cm) |
Thermal Conductivity: |
88 Btu-in/ft2hr-°F, (12.7 W/m-K) |
Product Name: |
A-286 |
Material: |
Nickel Chromium |
Density: |
0.287 Lb/in3, (7.94 G/cm3) |
Modulus Of Elasticity (E):: |
At 70°F (20°C): 28.8 X 103 Ksi (199 GPa) |
Modulus Of Rigidity (G):: |
At 70°F (20°C): 11.2 X 103 Ksi (77.0 GPa) |
Electrical Resistivity: |
35.8 µΩ.in, (91 µΩ.cm) |
Thermal Conductivity: |
88 Btu-in/ft2hr-°F, (12.7 W/m-K) |
Incoloy® alloy A-286 is an age-hardenable Iron-Nickel-Chromium alloy with high strength and corrosion resistance at elevated temperatures. Incoloy® A-286 can operate from cryogenic temperatures up to 750°F. This age hardenable, Iron-Nickel-Chromium alloy is designed for applications requiring high strength and good corrosion resistance at temperatures up to 700°C (1290°F). Incoloy® A286’s strength makes it ideal for various components as part of aircraft and industrial gas turbines. The alloy is also used in the offshore oil and gas industry, and for fastener applications in automotive engine and manifold components that are exposed to high levels of heat and stress.
Alloy A286 is an iron base, age-hardenable superalloy useful for applications requiring high strength and corrosion resistance up to 1300°F (704°C) and for lower stress applications at higher temperatures. The alloy is also used for low temperature applications requiring a ductile, non-magnetic high strength material at temperatures ranging from above room temperature down to at least -320°F (-196°C).
APPLICATIONS
| Element | Min % | Max % |
|---|---|---|
| C | 0.03 | 0.08 |
| Mn | 1.00 | 2.00 |
| Si | – | 0.50 |
| P | – | 0.02 |
| S | – | 0.015 |
| Cr | 13.50 | 16.00 |
| Ni | 24.00 | 27.00 |
| Mo | 1.00 | 1.50 |
| Ti | 1.90 | 2.30 |
| B | 0.003 | 0.01 |
| V | 0.10 | 0.50 |
| Co | – | 1.00 |
| Al | – | 0.35 |
| Cu | – | 0.50 |
| Pb | – | 0.005 |
| Fe | Bal |
