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Nickel Based Weldig Wire W. Nr. 2.4856 Uns No6625 (Inconel alloy 625)
| Place of Origin | CHINA |
|---|---|
| Brand Name | HUONA |
| Certification | ISO9001 |
| Model Number | Inconel 625 |
| Minimum Order Quantity | 10KG |
| Price | 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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xProduct Details
| Model NO. | Inconel 625 | Condition | Soft Annealed |
|---|---|---|---|
| Purity | >98% | Surface | Bright |
| Certificate | ISO9001,ROHS | Trademark | HUONA |
| Type | Wire | ||
| Highlight | Inconel alloy 625 welding wire,Nickel based alloy 2.4856 wire,UNS No6625 welding wire with warranty |
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Product Description
Nickel Based Welding Wire W. Nr. 2.4856 Uns No6625 (Inconel Alloy 625)
Product Specifications
| Attribute | Value |
|---|---|
| Model NO. | Inconel 625 |
| Condition | Soft Annealed |
| Purity | >98% |
| Surface | Bright |
| Certificate | ISO9001, ROHS |
| Trademark | HUONA |
| Type | Wire |
Product Description
Inconel is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures.
This nickel alloy is used from cryogenic temperatures up to long term service at 1200°F. One of the distinguishing features of Inconel 718's composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy's matrix and provide high strength without a strengthening heat treatment.
Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This superalloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
Application Field
High temperature components, such as:
- Turbine blades
- Guide vanes
- Turbine disks
- High pressure compressor disks
- Machine manufacturing
- Combustion chambers used in the manufacture of aviation, naval and industrial gas turbines
Material Composition Comparison
| Item | Inconel 600 | Inconel 601 | Inconel 617 | Inconel 625 | Inconel 690 | Inconel 718 | Inconel X750 | Inconel 825 |
|---|---|---|---|---|---|---|---|---|
| C | ≤0.15 | ≤0.1 | 0.05-0.15 | ≤0.08 | ≤0.05 | ≤0.08 | ≤0.08 | ≤0.05 |
| Mn | ≤1 | ≤1.5 | ≤0.5 | ≤0.35 | ≤0.5 | ≤0.35 | ≤1 | ≤1 |
| Fe | 6-10 | rest | ≤3 | rest | 7-11 | rest | 5-9 | ≥22 |
| P | ≤0.015 | ≤0.02 | ≤0.015 | -- | -- | -- | -- | -- |
| S | ≤0.015 | ≤0.015 | ≤0.015 | ≤0.015 | ≤0.015 | ≤0.01 | ≤0.01 | ≤0.03 |
| Si | ≤0.5 | ≤0.5 | ≤0.5 | ≤0.35 | ≤0.5 | ≤0.35 | ≤0.5 | ≤0.5 |
| Cu | ≤0.5 | ≤1 | -- | ≤0.3 | ≤0.5 | ≤0.3 | ≤0.5 | 1.5-3 |
| Ni | ≥7.2 | 58-63 | ≥44.5 | 50-55 | ≥58 | 50-55 | ≥70 | 38-46 |
| Co | -- | -- | 10-15 | ≤10 | -- | ≤1 | ≤1 | -- |
| Al | -- | 1-1.7 | 0.8-1.5 | ≤0.8 | -- | 0.2-0.8 | 0.4-1 | ≤0.2 |
| Ti | -- | -- | ≤0.6 | ≤1.15 | -- | -- | 2.25-2.75 | 0.6-1.2 |
| Cr | 14-17 | 21-25 | 20-24 | 17-21 | 27-31 | 17-21 | 14-17 | 19.5-23.5 |
| Nb+Ta | -- | -- | -- | 4.75-5.5 | -- | 4.75-5.5 | 0.7-1.2 | -- |
| Mo | -- | -- | 8-10 | 2.8-3.3 | -- | 2.8-3.3 | -- | 2.5-3.5 |
| B | -- | -- | ≤0.006 | -- | -- | -- | -- | -- |
Physical Properties
| Density | 8.40 g/cm³ |
| Ultimate Strength (≥ MPa) | 700 |
| Tensile Strength σb/MPa | 760 |
| Elongation δ5 (%) | 30 |
| Yield Strength σp0.2/MPa | 345 |
| Melting point | 1290-1350°C |
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