why we choose inconel material
Thermal expansion:
Inconel alloys have a relatively low coefficient of thermal expansion, which means they undergo minimal dimensional changes when exposed to temperature fluctuations.
This is important in applications where thermal cycling is common, as it helps to maintain the integrity of the overall system.
Oxidation resistance:
Inconel alloys form a protective oxide layer that helps to resist high-temperature oxidation, making them ideal for use in environments with high oxygen content.
This property is essential in applications like jet engines, where the materials are exposed to high-temperature, oxygen-rich environments.
Compatibility with other materials:
Inconel alloys can be easily welded, brazed, or joined with other materials, such as stainless steel, making them versatile for a wide range of applications.
How to use inconel wire to make mesh
Inconel is a nickel-based alloy that is known for its high-temperature resistance and corrosion resistance. The general steps to manufacture Inconel meshes are as follows:
Select the appropriate Inconel wire size. The wire diameter, strength, and flexibility will affect the final performance of the mesh. Typically, Inconel wires with a diameter of 0.1-0.5 mm are used.
Design the structure and dimensions of the mesh. Determine the required aperture size, density, and strength based on your application needs.
Use a mesh weaving or braiding machine to fabricate the mesh. Both manual weaving and mechanical braiding methods can be used. Pay attention to maintaining uniform tension in the wires during the weaving process.
Perform heat treatment and surface treatment on the woven mesh. Heat treatment can improve the strength and high-temperature resistance of the Inconel mesh. Surface treatment can enhance the appearance and corrosion resistance.
Inspect the quality and dimensions of the mesh to ensure they meet the requirements. Tensile strength and aperture size tests can be conducted.
Parameter:
Chemical Properties of Inconel 600
| C | Cr | Ni+Co | Al | Ti | Fe | Nb+Ta | Mn | Si | P | S | Cu |
| ≤0.15 | 14.0～17.0 | ≥72 | ≤0.35 | ≤0.50 | 6.0～10.0 | ≤1.0 | ≤1.0 | ≤0.5 | ≤0.04 | ≤0.015 | ≤0.5 |
| ITEM | θ/℃ | TENSIE STRENGTH | HBS |
| σb/MPa | σP0.2/MPa | δ5/% | φ/% |
| BAR/ROD | 20 | ≥585 | ≥240 | ≥30 | - | 134～217 |
| RING | 20 | ≥520 | ≥205 | ≥35 | - | ≥187 |
| HOT ROLL PLATE | 20 | ≥550 | ≥240 | ≥35 | ≥40 | - |
| 900 | ≥95 | ≥45 | ≥40 | ≥50 | - |
| COLD ROLLED SHEET | 20 | ≥550 | ≥240 | ≥30 | - | - |
| 900 | ≥90 | ≥40 | ≥60 | - | - |
| COLD ROLLED SHEET | 20 | ≥550 | ≥200 | ≥30 | - | - |
| STRIP | 20 | ≥550 | ≥240 | ≥30 | - | - |
| WIRE | 20 | | | | - | HV≤151 |
| Shape | Size(mm) |
| WIre | 0.5-7.5 |
| Rod/Bar | 8.0-200 |
| Strip | (0.5-2.5)*(5-180) |
| Tube | custom made |
| Plate | custom made |
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High Temperature Nickel Alloy Inconel 600 718 625 Wireused In The Aerospace Industries Images
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