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Model No: Inconel 625 Tube
AMS 5581 / Inconel 625 Nickel Alloy Tube
AMS 5581 Inconel 625 tube is typically used for parts primarily requiring corrosion or oxidation resistance at temperatures up to 1800 ° F. It is non-magnetic at room temperature. The material is in the form of Seamless or Welded Tubing in the solution heat treated (annealed) condition.
Delivery :
FOB
minimum order :
100 kilograms
Supply Ability :
5000Tonkilograms / Month
Stock Time :
7-10Day
Country of Origin :
CHINA
Quantity :
AMS 5581 is the aerospace material standard. This specification covers a corrosion and heat-resistant nickel alloy in the form of two types of tubing.
AMS 5581 Inconel 625 tube is typically used for parts primarily requiring corrosion or oxidation resistance at temperatures up to 1800 ° F.
It is non-magnetic at room temperature. Material is in the form of Seamless or Welded Tubing in the solution heat treated (annealed) condition. Room temperature yield strength is 60,000 psi minimum and tensile strength 120,000 minimum.
Chemical Composition
| Weight % | Ni | Cr | Mo | Nb + Ta | Fe | Ti | C | Mn | Si | S | P | Al | Co |
| Alloy 625 | 58.0 min | 20 - 23 | 8 -10 | 3.15 -4.15 | 5.0 max | 0.40 max | 0.10 max | 0.50 max | 0.50 max | 0.15 max | 0.15 max | 0.40 max | 1.0 max |
Mechanical Properties
| Material | Form and Condition | Tensile Strength MPa | Yield Strength (0.2% Offset) MPa | Elongation 4D(%) | Hardness HB | ||
| Ksi | MPa | Ksi | MPa | ||||
| Alloy 625 Tube Seamless and Welded | Annealed | 120 | 827 | 60 | 414 | 35 | - |
Applications
Aircraft engine components, including turbine blades, turbine discs, gas turbine blades, and other components
Combustion chamber of aerospace engine. It can withstand high-temperature and high-pressure combustion environments in the combustion chamber, ensuring stable operation of the combustion chamber.
Aerospace propulsion system: It can be used to manufacture key components of propulsion systems, such as jet engines and rocket engines, ensuring the efficient and stable operation of the propulsion system.
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