It is a kind of co-cr-ni solution-strengthened deformed superalloy, which is mainly used in the aerospace field in high-temperature environments. Here is a detailed analysis of the alloy:
Chemical Composition: Carbon(C): 005-0.15% - The carbon content has an impact on the strength and high temperature resistance of the alloy, and the lower carbon content helps to improve the strength and high temperature resistance.
Silicon (Si): 04% - The content of silicon is usually lower to reduce the hardness of the alloy and improve machinability.
Manganese (mn): 10-2.0% - The addition of manganese can improve the strength and corrosion resistance of the alloy.
Phosphorus (p): 004% - Phosphorus content limits help to reduce the adverse effects of impurities on alloy properties.
Sulfur (s): 003% - The limit of sulfur content helps to improve the creep and long-lasting properties of the alloy.
Chromium (Cr): 19-21% - The addition of chromium increases the high temperature oxidation resistance and corrosion resistance of the alloy.
Nickel (Ni): 9-11% - The nickel content helps to improve the strength and high temperature resistance of the alloy.
Cobalt (CO): Allowance - Cobalt is a fundamental component of this alloy and occupies the allowance of the alloy and is essential to improve its high-temperature performance.
Iron (Fe): 30% - The iron content is usually kept low to reduce the adverse effects of iron on the properties of the alloy.
Performance characteristics: density: the density of GH5605 alloy is 913 g cm, relatively tall.
Magnetic: The alloy is not magnetic, which can be important in some applications.
Temperature range: GH5605 alloy is suitable for high temperature environments below 1000 degrees Celsius and exhibits moderate durability and creep strength.
Modulus of elasticity: The modulus of elasticity varies from 231 GPA to 181 GPA at room temperature to 650 at room temperature, which indicates the stability of its mechanical properties at high temperatures.
International Corresponding Grades:
GH5605 is the new high-temperature name for this alloy.
The old name was GH605, and the two were usually equivalent.
Applications: GH5605 alloy is mainly used in the manufacture of high-temperature parts, such as aero engine guide vanes, turbine outer rings and vortex devices. In the aerospace industry, these critical components need to maintain strength and stability at high temperatures, and GH5605 alloy provides good performance to meet these requirements.
In conclusion, GH5605 alloy has specific chemical composition, performance characteristics and application fields, and is suitable for aerospace component manufacturing that requires high-temperature stability and strength. The alloy also has different names internationally, but its properties and range of applications are basically the same.