GH5605 is a Co-Cr-Ni based solution-strengthened deformed superalloy with excellent properties and a wide range of applications making it ideal for high-temperature applications. The following is a comprehensive introduction to the features, performance data, application areas and chemical composition of GH5605:
Features: Excellent high-temperature performance: GH5605 alloy is suitable for the temperature range below 1000 degrees Celsius, with good high-temperature strength and long-lasting performance.
Solution strengthening: The CR and W elements in the alloy are solution strengthened to give them moderate durability and creep strength below 815 degrees Celsius.
Performance Data: Chemical Composition:
Carbon (c): 005-0.15%
Silicon (Si): 04%
Manganese (mn): 10-2.0%
Phosphorus (p): 004%
Sulfur (s): 003%
Chromium (CR): 19-21%.
Nickel (Ni): 9-11%.
Cobalt (CO): Margin.
Iron (Fe): 30%
Physical Properties: Density: 913 g/cm³
Magnetic: None. Temperature-dependent performance:
Temperature ( ) Modulus of elasticity e (gpa).
Applications: GH5605 alloy has a wide range of applications in the following fields:
Aero engine guide vanes.
Turbine outer ring. High-temperature parts such as eddy currents.
Comparison with the previous product:
gh5605 vs.GH605: GH5605 is an updated version of GH605 with better high-temperature performance and long-lasting strength, making it suitable for a wider range of high-temperature applications.
Through the introduction of GH5605, we can see that its excellent performance and diverse applications make it one of the most favored materials in the field of high temperatures.