K465 is a nickel-based superalloy known for its exceptional high-temperature strength, oxidation resistance, and fatigue resistance. It is primarily used in applications that demand reliability and performance under extreme conditions, such as in the aerospace and power generation industries.
Element | Typical Percentage | Role and Contribution |
---|---|---|
Nickel (Ni) | ~50% | Provides overall strength and high-temperature stability. |
Chromium (Cr) | ~20% | Enhances oxidation and corrosion resistance. |
Cobalt (Co) | ~18% | Improves creep resistance and high-temperature strength. |
Aluminum (Al) | ~3.5% | Improves oxidation resistance and strengthens the alloy. |
Titanium (Ti) | ~2.5% | Enhances strength through precipitation hardening. |
Molybdenum (Mo) | ~2% | Provides additional high-temperature strength and creep resistance. |
Carbon (C) | ≤ 0.10% | Increases wear resistance while maintaining ductility. |
Property | Value | Significance |
---|---|---|
Density | ~8.3 g/cm³ | Provides a balance of strength and weight for aerospace applications. |
Melting Point | ~1280–1350°C | Suitable for high-temperature environments. |
Oxidation Resistance | Excellent | Ensures durability in oxidizing atmospheres. |
Corrosion Resistance | High | Performs well in aggressive chemical environments. |
Tensile Strength | ~1000–1300 MPa | Maintains structural integrity under stress. |
Creep Resistance | Superior | Resists deformation under prolonged high-temperature stress. |
Application | Industry | Details |
---|---|---|
Turbine Blades | Aerospace, Power Generation | Performs reliably under extreme thermal and mechanical stresses. |
Combustion Chambers | Aerospace | Resists oxidation and thermal fatigue in high-temperature exhaust environments. |
Industrial Gas Turbines | Energy | Provides durability and efficiency in power generation. |
Heat Exchangers | Aerospace, Energy | Operates efficiently in high-temperature and corrosive environments. |
Specification | Details |
---|---|
Form | Castings, bars, sheets |
Purity | ≥ 99.5% (for cast form). |
Standard Compliance | AMS 5392, ASTM B637. |
Particle Size Range | N/A (Typically cast or forged). |
Advantages | Limitations |
---|---|
Outstanding high-temperature strength and oxidation resistance. | Higher cost compared to some other alloys. |
Excellent creep resistance for long-term performance. | Requires precise manufacturing techniques. |
Excellent fatigue resistance in cyclic loading conditions. | Limited machinability due to hardness. |
What is K465 alloy?
K465 is a nickel-based superalloy designed for high-temperature applications, particularly in aerospace and power generation industries.
Why is K465 used in turbine components?
Its high-temperature strength, oxidation resistance, and creep resistance make it ideal for critical components like turbine blades.
What industries benefit from K465?
K465 is widely used in aerospace and energy sectors for components that must perform reliably in extreme environments.
How does the composition of K465 enhance its performance?
The combination of nickel, chromium, cobalt, and other elements provides high strength, oxidation resistance, and excellent performance at elevated temperatures.
Can K465 withstand extreme environments?
Yes, K465 is specifically designed to perform in high-temperature, oxidizing, and corrosive environments, making it suitable for demanding engineering applications.
K465 is a high-performance nickel-based superalloy designed to withstand extreme conditions. Its exceptional high-temperature strength, oxidation resistance, and fatigue resistance make it a preferred material for aerospace and power generation industries.
With its proven reliability and performance, K465 continues to be a critical material for advanced engineering applications requiring durability in the harshest environments.