IN738LC (Low Carbon) is a nickel-based superalloy renowned for its superior performance in high-temperature environments. It is widely used in industries such as aerospace and power generation for components like turbine blades, vanes, and combustion chambers, where strength, oxidation resistance, and thermal stability are critical.
Element | Typical Percentage | Role and Contribution |
---|---|---|
Nickel (Ni) | ~60% | Base element providing strength and thermal stability. |
Chromium (Cr) | ~16% | Enhances oxidation and corrosion resistance. |
Cobalt (Co) | ~8.5% | Improves high-temperature strength and creep resistance. |
Aluminum (Al) | ~3.4% | Contributes to oxidation resistance and microstructural stability. |
Titanium (Ti) | ~3.4% | Strengthens the alloy via precipitation hardening. |
Tungsten (W) | ~2.6% | Improves high-temperature strength. |
Molybdenum (Mo) | ~1.7% | Enhances creep resistance. |
Tantalum (Ta) | ~1.75% | Provides solid solution strengthening. |
Carbon (C) | ≤ 0.09% | Low carbon content reduces carbide formation, improving ductility. |
Property | Value | Significance |
---|---|---|
Density | ~8.1 g/cm³ | Balances strength and weight for high-performance applications. |
Melting Point | ~1260–1330°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 | ~900–1200 MPa | Maintains structural integrity under stress. |
Creep Resistance | Exceptional | Resists deformation under prolonged high-temperature stress. |
Application | Industry | Details |
---|---|---|
Turbine Blades | Aerospace, Power Generation | Withstands extreme thermal and mechanical stresses. |
Combustion Chambers | Aerospace | Resists oxidation and thermal fatigue. |
Nozzle Guide Vanes | Aerospace, Energy | Maintains performance in high-temperature exhaust streams. |
Industrial Gas Turbines | Energy | Provides efficiency and durability in power plants. |
Specification | Details |
---|---|
Form | Castings, bars, sheets |
Purity | ≥ 99.5% (for cast form). |
Standard Compliance | AMS 5383, ASTM B637. |
Particle Size Range | N/A (Typically cast or forged). |
Advantages | Limitations |
---|---|
Exceptional high-temperature and oxidation resistance. | Higher cost compared to standard alloys. |
Superior creep and fatigue resistance. | Requires precise manufacturing and processing techniques. |
Outstanding corrosion resistance in harsh environments. | Limited ductility compared to other alloys. |
What is IN738LC alloy?
IN738LC is a nickel-based superalloy designed for high-temperature applications, particularly in aerospace and power generation industries.
Why is IN738LC used in turbine blades?
Its high-temperature strength, oxidation resistance, and creep resistance make it ideal for turbine blades operating in extreme conditions.
What industries benefit from IN738LC?
IN738LC is widely used in aerospace and energy sectors for components requiring exceptional thermal and mechanical performance.
How does the low carbon content affect IN738LC?
The low carbon content reduces carbide formation, improving ductility and resistance to thermal fatigue.
Can IN738LC withstand extreme environments?
Yes, IN738LC excels in high-temperature, oxidizing, and corrosive environments, making it suitable for critical aerospace and energy applications.
IN738LC is a high-performance nickel-based superalloy tailored for high-temperature applications. Its exceptional oxidation resistance, creep resistance, and mechanical strength make it indispensable for aerospace and energy industries.
With its proven performance in demanding environments, IN738LC continues to be a preferred choice for advanced engineering solutions.