Main performance and applicati Anti-corrosion, anti-fatigue; manufacturing of heat-resistant and corrosion-resistant parts in the fields of petrochemical, aerospace, etc.
Product Specifications (microm 0-25,15-53,45-105,50-150
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Detail

IN738LC Alloy: A Nickel-Based Superalloy for High-Temperature Applications

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.


Composition and Features of IN738LC

Elemental Composition

ElementTypical PercentageRole 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.

Key Properties of IN738LC

PropertyValueSignificance
Density~8.1 g/cm³Balances strength and weight for high-performance applications.
Melting Point~1260–1330°CSuitable for high-temperature environments.
Oxidation ResistanceExcellentEnsures durability in oxidizing atmospheres.
Corrosion ResistanceHighPerforms well in aggressive chemical environments.
Tensile Strength~900–1200 MPaMaintains structural integrity under stress.
Creep ResistanceExceptionalResists deformation under prolonged high-temperature stress.

Applications of IN738LC

ApplicationIndustryDetails
Turbine BladesAerospace, Power GenerationWithstands extreme thermal and mechanical stresses.
Combustion ChambersAerospaceResists oxidation and thermal fatigue.
Nozzle Guide VanesAerospace, EnergyMaintains performance in high-temperature exhaust streams.
Industrial Gas TurbinesEnergyProvides efficiency and durability in power plants.

Specifications and Standards of IN738LC

SpecificationDetails
FormCastings, bars, sheets
Purity≥ 99.5% (for cast form).
Standard ComplianceAMS 5383, ASTM B637.
Particle Size RangeN/A (Typically cast or forged).

Advantages and Limitations of IN738LC

AdvantagesLimitations
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.

Frequently Asked Questions (FAQs)

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.


Conclusion

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.