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Inconel 939
Material

IN939 Master Alloy is a premium nickel-based casting master alloy specifically designed for manufacturing IN939 superalloy components used in high-temperature and corrosive service environments.

With elevated chromium and cobalt content, the alloy provides exceptional oxidation resistance, hot corrosion resistance, and thermal stability, making it one of the most widely used superalloys for industrial gas turbine applications.

The master alloy is commonly used in the production of turbine blades, combustor parts, guide vanes, and other critical cast components requiring long-term reliability.

Overview

IN939 Master Alloy is a premium nickel-based casting master alloy engineered for the production of IN939 superalloy castings used in extreme-temperature environments. Featuring high chromium and cobalt content together with optimized additions of titanium, aluminum, tantalum, and niobium, the alloy offers an excellent balance of oxidation resistance, hot corrosion resistance, creep strength, and long-term structural stability.

IN939 has become one of the most widely used cast nickel-based superalloys in industrial gas turbine applications due to its ability to maintain mechanical integrity under prolonged thermal exposure. The alloy is particularly suitable for manufacturing turbine blades, guide vanes, combustor components, and other hot-section castings operating at temperatures approaching 850°C and above.

Application

IN939 Master Alloy is widely used for producing:

  • Industrial Gas Turbine Blades
  • Turbine Guide Vanes
  • Nozzle Guide Vanes
  • Combustor Components
  • Transition Pieces
  • Burner Nozzles
  • Power Generation Turbine Castings
  • Aerospace Engine Components
  • High-Temperature Structural Castings

The alloy is especially suitable for components requiring prolonged service life under high-temperature oxidation and thermal fatigue conditions.

Chemical Composition (%)

 

Ni Cr Co Ti W Al Ta Nb C Zr B Fe
Balance 20.0 – 23.0 18.0 – 20.0 3.0 – 4.0 1.0 – 3.0 1.0 – 2.0 1.0 – 2.0 0.5 – 1.2 ≤0.15 ≤0.15 ≤0.015 ≤0.5
Mechanical Property

                                                                                                                                                                                   

Tensile Strength Yield Strength (0.2% Offset) Elongation Hardness Density Melting Range
≥ 1000 MPa ≥ 750 MPa ≥ 8% 32-42 HRC 8.19 g/cm³ 1280-1360°C

                                                                                                        

Room Temperature 650°C 760°C 850°C
1000 MPa 900 MPa 780 MPa 650 MPa
Corrosion Resistance

IN939 Master Alloy is specifically engineered to produce castings with outstanding resistance to hot corrosion, oxidation, and thermal degradation.

Its high chromium and cobalt content provides superior protection against aggressive combustion gases, sulfur-bearing environments, and long-term exposure to elevated temperatures, making it one of the preferred alloys for industrial gas turbine applications.

Heat Treatment

Master alloy feedstock is supplied in the as-cast condition and does not require heat treatment prior to remelting.

Heat treatment procedures are applied to the final IN939 casting to achieve the required combination of creep strength, thermal stability, and oxidation resistance.

Typical treatment cycles may include solution annealing and precipitation aging according to customer specifications.

Heating and Pickling

IN939 Master Alloy generally requires no pickling treatment before use.

Proper storage and handling are recommended to maintain surface cleanliness and prevent contamination during melting operations. Vacuum melting and controlled atmosphere processing are recommended to achieve optimum alloy quality.

Hot and Cold Forming

IN939 Master Alloy is not designed for hot-working or cold-forming applications.

The material serves as a high-quality feedstock for vacuum induction melting, investment casting, and other precision casting processes used in superalloy component production.

Machining

Master alloy ingots are primarily intended for remelting rather than direct machining.

When size reduction is required for charging operations, standard cutting methods such as band sawing or abrasive cutting can be employed.

Machining characteristics of finished components depend on the final casting condition and heat treatment status.

Welding

The master alloy itself is not intended for welding.

Welding procedures for finished IN939 castings should follow approved nickel-based superalloy fabrication standards to ensure structural integrity and service performance.

Product Forms

IN939 Master Alloy can be supplied as:

  • Master Alloy Ingots
  • Vacuum Melted Ingots
  • Lump Alloy
  • Block Alloy
  • Casting Feedstock Materials
  • Custom Alloy Charges

Packaging can be customized according to customer melting and foundry requirements.

Note

All chemical compositions are subject to manufacturing tolerances and customer-specific requirements.

Each production batch undergoes chemical analysis, quality inspection, and traceability verification to ensure consistent performance in aerospace, power generation, and industrial casting applications.

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