Jul 22, 2025 Leave a message

What is INCONEL 738 alloy

1. What is INCONEL 738 material?

INCONEL 738 is a high-performance nickel-based superalloy designed for extreme high-temperature applications, particularly in gas turbine engines. It is a vacuum-cast, precipitation-hardened alloy, engineered to deliver exceptional creep-rupture strength, oxidation resistance, and thermal stability at elevated temperatures-up to approximately 982°C (1800°F).
Key characteristics include:

Creep resistance: Maintains structural integrity under prolonged stress at high temperatures, critical for turbine components.

Corrosion and oxidation resistance: Resists degradation from hot gases, sulfur-containing environments, and high-temperature oxidation.

Mechanical strength: Retains high tensile and fatigue strength even after long-term exposure to thermal cycling.

Its primary applications are in gas turbine blades, vanes, and other hot-section components in industrial and aerospace gas turbines, where reliability under extreme heat and stress is paramount.

2. What is the composition of INCONEL 783?

INCONEL 783 is a nickel-cobalt-iron-based superalloy developed for low thermal expansion and high-temperature strength, often used in aerospace and industrial applications requiring dimensional stability. Its typical composition (by weight) is:
ElementContent (%)
Nickel (Ni)~28.5
Cobalt (Co)~34.0
Iron (Fe)~26.0
Aluminum (Al)~5.4
Chromium (Cr)~3.0
Titanium (Ti)~0.1
Other trace elements*<1.0
Trace elements may include small amounts of carbon, manganese, silicon, or boron to enhance specific properties like grain boundary strength.

3. What is the heat treatment for Inconel 738?

The heat treatment of INCONEL 738 is critical to optimize its precipitation-hardening phases (e.g., &gamma;'-Ni₃Al) and achieve maximum high-temperature strength. The standard process is:

Solution annealing: Heat to 1121&deg;C (2050&deg;F) and hold for 2 hours, then air-cool. This step dissolves alloying elements uniformly into the matrix and refines grain structure.

Aging (precipitation hardening): Heat to 843&deg;C (1550&deg;F) and hold for 24 hours, followed by air-cooling. This promotes the formation of fine, uniformly distributed &gamma;' precipitates, which significantly enhance creep and tensile strength.

This treatment balances strength and ductility, making INCONEL 738 suitable for high-stress, high-temperature service.
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4. What is the tensile strength of INCONEL 738?

INCONEL 738 exhibits high tensile strength, especially at room and elevated temperatures, due to its &gamma;'-strengthened microstructure. Typical tensile strength values are:

Room temperature (70&deg;F / 21&deg;C): ~159,000 psi (&asymp;1100 MPa).

Elevated temperatures: Retains significant strength; for example, at 816&deg;C (1500&deg;F), tensile strength is approximately 85,000&ndash;95,000 psi (&asymp;585&ndash;655 MPa), with excellent creep resistance under long-term stress.

These properties make it ideal for load-bearing components in gas turbines and other high-temperature systems.
 

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