High-Temperature Mechanical Properties of Incoloy 925
1. Key High-Temperature Mechanical Properties
Supplementary Notes
Impact Toughness: At temperatures up to 500°C, Incoloy 925 retains a Charpy V-notch impact toughness of ≥40 J. Beyond 550°C, toughness gradually decreases but remains sufficient for most structural applications.
Fatigue Strength: The high-cycle fatigue strength at 400°C is approximately 350–400 MPa (10⁷ cycles), which is 35–40% of its room-temperature tensile strength-significantly higher than many non-precipitation-hardened nickel alloys.
Creep and Stress-Rupture Resistance: This alloy exhibits outstanding creep resistance at 550°C under a stress of 300 MPa, with creep strain less than 0.2% after 10,000 hours. Its stress-rupture life at 600°C and 275 MPa exceeds 20,000 hours, making it suitable for long-term service in high-temperature, high-stress environments.
2. Trend of Strength with Temperature Increase
Temperature ≤500°C: Strength remains relatively stable. The γ′ and γ′′ precipitates are thermally stable in this range, effectively pinning dislocations and resisting deformation. At 500°C, its yield strength is still ~70–80% of the room-temperature value, with no sudden decline.
Temperature 500–600°C: Strength begins to decrease moderately. As temperature rises, the mobility of dislocations increases, and the precipitates start to coarsen slightly, reducing their strengthening effect. Even so, at 600°C, the yield strength is still ~60–70% of the room-temperature level, which is far higher than that of solid-solution-strengthened alloys like Incoloy 825.
Temperature >650°C: A more noticeable strength drop occurs. Beyond 650°C, the γ′′ precipitates dissolve into the matrix, and the γ′ precipitates coarsen rapidly. This leads to a significant loss of strength-at 700°C, the yield strength may drop to <40% of the room-temperature value, which is beyond the recommended service temperature of Incoloy 925.




3. Critical Factors Affecting High-Temperature Performance
Heat Treatment Quality: Over-aging (excessively high aging temperature or prolonged time) causes precipitate coarsening, which reduces both room-temperature and high-temperature strength. The optimal heat treatment is solution annealing at 980–1010°C for 1–2 hours, followed by aging at 718°C for 8 hours, cooling to 621°C at a rate of 55°C/hour, and holding for a further 8 hours.
Microstructure Uniformity: Segregation of alloying elements (e.g., Ti, Al, Nb) during casting or forging can lead to uneven precipitate distribution, resulting in localized strength loss at high temperatures.
Environmental Effects: In oxidizing or corrosive high-temperature environments, the formation of a dense, adherent Cr₂O₃ oxide film protects the alloy from surface degradation, which indirectly preserves its mechanical properties by preventing premature crack initiation.
4. Typical High-Temperature Applications
Oil and gas downhole components (tubing hangers, valve trim) operating at 300–550°C
Aerospace engine fasteners and structural parts
Steam turbine blades and boiler components in power plants
Chemical processing equipment handling high-temperature, corrosive fluids
Summary





