This comprehensive guide examines heat treatment processes for nickel and nickel alloys, focusing on five principal methods: annealing, stress relieving, stress equalizing, solution treating, and age hardening. The article details specific temperature requirements, atmospheric conditions, and processing parameters for various nickel alloys, from basic annealing to complex age-hardening treatments. Special attention is given to process control factors, including furnace atmosphere selection, temperature control, and contamination prevention, providing essential guidance for achieving optimal material properties.
Nickel and nickel alloys undergo various heat treatment processes to achieve specific mechanical and physical properties. The selection of appropriate heat treatment methods depends on chemical composition, fabrication requirements, and intended service conditions. Five principal heat treatment methods serve different purposes in nickel alloy processing.
Table 1. Nickel and nickel alloys composition
Material | Composition | ||||
Ni | Fe | Cu | Cr | Mo | |
Nickel 200 | 99.5 | 0.15 | 0.05 | - | - |
Nickel 201 | 99.5 | 0.15 | 0.05 | - | - |
Monel 400 | 66.0 | 1.35 | 31.5 | - | - |
Monel R-405 | 66.0 | 1.35 | 31.5 | - | - |
Monel K-500 | 65.0 | 1.00 | 29.5 | - | - |
Inconel 600 | 76.0 | 7.20 | 0.10 | 15.8 | - |
Inconel 601 | 60.5 | 14.1 | - | 23.0 | - |
Inconel 617 | 54.0 | - | - | 22.0 | 9.0 |
Inconel 625 | 61.0 | 2.5 | - | 21.5 | 9.0 |
Inconel 718 | 52.5 | 18.0 | 0.10 | 19.0 | 3.0 |
Inconel X-750 | 73.0 | 6.75 | 0.05 | 15.0 | - |
Hastelloy B | 64.0 | 5.0 | - | - | 28.0 |
Hastelloy C | 56.0 | 5.5 | - | 15.5 | 16.0 |
Hastelloy X | 48.0 | 18.5 | - | 22.0 | 9.0 |
Annealing produces a recrystallized grain structure and softening in work-hardened alloys, typically requiring temperatures between 705 and 1205°C. The process proves essential for materials hardened through cold working operations such as rolling, deep drawing, spinning, or severe bending, allowing continued fabrication through intermediate softening stages.
Three primary commercial annealing methods exist:
Open Annealing: Most commonly used, this method employs protective atmospheres from either combustion products or introduced reducing gases. Temperature control remains critical due to relatively short processing times.
Closed (Box) Annealing: Operating at lower temperatures than open annealing, this method requires longer processing times but offers less critical temperature control requirements.
Salt Bath Annealing: Specialized for small parts, this technique utilizes molten inorganic salts such as chlorides and carbonates of sodium, potassium, and barium.
Table 2. Soft-annealing methods for nickel and nickel alloys
Material | Open annealing°C | Closed annealing°C | Stress relieving°C |
Nickel 200 | 815 to 925 | 705 to 760 | 480 to 705 |
Nickel 201 | 760 to 870 | 705 to 760 | 480 to 705 |
Monel 400 | 870 to 980 | 760 to 815 | 540 to 565 |
Monel R-405 | 870 to 980 | 760 to 815 | - |
Monel K-500 | 870 to 1040 | Not applicable | - |
Inconel 600 | 925 to 1040 | 925 to 980 | 760 to 870 |
Inconel 601 | 1095 to 1175 | 1095 to 1175 | - |
Inconel 617 | 1120 to 1175 | 1120 to 1175 | - |
Inconel 625 | 980 to 1150 | 980 to 1150 | - |
Inconel 718 | 955 to 980 | Not applicable | - |
Inconel X-750 | 1095 to 1150 | Not applicable | - |
Hastelloy B | 1095 to 1185 | - | 1095 to 1185 |
Hastelloy C | 1215 | - | 1215 |
Hastelloy X | 1175 | 1175 | - |
Bright annealing requires careful atmosphere control to prevent surface oxidation. While nickel 200 and Monel 400 maintain brightness in reducing atmospheres, alloys containing chromium, titanium, and aluminum form thin oxide films. Protective atmospheres typically include:
Controlled fuel-air ratio combustion products Prepared atmospheres such as dried hydrogen, nitrogen, or dissociated ammonia Cracked or partially reacted natural gas.
Stress relieving occurs at temperatures between 425 and 870°C, removing or reducing stresses without recrystallization. Stress equalizing, performed at lower temperatures, balances stresses while maintaining strength from cold working.
Solution treating prepares age-hardenable materials for subsequent aging treatments through high-temperature exposure. This process dissolves precipitates and carbides into solid solution, creating a uniform structure for controlled precipitation during aging.
Age hardening develops maximum strength through controlled precipitation at intermediate temperatures between 425 and 870°C. The process may follow solution treatment or apply directly to worked material.
Table 3. Age-hardening practices for nickel and nickel alloys
Alloy | Solution treated | ||
Temperature | Cooling method | Age hardening | |
Monel K-500 | 980 °C | WQ | Heat to 595°C, hold 16h; furnace cool to 540oC, hold 6h; furnace cool to 480°C, hold 8h; air-cool |
Inconel 718 | 980 °C | AC | Heat to 720°C, hold 8h; furnace cool to 620°C, hold until furnace time for entire age-hardening cycle equals 18h; air cool |
Inconel X-750 | 1150 °C | AC | Heat to 845°C, hold 24h; air cool; reheat to 705°C, hold 20h; air cool |
980 °C | AC | Heat to 730°C, hold 8h; furnace cool to 620°C, hold until furnace time for entire age-hardening cycle equals 18h; air cool | |
Hastelloy X | 1175 °C | AC | Heat to 760°C, hold 3h; air cool; reheat to 595°C, hold 3h; air cool |
Successful heat treatment requires careful attention to furnace atmosphere composition. Sulfur-free environments prove essential for preventing embrittlement. Protective atmospheres must maintain reducing conditions while avoiding contamination.
Temperature control affects final properties significantly. Factors requiring attention include:
Heating rate control to prevent thermal shock Temperature uniformity throughout the furnace Proper cooling rate selection based on desired properties.
Surface protection during heat treatment influences final product quality. Considerations include:
Atmosphere composition and purity Prevention of contamination from foreign materials Post-treatment surface cleaning requirements.
Extended annealing at elevated temperatures produces exceptionally soft material, though typically at the expense of increased grain size. This specialized treatment serves applications where maximum formability outweighs grain size considerations.
Large components sometimes require localized treatment through techniques such as torch annealing. While not optimal for general use, these methods provide solutions for specific applications where full-component heat treatment proves impractical.
Successful heat treatment of nickel and nickel alloys requires careful attention to process parameters, atmospheric conditions, and temperature control. Understanding the relationships between processing conditions and final properties enables optimal treatment selection for specific applications.
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