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Numerical simulation on air-cooled quenching process of FGH96 superalloy turbine disks
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Yu WANG1, Mingli WANG2, Yufeng LIU1, Lingwei KONG1, Shengdong GAO3
Journal of Materials Engineering | 2026, 54(7) : 201 - 211
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Journal of Materials Engineering | 2026, 54(7): 201-211
• RESEARCH ARTICLE •
Numerical simulation on air-cooled quenching process of FGH96 superalloy turbine disks
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Yu WANG1, Mingli WANG2, Yufeng LIU1, Lingwei KONG1, Shengdong GAO3
Affiliations
  • 1.Science and Technology on Advanced High Temperature Structural Materials Laboratory,AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China
  • 2.HFYC(Zhenjiang) Superalloy Co. ,Ltd. ,Zhenjiang 212001,Jiangsu,China
  • 3.Harbin Institute of Technology,Harbin 150001,China
Published: 2026-07-20 doi: 10.11868/j.issn.1001-4381.2025.000478
Outline
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The cooling process following solution heat treatment significantly influences the microstructure and mechanical properties of powder metallurgy superalloy turbine disks. This study investigates the effects of air-forced cooling process parameters, including gas flow rate, air pipe diameter, and disk rotation, on the temperature distribution and cooling rate of turbine disk billets.The results reveal that an increase in the gas flow rate enhances the surface heat transfer of the turbine disk billet, creating a larger temperature gradient and achieving a higher cooling rate. When the gas flow rate remains constant, reducing the air pipe diameter leads to an increase in the local gas flow velocity, thereby strengthening the surface heat convection and raising the cooling rate. During rotation, the internal temperature gradient of the disk is reduced, resulting in a more uniform temperature distribution.The optimized air-forced cooling parameters, namely a gas flow rate of 240 m/s, an air pipe diameter of 10 mm, and disk rotation, are validated through experiments. After heat treatment, the grain size is uniformly distributed, measuring ASTM 7.5-8. The closer to the surface of the turbine disk billet, the higher the cooling rate, the finer the γ' phase, and the better the creep performance. Conversely, the core of the turbine disk billet has the lowest cooling rate, a coarser γ' phase size, and relatively poor creep performance.The grain size and creep properties of turbine disk billets quenched by air-forced cooling are comparable to those quenched by conventional oil cooling. Moreover, the creep plastic elongation at 68 h during creep is superior to that of oil-cooled quenching. Therefore, air-forced cooling quenching holds great promise as a turbine disk preparation process.

air-cooled quenching  /  numerical simulation  /  turbine disk  /  powder metallurgy superalloy
汪煜, 王明礼, 刘玉峰, 孔令伟, 高胜东. FGH96合金涡轮盘风冷淬火过程数值模拟. 材料工程, 2026 , 54 (7) : 201 -211 . DOI: 10.11868/j.issn.1001-4381.2025.000478
Yu WANG, Mingli WANG, Yufeng LIU, Lingwei KONG, Shengdong GAO. Numerical simulation on air-cooled quenching process of FGH96 superalloy turbine disks[J]. Journal of Materials Engineering, 2026 , 54 (7) : 201 -211 . DOI: 10.11868/j.issn.1001-4381.2025.000478
Year 2026 volume 54 Issue 7
66
30
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Article Info
doi: 10.11868/j.issn.1001-4381.2025.000478
  • Receive Date:2025-08-26
  • Online Date:2026-10-28
  • Published:2026-07-20
Article Data
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History
  • Received:2025-08-26
  • Accepted:2026-01-26
Affiliations
    1.Science and Technology on Advanced High Temperature Structural Materials Laboratory,AECC Beijing Institute of Aeronautical Materials,Beijing 100095,China
    2.HFYC(Zhenjiang) Superalloy Co. ,Ltd. ,Zhenjiang 212001,Jiangsu,China
    3.Harbin Institute of Technology,Harbin 150001,China
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)
属
Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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