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Research paper | Publishing Language: Chinese | Open Access

Effects of hyperthermal exposure on microstructures and mechanical properties of casting TiAl-4822 alloys

Qian LUO1,2,3Zhenwei WEI3Xin FENG1,2,3Changkui LIU3Yulong CHEN4Chunling ZHAO5Hai NAN1,2,3Xianfei DING1,2,3( )
BAIMTEC Material Co., Ltd, Beijing 100094, China
Beijing Engineering Research Center of Advanced Titanium Alloy Precision Forming Technology, Beijing 100094, China
AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China
AECC Sichuan Gas Turbine Research Institute, Chengdu 610213, China
AECC Hunan Aviation Power Machinery Research Institute, Zhuzhou 412002, Hunan, China
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Abstract

This work investigates the alterations in the microstructure and mechanical properties of the Ti-48Al-2Cr-2Nb alloy (referred to as 4822 alloy) following simulated short-term superheated service at 800-950 ℃. The research focuses on the effects of thermal exposure temperature and holding time on the microstructure, room-temperature and high-temperature tensile properties, and high-temperature endurance properties of 4822 alloy. The results reveal that after exposure at 800-950 ℃, the α2 phase within the α2/γ lamellar colonies dissolves, forming coarse γ lamellae. As the thermal exposure time increases, the dissolution of the α2 phase becomes more pronounced, the ends of the α2/γ lamellar structures coarsen, and the lamellae grow into adjacent colonies. After treatment at 900 ℃, spherical B2 precipitates form at the boundaries between lamellar colonies and equiaxed γ grains. At 950 ℃, fine B2 precipitates appear within the coarse γ lamellae inside the colonies, and the number of B2 precipitates increases. Prolonging the exposure time leads to the precipitation of extremely fine γ lamellae within blocky α2 phases, with their quantity increasing; equiaxed γ grains at colony boundaries gradually grow, and the number of equiaxed γ grains within the colonies also rises. After thermal exposure at 850 ℃/10 min, 850 ℃/120 min, and 900 ℃/10 min, both the room and high-temperature yield strengths of the alloy increase, while the room and high-temperature elongations decrease. However, after thermal exposure at 950 ℃/10 min, the room-temperature elongation of the alloy is (2.4±0.55)%, representing an increase of 5.73% compared to its original state. After thermal exposure at 850 ℃/10 min, 850 ℃/120 min, and 900 ℃/10 min, the stress rupture lives of the alloy under both 650 ℃/400 MPa and 700 ℃/350 MPa conditions are extended. However, after thermal exposure at 850 ℃/120 min, the stress rupture life under 650 ℃/400 MPa is (14.85±3.55) h, which decreased by 94.02% compared to its original state.

CLC number: V252 Document code: A

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Journal of Aeronautical Materials
Pages 118-129

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Cite this article:
LUO Q, WEI Z, FENG X, et al. Effects of hyperthermal exposure on microstructures and mechanical properties of casting TiAl-4822 alloys. Journal of Aeronautical Materials, 2026, 46(8): 118-129. https://doi.org/10.11868/j.issn.1005-5053.2026.000067

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Received: 24 March 2026
Published: 15 August 2026
© Journal of Aeronautical Materials 2026.

This is an open access article under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).