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Acta Metall Sin  2026, Vol. 62 Issue (5): 875-889    DOI: 10.11900/0412.1961.2025.00292
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Deformation and Damage Behavior of Single Crystal Superalloys Under Near-Service Conditions
ZHANG Jian(), WANG Dong(), LI Yawei, HUANG Yaqi, ZHAN Xin, XIE Guang
Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China
Cite this article: 

ZHANG Jian, WANG Dong, LI Yawei, HUANG Yaqi, ZHAN Xin, XIE Guang. Deformation and Damage Behavior of Single Crystal Superalloys Under Near-Service Conditions. Acta Metall Sin, 2026, 62(5): 875-889.

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Abstract  

Ni-based single crystal superalloys are key materials for turbine blades in aero-engines and gas turbines. Their deformation and damage behavior under the coupled effects of high temperature, complex stress states, and harsh environments directly affects blade service safety and lifespan. This paper systematically reviews recent research progress on single-crystal superalloys with respect to creep, fatigue, and thermo-mechanical fatigue (TMF), with an emphasis on the evolution of microstructures and damage mechanisms under multifield coupling conditions. For creep, the effects of thickness debit, hot corrosion, and multiaxial stress on material properties are summarized, and emerging phenomena and mechanisms associated with ultra-high-temperature exposure, long-term service, and nonisothermal creep are discussed. For fatigue, the transformation of crack initiation mechanisms under low-cycle, high-cycle, and very-high-cycle fatigue conditions is clarified; the synergistic effects of thermo-mechanical-environment coupling and multiaxial stress are examined; and the critical roles of surface condition and structural characteristics in component fatigue performance are highlighted. For TMF, the influences of phase relationship, crystal orientation, alloying elements, and coating-substrate interactions on damage behavior are reviewed. Additionally, this paper reviews the application and progress of in situ characterization techniques for elucidating deformation and damage mechanisms. Finally, future research directions in this field are outlined.

Key words:  single crystal superalloy      near-service      creep      fatigue      thermal-mechanical fatigue     
Received:  28 September 2025     
ZTFLH:  TG132.3  
Fund: National Key Research and Development Program of China(2021YFA1600603);National Natural Science Foundation of China(52201151);National Natural Science Foundation of China(52331005);National Natural Science Foundation of China(U2141206);National Science and Technology Major Project(J2019-IV-0006-0074);National Science and Technology Major Project(J2019-VI-0010-0124);CSNS Consortium on High-Performance Materials of Chinese Academy of Sciences(JZHKYPT-2021-01);International Partnership Program of Chinese Academy of Sciences(172GJHZ2022095FN);Postdoctoral Fellow-ship Program of CPSF(GZC20241762);Science and Technology Major Project of Liaoning Province(2024JH1/11700035)
Corresponding Authors:  ZHANG Jian, professor, Tel: (024)23971196, E-mail: jianzhang@imr.ac.cn; WANG Dong, Tel: (024)83970230, E-mail: dwang@imr.ac.cn

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https://www.ams.org.cn/EN/10.11900/0412.1961.2025.00292     OR     https://www.ams.org.cn/EN/Y2026/V62/I5/875

Fig.1  Thickness debit effect of creep property of single crystal superalloys[4-10] (SX—single-crystal)
Fig.2  Fatigue crack initiation mechanism under different loading conditions
(a) cracking of carbides is attributed to the combination of oxidizing and cyclic loading
(b) crack initiating from slip band shearing around casting pore
(c) γ′-rotation within the rough zone around casting pore is related to the operation of {111}<110> and {111}<112> slip systems (σ—stress)
(d) slip bands with different direction observed within eutectic show more uniform deformation
(e) hot isostatic pressing (HIP) specimens mainly fail from the surface oxidation and present the best fatigue property
Fig.3  Schematics of the thermal-mechanical fatigue (TMF) deformation mechanism in single-crystal superalloys (OP—out-of-phase, IP—in-phase)
(a) during IP-TMF cycling, alloy deformation mechanism is dominated by creep damage, with cracks preferentially initiating at carbides and casting pores
(b) under the OP-TMF cycling, highly localized twinning is the major deformation mechanism, and cracks propagate rapidly along the twinning planes. Recrystallization occurs within the deformation bands, with the interception of twins in different orientations serving as initiation sites (TCP—topologically close-packed phase)
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