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Chinese Journal of Materials Research  2026, Vol. 40 Issue (2): 92-98    DOI: 10.11901/1005.3093.2025.049
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Deformation Characteristics and Life Prediction of DZ411 Alloy under High Temperature Cyclic Loading
ZHI Yiheng, ZHOU Tongtong, ZHAO Jie(), CAO Tieshan(), CHENG Congqian
School of Materials Science and Engineering, Dalian University of Technology, Dalian 116024, China
Cite this article: 

ZHI Yiheng, ZHOU Tongtong, ZHAO Jie, CAO Tieshan, CHENG Congqian. Deformation Characteristics and Life Prediction of DZ411 Alloy under High Temperature Cyclic Loading. Chinese Journal of Materials Research, 2026, 40(2): 92-98.

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Abstract  

In order to study the deformation behavior of a directionally solidified nickel based high-temperature alloy DZ411 by cyclic loads (20-380 MPa) at temperatures (1173-1223 K) was studied via electronic creep testing machine, optical microscopy and electron field emission scanning electron microscopy etc. Meanwhile a model of the fracture life of the alloy was also established and compared with the test results. The results show that under constant and cyclic loads, the fracture life (tr) and minimum strain rate (ε˙min) of the alloy both conform to the Monkman-Grant equation and can be fitted well on the same data set. As the test temperature, stress amplitude, and average stress decrease, the fracture time increases and the internal damage of the alloy intensifies. The minimum strain rate and average stress of the alloy follow a power-law relationship, but considering the comprehensive effect of the average stress (σm) and stress amplitude (σa) on the fracture life in cyclic testing, the equivalent stress may be corrected according to (σeq=σmγσmax1-γ, γ = 0.1), and the Larson-Miller parameter method (Pσeq=TC+lgtr) is used to normalize the fracture life by different loading conditions, thus achieving life prediction by various temperature and loading conditions.

Key words:  nonferrous metals and their alloys      high temperature cycle      deformation characteristics      life prediction      DZ411 directionally solidified nickel based high-temperature alloy     
Received:  20 January 2025     
ZTFLH:  TG146.15  
Fund: Science Centre for Gas Turbine Project(P2021-A-IV-001-001);Basic Research Project for Marine Gas Turbines(MGT2023001);National Natural Science Foundation of China(51901035)
Corresponding Authors:  ZHAO Jie, Tel: (0411)84709076, E-mail: jiezhao@dlut.edu.cn;
CAO Tieshan, Tel: 13354054601, E-mail: tieshan@dlut.edu.cn

URL: 

https://www.cjmr.org/EN/10.11901/1005.3093.2025.049     OR     https://www.cjmr.org/EN/Y2026/V40/I2/92

Temperature / KLoading rate/ MPa·s-1Stress amplitude / MPaMean stress / MPa
11739.6130200
150180
1203130200
1223

0

130

200

150

130200
130250
150230
Table 1  Experimental parameters for high-temperature cyclic loading
Fig.1  Deformation curve under cyclic loading test with T = 1223 K, σm = 250 MPa, σa = 130 MPa (a) overall stress-strain curve, (b) stress-strain curves of individual cycles in regions 1, 2, 3 of Fig.1a
Fig.2  Strain/strain rate vs time curve of DZ411 alloy during high-temperature cyclic loading process (a, b) at T = 1223 K, different average stress conditions, (c, d) at σm = 200 MPa, different temperature conditions
Fig.3  Relationship between minimum strain rate and life of DZ411 alloy under constant load and cyclic load conditions
Fig.4  Under different loading conditions, the metallographic morphology of DZ411 alloy near the fracture surface parallel to the growth direction of columnar crystals (a) T = 1223 K, σa = 0, σm = 200 MPa, tr = 354.5 h, (b) T = 1223 K, σa = 130 MPa, σm = 200 MPa, tr = 22.7 h, (c) T = 1223 K, σa = 130 MPa, σm = 150 MPa, tr = 69.1 h, (d) T = 1203 K, σa = 130 MPa, σm = 200 MPa, tr = 33.5 h
Fig.5  Fracture morphology of DZ411 alloy under different loading conditions (a) T =1223 K, σa=0, σm=200 MPa, (b) T =1223 K, σa=130 MPa, σm=150 MPa, (c) T =1223 K, σa=130 MPa, σm=150 MPa, (d) T =1203 K, σa=130 MPa, σm=200 MPa
Fig.6  Double logarithmic plot of life and average stress under different temperatures and stress amplitudes
Fig.7  Schematic diagram of the variation of fitting coefficient R2 with stress correction coefficient γ at different temperatures
Fig.8  Double logarithmic plot of life and equivalent stress under different temperatures and stress amplitudes
Fig.9  Normalization of creep life under different loading conditions using Larson-Miller parameter method (a) and prediction results of life (b) of DZ411 alloy
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