Comparison of fatigue characteristics and failure analysis of Ni-based superalloy subjected to thermomechanical fatigue under different phase conditions

• In the IP case, failure was due to creep-fatigue interactions. • Cracks originated at high Ta and Hf concentrations in IP TMF tests. • Oxidation-assisted cracking was the primary damage mechanism in OP TMF tests. • An oxide multilayer with consumed Ni, Cr, Al, and Ta oxides was observed in OP. • Twinning-related deformation and the TCP phase also reduced fatigue life. In this research, the thermomechanical fatigue (TMF) characteristics of a second-generation Ni-based single-crystal superalloy were investigated. The combined effects of temperature cycling and mechanical stress were examined using a strain-controlled approach under different TMF testing conditions. The results indicated that cyclic softening occurred during the early stages during in-phase (IP) loading. In contrast, out-of-phase (OP) tests exhibited cyclic hardening, as evidenced by an increase in the stress range, which intensified at higher mechanical strain amplitudes. This resulted in a shorter fatigue life compared to the IP TMF case. The crack distribution patterns and damage mechanisms on the cross-sectional and fracture surfaces of the failed specimens were analyzed. In the OP TMF tests, oxidation-assisted cracking was identified as the primary damage mechanism. The dominance of oxide layers was a key distinguishing feature. Additionally, twinning-related deformation and topologically close-packed (TCP) phase particles were observed in specimens subjected to a higher mechanical strain of 0.6%, where they ran parallel to the main crack, contributing to a reduction in lifetime. Conversely, the IP TMF cases were mainly dominated by creep damage mechanisms, with some signs of oxidation penetration observed during testing. The application of the Ostergren model to the fatigue life prediction of a Ni-based single-crystal superalloy under both conditions was evaluated. As this model was insufficient, a modified Ostergren model was proposed by incorporating the maximum and amplitude stresses in the power law forms.

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Publication Details

Journal
Engineering Failure Analysis
Published
2024-08-26
DOI
https://doi.org/10.1016/j.engfailanal.2024.108814
Citations
7
Primary Topic
High Temperature Alloys and Creep
Type
article
Field-Weighted Citation Impact
1.49

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article

Comparison of fatigue characteristics and failure analysis of Ni-based superalloy subjected to thermomechanical fatigue under different phase conditions

Sang Koo Jeon, Hee Soo Yun, Jaeyeong Park, Van Hung Dao et al.
7 citations
Engineering Failure Analysis
High Temperature Alloys and Creep
1.49
article

Comparison of fatigue characteristics and failure analysis of Ni-based superalloy subjected to thermomechanical fatigue under different phase conditions

Sang Koo Jeon, Hee Soo Yun, Jaeyeong Park, Van Hung Dao, Seung Hoon Nahm
article en
7 citations

Abstract

• In the IP case, failure was due to creep-fatigue interactions. • Cracks originated at high Ta and Hf concentrations in IP TMF tests. • Oxidation-assisted cracking was the primary damage mechanism in OP TMF tests. • An oxide multilayer with consumed Ni, Cr, Al, and Ta oxides was observed in OP. • Twinning-related deformation and the TCP phase also reduced fatigue life. In this research, the thermomechanical fatigue (TMF) characteristics of a second-generation Ni-based single-crystal superalloy were investigated. The combined effects of temperature cycling and mechanical stress were examined using a strain-controlled approach under different TMF testing conditions. The results indicated that cyclic softening occurred during the early stages during in-phase (IP) loading. In contrast, out-of-phase (OP) tests exhibited cyclic hardening, as evidenced by an increase in the stress range, which intensified at higher mechanical strain amplitudes. This resulted in a shorter fatigue life compared to the IP TMF case. The crack distribution patterns and damage mechanisms on the cross-sectional and fracture surfaces of the failed specimens were analyzed. In the OP TMF tests, oxidation-assisted cracking was identified as the primary damage mechanism. The dominance of oxide layers was a key distinguishing feature. Additionally, twinning-related deformation and topologically close-packed (TCP) phase particles were observed in specimens subjected to a higher mechanical strain of 0.6%, where they ran parallel to the main crack, contributing to a reduction in lifetime. Conversely, the IP TMF cases were mainly dominated by creep damage mechanisms, with some signs of oxidation penetration observed during testing. The application of the Ostergren model to the fatigue life prediction of a Ni-based single-crystal superalloy under both conditions was evaluated. As this model was insufficient, a modified Ostergren model was proposed by incorporating the maximum and amplitude stresses in the power law forms.

Engineering Failure AnalysisVol. 165
Yonsei University (KR), Korea Institute of Energy Research (KR)
Ministry of Trade, Industry and Energy, Korea Institute of Energy Technology Evaluation and Planning
Climate action
Openalex Percentile: Top 20%
High Temperature Alloys and Creep
1.49
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