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Fatigue crack propagation and fracture characteristics of SiCf/TC17 composites under three-point bending
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Xiaowen CHEN1, 2, Xinxin LI3, Mingjun YANG1, Shilin ZHONG2, Wenlong ZHOU3
Journal of Materials Engineering | 2026, 54(7) : 307 - 315
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Journal of Materials Engineering | 2026, 54(7): 307-315
• RESEARCH ARTICLE •
Fatigue crack propagation and fracture characteristics of SiCf/TC17 composites under three-point bending
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Xiaowen CHEN1, 2, Xinxin LI3, Mingjun YANG1, Shilin ZHONG2, Wenlong ZHOU3
Affiliations
  • 1.School of Energy and Power Engineering,Dalian University of Technology,Dalian 116024,Liaoning,China
  • 2.AECC Sichuan Gas Turbine Establishment,Chengdu 610500,China
  • 3.School of Materials Science and Engineering,Dalian University of Technology,Dalian 116024,Liaoning,China
Published: 2026-07-20 doi: 10.11868/j.issn.1001-4381.2024.000567
Outline
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The issues of fiber bridging,crack deflection,and interfacial debonding during the fracture process of long fiber reinforced titanium matrix composites are one of the key concerns in the industry. In this work,the crack propagation behavior, fracture characteristics, and fiber bridging effect of SiCf/TC17 composites under three-point bending fatigue are investigated. The results show that the fatigue crack propagation curve morphology of SiCf/TC17 composites varies significantly under different stress ratios. When the stress ratio R is high,crack arrest occurs after the crack propagates for a certain distance. The trend of crack propagation rate varies under different stress ratios:at R=0.1,the overall propagation rate shows a continuous increasing trend;at R=0.3,the change in propagation rate tends to gradually decrease;at R=0.5,the propagation rate exhibits an overall continuous decreasing trend. The fatigue fracture surface morphology of the material is characterized by an uneven feature,consisting of many different shapes of fracture small planes,with obvious uneven height differences between adjacent small planes. A large number of fibers are in a pulled-out state on the fracture surface, and the fibers exhibit different failure modes during crack propagation. During the fatigue fracture process of materials,the crack deflects to a certain extent when bypassing the fibers. The debonding zone at the fiber/matrix interface extends longitudinally along the fibers,and bridging fibers show secondary fracture. The fiber/matrix debonding occurs at the interface between the matrix and the C coating.

titanium matrix composites  /  SiC fiber  /  fatigue crack propagation  /  fracture
陈晓文, 李鑫鑫, 杨明军, 钟世林, 周文龙. SiCf/TC17复合材料三点弯曲疲劳裂纹扩展与断裂特征. 材料工程, 2026 , 54 (7) : 307 -315 . DOI: 10.11868/j.issn.1001-4381.2024.000567
Xiaowen CHEN, Xinxin LI, Mingjun YANG, Shilin ZHONG, Wenlong ZHOU. Fatigue crack propagation and fracture characteristics of SiCf/TC17 composites under three-point bending[J]. Journal of Materials Engineering, 2026 , 54 (7) : 307 -315 . DOI: 10.11868/j.issn.1001-4381.2024.000567
Year 2026 volume 54 Issue 7
110
52
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Article Info
doi: 10.11868/j.issn.1001-4381.2024.000567
  • Receive Date:2024-08-12
  • Online Date:2026-10-28
  • Published:2026-07-20
Article Data
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History
  • Received:2024-08-12
  • Accepted:2024-10-29
Funding
Affiliations
    1.School of Energy and Power Engineering,Dalian University of Technology,Dalian 116024,Liaoning,China
    2.AECC Sichuan Gas Turbine Establishment,Chengdu 610500,China
    3.School of Materials Science and Engineering,Dalian University of Technology,Dalian 116024,Liaoning,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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