Heat Treatment of Metals ›› 2024, Vol. 49 ›› Issue (11): 302-307.DOI: 10.13251/j.issn.0254-6051.2024.11.047

• TEST AND ANALYSIS • Previous Articles     Next Articles

Fracture failure analysis of 60Si2MnA steel circlip

Chen Hehe1,2,3, Liu Chunjiang1,2,3, Jiang Tao1,2,3, Guo Chen4   

  1. 1. AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China;
    2. Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, Beijing 100095, China;
    3. Key Laboratory of Aeronautical Materials Testing and Evaluation, Aero Engine Corporation of China, Beijing 100095, China;
    4. Lingyun Technology Group Co., Ltd., Wuhan Hubei 430030, China
  • Received:2024-08-08 Revised:2024-08-28 Online:2024-11-25 Published:2025-01-09

Abstract: Circlip broke when installed in the hollow shaft of the rotor component. Macroscopic and microscopic morphologies on the fracture surface were observed, chemical composition of the raw material was tested, and the microstructure and hardness of the material were investigated in order to find out the failure mechanism of the circlip. The results show that the failure mode of the circlip is hydrogen embrittlement fracture. The circlip has a high sensitivity to hydrogen embrittlement due to its high hardness caused by low temperature tempering, and during electroplating, the accumulation of hydrogen inside the material increases, resulting in hydrogen embrittlement fracture during installation. Therefore, the heat treatment process of the circlip can be controlled to reduce the material hardness, meanwhile, the electroplating process can be controlled to reduce the thickness of the galvanized layer on the circlip.

Key words: circlip, 60Si2MnA steel, hydrogen embrittlement, hardness, galvanized layer

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