腐蚀-疲劳-冲击共同作用下螺栓连接件强度研究
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1中国特种飞行器研究所,荆门 448035;2中国民航大学中欧航空工程师学院,天津 300300

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TB332

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Study on the Strength of Bolted Joints Under Corrosion-fatigue-impact Effects
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1China Special Vehicle Research Institute,Jingmen 448035;2Sino-European Institute of Aviation Engineering,Civil Aviation University of China,Tianjin 300300

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    摘要:

    连接件在工程结构中扮演着至关重要的角色,而腐蚀、疲劳、冲击等因素常常同时存在于连接件服役过程中,须研究这些因素共同作用下连接件的力学性能。本文以金属-复合材料螺栓连接件为研究对象,通过试验和仿真方法,研究其在腐蚀-疲劳-冲击共同作用下的拉伸性能。研究结果表明,仿真结果与试验结果吻合良好,证明了仿真模型在模拟腐蚀-疲劳-冲击作用下螺栓连接件力学行为方面的有效性和准确性;腐蚀、疲劳和冲击的共同作用下对连接件拉伸强度的削弱效应显著,盐雾腐蚀时间越长,螺栓连接件的载荷-位移曲线峰值越低。

    Abstract:

    Corrosion,fatigue and impact often occured simultaneously during the service of joints which play a vital role in engineering structures.It was essential to study the mechanical behavior of joints under their combined effect.This paper investigated the tensile behavior of metal-composite bolted joints under the combined condition of corrosion,fatigue and impact by experimental and simulation methods.The research results show that the simulation results are in good agreement with the experimental results,which proves the effectiveness and accuracy of the simulation model in predicting the mechanical behavior of the connection under the combined action of corrosion,fatigue and impact.The combined effect of corrosion,fatigue and impact significantly reduces the tensile strength of the bolted joints.The peak value of the load-displacement curve of bolted joint becomes lower with the extension of the salt spray corrosion time.

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肖鹏,徐猛,万傲霜,李顶河,朱强,王振名.腐蚀-疲劳-冲击共同作用下螺栓连接件强度研究[J].宇航材料工艺,2026,56(2):38-47.

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  • 收稿日期:2024-09-19
  • 最后修改日期:2026-03-26
  • 录用日期:2025-04-21
  • 在线发布日期: 2026-05-07
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