肖瀚瑶,张勇,王安东,等. 缓蚀剂对航空用7050铝合金搭接件疲劳寿命的影响[J]. 失效分析与预防,2025,20(3):208-214. doi: 10.3969/j.issn.1673-6214.2025.03.006
    引用本文: 肖瀚瑶,张勇,王安东,等. 缓蚀剂对航空用7050铝合金搭接件疲劳寿命的影响[J]. 失效分析与预防,2025,20(3):208-214. doi: 10.3969/j.issn.1673-6214.2025.03.006
    XIAO Hanyao,ZHANG Yong,WANG Andong,et al. Influence of corrosion inhibitor on fatigue life of 7050 aluminium alloy lap joint for aviation[J]. Failure analysis and prevention,2025,20(3):208-214. doi: 10.3969/j.issn.1673-6214.2025.03.006
    Citation: XIAO Hanyao,ZHANG Yong,WANG Andong,et al. Influence of corrosion inhibitor on fatigue life of 7050 aluminium alloy lap joint for aviation[J]. Failure analysis and prevention,2025,20(3):208-214. doi: 10.3969/j.issn.1673-6214.2025.03.006

    缓蚀剂对航空用7050铝合金搭接件疲劳寿命的影响

    Influence of Corrosion Inhibitor on Fatigue Life of 7050 Aluminium Alloy Lap Joint for Aviation

    • 摘要: 为研究不同缓蚀剂对铝合金搭接件腐蚀疲劳寿命的影响,对未涂抹及涂抹TFHS-10缓蚀剂、TSN-7缓蚀剂的7050铝合金搭接件开展一定周期的预腐蚀实验,并进行疲劳实验和形貌观察,获得搭接件的疲劳寿命及腐蚀形貌,对比分析有无缓蚀剂及不同种类缓蚀剂对搭接件腐蚀疲劳寿命的影响。结果表明:经相同腐蚀时间后,未涂抹缓蚀剂的搭接件螺栓孔孔边和搭接面腐蚀程度较涂抹缓蚀剂的搭接件严重。涂抹缓蚀剂的搭接件较未涂抹缓蚀剂的搭接件在腐蚀后的疲劳寿命有所增加,涂抹TFHS-10、TSN-7缓蚀剂的搭接件腐蚀后的疲劳寿命增幅分别为77.9%、49.2%。腐蚀导致搭接件表面产生蚀坑,板材平均厚度减小,形成局部应力集中点,局部应力增大,更容易产生疲劳裂纹,缩短疲劳寿命。

       

      Abstract: The aim of the present work is to study the effect of different corrosion inhibitors on the corrosion fatigue life of aluminum alloy lap joints. Firstly, pre-corrosion tests were carried out for a period on the 7050 aluminum alloy lap joints covered with TFHS-10 or TSN-7 corrosion inhibitor as well as the joints without corrosion inhibitor. Then, fatigue testing and morphology observation were carried out to obtain the fatigue life and corrosion morphology of the lap joints. Finally, the effect of the presence or absence of corrosion inhibitor and different types of corrosion inhibitors on the corrosion fatigue life of the lap joints were compared and analyzed. The results show that after the same corrosion time, the corrosion degree of bolt hole sides and joint surfaces of the joints without corrosion inhibitor is more serious than that of the joints with corrosion inhibitor. Compared with uncoated joints, the fatigue life of the lap joints coated with TFHS-10 and TSN-7 corrosion inhibitor increases by 77.9% and 49.2% respectively. Corrosion caused corrosion pits on the surface of the lap joints, reduced the average thickness of the plates, and formed local stress concentration points, thereby increasing local stress. As a result, fatigue cracks were more likely to form, resulting in a shortened fatigue life.

       

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