中性盐雾腐蚀对AerMet100钢与TC18钛合金冲击疲劳寿命的影响研究
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Effect of neutral salt spray corrosion on impact fatigue life of AerMet100 steel and TC18 titanium alloy
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    摘要:

    部分航空金属结构在服役过程中常面临海洋腐蚀环境与反复冲击载荷的联合作用,从而导致材料表面发生腐蚀损伤并显著劣化其冲击疲劳性能。为深入探讨这一现象,本文对航空领域关键结构材料AerMet100钢与TC18钛合金在中性盐雾腐蚀不同时长作用下,对其冲击疲劳寿命的影响进行了系统研究。通过中性盐雾腐蚀试验、落锤冲击疲劳寿命测定试验及扫描电子显微镜(SEM)表征技术,系统揭示了腐蚀时长对2类缺口三点弯曲试样冲击疲劳寿命的影响及其损伤机制。结果显示,随着盐雾腐蚀时长的增加,AerMet100钢的U/V-90°型缺口试样和TC18钛合金U型缺口试样的疲劳寿命均呈现近似线性的衰减趋势,AerMet100钢在腐蚀240 h后疲劳寿命降至未腐蚀试样的约50%,而TC18钛合金的U型缺口试样在腐蚀480 h后降至未腐蚀试样的约50%,相比之下,TC18钛合金的V-90°型缺口试样由于缺口处较高的应力三轴度,其疲劳寿命主要受应力状态影响而非腐蚀损伤。另外,SEM结果分析表明,随着腐蚀时间的延长,AerMet100钢试样表面的腐蚀产物和点蚀坑数量显著增加,并伴随表面龟裂,因此促进了疲劳裂纹的萌生与扩展;而TC18钛合金因表面氧化膜对腐蚀介质的屏蔽效应,可有效阻止腐蚀介质的深入侵蚀,从而限制裂纹的扩展路径,保持较高的疲劳寿命。

    Abstract:

    Aviation metal structures often face the combined effect of Marine corrosion environment and repeated impact loads during service, which leads to corrosion damage on the material surface and significantly deteriorates its impact fatigue performance. In order to explore this phenomenon in depth, this paper systematically studied the impact fatigue life of AerMet100 steel and TC18 titanium alloy, the key structural materials in the aviation field, under different durations of neutral salt spray corrosion. The impact of corrosion duration on the impact fatigue life of two types of notched three-point bending specimens and the damage mechanism were systematically revealed by the neutral salt spray corrosion test, the dropping hammer impact fatigue life measurement test, and the scanning electron microscope (SEM) characterization technology. The results show: with the increase of salt spray corrosion time, the fatigue life of U/V-90° notched specimens of AerMet100 steel and TC18 titanium alloy U-notched specimens show a nearly linear decay trend, and the fatigue life of AerMet100 steel decreases to about 50% of that of non-corroded specimens after 240 h of corrosion. However, the U-notched specimen of TC18 titanium alloy decreases to about 50% of the uncorroded specimen after 480 h of corrosion. In contrast, the fatigue life of the V-90° notched specimen of TC18 titanium alloy is mainly affected by the stress state rather than the corrosion damage due to the high stress triaxial degree at the notch location. In addition, the SEM results show that with the extension of corrosion time, the number of corrosion products and pitting pits on the surface of AerMet100 steel samples increases significantly, accompanied by surface cracking, which promotes the initiation and propagation of fatigue cracks. Due to the shielding effect of the surface passivating film on the corrosive medium, the TC18 titanium alloy effectively prevents the in-depth erosion of the corrosive medium, limits the propagation path of the crack, and maintains a high fatigue life.

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王科翔,郭玉佩,周龙俊,朱亚新*,白春玉,杨强.中性盐雾腐蚀对AerMet100钢与TC18钛合金冲击疲劳寿命的影响研究[J].实验力学,2025,40(4):398~408

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  • 收稿日期:2025-02-13
  • 最后修改日期:2025-04-12
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  • 在线发布日期: 2025-09-29
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