Prediction of fatigue crack extension life and assessment of load reduction

IF 0.9 4区 材料科学 Q4 MATERIALS SCIENCE, MULTIDISCIPLINARY Journal of Mechanics of Materials and Structures Pub Date : 2024-03-27 DOI:10.2140/jomms.2024.19.491
Guangjie Min, Yong Dai, Afang Jin
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Abstract

In this paper, for the first time, a safety assessment process is proposed for predicting fatigue crack extension remaining life and crane load reduction use. The method is based on fracture mechanics to establish a simulation model of the main girder of a crane using on-site strain-gauge tests and related crack extension test results. Establishing a statistical model based on the real work experience of a crane, obtaining the stress-time history and load spectrum at the fatigue calculation point on the crane girder through dynamic simulation. Expansion simulations of a single initial crack with different deflection angles show that crack deflection slows down the crack expansion rate, i.e., the smaller the deflection angle, the smaller its lifetime. Expansion analyses of coplanar and adjacent parallel surfaces multicracks were also performed to investigate the effects of crack morphology changes during crack coalescence and coplanar crack interactions on crack coalescence, as well as the effects of defect spacing on fatigue life. For the single crack with a width of 4 mm, a load reduction analysis is performed, and the simulation results indicate that the load reduction range is 20%30%, the fatigue remaining life of the crack is increased to 2.053.08 times the original value, the degree of load reduction and the remaining life is compliant with the GB/T 41510-2022 Safety Assessment Rules for Lifting Appliances-General Requirements general requirements for crane safety evaluation, indicating that the proposed approach in this paper for estimating fatigue crack growth life and crane load reduction is viable and offers the benefits of a short cycle and low cost.

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疲劳裂纹扩展寿命预测和减载评估
本文首次提出了预测疲劳裂纹扩展剩余寿命和起重机减载使用的安全评估流程。该方法基于断裂力学,利用现场应变仪测试和相关裂纹扩展测试结果,建立起重机主梁的模拟模型。根据起重机的实际工作经验建立统计模型,通过动态模拟获得起重机大梁疲劳计算点的应力-时间历程和载荷谱。不同挠曲角的单个初始裂纹的扩展模拟表明,裂纹挠曲减缓了裂纹扩展速度,即挠曲角越小,其寿命越短。此外,还对共面和相邻平行面多裂纹进行了扩展分析,以研究裂纹凝聚过程中裂纹形态变化和共面裂纹相互作用对裂纹凝聚的影响,以及缺陷间距对疲劳寿命的影响。对于宽度为 4 mm 的单裂纹,进行了减载分析,模拟结果表明减载范围为 20%-30%,裂纹的疲劳剩余寿命提高到原值的 2.05-3.08 倍,减载程度和剩余寿命符合 GB/T 41510-2022 《起重机械安全评价规程-通用要求》中对起重机安全评价的一般要求,表明本文提出的估算疲劳裂纹增长寿命和起重机减载的方法是可行的,并具有周期短、成本低的优点。
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来源期刊
Journal of Mechanics of Materials and Structures
Journal of Mechanics of Materials and Structures 工程技术-材料科学:综合
CiteScore
1.40
自引率
0.00%
发文量
8
审稿时长
3.5 months
期刊介绍: Drawing from all areas of engineering, materials, and biology, the mechanics of solids, materials, and structures is experiencing considerable growth in directions not anticipated a few years ago, which involve the development of new technology requiring multidisciplinary simulation. The journal stimulates this growth by emphasizing fundamental advances that are relevant in dealing with problems of all length scales. Of growing interest are the multiscale problems with an interaction between small and large scale phenomena.
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