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Effect of nitrogen-doped type on fracture toughness improvement and crack growth resistance of carbon nanotube/epoxy nanocomposites: Combined multiscale analysis approach 掺氮类型对纳米碳管/环氧纳米复合材料断裂韧性改善和抗裂纹生长的影响多尺度综合分析方法
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-21 DOI: 10.1016/j.engfracmech.2024.110502
Recently, nitrogen-doped carbon nanotubes (N-doped CNTs) have received great attention in nanocomposite design. It has become highly necessary to develop predictive models to elucidate their toughning behavior. In this study, the effects of CNTs with three different types of N-doped functional groups (quaternary, pyrrolic, and pyridinic) on the fracture toughness (FT) and crack growth of polymer nanocomposites are predicted using a multiscale analysis approach. To scale up from the nanoscale to the macroscale, a multiscale analysis approach integrating molecular dynamics, micromechanics theory, linear fracture mechanics theory, and a phase-field fracture model (PFFM) is adopted. The toughness enhancement trends of the three different types of N-doped functional groups were quantified by considering four toughening mechanisms (CNT debonding, plastic nanovoid growth, CNT pull-out, and CNT rupture), and compared with experimental result. The results show that the excellent interphase and interfacial properties of quaternary and pyridinic functional groups significantly improve the FT and crack growth resistance of N-doped CNT/epoxy nanocomposites. Our study provides high-performance solutions for experimental studies pertaining to the FT and crack growth of N-doped CNT/epoxy nanocomposites.
最近,掺氮碳纳米管(N-doped CNTs)在纳米复合材料设计中受到极大关注。开发预测模型以阐明其韧性行为已变得十分必要。在本研究中,采用多尺度分析方法预测了三种不同类型的掺 N 官能团(季铵型、吡咯型和吡啶型)的 CNT 对聚合物纳米复合材料的断裂韧性(FT)和裂纹生长的影响。为了从纳米尺度扩展到宏观尺度,采用了一种综合了分子动力学、微观力学理论、线性断裂力学理论和相场断裂模型(PFFM)的多尺度分析方法。通过考虑四种增韧机制(CNT 脱粘、塑性纳米形体生长、CNT 拔出和 CNT 断裂),量化了三种不同类型的 N 掺杂官能团的韧性增强趋势,并与实验结果进行了比较。结果表明,季铵盐官能团和吡啶官能团具有优异的相间和界面性能,可显著提高掺杂 N 的 CNT/环氧纳米复合材料的 FT 和抗裂纹生长性能。我们的研究为掺杂 N 的 CNT/epoxy 纳米复合材料的耐挠曲和抗裂纹生长实验研究提供了高性能解决方案。
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引用次数: 0
A strain-based criterion for predicting size-dependent fracture resistance of quasi-brittle materials under mixed mode loading 基于应变的标准,用于预测混合模式加载下准脆性材料随尺寸变化的抗断裂性
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-21 DOI: 10.1016/j.engfracmech.2024.110513
In the present study, a strain-based approach called the modified maximum tangential strain criterion has been developed for evaluating size effect on the mixed-mode fracture resistance of quasi-brittle materials. This approach relies on the generalized maximum tangential strain criterion, which considers the singular (K) and the first non-singular (T) terms of Williams series expansion. Furthermore, as an important and size-dependent parameter in the proposed criterion, a new formulation is presented to calculate the critical distance (rc). The predictions of the new criterion are compared not only with the available experimental data, but also with the results estimated by another size effect criterion named the modified maximum tangential stress criterion. It is shown that the proposed strain-based criterion is highly capable of estimating the size-dependent mixed-mode fracture behavior of quasi-brittle materials without requiring to compute the other higher order terms.
本研究开发了一种基于应变的方法,称为修正的最大切向应变准则,用于评估尺寸对准脆性材料混合模式断裂抗力的影响。这种方法依赖于广义最大切向应变准则,它考虑了威廉姆斯数列展开的奇异项(K)和第一非奇异项(T)。此外,在所提出的准则中,临界距离 (rc) 是一个重要的、与尺寸有关的参数,因此提出了一种新的计算公式。新准则的预测结果不仅与现有的实验数据进行了比较,还与另一种尺寸效应准则--修正的最大切向应力准则--的估计结果进行了比较。结果表明,所提出的基于应变的准则能够很好地估计准脆性材料与尺寸相关的混合模式断裂行为,而无需计算其他高阶项。
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引用次数: 0
Experimental study and life prediction for aero-engine turbine blade considering creep-fatigue interaction effect 考虑蠕变-疲劳相互作用效应的航空发动机涡轮叶片实验研究与寿命预测
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-20 DOI: 10.1016/j.engfracmech.2024.110507
As an important failure form of the turbine blade, creep-fatigue interaction damage affects the safe operation and maintenance strategy of aero-engine, and has been the focus of scientific research and the academic community. Firstly, based on the Kachanov-Rabotnov-Lemaitre continuum damage mechanics theory and the nonlinear symmetry of creep damage and fatigue damage, a creep-fatigue life prediction model is constructed considering the interaction effect in this paper. Then, based on the thermal-fluid–solid multi-physical field coupling numerical simulation of the turbine blade, the equivalent method of creep-fatigue load spectrum was explored according to the equal damage criterion and linear damage rule, and the creep-fatigue interaction test of smooth samples of the blade material was conducted to analyze the creep-fatigue fracture morphology. Finally, the stress term in the creep-fatigue life prediction model of blade material is modified by the correction factor α, and the modified creep-fatigue life prediction model of the turbine blade is constructed considering the interaction effect. The results show that the modified creep-fatigue life prediction model considering the interaction effect has a high life prediction ability with an error of 3.9%. The above research has important scientific research value for the life extension design of turbine blades and the improvement of aero-engine maintenance strategy.
作为涡轮叶片的一种重要失效形式,蠕变-疲劳交互损伤影响着航空发动机的安全运行和维护策略,一直是科学研究和学术界关注的焦点。本文首先基于 Kachanov-Rabotnov-Lemaitre 连续损伤力学理论和蠕变损伤与疲劳损伤的非线性对称性,构建了考虑相互作用效应的蠕变-疲劳寿命预测模型。然后,基于涡轮叶片的热-流-固多物理场耦合数值模拟,根据等效损伤准则和线性损伤规则,探索了蠕变-疲劳载荷谱的等效方法,并对叶片材料的光滑试样进行了蠕变-疲劳相互作用试验,分析了蠕变-疲劳断口形貌。最后,通过修正系数α对叶片材料蠕变疲劳寿命预测模型中的应力项进行修正,构建了考虑相互作用效应的涡轮叶片蠕变疲劳寿命预测模型。结果表明,考虑相互作用效应的修正蠕变疲劳寿命预测模型具有较高的寿命预测能力,误差为 3.9%。上述研究对涡轮叶片的延寿设计和航空发动机维护策略的改进具有重要的科研价值。
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引用次数: 0
Analysis of failure properties of red sandstone with structural plane subjected to true triaxial stress paths 真实三轴应力路径下具有结构平面的红色砂岩的破坏特性分析
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-19 DOI: 10.1016/j.engfracmech.2024.110490
In order to study the mechanical behavior and failure characteristics of rock mass with the structural plane in complex deep stress environment, the QKX-YB200 true triaxial rockburst test system, acoustic emission, and digital video recorder were adopted to conduct true triaxial loading and unloading indoor tests on the red sandstone cube specimens. The results show that: (1) Under true triaxial loading conditions, all specimens propagate in the form of anti-wing crack, and the dip angle of the structural plane is linearly related to the average value of the anti-wing crack propagation angle; under true triaxial unloading conditions, the specimens with structural plane dip angles of 30°, 45°, and 60° propagate in the form of wing crack, while those with a 90° angle propagate anti-wing cracks, and the closure of structural plane is related to the the crack type at the tips of structural plane. (2) The unstable failure stages in the stress–strain curve under true triaxial unloading are longer and exhibit more pronounced fluctuations; the peak strength of the specimens under the conditions of true triaxial loading and unloading decrease first and then increase with the increase of the dip angle, reaching the lowest at 45°. (3) During the true triaxial unloading tests, the rockburst degree of the intact rock specimens is more violent than that of the specimens with a structural plane. Additionally, the dip angle of the structural plane influences the severity of rockbursts under the same stress path. (4) The crack propagation mechanism and the closure degree of structural planes under different true triaxial stress paths and dip angles are discussed. It is observed that the crack initiation mode around the structural plane tips and the crack mode near free surface are closely related to the stress environment in different areas of the specimens. (5) Based on the indoor test results and previous experimental data, the differences in peak strength characteristics between open structural planes and closed structural planes are preliminarily analyzed and compared.
为研究复杂深应力环境下结构面岩体的力学行为和破坏特征,采用QKX-YB200真三轴岩爆试验系统、声发射和数字视频记录仪对红砂岩立方体试件进行了真三轴加载和卸载室内试验。结果表明(1)在真三轴加载条件下,所有试件均以反翼裂纹形式扩展,结构面倾角与反翼裂纹扩展角的平均值成线性关系;在真三轴卸载条件下,结构面倾角为 30°、45°和 60°的试件均以翼裂纹形式扩展,而倾角为 90°的试件均以反翼裂纹形式扩展,结构面的闭合程度与结构面尖端的裂纹类型有关。(2)真三轴卸载下应力-应变曲线的不稳定破坏阶段较长,且波动较明显;真三轴加载和卸载条件下试样的峰值强度随倾角的增大先减小后增大,45°时达到最低。(3) 在真三轴卸载试验中,完整岩石试件的岩爆程度比有结构平面的试件更剧烈。此外,在相同的应力路径下,结构平面的倾角也会影响岩爆的严重程度。(4) 讨论了不同真三轴应力路径和倾角下结构平面的裂纹扩展机理和闭合程度。结果表明,结构平面顶端周围的裂纹起始模式和自由表面附近的裂纹模式与试件不同区域的应力环境密切相关。(5) 根据室内试验结果和先前的实验数据,初步分析和比较了开放式结构平面和封闭式结构平面在峰值强度特性上的差异。
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引用次数: 0
Cyclic frictional response of rough rock joints under shear disturbances: Laboratory experiment and numerical simulation 粗糙岩缝在剪切扰动下的循环摩擦响应:实验室实验和数值模拟
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-19 DOI: 10.1016/j.engfracmech.2024.110514

The cyclic frictional response of rock joints under shear disturbances is critical for understanding the stability and durability of rock engineering structures. Laboratory experiments and numerical simulations were conducted to examine the effects of varying cyclic shear displacement amplitudes, frequencies, and cycle numbers on the macroscopic and microscopic shear characteristics of rough rock joints. The experimental results reveal significant differences in shear strength between the first few cycle and subsequent cycles during the cyclic shear process. As the number of shear cycles increases, the asperities on the contact surface gradually sustain damage, leading to a reduction in normal displacement. During cyclic shear, the peak shear load exhibits a two-stage variation with the number of cycles: an initial sharp decline followed by a gradual increase as the cycles proceed. The peak shear strength shows no obvious pattern under different shear displacement amplitudes and frequencies in the early stages of cyclic shear. As cyclic shear progresses, the peak shear strength decreases with increasing shear displacement amplitude but increases with higher shear frequency. Numerical simulations indicate that significant plastic deformation and shear wear occur on the joint surface during the initial cycles. The growth of the wear area is primarily concentrated in regions of stress concentration. Additionally, the simulations reveal that the volume of shear wear increase nonlinearly with the number of cycles. This research provides new insights into the cyclic shear behavior of rough rock joints and offers valuable references for engineering applications.

岩石节理在剪切扰动下的循环摩擦响应对于了解岩石工程结构的稳定性和耐久性至关重要。通过实验室实验和数值模拟,研究了不同循环剪切位移振幅、频率和循环次数对粗糙岩石节理的宏观和微观剪切特性的影响。实验结果表明,在循环剪切过程中,最初几个循环与随后的循环之间的剪切强度存在显著差异。随着剪切循环次数的增加,接触面上的凸起逐渐受到破坏,导致法向位移减小。在循环剪切过程中,峰值剪切载荷随循环次数的变化呈现出两个阶段:最初急剧下降,随后随着循环次数的增加而逐渐增加。在循环剪切的早期阶段,峰值剪切强度在不同的剪切位移振幅和频率下没有明显的变化规律。随着循环剪切的进行,峰值剪切强度随着剪切位移振幅的增大而减小,但随着剪切频率的增大而增大。数值模拟表明,在最初的循环中,接头表面会发生显著的塑性变形和剪切磨损。磨损区域的增长主要集中在应力集中区域。此外,模拟结果表明,剪切磨损量随循环次数的增加而非线性增加。这项研究为粗糙岩石接缝的循环剪切行为提供了新的见解,并为工程应用提供了有价值的参考。
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引用次数: 0
Microcracking evolution and clustering fractal characteristics in coal failure under multi step and cyclic loading 多级和循环加载下煤炭失效的微裂纹演化和聚类分形特征
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-19 DOI: 10.1016/j.engfracmech.2024.110511

During the deep mining process, coal mass encounter intricate geo-environmental stress, such as periodic weighting loading and repeatedly excavation unloading–reloading cycles, which weakens coal’s mechanical integrity and predisposing it to severe coalburst accidents. To investigate the microcracking damage mechanisms and predictive indicators in coal failure under in-situ stress analogs, the multistage step and cyclic loading experiments are conducted on cubic coal specimens. Acoustic emission (AE) technology is employed to track the spatiotemporal-energy evolution of stress-induced damages and discern the microcracking nature through AF/RA assessments, and the power-law scaling relation of AE activity near the catastrophic failure of coal is investigated. Then the clustering fractal structures of microcracking events in the stressed coal are quantified across temporal, spatial and energetic domains, utilizing correlation integral methodologies and b-value derivations from magnitude-frequency relation. Findings indicate that irrespective of the loading mode (step or cyclic), escalating stress triggers an intensification of irreversible fatigue deformations. AE characteristic parameters manifest a gradual rise, culminating in a precipitous peak coinciding with the critical failure point. This escalation adheres to a power-law correlation between AE occurrence frequency and time to failure, observable in the immediate pre-failure seconds, reflecting a universal attribute of coal fracture. Prior to ultimate failure, a marked increase in shear microcracks is discernible, despite tensile-dominated cracks (constituting about 80 % of total microcracks) prevailing as inferred from the variation of AF/RA values, aligning with an inferred “X” conjugate wedge splitting pattern from AE event density and energy mapping. The microcracking events in the loaded coal exhibit a clustering fractal structure that spans across temporal, spatial, and energetic (or magnitude) domains. Notably, the temporal fractal dimension, spatial fractal dimension, and b-value (i.e., a parameter characterized the energetic fractal dimension) all follow a parallel decrease pattern as the loading stress escalates, with a pronounced diminution becoming especially evident as the specimen approaches its catastrophic failure threshold. This insight offers fresh perspectives for predicting rock/coal dynamic disasters, emphasizing the necessity of concurrently monitoring the shift from diffuse microcracking to localized failure across time, space and energy domains. These research findings contribute to a deeper understanding of microcracking damage evolution and failure mechanism of loaded coal, and provide a foundational basis for early warning of rock failure such as the coalburst disasters.

在深部开采过程中,煤块会遇到错综复杂的地质环境应力,如周期性加重加载和反复的挖掘卸载再加载循环,从而削弱了煤的机械完整性,使其容易发生严重的爆煤事故。为了研究煤炭在原位应力模拟下的微裂纹破坏机理和预测指标,对立方体煤炭试样进行了多级阶跃加载和循环加载实验。采用声发射(AE)技术跟踪应力诱发损伤的时空能量演化,通过 AF/RA 评估判别微裂纹性质,并研究了煤炭灾难性破坏附近 AE 活动的幂律缩放关系。然后,利用相关积分法和从幅度-频率关系推导出的 b 值,对受压煤中微裂纹事件在时间、空间和能量域的聚类分形结构进行量化。研究结果表明,无论加载模式(阶跃或循环)如何,应力的增加都会引发不可逆疲劳变形的加剧。AE 特性参数表现为逐渐上升,最终达到与临界失效点相吻合的急剧峰值。这种上升与 AE 发生频率和失效时间之间的幂律相关,在失效前的几秒钟内即可观察到,反映了煤断裂的普遍特性。根据 AF/RA 值的变化推断,尽管拉伸裂纹(约占微裂纹总数的 80%)占主导地位,但在最终破坏之前,剪切微裂纹明显增加,这与根据 AE 事件密度和能量图推断的 "X "共轭楔形分裂模式一致。装载煤中的微裂纹事件呈现出一种跨越时间、空间和能量(或幅度)域的聚类分形结构。值得注意的是,随着加载应力的增加,时间分形维度、空间分形维度和 b 值(即表征能量分形维度的参数)都呈现出平行下降的模式,尤其是当试样接近灾难性破坏临界值时,下降趋势更为明显。这一洞察力为预测岩石/煤炭动态灾害提供了新的视角,强调了同时监测从弥散微裂纹到跨时间、空间和能量域局部破坏转变的必要性。这些研究成果有助于加深对加载煤的微裂纹损伤演变和破坏机理的理解,并为煤爆灾害等岩石破坏的早期预警提供了基础。
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引用次数: 0
Finite element analyses of rail head cracks: Predicting direction and rate of rolling contact fatigue crack growth 轨头裂纹的有限元分析:预测滚动接触疲劳裂纹增长的方向和速度
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-18 DOI: 10.1016/j.engfracmech.2024.110503

A numerical framework in 3D for predicting crack growth direction and rate in a rail head is presented. An inclined semi-circular surface-breaking gauge corner crack with frictionless crack faces is incorporated into a 60E1 rail model. The investigated load scenarios are wheel–rail contact, rail bending, thermal loading, and combinations of these. The crack growth direction is predicted using an accumulative vector crack tip displacement criterion, and Paris-type equations are employed to estimate crack growth rates. Results are evaluated along the crack front for varying crack radii and crack plane inclinations. Under the combined load cases and in the presence of tractive forces, the crack is generally predicted to go deeper into the rail than under pure contact. Crack growth rates for the combined load cases are higher than (but still close to) that for pure contact. A tractive force will increase growth rates for smaller cracks, whereas a steeper (45°) inclination will decrease the growth rate under the studied conditions as compared to a shallower (25°) inclination. Results should be of use for rail maintenance planning where deeper cracks require more machining efforts.

本文提出了一种三维数值框架,用于预测轨头裂纹的生长方向和速度。在 60E1 钢轨模型中加入了一条倾斜的半圆形断面轨角裂纹,裂纹表面无摩擦。研究的载荷情况包括轮轨接触、轨道弯曲、热载荷以及这些情况的组合。采用累积矢量裂纹尖端位移准则预测裂纹生长方向,并采用巴黎式方程估算裂纹生长率。对不同裂缝半径和裂缝平面倾斜度的裂缝前沿进行了评估。在组合载荷情况下和存在牵引力的情况下,与纯接触情况相比,裂纹一般会深入钢轨内部。综合载荷情况下的裂纹增长率高于(但仍接近)纯接触情况下的增长率。对于较小的裂缝,牵引力会增加其生长率,而与较浅(25°)的倾角相比,在研究条件下,较陡(45°)的倾角会降低其生长率。研究结果应有助于轨道维护规划,因为较深的裂纹需要更多的加工努力。
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引用次数: 0
Bound-constrained optimization using Lagrange multiplier for a length scale insensitive phase field fracture model 利用拉格朗日乘法器对长度尺度不敏感的相场断裂模型进行边界约束优化
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-18 DOI: 10.1016/j.engfracmech.2024.110496

The classical phase field model using the second-order geometric function α(φ)=φ2 (i.e., AT2 model), where φ0,1 is an auxiliary phase field variable representing material damage state, has wide applications in static and dynamic scenarios for brittle materials, but nonlinearity and inelasticity are found in its stress–strain curve. The phase field model using the linear geometric function α(φ)=φ (i.e., AT1 model), can avoid this, and a linear elastic threshold is available in its stress–strain curve. However, both AT2 and AT1 models are length scale sensitive phase field models, which could have difficulty in adjusting fracture strength and crack band simultaneously through a single parameter (the length scale). In this paper, a generalized quadratic geometric function (linear combination of AT1 and AT2 models) is used in the phase field model, where the extra parameter in this geometric function makes it a length scale insensitive phase field model. Similar to the AT1 model, negative phases can happen in the proposed generalized quadratic geometric function model. To solve this problem, a bound-constrained optimization using the Lagrange multiplier is derived, and the Karush–Kuhn–Tucker (KKT) conditions change from strain energy and maximum history strain energy (an indirect method acting on phase) to phase and Lagrange multiplier (a direct method acting on phase). Several simulations successfully validated the proposed model. A single element analysis and a bar under cyclic loading show the different stress–strain curves obtained from different models. A simulation of Mode I Brazilian test is compared with the experiment conducted by the authors, and two more simulations of Mode II shear test and mixed mode PMMA tensile test are compared with results from the literature.

使用二阶几何函数 α(φ)=φ2(即 AT2 模型)的经典相场模型,其中φ∈0,1 是代表材料损伤状态的辅助相场变量,在脆性材料的静态和动态场景中应用广泛,但其应力应变曲线存在非线性和非弹性。使用线性几何函数 α(φ)=φ(即 AT1 模型)的相场模型可以避免这种情况,其应力-应变曲线中存在线性弹性阈值。然而,AT2 和 AT1 模型都是对长度尺度敏感的相场模型,难以通过单一参数(长度尺度)同时调整断裂强度和裂缝带。本文在相场模型中采用了广义二次几何函数(AT1 和 AT2 模型的线性组合),该几何函数中的额外参数使其成为对长度尺度不敏感的相场模型。与 AT1 模型类似,在所提出的广义二次几何函数模型中也可能出现负相位。为解决这一问题,推导出了使用拉格朗日乘法器的有界约束优化方法,并将卡鲁什-库恩-塔克(KKT)条件从应变能和最大历史应变能(作用于相位的间接方法)改为相位和拉格朗日乘法器(作用于相位的直接方法)。多次模拟成功验证了所提出的模型。单元素分析和循环加载下的棒材显示了不同模型得到的不同应力-应变曲线。模式 I 巴西试验的模拟与作者进行的实验进行了比较,模式 II 剪切试验和混合模式 PMMA 拉伸试验的另外两个模拟与文献结果进行了比较。
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引用次数: 0
Investigation of a secondary bonded pultrusion composite laminate containing a ply-drop, Part 2: A novel two-dimensional hybrid fracture discrete element for producing debond failure 含有层降的二次粘接拉挤复合材料层压板的研究,第 2 部分:用于产生脱粘失效的新型二维混合断裂离散元素
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-17 DOI: 10.1016/j.engfracmech.2024.110494
This is the second of two papers in which a novel numerical method to predict the debond failure of a secondary bonded pultrusion laminate is presented. In Part 1 of this study, experimental work was described which is used here in the development, calibration and validation of the numerical model. The structure investigated in this work may be represented by a bonded composite laminate with external ply-drops (PDs).
In this part of the study, a fully coupled mixed mode cohesive zone model is developed which relies upon a traction-separation relation and the virtual crack closure technique to obtain the mode mixity. These are used to develop a hybrid fracture discrete element (HFDE). Fracture toughness tests, as well as tests on PD specimens are used to calibrate the model. Based on these tests, run-arrest fracture criteria are defined. The model is validated by comparing test results for two other PD specimen types to those obtained with the HFDE and finite element analyses.
本文是两篇论文中的第二篇,介绍了一种预测二次粘接拉挤层压板脱粘失效的新型数值方法。本研究的第一部分介绍了用于开发、校准和验证数值模型的实验工作。在这部分研究中,开发了一个完全耦合的混合模式内聚区模型,该模型依赖于牵引分离关系和虚拟裂缝闭合技术来获得模式混合度。这些用于开发混合断裂离散元素(HFDE)。断裂韧性测试以及 PD 试样测试用于校准模型。在这些测试的基础上,定义了奔溃断裂标准。通过将其他两种 PD 试样的测试结果与 HFDE 和有限元分析得出的结果进行比较,对模型进行了验证。
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引用次数: 0
Enhancing fatigue performance of AA6063-T6 fasteners through novel electromagnetic cold expansion using a double-frequency discharge 利用双频放电的新型电磁冷膨胀技术提高 AA6063-T6 紧固件的疲劳性能
IF 4.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-09-17 DOI: 10.1016/j.engfracmech.2024.110509

Non-contact electromagnetic cold expansion process (EMCE) represents a highly promising way to enhance the fatigue performance of fasteners. However, within the current technological framework, the necessity for dual power supplies and an accurate discharge control system has constrained the development and application of this technique. To address this, a novel EMCE process utilizing a double-frequency discharge is proposed. This process is accompanied by the development of an electromagnetic system with only one set of power supply to generate a current composed of a gradual-ascending and rapid-descending stage. This current induces a significant radially outward Lorentz force, facilitating hole expansion and introducing residual compressive stress around the hole, thus increasing the fatigue life of the fasteners. The experimental results demonstrate a remarkable enhancement in fatigue life for samples treated with the EMCE process when compared to untreated ones, showing an impressive 6.8-fold, 4.9-fold, and 1.6-fold increase at stress loads of 120 MPa, 130 MPa, and 150 MPa, respectively. Microstructural analysis reveals that the processed components exhibit favorable surface integrity, and there is no significant grain refinement near the hole. Moreover, it is found that there existed optimal current waveform to maximize fatigue life. These findings hold significance in understanding the EMCE process and advancing its practical applicability.

非接触式电磁冷膨胀工艺(EMCE)是一种非常有前途的提高紧固件疲劳性能的方法。然而,在当前的技术框架下,双电源和精确放电控制系统的必要性限制了这一技术的开发和应用。为解决这一问题,我们提出了一种利用双频放电的新型 EMCE 工艺。该工艺伴随着电磁系统的开发,只需一套电源,就能产生由渐进上升和快速下降阶段组成的电流。该电流可产生明显的径向向外洛伦兹力,促进孔的扩张,并在孔周围产生残余压应力,从而延长紧固件的疲劳寿命。实验结果表明,与未经处理的样品相比,经过 EMCE 工艺处理的样品疲劳寿命显著提高,在应力载荷为 120 兆帕、130 兆帕和 150 兆帕时,分别提高了 6.8 倍、4.9 倍和 1.6 倍。微观结构分析表明,加工后的部件表现出良好的表面完整性,孔附近没有明显的晶粒细化。此外,还发现存在最佳电流波形,可最大限度地延长疲劳寿命。这些发现对理解 EMCE 工艺和推进其实际应用具有重要意义。
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Engineering Fracture Mechanics
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