首先阐明组合法求解有限板多孔MSD(multiple site damage)应力强度因子的基本原理,然后就组合法运用中比较难以解决的多孔边裂纹间的修正系数问题,提出一种基于复变函数法的有效解决方法。将完善后的组合法应用于有限板多孔MSD应力强度...首先阐明组合法求解有限板多孔MSD(multiple site damage)应力强度因子的基本原理,然后就组合法运用中比较难以解决的多孔边裂纹间的修正系数问题,提出一种基于复变函数法的有效解决方法。将完善后的组合法应用于有限板多孔MSD应力强度因子的求解,计算某型飞机典型铆接壁板无主裂纹和含主裂纹两种情况的数值算例。通过与有限元结果的比较可知,该方法的计算结果精确、可靠,计算过程简单、易行。提出的近似解析方法能很好地应用于任意分布的有限板多孔MSD裂纹结构,在工程断裂问题中有较好的应用价值。展开更多
考虑到飞机结构的多部位损伤(MSD,Multiple Site Damage)结构裂纹萌生位置的不同可能对结构的安全性能存在影响,分析结构失效概率对各应力集中部位裂纹萌生寿命和应力的敏感性,量化其对结构安全性能的影响.裂纹萌生寿命采用对数正态模型...考虑到飞机结构的多部位损伤(MSD,Multiple Site Damage)结构裂纹萌生位置的不同可能对结构的安全性能存在影响,分析结构失效概率对各应力集中部位裂纹萌生寿命和应力的敏感性,量化其对结构安全性能的影响.裂纹萌生寿命采用对数正态模型,通过定义核函数建立MSD结构失效的敏感性分析模型,采用Monte-Carlo模拟计算概率敏感度.该方法利用Monte-Carlo概率分析的结果,只需增加少许计算量即可得到失效概率对参数的敏感度.将该方法应用于共线多孔板分析,得到了给定寿命下失效概率对各关键位置应力和裂纹萌生寿命对数均值的敏感度,从而确定了对结构安全影响最大的位置.展开更多
老龄飞机中由于多裂纹的产生将导致结构剩余寿命大幅削减。针对如飞机机舱上布有沿纵向铆钉接头的隔板结构,文中给出一种分析多部位损伤结构剩余强度的方法。裂纹扩展模型是分析的基础,文中对两类(单参量和三参量)扩展模型进行讨论,给...老龄飞机中由于多裂纹的产生将导致结构剩余寿命大幅削减。针对如飞机机舱上布有沿纵向铆钉接头的隔板结构,文中给出一种分析多部位损伤结构剩余强度的方法。裂纹扩展模型是分析的基础,文中对两类(单参量和三参量)扩展模型进行讨论,给出裂纹在增量载荷下萌生与稳定扩展的处理方法。基于Irwin和Dugdale裂尖张开位移模型与Swift准则,给出较为完整的分析多部位损伤(multiple site damage,MSD)结构剩余强度的方法。最后,通过对飞机压力舱上的沿纵向铆钉接头的模拟计算,对文中方法进行验证。由分析结果可知,采用文中方法计算得到的剩余强度值与试验值符合得较好,该方法能较为准确有效地对复杂MSD结构的剩余强度进行分析。展开更多
针对飞机结构中存在的多部位损伤(MSD,Multiple Side Damage)问题,对预腐蚀后多细节结构MSD发生概率进行分析研究.预腐蚀条件选为3.5%NaCl溶液浸泡240 h.通过7B04-T74铝合金单细节预腐蚀-疲劳及常规环境疲劳试验,得到了预腐蚀影响系数C...针对飞机结构中存在的多部位损伤(MSD,Multiple Side Damage)问题,对预腐蚀后多细节结构MSD发生概率进行分析研究.预腐蚀条件选为3.5%NaCl溶液浸泡240 h.通过7B04-T74铝合金单细节预腐蚀-疲劳及常规环境疲劳试验,得到了预腐蚀影响系数C.确定了预腐蚀后的MSD发生概率与常规疲劳试验MSD发生概率之间的关系.建立了预腐蚀后的MSD发生概率公式.通过与试验结果对比表明:新的公式可以很好地反映试验结果.展开更多
Two simple and effective control strategies for a multi-axle heavy truck, modified skyhook damping (MSD) control and proportional-integration-derivative (PID) control, were implemented into functional virtual prototyp...Two simple and effective control strategies for a multi-axle heavy truck, modified skyhook damping (MSD) control and proportional-integration-derivative (PID) control, were implemented into functional virtual prototype (FVP) model and compared in terms of road friendliness and ride comfort. A four-axle heavy truck-road coupling system model was established using FVP technology and validated through a ride comfort test. Then appropriate passive air suspensions were chosen to replace the rear tandem suspensions of the original truck model for preliminary optimization. The mechanical properties and time lag of dampers were taken into account in simulations of MSD and PID semi-active dampers implemented using MATLAB/Simulink. Through co-simulations with Adams and MATLAB, the effects of semi-active MSD and PID control were analyzed and compared, and control parameters which afforded the best comprehensive performance for each control strategy were chosen. Simulation results indicate that compared with the passive air suspension truck, semi-active MSD control improves both ride comfort and road-friendliness markedly, with optimization ratios of RMS vertical acceleration and RMS tyre force ranging from 10.1% to 44.8%. However, semi-active PID control only reduces vertical vibration of the driver's seat by 11.1%, 11.1% and 10.9% on A, B and C level roads respectively. Both strategies are robust to the variation of road level.展开更多
应力强度因子(Stress intensity factor,SIF)分析是含多部位损伤(Multiple site damage,MSD)结构剩余强度和裂纹扩展寿命预测的基础和关键。考虑接触与摩擦,建立了含MSD搭接结构的三维有限元模型,研究了不同裂纹长度、铆钉类型以及损伤...应力强度因子(Stress intensity factor,SIF)分析是含多部位损伤(Multiple site damage,MSD)结构剩余强度和裂纹扩展寿命预测的基础和关键。考虑接触与摩擦,建立了含MSD搭接结构的三维有限元模型,研究了不同裂纹长度、铆钉类型以及损伤模式下裂纹尖端SIF分布情况和变化规律。结果表明,搭接件孔边裂纹Ⅰ型SIF起主导作用,Ⅱ型和Ⅲ型SIF可忽略不计。由于次弯曲、铆钉变形和板厚度等因素,SIF在外表面最小,接触面一侧较大,最大值多位于蒙皮内部。MSD会使裂纹间的干涉作用增强,SIF增大,且裂纹间距离越近干涉作用越强。裂纹长度相同时,埋头铆钉的孔边裂纹SIF积分均值大于平头铆钉,且接触面的SIF埋头铆钉大于平头铆钉,外表面则相反。展开更多
Two methods currently available for evaluating the probability of Multiple Site Damage(MSD)occurrence were studied in this paper.One of the methods is a probabilistic analysis approach based on the statistical theory ...Two methods currently available for evaluating the probability of Multiple Site Damage(MSD)occurrence were studied in this paper.One of the methods is a probabilistic analysis approach based on the statistical theory and fatigue characteristics of each structural detail,and the other is an approach which defines the initial damage scenario by means of Monte-Carlo simulation,and multiple initial crack scenarios are randomly generated.A modified method based on the Monte-Carlo simulation was proposed in this paper,in which the random fluctuation of the stress was considered to give more accurate evaluation results.In the presented method,the probability of MSD occurrence in a structural element containing multiple details was calculated based on the Monte-Carlo simulation and the p-S-N curve of a single structural detail.Fatigue tests were accomplished using specimens containing 21-similar-details to obtain the fatigue life corresponding to MSD occurrence.Tests on single-detail specimens and static calibration tests were also conducted to get the basic fatigue properties of the material and the degree of stress fluctuation.The aforementioned three methods were compared and validated via the test results.The influence of the stress random fluctuation degree on the probability of MSD occurrence and influence of the distribution types on evaluating the MSD occurrence probability were discussed.展开更多
文摘首先阐明组合法求解有限板多孔MSD(multiple site damage)应力强度因子的基本原理,然后就组合法运用中比较难以解决的多孔边裂纹间的修正系数问题,提出一种基于复变函数法的有效解决方法。将完善后的组合法应用于有限板多孔MSD应力强度因子的求解,计算某型飞机典型铆接壁板无主裂纹和含主裂纹两种情况的数值算例。通过与有限元结果的比较可知,该方法的计算结果精确、可靠,计算过程简单、易行。提出的近似解析方法能很好地应用于任意分布的有限板多孔MSD裂纹结构,在工程断裂问题中有较好的应用价值。
文摘考虑到飞机结构的多部位损伤(MSD,Multiple Site Damage)结构裂纹萌生位置的不同可能对结构的安全性能存在影响,分析结构失效概率对各应力集中部位裂纹萌生寿命和应力的敏感性,量化其对结构安全性能的影响.裂纹萌生寿命采用对数正态模型,通过定义核函数建立MSD结构失效的敏感性分析模型,采用Monte-Carlo模拟计算概率敏感度.该方法利用Monte-Carlo概率分析的结果,只需增加少许计算量即可得到失效概率对参数的敏感度.将该方法应用于共线多孔板分析,得到了给定寿命下失效概率对各关键位置应力和裂纹萌生寿命对数均值的敏感度,从而确定了对结构安全影响最大的位置.
文摘老龄飞机中由于多裂纹的产生将导致结构剩余寿命大幅削减。针对如飞机机舱上布有沿纵向铆钉接头的隔板结构,文中给出一种分析多部位损伤结构剩余强度的方法。裂纹扩展模型是分析的基础,文中对两类(单参量和三参量)扩展模型进行讨论,给出裂纹在增量载荷下萌生与稳定扩展的处理方法。基于Irwin和Dugdale裂尖张开位移模型与Swift准则,给出较为完整的分析多部位损伤(multiple site damage,MSD)结构剩余强度的方法。最后,通过对飞机压力舱上的沿纵向铆钉接头的模拟计算,对文中方法进行验证。由分析结果可知,采用文中方法计算得到的剩余强度值与试验值符合得较好,该方法能较为准确有效地对复杂MSD结构的剩余强度进行分析。
文摘针对飞机结构中存在的多部位损伤(MSD,Multiple Side Damage)问题,对预腐蚀后多细节结构MSD发生概率进行分析研究.预腐蚀条件选为3.5%NaCl溶液浸泡240 h.通过7B04-T74铝合金单细节预腐蚀-疲劳及常规环境疲劳试验,得到了预腐蚀影响系数C.确定了预腐蚀后的MSD发生概率与常规疲劳试验MSD发生概率之间的关系.建立了预腐蚀后的MSD发生概率公式.通过与试验结果对比表明:新的公式可以很好地反映试验结果.
基金Projects(51078087, 51178158) supported by the National Natural Science Foundation of ChinaProject(11040606Q39) supported by the Natural Science Foundation of Anhui Province, ChinaProjects(2012HGQC0015, 2011HGBZ0945) supported by the Fundamental Research Funds for the Central Universities
文摘Two simple and effective control strategies for a multi-axle heavy truck, modified skyhook damping (MSD) control and proportional-integration-derivative (PID) control, were implemented into functional virtual prototype (FVP) model and compared in terms of road friendliness and ride comfort. A four-axle heavy truck-road coupling system model was established using FVP technology and validated through a ride comfort test. Then appropriate passive air suspensions were chosen to replace the rear tandem suspensions of the original truck model for preliminary optimization. The mechanical properties and time lag of dampers were taken into account in simulations of MSD and PID semi-active dampers implemented using MATLAB/Simulink. Through co-simulations with Adams and MATLAB, the effects of semi-active MSD and PID control were analyzed and compared, and control parameters which afforded the best comprehensive performance for each control strategy were chosen. Simulation results indicate that compared with the passive air suspension truck, semi-active MSD control improves both ride comfort and road-friendliness markedly, with optimization ratios of RMS vertical acceleration and RMS tyre force ranging from 10.1% to 44.8%. However, semi-active PID control only reduces vertical vibration of the driver's seat by 11.1%, 11.1% and 10.9% on A, B and C level roads respectively. Both strategies are robust to the variation of road level.
文摘应力强度因子(Stress intensity factor,SIF)分析是含多部位损伤(Multiple site damage,MSD)结构剩余强度和裂纹扩展寿命预测的基础和关键。考虑接触与摩擦,建立了含MSD搭接结构的三维有限元模型,研究了不同裂纹长度、铆钉类型以及损伤模式下裂纹尖端SIF分布情况和变化规律。结果表明,搭接件孔边裂纹Ⅰ型SIF起主导作用,Ⅱ型和Ⅲ型SIF可忽略不计。由于次弯曲、铆钉变形和板厚度等因素,SIF在外表面最小,接触面一侧较大,最大值多位于蒙皮内部。MSD会使裂纹间的干涉作用增强,SIF增大,且裂纹间距离越近干涉作用越强。裂纹长度相同时,埋头铆钉的孔边裂纹SIF积分均值大于平头铆钉,且接触面的SIF埋头铆钉大于平头铆钉,外表面则相反。
文摘Two methods currently available for evaluating the probability of Multiple Site Damage(MSD)occurrence were studied in this paper.One of the methods is a probabilistic analysis approach based on the statistical theory and fatigue characteristics of each structural detail,and the other is an approach which defines the initial damage scenario by means of Monte-Carlo simulation,and multiple initial crack scenarios are randomly generated.A modified method based on the Monte-Carlo simulation was proposed in this paper,in which the random fluctuation of the stress was considered to give more accurate evaluation results.In the presented method,the probability of MSD occurrence in a structural element containing multiple details was calculated based on the Monte-Carlo simulation and the p-S-N curve of a single structural detail.Fatigue tests were accomplished using specimens containing 21-similar-details to obtain the fatigue life corresponding to MSD occurrence.Tests on single-detail specimens and static calibration tests were also conducted to get the basic fatigue properties of the material and the degree of stress fluctuation.The aforementioned three methods were compared and validated via the test results.The influence of the stress random fluctuation degree on the probability of MSD occurrence and influence of the distribution types on evaluating the MSD occurrence probability were discussed.
