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Experimental investigation and life prediction for the load spectrum with flight mission characteristics on a P/M superalloy
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作者 Renjie JIANG Xiaoguang YANG +2 位作者 Muwei CHENG Jia HUANG Duoqi SHI 《Chinese Journal of Aeronautics》 2025年第3期403-412,共10页
The service load on high temperature rotating components of aero-engines generally exhibits flight mission characteristics. The general shape of the load spectrum is that Type Ⅲ/Ⅳ cyclic loading and creep loading ar... The service load on high temperature rotating components of aero-engines generally exhibits flight mission characteristics. The general shape of the load spectrum is that Type Ⅲ/Ⅳ cyclic loading and creep loading are superimposed on Type Ⅰ cyclic loading. Meanwhile, the sequence of the Type Ⅲ/Ⅳ cyclic and creep loading varies with mission. This work performed load spectrum test with this characteristic on the Ni-based alloy FGH96. Then a life prediction method was developed based on the Chaboche fatigue damage accumulation model and a modified time fraction model. Creep followed by Fatigue (C-F) test was carried out to reveal the creep-fatigue interaction and calibrate parameters. The results show that most test results fall within the 2-fold deviation band. The sequence of creep-fatigue loading within the load spectrum exhibited a limited effect on life. Finally, simplified methods were developed to improve analysis efficiency, and cases where simplified methods could replace the proposed method were discussed. 展开更多
关键词 load spectrum Life prediction Flight mission loading sequence Niclel alloys
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An Artificial Intelligence-Based Scheme for Structural Health Monitoring in CFRE Laminated Composite Plates under Spectrum Fatigue Loading
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作者 Wael A.Altabey 《Structural Durability & Health Monitoring》 2025年第5期1145-1165,共21页
In the fabrication and monitoring of parts in composite structures,which are being used more and more in a variety of engineering applications,the prediction and fatigue failure detection in composite materials is a d... In the fabrication and monitoring of parts in composite structures,which are being used more and more in a variety of engineering applications,the prediction and fatigue failure detection in composite materials is a difficult problem.This difficulty arises from several factors,such as the lack of a comprehensive investigation of the fatigue failure phenomena,the lack of a well-defined fatigue damage theory used for fatigue damage prediction,and the inhomogeneity of composites because of their multiple internal borders.This study investigates the fatigue behavior of carbon fiber reinforced with epoxy(CFRE)laminated composite plates under spectrum loading utilizing a uniqueDeep LearningNetwork consisting of a convolutional neural network(CNN).Themethod includes establishing Finite Element Model(FEM)in a plate model under a spectrum fatigue loading.Then,a CNN is trained for fatigue behavior prediction.The training phase produces promising results,showing the model’s performance with 94.21%accuracy,92.63%regression,and 91.55%F-score.To evaluate the model’s reliability,a comparison is made between fatigue data from the CNN and the FEM.It was found that the error band for this comparison is less than 0.3878MPa,affirming the accuracy and reliability of the proposed technique.The proposed method results converge with available experimental results in the literature,thus,the study suggests the broad applicability of this method to other different composite structures. 展开更多
关键词 Deep learning structural health monitoring(SHM) CFRE convolutional neural network(CNN) spectrum fatigue loading composite plates
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Equivalent Constant Amplitude Spectrum Design Method and Experimental Verification of Structural Crack Growth Flight⁃by⁃Flight Spectrum
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作者 ZHU Gaoshang ZHAO Qia CAO Jing 《Transactions of Nanjing University of Aeronautics and Astronautics》 2026年第1期85-94,共10页
In fatigue damage tolerance verification tests of aircraft structures,the simulation and loading of flight-byflight spectra require considerable time and resources.To improve the efficiency of load spectrum design and... In fatigue damage tolerance verification tests of aircraft structures,the simulation and loading of flight-byflight spectra require considerable time and resources.To improve the efficiency of load spectrum design and testing,an equivalent constant-amplitude spectrum design method for flight-by-flight spectra is proposed based on the equivalence of crack growth behavior.By combining the Paris crack growth model with the Walker stress ratio correction,the equivalent stress amplitude is directly calculated using structural parameters and load spectrum characteristics,enabling a rapid transformation from variable-amplitude spectra to constant-amplitude spectra.The original spectrum is discretized based on the load-exceedance curve,and the equivalence relationship between multilevel block spectra and constant-amplitude spectra is established.Taking a typical lower wing skin structure of a transport aircraft as an example,two equivalent spectra are designed and validated through fatigue crack growth tests on 2024-T351 center-hole plate specimens.The experimental results show that the fatigue life deviation between the equivalent spectra and the original flight-by-flight spectrum is within 10%,demonstrating the effectiveness of the proposed method.Moreover,the equivalent spectrum constructed under the condition of invariant mean flight stress exhibits higher equivalence accuracy.The influence of spectral shape on the equivalent stress amplitude is further analyzed,revealing that the equivalent stress amplitude increases with the spectrum shape coefficient.The proposed method provides a useful reference for load spectrum design in aircraft structural damage tolerance verification tests. 展开更多
关键词 aircraft structure crack growth fatigue load spectrum equivalent test stress intensity factor
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Load spectrum analysis for combined frame of closed high-speed press 被引量:1
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作者 郑恩来 贾方 +1 位作者 张志胜 史金飞 《Journal of Southeast University(English Edition)》 EI CAS 2011年第1期40-46,共7页
Based on the basic theory of mechanics,kinematic and dynamic analysis for a slider-crank mechanism with a balance mechanism is performed.The theoretical formula of the load spectrum for the interaction between the cra... Based on the basic theory of mechanics,kinematic and dynamic analysis for a slider-crank mechanism with a balance mechanism is performed.The theoretical formula of the load spectrum for the interaction between the crank shaft and the bearing seat of the upper beam is achieved by approximately simplifying the mechanical model of the crank shaft.The simulation for the load spectrum data of combined frame under the operating conditions of blanking or piling is performed using Matlab and the law of the load spectrum curves under these two conditions is analyzed.The simulation results show that under a no-load condition,the load spectrum curves of the interaction between the crank shaft and the bearing seat of the upper beam present a form of periodic sine wave and under the piling condition,the load spectrum curves of the interaction between the crank shaft and the bearing seat of the upper beam present a form of periodic pulse wave.The simulation results can provide a theoretical foundation for the load determination during the process of analyzing the dynamic characteristics on the combined frame of a closed high-speed press through the finite element method. 展开更多
关键词 PRESS load spectrum crank shaft slider-crank mechanism
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Rain-Flow and Reverse Rain-Flow Counting Method for the Compilation of Fatigue Load Spectrum 被引量:3
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作者 宋玉普 王立成 李朝阳 《China Ocean Engineering》 SCIE EI 2001年第3期429-435,共7页
The rain-flow counting method is widely used to compile the fatigue load spectrum, The second stage counting of the rain-flow method is a troublesome process. In order to overcome this drawback, the rain-flow and reve... The rain-flow counting method is widely used to compile the fatigue load spectrum, The second stage counting of the rain-flow method is a troublesome process. In order to overcome this drawback, the rain-flow and reverse rain-flow counting method is proposed in this paper. In this counting method, the rule for counting of the rain-flow method is modified, so that the sequence of load-time need not be adjusted. This is a valid and useful method to count cycles and compile the load spectrum and it can be widely used in ocean engineering. 展开更多
关键词 rain-flow reverse rain-flow load spectrum FATIGUE
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Filtering Method of Aero⁃engine Load Spectrum Based on Rain Flow Counting 被引量:4
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作者 XU Cong SUN Zhigang +1 位作者 LU Qi SONG Yingdong 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2020年第6期947-954,共8页
A filtering method of aero-engine load spectrum based on the rain flow counting is proposed in this paper.Firstly,the original load spectrum is counted through the rain flow method to get the peak and valley values.Th... A filtering method of aero-engine load spectrum based on the rain flow counting is proposed in this paper.Firstly,the original load spectrum is counted through the rain flow method to get the peak and valley values.Then,some data points in the original load spectrum are added between the peak and valley values.Finally,the filtering spectrum is obtained.The proposed method can reflect the path information of the original load spectrum.In addition,it can also eliminate the noise in the signal and improve the efficiency of signal processing,which is of practical significance for the research of aero-engine. 展开更多
关键词 load spectrum FILTERING rain flow counting AERO-ENGINE
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Improved Data Processing of Loading Spectrum for Applications of Rainflow Counting Method
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作者 吕志强 彭卫文 黄洪钟 《Journal of Donghua University(English Edition)》 EI CAS 2015年第6期919-922,共4页
The rainflow counting method is a reasonable cyclecounting procedure for fatigue life calculation and simulation testing of structures.It defines cycles as closed stress /strain hysteresis loops.Application of the rai... The rainflow counting method is a reasonable cyclecounting procedure for fatigue life calculation and simulation testing of structures.It defines cycles as closed stress /strain hysteresis loops.Application of the rainflow counting method requires a data processing of the loading spectrum,which consists of the elimination of non-peak value data points,load time histories adjustment and loop extraction.In the data processing of the loading spectrum,if a stress point is neither the peak nor the valley,it will be identified and eliminated from the loading spectrum.Generally,the loading process is idealized as a single peak-valley straight line.But in actually,there are polylines or nearly straight lines between peaks and valleys which can't be ignored.Therefore,in the process of eliminating such data points,it will produce error in method itself.To reduce the error produced by the traditional method itself,a new method which can well simplify the polylines in data processing of loading spectrum is proposed in this paper.Comparing with the original approximation method,the proposed method has higher precision. 展开更多
关键词 fatigue life rainflow counting method loading spectrum LOOP peaks and valleys
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Research on Adaptive TSSA-HKRVM Model for Regression Prediction of Crane Load Spectrum
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作者 Dong Qing Qi Song +1 位作者 Shuangyun Huang Gening Xu 《Computer Modeling in Engineering & Sciences》 SCIE EI 2023年第9期2345-2370,共26页
For the randomness of crane working load leading to the decrease of load spectrum prediction accuracy with time,an adaptive TSSA-HKRVM model for crane load spectrum regression prediction is proposed.The heterogeneous ... For the randomness of crane working load leading to the decrease of load spectrum prediction accuracy with time,an adaptive TSSA-HKRVM model for crane load spectrum regression prediction is proposed.The heterogeneous kernel relevance vector machine model(HKRVM)with comprehensive expression ability is established using the complementary advantages of various kernel functions.The combination strategy consisting of refraction reverse learning,golden sine,and Cauchy mutation+logistic chaotic perturbation is introduced to form a multi-strategy improved sparrow algorithm(TSSA),thus optimizing the relevant parameters of HKRVM.The adaptive updatingmechanismof the heterogeneous kernel RVMmodel under themulti-strategy improved sparrow algorithm(TSSA-HKMRVM)is defined by the sliding window design theory.Based on the sample data of the measured load spectrum,the trained adaptive TSSA-HKRVMmodel is employed to complete the prediction of the crane equivalent load spectrum.Applying this method toQD20/10 t×43m×12mgeneral bridge crane,the results show that:compared with other prediction models,although the complexity of the adaptive TSSA-HKRVMmodel is relatively high,the prediction accuracy of the load spectrum under long periods has been effectively improved,and the completeness of the load information during thewhole life cycle is relatively higher,with better applicability. 展开更多
关键词 Heterogeneous kernel function RVM TSSA adaptive update mechanism equivalent load spectrum
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Study on fatigue life prediction under spectrum loading 被引量:2
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作者 WU Ying XIE Li-yang ZHANG Xiao-jin 《材料与冶金学报》 CAS 2011年第2期150-153,共4页
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TREATMENT OF COMPLEX LOAD HISTORY AND CONSTRUCTION OF FATIGUE LOAD SPECTRUM
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作者 Ping An Wang Dejun(Northeastern University) 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 1994年第4期320-323,共17页
A new, more actual approach for omitting small loads in a loading history was pres-ented according to crack closure, and load interactive effects which are large on damage of com-ponents were studied. Intrinsic period... A new, more actual approach for omitting small loads in a loading history was pres-ented according to crack closure, and load interactive effects which are large on damage of com-ponents were studied. Intrinsic periodic spectrum block representing a damage element of a loadhistory, a new concept, was put out. It has been proven by theoretic analysis and tests that themodes of constructing fatigue loading spectrum have little effect on damage of components,which will change the incomplete knowledges on constructing fatigue spectrum ago. 展开更多
关键词 Fatigue loading spectrum DAMAGE Crack closure
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着陆工况下飞行汽车动力学建模与冲击载荷分析
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作者 王美靖 阮新建 +4 位作者 李益涵 赵又群 王博 招启军 郭硕 《重庆理工大学学报(自然科学)》 北大核心 2026年第3期20-26,共7页
针对某型重载飞行汽车垂直着陆工况,提出一套集成的多体动力学建模与仿真方法。基于Kane方法构建包含车身6自由度运动与4个车轮垂向运动的10自由度全车动力学模型,描述着陆过程中的车身悬架轮胎耦合机制。通过数值仿真,分析飞行汽车以1 ... 针对某型重载飞行汽车垂直着陆工况,提出一套集成的多体动力学建模与仿真方法。基于Kane方法构建包含车身6自由度运动与4个车轮垂向运动的10自由度全车动力学模型,描述着陆过程中的车身悬架轮胎耦合机制。通过数值仿真,分析飞行汽车以1 m/s速度垂直着陆时关键连接点的动态载荷响应,完成了载荷谱与频谱的定量分析。结果表明:着陆过程中悬架系统承受的冲击载荷最显著,最大载荷出现在弹簧上安装点,转向系统所受冲击较小。频谱分析显示,悬架部位未出现明显共振频率,而转向连接点在极低频区(<1 Hz)表现出显著的动态响应。该模型可有效模拟飞行汽车从触地到稳定的全过程动力学行为,为飞行汽车着陆系统的结构设计、载荷评估与动态优化提供参考。 展开更多
关键词 飞行汽车 底盘振动 冲击载荷 载荷谱分析 频谱分析
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Coupling Singular Spectrum Analysis with Artificial Neural Network to Improve Accuracy of Sediment Load Prediction
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作者 Sokchhay Heng Tadashi Suetsugi 《Journal of Water Resource and Protection》 2013年第4期395-404,共10页
Sediment load estimation is generally required for study and development of water resources system. In this regard, artificial neural network (ANN) is the most widely used modeling tool especially in data-constraint r... Sediment load estimation is generally required for study and development of water resources system. In this regard, artificial neural network (ANN) is the most widely used modeling tool especially in data-constraint regions. This research attempts to combine SSA (singular spectrum analysis) with ANN, hereafter called SSA-ANN model, with expectation to improve the accuracy of sediment load predicted by the existing ANN approach. Two different catchments located in the Lower Mekong Basin (LMB) were selected for the study and the model performance was measured by several statistical indices. In comparing with ANN, the proposed SSA-ANN model shows its better performance repeatedly in both catchments. In validation stage, SSA-ANN is superior for larger Nash-Sutcliffe Efficiency about 24% in Ban Nong Kiang catchment and 7% in Nam Mae Pun Luang catchment. Other statistical measures of SSA-ANN are better than those of ANN as well. This improvement reveals the importance of SSA which filters noise containing in the raw time series and transforms the original input data to be near normal distribution which is favorable to model simulation. This coupled model is also recommended for the prediction of other water resources variables because extra input data are not required. Only additional computation, time series decomposition, is needed. The proposed technique could be potentially used to minimize the costly operation of sediment measurement in the LMB which is relatively rich in hydrometeorological records. 展开更多
关键词 Artificial NEURAL Network SINGULAR spectrum Analysis Coupled Model SEDIMENT load MEKONG BASIN
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基于设计载荷谱的纯电动乘用车减速器壳体疲劳寿命分析
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作者 邹喜红 周振 +3 位作者 周雨航 袁冬梅 熊锋 杨皓理 《兵器装备工程学报》 北大核心 2026年第2期17-23,共7页
针对某型纯电动乘用车减速器壳体疲劳寿命分析,存在开发周期长、预测结果差等问题,提出了一种基于设计载荷谱的某型纯电动乘用车减速器壳体疲劳寿命分析方法。本文利用采集减速器实测载荷谱,采用雨流计数法获取载荷谱均幅值频次分布,采... 针对某型纯电动乘用车减速器壳体疲劳寿命分析,存在开发周期长、预测结果差等问题,提出了一种基于设计载荷谱的某型纯电动乘用车减速器壳体疲劳寿命分析方法。本文利用采集减速器实测载荷谱,采用雨流计数法获取载荷谱均幅值频次分布,采用威布尔分布模型和正态分布模型分别对幅值与均值进行检验,并用参数法外推获得全寿命周期,以此推断恶劣工况极大载荷值,采用雨流矩阵模拟法获取时域重构设计载荷谱。在此基础上,建立减速器有限元模型,并基于实测载荷谱进行模型验证,分别在实测载荷谱和设计载荷谱2种载荷作用下,进行仿真分析,采用名义应力法,结合线性累积损伤理论和修正材料的S-N曲线对壳体进行疲劳寿命分析。结果表明,实测载荷谱和设计载荷谱作用下减速器壳体的损伤值相差较小,在保留计算精度的情况下,设计载荷谱能极大缩短减速器疲劳开发周期。 展开更多
关键词 某型纯电动乘用车 减速器壳体 设计载荷谱 疲劳寿命
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基于钎杆应力波分析的凿岩机辐射噪声产生机制与估测方法
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作者 高波 吴腾飞 朱高 《凿岩机械气动工具》 2026年第3期4-7,共4页
为揭示凿岩机辐射噪声的产生机制并开发一种便捷的现场噪声评估方法,聚焦钎杆弯曲应力波的传播特性及其与噪声的关联机制,阐明弯曲波的激发条件与传播规律;利用实验系统同步测量了YT24型与YO18型凿岩机钎杆的纵波与弯曲波应力。研究结... 为揭示凿岩机辐射噪声的产生机制并开发一种便捷的现场噪声评估方法,聚焦钎杆弯曲应力波的传播特性及其与噪声的关联机制,阐明弯曲波的激发条件与传播规律;利用实验系统同步测量了YT24型与YO18型凿岩机钎杆的纵波与弯曲波应力。研究结果表明,弯曲波主要由活塞撞击的偏心分量激发,其幅值与撞击速度及偏心距成正比;辐射噪声声压与弯曲波应力幅值存在显著的正相关关系。基于此,提出一种通过钎杆应力波检测间接估算凿岩机噪声级的方法,即基于已知型号凿岩机的噪声标定值及应力波幅值比,成功估算出另一型号凿岩机的噪声级。该方法将复杂的声学测量转化为易实施的力学信号测量,为现场快速评估凿岩机噪声提供了创新途径。 展开更多
关键词 凿岩机 辐射噪声 钎杆 弯曲波 应力波 噪声估测 冲击速度 载荷谱
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大长细比异形飞翼的风振响应特性研究
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作者 曹旭阳 张则宝 +1 位作者 李强 唐旭扬 《机械设计与制造》 北大核心 2026年第3期1-5,共5页
风荷载是影响高层及大跨度结构的重要动载荷之一,风致振动效应对结构的影响不可忽略。在完成某艺术场馆可动飞翼设计的基础上,为研究脉动风对工作状态下的大长细比飞翼强度及变形的影响,利用Davenport风速谱并采用线性滤波法中的自回归A... 风荷载是影响高层及大跨度结构的重要动载荷之一,风致振动效应对结构的影响不可忽略。在完成某艺术场馆可动飞翼设计的基础上,为研究脉动风对工作状态下的大长细比飞翼强度及变形的影响,利用Davenport风速谱并采用线性滤波法中的自回归AR模型,通过Matlab编写模拟脉动风速时程的程序,得到飞翼各点随时间变化的脉动风压,将此作为脉动风荷载并利用Ansys对飞翼进行时程响应分析,得到飞翼的应力和位移响应曲线,并与静风作用下的飞翼变形与应力进行比较,得出飞翼在不考虑风荷载脉动效应时计算结果偏于保守,研究方法也可为同类结构设计及风振研究提供技术支撑。 展开更多
关键词 大长细比飞翼 脉动风荷载 Davenport风速谱 线性滤波法 时程分析
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基于移动荷载谱的高速铁路简支梁标准跨度优化
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作者 李锦华 郭继栅 刘全民 《铁道科学与工程学报》 北大核心 2026年第1期1-13,共13页
为最小化列车引起的桥梁振动响应,针对桥梁单阶共振抵消、多阶共振响应包络值局部最小以及任意速度最小极限位移响应工况条件,基于一种等间距移动荷载谱频域方法,开展高速铁路简支梁标准跨度优化分析。首先回顾移动荷载谱公式的推导过程... 为最小化列车引起的桥梁振动响应,针对桥梁单阶共振抵消、多阶共振响应包络值局部最小以及任意速度最小极限位移响应工况条件,基于一种等间距移动荷载谱频域方法,开展高速铁路简支梁标准跨度优化分析。首先回顾移动荷载谱公式的推导过程,接着引入无量纲参数速度κ和桥梁跨度与荷载间距的比值(跨间比λ),进一步推导得到移动荷载共振幅值谱和移动荷载共振幅值包络谱,通过分析谱响应得出每类工况条件的最优跨间比λ。以京沪高铁工程案例为依托,运用有限元方法计算各类最优跨间比λ的桥梁跨中时程位移响应,经过时域结果与频域分析结论比较印证,得出极限位移响应最小的跨间比λ。研究结果表明,当桥梁同时满足共振与消振条件时,共振会被抵消;若发生共振的阶数j符合等式j_(-a)=2^((a-1))·(2b-1)(a和b均为非零自然数),那么桥梁就具有相同的共振抵消跨间比λ。当简支梁桥跨间比λ=1.5时,梁体奇数阶共振能得到有效抵消;跨间比λ=1.3890或者λ=1.6140时,梁体产生的多阶共振响应包络值有局部最小值。当简支梁桥跨间比λ=1.5976时,任意速度条件下其梁体极限位移响应最小,建议高速铁路简支梁桥的标准跨度设计优先采用该跨间比。研究结果可为进一步优化高速铁路简支梁桥设计建造提供参考。 展开更多
关键词 高速铁路 移动荷载幅值谱 桥梁最优跨度 共振 极限位移响应
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抽水蓄能电站钢蜗壳低周疲劳载荷谱编制方式研究
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作者 胡蕾 简敏 +2 位作者 张启灵 高晓峰 郭永成 《长江科学院院报》 北大核心 2026年第1期136-143,共8页
抽水蓄能电站机组在反复启停和变负荷运行状态下,钢蜗壳结构承受的静水压力会大幅度变化,长期作用下蜗壳可能发生低周疲劳破坏。以某抽水蓄能电站为例,在ABAQUS中完成了钢蜗壳结构的有限元仿真分析,再基于2016年全年水位监测数据编制不... 抽水蓄能电站机组在反复启停和变负荷运行状态下,钢蜗壳结构承受的静水压力会大幅度变化,长期作用下蜗壳可能发生低周疲劳破坏。以某抽水蓄能电站为例,在ABAQUS中完成了钢蜗壳结构的有限元仿真分析,再基于2016年全年水位监测数据编制不同时间长度的原型载荷谱,并在nCode Designlife平台利用雨流计数法对其处理计算,对比了原型载荷谱、处理后的载荷谱及几种极端情况下载荷谱计算得到的疲劳寿命。结果表明:(1)抽水蓄能电站充水保压蜗壳与混凝土间的间隙闭合存在一定的滞后性,与常规电站大直径充水保压蜗壳的间隙闭合规律相似,可能对抗疲劳性能不利。(2)低周疲劳载荷谱可采用雨流计数或常幅值简化编制方式,但对水位消落深度较大的电站,还需要进一步探索可靠的输入方式。(3)在电站运行期内,钢蜗壳无低周疲劳失效风险。研究结果可对钢蜗壳抗疲劳设计载荷的选取提供帮助。 展开更多
关键词 抽水蓄能电站 钢蜗壳结构 低周疲劳 载荷谱 雨流计数法
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高铁接触网无螺栓整体吊弦载荷谱编制与磨损失效损伤分析
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作者 胡颢蓝 高仕斌 +1 位作者 于龙 郑昕 《铁道科学与工程学报》 北大核心 2026年第3期1059-1070,共12页
随着我国高铁运行速度提升至350 km/h,接触网吊弦在高频振动、高应力循环下的疲劳失效问题日益凸显,传统螺栓连接吊弦因应力集中易断裂,而无螺栓整体吊弦的失效机理和寿命预测研究尚不完善。针对无螺栓整体吊弦采用弓网动力学仿真模拟... 随着我国高铁运行速度提升至350 km/h,接触网吊弦在高频振动、高应力循环下的疲劳失效问题日益凸显,传统螺栓连接吊弦因应力集中易断裂,而无螺栓整体吊弦的失效机理和寿命预测研究尚不完善。针对无螺栓整体吊弦采用弓网动力学仿真模拟吊弦在实际运行中的动态响应,提出一种基于自适应核密度估计和蒙特卡洛模拟的疲劳载荷谱编制方法,编制适用于工作条件的疲劳载荷谱,创新性地表征了实际工况下的载荷分布特性。其次,以无螺栓整体吊弦为研究对象,开展吊弦疲劳试验,通过电子显微镜观察和分析磨损断面特征,分析其失效机理。最后,通过对吊弦磨损过程的分析研究,建立磨损量模型,计算不同工况下的吊弦磨损寿命,并与编制好的疲劳载荷谱进行对比验证。研究结果表明,吊弦的磨损过程可划分为3个阶段,即初期磨损阶段、稳定磨损阶段和急剧磨损阶段,其中当吊弦上部磨损厚度达到8 mm时,可判定吊弦已达到失效状态;通过对试验获得的寿命数据进行数学拟合,采用逆幂律模型绘制了无螺栓整体吊弦的磨损寿命曲线,反映了其疲劳寿命随载荷变化的规律。此外,疲劳载荷谱所对应的累积磨损损伤值与单次列车通过吊弦时产生的磨损损伤值基本一致,验证了所编制疲劳载荷谱的准确性和实用性。研究结果为进一步降低接触网运行维护成本与新型吊弦寿命评估提供参考。 展开更多
关键词 接触网吊弦 弓网动力学 疲劳载荷谱 疲劳试验 寿命预测
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铆接残余应力对沉头铆钉振动疲劳性能的影响
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作者 符彬 安鲁陵 陈浩 《南京航空航天大学学报(自然科学版)》 北大核心 2026年第1期97-103,共7页
针对飞机发动机进气道安装边沉头铆钉在振动载荷作用下发生疲劳断裂的现象,从铆接残余应力的角度分析了故障原因。基于有限元方法,对铆钉的随机振动过程与铆接过程进行了仿真,获得铆钉的振动等效应力与铆接残余应力,采用Dirlik法计算了... 针对飞机发动机进气道安装边沉头铆钉在振动载荷作用下发生疲劳断裂的现象,从铆接残余应力的角度分析了故障原因。基于有限元方法,对铆钉的随机振动过程与铆接过程进行了仿真,获得铆钉的振动等效应力与铆接残余应力,采用Dirlik法计算了铆钉的振动疲劳寿命,设计了振动疲劳试验,对仿真结果进行了验证。研究表明,铆接残余应力是导致振动疲劳寿命劣化的关键因素,因此必须在疲劳寿命预测中考虑残余应力的影响。研究结论可为航空铆接结构的寿命预测与优化设计提供参考。 展开更多
关键词 铆接 振动 疲劳 载荷谱 残余应力
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考虑高速列车复杂工况的轴箱轴承载荷谱分析
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作者 丁西涛 方聪聪 +1 位作者 周伟 张欣超 《机械设计与制造》 北大核心 2026年第3期373-378,共6页
为了准确获得高速列车在复杂条件下的轴箱轴承载荷谱,及对轴箱轴承的摩擦学与动力学进行分析与强度与剩余寿命的评估,基于SIMPACK建立了CRH380A高速列车动力学模型,分析了CRH380A高速动车在侧风、侧风交汇、明洞运行、明洞交汇、隧道交... 为了准确获得高速列车在复杂条件下的轴箱轴承载荷谱,及对轴箱轴承的摩擦学与动力学进行分析与强度与剩余寿命的评估,基于SIMPACK建立了CRH380A高速列车动力学模型,分析了CRH380A高速动车在侧风、侧风交汇、明洞运行、明洞交汇、隧道交汇工况下轴箱轴承载荷变化,获得了轴箱轴承的垂向与横向载荷谱。发现在单侧风的作用下,使得列车风作用的一侧轴箱载荷会出现减小再增大的情况,非作用侧的轴箱再会增大再减小。当列车的气动力为三个方向时,列车此时运行比单侧风工况下要平稳,使得载荷波动小。横向载荷会在0kN附近震荡随着横向风变化而变化,垂向载荷保持70kN波动,在垂向风风向变化时,风作用侧的轴箱载荷会减小,非作用侧的载荷增大。结果表明:轴箱横向载荷、垂向载荷呈现周期变化,周期变化次数与风震荡有关,当风振幅较大,会导致载荷变化次数和大小增大。当处于单侧风工况时,轴箱轴承所处工况最为恶劣,随着单侧风风速的增大,轴箱轴承承受的横向载荷和垂向载荷波动更加剧烈,左右轴箱载荷变化幅度增大。 展开更多
关键词 机械工程 载荷谱 数值仿真 气动载荷 高速列车 轴箱轴承
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