12.7mm高射机枪模态试验与分析

本文利用实验模态分析技术和有限元法研究机枪—土壤系统的动态特性,通过模态试验获得机枪在硬质土壤支撑条件下的低阶模态信息,据此对机枪有限元模型的边界条件进行模拟,并从动力学角度分析影响射击精度的主要因素,为进一步研究机枪结构动力修改和质量评估提供依据,     

结合振动特征优选和GWOA-XGBoost的电机轴承故障诊断

为解决电机轴承故障状态难以识别,从而造成诊断精度不高的情况,提出了一种基于信号特征提取与极限梯度提升算法(extreme gradient boosting, XGBoost)结合的电机轴承故障诊断模型。使用优化的变分模态分解获得振动信号的固有模态函数(intrinsic mode function, IMF)分量,再基于多尺度熵理论计算各IMF分量的多尺度熵值进行特征重构。在鲸鱼优化算法(whale optimization algorithm, WOA)中引入遗传算法的选择、交叉、变异操作对WOA进行改进。用改进的WOA算法对XGBoost的超参数进行寻优,获得了帮助XGBoost取得最优分类效果的超参数组合,将7种不同故障类型的振动信号进行重构后输入优化的XGBoost模型进行故障诊断。实验结果表明,所提GWOA-XGBoost模型的电机轴承故障诊断精度能够达到97.14%,相较于传统诊断方法,性能提升效果显著。     

脉冲激励下船舶结构谐振响应预报及其模态阻尼参数识别

从模态识别基本原理出发,对脉冲激励下的时-频域响应、谐振激励下的时域响应的表达式进行推导,找到了其时-频域下的幅值关系,认为一定条件下谐振响应中伴随自由振动成分短时间内难以衰减,指出谐振激励力幅值与脉冲力幅值相等时,脉冲响应频谱对应频率下的幅频与谐振下的强迫振动幅值相等。在建立响应等价关系的基础上,推导了仅通过脉冲响应频谱上有限个谱线信息所确定的某阶模态阻尼比的计算公式。利用船体梁模型验证了响应预报及阻尼比估算的准确性。完成了2块不同材料典型船体板单元模型的前8阶模态阻尼比测试,通过数值计算结合试验响应频谱验证了方法的快速性、可靠性。     

多旋翼无人机减振分析与实验

针对多旋翼无人机机身系统振动过大导致飞行状态不稳的问题,基于有限元仿真技术与实验方法,进行了减振分析。通过频率分析,确定系统振动过大的原因为固有频率与激励频率耦合导致的共振现象,且共振频点的模态振型包含一阶挥舞、一阶摆振和二阶摆振振型。提出了优化机身壳体截面形状的设计方案,在不增加额外质量的情况下,将一阶挥舞、一阶摆振和二阶摆振振型对应的频点分别提高37.23%、22.47%和18.43%,有效规避了机身共振现象。仿真实验证明,提出的有限元仿真与实验结合的减振分析思〖BHDWG8,WK10YQ,DK1*2,WK1*2D〗〖XCMWL.TIF;%129%129〗听语音 聊科研与作者互动 路及优化设计方法,可为旋翼无人机减振设计提供参考依据。     

A higher order coupled frequency characteristics study of smartmagneto-electro-elastic composite plates with cut-outs using finite element methods

This article deals with investigating the effect of cut-outs on the natural frequencies of magneto-electro-elastic (MEE) plates incorporating finite element methods based on higher order shear deformation theory (HSDT). In order to consider the influence of cut-out, the energy of the cut-out domain is sub-tracted from the total energy of the entire plate. The governing equations of motions are derived through incorporating Hamilton's principle and the solution is obtained using condensation technique. The proposed numerical formulation is verified with the results of previously published literature as well as the numerical software. In addition, this research focuses on evaluating the effect of geometrical skewness and boundary conditions on the frequency response. The influence of cut-outs on the degree of coupling between magnetic, electric and elasticfields is also investigated.     

基于整车虚拟道路行驶试验的车辆零部件疲劳分析

针对现有车辆零部件精确疲劳分析依赖成本高昂的实车试验的问题,提出了一种利用整车虚拟样机仿真分析零部件疲劳寿命的方法。该方法通过在ADAMS/CAR中用整车虚拟样机在虚拟道路模型上进行行驶试验,利用多体系统动力学基于模态坐标的求解特点,使用模态应力恢复技术准确还原出了用于零部件疲劳寿命分析的载荷历程。将该方法应用于某车辆双横臂前悬中的下控制臂,在较短的时间内获得了该零件的预测疲劳寿命、寿命安全系数及危险部位等信息。应用结果表明,该方法可作为汽车设计过程与测试过程中的有效试验手段。     

机抖激光陀螺减振系统的模态分析

通过对惯性测量单元(Inertial Measurement Unit,IMU)进行减振,可以减小外部冲击、振动对IMU正常工作和测量精度的影响,提高系统导航精度。基于patran/marc有限元分析软件对激光陀螺IMU的减振系统进行模态分析,得到减振系统主要的模态及频率。主要通过仿真分析了减振橡胶块的温度、轴向压缩量和径向压缩量三项关键因素对减振系统模态的影响,提出了一种IMU减振系统的优化设计方案。结论表明:可通过改变结构参数方式来调整减振系统参数,从而满足机抖激光陀螺惯导的应用要求。     

Military Expenditures and Natural Resources: Evidence from Rentier States in the Middle East and North Africa

It has been argued that the discovery of a new natural resource greatly increases the risk of conflict. This research aims to study the effect of natural resources on military spending, using the data from rentier states in the Middle East and North Africa (MENA) countries from 1987 to 2012. In considering the ‘resource curse,’ the types of natural resources matter. Our empirical results demonstrate that the ‘resource curse’ arising from the abundance of certain natural resources, particularly oil and forest resources, leads to increases in military spending. In contrast, the rent from coal and natural gas has a negative impact on military spending, while the rent from minerals has no impact on military spending, controlling for GDP growth and per capita income.     

军用电子机箱模态分析及测试

对某军用电子机箱的固有频率从有限元分析和模态试验测试两个方面进行研究,并将理论分析结果和模态试验测试结果进行对比,确定了电子机箱的固有模态.为今后电子机箱的设计提供了参考依据,为仿真分析提供了有效的有限元建模方法.     

A new experimental way for the monitoring of the real/equivalent in-service-time of double base rocket propellant by coupling VST and PCA

The assessment of the real in-service-time(RIST)and the equivalent in-service-time(EIST)of double base rocket propellants(DBRPs)is of utmost importance for the safe storage and use of weapon systems as well as the efficiency of the accelerated aging plans.In this work,four DBRPs with similar chemical composition and different natural aging have been artificially aged at T = 338.65 K for 4 months with sampling every 30 days.The unaged and artificially aged samples have been investigated by vacuum stability test(VST)at five isothermal temperatures(T = 333.15 K,343.15 K,353.15 K,363.15 K,and 373.15 K).The volume of the evolved gases in VST was found to decrease with natural/artificial aging.Furthermore,the VST data were treated and subjected to principal component analysis(PCA).The results showed excellent discrimination of the DBRP samples according to their stability thermal properties.Most of the variance was described by the first principal component(PC1)whose scores were linearly correlated with the natural aging durations when PCA is applied on VST data obtained at T = 363.15 K.In light of the obtained results,a new experimental way for the estimation of the real/equivalent IST was proposed,which takes into account the impact of the natural aging of the sample.The approach predicts successfully the RIST of two similar DBRPs with a relative deviation of less than 2％.At the specific heating temperature T = 338.65 K,the developed model provides more conceivable EIST values,with asymptotic behavior against artificial aging duration evolution,thus overcoming some shortcomings of the common generalized van't Hoff formula(GvH).