Damage effect analysis and experiment for electronic equipment in impact vibration environment

This paper analyzes the electronic equipment＇s effect factors such as structure characteristics and environment.The radar equipment is taken as an experimental subject.The damage laws of electro-products in vibration environment are analyzed.The experiment shows that the damage of electro-products in vibration environment has relations with both the type and amplitude of vibration and their structure.

Nanoscale mass sensing based on vibration of single-layered graphene sheet in thermal environments

Based on vibration analysis, single-layered graphene sheet （SLGS） with multiple attached nanoparticles is developed as nanoscale mass sensor in thermal environments. Graphene sensors are assumed to be in simplysupported configuration. Based on the nonlocal plate the- ory which incorporates size effects into the classical theory, closed-form expressions lot the frequencies and relative fre- quency shills of SLGS-based mass sensor are derived using the Galerkin method. The suggested model is justified by a good agreement between the results given by the present model and available data in literature. The effects of tem- perature difference, nonlocal parameter, the location of the nanoparticle and the number of nanoparticles on the relative frequency shift of the mass sensor are also elucidated. The obtained results show that the sensitivity of the SLGS- based mass sensor increases with increasing temperature difference.

Vibration and Acoustic Response of Sandwich Panels with Flexible Core Under Thermal Environments

Sandwich panels are increasingly used in the aerospace industry in recent years. Aircrafts are always affected by the thermal and noise environment during their life in service. Analytical studies on the sound vibration response of the sandwich panels with flexible core under thermal environments are performed in the paper. Governing equations are obtained by applying Hamilton 's principle with both anti-symmetric and symmetric motions taken into consideration. Natural frequencies,mode shape and critical temperature are acquired with thermal stresses considered. The forced vibration response and sound radiation are obtained based on the mode superposition principle and the Rayleigh integral. The model is validated compared with the results in literature. Natural frequencies for both anti-symmetric and symmetric motions decrease with temperature rise.Lower order flexural mode and higher-order dilatational mode are sensitive to the temperature change. Symmetric motion induces the anti-resonance frequencies move to the low frequency range. The peaks of sound vibration response remove to the low frequency range as the temperature rise and the amplitude of the peaks decrease due to the enhanced damping.The proposed model may serve as an effective guideline for the application of sandwich panels in thermal environments.

Acoustic and Vibration Environment Prediction Technology of Instrument Cabin Based on Multi-Source Data

Noise characteristic is one of the important factors to be considered during the design of a launch vehicle system.In this paper,the acceptance conditions for the external noise environment of the instrument cabin are given based on multi-source data,including the measured data of the launch vehicle lift-off noise,the mechanical environment of the launch vehicle equipment,and the external noise environment of the instrument cabin deduced from empirical formula.Then an acoustic and vibration transfer model is established based on the response data of the instrument equipment used to conduct measurements in the noise test reverberation room.By using an external noise environment and a transfer model,the response of the instrument and equipment for the acceptance condition can be obtained.The acoustic and vibration prediction technology introduced in this paper can provide technical support in the environmental prediction analysis of heavy launch vehicles for the future.

Nonlocal vibration analysis of circular double-layered graphene sheets resting on an elastic foundation subjected to thermal loading

Based on the nonlocal elasticity theory, the vibration behavior of circular double-layered graphene sheets（DLGSs） resting on the Winkler- and Pasternak-type elastic foundations in a thermal environment is investigated.The governing equation is derived on the basis of Eringen＇s nonlocal elasticity and the classical plate theory（CLPT）.The initial thermal loading is assumed to be due to a uniform temperature rise throughout the thickness direction. Using the generalized differential quadrature（GDQ）method and periodic differential operators in radial and circumferential directions, respectively, the governing equation is discretized. DLGSs with clamped and simply-supported boundary conditions are studied and the influence of van der Waals（vd W） interaction forces is taken into account.In the numerical results, the effects of various parameters such as elastic medium coefficients, radius-to-thickness ratio,thermal loading and nonlocal parameter are examined on both in-phase and anti-phase natural frequencies. The results show that the thermal load and elastic foundation respectively decreases and increases the fundamental frequencies of DLGSs.

Influence of local stiffeners and cutout shapes on the vibration and stability characteristics of quasi-isotropic laminates under hygro-thermo-mechanical loadings

The perforated stiffened panel is generally found as a sub-component of sophisticated structures.The fundamental purpose of this panel is to withstand against buckling under complicated loading and environmental conditions.Hence,an accurate knowledge of critical buckling behaviour of stiffened panels is very much essential for a reliable and lightweight structural design.In this paper,the focus is on quasi-laminated panels with different cutout shapes of various sizes and their responses to hygrothermal environments under nonlinearly varying edge loads and is compared with the locally stiffened panels.Towards this,the modelling of the panel and stiffener is done by adopting nine-noded heterosis plate elements and three noded beam elements respectively.The stiffener formulation is suitably modified in order to take the torsional effect also into consideration along with the effect of shear deformation.Initially,the plate and the stiffener elements are treated separately,and then the displacement compatibility is maintained between them by using the transformation matrix.For a given loading and geometric discontinuity,the stress distribution within the perforated panel is highly non-uniform in nature and hence a dynamic approach has been used to calculate buckling loads by adopting two sets of boundary conditions,one set for pre-buckling stress analysis and the second set for buckling analysis.Four different quasi-isotropic stacking sequences are deliberated in this work by varying different ply-orientation in each scheme.The study also addresses the effect of various parameters such as nonlinear loads,hygro-thermal loads,cutout size and shapes,position of cutout,stiffener parameters,stacking sequences,thickness of plate and boundary conditions.

VIBRATION AND SOUND RADIATION OF AN ASYMMETRIC LAMINATED PLATE IN THERMAL ENVIRONMENTS

Analytical studies on the vibration and sound radiation characteristics of an asymmetric laminated rectangular plate are carried out in this paper. Theoretical formulations, in which the effects of thermal environments are taken into account, are derived for the vibration and sound radiation based on both first-order shear deformation plate theory and Rayleigh integral. It is found that the natural frequencies, the resonant amplitudes of vibration response and the sound pressure level decrease with the temperature rising. The natural frequencies of asym- metric plates are smaller than those of symmetric plates and the velocity responses of asymmetric plates are larger than those of symmetric plates.

Running train induced vibrations and noises of elevated railway structures and their influences on environment

The vibrations and noises of elevated railway structures have been cause for concern due to their effects on the environment and the people living near elevated lines.In this paper,the main structural features of some new elevated bridges and station hall were introduced.The generation mechanism of vibrations and noise of elevated structures induced by trains were investigated.The noise induced by different types of elevated bridges,their influences on the environment and the theoretical method for the analysis of structure borne noise was analyzed.Finally,several field measurements on train induced noises at the platforms of elevated subway stations and bridges were presented.

Vibration test condition for spacecraft lift-off environment

The purpose of the vibration test of spacecrafts is to assess their adaptability to low-frequency vibration environment during lift-off.This paper gives the simulation of the satellite ground vibration test(GVT) and the state of the satellite along with rocket during lift-off.The simulation results of these two states are compared on condition that the lateral vibration of satellite/launching vehicle(S/LV) interface is the same.It is shown that the dynamic responses of satellite vertex are totally different.This is because there is angular motion of S/LV interface during lift-off,but in the GVT,the angular motion is restrained.By means of numerical simulation of the lift-off state,the angular motion related to the translation motion of S/LV interface can be determined.Then,using this angular motion as supplementary condition to simulate the vibration test,the calculated dynamic responses of satellite vertex are identical with the lift-off state.It demonstrates that supplementing angular motion condition is an effective method to improve spacecraft ground vibration test more identically with the real lift-off environment.Furthermore,it is useful for the application of the multi-degree-of-freedom shaking table,and provides the basis for test condition requirement.

Finite element approach for free vibration and transient response of bi-directional functionally graded sandwich porous skew-plates with variable thickness subjected to blast load OA

At the first time,the finite element method was used to model and analyze the free vibration and transient response of non-uniform thickness bi-directional functionally graded sandwich porous(BFGSP)skew plates.The whole BFGSP skew-plates is placed on a variable visco-elastic foundation(VEF)in the hygro-thermal environment and subjected to the blast load.The BFGSP skew-plate thickness is permitted to vary non-linearly over both the length and width of the skew-plate,thereby faithfully representing the real behavior of the structure itself.The analysis is based on a four-node planar quadrilateral element with eight degrees of freedom per node,which is approximated using Lagrange Q_(4)shape function and C^(1)level non-conforming Hermite shape function based on refined higher-order shear deformation plate theory.The forced vibration parameters of the non-uniform thickness BFGSP skew-plate are fully determined using Hamilton's principle and the Newmark-βdirect integration technique.Accuracy of the calculation program is validated by comparing its numerical results with those from reputable sources.Furthermore,a thorough assessment is conducted to determine the impact of various parameters on the free and forced vibration responses of the non-uniform thickness BFGSP skew-plate.The findings of the paper may be used in the development of civil and military structures in situations that are prone to exceptional forces,such as explosions and impacts load.

无线无源力/热传感器与测试技术研究现状

针对力热传感器多数采用有线有源的技术方案,难以适用于高温、高压、强振以及机械动力旋转部件等环境下的力热参数原位测试问题,阐述了进行无线无源传感器件研究的重要意义,并对声表面波(surface acoustic wave,简称SAW)传感器、LC谐振互感耦合传感器以及超材料传感器等3类无线无源力热传感器进行了总结及现状分析。首先,描述了无线无源力热传感器的需求情况;其次,介绍了3类传感器的工作原理、传感性能及其在独特场景下的具体应用;最后,讨论了无线无源传感器发展过程中的瓶颈问题,指出了未来可能改善和提升的发展方向。

基于声振传递的飞行器噪声振动环境预示方法研究

针对高速飞行器飞行条件下的噪声、振动环境恶劣、复杂、难预示的问题,提出了基于声振传递的飞行器飞行条件下的噪声、振动环境预示方法。采用数值仿真、脉动压力风洞试验或工程分析等方法,获取飞行器在典型工况下的舱外脉动压力场;通过噪声试验或声振耦合仿真分析的方法,得到飞行器声振传递特性;根据获得的舱外脉动压力和声振能量传递特性,结合具体飞行参数得到实际飞行条件下的飞行器声振预示环境。采用该方法对某飞行器开展了振动环境预示研究,经地面及飞行试验验证振动环境量级预示精度可达1.6 dB。提出的基于声振传递的飞行声振环境预示方法可以广泛应用在导弹、火箭等飞行器的精细化环境设计中,对于提高飞行器总体性能、环境适应性和飞行可靠性具有重要的工程意义。

航空发动机振动环境谱统计归纳方法及振动试验台复现

为满足航空发动机及机载产品研制过程贴近使用环境的振动考核试验需求,需根据发动机实测振动数据给出振动考核试验所需的输入谱图。依据GJB/Z 126-99中给出的环境测量数据归纳方法,建立了发动机实测振动环境谱统计归纳方法并通过程序实现。利用发动机多架次实测试飞振动数据统计归纳得到发动机测点位置的振动实测谱。基于能量等效及信号频域特征分布一致原则,将归纳得到的实测谱转化为可用于振动台输入的振动环境谱,并在振动台上进行了振动信号的复现试验。结果表明:振动台输出信号与发动机实测振动信号频域分布特征一致,在统计频率带宽范围内振动总量最大相差5.7%,证明了转化方法是合理的,为航空发动机机载设备贴近使用环境的振动考核试验方法提供了真实的输入谱图。

典型舱段结构三轴振动/热复合环境虚拟试验方法研究

随着航天飞行器面临的力学环境愈发严酷,热与振动环境已成为造成结构损伤和破坏、产品功能下降或失效的关键因素。建立了一种考虑三轴振动与热复合环境的虚拟试验方法,以简化的筒形舱段为对象,分别建立石英灯阵高温加热仿真模型与三轴振动仿真模型,并通过实际试验数据得到振动台-夹具传递函数,将三者结合以建立三轴虚拟热振仿真模型。分别通过舱段结构单轴热振试验与三轴热振试验来验证所建模型的准确性,并基于验证后的模型获取三轴振动下结构中央测点随温度时变的传递函数变化情况。由舱段模态试验验证舱段有限元模型的准确性,对比前6阶模态频率误差不超过5%。在单轴热振试验中,仿真模型各测点响应均方根值(root mean square,RMS)与试验加速度响应RMS的误差不超过15%;在三轴向热振试验中RMS误差不超过20%,验证了所建虚拟热振模型的有效性。

同轴脉冲形成线振动环境适应性优化设计

以带有悬臂结构的同轴脉冲形成线为研究对象,开展提高振动环境适应性的优化设计。首先,通过实际工况分析及仿真计算,确定形成线内筒的盲孔螺钉可采用的防松措施有:使用施必劳螺纹并涂抹防松胶;优化螺钉数量。其次,通过仿真分析和绝缘试验,优化尾端绝缘子材料,提高悬臂支撑的中内筒连接刚度。最后,开展振动试验考核,优化后的形成线等效件可以通过长时间的振动考核,相比优化前的振动环境适应性有很大提高,验证了优化设计的有效性。该研究结果对同类型脉冲功率源的振动环境适应性设计具有参考意义。

冲击响应谱在炮击振动环境的谱编制应用研究

机载航炮是军机结构振动/冲击最严酷的载荷源之一,基于实测数据得到真实的环境谱,对于军机结构及机载设备的设计与考核非常重要。基于某飞机航炮实测响应数据,采用数字滤波法得到炮振环境下单点单次响应的冲击响应谱,并结合国军标和相关标准的要求,提出了基于不同统计数据类型的机载设备炮振环境分类方法,对每一组炮振实测数据进行归纳,得到了炮击振动环境实测谱和规范谱,最后通过某飞机舱段地面试验进行了验证。结果表明该方法相较于常用的位置区域分类和极值包络区域归纳方法更正确合理,且比行业内普遍采用的随机炮振通用谱更符合炮击真实环境。该方法可直接用于军机结构与机载设备的地面试验验证,具有较好的科学性和工程实用价值。

海洋环境及振动荷载联合作用下注聚平台桩基承载力特性研究

针对老区油田注聚开发过程中注聚泵长期持续高频、大幅值振动导致注聚平台桩基荷载大幅增加的问题,本文构建了海洋环境及注聚泵振动荷载下注聚平台桩土耦合整体及局部分析模型,进而研究了海洋环境及注聚泵振动对注聚平台动力响应及桩基承载力的影响规律。结果表明,注聚泵的振动会显著增加注聚平台桩基的基础承受的荷载,且随着注聚泵开启数量的增加,桩基承受的荷载呈线性增长趋势。与自重条件下桩基所受荷载相比,最大增长约35%,会导致桩基承载力安全系数明显降低。

国产磁选态铯束频率标准环境特性研究

铯原子频率标准具有长期稳定性好、可靠性高的优点,在导航定位、守时授时、通信电力、时频计量等领域有着广泛的应用。近年来由于军事领域对高精度时间频率源的需求,铯原子频标的使用环境从实验室走向了战车、舰船等机动平台。本文针对铯原子频标在战车、舰船、高原等复杂环境下的环境适应性,研究环境因素对整机指标的影响机理。通过仿真与试验对整钟设计进行优化,以提高整机在力学、热、磁场、低气压等复杂环境下的适应性。经过优化设计后的国产铯束频率标准样机通过了相关环境试验项目的考核,各项指标均满足要求。研究结果表明,铯原子钟电性能样机的稳定度优于8.73×10^(-15)/5 d,磁敏感度3.15×10^(-14)/Gauss,工作温度特性-8.18×10^(-14),这项工作为国产化铯钟的进一步应用提供了基础。

重力参数对非阻塞性颗粒阻尼减振特性的影响

针对非阻塞性颗粒阻尼(Non-obstructive Particle Damping,NOPD)在微重力、超重及离心等非常态环境中减振效果较差的问题,采用重力加速度表征这些非常态物理环境,利用离散元法(Discrete Element Method,DEM)研究重力参数对NOPD减振特性的影响,同时还分析NOPD最优填充比及最优粒径比等结构参数在不同重力条件下的变化规律。研究表明,重力加速度在0.7~1.0 g之间时NOPD减振效果最好。在微重力环境下,当重力参数变化时,NOPD最优填充比为0.85,最优粒径比为0.45。而当重力加速度大于1 g时,NOPD最优填充比及最优粒径比均随重力加速度的增加而减小,且其最优范围也均有所扩大。

超高层办公建筑暖通空调系统噪声控制分析

营造良好的室内声环境对人员身心健康至关重要。本文以某超高层办公楼为研究对象,分析了超高层办公建筑声学方面的特点、典型暖通空调系统的噪声传递途径;针对办公楼层剖析了声源降噪、隔绝机房噪声、办公区内空调末端及管道的噪声控制措施,并针对机电层的不同设备区域提出了相应的隔振、隔声、降噪做法。