基于PANDA平台的多点基础激励谐响应的并行计算

基于PANDA自主并行计算平台,采用模态叠加法对多点基础激励作用下的谐响应分析开展算法设计和并行实现研究,构建相应的并行求解模块.结合商业有限元软件对研发模块的正确性进行验证;将该模块应用于某光机装置,实现11.88亿自由度超大规模的高效并行求解.结果表明：研发的多点基础激励谐响应分析模块可用于复杂装备的高效精细数值模拟,具备强大的并行计算能力,最大可扩展CPU核数可达数千个,远超现有通用商业有限元软件.     

强脉动压力下飞行器随机振动分析算法与并行实现

以飞行器再入大气层过程中承受多点强相关脉动压力下的随机振动分析为研究背景,从自由体模态分析入手,考虑脉动压力之间的强相关性,建立自由体动力学方程并推导刚-弹模态耦合作用下的随机振动理论,完成算法设计并在自主并行软件平台PANDA中进行代码实现,通过典型飞行器算例开展正确性验证和应用研究。研究表明：飞行器再入过程的刚体运动对结构在低频段的响应影响显著,甚至起到主导作用,越靠近零频附近,这种影响越大;在中高频段,弹性响应逐渐占据主导地位。基于自主研发形成的随机振动分析模块可以较好地模拟飞行器再入过程脉动压力诱导的随机振动响应,具备超大规模并行计算能力。     

气浮隔振平台模态实验分析北大核心CSCD

采用ANSYS有限元方法分析了光学平台的自由模态,并以有限元结果作为参考,完成了实际工况下的模态实验,识别了平台整体结构的模态参数,得到了平台在垂向和横向的一阶频率,频率值分别为126.77Hz和361.427Hz。根据分析,该平台的刚度满足光学试验的要求。     

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为考察ITER真空室中子屏蔽结构组件对选址地法国Cadarache地震加速度频谱的单点响应情况,根据ITER真空室中子屏蔽组件的设计概念和结构特点,建立了组件结构的有限元分析模型。应用有限元分析软件ANSYS对组件进行了结构模态分析,并基于其结果进行了模态叠加。分析发现,组件结构的低阶振型与高阶振型有差异,且结构与低阶频率发生响应,但引起的位移与应力在允许的范围之内。结果表明,装配体结构更能适应结构抗震性的设计要求。仿真计算的结果为组件结构的优化设计和下一步的工程实现提供了可靠的依据。     

某光电雷达稳定平台关键部件转板的动态特性分析

 转板是光电雷达稳定平台的关键元件之一。为了更好地设计和分析某光电雷达稳定平台的转板,运用Pro E软件对其进行三维实体建模,合理简化后,进入Ansys软件界面建立有限元模型。应用有限元理论和Ansys软件对其进行动态特性分析,得到了转板前八阶模态的固有频率和振型,以及要求范围内的谐响应。对比了不同方法划分网格的网格质量,采取不同材料得到了不同模态。分析结果表明：设计的转板在关心的频段0~50 Hz,2 000 Hz~8 000 Hz内不发生共振,符合设计要求。     

某型内转子光电雷达稳定平台的模态分析与优化

为了更好地设计某型内转子光电雷达稳定平台,运用Pro-E软件对其进行了三维实体建模,合理简化后,进入Ansys软件建立有限元模型.应用有限元理论和Ansys软件对该平台进行了模态分析,得到稳定平台前八阶模态的固有频率和振型.其中对比了不同网格、不同材料产生的不同模态,对同类分析提供了参考,也为此稳定平台的设计优化提供了...     

车载光电经纬仪支撑平台稳定性研究

传统的车载支撑平台晃动量较大，难以满足车载光电经纬仪高精度不落地测量要求。为了兼顾轻量化、高刚度和便于制造的要求，采用离散体桁架拓扑优化方法设计了一种具有桁架蒙皮式结构的高比刚度车载支撑平台；建立了平台系统的有限元仿真模型，根据平台安装光电经纬仪的稳定性要求，分析了不同工况和载荷条件下平台系统的静力学和模态特性，搭建了支撑平台稳定性实验装置。结果表明，在经纬仪工作角加速度0.5(°)/s²～20(°)/s²范围的激励下，经纬仪基座的响应加速度为0.008～0.55 m/s²，无明显影响经纬仪跟踪性能的共振响应发生。同时，采用倾角传感器测量了平台晃动幅值，最大晃动量为7.2″。该支撑平台具有较高的支撑稳定性，适用于车载光电经纬仪高精度不落地测量。     

某型飞机武器控制系统计算机检测仪的设计与实现

为解决某型飞机武器控制系统计算机检测仪检测技术老旧且故障频发,不能满足作战和训练要求的问题,本文设计了一种新型的检测仪。基于该型飞机武器控制系统计算机的功能结构和维护保障规程,首先分析了该型计算机检测仪的功能需求;然后提出了基于Compact RIO平台和触摸屏式计算机的检测仪总体结构;最后设计了检测仪的硬件结构和匹配的软件设计思路。检测仪的硬件主要包括四个模块：控制模块、测量模块、显示模块和电源模块;软件实现采用LabVIEW图形化系统设计软件,设计过程分成开发模式和运行模式两阶段。该检测仪能够对武器控制系统中机载计算机的输入输出信号进行精确测量和分析,技术先进,且显示直观,能较好地提高维修保障效率。     

运载火箭结构动特性分析工具的设计与实现

运载火箭的结构模型复杂,只有通过开发专用的仿真分析软件,才能高效、便捷的对其开展动力学特性分析。为保证工具建设的实用性,该软件基于航天领域应用广泛的Patran/Nastran软件进行二次开发。针对仿真分析流程,设计实现了运载火箭结构动特性分析工具,涵盖了建模与计算模块、结果后处理模块、模态筛选模块与模型修正模块,并提炼了其中的关键技术。经工程实践表明,工具可提升设计效率,且计算结果准确、通用性与扩展性强,在工程中具备良好的应用价值。     

一种光学平台的力学稳定性分析

光学平台稳定性使用要求很高，结构形式复杂，使用环境苛刻，受不同类型载荷作用，对结构设计和加工工艺的要求非常严格。介绍了利用ANSYS结构分析软件对该光学平台在不同的简化结构条件下的计算机数值模拟结果，为其工程研制提供了理论依据。     

抑制大型折叠腔结构光斑抖动技术的研究

针对光腔镜盒的真空变形和振动对精密光学系统的影响,分析了传统刚性连接的光学调整架平台以及球关节连接结构在减振降噪设计的不足,从支撑和柔性密封连接的角度,设计了隔离振动和光腔镜盒真空变形的精密光学调整架平台,对应用于大型折叠腔的双层光学调整架平台的动力学特性进行ANSYS仿真,并完成了光斑抖动验证实验。结果显示框架式双层光学调整架平台的第一阶弹性体频率可达到126.5,172.3Hz,很好地满足折叠腔光学调整架平台的使用要求;应用在大型折叠腔,抽真空试验前后He-Ne导引光输出光斑位置无变化,形状变化很小,出光过程中输出抖动角均方根值为3.73″,隔离振动传递效果明显。     

Modified independent modal space control of m.d.o.f. systems

The performance of the independent modal space control (IMSC) algorithm for structural vibration control is examined in this paper. Both the theoretical analysis and numerical simulation show that, for a multi-degree-of-freedom system, the modal control forces may increase the contributions of the vibration of higher modes (uncontrolled modes) to the system response if the IMSC algorithm is used to design a structural control system. Therefore, the responses of the controlled structure may be underestimated if the effects of control forces on the higher modes are not considered in the response analysis. A new control algorithm—modified independent modal space control (MIMSC) algorithm is proposed in this paper for eliminating the effect of modal control force on the uncontrolled modes. Numerical example shows that the structural responses can be effectively reduced when control system design is carried out based on the proposed algorithm. By comparing the simulated results obtained by the IMSC and MIMSC algorithms, it is found that, in order to achieve the same control objective, the proposed algorithm is more effective than IMSC since the modal control forces do not have any effect on the uncontrolled modes. In order to verify the effectiveness of the proposed algorithm, a practical example—active control design of UCLA Math-Science Building is presented and discussed.     

Response of plates with unconstrained layer damping treatment to random acoustic excitation,part I: Damping and frequency evaluations

For theoretical evaluation of the response of a structure under random acoustic excitation a complete understanding is required of the various modes of vibration and the modal damping associated with each mode. In order to evaluate these parameters for plates with unconstrained layer damping treatment, some of the theoretical approaches applicable are used. Experimentally observed modal frequencies and associated loss factors are compared with those estimated by different theories for all edges simply supported and all edges clamped boundaries, after accounting for the damping at supports. The modes of vibration used in the theoretical analysis for these boundaries are compared with those observed in the experiments. These results are made use of in Part II for the evaluation of response under random acoustic excitation.     

Modal analysis by free vibration response only for discrete and continuous systems

This work aims to develop the algorithm for modal analysis by free vibration response only (MAFVRO), in particular for the general or non-proportional viscous damping system model. If the structural displacement or acceleration response due to free vibration can be measured, the system response matrices, including the displacement, velocity and acceleration, can be obtained through numerical differential or integration methods. These response matrices can then be applied to the developed MAFVRO method to determine the structural modal parameters. The numerical differential and integration methods are introduced and adopted to establish the modal parameter prediction program for the non-proportional damping model of MAFVRO. This work also shows the applications of MAFVRO to the multiple degree-of-freedom (mdof) systems and the cantilever beam, respectively. Both the discrete and continuous systems are demonstrated for the feasibility of the MAFVRO algorithm. The developed method uses the free vibration output response only and can obtain the structural modal parameters successfully.     

Use of speckle interferometry and modal assurance criterion for identification of component modes

One of the problems encountered in performing modal analysis is the identification of different modes occurring at close natural frequencies. This paper proposes to face such a problem by an original application of the modal assurance criterion (MAC) that is typically used to verify the reliability of numerical structural models by evaluating the correspondence between numerical and experimental mode shapes. To properly apply the MAC, experimental mode shapes must be retrieved acquiring data at a high number of experimental points suitably distributed on the surface of the structure. Using usual modal analysis techniques based on pointwise transducers, difficulties can be encountered to retrieve mode shapes with the required spatial resolution. In order to overcome such difficulties, Speckle interferometry techniques can be used. This paperproposes a procedure based on the application of a highly reliable MAC evaluated by time average Speckle interferometry for recognising the modes contributing to the stationary vibration patterns. The results obtained from the modal analysis of a thin square plate have shown that the proposed procedure is capable of pointing out the component modes.     

机载光电稳瞄平台减振技术研究北大核心CSCD

机载光电稳瞄平台受飞机作战环境的干扰因素,会引起设备环架的振动,对光电平台载荷视轴的稳定性及跟踪精度影响很大,减振的主要任务是有效隔离环境振动。与传统橡胶减振器比较,文章提出了一种新型机载光电稳瞄平台的柔性减振设计。并通过ANSYS仿真软件对新的减振模型进行了模态仿真分析,通过振动试验对设计的性能进行了有效评估,测试结果与仿真评估误差为0.56%,说明该设计对机载光电稳瞄平台具有减振性。