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1.
本文研究了红外探测器中红外焦平面列阵的象元———铁电薄膜微桥在红外辐射作用下的输出信号。用层合板壳作为微桥结构的力学模型,中间一层为压电材料,上下两层为金属材料电极。采用了力-电-热耦合的控制方程和变分原理,考虑了铁电薄膜的惯性力,推导出了基于Mindlin假设的压电材料层合板有限元公式。以红外探测器在夜间从飞机上探测地面的坦克为例,用有限单元法模拟了铁电薄膜微桥在红外辐射作用下的力、热、电输出信号,并对结果作了分析比较。  相似文献   

2.
本文研究了红外探测器中红外焦平面列阵的象元———铁电薄膜微桥在红外辐射作用下的输出信号。采用层合板作为力学模型,将铁电薄膜微桥结构简化为一块边长为微米量级、厚度为亚微米量级的夹层板,中间是铁电薄膜,上下表面为金属薄膜,上表面为金黑,下表面为铂(白金),上下表面都是电极。微桥的上表面接收周期为1/30秒的辐射方波脉冲信号。由于微桥十分微小,可以认为红外辐射在板面上均匀分布,又由于板的平面尺寸与厚度之比相当大,因此可以认为热传导只在板厚的方向进行,问题变为一维的。采用适当的力-电-热耦合的控制方程,利用级数解,算出铁电薄膜微桥在红外辐射作用下的力学响应和薄膜内的力、热、电输出信号,并对结果作了分析比较。  相似文献   

3.
研究了红外探测器中红外焦平面列阵的象元—BST铁电薄膜微桥在红外辐射作用下输出信号的分析方法.将BST铁电薄膜微桥结构简化为一块微米尺度的夹层板,中间是BST铁电薄膜,在极化模式下工作.微桥的上表面接收辐射脉冲信号.由于微桥十分微小,可以认为红外辐射在板面上均匀分布,又由于板的平面尺寸比厚度大得多,可以认为热传导只在板厚的方向进行.采用适当的力-电-热耦合的控制方程和非线性的本构方程,得到了铁电薄膜微桥在红外辐射作用下的的力、热、电输出信号的解析解,并将计算结果与实验结果作了比较.  相似文献   

4.
压电层合圆板传感器的非线性静力耦合分析   总被引:2,自引:0,他引:2  
本文基于von Karman薄板非线性理论,压电基本方程和经典层合板理论,对上,下表面粘有压电传感膜层的圆薄板压力传感器的力-电耦合特性进行了定理分析。首先,针对压电层合圆板传感器件建立了考虑几何非线性变形的力-意耦合模型。给出了压电薄膜层感应电量的计算公式;然后,采用级数解法进行了求解,得到了非线性静力耦合问题的幂级数精确解,给出了传感器静态测量过程中所关心的压力-电量特征曲线和中心挠度,电量特征曲线;同时,定量讨论了压电二次效应对感应电量和层合结构中心挠度的影响。通过所得结果,在压电式压力传感器设计中,为采用电信号直接输出有关结构的变形和外界载荷等待测参量提供了依据。  相似文献   

5.
基于损伤力学,考虑压电效应、几何非线性和损伤演化的影响,建立了集中载荷作用下压电层合板的非线性运动微分方程,考虑撞击物与压电层合板之间的弹性接触效应,确定了层合板所承受的冲击力.对此非线性动力问题,采用有限差分法进行求解,且引入损伤层合板单元模型,采用有限元方法模拟了冲击荷载作用下压电层合板的损伤演化.算例中,讨论了撞击物的冲击速度、压电材料以及损伤对压电层合板非线性动力响应的影响,以及周期冲击荷载下冲击速度和压电材料对压电层合板疲劳损伤寿命的影响.  相似文献   

6.
压电传感器探测层合板分层的数值分析   总被引:1,自引:0,他引:1  
尹林  王晓明  沈亚鹏 《力学学报》1995,27(Z1):58-65
用修正的准三维有限元法分析了受单轴拉伸表面覆盖有压电薄膜的复合材料层合板。文中首先讨论了压电薄膜层对层合板层间应力的影响,然后在存在分层裂纹的情况下,计算了压电层的电压分布。结果表明将压电薄膜作为传感器来进行分层探测是可行的。文中最后考虑了多种因素对传感灵敏度的影响。  相似文献   

7.
非线性压电效应下压电层合板的弯曲   总被引:2,自引:1,他引:2  
考虑非线性压电效应,即电致弹性和电致伸缩效应情况下压电层合板的弯曲。从非线性压电方程和几何方程导出了压电层合板合应力、合力矩与应变之间的广义本构关系,这些关系关于电场是非线性的。利用Ritz法和双傅立叶级数得到四边简支对称压电层合板在高电场作用下的非线性解并进行计算。结果表明,只考虑线性压电效应只能适应于作用电场较低或基础层的刚度比压电层的刚度要大得多的情况。  相似文献   

8.
粘贴压电层功能梯度材料Timoshenko梁的热过屈曲分析   总被引:1,自引:0,他引:1  
研究了上下表面粘贴压电层的功能梯度材料Timoshenko梁在升温及电场作用下的过屈曲行为。在精确考虑轴线伸长和一阶横向剪切变形的基础上,建立了压电功能梯度Timoshenko层合梁在热-电-机械载荷作用下的几何非线性控制方程。其中,假设功能梯度的材料性质沿厚度方向按照幂函数连续变化,压电层为各向同性均匀材料。采用打靶法数值求解所得强非线性边值问题,获得了在均匀电场和横向非均匀升温场内两端固定Timoshenko梁的静态非线性屈曲和过屈曲数值解。并给出了梁的变形随热、电载荷及材料梯度参数变化的特性曲线。结果表明,通过施加电压在压电层产生拉应力可以有效地提高梁的热屈曲临界载荷,延缓热过屈曲发生。由于材料在横向的非均匀性,即使在均匀升温和均匀电场作用下,也会产生拉-弯耦合效应。但是对于两端固定的压电-功能梯度材料梁,在横向非均匀升温下过屈曲变形仍然是分叉形的。  相似文献   

9.
压电层合板热屈曲问题的精确分析   总被引:8,自引:0,他引:8  
本文在作者们以前工作的基础上导出了热压电介弹性稳定性问题的控制微分方程,提出了热压电层合板热屈曲问题的数学和学解法。由于最后所得特征值问题的复杂性,热屈曲临界必须数值求解。文中对不同压电材非压电材料层构成的层合板作了具体计算,考虑了压电性对屈曲温度的影响。  相似文献   

10.
由于具有良好的结构、力学性能,复合材料层合板在现代飞行器上大量应用;而压电复合材料,作为一种新兴的智能材料,由于其独特的力电耦合性能得到了人们更多的关注。本文研究含有压电片的复合材料梁和板在电场作用下的变形控制问题。基于经典的梁理论和层合板理论,分别研究了下列问题:(1)双压电片布置的悬臂梁的变形;(2)含有压电层的层合板变形控制问题;(3)含有一对压电片的层合板的变形控制问题。针对上述问题,分别给出了理论解和数值解,并进行了相关讨论分析。结果表明压电材料可对结构进行精确控制,因此本文的结果可对复合材料梁和板在电场作用下的变形控制问题提供工程参考。  相似文献   

11.
Micro-bolometer pixel is an essential element in the infrared focal plane array(IRFPA) of infrared detectors.Its response to infrared radiation is analyzed in this paper.The pixel structure is modeled as a composite laminate thin plate whose sides are measured with the thickness from 0.1-1 μm.Its middle ply is a ferroelectric thin film.Its top surface is covered with a gold or platinum infrared absorber,while the bottom surface is deposited with platinum or lanthanum-nickel.Meanwhile both surfaces are a pair of electrodes.The top surface receives infrared radiation pulses successively.For the very tiny micro bolometer pixel,it is assumed that the infrared radiation is uniformly distributed on the plate.Furthermore,as the ratio of the side length to the thickness of the plate is dramatically large,it is assumed that heat transfer only takes place across the thickness of the plate.The thermal-electric-mechanical coupling governing equations are solved in a form of Fourier series.Results of the displacement,temperature variation and electric output signals of the micro bolometer pixel structure under infrared radiation are obtained,analyzed and compared with experimental data.  相似文献   

12.
本文在文献[2,3]的基础上,提出了一个解各向异性弹塑性中厚度板壳问题的有限元方法。考虑材料各向异性的特点,采用了Hill推广的Huber-Mises屈服准则;借用Owen的剪切修正系数,正确计及了叠层复合材料壳体的横向剪切效应;为了避免“自锁”现象,文中采用了9节点的Heterosis二次壳单元;特别是本文利用插值外推的思想,提出了一个带预测的弧长增量控制法,显著提高了确定变形路径的计算效率。几个数值算例表明本文给出的有限元方法对于各向异性中厚度板壳的弹塑性分析有较好的精度,尤其是对具有复杂变形路径的结构计算,收敛速度提高更快。  相似文献   

13.
ONCOMPLETENESSFORA3-DLINEARTHEORYOFCOMPOSITELAMINATEJiangYou-liang(蒋友谅)(DepartmentofAppliedMechanies.PekingInstituteofTechnol...  相似文献   

14.
According to recent studies of the generalized variational principle by Professor Chien Weizang, the more generalized hybrid variational principle for finite element method is given, from which a new kind of the generalized hybrid element model is etablished.Using the thin plate bending element with varying thickness as an example, we compare various hybrid elements based on different generalized variational principles.  相似文献   

15.
梁立孚  罗恩  冯晓九 《力学学报》2007,39(1):106-111
明确了分析力学初值问题的控制方程,按照广义力和广义位移之间的对应关系,将 各控制方程卷乘上相应的虚量,代数相加,进而在 原空间中建立了分析力学初值问题的一种变分原理形式,即建立了分析力学初值问题的卷积 型变分原理和卷积型广义变分原理. 推导了分析力学初值问题卷积型变分原理和卷积型广义 变分原理的驻值条件. 在建立分析力学初值问题的一种变分原理形式的同时, 将变积方法推广为卷变积方法.  相似文献   

16.
王玉鑫  张刚  卢翔 《应用力学学报》2020,(1):249-257,I0017,I0018
通过对湿热环境下阶梯挖补胶接修理后碳纤维/双马树脂(T300/QY8911)层合板振动特性的分析,探究了挖补修理后碳纤维/双马树脂层合板在不同湿热效应下的振动特性。基于Mindlin-Reissner板理论与最小势能变分原理,在考虑湿热效应前提下,推导了正交各向异性复合材料层合板的本构关系及四边简支条件下的自由振动控制方程;其次,利用ABAQUS软件建立了三维黏弹性有限元挖补修理模型,应用Fortran语言将湿热耦合下的应力-应变本构关系编入UMAT二次开发文件中,采用三维八节点五自由度等参单元进行了离散。通过与参考文献对照,验证了胶接修理后T300/QY8911层合板有限元模型和编译的湿热环境下UMAT子程序的合理性与有效性。算例结果表明:湿热环境对挖补修理后层合板固有频率的影响比对完整层合板严重;温度对材料性能的影响大于湿度;相比于材料性能变化对振动特性的影响,湿热残余应力对胶接修理后层合板振动特性的影响占主导;参考环境下,胶接修理后层合板的固有频率增大;湿应力对层合板固有频率的影响大于热应力。  相似文献   

17.
The two-region fin model captures the heat spreading behaviour in multilayered composite bodies (i.e., laminates), heated only over a small part of their domains (finite heat source), where there is an inner layer that has a substantial capacity for heat conduction parallel to the heat exchange surface (convection cooling). This resulting heat conduction behaviour improves the overall heat transfer process when compared to heat conduction in homogeneous bodies. Long-term heat storage using supercooling salt hydrate phase change materials, stovetop cookware, and electronics cooling applications could all benefit from this kind of heat-spreading in laminates. Experiments using laminate films reclaimed from post-consumer Tetra Brik cartons were conducted with thin rectangular and circular heaters to confirm the laminate body, steady-state, heat conduction behaviour predicted by the two-region fin model. Medium to high accuracy experimental validation of the two-region fin model was achieved in Cartesian and cylindrical coordinates for forced external convection and natural convection, the latter for Cartesian only. These were conducted using constant heat flux finite heat source temperature profiles that were measured by infrared thermography. This validation is also deemed valid for constant temperature heat sources.  相似文献   

18.
Beams and plates manufactured from laminates of composite materials have distinct advantages in a significant number of applications. However, the anisotropy arising from these materials adds a significant degree of complexity, and thus time, to the stress and deformation analyses of such components, even using numerical approaches such as finite elements. The analysis of composite laminate beams subjected to uniform extension, bending, and/or twisting loads was performed by a novel implementation of the usual finite element method. Due to the symmetric features of the deformations, only a thin slice of the beam to be analysed needs to be modelled. Conventional three-dimensional solid finite elements were used for the structural discretization. The accurate deformation relationships were formulated and implemented through the coupling of nodal translational degrees of freedom in the numerical analysis. A sample solution for a rectangular composite laminate beam is presented to show the validity and accuracy of the proposed method.  相似文献   

19.
In the present paper, a series of hierarchical warping functions is developed to analyze the static and dynamic problems of thin walled composite laminated helicopter rotors composed of several layers with single closed cell. This method is the development and extension of the traditional constrained warping theory of thin walled metallic beams, which had been proved very successful since 1940s. The warping distribution along the perimeter of each layer is expanded into a series of successively corrective warping functions with the traditional warping function caused by free torsion or free bending as the first term, and is assumed to be piecewise linear along the thickness direction of layers. The governing equations are derived based upon the variational principle of minimum potential energy for static analysis and Rayleigh Quotient for free vibration analysis. Then the hierarchical finite element method is introduced to form a numerical algorithm. Both static and natural vibration problems of sample box beams are analyzed with the present method to show the main mechanical behavior of the thin walled composite laminated helicopter rotor. The project supported by the National Natural Science Foundation of China (19932030)  相似文献   

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