混合作动系统的工作模式研究

具有非相似余度的混合作动系统(HAS)由功率电传作动器和传统的阀控液压伺服作动器(SHA)所组成,是未来多电飞机作动系统的发展趋势。阐述混合作动系统的结构组成及工作原理,建立其数学模型。对工作于两种传统模式——主动/主动模式和主动/被动模式时的混合作动系统进行了建模和理论分析。在此基础上,论述在一种全新的工作模式——主动/无载模式下,混合作动系统的结构组成和工作原理,并对其进行建模和理论分析。最后,对混合作动系统工作于每种模式下的优缺点进行了对比分析。分析结果对确定不同情况下混合作动系统的具体工作模式提供了依据。     

微型推力器阵列测试台研究

为了满足微型推力器阵列测试的需求,以4个高精度压电石英传感器为核心,设计了可以测试一个或者两个点火推力器的主推力并能计算出其位置坐标的测试台,并对测试系统进行了静态标定方法和动态谐响应分析研究,对台架X形板进行了去除材料85%以上的拓扑优化,最终使得本系统从理论上满足测试要求.      

变截面梁式压电智能板振动控制的小波模式

基于 Daubechies小波理论的尺度函数变换 ,对于变截面悬臂板结构的弯曲建立了由压电片感应器的观测电量识别挠曲变形构形的显式关系式。此基础上 ,采用具有位移与速度信号负反馈控制律后 ,建立了抑制振动的压电动力控制程序。由于小波尺度函数逼近具有低带通性质 ,即具有自动滤除高频分量的能力 ,该控制程序将不会出现由观测溢出与控制溢出耦合而造成的控制失稳 (即在抑制低频 (阶 )扰动时系统激发出高频 (阶 )扰动的现象 )。数值仿真结果表明 :该控制方法所能控制的模态阶数与压电片数相同 ,而且其控制程序在抑制外界干扰方面是有效的。     

二元智能复合材料结构变形分析

提出了嵌入形状记忆合金丝和压电陶瓷片作为联合变形驱动器的二元智能结构,并建立了有限元模型．驱动器镶嵌于层板表面或内部,其中压电陶瓷片作为压电铺层;形状记忆合金丝的驱动力当量为与温度相关的节点载荷．算例比较了不同种驱动方式的变形效果,并进行了试验验证．结果表明在二元智能结构的形状控制中,形状记忆合金丝承受主要的载荷,压电陶瓷片作变形修正,可以发挥各自的优点．      

基于PLZT的RAINBOW陶瓷的特性及其微观结构

RAINBOW陶瓷是一种具有内部应力偏移 ,并具有特殊的拱形结构的大位移驱动材料 ,它是通过将普通的压电陶瓷在高温下化学还原制备所得。实验表明 ,PLZT压电陶瓷具有较好的还原性能 ,还原层厚度与时间有线性关系 ,理想的还原条件为 :95 0℃保温 1～ 1 5h ;电镜照片显示RAINBOW陶瓷有明显的分层结构 ,还原层表现出穿晶断裂而未还原层则是沿晶断裂的特征。XRD谱发现还原层主要由金属Pb及PbO ,ZrO2 ,ZrTiO4等氧化物组成 ,原先的晶体结构已不存在 ;还原机制的理论分析与实验结果一致     

多电飞机电气系统关键技术研究

介绍了多电飞机电气系统关键技术的研究现状和发展趋势,阐述了电源系统结构,PSP和ELMC的结构与功能,电源系统BIT技术与容错技术以及电力作动技术等关键技术,并探讨了上述关键技术的设计方案。     

Energy Conversion Efficiency of Rainbow Shape Piezoelectric Transducer

With the aim to enhance the energy conversion efficiency of the rainbow shape piezoelectric transducer, an analysis model of energy conversion efficiency is established based on the elastic mechanics theory and piezoelectricity theory. It can be found that the energy conversion efficiency of the rainbow shape piezoelectric transducer mainly depends on its shape parameters and material properties from the analysis model. Simulation results show that there is an optimal length ratio to generate maximum energy conversion efficiency and the optimal length ratios and energy conversion efficiencies of beryllium bronze substrate transducer and steel substrate transducer are (0.65, 2.21%) and (0.65, 1.64%) respectively. The optimal thickness ratios and energy conversion efficiencies of beryllium bronze substrate transducer and steel substrate transducer are (1.16, 2.56%) and (1.49, 1.57%) respectively. With the increase of width ratio and initial curvature radius, both the energy conversion efficiencies decrease. Moreover, beryllium bronze flexible substrate transducer is superior to the steel flexible substrate transducer.     

Numerical Investigation of Flow Separation Control on a Highly Loaded Compressor Cascade by Plasma Aerodynamic Actuation

To discover the characteristic of separated flows and mechanism of plasma flow control on a highly loaded compressor cascade, numerical investigation is conducted. The simulation method is validated by oil flow visualization and pressure distribution. The loss coefficients, streamline patterns, and topology structure as well as vortex structure are analyzed. Results show that the numbers of singular points increase and three pairs of additional singular points of topology structure on solid surface generate with the increase of angle of attack, and the total pressure loss increases greatly. There are several principal vortices inside the cascade passage. The pressure side leg of horse-shoe vortex coexists within a specific region together with passage vortex, but finally merges into the latter. Corner vortex exists independently and does not evolve from the suction side leg of horse-shoe vortex. One pair of radial coupling-vortex exists near blade trailing edge and becomes the main part of backflow on the suction surface. Passage vortex interacts with the concentrated shedding vortex and they evolve into a large-scale vortex rotating in the direction opposite to passage vortex. The singular points and separation lines represent the basic separation feature of cascade passage. Plasma actuation has better effect at low freestream velocity, and the relative reductions of pitch-averaged total pressure loss coefficient with different actuation layouts of five and two pairs of electrodes are up to 30.8% and 26.7% while the angle of attack is 2°. Plasma actuation changes the local topology structure, but does not change the number relation of singular points. One pair of additional singular point of topology structure generates with plasma actuation and one more reattachment line appears, both of which break the separation line on the suction surface.     

压电网络板的振动控制原理与控制效果

在给出压电网络板机电耦合动力学方程的基础上对其进行求解,将压电网络板的响应表示为子模态压电系统响应的线性组合.通过分析压电网络板在脉冲激励下子模态压电系统的响应行为,揭示压电网络板可以通过两种途径控制自身振动.基于对传递函数的分析进一步得到子模态压电系统的最优电学参数;在此基础上研究了针对某一阶子模态压电系统设计最优电学参数时,各阶子模态压电系统的响应行为以及压电网络板的多模态控制效果.研究结果表明,压电网络板具有多模态控制效果,特别地,当对板的某一阶次的振动控制具有较高要求时,通过对最优电学参数进行设计,电感电阻并联型压电网络板可满足要求.     

压电陶瓷弹性支承干摩擦阻尼器减振实验

设计一种带有压电陶瓷执行机构的弹性支承干摩擦阻尼器,对其减振效果进行了实验验证.首先介绍了弹性支承干摩擦阻尼器的基本工作原理,接着回顾了一种电磁铁作动方式的弹性支承干摩擦阻尼器,提出了将压电陶瓷运用于其执行机构的方案,该方案可简化其结构,减少其质量,最后对该方案的减振效果进行了实验验证.结果表明:带有压电陶瓷执行机构的弹性支承干摩擦阻尼器对转子系统的振动具有明显的抑制作用,转子经过临界转速点的振幅最大减小约66%,并且与原阻尼器相比,结构更简单,质量减少一半,且功耗仅为5W.