翼型颤振压电俘能器的输出特性研究

压电俘能器能够为自然界中低功率的微机电系统持续供能.为了模拟机翼的沉浮-俯仰二自由度运动和有效俘获气动弹性振动能量,本文提出一种新颖的翼型颤振压电俘能器.基于非定常气动力模型,推导翼型颤振压电俘能器流-固-电耦合场的数学模型.建立有限元模型,模拟机翼的沉浮-俯仰二自由度运动,获得机翼附近的涡旋脱落和流场特性.搭建风洞实验系统,制作压电俘能器样机.利用实验验证理论和仿真模型的正确性,仿真分析压电俘能器结构参数对其气动弹性振动响应和俘获性能的影响.结果表明:理论分析、仿真模拟和实验研究获得的输出电压具有较好的一致性,验证建立数学和仿真模型的正确性.仿真分析获得机翼附近的压力场变化云图,表明交替的压力差驱动机翼发生二自由度沉浮-俯仰运动.当风速超过颤振起始速度时,压电俘能器发生颤振,并表现为极限环振荡.当偏心距为0.3和风速为16 m/s时,可获得最大输出电压为17.88 V和输出功率为1.278 m W.功率密度为7.99 m W/cm^(3),相比较于其他压电俘能器,能实现优越的俘获性能.研究结果对设计更高效的翼型颤振压电俘能器提供重要的指导意义.

Computations of Cross-Link Forces and Vibrations for the Test Bed of the Full Channel Gas

In order to control the cross? link forces and the vibration frequencies of the test bed of the full channel gas within the allowable ranges, the analyses of forces and deformation of the test bed was done, for the variously restrained elastic movable frame and the rigid one, the vibration frequencies were computed respectively by means of the methods of mechanics of materials, elasticity and vibration mechanics, the cross link forces and the vibration frequencies of the test bed were tested. The results of theoretical computation comparatively approach the experimental results. The computational methods could be used to availably estimate the design parameters relevant to the test bed of the full channel gas.

Wind-induced responses of super-large cooling towers

Traditional gust load factor(GLF)method,inertial wind load(IWL)method and tri-component method(LRC+IWL)cannot accurately analyze the wind-induced responses of super-large cooling towers,so the real combination formulas of fluctuating wind-induced responses and equivalent static wind loads(ESWLSs)were derived based on structural dynamics and random vibration theory.The consistent coupled method(CCM)was presented to compensate the coupled term between background and resonant response.Taking the super-large cooling tower(H=215 m)of nuclear power plant in Jiangxi Province,China,which is the highest and largest in China,as the example,based on modified equivalent beam-net design method,the aero-elastic model for simultaneous pressure and vibration measurement of super-large cooling tower is firstly carried out.Then,combining wind tunnel test and CCM,the effects of self-excited force on the surface pressures and wind-induced responses are discussed,and the wind-induced response characteristics of background component,resonant component,coupled term between background and resonant response,fluctuating responses,and wind vibration coefficients are discussed.It can be concluded that wind-induced response mechanism must be understood to direct the wind resistant design for super-large cooling towers.

Active control of supersonic/hypersonic aeroelastic flutter for a two-dimensional airfoil with flap

The flutter, post-flutter and active control of a two-dimensional airfoil with control surface operating in supersonic/hypersonic flight speed regions are investigated in this paper. A three-degree-of-freedom dynamic model is established, in which both the cubic nonlinear structural stiffness and the nonlinear aerodynamic load are accounted for. The third order Piston Theory is employed to derive the aerodynamic loads in the supersonic/hypersonic airflow. Nonlinear flutter happens with a phenomenon of limit cycle oscillations (LCOs) when the flight speed is less than or greater than linear critical speed. The LQR approach is employed to design a control law to increase both the linear and nonlinear critical speeds of aerodynamic flutter, and then a combined control law is proposed in order to reduce the amplitude of LCOs by adding a cubic nonlinear feedback control. The dynamic responses of the controlled system are given and used to compare with those of the uncontrolled system. Results of simulation show that the active flutter control method proposed here is effective.