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在主减速器斜撑杆上安装压电叠层作动器的直升机主动隔振
引用本文:王丽玮,夏品奇.在主减速器斜撑杆上安装压电叠层作动器的直升机主动隔振[J].南京航空航天大学学报,2018,50(2):233-238.
作者姓名:王丽玮  夏品奇
作者单位:南京航空航天大学直升机旋翼动力学国家级重点实验室
摘    要:采用安装在主减斜撑杆上的压电叠层作动器建立了直升机主动隔振系统。基于压电材料本构关系推导了压电叠层作动器的驱动方程,建立了压电叠层作动器驱动的主减主动隔振系统动力学模型。采用了自适应滤波控制方法,通过最小均方算法实现了自适应控制。直升机主动隔振仿真实验表明了该系统具有高效的隔振效果。

关 键 词:直升机主减  压电叠层作动器  主动隔振  自适应滤波控制
收稿时间:2017/12/15 0:00:00
修稿时间:2018/2/15 0:00:00

Active Vibration Isolation of Helicopter by Using Piezoelectric Stack Actuators Installed on Struts of Main Gearbox
WANG Liwei,XIA Pinqi.Active Vibration Isolation of Helicopter by Using Piezoelectric Stack Actuators Installed on Struts of Main Gearbox[J].Journal of Nanjing University of Aeronautics & Astronautics,2018,50(2):233-238.
Authors:WANG Liwei  XIA Pinqi
Institution:National Key Laboratory of Science and Tehnology on Rotorcraft Aeromechanics, Nanjing University of Aeronautics & Astronautics, Nanjing, 210016, China
Abstract:The active vibration isolation system of helicopter is established by using piezoelectric stack actuators installed on struts of main gearbox. Based on the constitutive relation of piezoelectric materials, the driving equation of the piezoelectric stack actuator is deduced, and the dynamic model of the main gearbox vibration isolation system driven by the piezoelectric stack actuators is established. The adaptive filtering process is realized by the least mean square(LMS) algorithm. The active vibration isolation simulation of helicopter is carried out, indicating that the system has an effective vibration isolation effect.
Keywords:helicopter main gearbox  piezoelectric stack actuator  active vibration isolation  adaptive filtering control
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