首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于光学自准直原理的喷管角度偏差测量方法研究
引用本文:陆油松,张大有,赵悄然,隋丽.基于光学自准直原理的喷管角度偏差测量方法研究[J].宇航计测技术,2020,39(4):41-45.
作者姓名:陆油松  张大有  赵悄然  隋丽
作者单位:1.海军装备部北京局驻北京地区第一军事代表室,北京100076;2. 吉林江机特种工业有限公司,吉林 132021;3. 北京航天计量测试技术研究所,北京 100076
基金项目:国家重点研发计划(2017YFF0205200)。
摘    要:提出了一种基于光学自淮直原理的喷管角度偏差测量方法,通过专用靶标将庭拟的喷管轴线等效替代为靶标轴端反光镜的法线,实现发动机喷管基淮孔轴线空间角度偏差的快速准确、实时測量,及时提供测量数据,有效保证零件、部件和发动机总装的质量一致性和可 靠性。利用该方法研制了一套发动机多喷管轴线角度偏差自动测量装置并进行了试验验证,结果表明该装置测量精度与三坐标表测量机的测量精度按近,符合测量误差分析,满足使用要求。

关 键 词:压电悬臂梁    流固耦合    颤振    输出电压    充电特性

Experimental and Simulation Study of Wind Induced Based Piezoelectric Generator
LU You-song,ZHANG Da-you,ZHAO Qiao-ran,SUI Li.Experimental and Simulation Study of Wind Induced Based Piezoelectric Generator[J].Journal of Astronautic Metrology and Measurement,2020,39(4):41-45.
Authors:LU You-song  ZHANG Da-you  ZHAO Qiao-ran  SUI Li
Institution:1. First Military Representative Office of Beijing Bureau of Naval Armament in Beijing Region, Beijing 100076, China;2. Jilin Jiangji Special Industries Co., Ltd,Jilin 132021, China;3. Beijing Aerospace Institute for Metrology and Measurement, Beijing 100076 China
Abstract:With the development of low-power MEMS device, more and more micro-generators have emerged, of which piezoelectric generators are typical representatives. This paper intends to conduct experimental and simulation study on Wind Induced Based Piezoelectric Cantilevers. The main contents include two parts. First, establishing fluid-structure interaction simulation model and analyzing mechanical environment and flutter mechanism of flexible beam submerged in axial flow. Second, investigating the voltage output characteristics of piezoelectric cantilever under the conditions of subcritical flutter velocity and supercritical flutter velocity. The output voltage and the charging performance under the conditions of subcritical and supercritical flutter velocity are explored. The results show that the peak output voltage is approximately 20V under the conditions of supercritical flutter velocity and close to zero under the conditions of subcritical flutter velocity. A single piezoelectric cantilever can charge a 10μF capacitor up to 22V in 10s. This paper illustrates the possibility of charging low-power MEMS devices with Micro-piezoelectric generators.
Keywords:Piezoelectric cantilever                                                                                                                        Fluid structure interaction                                                                                                                        Flutter                                                                                                                        Output voltage                                                                                                                        Charging performance
点击此处可从《宇航计测技术》浏览原始摘要信息
点击此处可从《宇航计测技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号