张学成,阎金贞,张保刚,秦旭峰,孙晓凤,吴君辉,张国军,刘陆广.板壳结构在声振联合试验下的振动响应耦合分析[J].装备环境工程,2024,2021(4):91-96. ZHANG Xuecheng,YAN Jinzhen,ZHANG Baogang,QIN Xufeng,SUN Xiaofeng,WU Junhui,ZHANG Guojun,LIU Luguang.Analysis of Response Coupling of Plate Shell Structure under Vibro-acoustic Test[J].Equipment Environmental Engineering,2024,2021(4):91-96.
板壳结构在声振联合试验下的振动响应耦合分析
Analysis of Response Coupling of Plate Shell Structure under Vibro-acoustic Test
投稿时间:2023-11-03  修订日期:2024-03-11
DOI:10.7643/issn.1672-9242.2024.04.011
中文关键词:  声振联合试验  板壳结构  环境载荷  交越频率  响应预测  极值包络法中图分类号:V416.5 文献标志码:A 文章编号:1672-9242(2024)04-0091-06
英文关键词:vibro-acoustic test  plate shell structure  environmental load  crossing frequency  response prediction  extremum envelope method
基金项目:
作者单位
张学成 陆军装备部驻上海地区第三军事代表室,上海 200031 
阎金贞 上海机电工程研究所,上海 201109 
张保刚 上海机电工程研究所,上海 201109 
秦旭峰 西南技术工程研究所,重庆 400039 
孙晓凤 上海航天精密机械研究所,上海 201600 
吴君辉 上海航天精密机械研究所,上海 201600 
张国军 上海航天精密机械研究所,上海 201600 
刘陆广 上海机电工程研究所,上海 201109 
AuthorInstitution
ZHANG Xuecheng Third Military Representative Office of Army Equipment Department in Shanghai, Shanghai 200031, China 
YAN Jinzhen Shanghai Electro-Mechanical Institute, Shanghai 201109, China 
ZHANG Baogang Shanghai Electro-Mechanical Institute, Shanghai 201109, China 
QIN Xufeng Southwest Institute of Technology and Engineering, Chongqing 400039, China 
SUN Xiaofeng Shanghai Spaceflight Precision Machinery Institute, Shanghai 201600, China 
WU Junhui Shanghai Spaceflight Precision Machinery Institute, Shanghai 201600, China 
ZHANG Guojun Shanghai Spaceflight Precision Machinery Institute, Shanghai 201600, China 
LIU Luguang Shanghai Electro-Mechanical Institute, Shanghai 201109, China 
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中文摘要:
      目的 研究具有工程实践意义的板壳组合结构在声振联合作用下的响应预测方法。方法 在噪声试验、振动试验和声振联合试验响应曲线的基础上,分析板壳组合结构在噪声和振动同时激励下的响应耦合规律,并根据噪声试验和振动试验的响应极值包络法,来预测在声振联合试验作用下板壳结构的响应分布。结果 声振联合试验响应曲线近似于噪声试验和振动试验的最大值包络线,噪声的面激励和随机振动的基础激励在不同的频率范围内对结构响应起着主要影响。试验件的噪声试验和振动试验响应曲线在给定的频率点出现相交,小于交越频率的声振联合试验响应与振动试验高度吻合,高于交越频率的响应则以噪声试验为主。结论 在工程实际中,可以直接利用振动试验和噪声试验的响应数据对声振联合试验的响应进行预测。由于交越频率难以事先获得,因此响应叠加法在实践中更易于实现。
英文摘要:
      The work aims to propose an engineering method with practical significance to predict the response of plate shell structure under vibro-acoustic coupling. Based on the response curves of noise test, vibration test and vibro-acoustic test, the response coupling law of plate shell structure under simultaneous excitation of noise and vibration was analyzed, and the response distribution of plate shell structure under vibro-acoustic test was predicted according to the response extremum envelope method of noise test and vibration test. The response curve of vibro-acoustic test was approximately the maximum envelope line of the noise test and vibration test. The surface excitation of noise and the basic excitation of random vibration mainly impacted the structural response in different frequency ranges. Response curves of noise test and vibration test intersected at the given frequency point. The response of vibro-acoustic test below the crossing frequency was highly consistent with the result of vibration test, while the response above the crossing frequency was mainly similar to the noise test. Based on these results, the extremum envelope method can be used to predict the response of plate shell structure under vibro-acoustic test by the response data of noise test and vibration test in engineering practices. In addition, the response superposition method is more suitable because it is difficult to obtain the crossing frequency in advance.
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