期刊文献+

高温环境下复合材料加筋壁板振动/噪声动态结构破坏模式研究

Study On Vibration/Noise Dynamic Structural Failure Mode of Composite Stiffened Panel Under High Temperature Environment
下载PDF
导出
摘要 复合材料优异的耐磨损和耐高温性能在众多材料中脱颖而出,被广泛应用于航天航空领域。本文基于随机振动试验和掠入射噪声试验方法,使用试验验证的手段对复合材料加筋壁板开展室温振动、室温噪声试验以及高温振动联合、高温噪声联合试验,试验过程中采集动态加速度响应,获取到不同试验状态下的响应变化特征,并对其破坏形式及破坏时间进行了记录。试验得到:在高温环境下,振动载荷或噪声载荷对复合材料加筋壁板造成的破坏模式,为该材料的结构设计和使用提供相关依据。 The excellent wear resistance and high temperature resistance of composite materials stand out among many materials and are widely used in the field of aerospace.Based on random vibration test and grazing-incidence noise test methods,this paper uses experimental verification methods to carry out room temperature vibration and noise tests as well as combined high temperature vibration and high temperature noise tests on composite reinforced panels.During the test,dynamic acceleration response,and the response change characteristics under different test states are obtained.The destruction form and time were recorded.The results show that the damage mode caused by vibration load or noise load to the composite stiffened panel under high temperature environment,which provides the relevant basis for the structural design and use of the material.
作者 孙玉昆 王和 陈国一 金龙 王明 SUN Yu-kun;WANG He;CHEN Guo-yi;JIN Long;WANG Ming(Tianjin Aerospace Relia Technology Co.,Ltd Shenyang Branch,Shenyang 110027;Beijing Institute of Structure&Environment Engineering,Beijing 100076)
出处 《环境技术》 2023年第12期64-69,共6页 Environmental Technology
关键词 复合材料 振动 噪声 温度 composites vibration noise temperature
  • 相关文献

参考文献4

二级参考文献37

  • 1沙云东,魏静,高志军,钟皓杰.热声激励下金属薄壁结构的随机疲劳寿命估算[J].振动与冲击,2013,32(10):162-166. 被引量:22
  • 2Blevins R D,Holehouse I,Wentz K R.Thermoacoustic loads and fatigue of hypersonic vehicle skin panels[J].Journal of Aircraft,1993,30(6):971-978.
  • 3Swanson A D,Coghlan S C,Pratt D M,et al.Hypersonic vehicle thermal test challenges[R].AIAA-2007-1670.
  • 4Clarkson B L.Review of sonic fatigue technology[R].NASA-N94-29407.
  • 5Mixson J S,Roussos L A.Acoustic fatigue:overview of activities at NASA Langley[R].NASA-N87-24965.
  • 6Leatherwood J D,Clevenson S A,Powell C A.et al.Acoustic testing of high-temperature panels[J].Journal of Aircraft,1992,29(6):1130-1136.
  • 7Bayerdoerfer G,Freyberg L.Thermoacoustic tests to quniify TPS-Design[C].ESA SP-386:591-596,1996.
  • 8Clevenson S A,Daniels E F.Capabilities of the thermal acoustic fatigue apparatus[R].NASA-N92-22212.
  • 9Rizzi S A.Improvements to progressive wave tube performance through closed-loop control[R].NASA/TM-2000-210623.
  • 10Pacla A.Swanson A,Wentz K,Gerardi T.Elevated temperature acoustic test chamber development and construction[R].AIAA 93-4337.

共引文献44

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部