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Two Degree-of-Freedom Dynamic Theoretical Model on Tile Thermal Protection System

机译:瓷砖热保护系统的二自由度动态理论模型

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摘要

In order to study the dynamic behaviors of the thermal protection system(TPS)and dynamic strength of the strain-isolation-pad(SIP),a two degree-of-freedom dynamic theoretical model is presented under the acoustic excitation and base excitation. The tile and SIP are both considered as the elastic body and simplified as a mass point, a linear spring and a damping element. The theoretical solutions are derived,and the reasonability of theoretical model is verified by comparing the theoretical results with the numerical results. Finally,the influences on the dynamic responses of TPS by the structural damping coefficient of TPS,elasticity modulus and thickness of SIP are analyzed. The results show that the material with higher damping,and SIP with thicker size and lower elastic modulus should be considered to reduce the dynamic responses and intensify the security of TPS. The researches provide a theoretical reference for studying the dynamic behaviors of TPS and the dynamic strength of SIP. Besides,the dynamic theoretical model can be used as a quick analysis tool for analyzing the dynamic responses of TPS during the initial design phase.
机译:为了研究热保护系统(TPS)的动态特性和应变隔离垫(SIP)的动态强度,提出了在声激励和基础激励下的两自由度动力学理论模型。瓦片和SIP都被视为弹性体,并简化为质量点,线性弹簧和阻尼元件。推导了理论解,并将理论结果与数值结果进行了比较,验证了理论模型的合理性。最后,分析了TPS的结构阻尼系数,弹性模量和SIP厚度对TPS动力响应的影响。结果表明,应考虑采用阻尼较大的材料,尺寸较大,弹性模量较低的SIP材料,以减小动力响应,增强TPS的安全性。这些研究为研究TPS的动态行为和SIP的动态强度提供了理论参考。此外,动态理论模型可以用作快速分析工具,以分析TPS在初始设计阶段的动态响应。

著录项

  • 来源
    《南京航空航天大学学报(英文版)》 |2019年第1期|139-145|共7页
  • 作者单位

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    AVIC Chengdu Aircraft Design and Research Institute,Chengdu 610091,P.R.China;

    AVIC Chengdu Aircraft Design and Research Institute,Chengdu 610091,P.R.China;

    AVIC Chengdu Aircraft Design and Research Institute,Chengdu 610091,P.R.China;

    AVIC Chengdu Aircraft Design and Research Institute,Chengdu 610091,P.R.China;

  • 收录信息 中国科学引文数据库(CSCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 随机振动;
  • 关键词

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