刘明辉, 王剑, 高海洋, 岳志勇, 张俊刚. 大型振动台结构设计中的有限元分析与应用[J]. 航天器环境工程, 2016, 33(3): 257-261 DOI: 10.12126/see.2016.03.005
引用本文: 刘明辉, 王剑, 高海洋, 岳志勇, 张俊刚. 大型振动台结构设计中的有限元分析与应用[J]. 航天器环境工程, 2016, 33(3): 257-261 DOI: 10.12126/see.2016.03.005
Liu Minghui,. Application of FEA in structure design of large vibration test bed[J]. Spacecraft Environment Engineering, 2016, 33(3): 257-261. DOI: 10.12126/see.2016.03.005
Citation: Liu Minghui,. Application of FEA in structure design of large vibration test bed[J]. Spacecraft Environment Engineering, 2016, 33(3): 257-261. DOI: 10.12126/see.2016.03.005

大型振动台结构设计中的有限元分析与应用

Application of FEA in structure design of large vibration test bed

  • 摘要: 振动台是振动试验系统的主体结构。文章以某大型振动台结构设计为例,探讨了有限元法在振动台结构设计中的应用。工程实践表明,有限元法在大型振动台结构分析设计中,可以解决复杂结构的力学计算问题,有助改进结构设计,提高振动台结构的合理性和可靠性。

     

    Abstract: The vibration test bed is the main structure of a large vibration test system. For a typical large vibration test bed, the finite element analysis method is applied for the structural design of the test bed. It is concluded that the finite element analysis method can be used for a complex structure, and for optimizing the structure to improve the rationality and reliability of the test bed.

     

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