陈天怡, 和卫平, 刘均, 等. 开孔球面舱壁特征应力组合代理模型预报方法[J]. 中国舰船研究, 2022, 17(6): 236–243. doi: 10.19693/j.issn.1673-3185.02390
引用本文: 陈天怡, 和卫平, 刘均, 等. 开孔球面舱壁特征应力组合代理模型预报方法[J]. 中国舰船研究, 2022, 17(6): 236–243. doi: 10.19693/j.issn.1673-3185.02390
CHEN T Y, HE W P, LIU J, et al. Combined surrogate model for stress prediction of spherical bulkhead with openings[J]. Chinese Journal of Ship Research, 2022, 17(6): 236–243. doi: 10.19693/j.issn.1673-3185.02390
Citation: CHEN T Y, HE W P, LIU J, et al. Combined surrogate model for stress prediction of spherical bulkhead with openings[J]. Chinese Journal of Ship Research, 2022, 17(6): 236–243. doi: 10.19693/j.issn.1673-3185.02390

开孔球面舱壁特征应力组合代理模型预报方法

Combined surrogate model for stress prediction of spherical bulkhead with openings

  • 摘要:
      目的  开孔球面舱壁结构参数众多,直接利用有限元方法对其开展参数研究费时费力,为此,提出一种特征应力组合代理模型预报方法。
      方法  提取开孔球面舱壁的几何特征参数,以此为设计变量构建一般形式的单开孔球面舱壁特征应力代理模型;采用代理模型对特征应力与结构参数进行相关性分析,提出一种缩减设计变量维度的组合代理模型方法,组合代理模型由基于柱−环−球壳参数构建的特征应力代理模型及基于开孔围栏参数和球壳厚度构建的特征应力修正系数代理模型组成。
      结果  结果显示,该组合代理模型能降低设计变量的维度,使得精度明显提升,相比直接构建的代理模型,其特征应力最大误差和平均误差分别降低了4.96%~22.95%和0.59%~5.43%;应用单开孔组合代理模型对典型的多个开孔球面舱壁特征应力进行的预报显示,特征应力误差为0.12%~11.42%。
      结论  所提的单开孔球面舱壁强度组合代理模型能用于多个开孔球面舱壁特征应力的快速预报。

     

    Abstract:
      Objective  A spherical bulkhead with openings has many structural parameters, and it is time-consuming and laborious to directly use the finite element method to carry out parameter research. Therefore, a combined surrogate model method for predicting characteristic stresses is proposed.
      Method  The geometric characteristic parameters of an opening spherical bulkhead are extracted and used as design variables to construct a surrogate model for the characteristic stresses of a spherical bulkhead with a single opening. After analyzing the correlation between the characteristic stresses and structural parameters using the surrogate model, a combined surrogate model method with lower dimensions of design variables is proposed. The combined surrogate model consists of a surrogate model of characteristic stresses based on the parameters of a cylindrical-toroidal-spherical shell and a surrogate model of characteristic stress correction coefficients based on the opening fence parameters and thickness of the spherical shell.
      Results  The results show that the accuracy of the combined surrogate model is significantly improved due to the lower dimensions of design variables. Compared with the results of the directly constructed surrogate model, the maximum error and average error of the characteristic stresses are reduced by 4.96%–22.95% and 0.59%–5.43% respectively. The single-opening combination surrogate model is used to predict the characteristic stresses of a typical spherical bulkhead with multiple openings, and the prediction errors of the characteristic stresses are 0.12%–11.42%.
      Conclusion  The proposed combined surrogate model for the strength of a spherical bulkhead with a single opening can be used for the rapid prediction of the characteristic stresses of spherical bulkheads with multiple openings.

     

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