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某型导弹固体发动机喷管防水板结构优化设计

陈科 任全彬 尤军峰 王立强

固体火箭技术2015,Vol.38Issue(5):707-711,5.
固体火箭技术2015,Vol.38Issue(5):707-711,5.DOI:10.7673/j.issn.1006-2793.2015.05.019

某型导弹固体发动机喷管防水板结构优化设计

Structure optimization of waterproof board for the SRM of some missile

陈科 1任全彬 1尤军峰 1王立强1

作者信息

  • 1. 中国航天科技集团公司四院四十一所,西安 710025
  • 折叠

摘要

Abstract

Five parameters of waterproof board( WB) for the SRM of some type of missile were investigated using artificial neu-ral network algorithm (ANN).The objective function employed in the present work was the max stress and the min mass of the SRM waterproof board which bears a hydraulic pressure.The deformation and the strain of the waterproof board under the force of 10 t at center position were obtained,and the correctness of the numerical simulation was verified by comparing to the experimental results. The objective function vs. design variables curves were plotted,and the parameters sensitivity analysis were carried out.Optimization can decrease the mass of the waterproof board effectively by 45. 59% compared to traditional methods. The results obtained can be used as a guidline for the optimal structure design of the SRM waterproof board.

关键词

人工神经网络算法/有限元静力分析/喷管防水板/结构优化

Key words

artificial neural network algorithm/finite element static analysis/the waterproof board of the nozzle/structure opti-mization

分类

航空航天

引用本文复制引用

陈科,任全彬,尤军峰,王立强..某型导弹固体发动机喷管防水板结构优化设计[J].固体火箭技术,2015,38(5):707-711,5.

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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