航空工程进展2024，Vol.15Issue(2)：77-89,13.DOI:10.16615/j.cnki.1674-8190.2024.02.09
基于正交试验的民用飞机抗爆结构参数敏感性分析
Sensitivity analysis of anti-explosion structure parameters of civil aircraft based on orthogonal experiment
薛小锋 1欧靖 1林心怡 1冯蕴雯 1杨祥2
作者信息
- 1. 西北工业大学 航空学院,西安 710072
- 2. 上海飞机设计研究院 机体集成部,上海 201210
- 折叠
摘要
Abstract
Least risk bomb location(LRBL)structure is a device for placing suspicious explosives on the aircraft.Exploring the influence of structure size and explosive location on its anti-explosion performance can provide a refer-ence for improving the design.Based on the method of combining orthogonal experimental design with numerical simulation,the maximum strain and deformation of each dangerous part of LRBL structure are used as evaluation indicators.The range analysis method and variance analysis method are respectively used to carry out parameter sensitivity analysis on the five influencing factors of the tank wall thickness,bottom cover thickness,connection boss thickness,shear pin diameter and explosive position of LRBL structure.The results show that when the explo-sive equivalent is determined as 200 g,the significant degree of influence of each factor on the antiknock perfor-mance of the LRBL structure from large to small is as follows:explosive position,tank wall thickness,bottom cov-er thickness,boss thickness and shear pin diameter;Based on comprehensive analysis of evaluation indicators,the LRBL structural design scheme at the optimal level of each factor is obtained.关键词
最小风险炸弹位置/参数敏感性分析/正交试验设计/结构优化/爆炸仿真Key words
least risk bomb location/parameter sensitivity analysis/orthogonal experimental design/structural op-timization/explosion simulation分类
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薛小锋,欧靖,林心怡,冯蕴雯,杨祥..基于正交试验的民用飞机抗爆结构参数敏感性分析[J].航空工程进展,2024,15(2):77-89,13.
