首页|碳纤维树脂基复合材料回转体的网格结构优化研究

碳纤维树脂基复合材料回转体的网格结构优化研究

Optimization of Grid Structure of Carbon Fiber Resin Matrix Composite Rotary Body

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针对复杂回转体的网格结构参数进行优化,以最大载荷质量比为优化目标,筋条几何参数及数量为设计变量,ABAQUS有限元屈曲分析为手段,确定模型结构承载效率的评价指标,进行单因素分析.其中,纵筋数量、纵筋宽度、筋条高度 3 种因素对模型承载效率影响较为显著.环筋数量与环筋宽度对模型承载效率的影响显著性较低,并结合实际制造条件分析得出用于正交试验的因素范围.利用数理上的正交性原理设计了L16(45)正交表与适用于复杂网格结构的正交试验方案.通过数值模拟,得到 16 组试验结果,并对试验结果进行极差分析.发现各因素对目标值影响程度的排序均为:纵筋宽度>筋条高度>纵筋数量>环筋数量>环筋宽度,并得出最优参数组合.最后对最优参数组合进行试验验证,找出使用最优参数组合的回转体所能承受最大载荷的理论值与实际值之间的差异,并分析差异出现的原因.
In this paper,the grid structure parameters of complex rotary body are optimized,with the maximum load-mass ratio as the optimization objective and the geometric parameters and number of ribs as the design variables,the evaluation index of load bearing efficiency of the model structure was determined,and the single factor analysis was carried out by using the buckling analysis of ABAQUS.The number of longitudinal ribs,width of longitudinal ribs and height of longitudinal ribs have significant effects on the model's bearing efficiency.The number and width of ring ribs have a low influence on the model's bearing efficiency.The factor range for orthogonal test is obtained by analyzing actual manufacturing conditions.The orthogonal table L16(45)is designed by using the principle of orthogonality in mathematics.An orthogonal test scheme suitable for complex grid structure is designed.Through numerical simulation,16 groups of test results were obtained,and the test results were analyzed by range analysis.It is found that the order of influence degree of each factor on the target value is:Longitudinal rib width>rib height>number of longitudinal rib>number of ring rib>ring rib width,and the optimal parameter combination is obtained.Finally,the optimal parameter combination is verified by experiment,and the difference between the theoretical value and the actual value of the maximum load of the rotary body using the optimal parameter combination is found,and the reason of the difference is analyzed.

Grid structureBuckling analysisBearing efficiencyOrthogonal testAutomatic laying

王显峰、林国军、李星泽、刘浩

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南京航空航天大学,南京 210016

网格结构 屈曲分析 承载效率 正交试验 自动铺放

2024

航空制造技术
北京航空制造工程研究所

航空制造技术

CSTPCD北大核心
影响因子:0.403
ISSN:1671-833X
年,卷(期):2024.67(14)