Crashworthiness analysis and structural optimization of shrink tube under interference condition

被引:3
|
作者
Xu, Ping [1 ,2 ,3 ]
Yang, Yuhui [1 ,2 ,3 ]
Yang, Chengxing [1 ,2 ,3 ]
Yao, Shuguang [1 ,2 ,3 ]
Xing, Jie [1 ,2 ,3 ]
Zou, Fan [1 ,2 ,3 ]
机构
[1] Cent South Univ, Sch Traff & Transportat Engn, Key Lab Traff Safety Track, Minist Educ, Changsha 410075, Peoples R China
[2] Joint Int Res Lab Key Technol Rail Traff Safety, Changsha 410075, Peoples R China
[3] Natl & Local Joint Engn Res Ctr Safety Technol Rai, Changsha 410075, Peoples R China
关键词
Shrink tube; Interference fit; Trolley test; Theoretical prediction; Crashworthiness design; Parametric optimization; ENERGY-ABSORPTION CHARACTERISTICS; CIRCULAR TUBES; THEORETICAL-MODEL; CRUSHING ANALYSIS; EXPANSION; ABSORBERS; ALUMINUM; DIE; BEHAVIOR; SHAPE;
D O I
10.1016/j.jestch.2023.101504
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper aims to study the crashworthiness of shrink tubes for rail vehicles under axial impact loading. A theoretical model of shrink tube for platform force prediction under interference fit conditions was proposed. The trolley crash test was used to experimentally study the structural energy absorption and characteristics during collision, and a corresponding finite element model was constructed and validated. The finite element model validated the accuracy of the theoretical model. The influence of structural parameters on the crashworthiness of shrink tube under interference conditions was then studied. Structural design variables, including the magnitude of interference (int pre), thickness (T), long right-angle edge (tri x) and short right-angle edge (tri z) were sampled using a full factorial and a Latin hypercube design method. Based on the above samples, the moving least squares method (MLSM) was used to construct an approximate model of peak force (Fmax), specific energy absorption (SEA), and platform force (Fplt). The main effects analysis illustrated that the tri z had the most significant effects on the peak force, specific energy absorption and platform force. To minimize Fmax and maximize SEA, the global response surface method (GRSM) was employed for parameter optimization. Finally, the optimized configurations were obtained with int pre = 0.067mm, T = 10.003mm, tri x = 21.485 mm, and tri z = 6.101mm. Compared to the initial design, the SEA value was increased by 16.41 %, while the Fmax value was decreased by 2.21%. The error of platform force derived from the optimal solution and theoretical prediction was 3.62%, which verified that the theoretical prediction model was credible within an acceptable range.
引用
收藏
页数:15
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