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基于正交实验法的弓网耦合除冰数值模拟

吴磊 徐梦楠 张华鹏 吴蔚 丁建明

南京航空航天大学学报(英文版)2023,Vol.40Issue(z1):29-41,13.
南京航空航天大学学报(英文版)2023,Vol.40Issue(z1):29-41,13.DOI:10.16356/j.1005-1120.2023.S1.003

基于正交实验法的弓网耦合除冰数值模拟

Numerical Simulation of Pantograph-Catenary Coupling De-icing Based on Orthogonal Experiment Method

吴磊 1徐梦楠 2张华鹏 2吴蔚 2丁建明3

作者信息

  • 1. 西南交通大学机械工程学院,成都 610031,中国||中国空气动力研究与发展中心结冰与防除冰重点实验室,绵阳 621000,中国
  • 2. 西南交通大学机械工程学院,成都 610031,中国
  • 3. 西南交通大学牵引动力国家重点实验室,成都 610031,中国
  • 折叠

摘要

Abstract

An investigation was conducted to examine the impact of the operating speed,ice thickness,pantograph head mass,pantograph head stiffness,and pantograph head damping on the de-icing rate.The investigation utilized the orthogonal experimental method and finite element simulation,employing a five-factor four-level orthogonal experimental design.Finite element models(FEM)were utilized to establish models for the ice-coating of the overhead contact system(OCS)and the coupling of the pantograph and catenary(PAC).The accuracy of the FEM was subsequently validated through a comparison between theoretical values and simulation results.The simulation results show that the operating speed and pantograph head mass have a significant impact on the contact force and contact wire lift amount,which in turn affects the de-icing rate.However,the influence of the pantograph head mass becomes less significant when it exceeds 17 kg.The results of the orthogonal experiment suggest that the de-icing rate is primarily influenced by the train speed,pantograph head mass,and ice thickness.The effects of pantograph head stiffness and damping are deemed insignificant.These results can provide references for improving train operation safety and PAC coupling de-icing technology.

关键词

正交试验法/有限元分析/弓网耦合/机械除冰

Key words

orthogonal experiment/finite element analysis/pantograph and catenary coupling/mechanical de-icing

分类

交通工程

引用本文复制引用

吴磊,徐梦楠,张华鹏,吴蔚,丁建明..基于正交实验法的弓网耦合除冰数值模拟[J].南京航空航天大学学报(英文版),2023,40(z1):29-41,13.

基金项目

This work was supported by Sichuan Science and Technology Program(No.2021YFG0194),and the Key Laboratory of Icing and Anti-icing,China Aerodynamics Research and Development Center(No.IADL20210410). (No.2021YFG0194)

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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