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永磁式磁阻尼制退机设计与优化方法

范雨萌 杨国来

弹道学报2025,Vol.37Issue(3):120-128,9.
弹道学报2025,Vol.37Issue(3):120-128,9.DOI:10.12115/ddxb.2024.07006

永磁式磁阻尼制退机设计与优化方法

Design and Optimization Method of Permanent Magnet Eddy Current Recoil Brake

范雨萌 1杨国来1

作者信息

  • 1. 南京理工大学 机械工程学院,江苏 南京 210094
  • 折叠

摘要

Abstract

Aiming at the forward design requirements of permanent-magnet eddy current recoil brakes(ECRB),an integrated design methodology was proposed by combining the recoil braking characteristic curve of anti-recoil mechanisms and the resistance characteristics of ECRB,achieving reverse-solving of structural parameters based on design specifications.Firstly,the recoil braking diagram corresponding to the ECRB was designed,and the desired braking force was obtained.By analyzing the design parameters and working point of the permanent magnet of ECRB,using the proportion of the overall size of the machine as a limitation,the design parameters can be calculated.According to a given set of design indexes,based on the parameter values obtained through the above design method,taking the smoothness of the braking force curve and the maximum recoil displacement as the optimization objectives,the dimensional parameters were further optimized.The optimization results were verified by finite element models.The optimized design parameters meet the design requirements and optimization expectations.Traditional eddy current damper design methods rely on analysis of resistance characteristic parameters,and require empirical parameter adjustments to approximately meet braking force requirements.The method proposed in this paper can directly derive key parameters from design specifications,and it can support multi-objective optimization design based on performance requirements,significantly enhancing design efficiency and accuracy.

关键词

磁阻尼制退机/反后坐装置/磁路设计/永磁式涡流阻尼器/动态响应优化

Key words

eddy current recoil brake/recoil mechanism/magnetic circuit design/permanent magnet eddy current brake/dynamic response optimization

分类

军事科技

引用本文复制引用

范雨萌,杨国来..永磁式磁阻尼制退机设计与优化方法[J].弹道学报,2025,37(3):120-128,9.

弹道学报

OA北大核心

1004-499X

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