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一种流口可控软后坐火炮反后坐装置设计与仿真

肖自强 贾亦卓 杨利

弹道学报2023,Vol.35Issue(4):35-42,8.
弹道学报2023,Vol.35Issue(4):35-42,8.DOI:10.12115/j.issn.1004-499X(2023)04-005

一种流口可控软后坐火炮反后坐装置设计与仿真

Design and Simulation of a Soft Recoil Device with Controllable Flow Port

肖自强 1贾亦卓 1杨利2

作者信息

  • 1. 陆军装甲兵学院 兵器与控制系,北京 100072
  • 2. 中国人民解放军 77626 部队,西藏 日喀则 857000
  • 折叠

摘要

Abstract

Soft recoil launching technology is an important technical way to reduce the recoil force of the gun.Soft recoil technology is normally achieved by fixed forward-rushing position.Because of the difference of bore pressure,the hydraulic resistance caused by recoil mechanism is remarkable in the process of firing.The moving parts cannot move to the right position normally when the ammunition is changed.In order to improve the performance and adaptability of the soft recoil gun,a soft recoil device with servo controlled adjustable flow port was proposed.By the application of before feedback control during firing,the hydraulic resistance can be adjusted effectively to adapt to multiply types of ammunition through forward-control.Based on the soft recoil launch test data of a conventional recoil device,the particle swarm optimization was used to identify the structural interval parameters.Then,the launching process of the proposed recoil device was simulated by combining the identified parameters and fluid simulation results.The simulation results show that the recoil mechanism can make the soft recoil gun work normally and stably under the condition of the different ammunition.The recoil force can be controlled within 400 kN,which meets the design requirements.Therefore,the new recoil mechanism has good adaptation for soft recoil firing of multiply types of ammunition,and it has great practical value,providing a certain reference for the design and application of the soft recoil gun.

关键词

软后坐火炮/反后坐装置/参数辨识/结构设计

Key words

soft recoil gun/recoil mechanism/identification/structural design

分类

军事科技

引用本文复制引用

肖自强,贾亦卓,杨利..一种流口可控软后坐火炮反后坐装置设计与仿真[J].弹道学报,2023,35(4):35-42,8.

弹道学报

OA北大核心CSCDCSTPCD

1004-499X

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