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大口径舰炮弹丸垂直装填卡膛影响因素分析

  • 刘瑞卿 , 1 ,
  • 杨力 1 ,
  • 庞喻 1 ,
  • 徐东明 2 ,
  • 王野 2
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  • 1 西安现代控制技术研究所,陕西 西安 710065
  • 2 辽沈工业集团有限公司,辽宁 沈阳 110045

刘瑞卿(1991—),男,高级工程师。E-mail:

收稿日期: 2024-07-05

  网络出版日期: 2025-03-12

Analysis of Influence Factors of Vertical Bayonet-chamber of Heavy Calibre Naval Gun Projectile

  • LIU Ruiqing , 1 ,
  • YANG Li 1 ,
  • PANG Yu 1 ,
  • XU Dongming 2 ,
  • WANG Ye 2
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  • 1 Xi'an Modern Control Technology Research Institute, Xi'an 710065,Shaanxi, China
  • 2 Liaoshen Industrial Group Co., Ltd., Shenyang 110045, Liaoning, China

Received date: 2024-07-05

  Online published: 2025-03-12

摘要

为研究影响大口径舰炮弹丸垂直装填惯性卡膛过程的因素,利用显式动力学有限元数值模拟和多体动力学仿真方法,并结合试验数据分析对比,综合考虑卡膛速度、铜带宽度、铜带外径、动摩擦系数以及入膛速度与卡膛速度的关系,得出了上述因素对卡膛结果的影响规律。研究结果表明:建立的基于显式动力学数值模拟方法可较好模拟弹丸卡膛过程,仿真结果与试验结果一致;影响卡膛深度和卡膛力的主要因素是卡膛速度与铜带宽度,而卡膛过载主要取决于卡膛速度的大小;为确保弹丸以最大偏移姿态完成卡膛的可靠性,弹丸的入膛速度应不小于6.35 m/s。

本文引用格式

刘瑞卿 , 杨力 , 庞喻 , 徐东明 , 王野 . 大口径舰炮弹丸垂直装填卡膛影响因素分析[J]. 弹箭与制导学报, 2025 , 45(1) : 85 -92 . DOI: 10.15892/j.cnki.djzdxb.2025.01.012

Abstract

In order to study the influence factors of vertical bayonet-chamber of heavy calibre naval gun projectile, a study is conducted using explicit dynamic finite element numerical simulation and multi-body dynamic simulation, combined with experimental data analysis and comparison. The influence of various factors on bayonet-chamber is obtained by analyzing bayonet-chamber velocity, copper strip width, copper strip outer diameter, dynamic friction coefficient, and the relationshipe between entry chamber velocity and bayonet-chamber velocity. The results are as follow: the established explicit dynamic numerical simulation method can effectively simulate the process of bayonet-chamber, and the simulation results are consistent with the experimental results. The main factors affecting the bayonet-chamber depth and force are the bayonet-chamber velocity and copper strip width, while the bayonet-chamber overload depends on the bayonet-chamber velocity. To ensure the bayonet-chamber reliability under maximum deviation attitude of projectile, the entry chamber velocity should not be less than 6.35 m/s.

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