速射火炮定向反射膨胀减后坐力机理研究

doi:10.3969/j.issn.1000-1093.2019.12.003

兵工学报 ›› 2019, Vol. 40 ›› Issue (12): 2407-2415.doi: 10.3969/j.issn.1000-1093.2019.12.003

速射火炮定向反射膨胀减后坐力机理研究

戴劲松¹，何福¹，苏晓鹏²，王茂森¹，谭添¹

(1.南京理工大学机械工程学院，江苏南京 210094; 2.国营第152厂，重庆 400071)

收稿日期:2019-01-19 修回日期:2019-01-19 上线日期:2020-02-14
作者简介:戴劲松（1968—），男，研究员，博士生导师。E-mail:djs101@163.com
基金资助:
兵器装备联合基金项目（6141B02040201）

Research on Directional Reflection Expansion Mechanism of Reducing Recoil Force of Rapid Fire Gun

DAI Jinsong¹, HE Fu¹, SU Xiaopeng², WANG Maosen¹, TAN Tian¹

(1.School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China; 2.State-owned No.152 Factory, Chongqing 400071, China)

Received:2019-01-19 Revised:2019-01-19 Online:2020-02-14

摘要/Abstract

摘要： 传统速射火炮在高射速连发射击时，膛口装置后喷的气体对炮位附近装置和人员影响较大，为此提出定向反射膨胀减小后坐力机理。通过身管上多个前倾斜孔将火药气体引入封闭定向反射膨胀腔室中，利用火药气体在定向反射膨胀腔室前部形成的高压区及其对装置反射面的冲击作用，达到减小火炮后坐力的目的。运用计算流体力学理论分析了该机理，通过分析计算得到装置的减后坐力最大效率为48.3%，与现有速射火炮膛口装置制退器的效率相当且无向斜后方喷射的气体。开展了相应的实验研究，验证了理论分析的正确性。该机理具有广泛适用性，可为速射火炮降低后坐力提供新的思路。

关键词: 速射火炮, 定向反射膨胀, 后坐力, 膛口制退, 气体动力学

Abstract: When the traditional rapid fire gun automatically fires at a high rate, the powder gas that is sprayed backward has a greater impact on the devices and personnel near gun emplacement. A mechanism of reducing the recoil force by directional reflection expansion is proposed. The powder gas is introduced into a directional reflection expansion cavity through several front inclined holes on the gun tube. The recoil force is reduced by a high pressure zone formed by powder gas in front of cavity and its impact on the reflecting surface of the device. The expansion mechanism is analyzed by using the computational fluid dynamics theory. The result shows that the maximum recoil force-reducing efficiency of the device can reach 48.3%, which is equivalent to the existing traditional muzzle attachment of rapid fire gun. The corresponding experimental research was made to verify the correctness of the theoretical analysis. Key

Key words: rapidfiregun, directionalreflectionexpansion, recoilforce, muzzlebrake, aerodynamics

中图分类号:

TJ301

戴劲松，何福，苏晓鹏，王茂森，谭添. 速射火炮定向反射膨胀减后坐力机理研究[J]. 兵工学报, 2019, 40(12): 2407-2415.

DAI Jinsong, HE Fu, SU Xiaopeng, WANG Maosen, TAN Tian. Research on Directional Reflection Expansion Mechanism of Reducing Recoil Force of Rapid Fire Gun[J]. Acta Armamentarii, 2019, 40(12): 2407-2415.

参考文献

［1］戴劲松.现代小口径自动炮设计理论与方法[M].北京:兵器工业出版社，2012:201-256.
DAI J S. Design theory and method of modern small caliber gun[M].Beijing: Publishing House of Ordnance Industry，2012:201-256. (in Chinese)
[2］尤国钊，许厚谦.中间弹道学[M].北京:国防工业出版社，2003.
YOU G Z, XU H Q. Intermediate ballistics[M]. Beijing: National Defense Industry Press, 2003.(in Chinese)
[3］ BHATNAGAR R M. Recoil motion theorem[J]. Proceedings of the Institution of Mechanical Engineers, Part K: Journal of Multi-body Dynamics, 2005, 219(2):173-176.
[4］ ZHANG H H, CHEN Z H, JIANG X H,et al. Investigations on the exterior flow field and the efficiency of the muzzle brake[J].Journal of Mechanical Science and Technology，2013, 27(1):95-101.
[5］ MITCHELL M R, LINK R E, WU Y C, et al. Dynamic characteristics of a recoil system when firing projectiles with Mach 4.4 muzzle velocity from a 105 mm cannon[J].Journal of Testing & Evaluation, 2011, 39(4):103062.
[6］张焕好,陈志华,姜孝海,等.膛口装置三维流场的数值模拟及制退效率计算[J].兵工学报，2011,32(5):513-519.
ZHANG H H，CHEN Z H，JIANG X H，et al.Numerical simulation of the 3D flow fields of a muzzle brake and its efficiency calculation [J]. Acta Armamentaiii, 2011,32(5):513-519.(in Chinese)
[7］张焕好,陈志华,姜孝海,等.高速弹丸穿越不同制退器时的膛口流场波系结构研究[J].兵工学报，2012,33(5):623-629.
ZHANG H H, CHEN Z H, JIANG X H, et al. Investigation on the blast wave structures of a high-speed projectile flying through different muzzle brakes[J].Acta Armamentaii, 2012,33(5):623-629. (in Chinese)
[8］刘嘉鑫,袁军堂,汪振华,等.新型钛合金炮口制退器结构设计与分析[J].兵器材料科学与工程，2019，42(1):32-35.
LIU J X, YUAN J T, WANG Z H, et al. Structural design and analysis of new titanium alloy in muzzle brake[J]. Ordnance Material Science and Engineering，2019,42(1):32-35. (in Chinese)
[9］肖俊波,杨国来,李洪强,等.身管武器时延式喷管减后坐动力学建模仿真[J].兵工学报，2017,38(10):1909-1917.
XIAO J B, YANG G L, LI H Q, et al. Dynamics modeling and simulation of recoil reduction of automatic weapon by time-delay nozzle device[J]. Acta Armamentaii, 2017,38(10):1909-1917. (in Chinese)

[10］宋杰,邱明,廖振强,等.两种喷管气流反推装置建模与发射性能对比分析[J].北京理工大学学报,2018,38(6):585-592，605.
SONG J, QIU M, LIAO Z Q, et al. Modeling of two jet gas devices and its firing efficiency comparison[J]. Transactions of Beijing Institute of Technology,2018,38(6):585-592，605.（in Chinese）
[11］王永河,张世全,赵静,等.炮口制退器高效率低危害技术探讨[J].火炮发射与控制学报，2007,29(3):37-39，49.
WANG Y H，ZHANG S Q，ZHAO J，et al. Discussion about muzzle brake of high efficiency but low hazard technology[J].Journal of Gun Launch & Control，2007,29(3):37-39，49. (in Chinese)
[12］王加刚,余永刚,周良梁.埋头弹火炮高效低危害炮口制退器的实验研究[J].兵工学报，2017,38(5):1035-1040.
WANG J G, YU Y G, ZHOU L L. Experimental study of high efficiency and low hazard muzzle brake for CTA gun [J]. Acta Armamentaii, 2017, 38(5):1035-1040. (in Chinese)
[13］ CHATURVEDI E, DWIVEDI R K. Computer aided design and analysis of a tunable muzzle brake[J]. Defence Technology, 2019,15(1):89-94.
[14］廖振强,邱明.自动武器气体动力学[M].北京:国防工业出版社，2015:160-196.
LIAO Z Q, QIU M. Gas dynamic of automatic weapons[M]. Beijing: National Defense Industry Press, 2015:160-196. (in Chinese)
[15］王福军.计算流体动力学分析——CFD软件原理与应用[M].北京:清华大学出版社，2004:120-124.
WANG F J.Computational fluid dynamics analysis principle and application of CFD software[M]. Beijing: Tsinghua University Press, 2004：120-124. (in Chinese)
[16］钱林方.火炮弹道学[M].北京:北京理工大学出版社，2009:155-162.
QIAN L F. Artillery ballistics [M].Beijing: Beijing Institute of Technology Press，2009:155-162. (in Chinese)

第40卷第12期
2019 年12月兵工学报ACTA
ARMAMENTARIIVol.40No.12Dec. 2019

[1]	庞春桥，陶钢，李召，闻鹏，任保祥，李智宇. 轻型无后坐力炮的动不平衡冲量特性[J]. 兵工学报, 2020, 41(12): 2424-2431.
[2]	庞春桥，陶钢，闻鹏，李智宇，任保祥，王小峰. 某单兵无后坐力炮后喷区域危险性综合评估[J]. 兵工学报, 2019, 40(7): 1546-1552.
[3]	赵欣怡，周克栋，赫雷，陆野，李峻松. 某大口径轻武器射流噪声的小波分析与数值模拟[J]. 兵工学报, 2019, 40(11): 2195-2203.
[4]	陆野，周克栋，赫雷，李峻松，黄雪鹰. 膛口制退器效率对某新型全枪浮动原理大口径机枪的影响研究[J]. 兵工学报, 2016, 37(9): 1585-1591.
[5]	石江波，栗保明. 电磁轨道炮后坐过程研究[J]. 兵工学报, 2015, 36(2): 227-233.
[6]	宋杰, 廖振强, 李佳圣, 肖俊波. 导气与枪管浮动混合式自动机动力学特性研究[J]. 兵工学报, 2014, 35(6): 753-761.
[7]	李佳圣, 廖振强, 宋杰, 咸东鹏. 膛口制退效能对转管机枪射击密集度影响研究[J]. 兵工学报, 2013, 34(10): 1215-1220.
[8]	张焕好，陈志华，姜孝海，韩珺礼. 高速弹丸穿越不同制退器时的膛口流场波系结构研究[J]. 兵工学报, 2012, 33(5): 623-629.
[9]	陶德进，史慧敏，王军，薄煜明，郭治. 基于共有分量分解的速射火炮毁伤概率计算模型[J]. 兵工学报, 2012, 33(11): 1358-1363.

速射火炮定向反射膨胀减后坐力机理研究

Research on Directional Reflection Expansion Mechanism of Reducing Recoil Force of Rapid Fire Gun

PDF

可视化

被引次数

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 9

编辑推荐

Metrics

本文评价