防务技术2024,Issue(1) :41-48.DOI:10.1016/j.dt.2022.12.017

Experimental research on the launching system of auxiliary charge with filter cartridge structure

Zi-Jun Chen Ze He Hong-Hao Ma Lu-Qing Wang Zhao-Wu Shen
防务技术2024,Issue(1) :41-48.DOI:10.1016/j.dt.2022.12.017

Experimental research on the launching system of auxiliary charge with filter cartridge structure

Zi-Jun Chen 1Ze He 1Hong-Hao Ma 2Lu-Qing Wang 1Zhao-Wu Shen1
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作者信息

  • 1. CAS Key Laboratory of Mechanical Behavior and Design of Materials,Department of Modern Mechanics,University of Science and Technology of China,Hefei,Anhui,230027,PR China
  • 2. CAS Key Laboratory of Mechanical Behavior and Design of Materials,Department of Modern Mechanics,University of Science and Technology of China,Hefei,Anhui,230027,PR China;State Key Laboratory of Fire Science,University of Science and Technology of China,Hefei,Anhui,230026,PR China
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Abstract

A launching system with a filter cartridge structure was proposed to improve the muzzle velocity of the projectile.The combustion chamber of the launching system is divided into two fixed chambers,one is located in the breech chamber,and the other is arranged in the barrel.The breech chamber charge was ignited first,and the charges in the auxiliary chambers were ignited by the high-temperature,high-pressure combustible gas trailing the projectile.In this way,the combustible gas in the auxiliary chambers could compensate for the pressure drop caused by the movement of the projectile.The pro-posed device features the advantage of launching a projectile with high muzzle velocity without exceeding the maximum pressure in the chamber.In order to obtain some internal ballistic character-istics of the launch system,some critical structure,such as the length of the filter cartridge auxiliary charge,the combustion degree of the propellant in the chamber,and the length of the barrel,are dis-cussed.The experimental results show that with the increased auxiliary charge length,a pressure plateau or even a secondary peak pressure can be formed,which is less than the peak pressure.The projectile velocity increased by 23.57%,14.64%,and 7.65%when the diaphragm thickness was 0 mm,1 mm,and 2 mm,respectively.The muzzle velocity of the projectile can be increased by 13.42%by increasing the length of the barrel.Under the same charge condition,with the increase of barrel length,the energy utilization rate of propellant increases by 28.64%.

Key words

Interior ballistics/Charge structures/Launch system/Charge design

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基金项目

National Natural Science Foundation of China(51874267)

National Natural Science Foundation of China(12272374)

Fundamental Research Funds for the Central Universities(WK2480000008)

Fundamental Research Funds for the Central Universities(WK2480000007)

Fundamental Research Funds for the Central Universities(WK2320000049)

出版年

2024
防务技术
中国兵工学会

防务技术

CSTPCD
影响因子:0.358
ISSN:2214-9147
参考文献量35
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