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高速飞行体无损回收试验研究

  • 霍力群 1 ,
  • 朱黎 2 ,
  • 黄楠 1 ,
  • 王争论 1
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  • 1 南京理工大学瞬态物理国家重点实验室,南京 210094
  • 2 重庆长安工业(集团)有限责任公司,重庆 401120

霍力群(1996—),女,内蒙古巴彦淖尔人,硕士研究生,研究方向:电磁发射技术。

收稿日期: 2020-09-18

  网络出版日期: 2025-02-20

Research on Nondestructive Recovery Technology of High-speed Flying Body

  • HUO Liqun 1 ,
  • ZHU Li 2 ,
  • HUANG Nan 1 ,
  • WANG Zhenglun 1
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  • 1 National Key Laboratory of Transient Physics,Nanjing University of Science and Technology,Nanjing 210094, China
  • 2 Chongqing Chang’an Industry (Group) Co., Ltd.,Chongqing 401120, China

Received date: 2020-09-18

  Online published: 2025-02-20

摘要

针对高速飞行体无损回收,建立飞行体穿越软介质的阻力模型,采用可清晰留痕的聚氨酯泡沫塑料为软回收介质材料设计无损回收装置,使用7.62 mm及14.5 mm弹丸模拟高速飞行体进行射击试验,在3.2 m距离内实现了对7.62 mm弹丸的无损回收。试验获得了飞行体穿越软介质的距离、速度、过载随时间的变化规律,得到飞行体穿越软介质的特征参数;观测软回收介质表面留存的飞行体的痕迹得到飞行体穿越软介质的空间姿态。

本文引用格式

霍力群 , 朱黎 , 黄楠 , 王争论 . 高速飞行体无损回收试验研究[J]. 弹箭与制导学报, 2021 , 41(3) : 128 -132 . DOI: 10.15892/j.cnki.djzdxb.2021.03.028

Abstract

For the non-destructive recovery of high-speed flying bodies, the resistance model of flying bodies through soft media was established. The non-destructive recovery device was designed with polyurethane foam that can clearly leave marks as the soft recovery media material. The 7.62 mm and 14.5 mm projectiles were used to simulate high-speed flying bodies for shooting tests, and the non-destructive recovery of 7.62 mm projectiles was achieved within a distance of 3.2 m. The experiment obtains the variation of the distance, speed, and overload of the flying body through the soft medium with time, and obtains the characteristic parameters of the flying body through the soft medium; the space attitude of the flying body passing through the soft medium is obtained by observing the traces of the flying body retained on the surface of the soft recovery medium.

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[1]
POPE M, MARTIN B, LAMBERT D, et al. Analysis of a soft catch for conventional warheads[C]//ASME. Proceeding of the 2005 ASME Pressure Vessels and Piping Division Conference.[S.l.]: ASME, 2005: 775-779.

[2]
ALLEN W A, MAYFIELD E B, MORRISON H L. Dynamics of a projectile penetrating sand: Part II[J]. Journal of Applied Physics, 1957, 28(11): 1331-1335.

[3]
ALLEN W A, MAYFIELD E B, MORRISON H L. Dynamics of projectile penetrating sand[J]. Journal of Applied Physics, 1957, 28(3): 370-376.

[4]
费东年. 高速飞行体无损回收装置的虚拟设计研究[D]. 南京: 南京理工大学, 2006.

[5]
毛磊, 方清. 弹丸高速侵彻水介质的理论分析与数值仿真[J]. 机械制造与自动化, 2015, 44(6):116-118.

[6]
毛磊. 软介质回收装置的关键技术研究[D]. 南京: 南京理工大学, 2015.

[7]
王俊晓, 向红军, 吕庆敖, 等. 电磁轨道炮U形铝质电枢回收过载极限分析[J]. 火炮发射与控制学报, 2019, 40(2):53-56.

[8]
陆鸣, 顾文彬, 唐勇, 等. 高速EFP软回收技术的试验研究[J]. 火炸药学报, 2008, 31(5):38-42.

[9]
蔡以涛. 多段式无损回收装置的概念设计技术研究[D]. 南京: 南京理工大学, 2007.

[10]
王俊晓, 向红军, 吕庆敖, 等. 电磁轨道炮超高速弹丸软回收技术需求及研究现状分析[J]. 飞航导弹, 2018(11):6-10.

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