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Research on Universal Flexible Cylinder Ejection

  • YANG Baosheng ,
  • JIANG Yi ,
  • SU Zhengyu ,
  • WANG Deng ,
  • YANG Lina
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  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received date: 2022-07-02

  Online published: 2025-02-01

Abstract

In order to further improving the compatibility of the catapult and realize the universalization of the catapult, this study proposes a universal flexible cylinder catapult with variable interior ballistics to realize the universalization of multi-type missiles. Based on the explicit dynamic theory, the finite element model of flexible cylinder ejection loads with multi-mode missile is established, and the research of flexible cylinder ejection for multi-mode missile based on particle method is realized. In this study, the pressure vessel test simulation of particle method and computational fluid dynamics method is compared, and the simulation results is consistent, which fully verifies the correctness and reliability of particle method. The research results show that continuous ejection will affect subsequent ejection, and the velocity of the second ejection is 8.7% lower than that of the first ejection, and the ejection overload is 4.4% lower. Further research shows that changing the opening timing of the inflatable valve can change the ejection performance, and opening the inflatable valve can effectively improve the ejection speed. Sequential opening helps to reduce the peak ejection overload. Changing the opening and closing diameter of the air valve and the opening time sequence can realize the universal ejection of multi-type missiles. The difference of ejection velocity between different orders of the same type missile is less than 12%, and the response time is less than 0.02 s.

Cite this article

YANG Baosheng , JIANG Yi , SU Zhengyu , WANG Deng , YANG Lina . Research on Universal Flexible Cylinder Ejection[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2023 , 43(1) : 70 -76 . DOI: 10.15892/j.cnki.djzdxb.2023.01.010

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[1]
赵克转, 张高峰. 导弹冷弹射过程建模及动力学仿真研究[J]. 弹箭与制导学报, 2012, 32(4): 45-48.

ZHAO K Z, ZHANG G F. Modeling and dynamic simulation studyon missile cold ejection process[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012, 32(4): 45-48.

[2]
杨寒, 王虹玥, 张家仙. 弹射器发展综述[J]. 推进技术, 2017(增刊1): 50-56.

YANG H, WANG H Y, ZHANG J X. Review of catapult development[J]. Journal of Propulsion Technology, 2017(S1): 50-56.

[3]
刘少伟, 关娇, 时建明, 等. 多燃气多时序点火优化技术[J]. 现代防御技术, 2019, 47(6): 27-33.

LIU S W, GUAN J, SHI J J M, et al. Optimization technique of asynchronous ignition time series with multi-gas Generators[J]. Modern Defense Technology, 2019, 47(6): 27-33.

[4]
赵勇. 通用飞行器地面电磁弹射工程系统研究[J]. 航空工程进展, 2015, 6(3): 387-394.

ZHAO Y. Study on general aircraft ground electromagnetic launch system[J]. Advances in Aeronautical Science and Engineering, 2015, 6(3): 387-394.

[5]
刘永亮, 任克亮, 马旭轮, 等. 模块化设计在舰载导弹垂直发射装置的应用[J]. 装备环境工程, 2021, 18(11): 77-82.

LIU Y L, REN K L, MA X L, et al. Modular design on the application of ship vertical launch[J]. Equipment Environmental Engineering, 2021, 18(11): 77-82.

[6]
柳忠彬, 肖守讷, 王欢. 非爆破柔性气缸弹射器研究[J]. 兵工学报, 2017, 38(2): 389-395.

DOI

LIU Z B, XIAO S N, WANG H. Research on non-blasting flexible cylinder launcher[J]. Acta Armamentarii, 2017, 38(2): 389-395

[7]
赵振, 姜毅, 刘相新, 等. 基于粒子法的柔性气缸导弹弹射数值仿真[J]. 兵工学报, 2022, 3(3): 533-541.

ZHAO Z, JIANG Y, LIU X X, et al. Numerical simulation of ejecting a missile from missile ejection system with flexible cylinder based on corpuscular method[J]. Acta Armamentarii, 2022, 43(3): 533-541.

DOI

[8]
WANG J T. An analytical model for an airbag with a hybrid inflator[J]. ASME, 1995, 30: 467-497.

[9]
WANG J T, NEFSKE D J. A new CAL3D airbag inflation model[J]. SAE Transactions, 1988, 97: 697-706.

[10]
OLOVSSON L. Corpuscular method for OOP Simulations, difficulty dealing with small vent holes[C]// IEEE. Proceedings of the 6th European LS-DYNA Users Conference. New York: IEEE, 2007: 1-4.

[11]
FREISINGER M, HOFFMANN J, STAHLSCHMIDT S. Investigation of the early inflation characteristics of a complex folded knee airbag with the new corpuscular method in LS-DYNA[C]// IEEE. Proceedings of the 6th European LS-DYNA Users Conference. New York: IEEE, 2007: 7-20.

[12]
MROZ K, PIPKORN B. Mathematical modelling of the early phase deployment of a passenger airbag-folding using origami theory and inflation using LS-DYNA particle method[C]// IEEE. Proceedings of the 6th European LS-DYNA Users Conference. New York: IEEE, 2007: 71-86.

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