[1]孟 艳,王 玺,郭锦炎,等.多级活塞缸式发射装置结构安全性分析[J].弹道学报,2020,32(02):56-61.[doi:10.12115/j.issn.1004-499X(2020)02-009]
 MENG Yan,WANG Xi,GUO Jinyan,et al.Analysis on Structure Safety of Multi-stage Piston CylinderLaunching Equipment[J].Journal Of Ballistics,2020,32(02):56-61.[doi:10.12115/j.issn.1004-499X(2020)02-009]
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多级活塞缸式发射装置结构安全性分析()
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《弹道学报》[ISSN:1004-499X/CN:32-1343/TJ]

卷:
32
期数:
2020年02期
页码:
56-61
栏目:
出版日期:
2020-06-30

文章信息/Info

Title:
Analysis on Structure Safety of Multi-stage Piston CylinderLaunching Equipment
文章编号:
1004-499X(2020)02-0056-06
作者:
孟 艳王 玺郭锦炎吴新跃杭立杰
北京航天发射技术研究所,北京 100076
Author(s):
MENG YanWANG XiGUO JinyanWU XinyueHANG Lijie
Beijing Institute of Space Launch Technology,Beijing 100076,China
关键词:
导弹 内弹道 多级活塞缸 运动分析 结构安全 动力学仿真
Keywords:
missile interior ballistics multistage-piston launching equipment kinematic analysis structure safety dynamic simulation
分类号:
TJ303.4
DOI:
10.12115/j.issn.1004-499X(2020)02-009
文献标志码:
A
摘要:
多级活塞缸式发射装置作为新型冷发射方式之一,具有兼容不同弹径、免装填等优点。为研究多级活塞缸式发射装置的结构安全性,通过理论分析、数值仿真等方法对多级活塞缸式发射装置的运动过程进行了梳理,分析了多级活塞缸式发射装置中缓冲材料的吸能需求,并揭示了结构质量特性偏差、装配姿态偏差、燃气动力偏差、缓冲材料特性偏差等因素对导弹离台姿态的影响规律。多级活塞缸式发射装置的运动规律由各级缸筒的几何参数和被推动导弹的质量参数决定,对缓冲吸能的需求较高,多模块的多级活塞缸式发射装置中导弹的离台姿态更加稳定。研究结果可为多级活塞缸式发射装置安全性设计提供理论支撑,为多级活塞缸式发射武器系统提供指标分解依据。
Abstract:
As one of the new cold launching methods,the multi-stage piston cylinder launching equipment has the advantages of compatibility with different sizes of missile and loading free. In order to analyze structure safety of multi-stage piston cylinder launching equipment,the kinematic mechanism of the multi-stage piston cylinder launching equipment was studied by theoretical analysis and numerical simulation method,and the critical demands in energy absorbing of multi-stage piston cylinders were established. Influences of mass properties deviation,assembly posture deviation,gas power deviation,and cushioning material deviation on the attitude of missile were studied. The kinematic mechanism of the multi-stage piston cylinder launching equipment is determined by the geometry of the cylinder and the mass properties of the propelled missile. There is a high demand of energy absorbing in multi-stage piston cylinders. The off-platform attitude of missile is more stable in multi-module multi-stage piston cylinder launching equipment. The results can provide theoretical support for safety design of multi-stage piston cylinder launching equipment structure and weapon system index decomposition.

参考文献/References:

[1] 江坤,王浩,郭锦炎,等. 拉杆活塞式发射装置内弹道建模与仿真[J]. 弹道学报,2011,23(1):13-17.
JIANG Kun,WANG Hao,GUO Jinyan,et al. Modeling and simulation of interior ballistics of slide rod piston launching device[J]. Journal of Ballistics,2011,23(1):13-17.(in Chinese)
[2]仝建禄,刘少伟,王洁. 某型战术导弹弹射器的仿真研究[J]. 战术导弹技术,2005(1):63-65.
TONG Jianlu,LIU Shaowei,WANG Jie. The model simulation of ejecting device of certain tactical missile[J]. Tactical Missile Technology,2005(1):63-65.(in Chinese)
[3]殷增振,毕世华. 车载导弹多柔体发射动力学仿真研究[J]. 弹箭与制导学报,2009,29(2):183-185.
YIN Zengzhen,BI Shihua. Simulation study on multi flexible body launching dynamics for a vehicular missile launcher[J]. Journal of Projectiles,Rockets,Missiles and Guidance,2009,29(2):183-185.(in Chinese)
[4]高星斗,白静,张平,等. 发射箱车载倾斜热发射过程下沉量影响因素研究[J]. 导弹与航天运载技术,2015(2):59-62.
GAO Xingdou,BAI Jing,ZHANG Ping,et al. Study on influence factors of falling quantity for a slant-launched missile launch container in vehicular launching process[J]. Missiles and Space Vehicles,2015(2):59-62.(in Chinese)
[5]康甜,贺卫亮. 基于偏差模型的导弹发射动力学仿真[J]. 北京航空航天大学学报,2012(8):1112-1117.
KANG Tian,HE Weiliang. Missile launching dynamic simulation based on variation model[J]. Journal of Beijing University of Aeronautics and Astronautics. 2012(8):1112-1117.(in Chinese)
[6]赵克转,张高峰,尹兵. 防空导弹行进中发射动力学仿真分析[J]. 弹箭与制导学报,2012,32(4):39-45.
ZHAO Kezhuan,ZHANG Gaofeng,YIN Bing. Dynamic simulation analysis on marching launch of air defense missile[J]. Journal of Projectiles,Rockets,Missiles and Guidance,2012,32(4):39-45.(in Chinese)
[7]唐垚,姜毅,王成德,等. 多级活塞缸式燃气弹射内弹道的研究[J]. 固体火箭技术,2018,41(4):524-531.
TANG Yao,JIANG Yi,WANG Chengde,et al. Research on the internal trajectory of multi-stage piston cylinder gas ejection[J]. Journal of Solid Rocket Technology,2018,41(4):524-531.(in Chinese)
[8]高钦和,黄先祥. 多级缸起竖系统运动过程的建模与仿真[J]. 系统仿真学报,2005(7):1563-1565,1568.
GAO Qinhe,HUANG Xianxiang. Dynamic modeling and simulation of erecting system with multi-stage cylinder[J]. Journal of System Simulation,2005(7):1563-1565,1568.(in Chinese)
[9]腰善伟. 多级液压缸系统分析与仿真研究[D]. 合肥:合肥工业大学,2012.
YAO Shanwei. Analysis and simulation research of the multi-stage hydraulic cylinder system[D]. Hefei:Hefei University of Technology,2012.(in Chinese)
[10]虞军胜,赵凯. 自卸车多级缸乱筒故障树分析及技术改进[J]. 液压气动与密封,2013(7):52-54.
YU Junsheng,ZHAO Kai. Tipper multi-stage cylinder random cylinder fault tree analysis and technical improvement[J]. Chinese Hydraulics & Pneumatics,2013(7):52-54.(in Chinese)
[11]张宗华. 轻质吸能材料和结构的耐撞性分析与设计优化[D]. 大连:大连理工大学,2011.
ZHANG Zonghua. Crashworthiness analysis and design optimization of lightweight materials and structures for energy absorption[D]. Dalian:Dalian University of Technology,2011.(in Chinese)

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备注/Memo

备注/Memo:
收稿日期:2020-03-02
作者简介:孟艳(1988- ),女,工程师,研究方向为系统仿真。E-mail:mmyy1997@qq.com。
更新日期/Last Update: 1900-01-01