运载火箭线式捆绑分离装置的设计、分析与优化

doi:10.3901/JME.2019.14.060

机械工程学报 ›› 2019, Vol. 55 ›› Issue (14): 60-68.doi: 10.3901/JME.2019.14.060

扫码分享

运载火箭线式捆绑分离装置的设计、分析与优化

毕祥军¹, 陈炳全^1,2, 吴浩³, 王立朋³, 蒋亮亮³, 王博¹, 周才华^1,4

1. 大连理工大学工业装备结构分析国家重点实验室大连 116024;
2. 中车长春轨道客车股份有限公司长春 130062;
3. 北京宇航系统工程研究所北京 100076;
4. 大连理工大学机械工程学院大连 116024

收稿日期:2018-09-05 修回日期:2019-01-09 出版日期:2019-07-20 发布日期:2019-07-20
通讯作者: 周才华(通信作者),男,1987年出生,博士后。主要研究方向为结构耐撞性与优化设计。E-mail:zhoucaihua@dlut.edu.cn
作者简介:毕祥军,男,1970年出生,硕士,副教授,硕士研究生导师。主要研究方向为实验力学。E-mail:bixj@dlut.edu.cn;陈炳全,男,1992年出生,硕士研究生。主要研究方向为结构优化设计。E-mail:chenbingquan@mail.dlut.edu.cn;王立朋,男,1979年出生,博士,高级工程师。主要研究方向为航天结构强度分析与优化设计。E-mail:wanglipeng79@126.com
基金资助:
工业装备结构分析国家重点实验室开放项目基金（GZ1510）、国家自然科学基金（11802051，11802053，11825202）、大连理工大学基本科研业务费（DUT17GF103）和中国博士后科学基金（2018M640252）资助项目。

Design, Analysis and Optimization of Linear Bundled Separation Device for Launch Vehicle

BI Xiangjun¹, CHEN Bingquan^1,2, WU Hao³, WANG Lipeng³, JIANG Liangliang³, WANG Bo¹, ZHOU Caihua^1,4

1. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024;
2. CRRC Changchun Railway Vehicles Co., Ltd., Changchun 130062;
3. Beijing Institute of Astronautical Systems Engineering, Beijing 100076;
4. School of Mechanical Engineering, Dalian University of Technology, Dalian 116024

Received:2018-09-05 Revised:2019-01-09 Online:2019-07-20 Published:2019-07-20

摘要/Abstract

摘要： 目前运载火箭的点式捆绑分离结构在承载过程中会产生过大的集中载荷。为解决这个问题，首次提出将线式分离系统应用在芯级与助推器的捆绑分离问题上，并对其进行结构优化设计，以提高结构的传力效率，实现结构轻量化。借助于有限元方法，分析捆绑状态下的受力状态和瞬态内压作用下分离系统的分离过程，深入地探讨出线式捆绑分离装置的捆绑和分离原理。基于Isight多学科优化平台集成ABAQUS，完成针对线式捆绑分离装置的优化设计。相比于传统的点式捆绑分离结构，优化后的线式捆绑分离装置减重48%，其点式结构产生的集中载荷过大问题得以有效缓解。线式捆绑分离装置的设计，和所运用的分析、优化体系，可以为我国未来运载火箭各类典型结构的设计提供参考。

关键词: 结构优化设计, 捆绑连接, 线式分离系统, 运载火箭

Abstract: Currently, the dotted strap-on linkage of launch vehicle has caused excessive concentrated load in the working process. In order to solve the problem, it's presented for the first time that a linear separation system can be applied to the issue of bundled separation between the central stage and the booster. And then linear bundled separation device is optimized to improve the power transmission efficiency and realize the lightweight design. FEM analysis is used to discuss the separation and linkage principle of linear bundled separation device, by simulating stress during binding and the separation process under transient internal pressures. Based on multidisciplinary optimization platform Isight and ABAQUS, the optimization design of linear bundled separation device is completed. Compared with the traditional dotted strap-on linkage, the optimized linear bundled separation device can lose the weight of the launch vehicle 48%, and the problem of excessive concentrated load is effectively solved. Design of linear bundled separation device and the analysis-optimization system will provide reference for our country's typical structures of launch vehicle in the future.

Key words: launch vehicle, linear separation joints, strap-on linkage, structural optimization design

中图分类号:

TG156

毕祥军, 陈炳全, 吴浩, 王立朋, 蒋亮亮, 王博, 周才华. 运载火箭线式捆绑分离装置的设计、分析与优化[J]. 机械工程学报, 2019, 55(14): 60-68.

BI Xiangjun, CHEN Bingquan, WU Hao, WANG Lipeng, JIANG Liangliang, WANG Bo, ZHOU Caihua. Design, Analysis and Optimization of Linear Bundled Separation Device for Launch Vehicle[J]. Journal of Mechanical Engineering, 2019, 55(14): 60-68.

参考文献

[1] 汪轶俊. 运载火箭固体捆绑技术研究[D]. 长沙:国防科学技术大学, 2007. WANG Yijun. Research on solid binding technology of launch vehicle[D]. Changsha:University of Defense Science and Technology, 2007.
[2] 马忠辉,冯韶伟,吴义田. 助推器超静定捆绑方案[J]. 导弹与航天运载技术, 2015(2):6-11. MA Zhonghui, FENG Shaowei, WU Yitian. Research on the scheme of hyper-static strap-on launch vehicle[J]. Missiles and Spcae Vehicles, 2015(2):6-11.
[3] STOREY R E. Dynamic analysis of clustered boosters with applications to TITAN Ⅲ[C]//Los Angeles:AIAA Summer Meeting, 1963:6224-6264.
[4] MARIETTA M. Corporation space shuttle external tank (lightweight model)[M]. New Orleans:System Definition Handbook, 1983.
[5] FENG Shaowei, LIU Zhusheng, MA Zhonghui, et al. Status of application of coupling technology in strap-on launch vehicle[J]. Missiles and Spcae Vehicles, 2012, 6:20-23.
[6] FLAURSEN E, VOCE J E. The proton launch vehicle system current status[R]. AIAA, 1996.
[7] 吴小宁,吴会强,史淑娟. 能源号重型火箭助推分离技术研究[J]. 导弹与航天运载技术, 2014(4):41-45. WU Xiaoning, WU Huiqiang, SHI Shujuan. Study on booster separation technology of energya super-heavy launch vehicle. missiles and spcae vehicles, 2014(4):41-45.
[8] GIGOU J. Ariane 5 solid-propellant stage development[C]//Huntsville, AL:AIAA Apace Programs and Technologies Conference, 1992, 1656-1665.
[9] 尚辉,才满瑞. H-ⅡA系列运载火箭[J]. 导弹与航天运载技术, 2006(5):24-30. SHANG Hui, CAI Manri. H-ⅡA launch vehicle family[J]. Missiles and Spcae Vehicles, 2006(5):24-30.
[10] FUJITA T, FUKUSHIMA Y, NAGATOMO M. H-Ⅱ solid rocket booster design and development[C]//Huntsivolle:AIAA Space Programs and Technologies Conference, 1992:1-6.
[11] NIU Fei, WANG Bo, CHENG Gengdong. Optimum topology design of structural part for concentration force transmission[J]. Chinese Journal of Theoretical and Applied Mechanics, 2012, 44(3):528-536.
[12] ZHANG Xiaoying, LI Linsheng, WU Huiqiang, et al. Research on concentrated force diffusion for weld thin-wall tank[J]. Structure & Environment Engineering, 2016, 43(5):38-44.
[13] 梅勇,冯韶伟,雷勇军, 等. 捆绑联接舱段集中力扩散结构优化设计[J]. 机械设计与制造, 2016(3):200-203. MEI Yong, FENG Shaowei, LEI Yongjun, et al. Structural optimization of the concentrated force diffusion structure in strap-on linkage section[J]. Machinery Design & Manufacture, 2016(3):200-203.
[14] WASSELL S G, RENFRO S L, DENSMORE H W, et al. Explosive release coupling:US, US 5331894 A[P]. 1994-07-26.
[15] 谢鲁. 膨胀管分离装置的研究[D]. 南京:南京理工大学, 2006. XIE Lu. Study on the separation device of the expansion tube[D]. Nanjing:Nanjing University of Science & Technology, 2006.
[16] HHOOPUTRA, HGESE H, HDELLH, et al. A comprehensive failure model for crashworthiness simulation of aluminium extrusions[J]. International Journal of Crashworthiness, 2004, 9(5):449-464.
[17] NIU F, XU S L, CHENG G D. A general formulation of structural topology optimization for maximizing structural stiffness[J]. Structural and Multidisciplinary Optimization, 2011, 3(4):561-572.
[18] 徐鹤鸣. 多目标粒子群优化算法的研究[D]. 上海:上海交通大学, 2013. XU Heming. Research on multiobjective particle swarm optimization algorithms[D]. Shanghai:Shanghai Jiao Tong University, 2013.

运载火箭线式捆绑分离装置的设计、分析与优化

Design, Analysis and Optimization of Linear Bundled Separation Device for Launch Vehicle

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 4

编辑推荐

Metrics

本文评价

[1]	霍家骥, 于洪杰, 潘鑫, 江志农, 宾光富. 大型旋转设备压液式自动平衡系统[J]. 机械工程学报, 2023, 59(18): 121-129.
[2]	王志祥, 雷勇军, 张大鹏, 欧阳兴, 王婕. 考虑加工误差的大型运载火箭框桁加强薄壁圆柱壳优化设计[J]. 机械工程学报, 2021, 57(18): 190-203.
[3]	段清娟, 殷成熙, 段宝岩. FAST 50 m模型馈源支撑系统的结构参数优化[J]. 机械工程学报, 2017, 53(17): 31-35.
[4]	杨健;肖宗亮;邓嘉胤;王乐勤;杨旭. 基于内流场数值模拟的微湍流发生器机械结构优化设计方法[J]. , 2007, 43(5): 127-132.