包带连接特性及星-箭-包带连接结构耦合动力学的研究进展

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doi:10.6052/1000-0992-11-035

清华大学精密仪器与机械学系, 北京 100084

基金项目:国家自然科学基金(11072123, 11102096), 国家“863” 计划项目(2009AA04Z401) 资助

详细信息

通讯作者:
褚福磊

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- 文章访问数:1964
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- 被引次数:0
出版历程
- 收稿日期:2011-03-24
- 修回日期:2011-05-25
- 刊出日期:2012-07-25

ADVANCES IN STUDY ON JOINT BEHAVIOR OF CLAMP BAND AND DYNAMICS OF SPACECRAFT-LAUNCH VEHICLE-CLAMP BAND COUPLING SYSTEM

Department of Precision Instruments and Mechanology, Tsinghua University, Beijing 100084, China

Funds:The project was supported by the National Natural Science Foundation of China (11072123, 11102096), China High Technology Research and Development Program by Ministry of Science and Technology (2009AA04Z401).

More Information

Corresponding author:CHU Fulei

摘要

摘要:包带连接结构是目前航天领域应用最广泛的星箭连接和分离机构. 包带连接结构通过组件间的接触、摩擦传递载荷, 在预紧力作用下实现星箭连接. 各组件间的接触、摩擦力学行为随外载荷的变化而改变, 从而导致包带连接刚度具有明显的非线性特征, 影响火箭的运载能力以及星箭系统的动力学特性. 本文对包带连接结构的局部连接特性及其对星箭整体系统动力学特性的影响进行了综述. 首先介绍了国内外针对包带连接特性开展的研究工作, 重点评述了有关包带连接结构的承载能力和连接刚度等问题的研究进展; 随后, 围绕包带连接结构在星箭系统模型中的表征及其对星箭系统动特性的影响等问题, 对星-箭-包带耦合动力学进行了论述; 最后, 指出了这一领域需要进一步研究的若干问题.
- 包带连接结构/
- 星-箭-包带耦合/
- 承载能力/
- 连接刚度/
- 动力学特性
Abstract:Clamp band joint is widely used as the mechanical attachment of spacecraft to the launch vehicle in the aerospace industry. The loads are transmitted between the spacecraft and the launch vehicle through frictional contacts between the components of the clamp band joint to realize the connection under pretightening forces. The contact and friction behaviors vary along with the variation of external loads, leading to the nonlinearity of the clamp band joint stiffness and consequently affecting the load capability and the dynamic characteristics of the launching system. In this paper, the study on local nonlinearity of the clamp band joint and its effects on the dynamics of the launching system are reviewed. Firstly, researches related to the joint characteristics of the clamp band joint are examined, where the load capability and the joint stiffness are discussed in detail. Then, studies on the dynamics of the spacecraft-launch vehicle-clamp band coupling system is summarized with focus laid on the representation of the clamp band joint in the launching system model and its effects on the dynamics of the launching system. Finally, existing problems and certain topics in need of further studies are pointed out.
- clamp band joint/
- spacecraft-launch vehicle-clamp band coupling/
- load capability/
- joint stiffness/
- dynamic characteristics

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参考文献 (52)

1 袁家军. 卫星结构设计与分析. 北京: 中国宇航出版社, 2004.434-478

2 长征四号乙运载火箭用户手册. 中国运载火箭技术研究院,1999. 55-1-55-28

3 Marman clamp system design guidelines. Guideline No. GD-ED-2214. NASA Goddard Space Flight Centre, 2000.1-8

4 张延珍. 战术导弹连接刚度的研究. 强度与环境, 1992, 2:28-35

5 谭雪峰, 阎绍泽. 星箭包带式连接结构动力学研究进展. 导弹与航天运载技术, 2010, 1: 1-6

6 Buffe J, Valli R. Shock analysis of the Ariane clampband release event on the Meteosat second generation satellite. In: Proceedings European Conference on Spacecraft Structures, 1998. 543-548

7 Takeuchi S, Onoda J. Estimation of separation shock of the Marman clamp system by using a simple band-mass model. Transactions of the Japan Society for Aeronauti- cal and Space Sciences, 2002, 45(147): 53-60

8 Chang K Y. V-band separation shock characteristics. NASA Jet Propulsion Laboratory, 2004, 10: 1-10

9 Iwasa T, Shi Q Z, Ando S, et al. Simplified SRS prediction method for pyroshock source of v-band clamp separation devices. In: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference,2007. 1-12

10 韩晓健, 焦安超, 王睿. 包带低冲击装置冲击试验及数据分析. 航天器环境工程, 2007, 24(5): 318-321

11 Lancho M, Larrauri I. CRSS: A separation system for launching very heavy payloads. Acta Astronautica, 2000,47: 153-162

12 Dowen D, Christiansen S. Development of a reusable, lowshock clamp band separation system for small spacecraft release applications. In: European Space Mechanisms & Tribology Symposium, 2001. 191-198

13 唐乾刚, 孙世贤. 包带式星箭紧锁预紧力分析. 国防科技大学学报, 1996, 18(2): 20-25

14 Di Tolla R, Ernst M. Nonlinear finite element evaluation of marman clamp structural capability. In: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 1994, 1: 320-330

15 Jacob I R, Vinay K G, Nicholas E M. Techniques for finite element analysis of clamp band systems. In:50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2009. 1-9

16 Fritskey J. Clamping and coupling with V-band retainers. Machine Design, 2003, 75(8): 68-70, 72

17 Shoghi K, Rao H V, Barrans S M. Stress in a flat section band clamp. In: Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2003, 217(7): 821-830

18 Shoghi K, Rao H V, Barrans S M. Stress in v-section band clamps. In: Proceedings of the Institution of Mechanical Engineers, Part C:Journal of Mechanical Engineering Sci- ence, 2004, 218(3): 251-262

19 Shoghi K, Barrans S, Ramasamy P. Axial load capacity of V-section band clamp joints. In: 8th International Conference on Turbochargers and Turbocharging, 2006. 273-285

20 秦朝烨, 阎绍泽, 褚福磊. 轴向拉力作用下包带锁紧装置连接特性研究. 第八届全国动力学与控制学术会议. 哈尔滨, 2008

21 秦朝烨, 褚福磊, 阎绍泽. 包带式星箭连接结构轴向刚度研究. 宇航学报, 2009, 30 (5): 2080-2085

22 Qin Z Y, Yan S Z, Chu F L. Dynamic analysis of clamp band joint system subjected to axial vibration. Journal of Sound and Vibration, 2010, 329: 4486-4500

23 白绍竣, 尉飞, 郑钢铁. 包带连接建模与非线性动力学特性分析. 振动与冲击, 2010, 29(5): 6-10

24 孙海霞, 范瑞祥. 星箭包带锁紧装置分离过程动态包络的动力学仿真. 导弹与航天运载技术, 2004(4): 15-18

25 Palmaer G D, Mitchell D H. Analysis and simulation of a high accuracy spacecraft separation system. Journal of Spacecraft and Rockets, 1966, 3(4): 458-463

26 李中郢, 崔乃刚. 载人飞船与运载火箭分离过程的仿真研究. 哈尔滨工业大学学报, 1999, 31(1): 119-122

27 Jeyakumar D, Rao B N. Dynamics of satellite separation system. Journal of Sound and Vibration, 2006(297): 444-455

28 谭雪峰, 阎绍泽. 星箭分离面径向冲击预示的简化圆环分析方法. 机械工程学报, 2010, 46(16): 95-100

29 谭雪峰, 阎绍泽. 包带式星箭连接结构的动力学模拟及故障分析. 清华大学学报(自然科学版), 2010, 50(8): 1205-1209

30 王毅, 朱礼文, 王明宇, 等. 大型运载火箭动力学关键技术及其进展综述. 导弹与航天运载技术, 2000, 1: 29-37

31 潘忠文. 运载火箭动力学建模及振型斜率预示技术. 中国科学E 辑: 技术科学, 2009, 39(3): 469-473

32 陈集丰, 王道锦, 杨云. 导弹、航天器结构分析与设计. 西安: 西北工业大学出版社, 1995. 166-196

33 Hurty W C. Dynamic analysis of structural systems using component modes. AIAA Journal, 1965, 3(4): 678-685

34 Craig Jr R R, Chang C J. Free-interface methods of substructure coupling for dynamic analysis. Journal of AIAA, 1976, 14(11): 1633-1635

35 Liew K M, Lee S E, Liu A Q. Mixed-interface substructures for dynamic analysis of flexible multibody systems. Engineering Structures, 1996: 18(7): 495-503

36 Lin C S, Cole T R. Dynamic model for Global Positioning System Block IIR space vehicle. Journal of Spacecraft and Rockets, 1997, 34(3): 334-359

37 侯悦民, 季林红, 金德闻. 结构局部刚度变化对小卫星动特性的影响. 宇航学报, 2003, 24(6): 588-593

38 Alley V L, Leadbetter S A. Prediction and measurement of natural vibrations of multistage launch vehicles. AIAA Journal. 1963, 1(2): 374-379

39 李效韩, 杨炳渊. 结构振动分析中的连接子结构. 宇航学报,1987, 1: 7-15

40 楼梦麟. 连接子结构与子结构模态综合法. 振动工程学报,1995, 8(1): 52-56

41 杨炳渊. 连接子结构试验建模的发展与应用. 温度与环境,2000, 1: 51-59

42 邱吉宝, 王建民. 运载火箭模态试验仿真技术研究新进展. 宇航学报, 2007, 28(3): 515-521

43 郑晓亚, 张铎, 姜晋庆. 连接刚度对导弹固有特性的影响. 弹箭与制导学报, 2005, 25(4): 667-669

44 南宫自军, 姜晋庆, 张铎. 固体火箭发动机连接结构接触应力研究. 推进技术, 1997, 18(4): 54-57

45 南宫自军, 张铎. 运载火箭级间分离面接触分析. 西北工业大学学报, 2000, 18(3): 466-468

46 周韶园. 考虑接触问题时某型导弹静、动特性分析: [硕士论文]. 西安: 西北工业大学, 2002. 29-72

47 宋波涛. 飞行器结构考虑连接面刚度的固有特性计算研究: [硕士论文]. 西安: 西北工业大学, 2003. 30-96

48 胡爱虔, 张铎. 飞行器结构考虑连接面刚度的固有特性计算研究. 弹箭与制导学报, 2005, 25(3): 298-301

49 王隆基. 套接结构的接触分析与试验研究: [硕士论文]. 西安: 西北工业大学, 2007. 5-32

50 郑晓亚, 张铎, 姜晋庆. 楔块连接的壳体力学特性分析. 机械科学与技术, 2008, 27(12): 1665-1669

51 Qin Z Y, Yan S Z, Chu F L. Dynamic characteristics of launch vehicle and spacecraft connected by clamp band. Journal of Sound and Vibration, 2011, 330(10): 2161-2173

52 马兴瑞, 王本利, 苟兴宇. 航天器动力学—— 若干问题进展及应用. 北京: 科学出版社, 2001. 1-29

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