拦阻索冲击的多体动力学仿真研究

Abstract
Figure/Table
References (17)
Related Citation (15)

Download: PDF (1740 KB) HTML (1 KB)
Export: BibTeX | EndNote (RIS)

Abstract

When aircraft is landing on carrier, the impact stress, generated at the moment of tail-hook arresting cross deck pendant, propagates to both ends of the wire rope. To simulate and understand the governing law of this stress wave, a cable element with contact and large displacement functionality was developed in this paper based on absolute nodal coordinate formulation under the framework of multi-body dynamics. And then a multi-body dynamic model of the whole arresting system was built. The results of simulation show that stress peaks are caused by reflection and superposition of transverse wave at deck sheaves and carrier-based aircraft tail-hook, after tail-hook arrests the cross deck pendant. The study further shows that damper sheave installation can reduce stress peak effectively, and replace the rope with lightweight material will also weak the stress peak. Besides, the multi-body model of full-size arresting system built here provides an effective simulation way to assist the design and optimization work of the whole arresting system.

Key words： cross deck pendant multi-body dynamics impact stress wave

Received: 12 September 2013 Published: 15 March 2015

	Service

	E-mail this article
	Add to my bookshelf
	Add to citation manager
	E-mail Alert
	RSS
	Articles by authors
	Shen Wenhou 1
	2
	Zhao Zhihua 1
	Ren Genxue 1
	Wang Ningyu 1

Cite this article:

Shen Wenhou 1,2,Zhao Zhihua 1, et al. Multi-body Dynamic Simulation of the Impact on Cross Deck Pendant[J]. JOURNAL OF VIBRATION AND SHOCK, 2015, 34(5): 73-77.

URL:

http://jvs.sjtu.edu.cn/EN/ OR http://jvs.sjtu.edu.cn/EN/Y2015/V34/I5/73

[1] Billec W. Dynamic Performance of a Mark 7 Mod 1 Arresting System Using 24-inch and 28-inch PD Fairlead Sheaves, AD483454[R]. Washington DC: DTIC, 1966.
[2] Gibson P, Cress H. Analytical Study of Aircraft Arresting Gear Cable Design, AD617788[R]. Washington DC: DTIC, 1965.
[3] Gibson P T, Alexander G H, Cress H A. Validation of Design Theory for Aircraft Arresting-gear Cable, AD665328[R]. Washington DC: DTIC, 1968.
[4] Billec W. The Effect of Deck Span upon Arresting Gear Performance, AD813761[R]. Washington DC: DTIC, 1967.
[5] Kamman J W, Huston R L. Multibody Dynamics Modeling of Variable Length Cable Systems[J]. Multibody System Dynamics, 2001, 5:211-221.
[6] 陈钦. 空间绳网系统设计与动力学研究[D]. 长沙:国防科技大学, 2010.
Chen Qin. Design and Dynamics of an Orbital Net-Capture System[D]. Changsha: National University of Defense Technology, 2010.
[7] Mikhaluk D, Voinov I, Borovkov A. Finite Element Modeling of the Arresting Gear and Simulation of the Aircraft Deck Landing Dynamics[Z]. 7th European LS-DYNA Conference, 2009.
[8] 梁利华, 万晨, 荀盼盼. 飞机拦阻索动态特性研究[J]. 航空学报, 网络出版时间：2012.09.13.
Liang Lihua, Wan Chen, Xun Panpan. Study on the Dynamic Performance of Aircraft Arresting Cable[J]. Acta Aeronautical et Astronautical Sinica, Network Published: 13 September 2012.
[9] Lihua L, Chen W, Panpan X. Dynamic Analysis of Aircraft Arresting Gear Based on Finite Element Method[C]. 2011 International Conference on System Science, Engineering Design and Manufacturing Informatization (ICSEM), 2011, pp. 118–121.
[10] 张新禹. 阻拦索的动力学特性分析及仿真研究[D]. 哈尔滨：哈尔滨工程大学, 2011.
Zhan Xinyu. Dynamic Analysis and Simulation of Arresting Cable[D]. Harbin ： Harbin Engineering University, 2011.
[11] Shabana A A, Yakoub R Y. Three Dimensional Absolute Nodal Coordinate Formulation for Beam Elements: Theory[J]. Journal of Mechanical Design, 2001, 123:606-613.
[12] Von Dombrowski S. Analysis of large flexible body deformation in multibody systems using absolute coordinates[J]. Multibody System Dynamics, 2002, 8:409-432.
[13] Garcíd, a-Vallejo D, Valverde J, et al. An internal damping model for the absolute nodal coordinate formulation[J]. Nonlinear Dynamics, 2005, 42:347-369.
[14] Naval Education And Training Program Development And Technology Center. Aviation boatswain's mate E [M]. United States: Naval Education And Training Program Development And Technology Center, 2001.
[15] 陆明万, 罗学富. 弹性理论基础上册[M]. 北京：清华大学出版社有限公司, 2001.
Lu Mingwan, Luo Xuefu. Foundations of Elasticity, 2nd ed.Ⅰ[M]. Beijing: Tsinghua University Press, 2001.
[16] Johnson K L. Contact mechanics[M]. London: Cambridge university press, 1987.
[17] 郭伟国, 李玉龙, 索涛. 应力波基础简明教程[M]. 西安：西北工业大学出版社, 2007.
Guo Weiguo, Li Yulong, Suo Tao. Concise Course of Stress Waves[M]. Xian: Northwestern Polytechnical University Press, 2007.