航天继电器多余物微粒碰撞噪声检测的冲击试验条件

Abstract
Figure/Table
References
Related Citation (15)

Download: PDF (397 KB) HTML (1 KB)
Export: BibTeX | EndNote (RIS)

Abstract Particle impact noise detection (PIND) is the standard for detecting remainders in aerospace relay and it is also an obligatory screening test after manufacture of the relays. Impact is an important process in particle impact noise detection. To identify the key factors of the peak acceleration and pulse duration of the impact. Investigate the activate effects of impact conditions for reminder particles, increase the success rate of testing. This paper establishes the mathematical model of impact, and then researches the influence of system parameters on the impact acceleration. The relationship between minimum impact acceleration and characteristic parameters of the reminder particles is investigated based on electricity image force theory; an equivalent impact condition table is given in this paper based on “the damage equivalent principle”; and corresponding experiments are carried on. The experimental results show that to choose different impact conditions can activate different size of reminder particles effectively.

Key words： Aerospace relay reminders particle impact noise detection impact

Received: 20 February 2010 Published: 07 March 2014

PACS:

TM581.3

	Service

	E-mail this article
	Add to my bookshelf
	Add to citation manager
	E-mail Alert
	RSS
	Articles by authors
	Wang Shujuan
	Wang Guotao
	Zhai Guofu
	Zhang Hui

Cite this article:

Wang Shujuan,Wang Guotao,Zhai Guofu等. Impact Test Condition of Particle Impact Noise Detection for Space Relay Remainders[J]. Transactions of China Electrotechnical Society, 2011, 26(1): 75-80.

URL:

http://dgjsxb.ces-transaction.com/EN/ OR http://dgjsxb.ces-transaction.com/EN/Y2011/V26/I1/75

[1] Ding Maosheng, Wang Gang, Li Xiaohua. Reliability analysis of digital relay[C]. 8th IEE International Conference on Developments in Power System Protection, The Netherlands, 2004, 1: 268-271.
[2] Roettjer P. Testing techniques to improve relay reliability[J]. EE: Evaluation Engineering, 2005, 44(4): 44-48.
[3] Ishikawa K, Miki T, Mamiya H, et al. Early-stage analysis for MEMS structural optimization II: its application to microrelay reliability[C]. Proceedings of the ASME/Pacific Rim Technical Conference and Exhibition on Integration and Packaging of MEMS, NEMS, and Electronic Systems: Advances in Electronic Packaging, 2005, Part C: 1631-1636.
[4] 郑南昌. 控制系统继电器可靠性分析与措施[J]. 火箭推进, 2005, 31(4): 58-62.
Zheng Nanchang. Reliability analysis and countermeasures of relays in the control system[J]. Journal of Rocket Propulsion, 2005, 31(4): 58-62.
[5] 李大南. 航天型号产品多余物及其预防和控制标准的实施检查[J]. 航天标准化, 2006(1): 17-20.
Li Danan. The implementation inspects of space product superabundance and its prevent and standards[J]. Astronautics standardization 2006(1): 17-20.
[6] Hammerstrom I, Kuhn M, Wittneben A. Channel adaptive scheduling for cooperative relay networks[C]. 2004 IEEE 60th Vehicular Technology Conference, 2004, 60(4): 2784-2788.
[7] GJB 65B-1999. 有可靠性指标的电磁继电器总规范[S].
[8] GJB 2888-1997. 有可靠性指标的功率型电磁继电器总规范[S].
[9] MIL-STD-883E 2020.7, Particle Impact Noise Detection Test[S].
[10] Zhang H, Wang S J, Zhai G F. Dynamic model of particle impact noise detection[C]. IEEE IECON, 2004: 2577-2581.
[11] Zhang H, Wang S J, Zhai G F. Test conditions discussion of particle impact noise detection for space relay[C]. IEEE IECON, 2004: 2566-2572.
[12] 张辉, 王淑娟, 翟国富. 航天继电器多余物微粒碰撞噪声检测的单周期稳定性分析[J]. 航空学报, 2005, 26(3): 362-366.
Zhang H, Wang S J, Zhai G F. One-period stability analysis of particle impact noise detection for space relay reminders[J]. Acta Aeronautica ET Astronautica Sinica, 2005, 26(3) : 362-366.
[13] 鲍重光. 静电技术原理[M]. 北京: 北京理工大学出版社, 1993.
[14] 汪凤泉. 电子设备振动与冲击手册[M]. 北京:科学出版社, 1998.