|Table of Contents|

STM32-based control system for foreign object debris in pipelines of liquid rocket engine(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2015年06期
Page:
86-91
Research Field:
测控与试验
Publishing date:

Info

Title:
STM32-based control system for foreign object debris in pipelines of liquid rocket engine
Author(s):
CAO Chun ZHANG Wei LI Zhigang GUAN Li
Beijing Institute of Aerospace Testing Technology, Beijing 100074, China
Keywords:
pipeline of liquid rocket engineSTM32 micro-controllerforeign object debris controlultrasonic cleaning
PACS:
V432-34
DOI:
-
Abstract:
The control of foreign object debris is an essential part in the design and testing of aerospace products. However, since efficiency and accuracy of current foreign object debris detecting methods are low, a STM32-based system for detecting and cleaning the foreign object debris in pipelines of liquid rocket engine was designed. It is composed of ultrasonic pipe cleaning device, foreign object debris detecting device, signal acquisition device and industrial computer. With the control function of STM32, the system can realize automatic detection and cleaning of the foreign object debris in pipeline of liquid rocket engine, real-time acquisition, transmission, display and storage of liquid level information and cleaning effect. In addition, re-cleaning procedure can be started according to the detection result. The system can be switched between automatic cleaning and manual cleaning, which can

References:

[1]袁牧. 多余物的过程控制[J]. 质量与可靠性. 2013, 16(7): 37-38.
[2]KANG P J, TAE K J, CHUL S M. High performance single chip implementation for a digital protective relay using FPGA[C]// Proceedings of the International Con- ference on VLSI. [S.l.].: [s.n.], 2004, 6: 504-508.
[3]王育红, 郑世才. 活动多余物的检测[J]. 宇航计测技术,1996, 16(3): 55-58.
[4]QJ2865-1996 航天产品多余物预防和控制[S].

[5]王淑娟, 张辉, 王世成. 航天继电器检测技术探讨[J]. 低压电器, 2004 (1): 6-9.

[6]PRAINE R R, ZIMMER W J. Statistical modeling for particle impact noise detection testing[C]// Proceedings of Annual Reliability and Maintainability symposium, 1991, 8: 536-540.
[7]张辉, 王淑娟, 王立忠, 等. 航天继电器多余物检测方法的综合分析与讨论[J]. 机电元件, 2003, 23(2): 53-60.
[8]Anon. STM32 32-bit ARM cortex MCUs [EB/OL]. (2013- 02-20)[2013-11-18]. http://www.st.com/web/en/catalog/ mmc/FM141/SC1169.
[9]POLASTRE J, SZEWCZYK R, MAINWARING A, et al. Analysis of wireless sensor networks for habitat monitoring[J]. Wireless Sensor Networks, 2004 (3): 399- 423.
[10]丁瑞荣. 产品多余物控制[J]. 航空精密制造技术, 1993(2): 43-44.
[11]郑世才. 航天产品活动多余物的检测[J]. 上海航天, 1997 (5): 56-60.
[12] 单黎波, 王建昌, 内窥镜检测方法技术研究[J]. 火箭推进, 2006, 32(4): 54-62. SHAN Libo, WANG Jianchang, Study on endoscope check method[J]. Journal of Rocket Propulsion, 2006, 32(4): 54-62.
[13] 窦双庆, 变推力发动机高模试验真空压力测量技术研究[J]. 火箭推进, 2013, 38(3): 99-104. DOU Shuang-qing, Research on measurement technology of vacuum pressure in altitude simulation test of rocket engine with variable thrust, Journal of Rocket Propulsion, 2013, 38(3): 99-104.

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