|Table of Contents|

Integrated design of four pneumatic solenoid valves for four engines(PDF)

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

Issue:
2014年03期
Page:
52-56
Research Field:
研究与设计
Publishing date:

Info

Title:
Integrated design of four pneumatic solenoid valves for four engines
Author(s):
ZHAO Chun-yun ZHANG Shi-yan JIAO Jin-cheng
Shanghai Institute of Space Propulsion, Shanghai 201112, China
Keywords:
pneumatic solenoid valve integrated design simulation analysis application
PACS:
V432-34
DOI:
-
Abstract:
Considering the harsh terms such as limited volume and less weight for the space aircraft engine control valves, it is necessary to guarantee the installation requirements of the gas/liquid supply line, four engines and oxidant/fuel tanks, so a novel integrated structure design of the four pneumatic solenoid valves came into being. The results of simulation analyses and test show that integration structure of four pneumatic solenoid valves possesses the characteristics of clever design and excellent performance.

References:

[1]BUSHWAY E D, NELSON E. Design and development of ligh tweight integated valve/injectors for the THAAD program, AIAA 94-3383[R]. USA: AIAA, 1994.
[2]MORASH D H, BARBARITS J K, LANGEL G. Prope- llant valve assembly for the upper stage of the Ariane 5 launch vehicle, AIAA 95-3095[R]. USA: AIAA, 1995.
[3]MATSUOKA K. Study on valve systems for pulse detonation engines, AIAA 2010-6672[R]. USA: AIAA, 2010.
[4]King P T. Magnetically-actuated manually-operated isola- tion valve: US, US2006/0124880 A1[P/OL]. 2004-12-14[2006-06-15]. http://www.google.com/patents/US200601 24880.
[5]廖湘恩. 航空电器[M]. 北京: 国防工业出版社, 1981.
[6]赵博. Ansoft12在工程电磁场中的应用[M]. 北京: 中国水利水电出版社, 2010.
[7]刘国强. Ansoft工程电磁场有限元分析[M]. 北京: 电子工业出版社, 2005.
[8]曹泰岳. 火箭发动机动力学[M]. 长沙: 国防科技大学出版社, 1999.
[9]朱宁昌. 液体火箭发动机设计(下)[M]. 北京: 宇航出版社, 1994.
[10]柳长安, 张蒙正. 弹道变轨对冲压动力反舰导弹的影响[J]. 火箭推进, 2012, 38(2): 20-26.
[11]丁凡, 姚健娣, 笪靖, 等. 高速开关阀的研究现状[J]. 中国工程机械学报, 2011, 9(3): 0351-0358.

Memo

Memo:
-
Last Update: 1900-01-01