PDF下载 分享
[1]赵春云,张石燕,焦金成.电磁气动阀四机集成设计[J].火箭推进,2014,40(03):52-56.
　ZHAO Chun-yun,ZHANG Shi-yan,JIAO Jin-cheng.Integrated design of four pneumatic solenoid valves for four engines[J].Journal of Rocket Propulsion,2014,40(03):52-56.
点击复制

电磁气动阀四机集成设计

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 40 期数: 2014年03期 页码: 52-56 栏目: 研究与设计 出版日期: 2014-06-27
Title:
Integrated design of four pneumatic solenoid valves for four engines
作者:
赵春云; 张石燕; 焦金成
上海空间推进研究所，上海 201112
Author(s):
ZHAO Chun-yun;  ZHANG Shi-yan;  JIAO Jin-cheng
Shanghai Institute of Space Propulsion, Shanghai 201112, China
关键词:
电磁气动控制阀; 集成设计; 仿真分析; 应用
Keywords:
pneumatic solenoid valve;  integrated design;  simulation analysis;  application
分类号:
V432-34
文献标志码:
A
摘要:
针对某空间飞行器对轨控发动机控制阀体积及重量的要求，统筹考虑气液路供应、4台发动机、氧化剂及燃料贮箱的安装要求，设计了新颖的电磁气动阀四机集成结构。经仿真分析及试验实测，结果表明：电磁气动阀四机集成结构具有设计巧妙、性能优良的特点。
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.

参考文献/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.

相似文献/References:

[1]张晨曦,马晓丹.火箭发动机涡轮泵集成设计系统[J].火箭推进,2015,41(04):79.
　ZHANG Chenxi,MA Xiaodan.Integration design system for turbo pump in rocket engine[J].Journal of Rocket Propulsion,2015,41(03):79.

备注/Memo

收稿日期：2014-02-12；修回日期：2014-03-11 作者简介：赵春云（1969—），女，高级工程师，研究领域为空间推进系统阀门设计

更新日期/Last Update: 1900-01-01