|Table of Contents|

Development of non-friction S-spring valve(PDF)

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

Issue:
2015年06期
Page:
41-45
Research Field:
研究与设计
Publishing date:

Info

Title:
Development of non-friction S-spring valve
Author(s):
HUANG Aiqing CAO Ming TANG Meifang YOU Gang
Shanghai Institute of Space Propulsion, Shanghai 201112, China
Keywords:
non-friction S-spring solenoid valve solenoid valve design aerospace
PACS:
V434-34
DOI:
-
Abstract:
With the increasing of spacecraft working life, the design of traditional solenoid valves can not meet the requirement of space propulsion system. The design scheme of a long-life, high-credibility, non-friction S-spring valve is introduced in this paper. An S-spring suspended armature style component is adopted in the solenoid to eliminate the redundancy residual caused by sliding friction in the valve. At present, this design scheme has passed mechanics and thermal environment test, and endured a million times of working life cycle. It has entered into engineering application phase.

References:

[1]SCHULTE G. High performance 400N MMH/NTO bipropellant engine for apogee boost maneuvers, AIAA 99- 2466[R]. USA: AIAA, 1999.
[2]HUFTALEN R L. Next generation propellant isolation valve eesign and eevelopment, AIAA 2006-4879[R]. USA: AIAA, 2006.
[3]TAIICHI N. The development of a Japanese 20 N thruster valve for a spacecraft propulsion system, AIAA 2006- 4876[R]. USA: AIAA, 2006.
[4]赵元修, 吴守生. 液体推进剂火箭发动机设计[M]. 北京:宇航出版社, 1973.

[5]寥湘恩. 航空电器[M]. 北京: 国防工业出版社, 1981.

[6]范钦珊. 压力容器的应力分析与强度设计[M]. 北京: 原子能出版社, 1999.
[7]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.
[8]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.

Memo

Memo:
-
Last Update: 1900-01-01