PDF下载 分享
[1]王立君,柳 珊,唐妹芳.一种新型Bang-Bang电磁阀的研制[J].火箭推进,2019,45(01):48-52.
　WANG Lijun,LIU Shan,TANG Meifang.Development of a new Bang-Bang solenoid valve[J].Journal of Rocket Propulsion,2019,45(01):48-52.
点击复制

一种新型Bang-Bang电磁阀的研制

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 45 期数: 2019年01期 页码: 48-52 栏目: 研究与设计 出版日期: 2019-02-28
Title:
Development of a new Bang-Bang solenoid valve
文章编号:
1672-9374(2019)01-0048-05
作者:
王立君1; 2; 柳 珊1; 2;  唐妹芳1; 2
(1.上海空间推进研究所,上海201112; 2.上海空间发动机工程技术研究中心,上海201112)
Author(s):
WANG Lijun1; 2;  LIU Shan1; 2;  TANG Meifang1; 2
(1.Shanghai Institute of Space Propulsion, Shanghai 201112, China; 2.Shanghai Engineering Research Center of Space Engine, Shanghai 201112, China)
关键词:
Bang-Bang电磁阀;  漏率;  长寿命
Keywords:
Bang-Bang solenoid valve;  leak rate;  long-life
分类号:
V432
文献标志码:
A
摘要:
针对系统提出的轻质长寿命、氙气工作介质的要求,特别设计了一种新型Bang-Bang电磁阀。该电磁阀采用“弹簧+单簧片”的设计方案,通过对5.70～6.72 MPa密封比压、0.12～0.14 mm配合间隙、0.20 mm行程等参数的合理选取,阀门顺利地通过了振动试验、最大量级1 600 g的冲击试验、20 g加速度试验、(10～75)℃热真空试验和(-10～+75)℃热循环等环境试验的考核以及100万次的寿命试验验证,试验前后阀门漏率及响应时间等参数稳定,满足了系统要求。
Abstract:
According to the long-life,light-weight and xenon working medium requirements proposed by the system, a new type of Bang-Bang solenoid valve was specially designed. By adopting the design scheme of “Spring and S-spring” and selecting the proper parameters of sealing pressure(5.70～6.72 MPa), matching gap(0.12～0.14mm), spool stroke(0.20mm)and others, the Bang-Bang solenoid valve has successfully passed the assessment of environmental tests such as vibration, shock(the maximum magnitude 1 600 g), acceleration(20 g), thermal vacuum(10～75℃)and thermal cycle(-10～+75℃)as well as a million times of life test verification. The parameters such as leak rate and response time of the valve were stable before and after the experiment, which greatly met the system requirements.

参考文献/References:

[1] SALIM A A.In-orbit performance of Lockheed Martin's electrical power subsystem for A2100 communication satellites: AIAA 2000-2809[R].Reston: AIAA,2000.
[2] 王辉,彭维峰,魏鑫, 等.XX-3B卫星平台电推进分系统及地面验证[C]//第十一届中国电推进技术学术研讨会文集.北京: 中国宇航学会,2015.
[3] 康小录,杭观容.霍尔电推进技术的发展与应用[J].火箭推进,2017,43(1):8-17.
KANG X L, HANG G R.Development and application of Hall electric propulsion technology[J].Journal of Rocket Propulsion,2017,43(1):8-17.
[4] 刘国球.液体火箭发动机原理[M].北京:宇航出版社,1993.
[5] 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.
[6] 朱宁昌.液体火箭发动机设计(下)[M].北京:宇航出版社,2005.
[7] 黄爱清,曹明,唐妹芳,等.一种无摩擦簧片式电磁阀的研制[J].火箭推进,2015,41(6):41-45.
HUANGA Q, CAO M, TANG M F, et al.Development of non-friction S-spring valve[J].Journal of Rocket Propulsion, 2015,41(6):41-45.
[8] 许闯,王强.悬空衔铁式电磁阀中S形簧片的研制[J].火箭推进,2017(5):58-62.
XU C, WANG Q.Development of S-shape spring insuspended armature solenoid valve[J].Journal of Rocket Propulsion,2017(5):58-62.
[9] 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.
[10] 王扬彬,徐兵.基于Ansoft及AMESim的电磁铁动态特性仿真分析[J].机床与液压,2008,36(9):104-108.
[11] 廖湘恩.航天电器[M].北京:国防工业出版社,1981.

备注/Memo

收稿日期:2017-12-25
基金项目:国家航天支撑技术项目(617010409)
作者简介:王立君(1987—),女,工程师,研究领域为阀门设计

更新日期/Last Update: 2019-02-20