航天推进技术研究院主办
[1]王乃世,罗 军,张俊锋.水击压力校准系统快关阀的研发与应用[J].火箭推进,2018,44(04):36-39.
WANG Naishi,LUO Jun,ZHANG Junfeng.Development and application of quick-closing valve for water hammer pressure calibration system[J].Journal of Rocket Propulsion,2018,44(04):36-39.
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WANG Naishi,LUO Jun,ZHANG Junfeng.Development and application of quick-closing valve for water hammer pressure calibration system[J].Journal of Rocket Propulsion,2018,44(04):36-39.
水击压力校准系统快关阀的研发与应用
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
44
期数:
2018年04期
页码:
36-39
栏目:
研究与设计
出版日期:
2018-08-31
- Title:
- Development and application of quick-closing valve for water hammer pressure calibration system
- 文章编号:
- 1672-9374(2018)04-0036-04
- 分类号:
- V434+.3-34
- 文献标志码:
- A
- 摘要:
- 为实现水击压力传感器现场动态校准,模拟液体水击压力产生的状态,研制了一套用于水击压力传感器现场校准的快关阀,并对阀关键部件脆性片材料进行重点选择和验证试验。测试结果证明:快关阀关闭时间满足设计要求,实用效果良好,可用于瞬态水击压力现场动态校准。
- Abstract:
- In order to realize the field dynamic calibration of water hammer pressure sensor and simulate the state of liquid water hammer pressure, a set of quick-closing valve used in the field calibration of water hammer pressure sensor was developed, and the material of brittle sheet as a key valve part was selected and verified. The test results show that the close time of quick-closing valve meets the design requirements, and the practical effect is good, which can provide an important basis for the dynamic calibration of dynamic water hammer pressure.
参考文献/References:
[1] 杨源泉.阀设计手册[M].北京:机械工业出版社,1992.
[2] 张力,俞锦,刘晶.用于高压动态校准的快开阀装置[J].航空计测技术,1996(5):7-9.
[3] 朱宁昌,董锡鉴,王新龄,等.液体火箭发动机设计[M].北京:中国宇航出版社,1993.
[4] 朱明武.动压测量[M].北京:国防工业出版社,1983.
[5] 陆培文,高凤琴.阀设计计算手册[M].北京:中国标准出版社,2009.
[6] 苏志东,尹玉杰,张清双.阀制造工艺[M].沈阳:化学工业出版社,2010.
[7] 陆培文.实用阀设计手册[M]. 3版. 北京:机械工业出版社,2012.
[8] 徐灏.机械设计手册[M].北京:机械工业出版社,2002.
[9] 史秋明,沈琦琳,王磊,等.主结构为回转体零件双车削中心制造单元研究[J].火箭推进,2016,42(4):73-79.
SHI Qiuming,SHEN Qilin,WANG Lei,et al.Research on double turning center manufacturing cell for parts with rotational main structure[J].Journal of rocket propulsion,2016,42(4):73-79.
[10] 成大先.机械设计手册[M].北京:化学工业出版社,2007.
备注/Memo
收稿日期:2017-06-07
作者简介: 王乃世(1984—),男,工程师,研究领域为液体火箭发动机试验技术
更新日期/Last Update:
1900-01-01