航天推进技术研究院主办
[1]陈维宇,程亚威,李小明,等.高压小流量稳流型调节器特性研究[J].火箭推进,2011,37(04):40-44.
CHEN Wei-yu,CHENG Ya-wei,LI Xiao-ming,et al.Characteristics of low-output flow-stabilized regulator under high working pressure[J].Journal of Rocket Propulsion,2011,37(04):40-44.
点击复制
CHEN Wei-yu,CHENG Ya-wei,LI Xiao-ming,et al.Characteristics of low-output flow-stabilized regulator under high working pressure[J].Journal of Rocket Propulsion,2011,37(04):40-44.
高压小流量稳流型调节器特性研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
37
期数:
2011年04期
页码:
40-44
栏目:
研究与设计
出版日期:
2011-08-15
- Title:
- Characteristics of low-output flow-stabilized regulator under high working pressure
- 文章编号:
- 1672-9374(2011)04-0040-05
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 介绍了一种小流量稳流型流量调节器，阐述了该调节器的结构及组成、工作原理。对调节器性能进行了仿真计算，分析了其影响因素。介绍了相关试验及试验结果。试验结果表明：该产品有很好的静特性和加载特性。
- Abstract:
- A low-output flow-stabilized regulator is introduced in this paper. The structure, composition and working principle of the regulator are elaborated. The simulation calculation of the regulator performance is conducted. The influence factors on the regulator performance are analyzed. The relevant testing results are given. The results show that the calculated results are in good agreement with the measured parameters and the static characteristics of the regulator meets the requirement.
参考文献/References:
[1]张贵田. 高压补燃液氧煤油发动机[M]. 北京: 国防工业出版社, 2005.
[2][俄] 格列克曼Б Ф. 液体火箭发动机自动调节[M]. 北京: 宇航出版社, 1995.
[3]液体火箭发动机设计[下] [J]. 北京: 宇航出版社, 1994.
[4]陈维宇, 刘站国, 王昕, 等. 流量调节器研制中的主要问题及结构改进 [J]. 火箭推进, 2009, 35(3): 45-50.
[5][美] 休泽尔D K. 液体火箭发动机现代工程设计[M]. 朱宁昌, 译. 北京: 宇航出版社, 1993.
[6]ШЕВЯКОВ А А, КАЛНИН В М. Теория автоматиче-
相似文献/References:
[1]刘 上,刘红军,陈建华,等.流量调节器在泵压式供应系统中的动力学特性[J].火箭推进,2014,40(02):28.
LIU Shang LIU Hong-jun CHEN Jian-hua CHENG Ya-wei.Dynamical characteristics of flow regulator in pump feed system[J].Journal of Rocket Propulsion,2014,40(04):28.
[2]陈维宇,刘站国,王 昕,等.流量调节器研制中的主要问题及结构改进[J].火箭推进,2009,35(06):31.
[3]王昕,王福民.流量调节器研制的全过程质量控制[J].火箭推进,2007,33(02):48.
Wang Xin,Wang Fumin.Overall quality control of the flow regulator development process[J].Journal of Rocket Propulsion,2007,33(04):48.
[4]王昕.流量调节器动态特性研究[J].火箭推进,2004,(03):19.
[5]黄智勇,李惠敏,胡钟兵,等.液体火箭发动机超高转速泵浮动密封环研究[J].火箭推进,2004,(04):10.
Huang Zhiyong,Li Huimin,Hu Zhongbing.Study on Floating Seal Ring of Hyper-rotate-speed Pump in Liquid Rocket Engine[J].Journal of Rocket Propulsion,2004,(04):10.
[6]许志宇,李小明.过载对流量调节器静态特性的影响研究[J].火箭推进,2016,42(03):63.
XU Zhiyu,LI Xiaoming.Effects of overload on static characteristics of liquid-flow regulator[J].Journal of Rocket Propulsion,2016,42(04):63.
[7]刘小杰,杜永清.基于LabVIEW的调节器低温动性能试验台测量系统设计[J].火箭推进,2016,42(05):110.[doi:10.3969/j.issn.1672-9374.2016.05.019]
LIU Xiaojie,DU Yongqing.Design of LabVIEW-based measuring system for cryogenic dynamic performance test bench for regulator[J].Journal of Rocket Propulsion,2016,42(04):110.[doi:10.3969/j.issn.1672-9374.2016.05.019]
备注/Memo
收稿日期：2011-01-13；修回日期：2011-01-27
基金项目：国家航天高技术项目
作者简介：陈维宇（1967—），男，高级工程师，研究领域为液体火箭发动机自动器
更新日期/Last Update:
1900-01-01