航天推进技术研究院主办
[1]李正兵,吴锦凤,宋秋凤,等.液体火箭发动机试验测量系统状态检测程序设计[J].火箭推进,2007,33(05):59-62.
Li Zhengbing,Wu Jinfeng,Song Qiufeng.Design of the state detection program of the measurement system for liquid rocket engine test[J].Journal of Rocket Propulsion,2007,33(05):59-62.
点击复制
Li Zhengbing,Wu Jinfeng,Song Qiufeng.Design of the state detection program of the measurement system for liquid rocket engine test[J].Journal of Rocket Propulsion,2007,33(05):59-62.
液体火箭发动机试验测量系统状态检测程序设计
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
33
期数:
2007年05期
页码:
59-62
栏目:
测控与试验
出版日期:
2007-10-30
- Title:
- Design of the state detection program of the measurement system for liquid rocket engine test
- 分类号:
- V434.1
- 文献标志码:
- A
- 摘要:
- 发动机试车准备过程中,测量系统的状态变化直接影响到发动机参数测量的准确度。为正确获得测量系统的状态变化,从测量系统的硬件组成出发,针对压力、温度等参数类型,提出了测量通道状态变化的检测判断方法。在Windows操作系统下,采用VB6.0语言,设计了相应的状态变化检测程序。试验证明:测量系统状态检测程序运行可靠,操作方便,提高了试车工作效率。
相似文献/References:
[1]沈传兵,白文浩,崔 海,等.动力系统试验工艺参数监视系统设计[J].火箭推进,2014,40(04):73.
LI Shan-feng,TANG Wei.Analysis and solution for interference with measurement
system in cycle precooling test[J].Journal of Rocket Propulsion,2014,40(05):73.
[2]李山峰,汤 伟.循环预冷试验中测量系统干扰问题分析与措施[J].火箭推进,2014,40(04):77.
LI Shan-feng,TANG Wei.Analysis and solution for interference with measurement system in cycle precooling test[J].Journal of Rocket Propulsion,2014,40(05):77.
[3]蒋兴加,李正兵,陈刚,等.液氧/煤油发动机试车测量系统的抗干扰技术[J].火箭推进,2005,31(03):54.
Jiang Xingjia,Li ZhengbingChen Gang.Anti-interference technique of measuring system in the LOX/kerosene engine test[J].Journal of Rocket Propulsion,2005,31(05):54.
[4]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(05):110.[doi:10.3969/j.issn.1672-9374.2016.05.019]
更新日期/Last Update:
1900-01-01