The intelligent pump test system based on virtual instrument

被引：1
|
作者：
Ma, JG [1 ]
Wang, SF [1 ]
Wang, ZL [1 ]
机构：
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100083, Peoples R China
来源：
FIFTH INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION AND CONTROL TECHNOLOGY | 2003年 / 5253卷
关键词：
virtual instrument; intelligent pump; computer aided test (CAT);
D O I：
10.1117/12.521992
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The intelligent pump system is the key component of the aircraft hydraulic system that can solve the problem, such as the temperature sharply increasing. As the performance of the intelligent pump directly determines that of the aircraft hydraulic system and seriously affects fly security and reliability. So it is important to test all kinds of performance parameters of intelligent pump during design and development, while the advanced, reliable and complete test equipments are the necessary instruments for achieving the goal. In this paper, the application of virtual instrument and computer network technology in aircraft intelligent pump test is presented. The composition of the hardware, software, hydraulic circuit in this system are designed and implemented.
引用
收藏
页码：589 / 592
页数：4
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