Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 589-592 |
| Number of pages | 4 |
| Journal | Proceedings of SPIE - The International Society for Optical Engineering |
| Volume | 5253 |
| DOIs | |
| State | Published - 2003 |
| Event | Fifth International Symposium on Instrumentation and Control Technology - Beijing, China Duration: 24 Oct 2003 → 27 Oct 2003 |
Keywords
- Computer aided test (CAT)
- Intelligent pump
- Virtual Instrument
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