The intelligent pump test system based on virtual instrument

  • Jungong Ma*
  • , Shifu Wang
  • , Zhanlin Wang
  • *Corresponding author for this work

Research output: Contribution to journalConference articlepeer-review

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 languageEnglish
Pages (from-to)589-592
Number of pages4
JournalProceedings of SPIE - The International Society for Optical Engineering
Volume5253
DOIs
StatePublished - 2003
EventFifth International Symposium on Instrumentation and Control Technology - Beijing, China
Duration: 24 Oct 200327 Oct 2003

Keywords

  • Computer aided test (CAT)
  • Intelligent pump
  • Virtual Instrument

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