Abstract
A system for measurement and control of some compressor experiments in a test cell is described. An economical scheme, which is effective for the steady data acquisition for turbomachinery, was demonstrated. By dint of the analysis of sources and influencing modes from the dynamic interferential signals, a method that can estimate the jam source is developed, and accordingly the remedies are taken. All this work provides the basis for the further experiments.
| Original language | English |
|---|---|
| Pages (from-to) | 402-407 |
| Number of pages | 6 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 19 |
| Issue number | 3 |
| State | Published - Jun 2004 |
Keywords
- Aerospace propulsion system
- Antijamming technology
- Compressor
- Data acquisition
- Grounding
- Shield
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