Abstract
In order to establish the design methodolog of ultra micro centrifugal compressor, which is the most important component of ultra micro gas turbine unit, a 10 times of the final target size model was designed, prototyped and tested. The problems to be solved for downsizing were examined and 2-dimensional impeller was chosen as the first model due to its productivity. The conventional ID prediction method, CFD and the inverse design were attempted. The prototyped compressor was driven by using a turbocharger and the performance characteristics were measured.
| Original language | English |
|---|---|
| Pages (from-to) | 33-37 |
| Number of pages | 5 |
| Journal | Journal of Thermal Science |
| Volume | 12 |
| Issue number | 1 |
| DOIs | |
| Publication status | Published - 2003 Jan 1 |
Keywords
- 2-dimensional impeller
- Centrifugal compressor
- Performance characteristics
ASJC Scopus subject areas
- Condensed Matter Physics
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Cite this
Mizuki, S., Yamaguchi, N., Minorikawa, G., Asaga, Y., Hirano, T., Ohta, Y., & Outa, E. (2003). Design and prototyping of micro centrifugal compressor. Journal of Thermal Science, 12(1), 33-37. https://doi.org/10.1007/s11630-003-0006-z