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Abstract
In order to establish the design methodology of ultra micro centrifugal compressor, which is the most important component of ultra micro gas turbine unit, a 10 times of the final target model size 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 1-dimensional prediction method was used for the impeller design. The prototyped compressor was driven by using a turbocharger and the performance characteristics were measured and compared with the prediction. The stress and the vibration analysis in the operating condition were also performed.
Journal
- 年次大会講演論文集 : JSME annual meeting [List of Volumes]
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年次大会講演論文集 : JSME annual meeting 2003(6), 323-324, 2003-08-05 [Table of Contents]
The Japan Society of Mechanical Engineers