Effect of Injection Nozzle Shape on Performance Characteristics of a Centrifugal Compressor
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- MIYA Masaaki
- 法政大学 大学院 工学研究科
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- HIRANO Toshiyuki
- 東京都立産業技術高等専門学校 ものづくり工学科
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- TSUJITA Hoshio
- 法政大学 理工学部 機械工学科
Bibliographic Information
- Other Title
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- 吹込みノズル形状が遠心圧縮機の性能へ及ぼす影響
- フキコミ ノズル ケイジョウ ガ エンシン アッシュクキ ノ セイノウ エ オヨボス エイキョウ
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Abstract
In the operation of a centrifugal compressor of turbocharger, instability phenomena such as rotating stall and surge are observed at lower flow rate than that at the designed point. Therefore, it is important to control the onset of instability phenomena to extend the stable operation range of centrifugal compressor to the low flow rate region. In the present study, the control of rotating stall and surge for a centrifugal compressor was tried by using a nozzle injection system in which a part of the flow from the delivery duct was re-circulated to the impeller inlet. The three types of air injection nozzle were used to investigate the effect of nozzle inner diameter on the performance characteristics. In addition, the circumferential position of the injection nozzle was changed in order to examine the relationship between the optimum position and the nozzle inner diameter.
Journal
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- Turbomachinery
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Turbomachinery 41 (2), 72-77, 2013
Turbomachinery Society of Japan
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Details 詳細情報について
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- CRID
- 1390282679521165696
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- NII Article ID
- 130005067929
- 10031140207
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- NII Book ID
- AN00004836
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- ISSN
- 18802338
- 03858839
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- NDL BIB ID
- 024245376
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- CiNii Articles
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- Abstract License Flag
- Disallowed