Control of Surge in Centrifugal Compressor by Using a Nozzle Injection System: Universality in Optimal Position of Injection Nozzle
The passive control method for surge and rotating stall in centrifugal compressors by using a nozzle injection system was proposed to extend the stable operating range to the low flow rate. A part of the flow at the scroll outlet of a compressor was recirculated to an injection nozzle installed on t...
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2012-01-01
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Series: | International Journal of Rotating Machinery |
Online Access: | http://dx.doi.org/10.1155/2012/259293 |
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doaj-c666c779c0174abda001b6c0d86275792020-11-24T22:36:09ZengHindawi LimitedInternational Journal of Rotating Machinery1023-621X1542-30342012-01-01201210.1155/2012/259293259293Control of Surge in Centrifugal Compressor by Using a Nozzle Injection System: Universality in Optimal Position of Injection NozzleToshiyuki Hirano0Takanori Uchida1Hoshio Tsujita2Production Systems Engineering Course, Tokyo Metropolitan College of Industrial Technology, 1-10-40 Higashiohi, Shinagawa-ku, Tokyo 140-0011, JapanGraduate School of Engineering, Hosei University, 3-7-2 Kajinocho, Koganei-shi, Tokyo 184-8584, JapanDepartment of Mechanical Engineering, Faculty of Science and Engineering, Hosei University, Tokyo, JapanThe passive control method for surge and rotating stall in centrifugal compressors by using a nozzle injection system was proposed to extend the stable operating range to the low flow rate. A part of the flow at the scroll outlet of a compressor was recirculated to an injection nozzle installed on the inner wall of the suction pipe of the compressor through the bypass pipe and injected to the impeller inlet. Two types of compressors were tested at the rotational speeds of 50,000 rpm and 60,000 rpm with the parameter of the circumferential position of the injection nozzle. The present experimental results revealed that the optimum circumferential position, which most effectively reduced the flow rate for the surge inception, existed at the opposite side of the tongue of the scroll against the rotational axis and did not depend on the compressor system and the rotational speeds.http://dx.doi.org/10.1155/2012/259293 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Toshiyuki Hirano Takanori Uchida Hoshio Tsujita |
spellingShingle |
Toshiyuki Hirano Takanori Uchida Hoshio Tsujita Control of Surge in Centrifugal Compressor by Using a Nozzle Injection System: Universality in Optimal Position of Injection Nozzle International Journal of Rotating Machinery |
author_facet |
Toshiyuki Hirano Takanori Uchida Hoshio Tsujita |
author_sort |
Toshiyuki Hirano |
title |
Control of Surge in Centrifugal Compressor by Using a Nozzle Injection System: Universality in Optimal Position of Injection Nozzle |
title_short |
Control of Surge in Centrifugal Compressor by Using a Nozzle Injection System: Universality in Optimal Position of Injection Nozzle |
title_full |
Control of Surge in Centrifugal Compressor by Using a Nozzle Injection System: Universality in Optimal Position of Injection Nozzle |
title_fullStr |
Control of Surge in Centrifugal Compressor by Using a Nozzle Injection System: Universality in Optimal Position of Injection Nozzle |
title_full_unstemmed |
Control of Surge in Centrifugal Compressor by Using a Nozzle Injection System: Universality in Optimal Position of Injection Nozzle |
title_sort |
control of surge in centrifugal compressor by using a nozzle injection system: universality in optimal position of injection nozzle |
publisher |
Hindawi Limited |
series |
International Journal of Rotating Machinery |
issn |
1023-621X 1542-3034 |
publishDate |
2012-01-01 |
description |
The passive control method for surge and rotating stall in centrifugal compressors by using a nozzle injection system was proposed to extend the stable operating range to the low flow rate. A part of the flow at the scroll outlet of a compressor was recirculated to an injection nozzle installed on the inner wall of the suction pipe of the compressor through the bypass pipe and injected to the impeller inlet. Two types of compressors were tested at the rotational speeds of 50,000 rpm and 60,000 rpm with the parameter of the circumferential position of the injection nozzle. The present experimental results revealed that the optimum circumferential position, which most effectively reduced the flow rate for the surge inception, existed at the opposite side of the tongue of the scroll against the rotational axis and did not depend on the compressor system and the rotational speeds. |
url |
http://dx.doi.org/10.1155/2012/259293 |
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