Effects of flow path height of impeller exit and diffuser on flow fields in a transonic centrifugal compressor

Isao Tomita, Seiichi Ibaraki, Koji Wakashima, Masato Furukawa, Kazutoyo Yamada, Dai Kanzaki

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

Today turbocharging has become a fundamental technology to realize engine downsizing, which is an attractive strategy for low carbon emissions. High efficiency and wide operating range are strongly required for the automotive turbochargers. Especially centrifugal compressors for automotive turbochargers are requested to operate with high efficiency from the surge limit to the choke limit. The internal flow in a centrifugal compressor is however three dimensional and shows very complex unsteady flow phenomena like a rotating stall and a surging, which have yet to be elucidated fully. In this study the effect of flow path height of impeller and diffuser on flow fields in a transonic centrifugal compressor has been investigated both numerically and experimentally. Detached Eddy Simulation (DES) has been applied and revealed the reduction of impeller exit flow path affects the accumulation of low momentum flow at impeller inlet as well as impeller exit. Also it has been confirmed experimentally the 15% reduction of the impeller exit flow path height can halve the surging flow rate with same choking capacity at pressure ratio of 2.6.

Original languageEnglish
Title of host publicationTurbomachinery
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791856659, 9780791856659
DOIs
Publication statusPublished - Jan 1 2015
EventASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015 - Montreal, Canada
Duration: Jun 15 2015Jun 19 2015

Publication series

NameProceedings of the ASME Turbo Expo
Volume2C

Other

OtherASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015
CountryCanada
CityMontreal
Period6/15/156/19/15

Fingerprint

Centrifugal compressors
Flow fields
Electric inductors
Unsteady flow
Momentum
Flow rate
Engines
Carbon

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Tomita, I., Ibaraki, S., Wakashima, K., Furukawa, M., Yamada, K., & Kanzaki, D. (2015). Effects of flow path height of impeller exit and diffuser on flow fields in a transonic centrifugal compressor. In Turbomachinery (Proceedings of the ASME Turbo Expo; Vol. 2C). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/GT2015-43271

Effects of flow path height of impeller exit and diffuser on flow fields in a transonic centrifugal compressor. / Tomita, Isao; Ibaraki, Seiichi; Wakashima, Koji; Furukawa, Masato; Yamada, Kazutoyo; Kanzaki, Dai.

Turbomachinery. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Turbo Expo; Vol. 2C).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Tomita, I, Ibaraki, S, Wakashima, K, Furukawa, M, Yamada, K & Kanzaki, D 2015, Effects of flow path height of impeller exit and diffuser on flow fields in a transonic centrifugal compressor. in Turbomachinery. Proceedings of the ASME Turbo Expo, vol. 2C, American Society of Mechanical Engineers (ASME), ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015, Montreal, Canada, 6/15/15. https://doi.org/10.1115/GT2015-43271
Tomita I, Ibaraki S, Wakashima K, Furukawa M, Yamada K, Kanzaki D. Effects of flow path height of impeller exit and diffuser on flow fields in a transonic centrifugal compressor. In Turbomachinery. American Society of Mechanical Engineers (ASME). 2015. (Proceedings of the ASME Turbo Expo). https://doi.org/10.1115/GT2015-43271
Tomita, Isao ; Ibaraki, Seiichi ; Wakashima, Koji ; Furukawa, Masato ; Yamada, Kazutoyo ; Kanzaki, Dai. / Effects of flow path height of impeller exit and diffuser on flow fields in a transonic centrifugal compressor. Turbomachinery. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Turbo Expo).
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