The effect of tip leakage vortex for operating range enhancement of centrifugal compressor

Isao Tomita, Seiichi Ibaraki, Masato Furukawa, Kazutoyo Yamada

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

3 Citations (Scopus)

Abstract

Recently, the application of turbochargers is increasing because they are effective in improving fuel consumption of engines. One of the most important turbocharger characteristics is compressor operating range, since it has been used in various driving patterns with the advent of variable geometry turbochargers. Owing to the complicated phenomena such as rotating stall occurring at low flow rate condition, flow analysis is very difficult and details of flow structure have not been fully understood for a long time since the early 1970's. In this study, two compressors with different operating range width were investigated with experimental and computational flow analysis. In the compressor with narrow operating range, the amplitude of blade passing pressure fluctuation decreases rapidly and rotating stall occurs near surging. On the other hand, in the compressor with wide operating range, the blockage by the tip leakage vortex breakdown play a role in stabilizing the flow filed and keeping up a high performance even at low flow rates.

Original languageEnglish
Title of host publicationASME Turbo Expo 2012
Subtitle of host publicationTurbine Technical Conference and Exposition, GT 2012
Pages735-743
Number of pages9
EditionPARTS A, B, AND C
DOIs
Publication statusPublished - Dec 1 2012
EventASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012 - Copenhagen, Denmark
Duration: Jun 11 2012Jun 15 2012

Publication series

NameProceedings of the ASME Turbo Expo
NumberPARTS A, B, AND C
Volume8

Other

OtherASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012
CountryDenmark
CityCopenhagen
Period6/11/126/15/12

Fingerprint

Centrifugal compressors
Compressors
Vortex flow
Flow rate
Flow structure
Fuel consumption
Engines
Geometry

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Tomita, I., Ibaraki, S., Furukawa, M., & Yamada, K. (2012). The effect of tip leakage vortex for operating range enhancement of centrifugal compressor. In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012 (PARTS A, B, AND C ed., pp. 735-743). (Proceedings of the ASME Turbo Expo; Vol. 8, No. PARTS A, B, AND C). https://doi.org/10.1115/GT2012-68947

The effect of tip leakage vortex for operating range enhancement of centrifugal compressor. / Tomita, Isao; Ibaraki, Seiichi; Furukawa, Masato; Yamada, Kazutoyo.

ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A, B, AND C. ed. 2012. p. 735-743 (Proceedings of the ASME Turbo Expo; Vol. 8, No. PARTS A, B, AND C).

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

Tomita, I, Ibaraki, S, Furukawa, M & Yamada, K 2012, The effect of tip leakage vortex for operating range enhancement of centrifugal compressor. in ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A, B, AND C edn, Proceedings of the ASME Turbo Expo, no. PARTS A, B, AND C, vol. 8, pp. 735-743, ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012, Copenhagen, Denmark, 6/11/12. https://doi.org/10.1115/GT2012-68947
Tomita I, Ibaraki S, Furukawa M, Yamada K. The effect of tip leakage vortex for operating range enhancement of centrifugal compressor. In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A, B, AND C ed. 2012. p. 735-743. (Proceedings of the ASME Turbo Expo; PARTS A, B, AND C). https://doi.org/10.1115/GT2012-68947
Tomita, Isao ; Ibaraki, Seiichi ; Furukawa, Masato ; Yamada, Kazutoyo. / The effect of tip leakage vortex for operating range enhancement of centrifugal compressor. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012. PARTS A, B, AND C. ed. 2012. pp. 735-743 (Proceedings of the ASME Turbo Expo; PARTS A, B, AND C).
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