Details
Original language | English |
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Title of host publication | Institution of Mechanical Engineers - 13th International Conference on Turbochargers and Turbocharging 2018 |
Pages | 71-87 |
Number of pages | 17 |
ISBN (electronic) | 9781510873872 |
Publication status | Published - 2018 |
Event | 13th International Conference on Turbochargers and Turbocharging 2018 - London, United Kingdom (UK) Duration: 16 May 2018 → 17 May 2018 |
Publication series
Name | Institution of Mechanical Engineers - 13th International Conference on Turbochargers and Turbocharging 2018 |
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Abstract
The feasibility of a compressor concept with variable-area inlet annulus, variable-width diffuser is investigated based on experimental measurements at a hot-gas test bench and an engine test bench. The experiments are carried out on two compressors stages with different flow ranges. The experimental results show the potential of flow range enhancement through variable cross-section. Both compressors achieve 50% reduction in surge mass flow and a 30-40% increase in operating range as measured by mass flow between stall and choke limits. The results of the engine tests verify the capability of the concept concerning low-end torque improvement of the engine. By means of the variation of compressor cross-section, the larger of the two compressors achieves an equal low-end torque as the smaller reference compressor.
ASJC Scopus subject areas
- Energy(all)
- Fuel Technology
- Engineering(all)
- Automotive Engineering
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Institution of Mechanical Engineers - 13th International Conference on Turbochargers and Turbocharging 2018. 2018. p. 71-87 (Institution of Mechanical Engineers - 13th International Conference on Turbochargers and Turbocharging 2018).
Research output: Chapter in book/report/conference proceeding › Conference contribution › Research › peer review
}
TY - GEN
T1 - Flow range of variable cross-section compressors
AU - Fischer, T.
AU - Kleine Sextro, T.
AU - Seume, J. R.
AU - Flinte, J.
AU - Eilts, P.
PY - 2018
Y1 - 2018
N2 - The feasibility of a compressor concept with variable-area inlet annulus, variable-width diffuser is investigated based on experimental measurements at a hot-gas test bench and an engine test bench. The experiments are carried out on two compressors stages with different flow ranges. The experimental results show the potential of flow range enhancement through variable cross-section. Both compressors achieve 50% reduction in surge mass flow and a 30-40% increase in operating range as measured by mass flow between stall and choke limits. The results of the engine tests verify the capability of the concept concerning low-end torque improvement of the engine. By means of the variation of compressor cross-section, the larger of the two compressors achieves an equal low-end torque as the smaller reference compressor.
AB - The feasibility of a compressor concept with variable-area inlet annulus, variable-width diffuser is investigated based on experimental measurements at a hot-gas test bench and an engine test bench. The experiments are carried out on two compressors stages with different flow ranges. The experimental results show the potential of flow range enhancement through variable cross-section. Both compressors achieve 50% reduction in surge mass flow and a 30-40% increase in operating range as measured by mass flow between stall and choke limits. The results of the engine tests verify the capability of the concept concerning low-end torque improvement of the engine. By means of the variation of compressor cross-section, the larger of the two compressors achieves an equal low-end torque as the smaller reference compressor.
UR - http://www.scopus.com/inward/record.url?scp=85064982034&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85064982034
T3 - Institution of Mechanical Engineers - 13th International Conference on Turbochargers and Turbocharging 2018
SP - 71
EP - 87
BT - Institution of Mechanical Engineers - 13th International Conference on Turbochargers and Turbocharging 2018
T2 - 13th International Conference on Turbochargers and Turbocharging 2018
Y2 - 16 May 2018 through 17 May 2018
ER -