Exhaust Gas Energy Recovery Via Electric Turbocompounding
This paper presents the development of a high performance Low Pressure Turbine for turbocompounding applicationsindownsized gasoline engines. The LPT was designed to fill the existing technology gap where no commercially available turbines can operate effectively at low pressure ratios (1.05 - 1.3),...
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sg-ntu-dr.10356-836622023-03-04T17:16:09Z Exhaust Gas Energy Recovery Via Electric Turbocompounding Rajoo, S. Petrovic, Simon Romagnoli, Alessandro Chiong, M. C. Martinez-Botas, R. F. Bin Mamat, A. M. I. School of Mechanical and Aerospace Engineering This paper presents the development of a high performance Low Pressure Turbine for turbocompounding applicationsindownsized gasoline engines. The LPT was designed to fill the existing technology gap where no commercially available turbines can operate effectively at low pressure ratios (1.05 - 1.3), in order to drive a small electric generator with continuouspower output of 1.0 kW. The newly designed LPT was tested in a gas test stand and its impact on Brake Specific Fuel Consumption was assessed with on engine testing carried out on a 1.0L EcoBoostgasoline engine. Published version 2015-12-10T08:52:51Z 2019-12-06T15:27:48Z 2015-12-10T08:52:51Z 2019-12-06T15:27:48Z 2015 Journal Article Bin Mamat, A. M. I., Martinez-Botas, R. F., Chiong, M. C., Rajoo, S., Petrovic, S., & Romagnoli, A. (2015). Exhaust Gas Energy Recovery Via Electric Turbocompounding. Energy Procedia, 75, 1555-1559. 1876-6102 https://hdl.handle.net/10356/83662 http://hdl.handle.net/10220/39043 10.1016/j.egypro.2015.07.336 en Energy Procedia © 2015 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/). Peer-review under responsibility of Applied Energy Innovation Institute. 5 p. application/pdf |
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This paper presents the development of a high performance Low Pressure Turbine for turbocompounding applicationsindownsized gasoline engines. The LPT was designed to fill the existing technology gap where no commercially available turbines can operate effectively at low pressure ratios (1.05 - 1.3), in order to drive a small electric generator with continuouspower output of 1.0 kW. The newly designed LPT was tested in a gas test stand and its impact on Brake Specific Fuel Consumption was assessed with on engine testing carried out on a 1.0L EcoBoostgasoline engine. |
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School of Mechanical and Aerospace Engineering |
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School of Mechanical and Aerospace Engineering Rajoo, S. Petrovic, Simon Romagnoli, Alessandro Chiong, M. C. Martinez-Botas, R. F. Bin Mamat, A. M. I. |
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Article |
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Rajoo, S. Petrovic, Simon Romagnoli, Alessandro Chiong, M. C. Martinez-Botas, R. F. Bin Mamat, A. M. I. |
spellingShingle |
Rajoo, S. Petrovic, Simon Romagnoli, Alessandro Chiong, M. C. Martinez-Botas, R. F. Bin Mamat, A. M. I. Exhaust Gas Energy Recovery Via Electric Turbocompounding |
author_sort |
Rajoo, S. |
title |
Exhaust Gas Energy Recovery Via Electric Turbocompounding |
title_short |
Exhaust Gas Energy Recovery Via Electric Turbocompounding |
title_full |
Exhaust Gas Energy Recovery Via Electric Turbocompounding |
title_fullStr |
Exhaust Gas Energy Recovery Via Electric Turbocompounding |
title_full_unstemmed |
Exhaust Gas Energy Recovery Via Electric Turbocompounding |
title_sort |
exhaust gas energy recovery via electric turbocompounding |
publishDate |
2015 |
url |
https://hdl.handle.net/10356/83662 http://hdl.handle.net/10220/39043 |
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1759855831652761600 |