LAPSE:2023.3312
Published Article
LAPSE:2023.3312
Hybrid Propulsion Efficiency Increment through Exhaust Energy Recovery—Part 1: Radial Turbine Modelling and Design
February 22, 2023
Abstract
The efficiency of Hybrid Electric Vehicles (HEVs) may be substantially increased if the energy of the exhaust gases, which do not complete the expansion inside the cylinder of the internal combustion engine, is efficiently recovered by means of a properly designed turbogenerator and employed for vehicle propulsion; previous studies, carried out by the same authors of this work, showed a potential hybrid vehicle fuel efficiency increment up to 15% by employing a 20 kW turbine on a 100 HP rated power thermal unit. The innovative thermal unit here proposed is composed of a supercharged engine endowed with a properly designed turbogenerator, which comprises two fundamental elements: an exhaust gas turbine expressly designed and optimized for the application, and a suitable electric generator necessary to convert the recovered energy into electric energy, which can be stored in the on-board energy storage system of the vehicle. In these two parts, the realistic efficiency of the innovative thermal unit for hybrid vehicle is evaluated and compared to a traditional turbocharged engine. In Part 1, the authors present a model for the prediction of the efficiency of a dedicated radial turbine, based on a simple but effective mean-line approach; the same paper also reports a design algorithm, which, owing to some assumptions and approximations, allows a fast determination of the proper turbine geometry for a given design operating condition. It is worth pointing out that, being optimized for quasi-steady power production, the exhaust gas turbine considered is quite different from the ones commonly employed for turbocharging application; for this reason, and in consideration of the required power size, such a turbine is not available on the market, nor has its development been previously carried out in the scientific literature. In the Part 2 paper, a radial turbine geometry is defined for the thermal unit previously calculated, employing the design algorithm described in Part 1; the realistic energetic advantage that could be achieved by the implementation of the turbogenerator on a hybrid propulsion system is evaluated through the performance prediction model under the different operating conditions of the thermal unit. As an overall result, it was estimated that, compared to a reference traditional turbocharged engine, the turbocompound system could gain vehicle efficiency improvement between 3.1% and 17.9%, depending on the output power level, while an average efficiency increment of 10.9% was determined for the whole operating range.
Keywords
compound engine, exhaust energy recovery, exhaust gas turbine, hybrid vehicle
Suggested Citation
Pipitone E, Caltabellotta S, Sferlazza A, Cirrincione M. Hybrid Propulsion Efficiency Increment through Exhaust Energy Recovery—Part 1: Radial Turbine Modelling and Design. (2023). LAPSE:2023.3312
Author Affiliations
Pipitone E: Department of Engineering, University of Palermo, 90128 Palermo, Italy [ORCID]
Caltabellotta S: Department of Engineering, University of Palermo, 90128 Palermo, Italy [ORCID]
Sferlazza A: Department of Engineering, University of Palermo, 90128 Palermo, Italy [ORCID]
Cirrincione M: School of Engineering and Physics, University of the South Pacific, Suva, Fiji Islands
Journal Name
Energies
Volume
16
Issue
3
First Page
1030
Year
2023
Publication Date
2023-01-17
ISSN
1996-1073
Version Comments
Original Submission
Other Meta
PII: en16031030, Publication Type: Journal Article
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LAPSE:2023.3312
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https://doi.org/10.3390/en16031030
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Feb 22, 2023
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