Abstract
The exhaust gas from an internal combustion engine contains approximately 30% of the thermal energy of combustion. Waste heat recovery systems aim to reclaim a proportion of this energy in a bottoming thermodynamic cycle to raise the overall system thermal efficiency. The inverted Brayton cycle considered as a potential exhaust-gas heat-recovery system is a little-studied approach, especially when applied to small automotive power-plants. Hence, a model of an air-standard, irreversible Otto-cycle and the inverted Brayton cycle using finite-time thermodynamics (FTT) is presented to study heat recovery applied to an automotive internal combustion engine. The other two alternatives power cycle, the pressurized Brayton cycle and the turbo-compounding system, are compared with the Inverted Brayton Cycle (IBC) to specify the strengths and weaknesses of three alternative cycles. In the current paper, an irreversible Otto-cycle model that includes an array of losses is used as a basis for the bottoming cycle. The deviation of the turbomachinery from the idealized behavior is described by the isentropic component efficiencies. The performance of the system as defined as the specific power output and thermal efficiency is considered using parametric studies. The results show that the performance of the inverted Brayton cycle can be positively affected by five critical parameters – the number of compression stages, the cycle inlet temperature and pressure, the isentropic efficiency of the turbomachinery and the effectiveness of the heat exchanger. There exists an optimum pressure ratio across the IBC turbine that delivers the maximum specific power. In the view of the specific power, installing a single-stage of the inverted Brayton cycle appears the best balance between performance and complexity. Three alternative cycles are compared in terms of the thermal efficiency. The results indicate that the pressurized and Inverted Brayton Cycle can improve the performance of the turbocharged engine only when the turbomachinery efficiencies are higher than a critical value which changes with the operating condition. High performance of the IBC turbomachinery is required to ensure that the turbocharged engine with the inverted Brayton cycle is superior to that with turbo-compounding system.
Original language | English |
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Title of host publication | Proceedings of ASME Turbo Expo |
Subtitle of host publication | Turbine Technical Conference and Exposition, 2015. Volume 8 - Microturbines, Turbochargers and Small Turbomachines; Steam Turbines |
Place of Publication | Montreal, Canada |
Publisher | American Society of Mechanical Engineers (ASME) |
Pages | V008T23A006 |
Number of pages | 15 |
ISBN (Print) | 9780791856796 |
DOIs | |
Publication status | Published - 2015 |
Event | ASME Turbo Expo, 2015 - Palais de Congres, Montreal, Canada Duration: 15 Jun 2015 → 19 Jun 2015 |
Conference
Conference | ASME Turbo Expo, 2015 |
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Country/Territory | Canada |
City | Montreal |
Period | 15/06/15 → 19/06/15 |