A comparison of strategies to extend the operating range of radial compressors for turbocharging

Abstract

The operating range extension of radial compressors is a crucial aspect in turbocharging the internal combustion engines in order to extend the operating range of the system at high efficiency for fuel and environmental impact reduction. The future scenario of automotive propulsion will have the fuel cells at the top of the ranking of possible reference systems in substitution of thermal reciprocating engines. Proton exchange membrane fuel cells for automotive or aerospace vehicles are frequently turbocharged because compressed air for the fuel cell stack is required in the cathode system. Therefore, like in turbocharged internal combustion engines, a radial compressor is combined and connected with a radial turbine to exploit the thermal energy of the exhaust gas from the fuel cell. The study and the development of this sort of radial turbomachinery is still strategic to guarantee high performance of the overall propulsion system. The operating range is an important issue and current turbocharger design must be adapted to the new requirements of the fuel cells systems with a need for extending it. Various techniques to extend the operating range of the centrifugal compressor have been investigated and a summary is reported in this work, with a focus on the casing treatment. Through a CFD simulation campaign with appropriate simplified models, the effects of installing the ported shroud, the shutter or the axial groove have been calculated with respect to a baseline configuration. These simulations have supported the identification of the main limits and advantages for each of these solutions at different operating regimes. The performance maps and some physical parameters of interest have been compared.

Instability Phenomena in Centrifugal Compressors and Strategies to Extend the Operating Range: A Review

“…Leichtfuß et al [114] evaluated axial grooves in different compressor configurations, showing a surge extension, especially for high speeds; it reduced the inlet recirculation and increased the pressure ratio, while the efficiency decreased by 2% due to mixing losses. Cravero and Marsano [115] compared the advantages of the axial groove with those Leichtfuß et al [114] evaluated axial grooves in different compressor configurations, showing a surge extension, especially for high speeds; it reduced the inlet recirculation and increased the pressure ratio, while the efficiency decreased by 2% due to mixing losses. Cravero and Marsano [115] compared the advantages of the axial groove with those of the ported shroud.…”

“…Cravero and Marsano [115] compared the advantages of the axial groove with those Leichtfuß et al [114] evaluated axial grooves in different compressor configurations, showing a surge extension, especially for high speeds; it reduced the inlet recirculation and increased the pressure ratio, while the efficiency decreased by 2% due to mixing losses. Cravero and Marsano [115] compared the advantages of the axial groove with those of the ported shroud. Configurations involving a circumferential groove casing treatment and an air bleeding circumferential groove casing treatment were analyzed on the KRAIN centrifugal compressor by Gao [116].…”