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Design and Experimental Study on a Turbo Air Compressor for Fuel Cell Applications  

Choi, Jae-Ho (Power Systems R&D Center, Samsung Techwin)
Publication Information
Transactions of the Korean hydrogen and new energy society / v.19, no.1, 2008 , pp. 26-34 More about this Journal
Abstract
This study presents an aerodynamic design and an experimental performance test of a turbo air compressor consisted of mixed-flow impeller and curved diffuser for the PEM fuel cell vehicle application. Many studies compare the efficiency, cost or noise level of high-pressure and low-pressure operation of PEM fuel cell systems. Pressure ratio 2.2:1 is considered as design target The goal of compressor design is to enlarge the flow margin of compressor from surge to choke mass flow rate to cover the operational envelope of FCV. Large-scale rig test is performed to evaluate the compressor performance and to compare the effects of compressor exit pipe volume to stall or surge characteristics. The results show that the mixed-flow compressor designed has large flow margin, and the flow margin of compressor configuration with small exit volume is larger than that with large exit volume.
Keywords
turbo compressor; fuel cell vehicle; surge margin; aerodynamic design; compressor characteristic curve;
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