作者: Diamantis P. Bakalis , Anastassios G. Stamatis
DOI: 10.1002/ER.3207
关键词: Gas compressor 、 Range (aeronautics) 、 Turbine 、 Turbomachinery 、 Mechanical engineering 、 Solid oxide fuel cell 、 Engineering 、 Gas turbines 、 Hybrid system
摘要: SUMMARY A methodology to improve the performance of a hybrid solid oxide fuel cell gas turbine (SOFC-GT) system for whole operating range is proposed. The method suggests way estimate geometric parameters turbomachinery components SOFC-GT system. It based on search compressor and lines giving optimum efficiency both in design part load operation. Turbomachinery models are used calculate geometry that produces desired maps corresponding lines. Based new design, shows clear advantage range. Copyright © 2014 John Wiley & Sons, Ltd.