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contributor authorA. F. Massardo
date accessioned2017-05-09T00:10:16Z
date available2017-05-09T00:10:16Z
date copyrightJanuary, 2003
date issued2003
identifier issn1528-8919
identifier otherJETPEZ-26819#67_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128414
description abstractThe aim of this work is to investigate the performance of internal reforming solid oxide fuel cell (IRSOFC) and gas turbine (GT) combined cycles. A mathematical model of the IRSOFC steady-state operation was presented in Part I of this work coupled to the thermodynamic analysis of a number of proposed IRSOFC-GT combined cycles, taking into account the influence of several technological constraints. In the second part of this work, both an exergy and a thermoeconomic analysis of the proposed cycles have been carried out using the TEMP code developed by the author. A suitable equation for IRSOFC cost evaluation based on cell geometry and performance has been proposed and employed to evaluate the electricity generation cost of the proposed combined systems. The results are presented and the influence of several parameters is discussed: external reformer operating conditions, fuel-to-air ratio, cell current density, compressor pressure ratio, etc. Diagrams proposed by the author for cost versus efficiency, cost versus specific work, and cost versus system pressure are also presented and discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleInternal Reforming Solid Oxide Fuel Cell Gas Turbine Combined Cycles (IRSOFC-GT)—Part II: Exergy and Thermoeconomic Analyses
typeJournal Paper
journal volume125
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1492837
journal fristpage67
journal lastpage74
identifier eissn0742-4795
keywordsPressure
keywordsFuels
keywordsCompressors
keywordsExergy
keywordsGas turbines
keywordsSolid oxide fuel cells
keywordsCycles
keywordsIndustrial plants
keywordsEquations
keywordsExergy analysis AND Current density
treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001
contenttypeFulltext


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