کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
5477324 1399217 2016 15 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Comparison of different gas turbine cycles and advanced exergy analysis of the most effective
ترجمه فارسی عنوان
مقایسه چرخه های توربین گاز مختلف و تجزیه و تحلیل اگزرژی پیشرفته از موثر ترین
کلمات کلیدی
توربین گاز تزریق بخار، خنک کننده هوا، روش خنک کننده خنک کننده اگزرژی، تجزیه و تحلیل پیشرفته اضافی،
موضوعات مرتبط
مهندسی و علوم پایه مهندسی انرژی انرژی (عمومی)
چکیده انگلیسی
Four gas turbine systems are compared: simple gas turbine (SGT), gas turbine with evaporative inlet air cooler (EVGT), steam injection gas turbine (STIG) and steam injection gas turbine with evaporative inlet air cooler (ESTIG). These comparisons are done on the basis of conventional exergy analysis and the results show that the ESTIG cycle is the most advantageous for the designer. After determining the ESTIG optimum conditions from maximum net work and maximum second law efficiency perspectives using conventional exergy analysis, advanced exergy analysis is performed for this system at its optimum conditions to provide detailed information about the improvement potential of the system components. The analysis is carried out on the basis of the engineering method and the thermodynamic cycle method is used to validate the endogenous exergy destruction rates of the system components. The results show that the optimization priority order for the system components is different when determined with advanced exergy analysis compared to conventional exergy analysis.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Energy - Volume 116, Part 1, 1 December 2016, Pages 701-715
نویسندگان
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