Enhanced dynamic exergy analysis of a micro-jet (μ-jet) engine at various modes

被引:11
作者
Balli, Ozgur [1 ]
Aygun, Hakan [2 ]
Turan, Onder [3 ]
机构
[1] Minist Natl Def, Gen Directorate Mil Factories, Air Maintenance Factory Directorate 1, TR-26120 Eskisehir, Turkey
[2] Firat Univ, Dept Air Frame & Power Plant, TR-23119 Elazig, Turkey
[3] Eskisehir Tech Univ, Fac Aeronaut & Astronaut, TR-26450 Eskisehir, Turkey
关键词
Advance exergy; Microjet; Turbojet; Propulsion; TURBOPROP ENGINE; PERFORMANCE; DESTRUCTION; EVALUATE;
D O I
10.1016/j.energy.2021.121911
中图分类号
O414.1 [热力学];
学科分类号
摘要
In the current study, advanced exergo-dynamic analysis of a micro-turbo jet (mu-jet) along with conventional exergy analysis is presented in various running shaft speed modes. In this context, major advanced exergetic indicators of mu-jet components are evaluated at the various running testing. The operation modes were represented as operation shaft speeds between 48,850 and 77,000 RPM (revolution per minute), while mu-jet produced within the range of 45.01-121.27 N thrust force in these modes. Improvement potentials of turbomachinery components and exergy destruction rates are calculated throughout the real-time testing modes. According to the analysis, the combustor has the lowest exergy efficiency ranging from 41.06% to 50.18%. Also, the study shows that the exergy efficiency values of the experimental mu-jet are found to be as 6.56% at Mode-1, 10.12% at Mode-2, 15.46% at Mode-3 and 17.02% at Mode-4, respectively. Other important findings for mu-jet are that unavoidable exergy destruction rate varies between 94.89% and 95.79%, while endogenous exergy destruction value changes between 89.79% and 91.47% in these modes. Thanks to the present analysis, the methods decreasing avoidable exergy destruction that changes between 4.21% and 5.11% could be focused. (C) 2021 Elsevier Ltd. All rights reserved.
引用
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页数:22
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