Exergy analysis of a turbofan aircraft engine

被引：45

作者：

Turgut, Enis T. ^{[1
]}

Karakoc, T. Hikmet ^{[1
]}

Hepbasli, Arif ^{[2
]}

Rosen, Marc A. ^{[3
]}

机构：

[1] Anadolu Univ, Sch Civil Aviat, TR-26470 Eskisehir, Turkey

[2] Ege Univ, Dept Mech Engn, Fac Engn, TR-35100 Izmir, Turkey

[3] Univ Ontario, Inst Technol, Fac Engn & Appl Sci, Oshawa, ON L1H 7K4, Canada

来源：

INTERNATIONAL JOURNAL OF EXERGY | 2009年 / 6卷 / 02期

关键词：

exergy analysis; turbofan engine; Brayton cycle; efficiency; aerospace; aircraft; SYSTEMS; FLOWS;

D O I：

10.1504/IJEX.2009.023997

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

An exergy analysis is reported for a General Electric turbofan engine (the CF6-80) using sea-level data. The effects on exergy efficiencies and exergy destructions are investigated of modifying the isentropic efficiencies of turbomachinery components. The most irreversible units in the system are found to be the fan and the core engine exhaust, with exergy loss rates of 47.3 MW and 35.9 MW, respectively, and the combustion chamber, with an exergy destruction rate of 31.5 MW. The exergy efficiencies of the fan and the core engine exhausts are found to be 12.9 and 12.7%, respectively.

引用

页码：181 / 199

页数：19

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