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Exergy analysis of a three-spool turboprop engine during the flight of a cargo aircraft
Aircraft Engineering and Aerospace Technology ( IF 1.2 ) Pub Date : 2020-07-29 , DOI: 10.1108/aeat-05-2020-0087
Ali Dinc , Yasin Şöhret , Selcuk Ekici

Purpose

This study aims to introduce exergy analysis of a three-spool turboprop engine during the complete flight.

Design/methodology/approach

In this study, a flight scenario of the aircraft is assumed. Operating parameters of the aircraft and its engine are modelled based on the assumed flight scenario with the aid of a genuine code. And then performance analysis of the engine is performed for each flight path point with the aid of exergy.

Findings

At the end of the study, major exergy parameters of the engine are calculated during the complete flight of a cargo aircraft three-spool turboprop engine.

Practical implications

Findings of the study may be beneficial for industry and practitioners to improve performance of the evaluated engine.

Originality/value

To the best of authors’ knowledge, this paper presented the exergy analysis of a three-spool turboprop engine during the complete flight for the first time. It was shown how the exergy destruction rate depends on the altitude and manoeuvre.



中文翻译:

三轴涡轮螺旋桨发动机在货机飞行过程中的火用分析

目的

这项研究的目的是介绍完整飞行过程中三阀芯涡轮螺旋桨发动机的火用分析。

设计/方法/方法

在这项研究中,假设飞机的飞行情况。航空器及其发动机的运行参数是根据假设的飞行情况在真实代码的帮助下建模的。然后借助火力对每个飞行路径点进行发动机性能分析。

发现

在研究结束时,发动机的主要火用参数是在货机三阀芯涡轮螺旋桨发动机的完整飞行过程中计算的。

实际影响

研究的结果可能对行业和从业者有益,以提高被评估发动机的性能。

创意/价值

据作者所知,本文首次介绍了三涡管螺旋桨发动机在整个飞行过程中的火用分析。结果表明,火用破坏率如何取决于海拔高度和机动性。

更新日期:2020-07-29
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