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2017 | OriginalPaper | Buchkapitel

23. Exergy Approach to Evaluate Performance of a Mini Class Turboprop Engine

verfasst von : Kahraman Coban, Yasin Şöhret, M. Ziya Sogut, Onder Turan, T. Hikmet Karakoc

Erschienen in: Energy Solutions to Combat Global Warming

Verlag: Springer International Publishing

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Abstract

In this chapter, performance assessment of a mini class turboprop engine is presented. Exergy analysis is used for this purpose on the basis of applicability on thermal systems. As a result of the component-based exergy analysis, relative irreversibility of the combustion chamber is higher relatively. Exergy destruction rates within the air compressor, combustion chamber and gas turbine components are 24.08 kW, 100.76 kW and 15.80 kW respectively. Additionally, exergy efficiencies of the components are 74.11, 69.68 and 98.99 % in order of air compressor, combustion chamber and gas turbine.

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Metadaten
Titel
Exergy Approach to Evaluate Performance of a Mini Class Turboprop Engine
verfasst von
Kahraman Coban
Yasin Şöhret
M. Ziya Sogut
Onder Turan
T. Hikmet Karakoc
Copyright-Jahr
2017
DOI
https://doi.org/10.1007/978-3-319-26950-4_23