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Assessment of altitude effects based on the consumption behavior of a piston-prop engine by entropy approach.

Authors :
Sogut, Mehmet Ziya
Source :
Aircraft Engineering & Aerospace Technology. 2024, Vol. 96 Issue 7, p945-953. 9p.
Publication Year :
2024

Abstract

Purpose: The altitude and weather conditions affect directly fuel consumption and engine efficiency of the aircraft engines. The thermo-physical properties of the weather of altitude play a significant role in this process. Unfortunately, engine performance based on altitude conditions also causes waste heat and environmental pollution due to engine entropy generation. However, environmental impact assessment is needed to improve environmental sustainability. This study aimed to analyse the energy and environmental performance of a piston engine based on altitude conditions. Design/methodology/approach: This study is based on the entropy approach, and it aims to assess the environmental impact of the engine. Exergy analysis with together two new indices to evaluate the environmental effects caused by the engine under altitude conditions was used. Findings: The analysis reveals that the exergy efficiency of the piston engine is 23.9% on average for the three referenced altitudes, while the exergy efficiency difference between altitude boundary conditions is 11%. In addition, the entropy production of the engine is on average 10.55 kW/K. In this case, the environmental pollution potential resulting from the entropy production of the engine is on average 3.29 times higher due to reversible conditions, while the improvement rate was found to be 58%. Originality/value: This analysis shows that engine efficiency increases as altitude increases. Similarly, it can also be said that the environmental impacts are reduced and the improvement of the engine has opportunities for operational processes. Besides, in the study, some suggestions for motor performance impact analysis were presented. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
17488842
Volume :
96
Issue :
7
Database :
Academic Search Index
Journal :
Aircraft Engineering & Aerospace Technology
Publication Type :
Academic Journal
Accession number :
179244503
Full Text :
https://doi.org/10.1108/AEAT-02-2024-0028