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Energy and performance analysis of a turbofan engine with the aid of dynamic component efficiencies

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  • Cihangir, Serhan Ahmet
  • Aygun, Hakan
  • Turan, Onder

Abstract

Assessment of performance of turbofan engine with different design parameters is crucial for meeting the performance requirements by considering each key components of the engine. To comprehend influences of component efficiencies to mitigate environmental effect from turbofans has been hot topics in aviation field recently. In this study, firstly, impacts of polytropic efficiencies of fan, compressor and turbine as well as pressure ratio of combustor (CPR) on several turbofan performance are dealt with at several flight conditions. Secondly, it is tried to show difference of performance metrics under ideal and real conditions. The discrepancy between performance parameters computed at ideal and real cases gets relatively high. Namely, at take-off condition, the difference between ideal and real specific fuel consumption is computed as 29.12% whereas it is found as 28.37% at cruise condition, which shows that considering the system as ideal makes the computations inappropriate for performance analysis. Moreover, performance parameters of turbofan is more sensitive to compressor efficiency compared with turbine. As the polytropic efficiencies of fan and compressor are close to highest, net thrust of the engine develops from 109.05 kN (baseline) to 124.71 kN at take-off while it increases from 26.36 kN (baseline) to 29.27 kN at cruise condition. With effect of the elevated pressure ratio of combustor and efficiency of turbine, thrust of the engine increases to 118.23 kN at take off and to 27.84 kN at cruise condition. Finally, as Mach number increases, the difference between ideal and real performance values sharply increases. Therefore, when analyzing on turbofan engines, the assumptions should be minimum as possible as, otherwise the findings make the engineers to misguide for system optimization. Besides, these outcomes show that if the components with higher polytropic efficiency can be obtained, overall efficiency of turbofan, thereby environmental sustainability could be elevated to upper level compared with baseline.

Suggested Citation

  • Cihangir, Serhan Ahmet & Aygun, Hakan & Turan, Onder, 2022. "Energy and performance analysis of a turbofan engine with the aid of dynamic component efficiencies," Energy, Elsevier, vol. 260(C).
  • Handle: RePEc:eee:energy:v:260:y:2022:i:c:s0360544222019806
    DOI: 10.1016/j.energy.2022.125085
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    1. Lai, Y.Y. & Christley, E. & Kulanovic, A. & Teng, C.C. & Björklund, A. & Nordensvärd, J. & Karakaya, E. & Urban, F., 2022. "Analysing the opportunities and challenges for mitigating the climate impact of aviation: A narrative review," Renewable and Sustainable Energy Reviews, Elsevier, vol. 156(C).
    2. Aygun, Hakan & Cilgin, Mehmet Emin & Turan, Onder, 2021. "Exergo-sustainability indicators of a target drone engine at dynamic loads," Energy, Elsevier, vol. 221(C).
    3. Yucer, Cem Tahsin, 2016. "Thermodynamic analysis of the part load performance for a small scale gas turbine jet engine by using exergy analysis method," Energy, Elsevier, vol. 111(C), pages 251-259.
    4. Turan, Onder, 2012. "Exergetic effects of some design parameters on the small turbojet engine for unmanned air vehicle applications," Energy, Elsevier, vol. 46(1), pages 51-61.
    5. Coban, Kahraman & Colpan, C. Ozgur & Karakoc, T. Hikmet, 2017. "Application of thermodynamic laws on a military helicopter engine," Energy, Elsevier, vol. 140(P2), pages 1427-1436.
    6. Zaporozhets, Oleksandr & Isaienko, Volodymyr & Synylo, Kateryna, 2020. "Trends on current and forecasted aircraft hybrid electric architectures and their impact on environment," Energy, Elsevier, vol. 211(C).
    7. Ji, Zhixing & Qin, Jiang & Cheng, Kunlin & Liu, He & Zhang, Silong & Dong, Peng, 2019. "Performance evaluation of a turbojet engine integrated with interstage turbine burner and solid oxide fuel cell," Energy, Elsevier, vol. 168(C), pages 702-711.
    8. Dahal, Karna & Brynolf, Selma & Xisto, Carlos & Hansson, Julia & Grahn, Maria & Grönstedt, Tomas & Lehtveer, Mariliis, 2021. "Techno-economic review of alternative fuels and propulsion systems for the aviation sector," Renewable and Sustainable Energy Reviews, Elsevier, vol. 151(C).
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