Iranian Journal of Mechanical Engineering Transactions of ISME

Iranian Journal of Mechanical Engineering Transactions of ISME

Thermodynamic and Exergy Analysis of an Environmentally Friendly Turbofan Engine for Use in Commercial Aircraft

Authors
1 PhD Student, Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran
2 Associate Professor, Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran
3 Professor Department of Aerospace Engineering, Malek Ashtar University of Technology, Isfahan, Iran
Abstract
In this article, the CFM56 turbofan engine has been analyzed from the perspective of thermodynamics and exergy. Exergy is a key parameter in determining the components with the highest losses in the system and facilitating to minimize these losses and related costs. In addition to performance simulation, the use of exergy analysis helps to make this device more efficient in using energy resources, reducing costs and also reducing environmental pollution. In this research, the effect of compressor pressure ratio, turbine inlet gas temperature, fan pressure ratio, and fuel type on the production thrust of the system, energy efficiency and exergy of the system, the Specific fuel consumption of the system and the amount of environmental pollution are investigated with the parametric study of the system. The results show that the best production thrust of the system is 1.23 kN.s/kg in the compressor pressure ratio of 20. Also, the results show that the energy and exergy efficiency of the system will be 0.49 and 0.62, respectively. The results show that the most exergy destruction occurs in the nozzle.
Keywords

Subjects


 

 
[1]               Y. Cangel, and M. A. Boles, “Thermodynamics: An Engineering Approach,” 4th Edition, in SI Units, Singapore (SI): McGraw-Hill, 2002, Cangel: Thermodynamics: an engineering approach 4th... - Google Scholar.
 
[2]               A. F. El-Sayed, “Engineering & Technology: Aircraft Propulsion and Gas Turbine Engines,” 2nd Edition, Boca Raton, CRC Press, 2017.
 
[3]               O. Turan, "Effect of Reference Altitudes for a Turbofan Engine with the Aid of Specific–exergy Based Methode," International Journal of Exergy, Vol. 11, No. 2, pp. 252-270, 2012, https://doi.org/10.1504/IJEX.2012.047337.
 
[4]               Y. Şöhret, A. Dinç, and T. H. Karakoç, "Exergy Analysis of a Turbofan Engine for an Unmanned Aerial Vehicle During a Surveillance Mission," Energy, Vol. 93, pp. 716-729, 2015, https://doi.org/10.1016/j.energy.2015.09.094.
 
[5]               O. Balli, "Advanced Exergy Analysis of a Turbofan Engine (TFE): Splitting Exergy Destruction into Unavoidable/Avoidable and Endogenous/Exogenous," International Journal of Turbo & Jet-Engines, Vol. 36, ZNo. 3, pp. 305-327, 2019, https://doi.org/10.1515/tjj-2018-0040.
 
[6]               E. Yalcin, "Thrust Performance Evaluation of a Turbofan Engine Based on Exergetic Approach and Thrust Management in Aircraft," International Journal of Turbo & Jet-Engines, Vol. 34, No. 2, pp. 177-186, 2017, https://doi.org/10.1515/tjj-2016-0045.
 
[7]               S. A. Shakariyants, J. P. van Buijtenen, W. P. J. Visser, and A Tarasov "A Multidisciplinary Aero-engine Exhaust Emission Study," in ASME Turbo Expo 2006: Power for Land, Sea, and Air, 2006, https://doi.org/10.1115/GT2006-90267.  
                                    
[8]               N. Chandrasekaran, and A. Guha, "Study of Prediction Methods for NOx Emission from Turbofan Engines," Journal of Propulsion and Power, Vol. 28, No. 1, pp. 170-180, 2012, https://doi.org/10.2514/1.B34203.
 
[9]               K. G. Kyprianidis, and E. Dahlquist, "On the Trade-off between Aviation NOx and Energy Efficiency," Applied Energy, Vol. 185, pp. 1506-1516, 2017, https://doi.org/10.1016/j.apenergy.2015.10.084.
 
[10]           F. Noori, M. GorjiA. Kazemi, and H. Nemati, "Thermodynamic Optimization of Ideal Turbojet with Afterburner Engines using Non-dominated Sorting Genetic Algorithm II," Proceedings of the Institution of Mechanical Engineers, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 224, No. 12, pp. 1285-1296, 2010, https://doi.org/10.1243/09544100JAERO771.     
 
[11]           V. Patel, V. Savsani, and A. Mudgal, "Efficiency, Thrust, and Fuel Consumption Optimization of a Subsonic/sonic Turbojet Engine” Energy, Vol. 144, pp. 992-1002, 2018,  https://doi.org/10.1016/j.energy.2017.12.080.   
 
 
[12]           H. Aygun, and O. Turan, "Exergetic Sustainability off-design Analysis of Variable-cycle Aero-engine in Various Bypass Modes," Energy, Vol. 195, pp. 117008, 2020, https://doi.org/10.1016/j.energy.2020.117008.
 
[13]           O. Turan, "Exergo-economic Analysis of a CFM56-7B Turbofan Engine," Energy, Vol. 259, pp. 124936, 2022, https://doi.org/10.1016/j.energy.2022.124936.
 
[14]           P. Kobra, O. BalliH. CaliskanS. Al-Rabeei, and U. Kale, "Energy, Exergy, Economic, Environmental, and Sustainability Assessments of the CFM56-3 Series Turbofan Engine used in the Aviation Sector," Energy, Vol. 269, pp. 126765, 2023, https://doi.org/10.1016/j.energy.2023.126765.

  • Receive Date 17 September 2024
  • Revise Date 16 June 2025
  • Accept Date 30 July 2025