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Comparative Performance Metric Assessment of A Military Turbojet Engine Utilizing Hydrogen And Kerosene Fuels Through Advanced Exergy Analysis Method

Author

Listed:
  • Burak Yuksel

    (Department of Mechanical Engineering, Ege University, Bornova, Izmir 35100, Turkey)

  • Ozgur Balli

    (First Air Maintenance Factory Directorate, Ministry of Defence, Eskisehir 26320, Turkey)

  • Huseyin Gunerhan

    (Department of Mechanical Engineering, Ege University, Bornova, Izmir 35100, Turkey)

  • Arif Hepbasli

    (Department of Energy Engineering, Yasar University, Bornova, Izmir 35100, Turkey)

Abstract

This study dealt with evaluating the (J85-GE-5H) military turbojet engine (TJE) in terms of exergetic and advanced exergetic analyses at Military (MIL) and Afterburner (AB) process modes by utilizing kerosene (JP-8) and hydrogen (H 2 ) fuels. First, exergy and advanced exergy analyses of the engine were performed using JP-8 fuel as per actual engine operating conditions. These analyses of the turbojet engine using hydrogen fuel were also examined parametrically. The performance evaluation of the engine was lastly executed by comparing the obtained results for both fuels. Based on the parametric studies undertaken, the entire engine’s exergetic efficiency with JP-8 was reckoned 30.85% at the MIL process mode while it was calculated as 16.98% at the AB process mode. With the usage of H 2 , the efficiencies of the engine decreased to 28.62% and 15.33% for the above mentioned two modes, respectively. As the supreme exergy destructions occurred in the combustion chamber (CC) and afterburner exhaust duct (ABED) segments, the new technological developments should be considered to design more efficient engines. As a result, the engine worked less efficiently with hydrogen fuel due to the enhancement in exergy destructions. Conversely, the greenhouse gas (GHG) emission parameters lessened with the utilization of H 2 fuel.

Suggested Citation

  • Burak Yuksel & Ozgur Balli & Huseyin Gunerhan & Arif Hepbasli, 2020. "Comparative Performance Metric Assessment of A Military Turbojet Engine Utilizing Hydrogen And Kerosene Fuels Through Advanced Exergy Analysis Method," Energies, MDPI, vol. 13(5), pages 1-22, March.
    • Handle: RePEc:gam:jeners:v:13:y:2020:i:5:p:1205-:d:329052
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    References listed on IDEAS

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    1. Burak Yuksel & Huseyin Gunerhan & Arif Hepbasli, 2020. "Assessing Exergy-Based Economic and Sustainability Analyses of a Military Gas Turbine Engine Fueled with Various Fuels," Energies, MDPI, vol. 13(15), pages 1-28, July.
    2. Andrzej Soboń & Daniel Słyś & Mariusz Ruszel & Alicja Wiącek, 2021. "Prospects for the Use of Hydrogen in the Armed Forces," Energies, MDPI, vol. 14(21), pages 1-12, October.
    3. Kagan Ayaz, S. & Caliskan, Hakan & Altuntas, Onder, 2023. "Environmental and second law analysis of a turbojet engine operating with different fuels," Energy, Elsevier, vol. 285(C).
    4. Akdeniz, Halil Yalcin & Balli, Ozgur, 2022. "Impact of different fuel usages on thermodynamic performances of a high bypass turbofan engine used in commercial aircraft," Energy, Elsevier, vol. 238(PA).

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