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Reactivity Model as a Tool to Compare the Combustion Process in Aviation Turbine Engines Powered by Synthetic Fuels

Author

Listed:
  • Tomasz Białecki

    (Fuels and Lubricants Division, Air Force Institute of Technology (ITWL), 01-494 Warsaw, Poland)

  • Wojciech Dzięgielewski

    (Fuels and Lubricants Division, Air Force Institute of Technology (ITWL), 01-494 Warsaw, Poland)

  • Mirosław Kowalski

    (Fuels and Lubricants Division, Air Force Institute of Technology (ITWL), 01-494 Warsaw, Poland)

  • Andrzej Kulczycki

    (Fuels and Lubricants Division, Air Force Institute of Technology (ITWL), 01-494 Warsaw, Poland)

Abstract

The paper aims to verify the thesis that the reactivity model, developed in earlier research, can be used to compare the fuels combustion processes in turbine engines, which is important for predicting the behavior of different alternative fuels in combustion process. Synthetic blending components from alcohol to jet and hydroprocessed esters and fatty acids technologies and their blends with conventional jet fuel were used in tests. The undertaken laboratory tests reveal the differences between the properties of the tested fuels. Bench tests were carried out on a test rig with a miniature turbojet engine, according to authorial methodology. For each blend, on selected points of rotational speed the carbon oxide concentration in the exhaust gases was recorded. The obtained results allowed the formulation of empirical power functions describing relations between carbon oxide concentration and fuel mass flow rate. Based on general assumptions, the reactivity model was adopted to compare the combustion processes of the different fuels in turbine engines. The directions of further research on the development of the proposed model were indicated.

Suggested Citation

  • Tomasz Białecki & Wojciech Dzięgielewski & Mirosław Kowalski & Andrzej Kulczycki, 2021. "Reactivity Model as a Tool to Compare the Combustion Process in Aviation Turbine Engines Powered by Synthetic Fuels," Energies, MDPI, vol. 14(19), pages 1-16, October.
  • Handle: RePEc:gam:jeners:v:14:y:2021:i:19:p:6302-:d:648991
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    References listed on IDEAS

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    2. Bartosz Gawron & Tomasz Białecki & Anna Janicka & Tomasz Suchocki, 2020. "Combustion and Emissions Characteristics of the Turbine Engine Fueled with HEFA Blends from Different Feedstocks," Energies, MDPI, vol. 13(5), pages 1-12, March.
    3. Suchocki, T. & Witanowski, Ł. & Lampart, P. & Kazimierski, P. & Januszewicz, K. & Gawron, B., 2021. "Experimental investigation of performance and emission characteristics of a miniature gas turbine supplied by blends of kerosene and waste tyre pyrolysis oil," Energy, Elsevier, vol. 215(PA).
    4. Zhang, Yayun & Duan, Dengle & Lei, Hanwu & Villota, Elmar & Ruan, Roger, 2019. "Jet fuel production from waste plastics via catalytic pyrolysis with activated carbons," Applied Energy, Elsevier, vol. 251(C), pages 1-1.
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    Cited by:

    1. Talal Yusaf & K. Kadirgama & Steve Hall & Louis Fernandes, 2022. "The Future of Sustainable Aviation Fuels, Challenges and Solutions," Energies, MDPI, vol. 15(21), pages 1-4, November.
    2. Mohsen Ayoobi & Pedro R. Resende & Alexandre M. Afonso, 2022. "Numerical Investigations of Combustion—An Overview," Energies, MDPI, vol. 15(9), pages 1-5, April.
    3. Urszula Kaźmierczak & Wojciech Dzięgielewski & Andrzej Kulczycki, 2022. "Miscibility of Aviation Turbine Engine Fuels Containing Various Synthetic Components," Energies, MDPI, vol. 15(17), pages 1-25, August.
    4. Bartosz Gawron & Aleksander Górniak & Tomasz Białecki & Anna Janicka & Radosław Włostowski & Adriana Włóka & Justyna Molska & Maciej Zawiślak, 2021. "Impact of a Synthetic Component on the Emission of Volatile Organic Compounds during the Combustion Process in a Miniature Turbine Engine," Energies, MDPI, vol. 14(24), pages 1-9, December.

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