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Fuel dilution and liquid fuel operational effects on ultra-high thermal intensity distributed combustor

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  • Arghode, Vaibhav K.
  • Khalil, Ahmed E.E.
  • Gupta, Ashwani K.

Abstract

Ultra-high thermal intensity colorless distributed combustion has been examined for methane and methane diluted with air, nitrogen or carbon dioxide gas and liquid fuel (ethanol) burning in air at a fixed thermal load. Fuel was diluted with inert gases and air to simulate the combustion of low heating value fuels with special focus on the emission of pollutants. Reverse cross-flow configuration has been investigated at very high thermal intensities in the range of 156–198MW/m3atm with specific focus on the exhaust emissions, and distribution of intermediate radical species emission and flowfield from within the combustor using novel but simplified geometry for easy transition to practical applications in ultra-high thermal intensity gas turbine engine applications. The ultra-high combustion intensity demonstrated here is significantly higher than that used in current stationary gas turbine engines. Numerical simulations are also performed under non-reacting conditions to understand the effects of fuel injection in cross flow configuration for both undiluted and diluted fuel cases. Ultra low NOx emissions are achieved for both the novel premixed (3ppm) and non-premixed (8ppm) mode using methane as fuel at equivalence ratio of 0.6. Carbon monoxide level of about 100ppm was obtained in both novel premixed and non-premixed modes of combustion at equivalence ratio of 0.6. Dilution of fuel significantly reduced NO emissions to 2ppm from 8ppm and slightly increased CO emissions in non-premixed mode at equivalence ratio of 0.6. Dilution of fuel suggested much lower OH* suggesting favorably mixed oxidizer prior to ignition that results in lower NO emissions. Liquid fuel (ethanol) was also examined and very low NO emission of about 6ppm was obtained in direct-injection mode and 2ppm in premixed–prevaporized mode at equivalence ratio of 0.6. CO emission of about 200ppm was observed in both the modes at equivalence ratio of 0.6.

Suggested Citation

  • Arghode, Vaibhav K. & Khalil, Ahmed E.E. & Gupta, Ashwani K., 2012. "Fuel dilution and liquid fuel operational effects on ultra-high thermal intensity distributed combustor," Applied Energy, Elsevier, vol. 95(C), pages 132-138.
    • Handle: RePEc:eee:appene:v:95:y:2012:i:c:p:132-138
    DOI: 10.1016/j.apenergy.2012.02.020
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    References listed on IDEAS

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    1. Arghode, Vaibhav K. & Gupta, Ashwani K., 2011. "Development of high intensity CDC combustor for gas turbine engines," Applied Energy, Elsevier, vol. 88(3), pages 963-973, March.
    2. Khalil, Ahmed E.E. & Gupta, Ashwani K., 2011. "Distributed swirl combustion for gas turbine application," Applied Energy, Elsevier, vol. 88(12), pages 4898-4907.
    3. Arghode, Vaibhav K. & Gupta, Ashwani K. & Bryden, Kenneth M., 2012. "High intensity colorless distributed combustion for ultra low emissions and enhanced performance," Applied Energy, Elsevier, vol. 92(C), pages 822-830.
    4. Arghode, Vaibhav K. & Gupta, Ashwani K., 2011. "Investigation of forward flow distributed combustion for gas turbine application," Applied Energy, Elsevier, vol. 88(1), pages 29-40, January.
    5. Arghode, Vaibhav K. & Gupta, Ashwani K., 2010. "Effect of flow field for colorless distributed combustion (CDC) for gas turbine combustion," Applied Energy, Elsevier, vol. 87(5), pages 1631-1640, May.
    6. Khalil, Ahmed E.E. & Gupta, Ashwani K., 2011. "Swirling distributed combustion for clean energy conversion in gas turbine applications," Applied Energy, Elsevier, vol. 88(11), pages 3685-3693.
    7. Arghode, Vaibhav K. & Gupta, Ashwani K., 2011. "Investigation of reverse flow distributed combustion for gas turbine application," Applied Energy, Elsevier, vol. 88(4), pages 1096-1104, April.
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    Cited by:

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    2. Kruse, Stephan & Kerschgens, Bruno & Berger, Lukas & Varea, Emilien & Pitsch, Heinz, 2015. "Experimental and numerical study of MILD combustion for gas turbine applications," Applied Energy, Elsevier, vol. 148(C), pages 456-465.
    3. Khalil, Ahmed E.E. & Arghode, Vaibhav K. & Gupta, Ashwani K., 2013. "Novel mixing for ultra-high thermal intensity distributed combustion," Applied Energy, Elsevier, vol. 105(C), pages 327-334.
    4. Arghode, Vaibhav K. & Gupta, Ashwani K., 2013. "Role of thermal intensity on operational characteristics of ultra-low emission colorless distributed combustion," Applied Energy, Elsevier, vol. 111(C), pages 930-956.
    5. Enagi, Ibrahim I. & Al-attab, K.A. & Zainal, Z.A., 2018. "Liquid biofuels utilization for gas turbines: A review," Renewable and Sustainable Energy Reviews, Elsevier, vol. 90(C), pages 43-55.
    6. Khalil, Ahmed E.E. & Gupta, Ashwani K., 2013. "Fuel flexible distributed combustion for efficient and clean gas turbine engines," Applied Energy, Elsevier, vol. 109(C), pages 267-274.
    7. Khalil, Ahmed E.E. & Gupta, Ashwani K., 2015. "Toward ultra-low emission distributed combustion with fuel air dilution," Applied Energy, Elsevier, vol. 148(C), pages 187-195.
    8. Li, Mingyu & He, Xiaomin & Zhao, Yuling & Jin, Yi & Ge, Zhenghao & Sun, Yuan, 2017. "Dome structure effects on combustion performance of a trapped vortex combustor," Applied Energy, Elsevier, vol. 208(C), pages 72-82.
    9. Ye, Jingjing & Medwell, Paul R. & Varea, Emilien & Kruse, Stephan & Dally, Bassam B. & Pitsch, Heinz G., 2015. "An experimental study on MILD combustion of prevaporised liquid fuels," Applied Energy, Elsevier, vol. 151(C), pages 93-101.
    10. Khalil, Ahmed E.E. & Gupta, Ashwani K., 2014. "Velocity and turbulence effects on high intensity distributed combustion," Applied Energy, Elsevier, vol. 125(C), pages 1-9.
    11. Khalil, Ahmed E.E. & Gupta, Ashwani K., 2014. "Swirling flowfield for colorless distributed combustion," Applied Energy, Elsevier, vol. 113(C), pages 208-218.
    12. Li, Mingyu & He, Xiaomin & Zhao, Yuling & Jin, Yi & Yao, Kanghong & Ge, Zhenghao, 2018. "Performance enhancement of a trapped-vortex combustor for gas turbine engines using a novel hybrid-atomizer," Applied Energy, Elsevier, vol. 216(C), pages 286-295.
    13. Zhang, R.C. & Fan, W.J. & Shi, Q. & Tan, W.L., 2014. "Combustion and emissions characteristics of dual-channel double-vortex combustion for gas turbine engines," Applied Energy, Elsevier, vol. 130(C), pages 314-325.

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