Research Papers: Gas Turbines: Combustion, Fuels, and Emissions

Bioethanol Combustion in an Industrial Gas Turbine Combustor: Simulations and Experiments

[+] Author and Article Information
Joost L. H. P. Sallevelt

Department of Energy Technology,
University of Twente,
Enschede 7522 NB, Netherlands
e-mail: j.l.h.p.sallevelt@utwente.nl

Artur K. Pozarlik, Gerrit Brem

Department of Energy Technology,
University of Twente,
Enschede 7522 NB, Netherlands

Martin Beran, Lars-Uno Axelsson

OPRA Turbines,
Hengelo 7554 TS, Netherlands

1Corresponding author.

Contributed by the Combustion and Fuels Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received December 11, 2013; final manuscript received January 20, 2014; published online February 18, 2014. Editor: David Wisler.

J. Eng. Gas Turbines Power 136(7), 071501 (Feb 18, 2014) (8 pages) Paper No: GTP-13-1448; doi: 10.1115/1.4026529 History: Received December 11, 2013; Revised January 20, 2014

Combustion tests with bioethanol and diesel as a reference have been performed in OPRA's 2 MWe class OP16 gas turbine combustor. The main purposes of this work are to investigate the combustion quality of ethanol with respect to diesel and to validate the developed CFD model for ethanol spray combustion. The experimental investigation has been conducted in a modified OP16 gas turbine combustor, which is a reverse-flow tubular combustor of the diffusion type. Bioethanol and diesel burning experiments have been performed at atmospheric pressure with a thermal input ranging from 29 to 59 kW. Exhaust gas temperature and emissions (CO, CO2, O2, NOx) were measured at various fuel flow rates while keeping the air flow rate and air temperature constant. In addition, the temperature profile of the combustor liner has been determined by applying thermochromic paint. CFD simulations have been performed with ethanol for five different operating conditions using ANSYS FLUENT. The simulations are based on a 3D RANS code. Fuel droplets representing the fuel spray are tracked throughout the domain while they interact with the gas phase. A liner temperature measurement has been used to account for heat transfer through the flame tube wall. Detailed combustion chemistry is included by using the steady laminar flamelet model. Comparison between diesel and bioethanol burning tests show similar CO emissions, but NOx concentrations are lower for bioethanol. The CFD results for CO2 and O2 are in good agreement, proving the overall integrity of the model. NOx concentrations were found to be in fair agreement, but the model failed to predict CO levels in the exhaust gas. Simulations of the fuel spray suggest that some liner wetting might have occurred. However, this finding could not be clearly confirmed by the test data.

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Balat, M., and Balat, H., 2009, “Recent Trends in Global Production and Utilization of Bio-Ethanol Fuel,” Appl. Energy, 86(11), pp. 2273–2282. [CrossRef]
Lupandin, V., Thamburaj, R., and Nikolayev, A., 2005, “Test Results of the OGT2500 Gas Turbine Engine Running on Alternative Fuels: BioOil, Ethanol, BioDiesel and Crude Oil,” ASME Turbo Expo 2005, Reno, NV, June 6–9, ASME Paper No. GT2005-68488, pp. 421–426. [CrossRef]
Razbin, V., and Coyle, I., 2004, “Emissions Tests on Magellan Aerospace Orenda Corporation, OGT 2500 Gas Turbine,” CETC Energy Technology Centre, Ottawa, Canada, Report No. CETC-O-ACT-04-043-1 (CF).
Moliere, M., Vierling, M., Aboujaib, M., Patil, P., Eranki, A., Campbell, A., Trivedi, R., Nainani, A., Roy, S., and Pandey, N., 2009, “Gas Turbines in Alternative Fuel Applications: Bio-Ethanol Field Test,” ASME Turbo Expo 2009, Orlando, FL, June 8-12, ASME Paper No. GT2009-59047, pp. 341–348. [CrossRef]
Breaux, B. B., and Acharya, S., 2013, “The Effect of Elevated Water Content on Swirl-Stabilized Ethanol/Air Flames,” Fuel, 105, pp. 90–102. [CrossRef]
Laranci, P., Bidini, G., Fantozzi, F., and Desideri, U., 2013, “CFD Analysis of an Annular Micro Gas Turbine Combustion Chamber Fuelled With Liquid Biofuels: Preliminary Results With Bioethanol,” ASME Turbo Expo 2013, San Antonio, TX, June 3–7, ASME Paper No. GT2013-95696. [CrossRef]
Fluent Inc., 2006, Fluent 6.3 User's Guide, Fluent Inc., Lebanon, NH.
Menter, F., 1994, “Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications,” AIAA J., 32(8), pp. 1598–1605. [CrossRef]
Engdar, U., and Klingmann, J., 2002, “Investigation of Two-Equation Turbulence Models Applied to a Confined Axis-Symmetric Swirling Flow,” ASME Pressure Vessels and Piping Conference, Vancouver, BC, Canada, August 5–9, ASME Paper No. PVP2002-1590, pp. 199–206. [CrossRef]
Cengel, Y., 2007, Heat and Mass Transfer: A Practical Approach, 3rd ed., McGraw-Hill, Boston, MA.
Merci, B., Roekaerts, D., and Sadiki, A., 2011, Experiments and Numerical Simulations of Diluted Spray Turbulent Combustion: Proceedings of the 1st International Workshop on Turbulent Spray Combustion, Vol. 17, Springer, New York.
Faeth, G. M., Hsiang, L. P., and Wu, P. K., 1995, “Structure and Breakup Properties of Sprays,” Int. J. Multiphase Flow, 21(S), pp. 99–127. [CrossRef]
Moin, P., and Apte, S. V., 2006, “Large-Eddy Simulation of Realistic Gas Turbine Combustors,” AIAA J., 44(4), pp. 698–708. [CrossRef]
Ranade, V., 2001, Computational Flow Modeling for Chemical Reactor Engineering, Vol. 5, Academic, New York.
Ashgriz, N. E., 2011, Handbook of Atomization and Sprays: Theory and Applications. Springer, New York.
Faeth, G. M., 1977, “Current Status of Droplet and Liquid Combustion,” Prog. Energy Combust. Sci., 3(4), pp. 191–224. [CrossRef]
Tseng, C. C., and Viskanta, R., 2005, “Effect of Radiation Absorption on Fuel Droplet Evaporation,” Combust. Sci. Technol., 177(8), pp. 1511–1542. [CrossRef]
Godsave, G. A. E., 1953, “Burning of Fuel Droplets,” Fourth Symposium (International) on Combustion, Vol. 4, Williams and Wilkins, Baltimore, MD, pp. 818–830.
Lefebvre, A. H., and Ballal, D. R., 2010, Gas Turbine Combustion: Alternative Fuels and Emissions, CRC Press, New York.
El-Shanawany, M. S., and Lefebvre, A. H., 1980, “Airblast Atomization: Effect of Linear Scale on Mean Drop Size,” J. Energy, 4(4), pp. 184–189. [CrossRef]
Liu, H., 1999, Science and Engineering of Droplets: Fundamentals and Applications. Noyes Publications, Norwich, NY.
Lefebvre, A., 1988, Atomization and Sprays, CRC Press, New York.
Röhl, O., and Peters, N., 2009, “A Reduced Mechanism for Ethanol Oxidation,” 4th European Combustion Meeting (ECM 2009), Vienna, Austria, April 14–17, pp. 14–17.
Lefebvre, A. H., 1984, “Flame Radiation in Gas Turbine Combustion Chambers,” Int. J. Heat Mass Transfer, 27(9), pp. 1493–1510. [CrossRef]
Lefebvre, A. H., 1980, “Airblast Atomization,” Progress Energy Combust. Sci., 6(3), pp. 233–261. [CrossRef]
Gepperth, S., Koch, R., and Bauer, H.-J., 2013, “Analysis and Comparison of Primary Droplet Characteristics in the Near Field of a Prefilming Airblast Atomizer,” ASME Turbo Expo, San Antonio, TX, June 3-7, ASME Paper No. GT2013-94033. [CrossRef]
Maqua, C., Castanet, G., Grisch, F., Lemoine, F., Kristyadi, T., and Sazhin, S. S., 2008, “Monodisperse Droplet Heating and Evaporation: Experimental Study and Modelling,” Int. J. Heat Mass Transfer, 51(15–16), pp. 3932–3945. [CrossRef]
Lavieille, P., Lemoine, F., Lavergne, G., and Lebouche, M., 2001, “Evaporating and Combusting Droplet Temperature Measurements Using Two-Color Laser-Induced Fluorescence,” Exp. Fluids, 31(1), pp. 45–55. [CrossRef]
Goldsmith, M., 1955, “The Burning of Single Drops of Fuel in Oxidizing Atmospheres,” Ph.D. dissertation, California Institute of Technology, Pasadena, CA.
Wood, B. J., and Wise, H., 1957, “Measurement of the Burning Constant of a Fuel Drop,” J. Applied Phys., 28(9), pp. 1068–1068. [CrossRef]


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Fig. 1

Scheme of the test rig and the location of sensors

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Fig. 2

Final grid used for the simulations

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Fig. 3

Calculated droplet size distribution curve for the ethanol spray in Case 3

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Fig. 4

Dimensionless liner temperature limits from the paint test and the profile used for CFD

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Fig. 5

Dimensionless temperature field (a) and OH field (b) in Case 3, shown on a cross section of the combustor

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Fig. 6

Measured and calculated dimensionless exhaust gas temperatures as function of the overall equivalence ratio

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Fig. 7

Measured and calculated CO2 concentration as function of the overall equivalence ratio

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Fig. 8

Measured and calculated O2 concentration as function of the overall equivalence ratio

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Fig. 9

Measured dimensionless CO concentration as function of the overall equivalence ratio, normalized to 15% O2

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Fig. 10

Measured and calculated dimensionless NOx concentration as function of the overall equivalence ratio

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Fig. 11

Calculated droplet diameter as function of the droplet travel time in Case 3

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Fig. 12

Calculated square droplet diameter as function of the droplet travel time in Case 3

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Fig. 13

Image of the ethanol flame without (a) and with (b) CH*-filter in front of the camera




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