Low calorific value fuelled distributed combustion with swirl for gas turbine applications

Distributed combustion offers significant performance improvement with near zero emissions for industrial gas turbine applications. Our efforts to further develop zero emission distributed combustion are explored here by utilizing swirl to the flow. The beneficial aspects of distributed swirl combustion using a cylindrical geometry combustor has shown low emissions of NO and CO, and significantly improved pattern factor using methane as the fuel at high thermal intensity. Biofuels, syngas and landfill gases offer superior use in gas turbine combustion. However, they are characterized by their low calorific value. Results are presented here from the distributed swirl combustor with simulated low calorific value fuels with defined mixture of methane diluted with nitrogen. The calorific value of the fuel obtained provided comparable adiabatic flame temperature and flame speed to those characteristic of low to medium calorific value syngas fuels. The results are compared with the methane fueled combustor. Experimental results from the distributed swirl combustor using methane fuel at an equivalence ratio of 0.6 and a heat release intensity of 27MW/m3-atm showed low levels of NO (∼9PPM) and low CO (∼21PPM) under non-premixed conditions. Novel Premixed Combustion design demonstrated 4PPM of NO and 11PPM of CO. In contrast methane diluted with nitrogen resulted in a dramatic decrease of NO emissions (30–50%), to provide NO emission of 7PPM (for non-premixed case) and 2.8PPM (premixed case), at the same conditions, with minimal impact on CO for all the conditions examined here. The combustor provided no instability or flame flashback at higher fuel flow rates (to maintain the same thermal load as with methane fuel). Results obtained with different calorific value fuels on the emissions of NO and CO, lean stability limit and OH* chemiluminescence are presented. The results showed favorable operation of the distributed swirl combustor for applications with both high and low calorific value fuels, such as, methane, synfuel and landfill gases to power the gas turbines without any combustor modifications.

[1]  A. Gupta,et al.  Distributed swirl combustion for gas turbine application , 2011 .

[2]  Dimosthenis Trimis,et al.  Combustion of Low Calorific Gases from Landfills and Waste Pyrolysis Using Porous Medium Burner Technology , 2006 .

[3]  Norbert Peters,et al.  Characteristics of the reaction zone in a combustor operating at mild combustion , 2001 .

[4]  A. Gupta,et al.  High Temperature Air Combustion: From Energy Conservation to Pollution Reduction , 2002 .

[5]  Min Chul Lee,et al.  Gas turbine combustion performance test of hydrogen and carbon monoxide synthetic gas , 2010 .

[6]  Gabriele Comodi,et al.  Energy production from landfill biogas: An italian case , 2011 .

[7]  Vaibhav K. Arghode,et al.  Development of high intensity CDC combustor for gas turbine engines , 2011 .

[8]  V. K. Arghode,et al.  Novel mixing for ultra-high thermal intensity distributed combustion , 2013 .

[9]  Zainal Alimuddin Zainal,et al.  Design and performance of a pressurized cyclone combustor (PCC) for high and low heating value gas combustion , 2011 .

[10]  W. T. Tsai,et al.  BIOENERGY FROM LANDFILL GAS (LFG) IN TAIWAN , 2007 .

[11]  Effect of Swirl on Flow Dynamics in Unconfined and Confined Gaseous Fuel Flames , 2004 .

[12]  Vaibhav K. Arghode,et al.  Effect of flow field for colorless distributed combustion (CDC) for gas turbine combustion , 2010 .

[13]  A. Gupta,et al.  Thermal Characteristics of Gaseous Fuel Flames Using High Temperature Air , 2004 .

[14]  Fokion N. Egolfopoulos,et al.  FUNDAMENTAL AND ENVIRONMENTAL ASPECTS OF LANDFILL GAS UTILIZATION FOR POWER GENERATION , 2001 .

[15]  R. Stone,et al.  Correlations for the Laminar-Burning Velocity of Methane/Diluent/Air Mixtures Obtained in Free-Fall Experiments , 1998 .

[16]  W. Meier,et al.  Investigations of a SYNGAS-FIRED Gas Turbine Model Combustor by Planar Laser Techniques , 2006 .

[17]  A. Lefebvre Gas Turbine Combustion , 1983 .

[18]  S. Correa A Review of NOx Formation Under Gas-Turbine Combustion Conditions , 1993 .

[19]  Richard A. Yetter,et al.  Asymmetric whirl combustion: A new low NOx approach , 2000 .

[20]  J. Wunning,et al.  Flameless oxidation to reduce thermal no-formation , 1997 .

[21]  Tim Lieuwen,et al.  Laboratory Investigations of Low-Swirl Injectors Operating With Syngases , 2008 .

[22]  Bradley T. Zigler,et al.  An experimental investigation of the ignition properties of hydrogen and carbon monoxide mixtures for syngas turbine applications , 2007 .

[23]  A. Gupta,et al.  Swirling distributed combustion for clean energy conversion in gas turbine applications , 2011 .

[24]  Vaibhav K. Arghode,et al.  Investigation of forward flow distributed combustion for gas turbine application , 2011 .

[25]  Arthur H. Lefebvre,et al.  The Role of Fuel Preparation in Low-Emission Combustion , 1995 .