Trapped vortex combustor (TVC) is a relatively new concept, having potential application in gas turbine engines. In this work, an attempt has been made to characterize the 2D twin cavity TVC experimentally in terms of its visible flame length, pollutant emission level, and exit temperature profile. Besides this, numerical results are also discussed to explain certain intricacies in flow and flame characteristics. Experimental results reveal that visible flame length value is sensitive to mainstream Reynolds number (Rems), primary (cavity) air velocity (Vp), and cavity equivalence ratio (Φc). For a particular Rems and Φc, an increase in Vp results in longer flame length; whereas, flame length gets shortened at higher mainstream Reynolds number cases. Numerical studies indicate that shortening of flame length at higher Rems cases is caused due to quenching of flame at the shear layer by the incoming flow. An attempt has been made to correlate flame length data with the operating parameters and Damkohler number (Da); Da takes care of flame quenching effects. Moreover, it is also brought out that the emission profile at the combustor exit is dependent on primary air velocity, mainstream Reynolds number, and cavity equivalence ratio. Emission studies indicate that higher primary air velocity cases make the carbon monoxide (CO) and unburned hydrocarbon (UHC) emission levels to lower values. Reduction in emission level is caused mainly due to the flame merging effects. Besides this, the influence of cavity flame merging on the exit temperature profile uniformity is also brought out. This study reveals that merging of cavity flames is essential for the optimized operation of a 2D trapped vortex combustor.
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July 2017
Research-Article
Combustion Characteristics of a Two-Dimensional Twin Cavity Trapped Vortex Combustor
P. K. Ezhil Kumar,
P. K. Ezhil Kumar
Combustion Laboratory,
Department of Aerospace Engineering,
Indian Institute of Technology,
Kanpur 208016, India
e-mail: [email protected]
Department of Aerospace Engineering,
Indian Institute of Technology,
Kanpur 208016, India
e-mail: [email protected]
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D. P. Mishra
D. P. Mishra
Combustion Laboratory,
Department of Aerospace Engineering,
Indian Institute of Technology,
Kanpur 208016, India
e-mail: [email protected]
Department of Aerospace Engineering,
Indian Institute of Technology,
Kanpur 208016, India
e-mail: [email protected]
Search for other works by this author on:
P. K. Ezhil Kumar
Combustion Laboratory,
Department of Aerospace Engineering,
Indian Institute of Technology,
Kanpur 208016, India
e-mail: [email protected]
Department of Aerospace Engineering,
Indian Institute of Technology,
Kanpur 208016, India
e-mail: [email protected]
D. P. Mishra
Combustion Laboratory,
Department of Aerospace Engineering,
Indian Institute of Technology,
Kanpur 208016, India
e-mail: [email protected]
Department of Aerospace Engineering,
Indian Institute of Technology,
Kanpur 208016, India
e-mail: [email protected]
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 15, 2014; final manuscript received December 16, 2016; published online March 7, 2017. Assoc. Editor: Joseph Zelina.
J. Eng. Gas Turbines Power. Jul 2017, 139(7): 071504 (10 pages)
Published Online: March 7, 2017
Article history
Received:
December 15, 2014
Revised:
December 16, 2016
Citation
Ezhil Kumar, P. K., and Mishra, D. P. (March 7, 2017). "Combustion Characteristics of a Two-Dimensional Twin Cavity Trapped Vortex Combustor." ASME. J. Eng. Gas Turbines Power. July 2017; 139(7): 071504. https://doi.org/10.1115/1.4035739
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