Flow and Combustion Characteristics of Wave Rotor–Trapped Vortex Combustor System
Author:
Kang Yiqin, Wang Chenlu, Fang Gangyi, Xing FeiORCID, Chan Shining
Abstract
Breaking through the limit of conventional compression and combustion, wave rotor and trapped vortex combustors are able to improve the thermal efficiency of gas turbines. Detailed two-dimensional numerical simulations based on Ansys Fluent were performed to study the flow and combustion characteristics of the wave rotor–trapped vortex combustor system. The calculated pressure characteristics agree with the experimental results giving a relative error for average pressure of 0.189% at Port 2 and of 0.672% at Port 4. The flow stratification characteristics and the periodic fluctuations were found to benefit the zonal organized combustion in the trapped vortex combustor. For the six cases of different rotor speeds, as the rotor speed increased, the oxygen mass fraction at the combustor inlet rose and then fell. The proportion of exhaust gas recirculation fell at first and then rose, and the combustion mode became unstable with the dominant frequencies of the fluctuations increasing.
Subject
Energy (miscellaneous),Energy Engineering and Power Technology,Renewable Energy, Sustainability and the Environment,Electrical and Electronic Engineering,Control and Optimization,Engineering (miscellaneous),Building and Construction
Reference22 articles.
1. Hsu, K., Gross, L., Trump, D., and Roquemore, W. (1995, January 9–12). Performance of a trapped-vortex combustor. Proceedings of the 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. 2. Katta, V., and Roquemore, W. (1996, January 1–3). Numerical studies of trapped-vortex combustor. Proceedings of the 32nd Joint Propulsion Conference and Exhibit, Lake Buena Vista, FL, USA. 3. Katta, V., and Roquemore, W. (1997, January 6–9). Study on trapped-vortex combustor-effect of injection on dynamics of non-reacting and reacting flows in a cavity. Proceedings of the 33rd Joint Propulsion Conference and Exhibit, Washington, DC, USA. 4. Meyer, T., Brown, M., Fonov, S., Goss, L., Gord, J., Shouse, D., Belovich, V., Roquemore, W., Cooper, C., and Kim, E. (2002, January 7–10). Optical diagnostics and numerical characterization of a trapped-vortex combustor. Proceedings of the 38th AIAA/ASME/SAE /ASEE Joint Propulsion Conference & Exhibit, Indianapolis, IN, USA. 5. Burrus, D.L., Johnson, A.W., Roquemore, W.M., and Shouse, D.T. (2009, January 4). Performance assessment of a prototype trapped vortex combustor concept for gas turbine application. Proceedings of the ASME Turbo Expo 2001: Power for Land, Sea, and Air, New Orleans, LA, USA.
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