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Numerical investigation of combustion characteristics for hydrogen mixed fuel in a can-type model of the gas turbine combustor
Affiliation:1. Department of Mechanical Engineering, Changwon National University, South Korea;2. Department of Smart Manufacturing Engineering, Changwon National University, South Korea;1. College of Transportation, Shandong University of Science and Technology, Qingdao, Shandong Province, P.R.China;2. Department of Mechanical and Energy Engineering, Indiana University - Purdue University Indianapolis, USA;3. Department of Materials Convergence and System Engineering, Changwon National University, Republic of Korea;4. Department of Engineering Technology, Indiana University - Purdue University Indianapolis, USA;1. School of Mechanical Engineering, Tongji University, 4800 Cao''an Road, Shanghai, 201804, China;2. Research and Development Department, ENN Energy Power Technology (Shanghai) Co. Ltd, 600 Xinyuan South Road, Shanghai, 201499, China;3. School of Mechanical and Aerospace Engineering, Nanyang Technological University, 50 Nanyang Avenue, Singapore, 639798, Singapore;1. School of Energy, Power and Mechanical Engineering, North China Electric Power University, Beijing 102206, China;2. School of Intelligent Manufacturing, Weifang University of Science and Technology, Weifang City 262700, Shandong Province, China;1. Department of Mechanical Engineering, MIT, Cambridge, MA, USA;2. Department of Mechanical Engineering, KFUPM, Dhahran, Saudi Arabia
Abstract:Numerical simulations are performed to analyze the combustion characteristics of propane fuel mixed with different amounts of hydrogen in a can-type combustor. The volume fraction of the hydrogen fuel varies from 0% to 100% in the fuel mixture. The results indicate that the hydrogen enrichment of the fuel significantly affects the flow structure, mixture fraction, and combustion characteristics. An increase in the volume fraction of hydrogen significantly affects the mean mixture fraction distribution, promotes combustion, and increases the flame temperature and the width of the flammable range within the combustor. Therefore, the degree of temperature uniformity at the outlet of the combustor increases with hydrogen enrichment, corresponding to an increase of 49.64% in the uniformity factor. The hydrogen enriched fuel can also reduce the emissions of CO and CO2, owing to the reduced amount of carbonaceous fuel.
Keywords:Numerical simulation  Combustion  Can-type combustor  Hydrogen fuel  Gas turbine
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