Affiliation:
1. Department of Fuel and Energy, University of Leeds
Abstract
Experimental combustion and NOx emissions results are summarized for a range of jet shear layer combustion systems that have rapid fuel and air mixing, short intense flames, a high turn-down ratio and low NOx characteristics. Two burner sizes of 76 and 140 mm are investigated for propane and natural gas. Three jet shear layer burners are compared with axial and radial swirlers. The combustion techniques were developed for application to low NOx combustion systems for industrial gas turbines, where NOx emissions as low as 10 ppm at 15 per cent oxygen have been demonstrated. It is shown that at one bar pressure, gas turbine combustors and high-intensity burners operate at similar air flow, blockage and pressure loss conditions.
Subject
Mechanical Engineering,Energy Engineering and Power Technology
Reference22 articles.
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2. Al Dabbagh N. A., Andrews G. E. The influence of flame stabiliser pressure loss on mixing, combustion performance and flame stability. Sixth International Symposium on Air breathing engines, Paris, 1983, pp. 172–181 (AIAA, Washington).
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