Pollution emissions from single swirl-can combustor modules at parametric test conditions
暂无分享,去创建一个
Exhaust pollutant emissions were measured from single swirl-can combustor modules operating over a pressure range of 69 to 276 N/sq cm (100 to 400 psia), over a fuel-air ratio range of 0.01 to 0.04, at an inlet air temperature of 733 K (860 F), and at a constant reference velocity of 23.2 m/sec). Many swirl-can module designs were evaluated; the 11 most promising designs exhibited oxides of nitrogen emission levels lower than that from conventional gas-turbine combustors. Although these single module test results are not necessarily indicative of the performance characteristics of a large array of modules, the results are very promixing and offer a number of module designs that should be tested in a full combustor.
[1] Climatic Impact Assessment Program , 1975 .
[2] R. Jones,et al. Parametric test results of a swirl-can combustor , 1973 .
[3] R. E. Jones,et al. Advanced Technology for Reducing Aircraft Engine Pollution , 1974 .
[4] A. J. Juhasz,et al. Performance of a swirl-can primary combustor to outlet temperatures of 3600 F /2256 K/ , 1970 .
[5] A. M. Trout,et al. Performance of a swirl-can combustor at idle conditions , 1972 .