| contributor author | Roediger, Tim | |
| contributor author | Lammel, Oliver | |
| contributor author | Aigner, Manfred | |
| contributor author | Beck, Christian | |
| contributor author | Krebs, Werner | |
| date accessioned | 2017-05-09T00:58:07Z | |
| date available | 2017-05-09T00:58:07Z | |
| date issued | 2013 | |
| identifier issn | 1528-8919 | |
| identifier other | gtp_135_3_031503.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/151583 | |
| description abstract | A large operational envelope is a key requirement for modern gas turbines. Fuel staging is used here to improve the part load performance of an enhanced FLOXآ® type combustor. A swirlstabilized pilot stage is integrated in the FLOXآ® burner and the results of high pressure labscale experiments at system relevant conditions are presented. The operational envelope of the piloted system could be extended by approximately 10%. Pressure scaling and variations of air preheat temperature and jet velocity describe fundamental characteristics of the piloted system. OH* chemiluminescence imaging is used to investigate flame shapes and the effect of the interacting flames. Emissions and pressure pulsations define limits, and optimum operation conditions of the combustor and show the influence of part load relevant parameters. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Part Load Operation of a Piloted FLOXآ® Combustion System | |
| type | Journal Paper | |
| journal volume | 135 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4007754 | |
| journal fristpage | 31503 | |
| journal lastpage | 31503 | |
| identifier eissn | 0742-4795 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 003 | |
| contenttype | Fulltext | |
