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Keywords: FLOX®
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Proceedings Papers

Proc. ASME. GT2021, Volume 3A: Combustion, Fuels, and Emissions, V03AT04A031, June 7–11, 2021
Paper No: GT2021-59029
...Abstract Abstract Increased global demand for cleaner energy production and growing concern about using fossil fuels have urged many researchers to focus their work on developing more efficient and flexible combustion processes. In this regard, a FLOX ® -based liquid fuel single-nozzle burner...
Proceedings Papers

Proc. ASME. GT2020, Volume 4B: Combustion, Fuels, and Emissions, V04BT04A002, September 21–25, 2020
Paper No: GT2020-15231
... the mixing duct sections of high momentum jet stabilized combustors for gas turbines, e.g. high axial air velocities without swirl generation and high preheat temperatures. High momentum jet stabilized combustors based on the FLOX® burner concept are used successfully in gas turbines due to its fuel and load...
Proceedings Papers

Proc. ASME. GT2020, Volume 4B: Combustion, Fuels, and Emissions, V04BT04A016, September 21–25, 2020
Paper No: GT2020-15556
..., this paper studies the influence of different biogas mixtures compared to natural gas on the combustion in a FLOX ® -based six nozzle combustor. The single staged combustor is suitable for the use in a micro gas turbine (MGT) based combined heat and power (CHP) system with an electrical power output of 3 kW...
Proceedings Papers

Proc. ASME. GT2020, Volume 4A: Combustion, Fuels, and Emissions, V04AT04A028, September 21–25, 2020
Paper No: GT2020-14564
...Abstract Abstract As an alternative to the commonly used swirl burners in micro gas turbines (MGT), the FLOX ® -based combustion concept promises great potential for the nitric oxide emission reduction and increased fuel flexibility. Previous research on FLOX ® -based MGT combustors mainly...
Proceedings Papers

Proc. ASME. GT2019, Volume 4B: Combustion, Fuels, and Emissions, V04BT04A023, June 17–21, 2019
Paper No: GT2019-91377
... high pressure test rig. The generic burner rep- resents a full scale single nozzle of a high temperature FLOX® gas turbine combustor including a pilot stage. 1D-laser Raman measurements were performed on both an unpiloted and a piloted flame and evaluated on a single shot basis revealing...
Proceedings Papers

Proc. ASME. GT2019, Volume 4B: Combustion, Fuels, and Emissions, V04BT04A013, June 17–21, 2019
Paper No: GT2019-91177
..., that the evaporation of most of the liquid fuel takes place near the hot gas region, as a large proportion of droplets are car- ried far downstream of the nozzle by the high momentum jet. Keywords: high momentum jet flame, FLOX®, gas turbine combustion, fuel flexibility, liquid fuel, spray flames, high pres- sure test...
Proceedings Papers

Proc. ASME. GT2012, Volume 2: Combustion, Fuels and Emissions, Parts A and B, 701-712, June 11–15, 2012
Paper No: GT2012-68997
... Presented in this paper is a novel gas turbine combustor: EZEE ® based upon the FLOX ® combustion technology. The specific feature of this combustor is the ability to modulate the power density P A for natural gas (NG) combustion on a high thermal power level between P A = 13.3 MW/m 2...
Proceedings Papers

Proc. ASME. GT2012, Volume 2: Combustion, Fuels and Emissions, Parts A and B, 737-748, June 11–15, 2012
Paper No: GT2012-69006
... 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 FLOX ® type combustor. A swirl-stabilized pilot stage is integrated in the FLOX ® burner and the results of high pressure lab-scale...
Proceedings Papers

Proc. ASME. GT2011, Volume 2: Combustion, Fuels and Emissions, Parts A and B, 117-127, June 6–10, 2011
Paper No: GT2011-45111
... were configured to enable flame stabilization by recirculation of hot combustion products. The geometry of the rectangular confinement and an off-center positioning of the jet nozzle were chosen to resemble one burner nozzle of a FLOX ® -based combustor. The off-center jet arrangement caused...
Proceedings Papers

Proc. ASME. GT2010, Volume 2: Combustion, Fuels and Emissions, Parts A and B, 1069-1081, June 14–18, 2010
Paper No: GT2010-23385
... 1 Copyright © 2010 by ASME Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air GT2010 June 14-18, 2010, Glasgow, UK GT2010-23385 FLOX® COMBUSTION AT HIGH POWER DENSITY AND HIGH FLAME TEMPERATURES Oliver Lammel, Harald Schütz, Guido Schmitz, Rainer Lückerath, Michael Stöhr, Berthold...
Proceedings Papers

Proc. ASME. GT2007, Volume 2: Turbo Expo 2007, 241-249, May 14–17, 2007
Paper No: GT2007-27337
... 10 03 2009 In Flameless Oxidation (FLOX ® ) the combustion is distributed over a large volume by a high internal flue gas recirculation. This technology has been successfully used for many years in technical furnaces under atmospheric conditions with very low NO x emissions...