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Keywords: high pressure test rigClose
Fabian Hampp, James Dakshina Gounder, Holger Ax, Rainer Lükerath, Oliver Lammel, Matthias Hase, Bertram Janus
Proc. ASME. GT2020, Volume 4A: Combustion, Fuels, and Emissions, V04AT04A033, September 21–25, 2020
Paper No: GT2020-14619
... models. Keywords: high momentum jet flame, liquid fuel, gas tur- bine combustion, high pressure test rig, laser diagnostics, fuel and load flexibility, droplet sizing Corresponding author: firstname.lastname@example.org INTRODUCTION Gas turbines (GT) continue to play a key role in future power generation markets...
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...
Proc. ASME. GT2019, Volume 4B: Combustion, Fuels, and Emissions, V04BT04A013, June 17–21, 2019
Paper No: GT2019-91177
... configuration. All measurements were carried out at the high pressure combus- tion test rig (HBK-S) at the German Aerospace Center (DLR) in Stuttgart. The generic single nozzle model combustor has been oper- ated in a high-pressure test rig with large optical access in order to gain a detailed understanding...
Proc. ASME. GT2012, Volume 2: Combustion, Fuels and Emissions, Parts A and B, 737-748, June 11–15, 2012
Paper No: GT2012-69006
... temperature gas turbine operational flexibility part load pilot burner fuel staging high pressure test rig laser diagnostics PART-LOAD OPERATION OF A PILOTED FLOX® COMBUSTION SYSTEM Tim Roediger, Oliver Lammel , Manfred Aigner German Aerospace Center (DLR), Institute of Combustion Technology...
Rainer Lu¨ckerath, Oliver Lammel, Michael Sto¨hr, Isaac Boxx, Ulrich Stopper, Wolfgang Meier, Bertram Janus, Bernhard Wegner
Proc. ASME. GT2011, Volume 2: Combustion, Fuels and Emissions, Parts A and B, 725-736, June 6–10, 2011
Paper No: GT2011-45790
...-emission, and reliable combustion system a better understanding of the flow field – flame interaction and the flame stabilization mechanism is necessary. For this purpose, a down-scaled staged can combustion system provided with an optical combustion chamber was investigated in a high pressure test rig...
Oliver Lammel, Harald Schu¨tz, Guido Schmitz, Rainer Lu¨ckerath, Michael Sto¨hr, Berthold Noll, Manfred Aigner, Matthias Hase, Werner Krebs
Proc. ASME. GT2010, Volume 2: Combustion, Fuels and Emissions, Parts A and B, 1069-1081, June 14–18, 2010
Paper No: GT2010-23385
... combustion, gas turbine combustion, high temperature gas turbine, fuel flexibility, hydrogen combustion, numerical simulation, high pressure test rig, laser diagnostics NOMENCLATURE Nozzle diameter Ønozzle [mm] Nozzle exit velocity vnozzle [m/s] Pressure p [bar] Air equivalence ratio local local global...
Proc. ASME. GT2004, Volume 1: Turbo Expo 2004, 121-128, June 14–17, 2004
Paper No: GT2004-53274
... ,K 5 1 % L" 2 U68 7 K L H " T 1 5 O gas turbine combustion high pressure test rig low BTU fuels In 1991 ENEL started a research program on gas turbine problems, an important activity which contributed to the realisation of the ENEL Sesta Gas Turbine Test...