Rackwitz, L. and Heinze, J. and Becker, J. (2004) Development of a piloted lean burner for an aero-engine combustor: influence of liquid fuel placement on pollutant emissions. In: 19th ilass Europe'04, 19, pp. 25-31. Alpha Graphics Nottingham. 19. Int. Conf. on Liquid Atomization and Spray Systems.
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Detailed investigations of different liquid fuel injectors for the main stage of a lean burnner were carried out. The main injector follows a jet in cross flow arrangement. Two other concepts with a prefilmer and trailing edge injection were additionally derived. It was found that the fuel split between main and pilot injector has a significant influence on flame structure. Low NOx emissions are observed with main burners with a low fuel penetration into the central recirculation zone.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Development of a piloted lean burner for an aero-engine combustor: influence of liquid fuel placement on pollutant emissions|
|Journal or Publication Title:||19th ilass Europe'04|
|Page Range:||pp. 25-31|
|Publisher:||Alpha Graphics Nottingham|
|Series Name:||ILASS Europe|
|Keywords:||Atomization, fuel placement, aeroengine, combustor|
|Event Title:||19. Int. Conf. on Liquid Atomization and Spray Systems|
|Organizer:||Institute for Liquid Atomization and Spray Systems-Europe (ILASS-Europe)|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Propulsion Systems|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ER - Engine Research|
|DLR - Research theme (Project):||L - Combustion Chamber Technologies|
|Institutes and Institutions:||Institute of Propulsion Technology|
|Deposited By:||Dr.-Ing. Christoph Hassa|
|Deposited On:||16 Sep 2005|
|Last Modified:||06 Jan 2010 13:36|
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