For lean burn combustor development in low emission aero-engines, the pilot stage of the fuel injector plays a key role with respect to stability, operability, NOx emissions, and smoke production. Therefore it is of considerable interest to characterize the pilot module in terms of pilot zone mixing, fuel placement, flow field, and interaction with the main stage. This contribution focuses on the investigation of soot formation during pilot-only operation. Optical test methods were applied in an optically accessible single sector rig at engine idle conditions. Using planar laser-induced incandescence (LII), the distribution of soot and its dependence on air/fuel ratio, as well as geometric injector parameters, was studied. The data shows that below a certain air/fuel ratio, an increase of soot production occurs. This is in agreement with smoke number measurements in a standard single sector flame tube rig without optical access. Reaction zones were identified using chemiluminescence of OH radicals. In addition, the injector flow field was investigated with PIV. A hypothesis regarding the mechanism of pilot smoke formation was made based on these findings. This along with further investigations will form the basis for developing strategies for smoke improvement at elevated pilot-only conditions.
Characterization of Lean Burn Module Air Blast Pilot Injector With Laser Techniques
Contributed by the Combustion and Fuels Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received July 16, 2013; final manuscript received July 24, 2013; published online September 23, 2013. Editor: David Wisler.
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Meier, U., Freitag, S., Heinze, J., Lange, L., Magens, E., Schroll, M., Willert, C., Hassa, C., Bagchi, I. K., Lazik, W., and Whiteman, M. (September 23, 2013). "Characterization of Lean Burn Module Air Blast Pilot Injector With Laser Techniques." ASME. J. Eng. Gas Turbines Power. December 2013; 135(12): 121508. https://doi.org/10.1115/1.4025148
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