| description abstract | Abstract. A multi-injector combustion system consisting of seven premix/micromix injectors is studied in the high-pressure optically accessible combustion rig (OACR), which is commissioned for the first time at the National Research Council Canada (NRC). The clustered design mimics the packaging expected in industrial applications where hundreds of such injectors will be needed to provide the desired power output. The pressure vessel and test facility allow for an investigation of the combustion system up to 922 K and 20 bar inlet temperature and pressure, respectively. It provides conditions closer to gas turbine operation to investigate the impact of pressure on micromixed flames and provide pressure scaling, such as for emissions and flame characteristics, to be used for extrapolating to full gas turbine load. Three of the five optical windows of the OACR are used in the current experimental configuration to monitor the flames with direct imaging and perform nonintrusive OH-planar laser-induced fluorescence (OH-PLIF), for the first time in this rig. The current work focuses on the combustion of pure hydrogen in micromixed flames to commission the added hydrogen capabilities of the test cell and the laser diagnostics. Globally-lean hydrogen flames operating at the same preheated air temperature, target flame temperature, and pressure drop across the injectors are investigated at pressures of 2.5, 5, 7, 10, and 15 bar to isolate the impact of pressure on combustion. Increasing pressure is found to significantly deteriorate the quality of raw OH-PLIF images, down to a mean signal-to-noise ratio (SNR) of 1.7 at 15 bar. Spatial filtering corrects for horizontal intensity striations believed to be caused by combustor cooling in the high-pressure environment, before a qualitative exponential relationship is used to correct for laser attenuation in the high-pressure environment and through multiple flames. The laser sheet slicing across the centerline axis of three inline nozzles mostly captures the main flame body in the turbulent wake of the micromix jets of the complex tridimensional structures. Little changes in flame structures are observed with increasing pressure, with the 15 bar condition moving slightly downstream from the nozzle exit. The results suggest that injector concept screening at lower pressure while maintaining the other operating conditions similar may be possible before pursuing additional elevated-pressure testing. | |
