1. Characterizing particulate matter emissions in an aviation kerosene-fueled model combustor at elevated pressures and temperatures
- Author
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Chi Zhang, Xin Hui, Yuzhen Lin, Xiaotong Mi, Hukam C. Mongia, Longfei Chen, and Chih-Jen Sung
- Subjects
Materials science ,020209 energy ,General Chemical Engineering ,Organic Chemistry ,Analytical chemistry ,Energy Engineering and Power Technology ,02 engineering and technology ,Particulates ,Atmospheric temperature range ,Combustion ,medicine.disease_cause ,Soot ,Fuel Technology ,020401 chemical engineering ,Particle-size distribution ,0202 electrical engineering, electronic engineering, information engineering ,Combustor ,medicine ,Particle ,Particle size ,0204 chemical engineering - Abstract
The present study investigated the characteristics of particulate matter (PM) emissions in a single-dome, Rich-Quench-Lean, model combustor under different operating conditions typical for aero-engines, with special emphasis on identifying the individual effects of pressure, temperature, and equivalence ratio on PM emissions in aero-combustors. Results showed that the number-based particle size distribution was shifted from the nucleation mode ( 60 nm for the different pressure cases investigated. Regarding the influence of combustion temperature, a non-monotonic response of particle geometric mean diameter with increasing primary zone average temperature was found in that particle size increased and decreased in the temperature range below and above 2270 K respectively. This non-monotonic response with temperature variation is likely caused by the competition between soot growth rate and oxidation rate. It is postulated that the increasing trend of particle size is a result of more carbonaceous particles formed under elevated temperatures providing surface areas available for the condensation of organic compounds, while the soot oxidation rate eventually overtakes at higher temperatures leading to the observed decreasing trend.
- Published
- 2019
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