Affiliation:
1. Key Laboratory of Aero-Engine Thermal Environment and Structure, Ministry of Industry and Information Technology, Nanjing University of Aeronautics and Astronautics, 29 Yudao St., Nanjing 210016, China
2. School of National Defense Engineering, Army Engineering University of PLA, 88 Biaoying Rd., Nanjing, 210007 Jiangsu, China
Abstract
The reverse-flow combustor is extensively applied in small engines due to its compact structure. The cold-state flow characteristics, the ignition process, and flame chemiluminescence characteristics of the reserve-flow combustor were investigated experimentally. Using the particle imaging velocimeter, the cold-state time-averaged flow fields at three different total pressure loss coefficients
are examined. The ignition processes of the combustor, as well as flame characteristics during stable combustion at different equivalent ratios
, are analyzed based on flame chemiluminescence imaging when
is 3%. As
increases from 1% to 5%, the flow field of the combustor remains almost unchanged while the flow velocity increases. For
=3%, the ignition time
drops from 26 ms to 16 ms with an increase of
. In addition, the ignition performance is enhanced. Proportions of the T2 phase (quasi-stable phase) are 73%, 68%, and 66%, respectively, suggesting that the quasi-stable phase is the key to successful ignition. As
increases, the flame becomes thinner and shorter. Furthermore, standard deviations of continuous image areas of
and
drop from 0.0143 and 0.0132 to 0.0115 and 0.0109, respectively, which indicates the enhancement of combustion stability. According to the brightness distributions of
and
along the axial direction of the combustor at different equivalent ratios, the production of
is significantly affected by the temperature. It can be adopted as an important sign of heat release during combustion.
Funder
National Science and Technology Major Project