The experimental unit and correction method for estimation of performance of fuel distribution based on planar laser induced fluorescence (PLIF) method were established
and the correction method was validated. The comparisons between results of PLIF method and planar laser scattering (PLS) method indicate that
the results of PLS method overrepresents droplet concentration for droplets less than 50μm and PLIF is suitable for fuel distribution measurement. To make sure the quality of machining and performances of the atomizers
the distributions of droplets were evaluated comprehensively by PLIF method in terms of spray cone angle
non-uniformity of circumferential distribution and patternation index
and then
the results of eccentricity and grooves of different sizes for the poor droplets distribution show that
the factors for non-uniformity include the roughness of internal flow wall
roundness of nozzle and coaxiality of parts. The opening processes of spray cones in the direction of ejection were visualized by PLIF method at pressure differential of 0.14
0.25 and 2.5 MPa
respectively
and the droplets dispersed from annulus to round in cross-sectional plane with development of the spray. Furthermore
the rate of droplets dispersion increased with the growing pressure differential of fuel.
Experiment of swirled air effect on spray characteristic of double-line pressure-swirl atomizer
Measurement and analysis of atomization characteristics of oxygenated bio-fuel
基于自适应MOMEDA滚动轴承故障特征提取方法
基于三维接触摩擦单元的套齿连接解析建模研究
考虑多源不确定性的复合材料风扇叶片高周疲劳失效概率评估
Related Author
ZHOU Bing
JI Hong-hu
ZHANG Bao-cheng
ZHANG Chi
FU Qi-hui
RONG Long
LIN Yu-zhen
XU Quan-hong
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
College of Energy and Power Engineering, Shenyang University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energh and Power Engineering, Beijing University of Aeronautics and Astronautics
School of Biological Science and Medical Engineering, Beijing University of Aeronautics and Astronautics