FACTORS INFLUENCING THE EFFECTIVE SPRAY CONE ANGLE OF PRESSURE-SWIRL ATOMIZERS

被引:76
作者
CHEN, SK [1 ]
LEFEBVRE, AH [1 ]
ROLLBUHLER, J [1 ]
机构
[1] NASA,LEWIS RES CTR,CLEVELAND,OH 44135
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 1992年 / 114卷 / 01期
关键词
D O I
10.1115/1.2906313
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The spray cone angles produced by several simplex pressure-swirl nozzles are examined using three liquids whose viscosities range from 0.001 to 0.012 kg/ms (1 to 12 cp). Measurements of both the visible spray cone angle and the effective spray cone angle are carried out over wide ranges of injection pressure and for five different values of the discharge orifice length/diameter ratio. The influence of the number of swirl chamber feed slots on spray cone angle is also examined. The results show that the spray cone angle widens with increase in injection pressure but is reduced by increases in liquid viscosity and/or discharge orifice length/diameter ratio. Variation in the number of swirl chamber feed slots between one and three has little effect on the effective spray cone angle.
引用
收藏
页码:97 / 103
页数:7
相关论文
共 12 条
[1]  
[Anonymous], 1983, GAS TURBINE COMBUSTI
[2]  
Carlisle D.R., 1955, P I MECH ENG, V169, P101
[3]  
DFECORSO SM, 1957, T ASME, V79, P607
[4]  
Giffen E, 1950, 19505 MOT IND RES AS
[5]  
Giffen E, 1953, ATOMIZATION LIQUID F
[6]  
Lefebvre A. H., 1987, ATOMIZ SPRAY TECHNOL, V3, P37
[7]  
Lefebvre AH, 2017, ATOMIZATION SPRAY
[8]   FUEL DISTRIBUTIONS FROM PRESSURE-SWIRL ATOMIZERS [J].
ORTMAN, J ;
LEFEBVRE, AH .
JOURNAL OF PROPULSION AND POWER, 1985, 1 (01) :11-15
[9]   INTERNAL FLOW CHARACTERISTICS OF SIMPLEX SWIRL ATOMIZERS [J].
RIZK, NK ;
LEFEBVRE, AH .
JOURNAL OF PROPULSION AND POWER, 1985, 1 (03) :193-199
[10]  
RIZK NK, 1985, 3RD P INT C LIQ AT S, P3