Improved Atomization via a Mechanical Atomizer with Optimal Geometric Parameters and an Air-Assisted Component

被引:10
作者
Levitsky, Inna [1 ]
Tavor, Dorith [1 ,2 ]
机构
[1] Shamoon Coll Engn, Dept Chem Engn, POB 950, IL-84100 Beer Sheva, Israel
[2] Shamoon Coll Engn, Green Proc Ctr, POB 950, IL-84100 Beer Sheva, Israel
关键词
mechanical atomizer; air-assisted atomizer; swirl chamber; drop diameters; air; liquid mass flow ratio; GAS-TURBINE ENGINES; SPRAY CHARACTERISTICS; INTERNAL FLOW; PRESSURE; NOZZLE;
D O I
10.3390/mi11060584
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
Atomization of liquid media is a key aim in various technological disciplines, and solutions that improve spray performance, while decreasing energy consumption, are in great demand. That concept is very important in the development of liquid fuel spray atomizers in high-efficiency microturbines and other generator systems with low inlet pressure and a wide range of power supply. Here we present a study of the liquid atomization characteristics for a new mechanical atomizer that has optimal geometric parameters and a preliminary swirl stage. In our air-assisted atomizer, air is introduced through a swirl chamber positioned at the exit of the mechanical atomizer. The optimized mechanical atomizer alone can achieveD(32)drop diameters in the range of 80 to 40 mu m at water supply pressures of 2 to 5 bar, respectively. The addition of an air swirl chamber substantially decreases drop sizes. At an air-liquid ratio (ALR) equal to 1, water pressures of 2.5 to 3 bar and air supply pressures 0.35 to 1 bar,D(32)drops with diameters of 20-30 mu m were obtained. In an air-assisted atomizer the parameters of the mechanical atomizer have a much stronger influence on drop diameters than do characteristics of the air-swirl chamber. Using a mechanical atomizer with optimal geometrical dimensions allows limiting the liquid supply pressure to 5 bar; but when an air-assisted component is introduced we can recommend an ALR approximate to 1 and an air supply pressure of up to 1 bar.
引用
收藏
页码:1 / 15
页数:15
相关论文
共 49 条
[1]  
[Anonymous], 2003, EXP FLUID MECH
[2]  
Bayrel L., 1993, Liquid atomization
[3]   Experimental study on spray characteristics of pressure-swirl nozzle in China advanced PWR containment [J].
Bian, Jiawei ;
Zhang, Dalin ;
Sun, Rulei ;
Wu, Yingwei ;
Tian, Wenxi ;
Su, G. H. ;
Qiu, Suizheng .
NUCLEAR ENGINEERING AND DESIGN, 2019, 350 :158-175
[4]  
Black DL, 1996, PROG ENERG COMBUST, V22, P267
[5]   Inlet fogging of gas turbine engines detailed climatic analysis of gas turbine evaporation cooling potential in the USA [J].
Chaker, M ;
Meher-Homji, CB ;
Mee, T ;
Nicholson, A .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2003, 125 (01) :300-309
[6]   Inlet fogging of gas turbine engines: Experimental and analytical investigations on impaction pin fog nozzle behavior [J].
Chaker, Mustapha A. ;
Meher-Homji, Cyrus B. ;
Mee, Thomas, III .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2006, 128 (04) :826-839
[7]   EXPERIMENTAL AND THEORETICAL-STUDY ON HOLLOW-CONE SPRAY [J].
CHANG, KC ;
WANG, MR ;
WU, WJ ;
HONG, CH .
JOURNAL OF PROPULSION AND POWER, 1993, 9 (01) :28-34
[8]   FACTORS INFLUENCING THE EFFECTIVE SPRAY CONE ANGLE OF PRESSURE-SWIRL ATOMIZERS [J].
CHEN, SK ;
LEFEBVRE, AH ;
ROLLBUHLER, J .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1992, 114 (01) :97-103
[9]   Viscosity effect on the pressure swirl atomization of an alternative aviation fuel [J].
Dafsari, Reza Alidoost ;
Lee, Hyung Ju ;
Han, Jeongsik ;
Park, Dong-Chang ;
Lee, Jeekeun .
FUEL, 2019, 240 :179-191
[10]   Swirl Atomizer Design for Evaporative Cooling of High Temperature Compressed Air Stream [J].
Dar, Uzair Ahmed ;
Bannikov, Mykola .
INTERNATIONAL JOURNAL OF FLUID MECHANICS RESEARCH, 2014, 41 (01) :51-70