| Citation: | MIAO Junjie, WU Weiqiu, LI Xiankai, et al. Experiment on flash-boiling spray characteristics of single-orifice/dual-orifice nozzle[J]. Journal of Aerospace Power, 2024, 39(11):20220940 doi: 10.13224/j.cnki.jasp.20220940 |
The flash-boiling spray characteristics of RP-3 aviation kerosene inside single-orifice/dual-orifice nozzle were experimentally studied to analyze the influence of superheat degree and nozzle structural parameters on in-nozzle flow and near-nozzle jet. Results showed that increasing the length-diameter ratio of single-orifice nozzle can inhibit the cavitation effect inside the nozzle, helping to increase the kerosene gasification rate from wall boiling inside the nozzle, resulting in better atomization effect of fuel jet. The expansion chamber of dual-orifice nozzle could play the role of increasing the discharge-orifice’s gasification rate; however, excessive aspect ratio of expansion chamber may decrease the superheat degree inside the nozzle, which impaired the near-nozzle atomization effect and spray symmetry. Compared with single-orifice nozzle, dual-orifice nozzle allows more easily to promote the transformation of aviation kerosene from subcooled spray to flash-boiling spray by increasing the residence time for phase transition, helping to improve the fuel atomization and obtain larger spray width and spray cone angle. Thus, using dual-orifice nozzle is a potential technical way to realize flash-boiling spray in the combustion chamber of aero-engine.
| [1] |
YU G,LI J G,ZHAO J R,et al. An experimental study of kerosene combustion in a supersonic model combustor using effervescent atomization[J]. Proceedings of the Combustion Institute,2005,30(2): 2859-2866. doi: 10.1016/j.proci.2004.07.050
|
| [2] |
EREMEEV A,GRISHIN V,NIKITENKO L,et al. Enhanced ignition and mixing of kerosene in high-speed air streams[R]. AIAA 2005-614,2005.
|
| [3] |
MAURICE L Q,LANDER H,EDWARDS T,et al. Advanced aviation fuels: a look ahead via a historical perspective[J]. Fuel,2001,80(5): 747-756. doi: 10.1016/S0016-2361(00)00142-3
|
| [4] |
QIN J,ZHANG S L,BAO W,et al. Thermal management method of fuel in advanced aeroengines[J]. Energy,2013,49: 459-468. doi: 10.1016/j.energy.2012.10.050
|
| [5] |
BROWN R,YORK J L. Sprays formed by flashing liquid jets[J]. AIChE Journal,1962,8(2): 149-153. doi: 10.1002/aic.690080204
|
| [6] |
SENDA J,WADA Y,KAWANO D,et al. Improvement of combustion and emissions in diesel engines by means of enhanced mixture formation based on flash boiling of mixed fuel[J]. International Journal of Engine Research,2008,9(1): 15-27. doi: 10.1243/14680874JER02007
|
| [7] |
WANG Z M,BADAWY T,WANG B,et al. Experimental characterization of closely coupled split isooctane sprays under flash boiling conditions[J]. Applied Energy,2017,193: 199-209. doi: 10.1016/j.apenergy.2017.02.009
|
| [8] |
GUO H J,WANG B,LI Y F,et al. Characterizing external flashing jet from single-hole GDI injector[J]. International Journal of Heat and Mass Transfer,2018,121: 924-932. doi: 10.1016/j.ijheatmasstransfer.2018.01.042
|
| [9] |
DU J G,MOHAN B,SIM J,et al. Study of spray collapse phenomenon at flash boiling conditions using simultaneous front and side view imaging[J]. International Journal of Heat and Mass Transfer,2020,147: 118824. doi: 10.1016/j.ijheatmasstransfer.2019.118824
|
| [10] |
LIAO Y X,LUCAS D. Computational modelling of flash boiling flows: a literature survey[J]. International Journal of Heat and Mass Transfer,2017,111: 246-265. doi: 10.1016/j.ijheatmasstransfer.2017.03.121
|
| [11] |
GUO H J,LI Y F,WANG B,et al. Numerical investigation on flashing jet behaviors of single-hole GDI injector[J]. International Journal of Heat and Mass Transfer,2019,130: 50-59. doi: 10.1016/j.ijheatmasstransfer.2018.10.088
|
| [12] |
ZHANG G M,HUNG D L S,XU M. Experimental study of flash boiling spray vaporization through quantitative vapor concentration and liquid temperature measurements[J]. Experiments in Fluids,2014,55(8): 1804. doi: 10.1007/s00348-014-1804-7
|
| [13] |
ZEIGERSON-KATZ M,SHER E. Spray formation by flashing of a binary mixture: a parametric study[J]. Atomization and Sprays,1998,8(3): 255-266. doi: 10.1615/AtomizSpr.v8.i3.20
|
| [14] |
FAN Z C,FAN W,ZHAO L,et al. Experimental study on flash atomization of aviation kerosene[J]. Atomization and Sprays,2012,22(2): 163-183. doi: 10.1615/AtomizSpr.2012004932
|
| [15] |
PARK B S,LEE S Y. An experimental investigation of the flash atomization mechanism[J]. Atomization and Sprays,1994,4(2): 159-179. doi: 10.1615/AtomizSpr.v4.i2.30
|
| [16] |
XU H M,WANG C M,MA X,et al. Fuel injector deposits in direct-injection spark-ignition engines[J]. Progress in Energy and Combustion Science,2015,50: 63-80. doi: 10.1016/j.pecs.2015.02.002
|
| [17] |
RAWSON P. Evaluation of a jet fuel thermal stability rig[R].Victoria,Canada: DSTO Platforms Science Laboratory DSTO-TR-1643, 2004.
|
| [18] |
RASHKOVAN A,SHER E. Flow pattern observations of gasoline dissolved CO2 inside an injector[J]. Atomization and Sprays,2006,16(6): 615-626. doi: 10.1615/AtomizSpr.v16.i6.20
|
| [19] |
SHER E,BAR-KOHANY T. Subsonic effervescent atomization: a theoretical approach[J]. Atomization and Sprays,2004,14(6): 495-510. doi: 10.1615/AtomizSpr.v14.i6.10
|
| [20] |
JU D H,FANG J H,ZHANG T T,et al. High-speed shadow imaging in internal flow pattern and macroscopic characteristics of a R134a flash-boiling spray discharged through a vertical twin-orifice atomizer[J]. International Journal of Multiphase Flow,2015,75: 224-236. doi: 10.1016/j.ijmultiphaseflow.2015.06.002
|
| [21] |
JU D H,HUANG Z,JIA X X,et al. Macroscopic characteristics and internal flow pattern of dimethyl ether flash-boiling spray discharged through a vertical twin-orifice injector[J]. Energy,2016,114: 1240-1250. doi: 10.1016/j.energy.2016.08.082
|
| [22] |
SHER E,BAR-KOHANY T,RASHKOVAN A. Flash-boiling atomization[J]. Progress in Energy and Combustion Science,2008,34(4): 417-439. doi: 10.1016/j.pecs.2007.05.001
|
| [23] |
程晓军. 串联式TBCC超级燃烧室燃烧组织及性能研究[D]. 南京: 南京航空航天大学,2015. CHENG Xiaojun. Investigation of combustion organization and performance of tandem type turbine based combined cycle hyperburner[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2015. (in Chinese
CHENG Xiaojun. Investigation of combustion organization and performance of tandem type turbine based combined cycle hyperburner[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015. (in Chinese)
|