Development and verification of a fuel slinger atomization test bench

GAO Xiang; WANG Fang; XIAO Yangchun; WU Zhaoyang; JIN Jie

doi:10.16511/j.cnki.qhdxxb.2019.26.034

PDF(4548 KB)

Journal of Tsinghua University(Science and Technology) ›› 2020, Vol. 60 ›› Issue (3) : 212-218. DOI: 10.16511/j.cnki.qhdxxb.2019.26.034

SPECIAL SECTION: AEROSPACE AND ENGINEERING MECHANICS

Development and verification of a fuel slinger atomization test bench

{{article.zuoZhe_EN}}

Author information +

History +

Abstract

Fuel slingers are commonly used fuel injection devices for small and medium-sized aeroengines. This study developed a fuel slinger atomization test bench to provide reference data to improve fuel slinger designs and combustion chamber performance tests. The test bench included a water supply system, rotating system, ventilation system, test system, control system, and data acquisition system. Analyses of the key operating parameters such as the water supply pressure, water supply flow rate and vibrations of the rotating system shows that the test bench gives reliable, accurate experimental data. A phase Doppler particle analyzer (PDPA) was used to measure the particle size statistics and the variation of the Sauter mean diameter (SMD) for various rotational speeds. The experimental results show that the particle size in the fuel slinger has a normal distribution and the SMD decreases with increasing fuel slinger speed with an SMD of 41 μm above 12 000 r/min. The experimental results are consistent with the conclusions of previous papers, further indicating the reliability of the test bench.

Key words

aeroengine fuel slinger / test bench development / atomization characteristics / phase Doppler particle analyzer (PDPA)

Cite this article

EndNote

Ris (Procite)

Bibtex

Download Citations

GAO Xiang, WANG Fang, XIAO Yangchun, WU Zhaoyang, JIN Jie. Development and verification of a fuel slinger atomization test bench[J]. Journal of Tsinghua University(Science and Technology). 2020, 60(3): 212-218 https://doi.org/10.16511/j.cnki.qhdxxb.2019.26.034

References

[1] 宋双文, 罗辉. 离心甩油盘特性浅析[C]//中国航空学会(动力)第三届小发动机, 中国航空学会(直升机)第三届动力与传动学术讨论会论文集. 温州, 中国:中国航空学会, 2000:125-133. SONG S W, LUO H. Analysis of centrifugal fuel slinger[C]//Proceedings of the 3rd Small Engine Academic Symposium of Chinese Society of Aeronautics and Astronautics. Wenzhou, China:Chinese Society of Aeronautics and Astronautics, 2000:125-133. (in Chinese)
[2] MASKEY H C, MARSH F X. The annular combustion chamber with centrifugal fuel injection[C]//Proceedings of the Society of Automotive Engineers. New York, USA:SAE, 1962:620007.
[3] ROGO C, TRAUTH R L. Design of high heat release slinger combustor with rapid acceleration requirement[C]//Proceedings of the Society of Automotive Engineers. New York, USA:SAE, 1974:740167.
[4] MORISHITA T. A development of the fuel atomizing device utilizing high rotational speed[C]//Proceedings of the ASME 1981 International Gas Turbine Conference and Products Show. Houston, Texas, USA:ASME, 1981:V001T04A007.
[5] DAHM W J A, PATEL P R, LERG B H. Visualization and fundamental analysis of liquid atomization by fuel slingers in small gas turbines[C]//Proceedings of the 32nd AIAA Fluid Dynamics Conference and Exhibit. St Louis, Missouri, USA:AIAA, 2002:3183.
[6] CHOI S, LEE D, PARK J. Ignition and combustion characteristics of the gas turbine slinger combustor[J]. Journal of Mechanical Science and Technology, 2008, 22(3):538-544.
[7] CHOI S M, JANG S H, LEE D H, et al. Spray characteristics of the rotating fuel injection system of a micro-jet engine[J]. Journal of Mechanical Science and Technology, 2010, 24(2):551-558.
[8] 贾永忠. 甩油盘的雾化分析[J]. 推进技术, 1995, 16(4):45-49. JIA Y Z. An analysis on atomization of fuel slinger[J]. Journal of Propulsion Technology, 1995, 16(4):45-49. (in Chinese)
[9] 熊纯, 宋双文, 陈剑, 等. 一种离心甩油盘雾化性能的试验[J]. 航空动力学报, 2012, 27(7):1517-1522. XIONG C, SONG S W, CHEN J, et al. Experimental study of atomization performance on a fuel slinger[J]. Journal of Aerospace Power, 2012, 27(7):1517-1522. (in Chinese)
[10] 蒋雪辉. 气液2相离心甩油盘设计[J]. 航空发动机, 2016, 42(2):7-10. JIANG X H. Design of a gas-liquid two-phase slinger[J]. Aeroengine, 2016, 42(2):7-10. (in Chinese)
[11] 陈晓丽, 蒋雪辉, 何悟, 等. 微小型甩油盘式燃烧室若干关键技术研究[J]. 推进技术, 2016, 37(2):296-303. CHEN X L, JIANG X H, HE W, et al. A study on key technologies of micro combustor with a slinger injector[J]. Journal of Propulsion Technology, 2016, 37(2):296-303. (in Chinese)
[12] 刘睿. 甩油盘雾化性能测试及雾化特性分析[D]. 北京:北京航空航天大学, 2018.LIU R. Atomization performance test and characteristics analysis of fuel slinger[D]. Beijing:Beihang University, 2018. (in Chinese)
[13] 李宏伟. 甩油盘的雾化试验台建设及雾化特性分析[D]. 北京:北京航空航天大学, 2018.LI H W. Construction of the test bench used for experimental study of atomization performance on a fuel flinger in small aero Engine[D]. Beijing:Beihang University, 2018. (in Chinese)
[14] 叶宇隆. 直连式甩油盘雾化特性的数值模拟[D]. 北京:北京航空航天大学, 2018.YE Y L. A simulation of the fuel slinger with a tube welded on it[D]. Beijing:Beihang University, 2018. (in Chinese)