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航空煤油活塞发动机空气辅助喷射系统喷雾特性试验研究.

Authors :
高宏力
张付军
王苏飞
武浩
周磊
赵振峰
刘波澜
Source :
Acta Armamentarii. may2019, Vol. 40 Issue 5, p927-937. 11p.
Publication Year :
2019

Abstract

Based on the air-assisted spray characteristics of two-stroke aviation kerosene piston engine, the systemic experimental study was performed, and the effects of ambient pressure, temperature and control parameters,including fuel injection duration, interval among fuel and air, and air injection duration, on spray width, penetration, spatial diffusion area and Souter mean diameter were analyzed using a high-speed camera and a phase Doppler particle analyzer combining with image processing technology in order to obtain a desired gas mixture and ensure a good match between the spray characteristics and the time-varying environment of cylinder. The results show that the increased ambient pressure is not conducive to the spray spatial diffusion, while the atomization is worsen; and the increased ambient temperature is beneficial to the evaporation and breakup of fuel droplets in the case of constant control parameters; and the decreased or increased air injection duration facilitates the extension of spray along the direction of the nozzle, and promotes the expansion and breakup of droplets. The experimental results show that the air-assisted injection system has good adaptability. [ABSTRACT FROM AUTHOR]

Details

Language :
Chinese
ISSN :
10001093
Volume :
40
Issue :
5
Database :
Academic Search Index
Journal :
Acta Armamentarii
Publication Type :
Academic Journal
Accession number :
137678327
Full Text :
https://doi.org/10.3969/j.issn.1000-1093.2019.05.004