커먼 레일 시스템 고압 연료 분사용 스월 노즐 인젝터의 분사 특성에 관한 연구

Abstract

In this work, the evaluation of swirl nozzle injector performance was conducted by investigating effective area (<TEX>$A_{eff}$</TEX>), injection mass (<TEX>$m_{inj}$</TEX>), injection rate (<TEX>$Q_{inj}$</TEX>), and injection delay (<TEX>$t_{delay}$</TEX>) under various test conditions. To achieve these, fuel injection analysis system which was composed of fuel supply system, injection system, and control system was installed. At the same time, the swirl nozzle that had 12 orifice hole with <TEX>$120^{\circ}$</TEX> injection angle was used in this work. It was revealed that the difference of injection mass (<TEX>$m_{inj}$</TEX>) between base and swirl nozzle injector increased as the injection pressure (<TEX>$P_{inj}$</TEX>) and energizing duration (<TEX>$t_{eng}$</TEX>) decreased under the same test conditions. The maximum injection rate (<TEX>$Q_{inj}$</TEX>) of swirl nozzle injector was higher than base nozzle injector about 2~5%. The injection performance of swirl nozzle was better than base nozzle at low injection pressure (<TEX>$P_{inj}$</TEX>) and short energizing duration (<TEX>$t_{eng}$</TEX>) conditions.