现代电子技术
現代電子技術
현대전자기술
MODERN ELECTRONICS TECHNIQUE
2014年
9期
125-127,130
,共4页
刘伟%毕玉华%申立中%雷基林%王俊
劉偉%畢玉華%申立中%雷基林%王俊
류위%필옥화%신립중%뢰기림%왕준
海拔高度的影响%EGR%柴油机%性能研究
海拔高度的影響%EGR%柴油機%性能研究
해발고도적영향%EGR%시유궤%성능연구
altitude effect%EGR%diesel engine%performance study
随着海拔的变化,大气压力和氧气浓度都会发生改变,引入EGR后发动机的性能必然会出现不同于标准大气压环境时的情况。建立了某型号发动机的Boost模型,用标准大气压下的台架试验数据对模型进行了标定验证;模拟研究了不同大气压力下EGR对发动机性能和排放的影响,并比较分析了同一EGR率时不同大气压力下发动机性能的差异。结果表明,除全负荷工况外EGR对发动机的动力性和经济性影响比较小,NOx随EGR率的增加会急剧减少,但大EGR率时Soot排放会急剧恶化;同一EGR率时在中高负荷下,随着海拔的增加,发动机的动力性、经济性和Soot的排放会出现明显恶化。
隨著海拔的變化,大氣壓力和氧氣濃度都會髮生改變,引入EGR後髮動機的性能必然會齣現不同于標準大氣壓環境時的情況。建立瞭某型號髮動機的Boost模型,用標準大氣壓下的檯架試驗數據對模型進行瞭標定驗證;模擬研究瞭不同大氣壓力下EGR對髮動機性能和排放的影響,併比較分析瞭同一EGR率時不同大氣壓力下髮動機性能的差異。結果錶明,除全負荷工況外EGR對髮動機的動力性和經濟性影響比較小,NOx隨EGR率的增加會急劇減少,但大EGR率時Soot排放會急劇噁化;同一EGR率時在中高負荷下,隨著海拔的增加,髮動機的動力性、經濟性和Soot的排放會齣現明顯噁化。
수착해발적변화,대기압력화양기농도도회발생개변,인입EGR후발동궤적성능필연회출현불동우표준대기압배경시적정황。건립료모형호발동궤적Boost모형,용표준대기압하적태가시험수거대모형진행료표정험증;모의연구료불동대기압력하EGR대발동궤성능화배방적영향,병비교분석료동일EGR솔시불동대기압력하발동궤성능적차이。결과표명,제전부하공황외EGR대발동궤적동력성화경제성영향비교소,NOx수EGR솔적증가회급극감소,단대EGR솔시Soot배방회급극악화;동일EGR솔시재중고부하하,수착해발적증가,발동궤적동력성、경제성화Soot적배방회출현명현악화。
Atmospheric pressure and oxygen concentration will change with the change of altitude,and engine performance will inevitably appear different from the standard air environment by using EGR. In this paper,the Boost model of an engine was established and verified according to the basic structure and bench test data of engine under standard air environment. The influence of EGR on engine performance and emissions at different altitudes was simulated and studied. The difference between the different atmospheric environments at the same EGR rate was analyzed. Simulation results shows the influence of EGR on en-gine power and economical efficiency is small except full load case,NOx emission is greatly reduced with the increase of EGR rate,but when the EGR rate is high,the Soot emission will worsen sharply,and the performance and Soot emission of engine will be significantly worse at high load with the same EGR rate while altitude increases.