燃烧科学与技术
燃燒科學與技術
연소과학여기술
JOURNAL OF COMBUSTION SCIENCE AND TECHNOLOGY
2013年
5期
388-394
,共7页
董素荣%刘瑞林%周广猛%王威%张众杰%何西常
董素榮%劉瑞林%週廣猛%王威%張衆傑%何西常
동소영%류서림%주엄맹%왕위%장음걸%하서상
柴油机%高原%数值模拟%碳烟
柴油機%高原%數值模擬%碳煙
시유궤%고원%수치모의%탄연
diesel engine%plateau%numerical simulation%soot
采用 AVL FIRE 数值分析软件对共轨柴油机高海拔(低气压)燃烧过程的燃油浓度场、温度场分布及碳烟形成历程进行了模拟计算,研究了不同海拔大气压力对共轨柴油机低速全负荷工况燃烧过程及碳烟排放的影响.结果表明,在不同海拔(0,m、3,000,m、4,000,m 和5,000,m)条件下,计算燃烧压力和放热率与试验值具有较好的一致性,验证了所建数值分析模型的有效性.随着海拔的升高,燃烧后期浓混合气分布区域、燃烧高温区域以及碳烟形成区域明显增大.在燃烧初期,碳烟质量分数逐渐增大,在15~17°,CA ATDC 出现峰值,且碳烟峰值随海拔的升高而增大,海拔5,000,m碳烟质量分数峰值是海拔0,m的1.87倍;燃烧后期,随海拔的升高,碳烟氧化速率降低,排放增加.
採用 AVL FIRE 數值分析軟件對共軌柴油機高海拔(低氣壓)燃燒過程的燃油濃度場、溫度場分佈及碳煙形成歷程進行瞭模擬計算,研究瞭不同海拔大氣壓力對共軌柴油機低速全負荷工況燃燒過程及碳煙排放的影響.結果錶明,在不同海拔(0,m、3,000,m、4,000,m 和5,000,m)條件下,計算燃燒壓力和放熱率與試驗值具有較好的一緻性,驗證瞭所建數值分析模型的有效性.隨著海拔的升高,燃燒後期濃混閤氣分佈區域、燃燒高溫區域以及碳煙形成區域明顯增大.在燃燒初期,碳煙質量分數逐漸增大,在15~17°,CA ATDC 齣現峰值,且碳煙峰值隨海拔的升高而增大,海拔5,000,m碳煙質量分數峰值是海拔0,m的1.87倍;燃燒後期,隨海拔的升高,碳煙氧化速率降低,排放增加.
채용 AVL FIRE 수치분석연건대공궤시유궤고해발(저기압)연소과정적연유농도장、온도장분포급탄연형성역정진행료모의계산,연구료불동해발대기압력대공궤시유궤저속전부하공황연소과정급탄연배방적영향.결과표명,재불동해발(0,m、3,000,m、4,000,m 화5,000,m)조건하,계산연소압력화방열솔여시험치구유교호적일치성,험증료소건수치분석모형적유효성.수착해발적승고,연소후기농혼합기분포구역、연소고온구역이급탄연형성구역명현증대.재연소초기,탄연질량분수축점증대,재15~17°,CA ATDC 출현봉치,차탄연봉치수해발적승고이증대,해발5,000,m탄연질량분수봉치시해발0,m적1.87배;연소후기,수해발적승고,탄연양화속솔강저,배방증가.
Numerical simulation of the fuel concentration field,temperature field distribution and soot formation histories in a common rail diesel engine at high altitude(low air pressure)was carried out by means of AVL FIRE nu-merical analysis. The influences of air pressure at different altitude on combustion process and soot emissions at low speed full-load in a common rail diesel engine were investigated. The in-cylinder pressure and heat release rate from simulation are consistent with the experimental data at different altitude(0,m,3,000,m,4,000,m,5,000,m). There-fore,the effectiveness of the numerical model is verified. The results indicated that rich fuel mixture area,high com-bustion temperature area and soot formation area were enlarged obviously during the late combustion period with the altitude increasing. The mass fraction of soot increased gradually during the early combustion period and the peak value appeared at 15~17,°CA ATDC. The soot mass fraction peak value increased with the altitude increasing,and the peak value at 5,000,m was 1.87,times that at 0,m altitude. During the late combustion period,the oxidation rate of soot was reduced with the altitude increasing,which resulted in the increase of soot emission.