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不同过量空气系数下天然气发动机循环变动特性研究 总被引:1,自引:1,他引:0
试验研究了过量空气系数对天然气发动机循环变动特性的影响,研究结果表明,当过量空气系数从1逐渐增大到1.8时,发动机的循环变动增大。最高燃烧压力(pmax)与平均指示压力(pmi)有一定的相关性,高的pmax循环对应着高的pmi循环。高的pmi和pmax对应着短的火焰发展期(θd),短的50%质量已燃持续期(θx=0~0.5)和短的燃烧持续期(θb)。而且,pmax与其对应的曲轴转角(φpmax),最大压力升高率(λpmax)与pmi,θd与θx=0~0.5,θd与θb都存在很好的对应关系。 相似文献
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《车用发动机》2020,(1)
微量柴油引燃高压直喷天然气发动机排放低于同排量柴油机,热效率与同排量柴油机相当,具有良好的发展前景。对于高压直喷天然气发动机,循环变动特性直接影响了其运行的稳定性,但目前的研究大多针对发动机的燃烧和排放特性,对循环变动的研究十分有限。以一台微量柴油引燃高压直喷天然气发动机为研究对象,对其外特性工况下不同运行参数的循环变动进行了研究。结果表明:随天然气喷射提前角增加,最大燃烧压力的循环变动呈现先增加后减小的趋势,低速下最大燃烧压力的循环变动相对较高;滞燃期和50%燃料燃烧相位角的循环变动随天然气喷射的提前和转速的增加而增加;在24MPa喷射压力下,平均有效压力的循环变动随天然气喷射提前角的增加而增加,而在30MPa下,平均有效压力循环变动随天然气喷射提前角的变化规律与转速有关;在高转速下,平均有效压力的循环变动相对较高;燃料的喷射压力对各参数的循环变动影响很小。 相似文献
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在1台两缸直喷式柴油机上对比测试了生物柴油的燃烧特性,分析了进油温度对发动机峰值燃烧压力分布以及循环变动率的影响。结果表明,随着进油温度的增加,生物柴油发动机表现出如下燃烧特性:燃烧延迟,高负荷时延迟更明显;峰值燃烧压力降低,其循环分布向低值偏移;峰值燃烧压力分布最高值增加且其循环变化幅度明显降低,循环变动率降低,循环变动减弱;负荷或转速增加均导致循环变化幅度明显降低,循环变动减弱。研究结果证明,进油温度对燃用生物柴油的燃烧压力及其循环变动有重要影响,进油温度增加可以提高燃烧稳定程度,从而改善燃烧过程。 相似文献
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本文采用复燃料供给方式,在单缸直喷式柴油机上进行了LPG/柴油双燃料的优化试验研究,对比分析了柴油和双燃料及不同掺烧比下双燃料的燃烧特性,着重研究了分析了双燃料发动机在不同压缩比下的最高燃烧压力、最大压力升高率、压力循环变动及燃烧放热规律,并以此为依据优选了双燃烧发动机的压缩比。试验结果表明,降低压缩比后,双燃料发动机的最高燃烧压力及最大压力升高率均有较大降低,同时压力循环变动变小,但着火延迟期,燃烧持续期都会有所增加。 相似文献
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分析了自行研制的新型复合含氧添加剂(记为FHYJ)的理化特性,在车用BJ493Q柴油机上进行了燃用FHYJ掺烧比例为9%的FHYJ—柴油混合燃料的试验,测量了缸内压力、压力升高率和放热率。比较和分析了燃用柴油和FHYJ—柴油混合燃料的燃烧特性,探讨了添加剂和混合燃料对柴油机滞燃期、预混合燃烧期、扩散燃烧期以及燃烧持续期等参数的影响。结果表明,在柴油机不作任何改动的前提下,掺烧FHYJ清洁燃料复合含氧添加剂,缸内压力、压力升高率和放热率在低负荷下均与原机基本相当,在中、高负荷有所下降,滞燃期、预混燃烧期均较原机延长,扩散燃烧期和燃烧持续期均较原机缩短,且其变化程度均随负荷的增大而增大。 相似文献
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Z. C. Kan D. M. Lou Z. Z. Cao Z. Y. Hu S. Liu Z. H. Yang 《International Journal of Automotive Technology》2017,18(2):209-217
Altitude has a significant effect on combustion of heavy-duty diesel engines, especially during cold start. An experimental study on a heavy-duty diesel engine operating at different altitudes was conducted. Tests were based on a direct injection (DI) turbocharged diesel engine with intake and exhaust pressure controlled by the plateau simulation test system to stimulate altitude conditions including 0 m, 1000 m, 2000 m, 3000 m and 4000 m. Results indicated that the compression and expansion resistance moment reduced and the speed increased during the cranking period. The peak pressure of several cycles was increased during the start-up period; however, the expansion pressure dropped more and the indicated mean effective pressure (IMEP) reduced as the altitude rose. While at an altitude of over 2000 m, the peak pressure fluctuated obviously during the start-up period. The higher the altitude was, the more the fluctuation amplitude and cycle number increased and combustion instability enhanced, which resulted the start-up period time increasing at high altitude. When the altitude rose, the cycle-to-cycle variation of the peak pressure and speed fluctuation increased during the idle, the ignition and CA50 were delayed and the combustion duration was shortened. The effect of altitude on combustion characteristics of the diesel engine was more significant during the start-up period than during its idle period. 相似文献
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Fuel injection during negative valve overlap period was used to realize diesel homogeneous charge compression ignition (HCCI)
combustion. In order to control the combustion, CO2 in-cylinder injection was used to simulate external EGR. Effects of CO2 injection parameters (injection timing, quantity, pressure) on HCCI combustion and emission characteristics were investigated.
Experimental results revealed that CO2 in-cylinder injection can control the start of combustion and effectively reduce NOx emission. Either advancing CO2 injection timing or increasing CO2 injection quantity can reduce peak cylinder pressure and mean gas temperature, delay the starts of low temperature reaction
(LTR) and high temperature reaction (HTR), and lower pressure rise rate; NOx emission was reduced, while smoke, HC, and CO emissions increased. Since the combustion phase was improved, the indicated
thermal efficiency was also improved. Injection pressure determines the amount of disturbance introduced into the cylinder.
Generally, with the same injection quantity, higher injection pressure results in higher momentum flux and total momentum.
Larger momentum flux and momentum has a stronger disturbance to air-fuel mixture, resulting in a more homogeneous mixture;
therefore, larger injection pressure leads to lower NOx and smoke emissions. 相似文献
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以点燃式汽油转子发动机为研究对象,建立了相应的湍流和燃烧模型,实现了发动机工作过程的三维动态模拟,并利用试验结果进行对比验证。在此模型基础上,模拟计算和分析了4种不同点火位置对缸内压力、温度、火焰传播及NO_x生成的影响。结果表明:点火位置选择在燃烧室中轴线上,与转子凹坑中心位置重合,能优化燃烧,获取较大的功率;在燃烧室后部点火时,燃烧初期火焰传播速度快,压力升高率大,但是受限于燃烧室后部燃料少,压力峰值不高,且NO_x的生成量偏高;在燃烧室前部点火时,在补燃期阶段燃烧速度最快,但是点燃后压力升高阶段的燃烧效率一般;点火位置位于燃烧中轴线两侧错位排布时,燃烧效率低下导致压力峰值最低,同时NO_x的生成量稍高;一定工况下,双点火位置的坐标分别为(10 mm,-56 mm,-37.2 mm)和(-10 mm,-56 mm,-37.2mm)时,该发动机能获得最大的功率且NO_x生成量较少。 相似文献
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在柴油机结构不做改动的情况下,基于燃烧示功图的分析,定量研究了甲醇含量对燃烧压力、压力升高率、燃烧放热规律和循环变动量的影响。结果表明:甲醇的含量越大,滞燃期越长;燃烧压力和最大压力升高率均增大且出现的位置后移,其中燃用M15最大压力升高率接近0.45 MPa/°CA;累积放热率达到95%时,燃用柴油为上止点后55°CA,燃用M5和M10为上止点后53°CA,燃用M15为上止点后57°CA,位置差别不大。甲醇含量增加,柴油机循环变化量增大,燃用M0的COVpmi为1.61%,燃用M10的COVpmi为1.82%,燃用M15的COVpmi为3.32%。 相似文献