高速直喷柴油机的燃烧特性和排放试验研究

本文对一台四缸高速直喷柴油机的燃烧和排放特性进行了试验研究,分析研究了负荷及燃油喷射压力和供油提前角对该柴油机的着火延迟、瞬时放热率、NOx、CO及HC排放的影响。结果显示随着负荷及燃油喷射压力的提高着火延迟缩短、NOx排放增加;随着供油提前角的推迟NOx排放显著减少;而CO和HC的排放量与负荷及供油提前角的关系不大。     

直喷式柴油机燃用二甲基醚(DME)试验研究

介绍了在1100单缸直喷式柴油机上燃用DME的发动机试验研究结果。研究表明：通过增加循环供油量可使柴油机燃用DME后恢复到原机略低，同时缸内最大爆发压力降低，发动机碳烟排放为零，HC和CO排放比原机略高，NOx排放比原柴油机降低约50%以上，供油提前角减少，缺内最大爆发压力降低，NOx排放可进一步大幅度降低，但HC排放略有升高；加大喷孔直径，缸内爆发压力升高，NOx排放升高，HC和CO排放在中低负荷相差不大，但在大负荷工况有所升高。     

不同海拔条件下喷油参数对柴油机性能的影响

通过内燃机高原环境模拟试验台,研究了不同海拔条件下高压共轨柴油机在最大转矩转速点(1500 r/min)全负荷(2300 N·m)和部分负荷(500 N·m)工况下喷油提前角、共轨压力及循环喷油量(全负荷)对柴油机燃烧特性与性能的影响规律.结果表明:全负荷工况下,随着喷油提前角增加,柴油机滞燃期增加,最高燃烧压力和最大压力升高率增大,增大趋势随海拔增加而降低,柴油机转矩在0 km和3 km海拔先增加后减小,在5 km海拔时逐步增加.随着共轨压力增加,柴油机燃烧相位提前,最高燃烧压力、最大压力升高率和转矩均增加,排温降低;部分负荷工况下,有效燃油消耗率随共轨压力增加而降低.随循环喷油量增加,转矩、排温和缸内压力均逐渐增大,最大压力升高率在3 km海拔范围内逐渐增加、在5 km海拔时逐渐减小.海拔每升高1 km,柴油机在全负荷工况下,最佳循环喷油量平均降低5.81%,最佳喷油提前角和共轨压力在全负荷和部分负荷工况下平均分别增加了1.2°,CA、0.8°,CA和4 MPa、3 MPa.     

火花点火式煤层气发动机的燃烧过程实验研究

对由S195柴油机改装得到的燃用变组分煤层气发动机进行了全面的测试和分析，包括缸内示功图、燃烧放热率、主燃期、点火提前角、火焰发展期以及最大压力循环波动等。结果表明：甲烷浓度、点火提前角、负荷的大小对火焰发展期、循环波动以及燃烧有着至关重要的影响。     

某柴油机放热过程分析研究

柴油机的放热过程影响着循环效率、最高燃烧压力和压力升高率,从而决定了柴油机的动力性和经济性.本文针对某车用柴油机,在现有供油系统和进气系统的条件下,通过分析不同工况、不同供油提前角的缸内放热规律,确定了不同工况的最佳提前角,其结论对改善该柴油机的动力性和经济性有着积极意义.     

小型高速直喷柴油机循环变动及影响因素分析

研究了采用低涡流进气、浅ω型燃烧系统的SD2100直喷高速柴油机的转速与负荷对循环变动的影响.分析了最大爆发压力pmax及其出现相位Фa,平均指示压力pi的循环变动.经分析发现不同转速下负荷对循环变动的影响不同,转速越高负荷对循环变动的影响越大,循环变动随负荷的增加而呈现增大趋势,最大值之后再降低.     

供油提前角对柴油/水煤浆混合燃料燃烧排放性能的影响

通过柴油机台架试验,分析了供油提前角变化对柴油/水煤浆混合燃料燃烧排放的影响.试验结果表明:当供油提前角调定为18 ℃A时,柴油/水煤浆混合燃料的有效燃油消耗率降低,热效率升高,燃烧持续期最短,增加或减少供油提前角都将延长燃烧持续期;供油提前角变化对柴油/水煤浆混合燃料的排放有较大影响,逐步增大供油提前角(由17到18 ℃A,再到19 ℃A),混合燃烧的烟度排放降低,Nox的排放先降低再升高,CO的排放先升高再降低,HC排放升高.     

增压中冷柴油-天然气双燃料发动机燃烧特性的实验研究

对天然气替代率、引燃柴油喷油时刻和中冷后进气温度等燃烧系统参数对增压中冷柴油—天然气双燃料发动机燃烧特性的影响进行了实验研究。研究结果表明：增压中冷柴油—天然气双燃料发动机的燃烧放热速率比纯柴油快，引燃柴油的着火时刻和缸内燃料空燃比值决定着双燃料发动机的燃烧特性，即着火时刻在上止点前且空燃比值较小时，其燃烧接近于定容燃烧过程，随着天然气替代率的升高，缸内最大爆发压力和最高燃烧温度升高；而着火时刻在上止点后且空燃比值较大时，其燃烧接近于等压燃烧过程，随着天然气替代率升高，缸内最大爆发压力和最高燃烧温度降低。最大爆发压力、最高燃烧放热率和最高燃烧温度随引燃柴油喷油提前角的增大而升高；而随着进气温度升高，最大爆发压力和缸内温度增大。     

柴油机燃用微乳化甲醇柴油燃烧噪声研究

在柴油机上分别燃用柴油和甲醇柴油进行了燃烧特性试验,获得了柴油和微乳化甲醇柴油的燃烧噪声在标定工况、最大扭矩工况、不同负荷及不同供油提前角时的变化规律。试验结果表明:柴油机在标定工况和最大扭矩工况运行时,与纯柴油相比,甲醇柴油的燃烧噪声在低频段相差很小,中频段高出较多,高频段略高;甲醇柴油气缸压力A声级的负荷特性变化趋势与纯柴油基本一致,气缸压力A声级负荷特性曲线随甲醇含量增加而升高;供油提前角为12°CA时,M10气缸压力A声级比M0略高,供油提前角为10°CA时,M10气缸压力A声级比M0高较多。     

增压中冷稀燃天然气发动机燃烧特性试验研究

以190型天然气发动机为对象,采集了发动机的示功图,分析了点火提前角及负荷对燃烧过程的影响规律。试验结果表明,在BTDC28℃A到BTDC36℃A范围内,最高燃烧压力和最大瞬时放热率以及缸内最高燃烧温度随点火提前角的增大而增大;BTDC33℃A点火提前角下最高燃烧压力和最大瞬时放热率以及缸内最高燃烧温度随负荷的增大而增大;火焰发展期随点火提前角增大而增大,随负荷增加而减小;50%燃烧相位角随点火提前角、负荷的增加而减小,速燃期随点火提前角的增大先增大后减小,随负荷增加呈减小趋势。     

四气门汽油机低速低负荷燃烧过程的试验研究

在发动机试验台上,用CB-466燃烧分析仪对四气门汽油机低速低负荷燃烧压力循环变动进行了试验研究。试验结果表明,转速不变时,随着负荷的增加,指示热效率逐渐增加,达到最大值后又逐渐减小,最高燃烧压力及其标准偏差和平均指示压力逐渐增加,最高燃烧压力循环变动率和平均指示压力循环变动率则随之减小;中等负荷与小负荷相比,最高燃烧压力循环变动率减少了28.3%,平均指示压力循环变动率减少了47.6%。在负荷不变的条件下,随着转速的增加,指示热效率逐渐增加,低转速时的指示热效率仅为中等转速时的指示热效率的57.4%,最高燃烧压力随之减小,最高燃烧压力循环变动率、平均指示压力及其标准偏差和平均指示压力循环变动率逐渐增加。平均指示压力循环变动率与最高燃烧压力循环变动率相比较小,平均指示压力循环变动率仅为最高燃烧压力循环变动率的37.1%。     

Effects of Fischer-Tropsch diesel fuel on combustion and emissions of direct injection diesel engine

Effects of Fischer-Tropsch (F-T) diesel fuel on the combustion and emission characteristics of a single-cylinder direct injection diesel engine under different fuel delivery advance angles were investigated. The experimental results show that F-T diesel fuel exhibits shorter ignition delay, lower peak values of premixed burning rate, lower combustion pressure and pressure rise rate, and higher peak value of diffusion burning rate than conventional diesel fuel when the engine remains unmodified. In addition, the unmodified engine with F-T diesel fuel has lower brake specific fuel consumption and higher effective thermal efficiency, and presents lower HC, CO, NO_x and smoke emissions than conventional diesel fuel. When fuel delivery advance angle is retarded by 3 crank angle degrees, the combustion duration is obviously shortened; the peak values of premixed burning rate, the combustion pressure and pressure rise rate are further reduced; and the peak value of diffusion burning rate is further increased for F-T diesel fuel operation. Moreover, the retardation of fuel delivery advance angle results in a further significant reduction in NO_x emissions with no penalty on specific fuel consumption and with much less penalty on HC, CO and smoke emissions.     

F-T柴油对直喷式柴油机燃烧和排放的影响

在两种不同供油提前角下研究了燃用F-T柴油对直喷式柴油机燃烧和排放特性的影响,结果表明:发动机不做任何调整时,与0号柴油相比,燃用F-T柴油的滞燃期较短,预混燃烧放热峰值较低,扩散燃烧放热峰值较高,最高燃烧压力和最大压力升高率较低,燃油消耗率和热效率都得到了改善,HC、CO、NOx和碳烟排放同时降低。当供油提前角推迟3℃A时,燃用F-T柴油燃烧持续期明显缩短,预混燃烧放热峰值、最高燃烧压力和最大压力升高率进一步降低,扩散燃烧放热峰值略有升高,燃油消耗率变化不大,NOx排放进一步降低, HC、CO和碳烟略有增加,其中HC排放与原柴油机相当,而CO和碳烟仍远低于原柴油机。     

Effects of Fischer-Tropsch diesel fuel on combustion and emissions of direct injection diesel engine

Effects of Fischer-Tropsch (F-T) diesel fuel on the combustion and emission characteristics of a single-cylinder direct injection diesel engine under different fuel delivery advance angles were investigated. The experimental results show that F-T diesel fuel exhibits shorter ignition delay, lower peak values of premixed burning rate, lower combustion pressure and pressure rise rate, and higher peak value of diffusion burning rate than conventional diesel fuel when the engine remains unmodified. In addition, the unmodified engine with F-T diesel fuel has lower brake specific fuel consumption and higher effective thermal efficiency, and presents lower HC, CO, NO _x and smoke emissions than conventional diesel fuel. When fuel delivery advance angle is retarded by 3 crank angle degrees, the combustion duration is obviously shortened; the peak values of premixed burning rate, the combustion pressure and pressure rise rate are further reduced; and the peak value of diffusion burning rate is further increased for F-T diesel fuel operation. Moreover, the retardation of fuel delivery advance angle results in a further significant reduction in NO _x emissions with no penalty on specific fuel consumption and with much less penalty on HC, CO and smoke emissions. __________ Translated from Chinese Internal Combustion Engine Engineering, 2007, 28(2): 19–23 [译自: 内燃机工程]     

LPG/柴油双燃料发动机压缩比优化研究

采用燃料复合供给方式 ,在单缸直喷式柴油机上进行了LPG/柴油双燃料发动机压缩比的优化试验研究 ,对比分析了使用纯柴油和LPG/柴油双燃料的燃烧特性 ,着重研究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、压力循环波动及燃烧放热率 ,并以此为依据优选了双燃料发动机的压缩比。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 ,同时压力循环波动变小 ,但滞燃期、燃烧持续期都会有所增加。经过优化 ,压缩比确定为 14.5时 ,ZH110 5W柴油机改燃LPG/柴油双燃料后在高负荷工况下无严重爆震现象 ,压力循环波动较小 ,且经济性较好 ,热效率损失不大     

柴油-小桐子掺混油柴油机工作过程及循环变动分析

以柴油和柴油-小桐子掺混油在单缸水冷四冲程柴油机上进行试验,测录了多循环的瞬时气缸压力与高压油管燃油压力,对比分析了不同转速的全负荷工况与标定点转速不同负荷工况,燃用柴油与掺混油的喷油与燃烧过程及燃烧过程中各参数的循环变动.结果发现,喷油率随转速升高而升高;喷油始点随转速升高略微推迟,随负荷增大而提前;掺混油燃烧始点早于柴油,燃烧始点随转速升高延后,随负荷增大而提前,燃烧始点的循环变动量随转速升高而增大;高转速、高负荷时的最高燃烧压力循环变动率较小;掺混油的最大燃烧压力升高率低于柴油,最大压力升高率循环变动率随转速升高、负荷减小而增大.     

天然气发动机在不同喷射和点火时刻下的性能优化研究

为解决改装的天然气发动机动力性比原柴油机低,燃料消耗率比原柴油机高的问题,对影响燃烧时刻的喷射提前角与点火提前角这两个重要参数进行模拟实验,研究其对发动机的缸内压力与功率、燃气消耗率的影响,并根据研究结果进行优化设计。结果表明,对于缸内直喷天然气发动机,适当增大喷气提前角和选择恰当的点火提前角能在较经济的情况下提高发动机的动力性;发动机转速增加,点火提前角和喷射提前角也应提前,保证燃料的充分混合和最大化做功能力;在所有转速下,天然气发动机的功率都能恢复到原柴油机的水平。     

Comparison of cycle-by-cycle variation of measured exhaust-gas temperature and in-cylinder pressure measurements

Closed-loop control of the combustion process in the internal-combustion engine on a cycle-to-cycle basis is desirable to achieve better fuel economy and reduce pollutant emissions. This work explores the possibility of monitoring the in-cylinder combustion process of a spark-ignition engine by measuring exhaust-gas temperature. A small-diameter thermocouple (25.4 μm or 0.001 in.) is inserted into the exhaust manifold to measure exhaust-gas temperature, while in-cylinder pressure is monitored with a pressure transducer. Cycle-by-cycle variations of the measured exhaust-gas temperature are compared to IMEP variation for groups of cycles. The experimental results show that coefficient of variation of maximum temperature follows the same trend as the coefficient of variation of indicated mean effective pressure. Cycle-by-cycle variation of IMEP is reflected in cyclic variation of measured exhaust-gas temperatures for operating conditions under which the engine is working at a fixed speed or load and when cyclic variability is caused by changing engine parameters such as spark timing, injection timing, and air/fuel ratio. Finally, by using a moving window covering a small number of cycles, it is possible to show that the COV trend of maximum exhaust temperature mirrors that of IMEP.     

Syngas (H2/CO) in a spark-ignition direct-injection engine. Part 1: Combustion,performance and emissions comparison with CNG

The combustion, performance, and emissions of syngas (H₂/CO) in a four-stroke, direct-injection, spark-ignition engine were experimentally investigated. The engine was operated at various speeds, ranging from 1500 to 2400 rev/min, with the throttle being held in the wide-open position. The start of fuel injection was fixed at 180° before the top dead center, and the ignition advance was set at the maximal brake torque. The air/fuel ratio was varied from the technically possible lowest excess air ratio (λ) to lean operation limits. The results indicated that a wider air/fuel operating ratio is possible with syngas with a very low coefficient of variation. The syngas produced a higher in-cylinder peak pressure and heat-release rate peak and faster combustion than for CNG. However, CNG produced a higher brake thermal efficiency (BTE) and lower brake specific fuel consumption (BSFC). The BTE and BSFC of the syngas were on par to those of CNG at higher speeds. For the syngas, the total hydrocarbon emission was negligible at all load conditions, and the carbon monoxide emission was negligible at higher loads and increased under lower load conditions. However, the emission of nitrogen oxides was higher at higher loads with syngas.