点燃型预燃室在大缸径甲醇发动机上的应用

通过计算流体动力学数值模拟,探索点燃型预燃室在大缸径(320mm)甲醇发动机上的应用效果,计算了过量空气系数和点火正时对燃烧和性能的影响。结果表明,点燃型预燃室发动机的燃烧放热过程先缓后急,热效率较高,NO_x排放很低,SO_x排放为零,不经后处理即可满足国际海事组织TierⅢ排放法规。随着缸内过量空气系数的增加,缸内压力、压力升高率、声响强度和NO_x排放均显著降低,指示热效率先升后降,在过量空气系数为2.4时达到最高值49.2%;随着点火正时的延迟,缸内压力、压力升高率、声响强度、指示热效率逐渐下降,NO_x排放先减后增。基于计算结果,提出了一种燃烧控制策略:在平均有效压力低于1.8MPa时控制缸内过量空气系数为2.4并匹配较早的点火正时,在平均有效压力高于1.8MPa时控制过量空气系数为2.1并匹配较晚的点火正时。采用该策略可使部分负荷热效率最佳,且整机具有较高的动力性。     

主动预燃室式直喷汽油机稀薄燃烧性能研究

为明晰不同点火方式对汽油机稀薄燃烧特性的影响规律,在一款排量为0.5L的研究型单缸机上试验研究了传统火花塞和主动预燃室两种不同点火方式下发动机燃烧及排放特性,探索主动预燃室拓展稀薄燃烧极限的多种影响因素。研究结果表明,稀薄燃烧可有效降低油耗,提高发动机热效率。传统点火线圈的稀燃极限处于过量空气系数1.5附近,最高指示热效率为45.0%,而采用主动预燃室系统后,稀燃极限可进一步拓展,过量空气系数可达2.0,指示热效率提升至46.5%,氮氧化物排放比采用传统火花塞点火技术时降低约88%;主动预燃室匹配高压缩比14.80的燃烧系统,可进一步拓展稀燃极限至过量空气系数2.1,指示热效率可达48.0%,氮氧化物排放继续降低,在过量空气系数采用2.1时NOx排放最低可达58×10-6。     

预燃室射流点火对汽油发动机性能影响

基于一台单缸汽油发动机,设计了主动预燃室系统,试验了预燃室混合气状态对燃烧及排放的影响,通过对比不同点火能量的火花塞点火和预燃室点火,明确预燃室射流点火对燃烧过程影响机理．结果表明：随着预燃室内喷油量的增加,颗粒物数量(PN)排放增加;预燃室内浓混合气能改善燃烧相位、加快燃烧速度,提高点火性能,但预燃室内当量比附近的混合气有更大的节油潜力．当全局过量空气系数φglobal小于1.4时,预燃室点火燃油消耗率恶化;当φglobal大于1.4时,预燃室改善热效率的能力开始凸显．当预燃室中燃油量占总循环油量的分数为2%时,预燃室点火能将稀燃极限扩展至φglobal为2.1,在φglobal为1.8时总指示热效率达到48.5%的最大值．     

稀燃条件下主动预燃室式直喷汽油机燃烧和排放特性研究

为明晰不同点火方式对汽油机稀薄燃烧特性的影响规律,在一款排量为0.5 L的研究型单缸机上试验研究了传统火花塞和主动预燃室两种不同点火方式下发动机燃烧及排放特性,探索主动预燃室拓展稀薄燃烧极限的多种影响因素.研究结果表明,稀薄燃烧可有效降低油耗,提高发动机热效率.传统点火线圈的稀燃极限处于过量空气系数1.5附近,最高指示...     

预燃室湍流射流点火甲醇发动机稀薄燃烧和排放特性试验研究

基于一台四冲程单缸发动机开展预燃室湍流射流点火(turbulent jet ignition,TJI)甲醇发动机燃烧特性、性能表现和排放特性的试验研究。结果表明,TJI燃烧模式燃烧速率较快,放热率(heat release rate,HRR)峰值明显较高,且具有更短的滞燃期和燃烧持续期。随着过量空气系数变大,缸内压力和放热率峰值变小,TJI和火花塞点火(spark ignition,SI)燃烧模式滞燃期和燃烧持续期均变长。此外,TJI燃烧模式可有效提升甲醇发动机的稀薄燃烧稳定性,可将稀燃极限拓展至过量空气系数2.0。TJI燃烧模式下平均指示压力略低于SI模式;然而对于过量空气系数大于1.1的稀燃工况,TJI燃烧模式指示燃油消耗率更低,在过量空气系数1.3时低于570 g/(k W·h),说明其具有更好的燃油经济性。TJI燃烧模式下氮氧化物排放量明显低于SI燃烧模式,过量空气系数1.1时降低约37.2%,并且在过量空气系数大于1.3的极稀燃工况具有相对较低的甲醛CH₂O和碳氢化合物排放。     

异辛烷、乙醇及其混合燃料HCCI燃烧的试验研究和分析

在一台改制的发动机上进行了异辛烷、乙醇及其混合燃料HCCI燃烧的研究。发动机性能用缸内压力评估,研究用的参数包括放热率、平均指示压力和热效率。试验结果表明,乙醇着火时刻早于异辛烷;在乙醇中加入异辛烷可以推迟着火,并导致平均指示压力和热效率的降低;对某种特定燃料,HCCI燃烧的发生主要取决于进气充量温度,初始充量温度的增加将导致HCCI燃烧提前;充量温度低或发动机转速低时,混合气形成质量差,对HCCI燃烧有不良影响;指示热效率为30%~43%,其值高于火花点火发动机;预燃室的存在有利于稳定的HCCI燃烧;超稀充量运行可以显著降低NOx排放。     

稀燃对甲醇直喷点燃式发动机性能的影响北大核心CSCD

将一台增压直喷米勒循环汽油机改制成高压缩比(13.8)甲醇直喷点燃式发动机,在2 750 r/min、平均有效压力(brake mean effective pressure,BMEP)为1.1 MPa及1.5 MPa工况下研究了稀燃对甲醇直喷发动机燃烧、排放及热效率的影响。结果表明:随过量空气系数λ增大,甲醇直喷发动机滞燃期和燃烧持续期逐渐延长,高稀释率下燃烧滞燃期和持续期明显短于汽油原机。在1.1 MPa BMEP工况下,发动机的稳定燃烧极限从汽油原机的λ=1.5拓宽到甲醇直喷的1.7以上。气体排放方面,随λ增大,甲醇直喷发动机HC排放逐渐增加,而CO排放先降低后升高,在λ=1.1附近CO排放最低。与汽油原机相比,甲醇直喷发动机在各过量空气系数下均表现出更低的NOx、HC及CO排放。热效率方面,发动机在BMEP为1.1 MPa下,汽油原机和甲醇直喷的最大有效热效率分别为39.8%和44.1%,热效率绝对值分别较当量比燃烧提升2.5%和3.2%。BMEP提高到1.5 MPa后,甲醇直喷发动机在λ=1.4实现了44.5%的最大有效热效率。     

预燃室射流点火技术对汽油机性能影响的研究

在一款增压直喷小型强化废气涡轮增压汽油机上,进行了加装预燃室与传统点火在低速外特性、中转速负荷特性的燃烧特性、经济性和排放特性对比试验,分析了预燃室火焰射流点火过程与传统点火对汽油机性能影响的规律。研究结果表明,在1500r/min、平均有效压力为2MPa工况,采用预燃室点火后缸内燃烧等容度提高,最高燃烧压力增大,燃烧相位提前7.1°,有效燃油消耗率下降约24g/（kW·h）;在2000r/min负荷特性的试验工况,相比于传统点火,预燃室点火燃烧循环变动均获得改善,燃烧持续期缩短,低负荷时燃烧相位不变而比油耗略微上升,高负荷时燃烧相位大幅提前,比油耗改善约7g/（kW·h）,且最高有效热效率由36.9%上升至37.5%。就气体排放物而言,预燃室点火加速燃烧使NOx排放最高上升约15%,HC排放最多下降约36%,而CO排放低负荷时基本维持不变,在高负荷时略有下降。     

纯氢和天然气掺氢燃料发动机的试验研究

在某点燃式发动机上,试验研究了纯氢和不同比例天然气掺氢的燃烧与排放特性。结果表明：纯氢燃料燃烧快,燃烧持续期短,缸压和放热率升高率大且峰值较高,λ=1．1时,峰值压力为3．9MPa,燃烧持续期为12℃A。氢燃料的稀燃界限宽,过量空气系数λ=3时,峰值压力降低到1．7MPa,NOx排放趋于零。天然气掺氢可以改善天然气燃烧特性,拓展天然气的稀燃极限。在相同工况下,掺氢30％的混合气燃烧持续期比天然气缩短20℃A,但缸压峰值和NOx排放增加,这可以通过稀燃和优化点火提前角来降低峰值压力和NOx排放。掺氢30％的混合气可以在λ=1．857时稳定的工作,此时峰值压力降低到1．57MPa,NOx的排放小于50×10^-6。     

湍流射流点火对天然气发动机燃烧特性影响的试验研究

湍流射流点火（Turbulent Jet Ignition,TJI）是一种有效的燃烧增强技术,可提供更高的点火能量,使发动机稳定着火,且可以提高燃烧压力和燃烧速率,缩短燃烧持续期,是实现发动机稀薄燃烧的有效手段。基于一台带有预燃室的点燃式单缸试验机,开展了TJI模式下天然气发动机性能的试验研究。首先,研究了不同过量空气系数下TJI对天然气发动机动力性能、排放性能及燃烧特性的影响,并与火花塞点火（Spark Ignition,SI）模式进行对比;其次,在稀燃条件下分别探究了进气增压和预燃室喷氢对天然气发动机动力性、经济性及燃烧过程的优化作用。结果表明：TJI的使用可有效拓展天然气发动机的稀燃极限,且燃烧滞燃期和燃烧持续期均更短,放热率更高;过量空气系数1.5为甲烷TJI最佳稀燃工况,此时燃油消耗率最低,且可实现氮氧化物近零排放;此外,采用进气增压的方式可以提高TJI发动机在高负荷下的经济性;TJI模式下,相较于预燃室喷甲烷,预燃室喷氢气可进一步缩短滞燃期和燃烧持续期,提高放热率,达到提升TJI性能的效果。     

浅析循环流化床锅炉的三种点火方式

通过对利用燃油点火方式、木柴点火方式、热渣点火方式点燃循环流化床锅炉的经验总结,对利用这三种方式点燃循环流化床锅炉的方法进行了简述,剖析了这三种点火方式的优缺点,并指出了较佳的点火方式。     

A review of spray ignition phenomena: Present status and future research

Theoretical and experimental studies dealing with the spray ignition phenomena are reviewed. Two major topics covered are external-source ignition of liquid fuel sprays and spontaneous spray ignition. Experimental and theoretical investigations of external-source ignition of sprays employing different configurations are discussed first. Three major topics included here are: (i) ignition of quiescent and flowing fuel sprays; (ii) ignition of monodisperse and polydisperse sprays; and (iii) ignition of single-component and multicomponent fuel sprays. Then, experimental studies of autoignition of sprays employing constant-volume enclosures, injection in a uniform air flow, and shock tube techniques, are discussed. Theoretical investigations dealing with spray autoignition phenomena range from phenomenological models to one-dimensional numerical models using global one-step as well as detailed multistep chemistry, and to multidimensional simulations with reduced mechanisms. These models are also discussed in the review. Finally, some advanced topics which are common to both external-source ignition and spontaneous ignition are identified and discussed. An attempt is made to provide a common link between the three dominant ignition modes in sprays, namely individual droplet ignition, droplet cluster ignition, and spray ignition. In a similar manner, common features of external-source ignition and spontaneous ignition of sprays are identified. A general spray ignition model along with important numerical and physical issues are presented. The effect of pressure on spray ignition processes is also discussed. Potential topics for further research are suggested.     

Effects of turbulence on nonpremixed ignition of hydrogen in heated counterflow

Experiments were conducted to determine the effects of turbulence on the temperature of a heated air jet required to ignite a counterflowing cold hydrogen/nitrogen jet. In contrast to pseudo-turbulent flows, where turbulence was generated by only a perforated plate on the fuel side, resulting in little effect on ignition in a hydrogen system, fully turbulent flows with perforated plates on both sides of the flow were found to produce noticeable effects. The difference was attributed to the fact that in fully turbulent flows, a significantly larger range of turbulent eddies extend to smaller scales than in pseudo-turbulent flows. At atmospheric pressure, the lowest turbulence intensity studied had ignition temperatures notably lower than laminar ones, while further increases in turbulence intensity resulted in rising ignition temperatures. As a result, optimal conditions for nonpremixed hydrogen ignition exist in weakly turbulent flows where the ignition temperature is lower than can be obtained in other laminar or turbulent flows at the same pressure. Similar trends were seen for all fuel concentrations and at all pressures in the second ignition limit (below 3-4 atm). At higher pressures, turbulent flows caused the ignition temperatures to continue to follow the second limit resulting in ignition temperatures higher than the laminar values. The extension of the second limit ends at the highest pressures (7 to 8 atm) where evidence of third limit behavior appears. Three mechanisms were noted to explain the experimental results. First, turbulent eddies similar in size to the ignition kernel can promote discrete mixing of otherwise isolated pockets of gas. Second, this mixing can promote HO₂ chain branching pathways, which can account for the enhanced ignition noted in the second limit where reaction is governed by crossover temperature chemistry. Third, turbulence limits the excursion times available for reaction, inordinately affecting the slower HO₂ reactions. This is responsible for the increasing ignition temperature with turbulence intensity and pressure.     

An experimental study on ignition of single coal particles at low oxygen concentrations

An experimental study on the ignition of single coal particles at low oxygen concentrations (X_{{\mathrm{O}}_2}<21%) was conducted using a tube furnace. The surface temperature (T_s) and the center temperature (T_c) of the coal particles were obtained from the images taken by an infrared camera and thermocouples respectively. The ignition processes were recorded by a high-speed camera at different X_{{\mathrm{O}}_2} values and furnace temperatures T_w. Compared with literature experimental data obtained at a high X_{{\mathrm{O}}_2} value, the ignition delay time t_i decreases more rapidly as X_{{\mathrm{O}}_2} increases at the low X_{{\mathrm{O}}_2} region. The responses of T_s and T_c to the variation of X_{{\mathrm{O}}_2} are different: T_s decreases while T_c remains nearly constant with increasing X_{{\mathrm{O}}_2} at a low X_{{\mathrm{O}}_2} value. In addition, t_i is less sensitive to T_w while the ignition temperature T_i is more sensitive to T_w at a low X_{{\mathrm{O}}_2} value than in air. Observations of the position of flame front evolution illustrate that the ignition of a coal particle may change from a homogeneous mode to a heterogeneous or combined ignition mode as X_{{\mathrm{O}}_2} decreases. At a low X_{{\mathrm{O}}_2} value, buoyancy plays a more significant role in sweeping away the released volatiles during the ignition process.     

煤粉气流强迫点火特性试验研究

在一座小型煤粉燃烧试验台上,对不同条件下,两种煤粉气流的强迫点火特性进行了试验研究。结果表明,用火炬引燃煤粉气流,存在一个对应于最低煤粉浓度的最佳点燃速度;煤粉气流的着火界限主要受初始温度、点火源温度、煤种和煤粉细度的影响;提高煤粉气流的初始温度、点火源温度和煤粉细度均可使着火范围变宽,挥发份含量高的煤种点火容易。在相同条件下,直流煤粉气流比旋转煤粉气流容易点燃。     

无油直接点火燃烧器在煤粉锅炉上应用的若干问题

无油直接点火燃烧器在常规煤粉锅炉中的应用 ,是一个重要的科技改进。同时 ,这一技术在不断的完善。点火燃烧器的功能 ,在开始的若干工程实践中 ,使其仅具有点火与稳燃功能 ,应该是比较客观的 ,待该技术日益成熟之后 ,使其具有主燃烧器的功能。需从点火器本身功能的加强与合理的点火器布置、形成一个良好的空气动力场两个方面强化点火燃烧器的点火能力。无油直接点火燃烧器在锅炉启动过程中 ,与以前的油枪点火有很大的不同 ,需要对启动程序以及相应的设备进行调整     

Pulverized coal particle ignition in a combustion environment with a reducing-to-oxidizing transition

A reducing-to-oxidizing (RO) environment is characteristic of what a coal particle experiences in the near-burner region of pulverized coal (pc) furnaces. The RO environment can influence early-stage coal combustion processes such as ignition, aerosol formation, and char burnout. However, fundamental studies have focused on either oxidizing conditions (mimicking the post-flame region) or reducing conditions (mimicking the devolatilization region). The effect of this RO environment on early-stage coal combustion has, until now, not been considered. Here, the role of this reducing-to-oxidizing environment on single-particle ignition is evaluated. Powder River Basin (PRB) sub-bituminous coal was used, with a particle size of 125–149 μm and two nominal gas temperatures of 1300 K and 1800 K. The experimental findings for purely-oxidizing conditions with 20 vol% oxygen are compared with those of reducing-to-oxidizing environment. Single particles were tracked using high speed, high resolution videography. Emission intensities of the particles were used to evaluate the prevailing ignition modes, and to determine the characteristic ignition and induction times in both oxidizing and reducing-to-oxidizing environments. Experimental findings show that homogeneous-to-heterogeneous mode of ignition is prevalent for purely oxidizing conditions for both nominal gas temperatures of 1300 K and 1800 K. However, hetero-homogeneous ignition is favored in reducing-to-oxidizing environment at 1800 K and heterogeneous ignition at 1300 K gas flame temperature. The reducing-to-oxidizing environment leads to longer ignition delay times of about 20% and 40% on average for 1300 K and 1800 K nominal gas temperatures respectively but shorter induction times than those of oxidizing condition. The results show that ignition behavior in a reducing-to-oxidizing post-flame environments can be quite different from those in oxidizing environments.     

An approach of droplet ignition delay time

When a droplet is suddenly injected into a high‐temperature environment, the droplet self‐ignition phenomenon occurs. A simple model, based on the temperature history of target gas mixture of which the equivalent ratio is equal to 1, was proposed to predict the droplet ignition delay time in this paper. This approach clearly divides the droplet self‐ignition delay into two parts, the physical delay and the chemical delay. The predicted droplet ignition times agree well with the experimental data and numerical simulation results. In addition, the influence of droplet diameter on the droplet ignition delay was discussed in detail using this approach. © 2008 Wiley Periodicals, Inc. Heat Trans Asian Res; Published online in Wiley InterScience ( www.interscience.wiley.com ). DOI 10.1002/htj.20240     

我国电站燃煤锅炉节油点火技术的分析及现状

针对现阶段我国电站燃煤锅炉运行状况,分析微油点火技术和等离子点火技术的工作原理、系统组成及应用,从技术和经济的角度指出其各自的特点,并对节油及运行中出现的问题提出改进措施。