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CN111472891A - 一种柴油引燃天然气发动机燃烧系统及其控制方法 - Google Patents

一种柴油引燃天然气发动机燃烧系统及其控制方法 Download PDF

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CN111472891A
CN111472891A CN202010336977.6A CN202010336977A CN111472891A CN 111472891 A CN111472891 A CN 111472891A CN 202010336977 A CN202010336977 A CN 202010336977A CN 111472891 A CN111472891 A CN 111472891A
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natural gas
engine
diesel
cylinder
valve
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陈贵升
张敬贤
沈颖刚
李冰
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Kunming University of Science and Technology
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Abstract

本发明涉及一种柴油引燃天然气发动机燃烧系统及其控制方法,包括发动机主体、柴油进气系统、天然气进气系统、可变截面涡轮增压器VGT、废气再循环系统EGR、可变气门调节器VVT、双燃料ECU、综合ECU、计算机、电源;废气再循环系统EGR包括EGR中冷器、EGR阀。本发明根据发动机不同运行工况,通过调节气道和缸内喷气阀喷气策略实现燃气量的精确控制,在气缸内形成不同充量和分层状态的混合气,在此基础上耦合热力学状态控制,通过可变气门调节器VVT与废气再循环系统EGR联合控制并配合不同当量比,实现各个工况下的稳定着火和可控分层燃烧,并进一步提升双燃料发动机的天然气替代比例,实现更宽工况运行范围内的高效、清洁燃烧。

Description

一种柴油引燃天然气发动机燃烧系统及其控制方法
技术领域
本发明涉及一种柴油引燃天然气发动机燃烧系统及其控制方法,属于内燃机燃烧技术领域。
技术背景
面对环境污染,日趋苛刻的排放法规不断推动内燃机向零排放迈进。在众多代用燃料中,天然气因存储量丰富且价格低廉,现已广泛应用于重型卡车、城市公交、船舶等领域。天然气主要成分是甲烷(CH4),具有辛烷值高、化学活性低和抗爆性能好等特点,利于发动机提高平均有效压力(BMEP)和热效率(可提高压缩比);同时,天然气的H/C比率高、含硫低且无芳香烃,利于降低颗粒物和CO2排放;此外,天然气层流火焰传播速度慢、可燃界限宽,利于减少NOx和扩展稀燃极限。因此,天然气作为低碳燃料被视为具有实现发动机高效洁净燃烧与降低CO2的优质替代燃料。目前,天然气发动机中天然气主要采用进气道喷射(Port Fuel Injection-PFI)方式。这种方式在小负荷工况,随替代率增加,缸内混合气越加均匀,混合气化学活性及活性分层降低导致燃烧稳定性变差且易失火;在大负荷工况,大量均质混合气快速燃烧,通常采用降低压缩比、推迟燃烧相位或高比例EGR稀释等手段避免爆震以提升替代率,但导致热效率下降。缸内形成大量均质混合气是导致天然气点火和高替代率天然气/柴油发动机小负荷燃烧稳定性差、大负荷易爆震(压缩比受限)的根本原因。而相比气道喷射,采用天然气缸内直喷模式,可提高发动机小负荷燃烧稳定性、扩展稀燃极限并抑制大负荷燃烧速率。但是这种方式,天然气与空气混合时间较短,缸内混合气不均匀,起燃时刻混合气浓度或成分易因缸内流场和湍流脉动发生循环变动,且天然气直喷气相射流贯穿距离和湍动能明显低于液体燃料,影响缸内燃烧过程。
发明内容
本发明的目的在于提供一种柴油引燃天然气发动机燃烧系统及其控制方法,借助天然气直喷和气道复合喷射策略、可变气门技术、废气再循环策略实现天然气缸内分层与热力学状态耦合控制的柴油引燃天然气发动机燃烧,解决目前天然气进气道喷射发动机面临的高替代率下小负荷燃烧稳定性差、高压缩比下大负荷易爆震等问题,并进一步提升双燃料发动机的天然气替代比例,实现更宽工况运行范围内的高效、清洁燃烧。
本发明采用的技术方案是:一种柴油引燃天然气发动机燃烧系统,包括发动机主体、柴油进气系统、天然气进气系统、可变截面涡轮增压器VGT29、废气再循环系统EGR、可变气门调节器VVT12、双燃料ECU13、综合ECU15、计算机14、电源19;废气再循环系统EGR包括EGR中冷器22、EGR阀25;
发动机主体包括气缸盖32、气缸33、活塞34、气门11,气缸盖32、气缸33和活塞34构成燃烧室,天然气进气系统包括天然气罐1、天然气轨5、天然气气道喷射器7、天然气缸内喷射器8,天然气罐1与天然气轨5之间的气道上设有进气调节器4,天然气轨5的两个出气口分别连接天然气气道喷射器7、天然气缸内喷射器8,天然气轨5上方安装有天然气压力和温度传感器6,天然气气道喷射器7安装在气缸33前的进气道35上,天然气缸内喷射器8安装在燃烧室顶部,空气过滤器30与可变截面涡轮增压器VGT29连接,可变截面涡轮增压器VGT29的一端通过空气中冷器31与气缸33前的进气道35连接,另一端连接在气缸33后的排气道36上,气缸33后的排气道36上设有分支废气排气道,分支废气排气管道通过EGR中冷器22与EGR阀25连接,EGR阀25的出气端与气缸33前的进气道35连接,气门11与可变气门调节器VVT12连接,进气调节器4、天然气轨5、天然气压力和温度传感器6、天然气气道喷射器7、天然气缸内喷射器8均与双燃料ECU13连接,可变气门调节器VVT12、可变截面涡轮增压器VGT29、EGR阀25均与综合ECU15连接,双燃料ECU13、综合ECU15均与计算机14连接,双燃料ECU13、综合ECU15均与电源19连接。
优选地,所述的天然气进气系统还包括与双燃料ECU13连接的关闭阀2、流量计3,关闭阀2、流量计3安装在天然气罐1与进气调节器4之间的气道上。
优选地,所述的柴油供油系统包括油箱18、高压油泵16、柴油滤清器17、柴油高压共轨9、柴油喷油器10,油箱18通过高压油泵16和柴油滤清器17连通柴油共轨9,柴油共轨9的出油端连接柴油喷油器10,柴油喷油器10安装在燃烧室顶部,高压油泵16、柴油滤清器17、柴油共轨9、柴油喷油器10均与综合ECU15连接。
优选地,所述柴油共轨9上设有与综合ECU15连接的柴油轨压传感器。
优选地,所述可变气门调节器VVT12上设有气门位置传感器、进气道35内设有氧传感器,排气道36内设有废气温度和压力传感器,气门位置传感器、氧传感器、废气温度和压力传感器均与综合ECU15连接。
优选地,所述发动机主体外部连接用来测功的涡流测功机24、控制发动机运行工况的发动机控制器20、发动机油路和水路控制器21,发动机曲轴位置安装有曲轴位置传感器23,涡流测功机24与发动机控制器20连接,曲轴位置传感器23、发动机控制器20、发动机油路和水路控制器21均与综合ECU15连接。
优选地,所述的排气道36的尾端设有尾气分析仪27、烟气分析仪28,尾气分析仪27、烟气分析仪28均与综合ECU15连接。
一种所述的柴油引燃天然气发动机燃烧系统的控制方法,
在发动机压缩行程中、前期,采用天然气缸内直喷或直喷和气道复合喷射模式形成不同当量比梯度分布的天然气和空气分层混合气,依靠压缩上止点附近喷射少量柴油低温和高温燃烧反应诱导形成的活化热氛围触发点燃,实现气缸内分层混合气多点可控燃烧,在此基础上与可变截面涡轮增压器VGT29、废气再循环系统EGR的缸内热力学状态调控手段相结合,实现耦合协同控制;
当发动机处于低负荷时,基于发动机压缩行程中、前期时混合气浓度分层调控,结合可变气门调节器VVT12,通过可变气门调节器VVT12控制气门11在排气行程中使进气门二次开启以及在进气行程中使排气门二次开启,从而实现高温废气倒吸入进气道35后再进入气缸33内,排气道36内高温废气倒吸入气缸33内的两种内部EGR模式,再与EGR阀25控制的外部EGR循环系统联合控制,并利用可变截面涡轮增压器VGT29改变增压条件进而调节不同当量比,实现对缸内热力学状态的控制;
当发动机处于大负荷时,基于发动机压缩行程中、前期时所述的混合气浓度分层调控,通过控制进气调节器4、天然气轨5、天然气缸内喷射器8改变天然气直喷策略,并借助可变气门调节器VVT12控制气门11实现进气门晚关策略,两者实现耦合控制。此基础上,配合可变截面涡轮增压器VGT29实现的进气增压等燃烧控制手段对燃烧进行综合优化。
本发明的有益效果是:本发明通过天然气复合喷射策略优化实现对缸内天然气浓度分层的灵活调控,并协同柴油直喷策略控制缸内诱导引燃活化空间热分层实现对缸内混合气浓度分层调控;通过VVT技术和EGR技术的应用,实现缸内热力学状态的调控;通过VGT技术的应用,实现当量比的优化匹配;综合以上的应用,能满足发动机不同负荷工况的要求,提高发动机高替代下小负荷燃烧稳定性,抑制高压缩比下大负荷爆震,并进一步提升双燃料发动机的天然气替代比例,实现更宽工况运行范围内的高效、清洁燃烧。
附图说明
图1是本发明的燃烧系统示意图;
图2为图1中活塞、气缸、气缸盖部分的结构放大图。
图中各标号为:1-天然气罐、2-关闭阀、3-气体质量流量计、4-进气调节器、5-天然气轨、6-天然气压力和温度传感器、7-天然气气道喷射器、8-天然气缸内喷射器、9-柴油共轨、10-柴油喷油器、11-气门、12-可变气门调节器VVT、13-双燃料ECU、14-计算机、15-综合ECU、16-高压油泵、17-柴油滤清器、18-油箱、19-电池、20-发动机控制器、21-发动机油路和水路控制器、22-EGR中冷器、23-曲轴位置传感器、24-涡流测功机、25-EGR阀、26-废气温度和压力传感器、27-尾气分析仪、28-烟气分析仪、29-可变截面涡轮增压器VGT、30-空气过滤器、31-空气中冷器、32-气缸盖、33-气缸、34-活塞、35-进气道、36-排气道。
具体实施方式
下面结合附图和具体实施例对本发明做更详细地描述。
实施例1:如图1-2所示,一种柴油引燃天然气发动机燃烧系统,包括发动机主体、柴油进气系统、天然气进气系统、可变截面涡轮增压器VGT29、废气再循环系统EGR、可变气门调节器VVT12、双燃料ECU13、综合ECU15、计算机14、电源19;废气再循环系统EGR包括EGR中冷器22、EGR阀25;
发动机主体包括气缸盖32、气缸33、活塞34、气门11,气缸盖32、气缸33和活塞34构成燃烧室,天然气进气系统包括天然气罐1、天然气轨5、天然气气道喷射器7、天然气缸内喷射器8,天然气罐1与天然气轨5之间的气道上设有进气调节器4,天然气轨5的两个出气口分别连接天然气气道喷射器7、天然气缸内喷射器8,天然气轨5上方安装有天然气压力和温度传感器6,天然气气道喷射器7安装在气缸33前的进气道35上,天然气缸内喷射器8安装在燃烧室顶部,空气过滤器30与可变截面涡轮增压器VGT29连接,可变截面涡轮增压器VGT29的一端通过空气中冷器31与气缸33前的进气道35连接,另一端连接在气缸33后的排放道36上,气缸33后的排气道36上设有分支废气排气道,分支废气排气道通过EGR中冷器22与EGR阀25连接,EGR阀25的出气端与气缸33前的进气道35连接,气门11与可变气门调节器VVT12连接,进气调节器4、天然气轨5、天然气压力和温度传感器6、天然气气道喷射器7、天然气缸内喷射器8均与双燃料ECU13连接,可变气门调节器VVT12、可变截面涡轮增压器VGT29、EGR阀25均与综合ECU15连接,双燃料ECU13、综合ECU15均与计算机14连接,双燃料ECU13、综合ECU15均与电源19连接。
进一步地,所述的天然气进气系统还包括与双燃料ECU13连接的关闭阀2、流量计3,关闭阀2、流量计3安装在天然气罐1与进气调节器4之间的气道上。通过关闭阀2、流量计3可以使双燃料ECU13很好的控制天然气进气量。
进一步地,所述的柴油供油系统包括油箱18、高压油泵16、柴油滤清器17、柴油共轨9、柴油喷油器10,油箱18通过高压油泵16和柴油滤清器17连通柴油共轨9,柴油共轨9的出油端连接柴油喷油器10,柴油喷油器10安装在燃烧室顶部,高压油泵16、柴油滤清器17、柴油共轨9、柴油喷油器10均与综合ECU15连接。
进一步地,所述柴油共轨9上设有与综合ECU15连接的柴油轨压传感器。
进一步地,所述可变气门调节器12上设有气门位置传感器、进气道35内设有氧传感器,排气道36内设有废气温度和压力传感器,气门位置传感器、氧传感器、废气温度和压力传感器均与综合ECU15连接。
进一步地,所述发动机主体外部连接用来测功的涡流测功机24、控制发动机运行工况的发动机控制器20、发动机油路和水路控制器21,发动机曲轴位置安装有曲轴位置传感器23,涡流测功机24与发动机控制器20连接,曲轴位置传感器23、发动机控制器20、发动机油路和水路控制器21均与综合ECU15连接。曲轴位置传感器23是为了进一步监测发动机工况,安置在曲轴位置。
进一步地,所述的排气道36的尾端设有尾气分析仪27、烟气分析仪28,尾气分析仪27、烟气分析仪28均与综合ECU15连接。综合ECU15根据尾气分析仪27、烟气分析仪28可以很清楚的知道发动机是否充分燃烧。
发动机主体包括较多结构,这里仅以单一气缸为基准来描述本发明相关内容,电控单元综合ECU15、双燃料ECU13由电池19提供电源,各个检测传感器由两ECU13、15提供电源。发动机有两套燃料供给系统。第一套柴油喷射供给系统包括安装在气缸内的柴油喷油器10,柴油喷油器10通过供油管路先连接至柴油共轨9,再连接至油箱18,在供油管路上安装有高压油泵16和柴油滤清器17,喷油器10、高压油泵16和柴油共轨9均与发动机控制单元综合ECU15电连接,可通过计算机14控制柴油喷射策略。第二套天然气喷射供给系统包括位于气缸内的天然气缸内喷射器8、位于进气道35内的天然气气道喷射器7,两喷射器均先通过燃气管路连接至天然气轨5,再连接至天然气罐1,在供气管路上安装有控制气体流量的关闭阀2、进气调节器4、测量流量的气体质量流量计3,在天然气轨5上还安装有天然气压力和温度传感器6,天然气压力和温度传感器6与天然气气道喷射器7、天然气缸内喷射器8均与双燃料控制单元ECU13电连接,可通过计算机14改变天然气喷射策略。空气经过空气过滤器30进入进气系统,在可变截面涡轮增压器29的作用下进行增压,增压后温度升高,进入中冷器31降温,以提高充量系数,其中可变截面涡轮增压器29开度可由计算机14通过综合ECU15控制。针对排放问题,加入了废气再循环系统EGR,高温废气可通过排气道36的分支经EGR中冷器22冷却后,通过由控制单元综合ECU15控制的EGR阀25回到进气系统。为实现缸内成分分层采用了可变气门调节器VVT12,由综合ECU15控制可变气门调节器VVT12调节气门11运动来实现。此外,为了检测本系统的排放特性,在排气道36中设置了废气道温度和压力传感器26,在尾端还设置了尾气分析仪27和烟气分析仪28。
双燃料ECU 13用于控制柴油和天然气两种燃料供给以及喷射系统并能完成其自动、平顺调节,综合ECU 15能实现可变气门调节器VVT12内气门11控制、可变截面涡轮增压器VGT29内涡流截面导流叶片控制、EGR阀25开度控制并能对发动机主体进行有效控制的,计算机14用于处理数据、提供计算、记录和分析。
一种所述的柴油引燃天然气发动机燃烧系统的控制方法,其具体如下:
在发动机压缩行程中、前期,天然气依靠天然气气道喷射器7、天然气缸内喷射器8采用缸内直喷或直喷和气道复合双喷射,电控单元的双燃料ECU 13根据发动机实际工况调整复合喷射比例、喷射定时、喷射压力和喷射量,形成不同当量比梯度分布的天然气和空气分层混合气,并依靠双燃料ECU13调控喷油器10在压缩上止点附近喷射少量的柴油形成的活化热氛围(活性基、易燃中间产物、温度)触发点燃,实现缸内分层混合气多点可控燃烧。这种模式既可以借助少量直喷引燃柴油在缸内形成稳定的多点点火源诱导引燃优点,又可以灵活发挥直喷分层协同气道喷射提高高替代率下小负荷燃烧稳定性与抑制高压缩比下大负荷燃烧速率的双重优势,有利于进一步提升双燃料发动机的天然气替代比例,实现更宽工况运行范围内的高效、清洁燃烧。
当发动机处于小负荷时,基于发动机压缩行程中、前期时混合气浓度分层调控,由综合ECU 15控制发动机的可变气门调节器VVT12来控制气门11在排气行程中使进气门二次开启以及在进气行程中使排气门二次开启,从而实现高温废气倒吸入进气道35后再进入气缸33内,排气道36内高温废气倒吸入气缸33内的两种内部EGR模式。与由综合ECU 15控制EGR阀25开度实现的外部EGR循环系统联合控制,可改善内燃机低温燃烧小负荷工况的燃烧、性能及排放(降低NOx),同时通过高温废气加热使缸内工质温度升高,可以提升排气温度,有利于尾气后处理。再配合综合ECU 15控制可变截面涡轮增压器29内涡轮叶片开度实现的增压条件,进而实现不同进气量即当量比的调控,可同时保持较高缸内温度和氧浓度,从而拓展稳定运行的负荷下限。这样3种技术的结合,完成了对缸内热力学状态(压力、温度、活性热分层)的控制,为进一步提升发动机小负荷燃烧稳定性并降低柴油引燃量(提高替代率)提供途径。
当发动机处于大负荷时,若仅借助天然气/柴油复合直喷策略形成浓度梯度较高的分层混合气来抑制爆震,则会导致颗粒物和过稀区域增加。与此同时,EGR是目前降低NOx最主要的机内净化手段,采用EGR会导致缸内氧浓度降低,增强混合气高浓度分层对颗粒物生成的贡献度;而采用混合气适度分层,则抑制爆震的作用又会减弱。Miller(米勒循环)通过进气门在下止点前和后关闭(早关、晚关)可使发动机实际压缩比与膨胀比分离,且有效压缩行程小于膨胀行程。大量研究表明,基于进气门晚关的米勒循环能有效控制缸内热力状态(缸内最高压力,温度)而抑制发动机爆震、扩展发动机压缩比应用范围,其是提升均质或准均质新型内燃机热效率的一种高效热力循环。故将天然气直喷技术与气门控制技术结合,借助综合ECU 15控制的可变气门调节器VVT12实现进气门晚关策略(米勒热力循环),并配合控制EGR阀25开度来调控的外部中冷EGR率(降低NOx排放、降低燃烧反应速率以一直爆震),利用可变截面涡轮增压器29调节的进气增压(削弱进气门晚关对进气的不理影响,提高中冷EGR率应用范围)等燃烧控制手段综合优化,可以实现高效、低排放的同时抑制爆震,为提高压缩比以提升热效率提供途径。
以上结合附图对本发明的具体实施方式作了详细说明,但是本发明并不限于上述实施方式,在本领域普通技术人员所具备的知识范围内,还可以在不脱离本发明宗旨的前提下作出各种变化。

Claims (8)

1.一种柴油引燃天然气发动机燃烧系统,其特征在于:包括发动机主体、柴油进气系统、天然气进气系统、可变截面涡轮增压器VGT(29)、废气再循环系统EGR、可变气门调节器VVT(12)、双燃料ECU(13)、综合ECU(15)、计算机(14)、电源(19);废气再循环系统EGR包括EGR中冷器(22)、EGR阀(25);
发动机主体包括气缸盖(32)、气缸(33)、活塞(34)、气门(11),气缸盖(32)、气缸(33)和活塞(34)构成燃烧室,天然气进气系统包括天然气罐(1)、天然气轨(5)、天然气气道喷射器(7)、天然气缸内喷射器(8),天然气罐(1)与天然气轨(5)之间的气道上设有进气调节器(4),天然气轨(5)的两个出气口分别连接天然气气道喷射器(7)、天然气缸内喷射器(8),天然气轨(5)上方安装有天然气压力和温度传感器(6),天然气气道喷射器(7)安装在气缸(33)前的进气道(35)上,天然气缸内喷射器(8)安装在燃烧室顶部,空气过滤器(30)与可变截面涡轮增压器VGT(29)连接,可变截面涡轮增压器VGT(29)的一端通过空气中冷器(31)与气缸(33)前的进气道(35)连接,另一端连接在气缸(33)后的排气道(36)上,气缸(33)后的排气道(36)上设有分支废气排气道,分支废气排气道通过EGR中冷器(22)与EGR阀(25)连接,EGR阀(25)的出气端与气缸(33)前的进气道(35)连接,气门(11)与可变气门调节器VVT(12)连接,进气调节器(4)、天然气轨(5)、天然气压力和温度传感器(6)、天然气气道喷射器(7)、天然气缸内喷射器(8)均与双燃料ECU(13)连接,可变气门调节器VVT(12)、可变截面涡轮增压器VGT(29)、EGR阀(25)均与综合ECU(15)连接,双燃料ECU(13)、综合ECU(15)均与计算机(14)连接,双燃料ECU(13)、综合ECU(15)均与电源(19)连接。
2.根据权利要求1所述的柴油引燃天然气发动机燃烧系统,其特征在于:所述的天然气进气系统还包括与双燃料ECU(13)连接的关闭阀(2)、流量计(3),关闭阀(2)、流量计(3)安装在天然气罐(1)与进气调节器(4)之间的气道上。
3.根据权利要求1所述的柴油引燃天然气发动机燃烧系统,其特征在于:所述的柴油供油系统包括油箱(18)、高压油泵(16)、柴油滤清器(17)、柴油共轨(9)、柴油喷油器(10),油箱(18)通过高压油泵(16)和柴油滤清器(17)连通柴油共轨(9),柴油共轨(9)的出油端连接柴油喷油器(10),柴油喷油器(10)安装在燃烧室顶部,高压油泵(16)、柴油滤清器(17)、柴油共轨(9)、柴油喷油器(10)均与综合ECU(15)连接。
4.根据权利要求3所述的柴油引燃天然气发动机燃烧系统,其特征在于:所述柴油共轨(9)上设有与综合ECU(15)连接的柴油轨压传感器。
5.根据权利要求1所述的柴油引燃天然气发动机燃烧系统,其特征在于:所述的可变气门调节器VVT(12)上设有气门位置传感器、进气道(35)内设有氧传感器,排气道(36)内设有废气温度和压力传感器(26),气门位置传感器、氧传感器、废气温度和压力传感器(26)均与综合ECU(15)连接。
6.根据权利要求1所述的柴油引燃天然气发动机燃烧系统,其特征在于:所述发动机主体外部连接用来测功的涡流测功机(24)、控制发动机运行工况的发动机控制器(20)、发动机油路和水路控制器(21),发动机曲轴位置安装有曲轴位置传感器(23),涡流测功机(24)与发动机控制器(20)连接,曲轴位置传感器(23)、发动机控制器(20)、发动机油路和水路控制器(21)均与综合ECU(15)连接。
7.根据权利要求1所述的柴油引燃天然气发动机燃烧系统,其特征在于:所述的排气道(36)的尾端设有尾气分析仪(27)、烟气分析仪(28),尾气分析仪(27)、烟气分析仪(28)均与综合ECU(15)连接。
8.一种权利要求1-7任一项所述的柴油引燃天然气发动机燃烧系统的控制方法,其特征在于:
在发动机压缩行程中、前期,采用天然气缸内直喷或直喷和气道复合喷射模式形成不同当量比梯度分布的天然气和空气分层混合气,依靠压缩上止点附近喷射少量柴油低温和高温燃烧反应诱导形成的活化热氛围触发点燃,实现气缸内分层混合气多点可控燃烧,在此基础上与可变截面涡轮增压器VGT(29)、废气再循环系统EGR的缸内热力学状态调控手段相结合,实现耦合协同控制;
当发动机处于低负荷时,基于发动机压缩行程中、前期时混合气浓度分层调控,结合可变气门调节器VVT(12),通过可变气门调节器VVT(12)控制气门(11)在排气行程中使进气门二次开启以及在进气行程中使排气门二次开启,从而实现高温废气倒吸入进气道(35)后再进入气缸(33)内,排气道(36)内高温废气倒吸入气缸(33)内的两种内部EGR模式,再与EGR阀(25)控制的外部EGR循环系统联合控制,并利用可变截面涡轮增压器VGT(29)改变增压条件进而调节不同当量比,实现对缸内热力学状态的控制;
当发动机处于大负荷时,基于发动机压缩行程中、前期时所述的混合气浓度分层调控,通过控制进气调节器(4)、天然气轨(5)、天然气缸内喷射器(8)改变天然气直喷策略,并借助可变气门调节器VVT(12)控制气门(11)实现进气门晚关策略,两者实现耦合控制,此基础上,配合可变截面涡轮增压器VGT(29)实现的进气增压等燃烧控制手段对燃烧进行综合优化。
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