CN107939558B - An internal combustion engine exhaust system with exhaust gas recirculation - Google Patents
An internal combustion engine exhaust system with exhaust gas recirculation Download PDFInfo
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- CN107939558B CN107939558B CN201710928487.3A CN201710928487A CN107939558B CN 107939558 B CN107939558 B CN 107939558B CN 201710928487 A CN201710928487 A CN 201710928487A CN 107939558 B CN107939558 B CN 107939558B
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/02—EGR systems specially adapted for supercharged engines
- F02M26/04—EGR systems specially adapted for supercharged engines with a single turbocharger
- F02M26/05—High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/08—Other arrangements or adaptations of exhaust conduits
- F01N13/10—Other arrangements or adaptations of exhaust conduits of exhaust manifolds
- F01N13/107—More than one exhaust manifold or exhaust collector
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
- F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/13—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
- F02M26/14—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories in relation to the exhaust system
- F02M26/16—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories in relation to the exhaust system with EGR valves located at or near the connection to the exhaust system
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Exhaust-Gas Circulating Devices (AREA)
- Supercharger (AREA)
Abstract
本发明公布了一种带废气再循环的内燃机排气系统,包括多个发动机气缸、排气歧管、EGR阀、EGR冷却器、进气歧管、涡轮机、增压器压气机、增压中冷器和中冷后进气管;其特征在于:多个所述发动机气缸分组分别连接多根所述排气歧管;所述涡轮机具有多个涡轮蜗壳腔室通向涡轮叶轮;多根所述排气歧管分别进入对应的多个所述涡轮蜗壳腔室;至少部分所述排气歧管同时与所述EGR阀相连接。本发明的有益效果在于三流道增压器蜗壳和排气歧管布置更有利于减小各缸排气间干扰,利用排气脉冲效应,便于排气能量的保持。本发明的有益效果还在于三流道增压器蜗壳内设置有不同截面积蜗壳腔,可以形成不同梯度的蜗壳非对称度,便于发动机不同工况下EGR率优化。
The invention discloses an internal combustion engine exhaust system with exhaust gas recirculation, including a plurality of engine cylinders, exhaust manifolds, EGR valves, EGR coolers, intake manifolds, turbines, supercharger compressors, supercharger Air cooler and intercooling rear intake pipe; it is characterized in that: a plurality of said engine cylinders are grouped and respectively connected with a plurality of said exhaust manifolds; said turbine has a plurality of turbine volute chambers leading to the turbine impeller; a plurality of said Exhaust manifolds respectively enter the corresponding plurality of turbine volute chambers; at least part of the exhaust manifolds are simultaneously connected with the EGR valve. The beneficial effect of the invention is that the three-channel supercharger volute and the exhaust manifold arrangement are more conducive to reducing the interference between the exhaust of each cylinder, and the exhaust pulse effect is used to facilitate the maintenance of exhaust energy. The beneficial effect of the present invention is that the volute chambers of different cross-sectional areas are arranged in the volute of the three-channel supercharger, which can form the asymmetry of the volute with different gradients, and facilitate the optimization of the EGR rate under different working conditions of the engine.
Description
技术领域technical field
本发明属于涡轮增压内燃机技术领域,特别是涉及一种采用非对称涡轮增压器的带废气再循环的内燃机排气系统。The invention belongs to the technical field of turbocharged internal combustion engines, in particular to an exhaust system of an internal combustion engine with exhaust gas recirculation using an asymmetrical turbocharger.
背景技术Background technique
为满足发动机排放要求,通过非对称涡轮增压器、EGR阀及相关排气系统为发动机提供恰当的EGR率。In order to meet the engine emission requirements, the engine is provided with the proper EGR rate through the asymmetric turbocharger, EGR valve and related exhaust system.
目前存在的解决方案主要为专利CN104508284(A)所公开的内容,即通过非对称双流道增压器和所述的EGR阀,通过控制EGR阀来满足发动机不同工况下EGR率要求。其不足之处在于,当涡轮机蜗壳非对称度较大时,难以产生大的废气压力,只能通过强制EGR阀来满足EGR率要求。而非对称度较小时,在高速大负荷,排气背压较高,将产生过大EGR率。Daimler公司倾向于采用采用较大的非对称度,在部分工况通过强制EGR阀来满足EGR率要求。The currently existing solution is mainly disclosed in the patent CN104508284 (A), that is, through the asymmetric dual-channel supercharger and the EGR valve, the EGR rate requirements under different working conditions of the engine are met by controlling the EGR valve. Its disadvantage is that when the asymmetry of the turbine volute is large, it is difficult to generate a large exhaust gas pressure, and the EGR rate requirement can only be met through a forced EGR valve. When the asymmetry is small, at high speed and heavy load, the exhaust back pressure is high, and an excessive EGR rate will be generated. Daimler tends to adopt a larger asymmetry and meet the EGR rate requirements by forcing the EGR valve in some working conditions.
该方案的主要缺点为:1)三缸共用一个蜗壳排气流道,使得各缸间排气能量耗散较多。2)强制EGR阀直接承受高温排气冲刷,带来较高的热负荷,可靠性较差。此外,强制EGR阀也带来排气能量的损耗。The main disadvantages of this solution are: 1) The three cylinders share one volute exhaust flow channel, which causes more exhaust energy dissipation among the cylinders. 2) The forced EGR valve is directly subjected to high-temperature exhaust scour, which brings high thermal load and poor reliability. In addition, the forced EGR valve also brings exhaust energy loss.
发明内容Contents of the invention
本发明的目的在于提供一种涡轮增压器及采用非对称涡轮增压器的带废气再循环的内燃机排气系统,在满足发动机EGR率的同时,尽可能提高涡轮增压器排气能量利用率。The purpose of the present invention is to provide a turbocharger and an internal combustion engine exhaust system with exhaust gas recirculation using an asymmetrical turbocharger, which can improve the exhaust energy utilization of the turbocharger as much as possible while satisfying the EGR rate of the engine Rate.
本发明为实现上述目的,采用如下技术方案:In order to achieve the above object, the present invention adopts the following technical solutions:
一种带废气再循环的内燃机排气系统,包括多个发动机气缸、排气歧管、EGR阀、EGR冷却器、进气歧管、涡轮机、增压器压气机、增压中冷器和中冷后进气管;所述发动机气缸的排气经所述排气歧管部分进入所述涡轮机,部分经EGR阀、EGR冷却器、进气歧管再次进入所述发动机气缸;所述发动机气缸的进气经增压器压气机、增压中冷器和中冷后进气管后回到所述发动机气缸,其特征在于:多个所述发动机气缸分组分别连接多根所述排气歧管;所述涡轮机具有多个涡轮蜗壳腔室通向涡轮叶轮;多根所述排气歧管分别进入对应的多个所述涡轮蜗壳腔室;至少部分所述排气歧管同时与所述EGR阀相连接。An internal combustion engine exhaust system with exhaust gas recirculation, including multiple engine cylinders, exhaust manifold, EGR valve, EGR cooler, intake manifold, turbine, supercharger compressor, charge intercooler and intercooler Intake pipe after cooling; the exhaust gas of the engine cylinder partly enters the turbine through the exhaust manifold, and partly enters the engine cylinder again through the EGR valve, EGR cooler and intake manifold; the intake air of the engine cylinder The gas returns to the engine cylinder after passing through the supercharger compressor, the supercharged intercooler and the intercooled intake pipe, and it is characterized in that: a plurality of the engine cylinders are grouped and respectively connected to a plurality of the exhaust manifolds; The turbine has a plurality of turbine volute chambers leading to the turbine wheel; a plurality of exhaust manifolds respectively enter the corresponding plurality of turbine volute chambers; at least part of the exhaust manifolds are simultaneously connected with the EGR valve connected.
其进一步特征在于:每根所述排气歧管至少连接两个发动机气缸排气。It is further characterized in that: each of the exhaust manifolds is at least connected to the exhaust gas of two engine cylinders.
优选的:所述发动机气缸为六个,两两组合与三根排气歧管相连,所述涡轮机包括第一涡轮蜗壳腔、第二涡轮蜗壳腔、第三涡轮蜗壳腔;三根所述排气歧管中的第一排气歧管同时连接所述EGR阀和所述第一涡轮蜗壳腔,第二排气歧管同时连接所述EGR阀和所述第二涡轮蜗壳腔,第三排气歧管单独与所述第三涡轮蜗壳腔相连接。Preferably: the number of cylinders of the engine is six, and the two-by-two combination is connected with three exhaust manifolds, and the turbine includes a first turbine volute cavity, a second turbine volute cavity, and a third turbine volute cavity; The first exhaust manifold in the exhaust manifold is simultaneously connected to the EGR valve and the first turbine volute cavity, and the second exhaust manifold is simultaneously connected to the EGR valve and the second turbine volute cavity, The third exhaust manifold is separately connected with the third turbine volute cavity.
所述第一涡轮蜗壳腔、第二涡轮蜗壳腔、第三涡轮蜗壳腔截面积呈梯度排列。The cross-sectional areas of the first turbine volute cavity, the second turbine volute cavity and the third turbine volute cavity are arranged in gradients.
优选的:所述第三涡轮蜗壳腔截面积大于第二涡轮蜗壳腔和第一涡轮蜗壳腔。Preferably: the cross-sectional area of the third turbine volute cavity is larger than that of the second turbine volute cavity and the first turbine volute cavity.
所述第二涡轮蜗壳腔和第三涡轮蜗壳腔截面非对称设置。The sections of the second turbine volute cavity and the third turbine volute cavity are arranged asymmetrically.
所述EGR阀为三通阀。The EGR valve is a three-way valve.
本发明的有益效果在于三流道增压器蜗壳和排气歧管布置更有利于减小各缸排气间干扰,利用排气脉冲效应,便于排气能量的保持。本发明的有益效果还在于三流道增压器蜗壳内设置有不同截面积蜗壳腔,可以形成不同梯度的蜗壳非对称度,便于发动机不同工况下EGR率优化。The beneficial effect of the invention is that the arrangement of the volute of the three-channel supercharger and the exhaust manifold is more conducive to reducing the interference between the exhaust of each cylinder, and the use of the exhaust pulse effect facilitates the maintenance of exhaust energy. The beneficial effect of the present invention is that the volute chambers of different cross-sectional areas are arranged in the volute of the three-channel supercharger, which can form the asymmetry of the volute with different gradients, and facilitate the optimization of the EGR rate under different working conditions of the engine.
附图说明Description of drawings
图 1 为本发明的发动机系统架构示意图。Figure 1 is a schematic diagram of the engine system architecture of the present invention.
图 2 为本发明涡轮机的一种涡轮蜗壳腔结构示意图。Fig. 2 is a schematic diagram of the structure of a turbine volute cavity of the turbine of the present invention.
图 3 为本发明第二种涡轮蜗壳腔结构示意图。Fig. 3 is a schematic diagram of the structure of the second turbine volute cavity of the present invention.
图 4 为本发明第三种涡轮蜗壳腔结构示意图。Fig. 4 is a schematic diagram of the structure of the third turbine volute cavity of the present invention.
图 5-9为EGR阀在不同工况下的状态示意图。Figure 5-9 is a schematic diagram of the state of the EGR valve under different working conditions.
具体实施方式Detailed ways
如图1所示一种采用非对称涡轮增压器的带废气再循环的内燃机排气系统,包括多个发动机气缸、排气歧管、EGR阀20、EGR冷却器19、EGR冷却后管路18、进气歧管17、涡轮机、增压器压气机28、增压中冷器29和中冷后进气管30;发动机气缸的排气经排气歧管部分进入涡轮机,部分经EGR阀20、EGR冷却器19、进气歧管17再次进入发动机气缸。发动机气缸的第一气缸11和第二气缸12排出的气体引入第一排气歧管21;第三气缸13和第四气缸14排出的气体引入第二排气歧管22;第五气缸15和第六气缸16排出的气体引入第三排气歧管23。第二排气歧管22和第三排气歧管23中流出的气体至少部分再循环至进气歧管17。将第一排气歧管21、第二排气歧管22和第三排气歧管23中的气体分别送入涡轮机的第一涡轮蜗壳腔24、第二涡轮蜗壳腔25和第三涡轮蜗壳腔26中,再推动涡轮叶轮27。As shown in Figure 1, an internal combustion engine exhaust system with exhaust gas recirculation using an asymmetric turbocharger includes a plurality of engine cylinders, an exhaust manifold, an EGR valve 20, an EGR cooler 19, and a pipeline after EGR cooling 18. Intake manifold 17, turbine, supercharger compressor 28, supercharged intercooler 29 and intercooled rear intake pipe 30; the exhaust gas from the engine cylinder enters the turbine partly through the exhaust manifold, partly through the EGR valve 20, The EGR cooler 19, intake manifold 17 again enters the engine cylinders. The gas discharged from the first cylinder 11 and the second cylinder 12 of the engine cylinder is introduced into the first exhaust manifold 21; the gas discharged from the third cylinder 13 and the fourth cylinder 14 is introduced into the second exhaust manifold 22; the fifth cylinder 15 and Gas exhausted from the sixth cylinder 16 is introduced into the third exhaust manifold 23 . Gases flowing out of the second exhaust manifold 22 and the third exhaust manifold 23 are at least partially recirculated to the intake manifold 17 . The gas in the first exhaust manifold 21, the second exhaust manifold 22 and the third exhaust manifold 23 are sent to the first turbine volute cavity 24, the second turbine volute cavity 25 and the third turbine volute cavity of the turbine respectively. In the turbine volute cavity 26, the turbine impeller 27 is pushed.
如图2所示,上述的非对称涡轮增压器,包括涡轮机,涡轮机包括蜗壳和涡轮叶片31部分。在涡轮机蜗壳内设置有三个蜗壳腔,第一涡轮蜗壳腔24、第二涡轮蜗壳腔25、第三涡轮蜗壳腔26。三个蜗壳腔分别连接三组不同排气歧管。其中第三涡轮蜗壳腔26具有相对于第二涡轮蜗壳腔25、第一涡轮蜗壳腔24具有较大的截面积。其中进入第一排气歧管21、第二排气歧管22的气体一部分通过EGR实现再循环,剩余部分分别进入涡轮机第一涡轮蜗壳腔24、第二涡轮蜗壳腔25。与现有技术相比,本发明相对于蜗壳腔26,设置了具有不同非对称度的蜗壳腔25和蜗壳腔24。设置的非对称流道更有利于形成不同梯度的EGR率,便于发动机不同工况下EGR率优化。As shown in FIG. 2 , the above-mentioned asymmetric turbocharger includes a turbine, and the turbine includes a volute and a turbine blade 31 . Three volute chambers are arranged in the turbine volute, a first turbine volute chamber 24 , a second turbine volute chamber 25 , and a third turbine volute chamber 26 . The three volute chambers are respectively connected with three different sets of exhaust manifolds. The third turbine volute cavity 26 has a larger cross-sectional area than the second turbine volute cavity 25 and the first turbine volute cavity 24 . Part of the gas entering the first exhaust manifold 21 and the second exhaust manifold 22 is recirculated through EGR, and the remaining part enters the first turbine volute cavity 24 and the second turbine volute cavity 25 of the turbine respectively. Compared with the prior art, the present invention sets the volute cavity 25 and the volute cavity 24 with different degrees of asymmetry relative to the volute cavity 26 . The set asymmetric flow channel is more conducive to the formation of EGR rates with different gradients, which facilitates the optimization of EGR rates under different engine operating conditions.
通过图2所示结构,可以产生如下效果。发动机三组排气歧管分别与第一涡轮蜗壳腔24、第二涡轮蜗壳腔25、第三涡轮蜗壳腔26相连。通过蜗壳腔进入涡轮膨胀做功。由于第一涡轮蜗壳腔24、第二涡轮蜗壳腔25、第三涡轮蜗壳腔26具有不同的喉口面积,使的三组蜗壳腔内气流收到不同程度的节流。气流在第三涡轮蜗壳腔26收到的节流较小,因此第三涡轮蜗壳腔26内气体能量保持较好,气体压力较低,能保证涡轮较高的工作效率。第一涡轮蜗壳腔24、第二涡轮蜗壳腔25、第三涡轮蜗壳腔26喉口面积依次增加。在节流作用的影响下,第一涡轮蜗壳腔24、第二涡轮蜗壳腔25、第三涡轮蜗壳腔26的压力依次减小。第一涡轮蜗壳腔24、第二涡轮蜗壳腔25相对于第三涡轮蜗壳腔26具有较高的压力,因此相对于增压后的进气,其能形成适当的压力梯度。这便于利用热端EGR阀,提供发动机所需的EGR率。进一步的,第一涡轮蜗壳腔24具有相对于第二涡轮蜗壳腔25更小的喉口面积,因此相对于增压后的进气,其能形成更大的压力梯度。便于在发动机低速工况,提供较小量的废气再循环。当发动机需要较大量的EGR时,可以通过EGR管路,将第一排气歧管21、第二排气歧管22中的部分排气,利用第一涡轮蜗壳腔24、第二涡轮蜗壳腔25形成的压差,同时引入EGR冷却器。Through the structure shown in Fig. 2, the following effects can be produced. The three sets of exhaust manifolds of the engine are respectively connected with the first turbine volute cavity 24 , the second turbine volute cavity 25 and the third turbine volute cavity 26 . It enters the turbine through the volute cavity and expands to do work. Since the first turbine volute cavity 24 , the second turbine volute cavity 25 and the third turbine volute cavity 26 have different throat areas, the airflows in the three groups of volute cavities are throttled to different degrees. The throttling of the air flow in the third turbine volute cavity 26 is relatively small, so the energy of the gas in the third turbine volute cavity 26 is well maintained, and the gas pressure is low, which can ensure a higher working efficiency of the turbine. The throat areas of the first turbine volute cavity 24 , the second turbine volute cavity 25 , and the third turbine volute cavity 26 increase sequentially. Under the influence of throttling, the pressures of the first turbine volute cavity 24 , the second turbine volute cavity 25 and the third turbine volute cavity 26 decrease sequentially. The first turbine volute cavity 24 and the second turbine volute cavity 25 have higher pressure than the third turbine volute cavity 26 , so they can form an appropriate pressure gradient relative to the pressurized intake air. This facilitates use of the hot end EGR valve to provide the EGR rate required by the engine. Further, the first turbine volute cavity 24 has a smaller throat area than the second turbine volute cavity 25 , so it can form a larger pressure gradient relative to the boosted intake air. It is convenient to provide a smaller amount of exhaust gas recirculation at low engine speeds. When the engine needs a large amount of EGR, the first exhaust manifold 21 and the second exhaust manifold 22 can be partially exhausted through the EGR pipeline, and the first turbine volute cavity 24 and the second turbine volute can be used to The pressure difference formed by the shell cavity 25 is introduced into the EGR cooler at the same time.
图 5-9为EGR阀在不同工况下的状态示意图。Figure 5-9 is a schematic diagram of the state of the EGR valve under different working conditions.
当发动机在低速大负荷运行时,发动机需要较低的EGR率,如图9所示,此时EGR阀板36将第二流道35关闭,第一流道34敞开,EGR经EGR冷却器19进入进气歧管17。当发动机在低速小负荷运行时,需要较高的EGR率, EGR阀板36将第二流道35、第一流道34部分打开或者全开,如图6、7所示。当发动机需要中等EGR率时,EGR阀板36将第二流道35部分打开,或者EGR阀板36将第一流道34关闭,如图5和图8所示。When the engine is running at low speed and high load, the engine needs a lower EGR rate, as shown in Figure 9, at this time, the EGR valve plate 36 closes the second flow passage 35, the first flow passage 34 is opened, and EGR enters through the EGR cooler 19 Intake manifold 17. When the engine is running at low speed and low load, a higher EGR rate is required, and the EGR valve plate 36 partially opens or fully opens the second flow passage 35 and the first flow passage 34, as shown in FIGS. 6 and 7 . When the engine requires a moderate EGR rate, the EGR valve plate 36 partially opens the second flow passage 35 , or the EGR valve plate 36 closes the first flow passage 34 , as shown in FIGS. 5 and 8 .
在本发明中也可以设置第二蜗壳腔25小于第一涡轮蜗壳腔24,如图3所示。或如图4所示,所述的非对称涡轮增压器,包括涡轮机,涡轮机包括蜗壳和涡轮叶片31部分。在涡轮机蜗壳内设置有三个蜗壳腔,第一涡轮蜗壳腔24、第二涡轮蜗壳腔25、第三涡轮蜗壳腔26。三个蜗壳腔分别连接三组不同排气歧管。其中涡轮机蜗壳第二蜗壳腔25具有相对于第一涡轮蜗壳腔24、第三涡轮蜗壳腔26较大的截面积。其中进入第一排气歧管21、第二排气歧管22的气体一部分通过EGR实现再循环,剩余部分分别进入涡轮机第一涡轮蜗壳腔24、第三涡轮蜗壳腔26。In the present invention, it is also possible to set the second volute cavity 25 to be smaller than the first turbine volute cavity 24, as shown in FIG. 3 . Or as shown in FIG. 4 , the asymmetric turbocharger includes a turbine, and the turbine includes a volute and a turbine blade 31 . Three volute chambers are arranged in the turbine volute, a first turbine volute chamber 24 , a second turbine volute chamber 25 , and a third turbine volute chamber 26 . The three volute chambers are respectively connected with three different sets of exhaust manifolds. The second volute cavity 25 of the turbine volute has a larger cross-sectional area than the first turbine volute cavity 24 and the third turbine volute cavity 26 . Part of the gas entering the first exhaust manifold 21 and the second exhaust manifold 22 is recirculated through EGR, and the remaining part enters the first turbine volute cavity 24 and the third turbine volute cavity 26 of the turbine respectively.
上面对本发明进行了描述,显然本发明具体实现并不受上述方式的限制,只要采用了本发明的方法构思和技术方案进行的各种非实质性的改进,或未经改进将本发明的构思和技术方案直接应用于其它场合的,均在本发明的保护范围内。The present invention has been described above, and it is obvious that the specific implementation of the present invention is not limited by the above-mentioned mode, as long as various insubstantial improvements are adopted in the method concept and technical scheme of the present invention, or the concept of the present invention is not improved. And technical solutions that are directly applied to other occasions are within the protection scope of the present invention.
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