CN103291433A - Triaxial synchronous type variable exhaust branch reducing rate system - Google Patents

Triaxial synchronous type variable exhaust branch reducing rate system Download PDF

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CN103291433A
CN103291433A CN2013101856185A CN201310185618A CN103291433A CN 103291433 A CN103291433 A CN 103291433A CN 2013101856185 A CN2013101856185 A CN 2013101856185A CN 201310185618 A CN201310185618 A CN 201310185618A CN 103291433 A CN103291433 A CN 103291433A
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branch pipe
exhaust branch
pipe
exhaust
rotating
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胡志龙
石磊
杨顺及
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Shanghai Jiao Tong University
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Abstract

一种机械设计技术领域的三轴同步式排气支管缩口率可变系统,包括容积腔、弹性部件、旋转体、隔板、旋转轴、旋转板和链条,容积腔的纵截面为圆环状,旋转体的纵截面为圆弧状,第三连接轴的一端穿过容积腔后镶嵌在容积腔的侧壁上,第一旋转轴的一端穿过第一排气支管后镶嵌在第一排气支管的侧壁上。当发动机进气管压力较高时,旋转体带动旋转板逆时针旋转,排气支管出口面积相对较大,发动机泵气损失较小;当发动机进气管压力较低时,旋转体带动旋转板顺时针旋转,排气支管出口面积相对较小,脉冲能量可以充分利用,涡轮前可用能较多。本发明设计合理,结构简单,适用于涡轮进口有一个且涡轮侧置的涡轮增压系统。

Figure 201310185618

A three-axis synchronous exhaust branch pipe necking rate variable system in the technical field of mechanical design, including a volume chamber, an elastic component, a rotating body, a partition, a rotating shaft, a rotating plate and a chain, and the longitudinal section of the volume chamber is a ring shape, the longitudinal section of the rotating body is arc-shaped, one end of the third connecting shaft passes through the volume chamber and is embedded on the side wall of the volume chamber, and one end of the first rotation shaft passes through the first exhaust branch pipe and is embedded in the first on the side wall of the exhaust manifold. When the engine intake pipe pressure is high, the rotating body drives the rotating plate to rotate counterclockwise, the outlet area of the exhaust branch pipe is relatively large, and the engine pumping loss is small; when the engine intake pipe pressure is low, the rotating body drives the rotating plate clockwise Rotating, the outlet area of the exhaust branch pipe is relatively small, the pulse energy can be fully utilized, and the available energy before the turbine is more. The invention is reasonable in design and simple in structure, and is suitable for a turbocharging system with one turbine inlet and the turbine side-mounted.

Figure 201310185618

Description

三轴同步式排气支管缩口率可变系统Three-axis Synchronous Exhaust Branch Pipe Shrinkage Variable System

技术领域technical field

本发明涉及的是一种机械设计技术领域的涡轮增压系统,特别是一种三轴同步式排气支管缩口率可变系统。The invention relates to a turbocharger system in the technical field of mechanical design, in particular to a three-axis synchronous exhaust branch pipe shrinkage variable system.

背景技术Background technique

随着社会的发展和环保要求的提高,发动机增压技术的应用越来越广泛,中大功率的发动机大都采用涡轮增压技术,以提高功率和降低燃油消耗率。涡轮增压系统的两种基本型式为定压增压系统和脉冲增压系统。定压增压系统,各缸共用一根容积较大的排气管,排气管系结构比较简单,排气管内压力基本上保持恒定,压力大小仅与发动机的负荷和转速有关,不同缸数柴油机的增压系统可以进行统一设计。定压增压系统在高速工况时,泵气损失较小,涡轮效率较高,性能较优;但是在低速工况时,不能充分利用排气脉冲能量。脉冲增压系统,依据各缸发火顺序,将排气不发生干扰的两个气缸或三个气缸和同一根排气管相连接,排气管系管径较小,排气脉冲能量可以充分利用,低速工况和瞬态工况性能较好;但是在高速工况时,泵气损失较大。由此可见,如果一台发动机的排气管容积可以随着工况的变换而变化,高速工况时使排气管容积变大,低速工况时使排气管容积变小,这是较为理想的。在排气管容积不变的前提下,通过改变排气支管的出口面积,也可以实现发动机高低转速工况的兼顾。在低速工况排气支管出口面积变小,涡轮前可用能较多;在高速工况排气支管出口面积变大,泵气损失较小,这也是较为理想的。With the development of society and the improvement of environmental protection requirements, the application of engine supercharging technology is becoming more and more extensive. Most of the engines with medium and high power adopt turbocharging technology to improve power and reduce fuel consumption. The two basic types of turbocharging systems are constant pressure supercharging system and pulse supercharging system. Constant pressure supercharging system, each cylinder shares an exhaust pipe with a large volume, the structure of the exhaust pipe system is relatively simple, the pressure in the exhaust pipe is basically kept constant, the pressure is only related to the load and speed of the engine, different cylinder numbers The supercharging system of the diesel engine can be designed uniformly. The constant pressure supercharging system has less pumping loss, higher turbine efficiency and better performance under high-speed conditions; however, it cannot fully utilize the exhaust pulse energy under low-speed conditions. Pulse supercharging system, according to the firing sequence of each cylinder, connects two cylinders or three cylinders that do not interfere with the exhaust with the same exhaust pipe. The diameter of the exhaust pipe system is small, and the exhaust pulse energy can be fully utilized , the low-speed working condition and the transient working condition have better performance; but in the high-speed working condition, the pumping loss is larger. It can be seen that if the volume of the exhaust pipe of an engine can change with the change of working conditions, the volume of the exhaust pipe will be enlarged under high-speed conditions, and the volume of the exhaust pipe will be reduced under low-speed conditions. ideal. On the premise that the volume of the exhaust pipe remains unchanged, by changing the outlet area of the exhaust branch pipe, it is also possible to achieve both high and low engine speed conditions. In the low-speed working condition, the outlet area of the exhaust branch pipe becomes smaller, and the available energy before the turbine is more; in the high-speed working condition, the outlet area of the exhaust branch pipe becomes larger, and the pumping loss is smaller, which is also ideal.

经过对现有技术文献的检索发现,中国专利号ZL201020532937.0,专利名称:排气管出口面积可变的涡轮增压装置,该专利技术提供了一种排气管出口面积连续可变的装置,能较好地兼顾发动机的高低转速工况;但是其排气管出口面积的变化是通过旋转把手的旋转来实现的,这就需要增加一套专门的控制机构来控制旋转把手的旋转,从而使增压系统结构变的比较复杂。After searching the existing technical literature, it is found that Chinese patent number ZL201020532937.0, patent name: turbocharger device with variable exhaust pipe outlet area, this patent technology provides a device with continuously variable exhaust pipe outlet area , can better take into account the high and low speed conditions of the engine; but the change of the outlet area of the exhaust pipe is realized by the rotation of the rotary handle, which requires adding a special control mechanism to control the rotation of the rotary handle, so that Make the booster system structure more complicated.

发明内容Contents of the invention

本发明针对上述现有技术的不足,提供了一种三轴同步式排气支管缩口率可变系统,使其排气支管出口面积可以自我调节,较好地兼顾发动机的高低转速工况,而且结构简单,不需要专门的控制机构。The present invention aims at the deficiencies of the above-mentioned prior art, and provides a three-axis synchronous exhaust branch pipe shrinking rate variable system, so that the outlet area of the exhaust branch pipe can be adjusted by itself, and the high and low speed conditions of the engine can be better taken into account. Moreover, the structure is simple and does not require a special control mechanism.

本发明是通过以下技术方案来实现的,本发明包括压气机进气管、压气机、发动机进气管、发动机、第一排气支管、第二排气支管、排气管、涡轮、涡轮排气管、连接轴、连接管、容积腔、弹性部件、旋转体、隔板、第三旋转轴、第一旋转轴、第一旋转板、第二旋转轴、第二旋转板和链条,压气机的进出气口分别与压气机进气管的出气口、发动机进气管的进气口相连接,发动机的进气口与发动机进气管的排气口相连接,第一排气支管的进气口、第二排气支管的进气口分别与发动机的排气道相连接,第一排气支管的出气口、第二排气支管的出气口均与排气管相连接,涡轮的进出气口分别与排气管的出气口、涡轮排气管的进气口相连接,压气机与涡轮通过连接轴同轴相连,容积腔的纵截面为圆环状,旋转体的纵截面为圆弧状,容积腔与旋转体的横截面均为长方形,第三连接轴的轴线与容积腔的轴线重合,第三连接轴的一端穿过容积腔后镶嵌在容积腔的侧壁上,隔板安装在容积腔内并与容积腔的内壁面固结为一体,隔板的上端面与第三连接轴密封接触,旋转体安装在容积腔内且与容积腔的内壁面密封接触,旋转体与容积腔内的第三连接轴固结为一体,隔板的左端面通过弹性部件与旋转体相连接,连接管的一端与隔板右侧的容积腔相连通,连接管的另一端与发动机进气管相连通,第一排气支管的横截面为长方形,第一旋转轴的一端穿过第一排气支管后镶嵌在第一排气支管的侧壁上,第一旋转板安装在第一排气支管内并与第一排气支管内的第一旋转轴固结为一体,第二排气支管的横截面为长方形,第二旋转轴的一端穿过第二排气支管后镶嵌在第二排气支管的侧壁上,第二旋转板安装在第二排气支管内并与第二排气支管内的第二旋转轴固结为一体,第三旋转轴的另一端、第一旋转轴的另一端、第二旋转轴的另一端通过链条相连接。The present invention is achieved through the following technical proposals, the present invention comprises a compressor intake pipe, a compressor, an engine intake pipe, an engine, a first exhaust branch pipe, a second exhaust branch pipe, an exhaust pipe, a turbine, and a turbine exhaust pipe , connecting shaft, connecting pipe, volume cavity, elastic component, rotating body, partition, third rotating shaft, first rotating shaft, first rotating plate, second rotating shaft, second rotating plate and chain, compressor access The gas ports are respectively connected with the air outlet of the compressor intake pipe and the air intake of the engine intake pipe, the engine air intake is connected with the exhaust port of the engine intake pipe, the air intake of the first exhaust branch pipe, the second row The air inlet of the air branch pipe is connected with the exhaust duct of the engine respectively, the air outlet of the first exhaust branch pipe and the air outlet of the second exhaust branch pipe are connected with the exhaust pipe, and the air inlet and outlet of the turbine are connected with the exhaust pipe respectively. The air outlet of the exhaust pipe of the turbine is connected to the air inlet of the turbine exhaust pipe. The compressor and the turbine are connected coaxially through the connecting shaft. The cross-section of the body is rectangular, the axis of the third connecting shaft coincides with the axis of the volume cavity, one end of the third connection shaft passes through the volume cavity and is embedded on the side wall of the volume cavity, and the partition plate is installed in the volume cavity and connected with the volume cavity. The inner wall surface of the volume chamber is consolidated into one body, the upper end surface of the partition is in sealing contact with the third connecting shaft, the rotating body is installed in the volume chamber and is in sealing contact with the inner wall surface of the volume chamber, and the rotating body is connected to the third connection shaft in the volume chamber The shaft is consolidated into one body, the left end surface of the partition is connected with the rotating body through elastic parts, one end of the connecting pipe is connected with the volume cavity on the right side of the partition, the other end of the connecting pipe is connected with the engine intake pipe, the first row The cross-section of the air branch pipe is rectangular, and one end of the first rotating shaft passes through the first exhaust branch pipe and is inlaid on the side wall of the first exhaust branch pipe. The first rotating plate is installed in the first exhaust branch pipe and The first rotation shaft in the exhaust branch pipe is consolidated into one body, the cross section of the second exhaust branch pipe is rectangular, and one end of the second rotation shaft passes through the second exhaust branch pipe and is inlaid on the side wall of the second exhaust branch pipe , the second rotating plate is installed in the second exhaust branch pipe and consolidated with the second rotating shaft in the second exhaust branch pipe, the other end of the third rotating shaft, the other end of the first rotating shaft, the second rotating The other end of the shaft is connected by a chain.

进一步地,在本发明中,弹性部件为弹簧,第一旋转板、第二旋转板均为平板。Further, in the present invention, the elastic component is a spring, and both the first rotating plate and the second rotating plate are flat plates.

在本发明的工作过程中,旋转体可以在容积腔内旋转,旋转体与第三旋转轴固结为一体,第一旋转轴与第一旋转板固结在一起,第二旋转轴与第二旋转板固结在一起;当旋转体旋转时,链条带动第一旋转板、第二旋转板同步同方向旋转。当发动机进气管内压力较高时,隔板右侧的容积腔内压力也较高,旋转体带动第一旋转板、第二旋转板逆时针旋转并压缩弹性部件,从而使第一排气管、第二排气支管的缩口率变大,发动机的泵气损失较小;当发动机进气管内压力较低时,隔板右侧的容积腔内压力也较低,在弹性部件的弹性作用下,旋转体带动第一旋转板、第二旋转板顺时针旋转,从而使第一排气管、第二排气支管的缩口率变小,脉冲能量可以充分利用,涡轮前可用能较多。In the working process of the present invention, the rotating body can rotate in the volume chamber, the rotating body is consolidated with the third rotating shaft, the first rotating shaft is consolidated with the first rotating plate, the second rotating shaft is connected with the second The rotating plates are fixed together; when the rotating body rotates, the chain drives the first rotating plate and the second rotating plate to rotate synchronously and in the same direction. When the pressure in the intake pipe of the engine is high, the pressure in the volume cavity on the right side of the partition is also high, and the rotating body drives the first rotating plate and the second rotating plate to rotate counterclockwise and compress the elastic parts, so that the first exhaust pipe , The shrinkage rate of the second exhaust branch pipe becomes larger, and the pumping loss of the engine is smaller; when the pressure in the engine intake pipe is low, the pressure in the volume cavity on the right side of the partition is also low, and the elastic effect of the elastic component Next, the rotating body drives the first rotating plate and the second rotating plate to rotate clockwise, so that the shrinkage ratio of the first exhaust pipe and the second exhaust branch pipe becomes smaller, the pulse energy can be fully utilized, and the available energy before the turbine is more .

与现有技术相比,本发明具有如下有益效果为:本发明设计合理,结构简单,适用于涡轮进口有一个且涡轮侧置的涡轮增压系统,既能兼顾发动机的高低转速工况,又能使增压系统不需要专门的排气支管出口面积控制机构。Compared with the prior art, the present invention has the following beneficial effects: the present invention is reasonable in design and simple in structure, and is suitable for a turbocharging system with one turbine inlet and the turbine is placed on the side, which can take into account the high and low speed conditions of the engine, and It can make the supercharging system not need a special control mechanism for the outlet area of the exhaust branch pipe.

附图说明Description of drawings

图1为本发明的结构示意图;Fig. 1 is a structural representation of the present invention;

图2为图1中A-A剖面的结构示意图;Fig. 2 is the structural representation of A-A section among Fig. 1;

图3为图1中B-B剖面的结构示意图;Fig. 3 is the structural representation of B-B section among Fig. 1;

图4为图1中C-C剖面的结构示意图;Fig. 4 is the structural representation of C-C section among Fig. 1;

图5为图1中D-D剖面的结构示意图;Fig. 5 is the structural representation of D-D section among Fig. 1;

图6为本发明中链条连接的结构示意图;Fig. 6 is the structural representation of chain connection among the present invention;

其中:1、压气机进气管,2、压气机,3、发动机进气管,4、发动机,5、第一排气支管,6、第二排气支管,7、排气管,8、涡轮,9、涡轮排气管,10、连接轴,11、连接管,12、容积腔,13、弹性部件,14、旋转体,15隔板,16、第三旋转轴,17、第一旋转轴,18、第一旋转板,19、第二旋转轴,20、第二旋转板,21、链条。Among them: 1. Compressor intake pipe, 2. Compressor, 3. Engine intake pipe, 4. Engine, 5. First exhaust branch pipe, 6. Second exhaust branch pipe, 7. Exhaust pipe, 8. Turbine, 9. Turbine exhaust pipe, 10. Connecting shaft, 11. Connecting pipe, 12. Volume cavity, 13. Elastic component, 14. Rotating body, 15 Partition plate, 16. Third rotating shaft, 17. First rotating shaft, 18, the first rotating plate, 19, the second rotating shaft, 20, the second rotating plate, 21, the chain.

具体实施方式Detailed ways

下面结合附图对本发明的实施例作详细说明,本实施例以本发明技术方案为前提,给出了详细的实施方式和具体的操作过程,但本发明的保护范围不限于下述的实施例。The embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. This embodiment is based on the technical solution of the present invention, and provides detailed implementation methods and specific operating procedures, but the scope of protection of the present invention is not limited to the following embodiments. .

实施例Example

如图1至图6所示,本发明包括:包括压气机进气管1、压气机2、发动机进气管3、发动机4、第一排气支管5、第二排气支管6、排气管7、涡轮8、涡轮排气管9、连接轴10、连接管11、容积腔12、弹性部件13、旋转体14、隔板15、第三旋转轴16、第一旋转轴17、第一旋转板18、第二旋转轴19、第二旋转板20和链条21,压气机2的进出气口分别与压气机进气管1的出气口、发动机进气管3的进气口相连接,发动机4的进气口与发动机进气管3的排气口相连接,第一排气支管5的进气口、第二排气支管6的进气口分别与发动机4的排气道相连接,第一排气支管5的出气口、第二排气支管6的出气口均与排气管7相连接,涡轮8的进出气口分别与排气管7的出气口、涡轮排气管9的进气口相连接,压气机2与涡轮8通过连接轴10同轴相连,容积腔12的纵截面为圆环状,旋转体14的纵截面为圆弧状,容积腔12与旋转体14的横截面均为长方形,第三连接轴16的轴线与容积腔12的轴线重合,第三连接轴16的一端穿过容积腔12后镶嵌在容积腔12的侧壁上,隔板15安装在容积腔12内并与容积腔12的内壁面固结为一体,隔板15的上端面与第三连接轴16密封接触,旋转体14安装在容积腔12内且与容积腔12的内壁面密封接触,旋转体14与容积腔12内的第三连接轴16固结为一体,隔板15的左端面通过弹性部件13与旋转体14相连接,连接管11的一端与隔板15右侧的容积腔12相连通,连接管11的另一端与发动机进气管3相连通,第一排气支管5的横截面为长方形,第一旋转轴17的一端穿过第一排气支管5后镶嵌在第一排气支管5的侧壁上,第一旋转板18安装在第一排气支管5内并与第一排气支管5内的第一旋转轴17固结为一体,第二排气支管6的横截面为长方形,第二旋转轴19的一端穿过第二排气支管6后镶嵌在第二排气支管6的侧壁上,第二旋转板20安装在第二排气支管6内并与第二排气支管6内的第二旋转轴19固结为一体,第三旋转轴16的另一端、第一旋转轴17的另一端、第二旋转轴19的另一端通过链条21相连接,弹性部件13为弹簧,第一旋转板18、第二旋转板20均为平板。As shown in Figures 1 to 6, the present invention includes: a compressor intake pipe 1, a compressor 2, an engine intake pipe 3, an engine 4, a first exhaust branch pipe 5, a second exhaust branch pipe 6, and an exhaust pipe 7 , turbine 8, turbine exhaust pipe 9, connecting shaft 10, connecting pipe 11, volume cavity 12, elastic member 13, rotating body 14, partition 15, third rotating shaft 16, first rotating shaft 17, first rotating plate 18, the second rotating shaft 19, the second rotating plate 20 and the chain 21, the air inlet and outlet of the compressor 2 are respectively connected with the air outlet of the compressor air inlet pipe 1 and the air inlet of the engine air inlet pipe 3, and the air inlet of the engine 4 The port is connected with the exhaust port of the engine intake pipe 3, the air inlet of the first exhaust branch pipe 5, and the air inlet of the second exhaust branch pipe 6 are respectively connected with the exhaust passage of the engine 4, and the first exhaust branch pipe The gas outlet of 5 and the gas outlet of the second exhaust branch pipe 6 are all connected with exhaust pipe 7, and the air inlet and outlet of turbine 8 are connected with the gas outlet of exhaust pipe 7 and the air inlet of turbine exhaust pipe 9 respectively, The compressor 2 and the turbine 8 are connected coaxially through the connecting shaft 10, the longitudinal section of the volume chamber 12 is circular, the longitudinal section of the rotating body 14 is arc-shaped, and the cross sections of the volume chamber 12 and the rotating body 14 are rectangular. The axis of the third connection shaft 16 coincides with the axis of the volume chamber 12, and one end of the third connection shaft 16 passes through the volume chamber 12 and is embedded on the side wall of the volume chamber 12. The inner wall surface of the cavity 12 is consolidated into one body, the upper end surface of the partition plate 15 is in sealing contact with the third connecting shaft 16, the rotating body 14 is installed in the volume cavity 12 and is in sealing contact with the inner wall surface of the volume cavity 12, the rotating body 14 is in sealing contact with the volume cavity The third connecting shaft 16 in the chamber 12 is consolidated into one body, the left end surface of the partition 15 is connected with the rotating body 14 through the elastic member 13, and one end of the connecting pipe 11 communicates with the volume chamber 12 on the right side of the partition 15, and connects The other end of pipe 11 is connected with engine intake pipe 3, and the cross section of first exhaust branch pipe 5 is rectangular, and one end of first rotating shaft 17 passes through first exhaust branch pipe 5 and is embedded in the first exhaust branch pipe 5. On the side wall, the first rotating plate 18 is installed in the first exhaust branch pipe 5 and consolidated with the first rotating shaft 17 in the first exhaust branch pipe 5. The cross section of the second exhaust branch pipe 6 is rectangular. One end of the second rotating shaft 19 passes through the second exhaust branch pipe 6 and is embedded on the side wall of the second exhaust branch pipe 6. The second rotating plate 20 is installed in the second exhaust branch pipe 6 and connected with the second exhaust branch pipe. The second rotating shaft 19 in 6 is consolidated into one body, the other end of the third rotating shaft 16, the other end of the first rotating shaft 17, and the other end of the second rotating shaft 19 are connected by a chain 21, and the elastic member 13 is a spring , the first rotating plate 18 and the second rotating plate 20 are both flat plates.

在本发明的工作过程中,旋转体14可以在容积腔12内旋转,旋转体14与第三旋转轴16固结为一体,第一旋转轴17与第一旋转板18固结在一起,第二旋转轴19与第二旋转板20固结在一起;当旋转体14旋转时,链条21带动第一旋转板18、第二旋转板20同步同方向旋转。当发动机进气管3内压力较高时,隔板15右侧的容积腔12内压力也较高,旋转体14带动第一旋转板18、第二旋转板20逆时针旋转并压缩弹性部件13,从而使第一排气管5、第二排气支管6的缩口率变大,发动机4的泵气损失较小;当发动机进气管3内压力较低时,隔板15右侧的容积腔12内压力也较低,在弹性部件13的弹性作用下,旋转体14带动第一旋转板18、第二旋转板20顺时针旋转,从而使第一排气管5、第二排气支管6的缩口率变小,脉冲能量可以充分利用,涡轮8前可用能较多。During the working process of the present invention, the rotating body 14 can rotate in the volume cavity 12, the rotating body 14 is consolidated with the third rotating shaft 16, the first rotating shaft 17 is consolidated with the first rotating plate 18, and the second The two rotating shafts 19 and the second rotating plate 20 are fixed together; when the rotating body 14 rotates, the chain 21 drives the first rotating plate 18 and the second rotating plate 20 to rotate synchronously and in the same direction. When the pressure in the engine intake pipe 3 is high, the pressure in the volume cavity 12 on the right side of the partition 15 is also high, and the rotating body 14 drives the first rotating plate 18 and the second rotating plate 20 to rotate counterclockwise and compress the elastic member 13, Thereby the shrinkage rate of the first exhaust pipe 5 and the second exhaust branch pipe 6 becomes large, and the pumping loss of the engine 4 is small; The internal pressure of 12 is also low. Under the elastic action of the elastic member 13, the rotating body 14 drives the first rotating plate 18 and the second rotating plate 20 to rotate clockwise, so that the first exhaust pipe 5 and the second exhaust branch pipe 6 The shrinkage rate becomes smaller, the pulse energy can be fully utilized, and the available energy before the turbine 8 is more.

Claims (2)

1.一种三轴同步式排气支管缩口率可变系统,包括压气机进气管(1)、压气机(2)、发动机进气管(3)、发动机(4)、第一排气支管(5)、第二排气支管(6)、排气管(7)、涡轮(8)、涡轮排气管(9)和连接轴(10),压气机(2)的进出气口分别与压气机进气管(1)的出气口、发动机进气管(3)的进气口相连接,发动机(4)的进气口与发动机进气管(3)的排气口相连接,第一排气支管(5)的进气口、第二排气支管(6)的进气口分别与发动机(4)的排气道相连接,第一排气支管(5)的出气口、第二排气支管(6)的出气口均与排气管(7)相连接,涡轮(8)的进出气口分别与排气管(7)的出气口、涡轮排气管(9)的进气口相连接,压气机(2)与涡轮(8)通过连接轴(10)同轴相连,其特征在于,还包括连接管(11)、容积腔(12)、弹性部件(13)、旋转体(14)、隔板(15)、第三旋转轴(16)、第一旋转轴(17)、第一旋转板(18)、第二旋转轴(19)、第二旋转板(20)和链条(21),容积腔(12)的纵截面为圆环状,旋转体(14)的纵截面为圆弧状,容积腔(12)与旋转体(14)的横截面均为长方形,第三连接轴(16)的轴线与容积腔(12)的轴线重合,第三连接轴(16)的一端穿过容积腔(12)后镶嵌在容积腔(12)的侧壁上,隔板(15)安装在容积腔(12)内并与容积腔(12)的内壁面固结为一体,隔板(15)的上端面与第三连接轴(16)密封接触,旋转体(14)安装在容积腔(12)内且与容积腔(12)的内壁面密封接触,旋转体(14)与容积腔(12)内的第三连接轴(16)固结为一体,隔板(15)的左端面通过弹性部件(13)与旋转体(14)相连接,连接管(11)的一端与隔板(15)右侧的容积腔(12)相连通,连接管(11)的另一端与发动机进气管(3)相连通,第一排气支管(5)的横截面为长方形,第一旋转轴(17)的一端穿过第一排气支管(5)后镶嵌在第一排气支管(5)的侧壁上,第一旋转板(18)安装在第一排气支管(5)内并与第一排气支管(5)内的第一旋转轴(17)固结为一体,第二排气支管(6)的横截面为长方形,第二旋转轴(19)的一端穿过第二排气支管(6)后镶嵌在第二排气支管(6)的侧壁上,第二旋转板(20)安装在第二排气支管(6)内并与第二排气支管(6)内的第二旋转轴(19)固结为一体,第三旋转轴(16)的另一端、第一旋转轴(17)的另一端、第二旋转轴(19)的另一端通过链条(21)相连接。1. A three-axis synchronous exhaust branch pipe shrinkage ratio variable system, including compressor intake pipe (1), compressor (2), engine intake pipe (3), engine (4), and first exhaust branch pipe (5), the second exhaust branch pipe (6), exhaust pipe (7), turbine (8), turbine exhaust pipe (9) and connecting shaft (10), the inlet and outlet of the compressor (2) are respectively connected with the compressor The air outlet of the engine intake pipe (1) is connected with the air intake of the engine intake pipe (3), the air intake of the engine (4) is connected with the exhaust port of the engine intake pipe (3), and the first exhaust branch pipe The air inlet of (5) and the air inlet of the second exhaust branch pipe (6) are respectively connected with the exhaust passage of the engine (4), and the air outlet of the first exhaust branch pipe (5) and the second exhaust branch pipe The air outlets of (6) are all connected with the exhaust pipe (7), and the air inlet and outlet of the turbine (8) are respectively connected with the air outlet of the exhaust pipe (7) and the air inlet of the turbine exhaust pipe (9), The compressor (2) and the turbine (8) are coaxially connected through the connecting shaft (10), and it is characterized in that it also includes a connecting pipe (11), a volume chamber (12), an elastic component (13), a rotating body (14), Partition plate (15), third rotating shaft (16), first rotating shaft (17), first rotating plate (18), second rotating shaft (19), second rotating plate (20) and chain (21) , the longitudinal section of the volume chamber (12) is circular, the longitudinal section of the rotating body (14) is arc-shaped, the cross sections of the volume chamber (12) and the rotating body (14) are both rectangular, and the third connecting shaft ( The axis of 16) coincides with the axis of the volume chamber (12), and one end of the third connecting shaft (16) passes through the volume chamber (12) and is inlaid on the side wall of the volume chamber (12), and the partition (15) is installed on The volume chamber (12) is integrated with the inner wall surface of the volume chamber (12), the upper end surface of the partition (15) is in sealing contact with the third connecting shaft (16), and the rotating body (14) is installed in the volume chamber ( 12) and is in sealing contact with the inner wall of the volume cavity (12), the rotating body (14) is consolidated with the third connecting shaft (16) in the volume cavity (12), and the left end surface of the partition (15) passes through The elastic part (13) is connected with the rotating body (14), one end of the connecting pipe (11) is connected with the volume chamber (12) on the right side of the partition (15), and the other end of the connecting pipe (11) is connected with the engine intake pipe (3) are connected, the cross section of the first exhaust branch pipe (5) is rectangular, and one end of the first rotating shaft (17) passes through the first exhaust branch pipe (5) and is embedded in the first exhaust branch pipe (5) On the side wall, the first rotating plate (18) is installed in the first exhaust branch pipe (5) and consolidated with the first rotating shaft (17) in the first exhaust branch pipe (5), the second row The cross section of the air branch pipe (6) is rectangular, and one end of the second rotating shaft (19) passes through the second exhaust branch pipe (6) and is inlaid on the side wall of the second exhaust branch pipe (6). The second rotating plate (20) Installed in the second exhaust branch pipe (6) and consolidated with the second rotation shaft (19) in the second exhaust branch pipe (6), the third rotation shaft (16) The other end, the other end of the first rotating shaft (17) and the other end of the second rotating shaft (19) are connected by a chain (21). 2.根据权利要求1所述的三轴同步式排气支管缩口率可变系统,其特征是,弹性部件(13)为弹簧,第一旋转板(18)、第二旋转板(20)均为平板。2. The three-axis synchronous exhaust branch pipe shrinkage variable system according to claim 1, characterized in that the elastic member (13) is a spring, the first rotating plate (18), the second rotating plate (20) All are flat.
CN2013101856185A 2013-05-17 2013-05-17 Triaxial synchronous type variable exhaust branch reducing rate system Pending CN103291433A (en)

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CN103573477A (en) * 2013-09-24 2014-02-12 上海交通大学 Flow control system with area-adjustable throat part
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CN103089411A (en) * 2013-01-15 2013-05-08 上海交通大学 Variable air exhaust through flow area air exhaust pressure control type adjusting mechanism for turbocharged engine

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* Cited by examiner, † Cited by third party
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EP1510739A1 (en) * 2003-08-28 2005-03-02 Gustav Wahler GmbH u. Co.KG Exhaust valve
US20090183497A1 (en) * 2008-01-17 2009-07-23 Denso Corporation Exhaust gas purifying apparatus
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Cited By (5)

* Cited by examiner, † Cited by third party
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CN103541823A (en) * 2013-09-24 2014-01-29 上海交通大学 Annular shaft-valve simultaneous rotation system
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Application publication date: 20130911