CN102767425B - Switching device for admission passage and exhaust passage - Google Patents

Switching device for admission passage and exhaust passage Download PDF

Info

Publication number
CN102767425B
CN102767425B CN201210245944.6A CN201210245944A CN102767425B CN 102767425 B CN102767425 B CN 102767425B CN 201210245944 A CN201210245944 A CN 201210245944A CN 102767425 B CN102767425 B CN 102767425B
Authority
CN
China
Prior art keywords
pipe
engine
turbine
compressor
connecting pipe
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201210245944.6A
Other languages
Chinese (zh)
Other versions
CN102767425A (en
Inventor
梅琼风
于沪平
申昱
贾敬华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Jiao Tong University
Original Assignee
Shanghai Jiao Tong University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Jiao Tong University filed Critical Shanghai Jiao Tong University
Priority to CN201210245944.6A priority Critical patent/CN102767425B/en
Publication of CN102767425A publication Critical patent/CN102767425A/en
Application granted granted Critical
Publication of CN102767425B publication Critical patent/CN102767425B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Supercharger (AREA)

Abstract

一种内燃机技术领域的进排气气路切换装置,包括:压气机、进气管、发动机、排气管、涡轮、容积腔、连接管、移动体、弹簧和贯穿管,移动体安装在容积腔内并与容积腔的内壁面密封接触,贯穿管贯穿移动体的左右两壁面,移动体的上壁面通过弹簧与容积腔上壁面相连接。当发动机处于低速工况时,移动体向上移动,仅有第一压气机与第一涡轮工作,脉冲能量充分利用,发动机进气压力较高,发动机整机性能较优;当发动机处于高速工况时,移动体向下移动,第一压气机、第二压气机、第一涡轮、第二涡轮同时工作,发动机泵气损失较小,发动机整机性能较优。本发明设计合理,结构简单,适用于带有两个涡轮增压器的涡轮增压系统。

An intake and exhaust gas path switching device in the technical field of internal combustion engines, comprising: a compressor, an intake pipe, an engine, an exhaust pipe, a turbine, a volume chamber, a connecting pipe, a moving body, a spring and a through pipe, and the moving body is installed in the volume chamber The penetrating tube runs through the left and right walls of the moving body, and the upper wall of the moving body is connected to the upper wall of the volume chamber through a spring. When the engine is in a low-speed working condition, the mobile body moves upwards, only the first compressor and the first turbine work, the pulse energy is fully utilized, the intake pressure of the engine is high, and the overall performance of the engine is better; when the engine is in a high-speed working condition , the moving body moves downward, the first compressor, the second compressor, the first turbine, and the second turbine work simultaneously, the engine pumping loss is small, and the overall performance of the engine is better. The invention has reasonable design and simple structure, and is suitable for a turbocharging system with two turbochargers.

Description

进排气气路切换装置Inlet and exhaust gas path switching device

技术领域 technical field

本发明涉及的是一种内燃机领域的涡轮增压系统,特别是一种进排气气路切换装置。The invention relates to a turbocharging system in the field of internal combustion engines, in particular to an intake and exhaust gas path switching device.

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,涡轮当量流通面积较大,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,涡轮当量流通面积也较小,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,如果一台发动机的涡轮当量流通面积可以随着工况的变换而变化,高速工况时使涡轮当量流通面积变大,低速工况时使涡轮当量流通面积变小,这是较为理想的。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 a large-volume exhaust pipe, the structure of the exhaust pipe system is relatively simple, the equivalent flow area of the turbine is relatively large, the pressure in the exhaust pipe is basically kept constant, and the pressure is only related to the load of the engine It is related to the rotational speed, and the supercharging systems of diesel engines with different cylinder numbers 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 gas with the same exhaust pipe, the diameter of the exhaust pipe system is small, and the equivalent flow area of the turbine is also small , the exhaust pulse energy can be fully utilized, and the performance is better in low-speed and transient conditions; but in high-speed conditions, the pumping loss is relatively large. It can be seen that if the turbine equivalent flow area of an engine can change with the change of working conditions, the equivalent flow area of the turbine will be increased under high-speed conditions, and the equivalent flow area of the turbine will be reduced under low-speed conditions. ideal.

经过对现有技术文献的检索发现,中国专利号ZL200820226936.6,专利名称:一种涡轮增压器的压气机并联增压装置,该专利技术提供了一种压气机壳体可变的装置,能较好地兼顾发动机的高低转速工况;但是其壳体的变化需要一套专门的控制机构,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 ZL200820226936.6, patent name: a compressor parallel supercharging device for a turbocharger, this patent technology provides a device with a variable compressor shell, It can better take into account the high and low speed conditions of the engine; but the change of its housing requires a set of special control mechanisms, which makes the structure of the booster system more complicated.

发明内容 Contents of the invention

本发明针对上述现有技术的不足,提供了一种进排气气路切换装置,使增压系统可以自我调节,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 an intake and exhaust gas path switching device, which enables the supercharging system to self-regulate, and better takes into account the high and low speed conditions of the engine, and has a simple structure and does not require special control mechanism.

本发明是通过以下技术方案来实现的,本发明包括:第一吸气管、第一压气机、发动机进气管、发动机、发动机排气管、第一涡轮、第一出气管、第一连接轴、容积腔、容积腔上壁面、容积腔下壁面、容积腔左壁面、容积腔右壁面、容积腔前壁面、容积腔后壁面、弹簧、第一连接管、第二连接管、第三连接管、第四连接管、贯穿管、移动体、第二压气机、第二涡轮、第二吸气管、第二出气管和第二连接轴,第一压气机的进出气口分别与第一吸气管的出气口、发动机进气管的进气口相连接,发动机的进出气口分别与发动机进气管的出气口、发动机排气管的进气口相连接,第一涡轮的进出气口分别与发动机排气管的出气口、第一出气管的进气口相连接,第一压气机与第一涡轮通过第一连接轴相连接,容积腔的横截面为长方形,容积腔上壁面、容积腔下壁面、容积腔左壁面、容积腔右壁面、容积腔前壁面、容积腔后壁面固接为一体,第一连接管的两端分别与发动机进气管、容积腔上壁面相连通,第二连接管的两端分别与发动机排气管、容积腔左壁面相连通,第三连接管的两端分别与第二压气机的出气口、容积腔右壁面相连通,第四连接管的两端分别与第二涡轮的进气口、容积腔右壁面相连通,第二吸气管的出气口与第二压气机的进气口相连接,第二出气管的进气口与第二涡轮的出气口相连接,第二压气机与第二涡轮通过第二连接轴相连接,移动体安装在容积腔内并与容积腔的内壁面密封接触,贯穿管贯穿移动体的左右两壁面,移动体的上壁面通过弹簧与容积腔上壁面相连接。The present invention is achieved through the following technical solutions, the present invention includes: a first air intake pipe, a first compressor, an engine intake pipe, an engine, an engine exhaust pipe, a first turbine, a first air outlet pipe, and a first connecting shaft , volume cavity, volume cavity upper wall, volume cavity lower wall, volume cavity left wall, volume cavity right wall, volume cavity front wall, volume cavity rear wall, spring, first connecting pipe, second connecting pipe, third connecting pipe , the fourth connecting pipe, the penetrating pipe, the moving body, the second compressor, the second turbine, the second suction pipe, the second outlet pipe and the second connecting shaft, the inlet and outlet of the first compressor are respectively connected with the first suction The air outlet of the engine intake pipe is connected with the air inlet of the engine intake pipe, the air inlet and outlet of the engine are respectively connected with the air outlet of the engine intake pipe and the air inlet of the engine exhaust pipe, and the air inlet and outlet of the first turbine are connected with the engine exhaust pipe respectively. The air outlet of the pipe is connected with the air inlet of the first air outlet pipe, the first compressor is connected with the first turbine through the first connecting shaft, the cross section of the volume chamber is rectangular, the upper wall of the volume chamber, the lower wall of the volume chamber, The left wall of the volume cavity, the right wall of the volume cavity, the front wall of the volume cavity, and the rear wall of the volume cavity are fixedly connected as one. The two ends of the first connecting pipe are respectively connected with the engine intake pipe and the upper wall of the volume chamber. The two ends of the third connecting pipe are respectively connected with the outlet of the second compressor and the right wall of the volume chamber, and the two ends of the fourth connecting pipe are respectively connected with the second The air inlet of the turbine is connected with the right wall of the volume chamber, the air outlet of the second suction pipe is connected with the air inlet of the second compressor, and the air inlet of the second air outlet pipe is connected with the air outlet of the second turbine , the second compressor is connected to the second turbine through the second connecting shaft, the moving body is installed in the volume cavity and is in sealing contact with the inner wall of the volume cavity, the penetrating pipe runs through the left and right walls of the moving body, and the upper wall of the moving body passes through The spring is connected with the upper wall of the volume chamber.

进一步地,在本发明中第二连接管、第四连接管、贯穿管均为等截面圆管且内径均相同,第二连接管的轴线与第四连接管的轴线重合,第二连接管的轴线、第四连接管的轴线、贯穿管的轴线均在同一平面上。Further, in the present invention, the second connecting pipe, the fourth connecting pipe, and the through pipe are all round pipes with the same cross-section and the same inner diameter, the axis of the second connecting pipe coincides with the axis of the fourth connecting pipe, and the axis of the second connecting pipe The axis, the axis of the fourth connecting pipe, and the axis of the through pipe are all on the same plane.

在本发明中,移动体可以在容积腔内上下移动。当发动机处于低速工况时,发动机进气管内压力较低,移动体上方的容积腔内压力也较低,在弹簧的拉伸作用下,移动体向上移动,从而使第一连接管与第三连接管相隔断,第二连接管与第四连接管相隔断,在整个增压系统中仅有第一压气机和第一涡轮在工作,涡轮当量入口面积较小,脉冲能量可以充分利用,发动机进气压力较大,发动机整机性能较优;当发动机处于高速工况时,发动机进气管内压力较高,移动体上方的容积腔内压力也较高,移动体向下移动并拉伸弹簧,从而使第一连接管与第三连接管相连通,第二连接管与第四连接管相连通,在整个增压系统中第一压气机、第二压气机、第一涡轮和第二涡轮均同时在工作,涡轮当量入口面积较大,发动机泵气损失较小,发动机整机性能较优。In the present invention, the moving body can move up and down in the volume cavity. When the engine is in a low-speed working condition, the pressure in the engine intake pipe is low, and the pressure in the volume cavity above the moving body is also low. Under the tension of the spring, the moving body moves upward, so that the first connecting pipe and the third The connecting pipes are separated, the second connecting pipe is separated from the fourth connecting pipe, only the first compressor and the first turbine are working in the whole booster system, the equivalent inlet area of the turbine is small, the pulse energy can be fully utilized, and the engine The higher the air intake pressure, the better the overall performance of the engine; when the engine is at high speed, the pressure in the engine intake pipe is higher, and the pressure in the volume cavity above the moving body is also higher, and the moving body moves down and stretches the spring , so that the first connecting pipe communicates with the third connecting pipe, and the second connecting pipe communicates with the fourth connecting pipe. In the whole booster system, the first compressor, the second compressor, the first turbine and the second turbine Both are working at the same time, the turbine equivalent inlet area is larger, the engine pumping loss is smaller, and the overall performance of the engine is better.

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,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, can take into account the high and low rotational speed conditions of the engine, and can make the supercharging system not require a special control mechanism.

附图说明 Description of drawings

图1为本发明进排气气路切换装置的结构示意图;Fig. 1 is a schematic structural view of the intake and exhaust gas path switching device 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;

其中:1、第一吸气管,2、第一压气机,3、发动机进气管,4、发动机,5、发动机排气管,6、第一涡轮,7、第一出气管,8、第一连接轴,9、容积腔,10、容积腔上壁面,11、容积腔下壁面,12、容积腔左壁面,13、容积腔右壁面,14、容积腔前壁面,15、容积腔后壁面,16、弹簧,17、第一连接管,18、第二连接管,19、第三连接管,20、第四连接管,21、贯穿管,22、移动体,23、第二压气机,24、第二涡轮,25、第二吸气管,26、第二出气管,27、第二连接轴。Among them: 1. The first suction pipe, 2. The first compressor, 3. The engine intake pipe, 4. The engine, 5. The engine exhaust pipe, 6. The first turbine, 7. The first outlet pipe, 8. The first One connecting shaft, 9, volume cavity, 10, volume cavity upper wall, 11, volume cavity lower wall, 12, volume cavity left wall, 13, volume cavity right wall, 14, volume cavity front wall, 15, volume cavity rear wall , 16, spring, 17, first connecting pipe, 18, second connecting pipe, 19, third connecting pipe, 20, fourth connecting pipe, 21, through pipe, 22, moving body, 23, second compressor, 24, the second turbine, 25, the second air intake pipe, 26, the second air outlet pipe, 27, the second connecting shaft.

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和图2所示,本发明包括:第一吸气管1、第一压气机2、发动机进气管3、发动机4、发动机排气管5、第一涡轮6、第一出气管7、第一连接轴8、容积腔9、容积腔上壁面10、容积腔下壁面11、容积腔左壁面12、容积腔右壁面13、容积腔前壁面14、容积腔后壁面15、弹簧16、第一连接管17、第二连接管18、第三连接管19、第四连接管20、贯穿管21、移动体22、第二压气机23、第二涡轮24、第二吸气管25、第二出气管26和第二连接轴27,第一压气机2的进出气口分别与第一吸气管1的出气口、发动机进气管3的进气口相连接,发动机4的进出气口分别与发动机进气管3的出气口、发动机排气管5的进气口相连接,第一涡轮6的进出气口分别与发动机排气管5的出气口、第一出气管7的进气口相连接,第一压气机2与第一涡轮6通过第一连接轴8相连接,容积腔9的横截面为长方形,容积腔上壁面10、容积腔下壁面11、容积腔左壁面12、容积腔右壁面13、容积腔前壁面14、容积腔后壁面15固接为一体,第一连接管17的两端分别与发动机进气管3、容积腔上壁面10相连通,第二连接管18的两端分别与发动机排气管5、容积腔左壁面12相连通,第三连接管19的两端分别与第二压气机23的出气口、容积腔右壁面13相连通,第四连接管20的两端分别与第二涡轮24的进气口、容积腔右壁面13相连通,第二吸气管25的出气口与第二压气机23的进气口相连接,第二出气管26的进气口与第二涡轮24的出气口相连接,第二压气机23与第二涡轮24通过第二连接轴27相连接,移动体22安装在容积腔9内并与容积腔9的内壁面密封接触,贯穿管21贯穿移动体22的左右两壁面,移动体22的上壁面通过弹簧16与容积腔上壁面10相连接,第二连接管18、第四连接管20、贯穿管21均为等截面圆管且内径均相同,第二连接管18的轴线与第四连接管20的轴线重合,第二连接管18的轴线、第四连接管20的轴线、贯穿管21的轴线均在同一平面上。As shown in Figures 1 and 2, the present invention includes: a first air intake pipe 1, a first compressor 2, an engine intake pipe 3, an engine 4, an engine exhaust pipe 5, a first turbine 6, and a first air outlet pipe 7 , the first connecting shaft 8, the volume cavity 9, the volume cavity upper wall 10, the volume cavity lower wall 11, the volume cavity left wall 12, the volume cavity right wall 13, the volume cavity front wall 14, the volume cavity rear wall 15, the spring 16, First connecting pipe 17, second connecting pipe 18, third connecting pipe 19, fourth connecting pipe 20, through pipe 21, moving body 22, second compressor 23, second turbine 24, second suction pipe 25, The second air outlet pipe 26 and the second connecting shaft 27, the air inlet and outlet of the first compressor 2 are connected with the air outlet of the first air intake pipe 1 and the air inlet of the engine intake pipe 3 respectively, and the air inlet and outlet of the engine 4 are respectively connected with The air outlet of engine intake pipe 3, the air inlet of engine exhaust pipe 5 are connected, the air inlet and outlet of first turbine 6 are connected with the air outlet of engine exhaust pipe 5, the air inlet of the first air outlet pipe 7 respectively, The first compressor 2 is connected to the first turbine 6 through the first connecting shaft 8. The cross section of the volume chamber 9 is rectangular, and the upper wall surface 10 of the volume chamber, the lower wall surface 11 of the volume chamber, the left wall surface 12 of the volume chamber, and the right wall surface of the volume chamber 13. The front wall surface 14 of the volume chamber and the rear wall surface 15 of the volume chamber are fixedly connected as one. The two ends of the first connecting pipe 17 are respectively connected with the engine intake pipe 3 and the upper wall surface 10 of the volume chamber. The two ends of the second connecting pipe 18 are respectively It communicates with the engine exhaust pipe 5 and the left wall surface 12 of the volume chamber, the two ends of the third connecting pipe 19 communicate with the air outlet of the second compressor 23 and the right wall surface 13 of the volume chamber respectively, Connect with the air inlet of the second turbine 24 and the right wall surface 13 of the volume chamber respectively, the air outlet of the second suction pipe 25 is connected with the air inlet of the second compressor 23, the air inlet of the second air outlet pipe 26 Connected to the gas outlet of the second turbine 24, the second compressor 23 is connected to the second turbine 24 through the second connecting shaft 27, the moving body 22 is installed in the volume chamber 9 and is in sealing contact with the inner wall surface of the volume chamber 9, The penetrating pipe 21 runs through the left and right walls of the mobile body 22, and the upper wall of the mobile body 22 is connected to the upper wall surface 10 of the volume cavity through the spring 16. The pipes have the same inner diameter, the axis of the second connecting pipe 18 coincides with the axis of the fourth connecting pipe 20, the axis of the second connecting pipe 18, the axis of the fourth connecting pipe 20, and the axis of the through pipe 21 are all on the same plane.

在本发明中,移动体22可以在容积腔9内上下移动。当发动机4处于低速工况时,发动机进气管3内压力较低,移动体22上方的容积腔9内压力也较低,在弹簧16的拉伸作用下,移动体22向上移动,从而使第一连接管17与第三连接管19相隔断,第二连接管18与第四连接管20相隔断,在整个增压系统中仅有第一压气机2和第一涡轮6在工作,涡轮当量入口面积较小,脉冲能量可以充分利用,发动机4进气压力较大,发动机4的整机性能较优;当发动机4处于高速工况时,发动机进气管3内压力较高,移动体22上方的容积腔9内压力也较高,移动体22向下移动并拉伸弹簧16,从而使第一连接管17与第三连接管19相连通,第二连接管18与第四连接管20相连通,在整个增压系统中第一压气机2、第二压气机23、第一涡轮6和第二涡轮24均同时在工作,涡轮当量入口面积较大,发动机4的泵气损失较小,发动机4整机性能较优。因此,本发明可以较好的兼顾发动机4的高低转速工况。In the present invention, the moving body 22 can move up and down in the volume cavity 9 . When the engine 4 is in a low-speed working condition, the pressure in the engine intake pipe 3 is low, and the pressure in the volume chamber 9 above the moving body 22 is also low. Under the stretching action of the spring 16, the moving body 22 moves upward, thereby making the first A connecting pipe 17 is separated from the third connecting pipe 19, and the second connecting pipe 18 is separated from the fourth connecting pipe 20. In the whole booster system, only the first compressor 2 and the first turbine 6 are working, and the turbine equivalent The inlet area is small, the pulse energy can be fully utilized, the intake pressure of the engine 4 is relatively large, and the overall performance of the engine 4 is better; The pressure in the volume chamber 9 is also relatively high, the moving body 22 moves down and stretches the spring 16, so that the first connecting pipe 17 communicates with the third connecting pipe 19, and the second connecting pipe 18 connects with the fourth connecting pipe 20 Generally, the first compressor 2, the second compressor 23, the first turbine 6 and the second turbine 24 are all working at the same time in the entire supercharging system, the equivalent inlet area of the turbine is relatively large, and the pumping loss of the engine 4 is relatively small. Engine 4 complete machine performance is better. Therefore, the present invention can better take into account the high and low rotational speed working conditions of the engine 4 .

Claims (2)

1.一种进排气气路切换装置,包括:第一吸气管(1)、第一压气机(2)、发动机进气管(3)、发动机(4)、发动机排气管(5)、第一涡轮(6)、第一出气管(7)、第一连接轴(8)、第二压气机(23)、第二涡轮(24)、第二吸气管(25)、第二出气管(26)和第二连接轴(27),第一压气机(2)的进出气口分别与第一吸气管(1)的出气口、发动机进气管(3)的进气口相连接,发动机(4)的进出气口分别与发动机进气管(3)的出气口、发动机排气管(5)的进气口相连接,第一涡轮(6)的进出气口分别与发动机排气管(5)的出气口、第一出气管(7)的进气口相连接,第一压气机(2)与第一涡轮(6)通过第一连接轴(8)相连接,第二吸气管(25)的出气口与第二压气机(23)的进气口相连接,第二出气管(26)的进气口与第二涡轮(24)的出气口相连接,第二压气机(23)与第二涡轮(24)通过第二连接轴(27)相连接,其特征在于还包括容积腔(9)、容积腔上壁面(10)、容积腔下壁面(11)、容积腔左壁面(12)、容积腔右壁面(13)、容积腔前壁面(14)、容积腔后壁面(15)、弹簧(16)、第一连接管(17)、第二连接管(18)、第三连接管(19)、第四连接管(20)、贯穿管(21)、移动体(22),容积腔(9)的横截面为长方形,容积腔上壁面(10)、容积腔下壁面(11)、容积腔左壁面(12)、容积腔右壁面(13)、容积腔前壁面(14)、容积腔后壁面(15)固接为一体,第一连接管(17)的两端分别与发动机进气管(3)、容积腔上壁面(10)相连通,第二连接管(18)的两端分别与发动机排气管(5)、容积腔左壁面(12)相连通,第三连接管(19)的两端分别与第二压气机(23)的出气口、容积腔右壁面(13)相连通,第四连接管(20)的两端分别与第二涡轮(24)的进气口、容积腔右壁面(13)相连通,移动体(22)安装在容积腔(9)内并与容积腔(9)的内壁面密封接触,贯穿管(21)贯穿移动体(22)的左右两壁面,移动体(22)的上壁面通过弹簧(16)与容积腔上壁面(10)相连接。1. An intake and exhaust gas path switching device, comprising: a first air intake pipe (1), a first compressor (2), an engine intake pipe (3), an engine (4), and an engine exhaust pipe (5) , the first turbine (6), the first outlet pipe (7), the first connecting shaft (8), the second compressor (23), the second turbine (24), the second suction pipe (25), the second The air outlet pipe (26) and the second connecting shaft (27), the air inlet and outlet of the first compressor (2) are respectively connected with the air outlet of the first air suction pipe (1) and the air inlet of the engine air intake pipe (3) , the air inlet and outlet of the engine (4) are respectively connected with the air outlet of the engine intake pipe (3) and the air inlet of the engine exhaust pipe (5), and the air inlet and outlet of the first turbine (6) are respectively connected with the engine exhaust pipe ( 5) is connected to the air outlet of the first outlet pipe (7), the first compressor (2) is connected to the first turbine (6) through the first connecting shaft (8), and the second suction pipe The air outlet of (25) is connected with the air inlet of the second compressor (23), the air inlet of the second air outlet pipe (26) is connected with the air outlet of the second turbine (24), and the second air compressor ( 23) It is connected with the second turbine (24) through the second connecting shaft (27), and it is characterized in that it also includes volume cavity (9), volume cavity upper wall surface (10), volume cavity lower wall surface (11), volume cavity left Wall surface (12), volume cavity right wall surface (13), volume cavity front wall surface (14), volume cavity rear wall surface (15), spring (16), first connecting pipe (17), second connecting pipe (18), The third connecting pipe (19), the fourth connecting pipe (20), the through pipe (21), the moving body (22), the cross section of the volume cavity (9) is rectangular, the upper wall of the volume cavity (10), the lower surface of the volume cavity The wall (11), the left wall of the volume cavity (12), the right wall of the volume cavity (13), the front wall of the volume cavity (14), and the rear wall of the volume cavity (15) are fixedly connected as one, and the two parts of the first connecting pipe (17) The two ends of the second connecting pipe (18) are respectively connected with the engine exhaust pipe (5) and the left wall of the volume chamber (12). The two ends of the third connecting pipe (19) are respectively connected with the air outlet of the second compressor (23) and the right wall of the volume chamber (13), and the two ends of the fourth connecting pipe (20) are connected with the second turbine (24) respectively. ) and the right wall of the volume chamber (13), the moving body (22) is installed in the volume chamber (9) and is in sealing contact with the inner wall of the volume chamber (9), and the through pipe (21) runs through the moving body The left and right walls of (22) and the upper wall of the moving body (22) are connected with the upper wall of the volume cavity (10) through a spring (16). 2.根据权利要求1所述的进排气气路切换装置,其特征是所述第二连接管(18)、第四连接管(20)、贯穿管(21)均为等截面圆管且内径均相同,第二连接管(18)的轴线与第四连接管(20)的轴线重合,第二连接管(18)的轴线、第四连接管(20)的轴线、贯穿管(21)的轴线均在同一平面上。2. The intake and exhaust air path switching device according to claim 1, characterized in that the second connecting pipe (18), the fourth connecting pipe (20), and the through pipe (21) are all circular pipes with equal cross-sections and The inner diameters are the same, the axis of the second connecting pipe (18) coincides with the axis of the fourth connecting pipe (20), the axis of the second connecting pipe (18), the axis of the fourth connecting pipe (20), the through pipe (21) axes are on the same plane.
CN201210245944.6A 2012-07-16 2012-07-16 Switching device for admission passage and exhaust passage Expired - Fee Related CN102767425B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210245944.6A CN102767425B (en) 2012-07-16 2012-07-16 Switching device for admission passage and exhaust passage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210245944.6A CN102767425B (en) 2012-07-16 2012-07-16 Switching device for admission passage and exhaust passage

Publications (2)

Publication Number Publication Date
CN102767425A CN102767425A (en) 2012-11-07
CN102767425B true CN102767425B (en) 2014-07-02

Family

ID=47094957

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210245944.6A Expired - Fee Related CN102767425B (en) 2012-07-16 2012-07-16 Switching device for admission passage and exhaust passage

Country Status (1)

Country Link
CN (1) CN102767425B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103089402A (en) * 2013-01-21 2013-05-08 上海交通大学 Through pipe adjusting type parallel connection air circuit system
CN103089404A (en) * 2013-01-21 2013-05-08 上海交通大学 Movable body control type serial connection air circuit device
CN103089401A (en) * 2013-01-21 2013-05-08 上海交通大学 Connection pipe control type parallel connection air circuit system

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3903563C1 (en) * 1988-07-19 1990-03-22 Mtu Friedrichshafen Gmbh
DE4310148C2 (en) * 1993-03-29 1995-03-16 Daimler Benz Ag Internal combustion engine with supercharging
DE102007028522A1 (en) * 2007-06-21 2008-12-24 Ford Global Technologies, LLC, Dearborn Method for operating turbocharged internal combustion engine, involves discharging exhaust gas mass flow, where two exhaust pipes are provided, and two exhaust gas turbo chargers are connected parallel to one another
JP4950082B2 (en) * 2008-01-10 2012-06-13 三菱重工業株式会社 Marine diesel engine

Also Published As

Publication number Publication date
CN102767425A (en) 2012-11-07

Similar Documents

Publication Publication Date Title
CN103382886B (en) Twoly run through pipe type rotation mechanism
CN102562271A (en) Turbocharging system with two rotating plates in front of turbine inlet
CN103382888A (en) Two-axis synchronous exhaust pipe throat area control mechanism
CN102767423A (en) Parallel gas path system with switching mechanism
CN102808688A (en) Switchable turbocharging system
CN102817700A (en) Parallel system of twin-turbo supercharger
CN102817704A (en) Engine system with variable effective circulation area of turbines
CN102767425B (en) Switching device for admission passage and exhaust passage
CN102767418B (en) Synchronous double-moving-body moving device
CN103452644A (en) Exhaust pipe pressure control device with chain
CN103291433A (en) Triaxial synchronous type variable exhaust branch reducing rate system
CN102889121B (en) Intake pressure main control pipeline device
CN102877933A (en) Pipeline system capable of controlling intake pressure and exhaust pressure synchronously and mainly
CN103573394B (en) Multi-part synchronous rotating mechanism
CN102518505A (en) Turbocharger system with movable body arranged in air exhaust pipe
CN102444468B (en) Turbocharging system with moving plate in front of turbine inlet
CN102767420A (en) Partitioning device for connecting pipes
CN103452646B (en) Exhaust manifold circulation area self-regulation type engine system
CN102720581A (en) Mechanically telescopic device with three connection pipes
CN102817702A (en) Engine system with airway switching device
CN103452649B (en) Mechanical exhaust pipe pressure regulating system
CN102383916B (en) Continuously adjustable turbocharger system with exhaust pipe volume
CN102828816A (en) Engine system with double turbine
CN103452647A (en) Circulation area self-adaption system of exhaust manifold
CN103470363A (en) Rotary Exhaust Manifold Throat Area Variable Booster System

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140702

Termination date: 20170716