[go: up one dir, main page]

CN203098039U - Two-stage turbocharger applicable to heavy-duty diesel engine - Google Patents

Two-stage turbocharger applicable to heavy-duty diesel engine Download PDF

Info

Publication number
CN203098039U
CN203098039U CN2012207114103U CN201220711410U CN203098039U CN 203098039 U CN203098039 U CN 203098039U CN 2012207114103 U CN2012207114103 U CN 2012207114103U CN 201220711410 U CN201220711410 U CN 201220711410U CN 203098039 U CN203098039 U CN 203098039U
Authority
CN
China
Prior art keywords
pressure stage
low
volute
turbocharger
exhaust gas
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 - Lifetime
Application number
CN2012207114103U
Other languages
Chinese (zh)
Inventor
王岩
程五九
任官新
巩景林
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.)
Wuxi Cummins Turbo Technologies Co Ltd
Original Assignee
Wuxi Cummins Turbo Technologies Co Ltd
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 Wuxi Cummins Turbo Technologies Co Ltd filed Critical Wuxi Cummins Turbo Technologies Co Ltd
Priority to CN2012207114103U priority Critical patent/CN203098039U/en
Application granted granted Critical
Publication of CN203098039U publication Critical patent/CN203098039U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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

本实用新型涉及涡轮增压器,属于热能与动力机械的结构方领域,具体地说是一种应用于重型柴油机的两级涡轮增压器,包括固定连接在一起的低压级废气涡轮增压器和高压级废气涡轮增压器,所述低压级废气涡轮增压器包括依次安装在一起的第一压气机、第一中间壳、低压级涡壳,所述高压级废气涡轮增压器包括依次安装在一起的第二压气机、第二中间壳、高压级涡壳。本实用新型可以减少压气机端管路安装所需的空间,使整个两级涡轮增压器结构更紧凑,使得在发动机布置上有更好的空间布置优势。

Figure 201220711410

The utility model relates to a turbocharger, which belongs to the structural field of thermal energy and power machinery, in particular to a two-stage turbocharger applied to a heavy-duty diesel engine, including a low-pressure exhaust gas turbocharger fixedly connected together and a high-pressure stage exhaust gas turbocharger, the low-pressure stage exhaust gas turbocharger includes a first compressor, a first intermediate casing, and a low-pressure stage volute installed together in sequence, and the high-pressure stage exhaust gas turbocharger includes sequentially The second compressor, the second intermediate casing, and the high-pressure stage volute installed together. The utility model can reduce the space required for the installation of the pipeline at the compressor end, make the structure of the whole two-stage turbocharger more compact, and have better space arrangement advantages in engine arrangement.

Figure 201220711410

Description

一种应用于重型柴油机的两级涡轮增压器A Two-Stage Turbocharger Applied to Heavy-Duty Diesel Engines

技术领域 technical field

本实用新型涉及涡轮增压器,属于热能与动力机械的结构方领域,具体地说是一种应用于重型柴油机的两级涡轮增压器。 The utility model relates to a turbocharger, which belongs to the structural field of thermal energy and power machinery, in particular to a two-stage turbocharger applied to a heavy-duty diesel engine.

背景技术 Background technique

在两级增压废气涡轮增压器应用中,发动机排出的废气经排气歧管首先进入高压级涡轮壳进行第一级膨胀做功,然后通过与高压级蜗壳、低压级蜗壳分别连接的中间管路,进入到低压级涡轮进行第二级膨胀做功;因为系统中带有中间管路,及连接管路用的V型卡箍或者螺栓,导致传统的通过中间管路连接的两级增压器系统就具有一些不足,如系统零部件数量较多;系统要求的发动机安装空间较大,同时连接接口也比较多,严重影响管路的气密性。 In the application of a two-stage supercharged exhaust gas turbocharger, the exhaust gas discharged from the engine first enters the high-pressure stage turbine casing through the exhaust manifold to perform the first-stage expansion work, and then passes through the high-pressure stage volute and the low-pressure stage volute respectively. The intermediate pipeline enters the low-pressure stage turbine for the second-stage expansion work; because the system has an intermediate pipeline and V-shaped clamps or bolts used to connect the pipeline, the traditional two-stage booster connected through the intermediate pipeline The compressor system has some shortcomings, such as a large number of system components; the system requires a large engine installation space, and at the same time there are many connection interfaces, which seriously affect the airtightness of the pipeline.

发明内容 Contents of the invention

本实用新型针对上述问题,提供一种应用于重型柴油机的两级涡轮增压器,该两级涡轮增压器不需要中间辅助连接管路或额外的连接零件,可以减少压气机端管路安装所需的空间。 In view of the above problems, the utility model provides a two-stage turbocharger applied to heavy-duty diesel engines. The two-stage turbocharger does not need intermediate auxiliary connecting pipelines or additional connecting parts, which can reduce the installation of pipelines at the compressor end. space required.

按照本实用新型的技术方案:一种应用于重型柴油机的两级涡轮增压器,包括固定连接在一起的低压级废气涡轮增压器和高压级废气涡轮增压器,所述低压级废气涡轮增压器包括依次安装在一起的第一压气机、第一中间壳、低压级涡壳,所述高压级废气涡轮增压器包括依次安装在一起的第二压气机、第二中间壳、高压级涡壳,特征是:所述低压级涡壳的进气口直接密封连接高压级涡壳的第一出气口,所述第二压气机的第二出气口朝向与第二压气机轴向平行,指向第二中间壳一侧。 According to the technical solution of the utility model: a two-stage turbocharger applied to heavy-duty diesel engines, including a low-pressure stage exhaust gas turbocharger and a high-pressure stage exhaust gas turbocharger fixedly connected together, the low-pressure stage exhaust gas turbocharger The supercharger includes a first compressor, a first intermediate casing, and a low-pressure stage volute that are installed together in sequence, and the high-pressure stage exhaust gas turbocharger includes a second compressor, a second intermediate casing, and a high-pressure stage that are installed together in sequence. The stage volute is characterized in that: the inlet of the low-pressure stage volute is directly sealed to the first gas outlet of the high-pressure stage volute, and the second gas outlet of the second compressor is oriented parallel to the axial direction of the second compressor , pointing to the side of the second middle shell.

作为本实用新型的进一步改进,所述低压级涡壳上设置有一个以上的安装支架。 As a further improvement of the utility model, more than one mounting bracket is arranged on the low-pressure stage volute.

作为本实用新型的进一步改进,所述低压级涡壳的进气口与所述高压级涡壳的第一出气口通过螺栓固定连接。 As a further improvement of the present utility model, the air inlet of the low-pressure stage volute is fixedly connected with the first air outlet of the high-pressure stage volute by bolts.

作为本实用新型的进一步改进,所述低压级涡壳的进气口与所述高压级涡壳的第一出气口通过V型卡箍固定连接。 As a further improvement of the present utility model, the air inlet of the low-pressure stage volute is fixedly connected with the first air outlet of the high-pressure stage volute through a V-shaped clamp.

本实用新型的技术效果在于:本实用新型通过将高、低压级废气涡轮增压器直接连接,减少了高、低压级涡壳间连接的零件数量,此结构具有较少的密封面和连接件,从而提高了系统的可靠性;同时低压级蜗壳上设置通安装支架,可以直接与发动机连接固定,减少了增压器系统的零件数量,系统结构更紧凑,要求的安装空间更小;高压级压气机出口走向做了优化设计,可以减少压气机端管路安装所需的空间,使整个两级涡轮增压器结构更紧凑,使得在发动机布置上有更好的空间布置优势。 The technical effect of the utility model lies in: the utility model reduces the number of parts connected between the high and low pressure volutes by directly connecting the high and low pressure exhaust gas turbochargers, and this structure has fewer sealing surfaces and connectors , thereby improving the reliability of the system; at the same time, the low-pressure stage volute is provided with a through-mount bracket, which can be directly connected to the engine and fixed, reducing the number of parts of the turbocharger system, the system structure is more compact, and the required installation space is smaller; The outlet direction of the two-stage compressor has been optimized, which can reduce the space required for the installation of the pipeline at the compressor end, make the structure of the entire two-stage turbocharger more compact, and have better space layout advantages in engine layout.

附图说明 Description of drawings

图1为本实用新型的结构示意图。 Fig. 1 is the structural representation of the utility model.

图2为本实用新型的结构侧视图。 Fig. 2 is a structural side view of the utility model.

图3为本实用新型的结构侧视图。 Fig. 3 is a side view of the structure of the utility model.

具体实施方式 Detailed ways

下面结合附图对本实用新型的具体实施方式作进一步的说明。 Below in conjunction with accompanying drawing, the specific embodiment of the present utility model is described further.

图1~图3所示,包括低压级废气涡轮增压器1、高压级废气涡轮增压器2、第一压气机3、低压级涡壳4、第二压气机5、高压级涡壳6、进气口7、第一出气口8、第二出气口9、第二中间壳10、第一中间壳11、安装支架12等。 As shown in Figures 1 to 3, it includes a low-pressure stage exhaust gas turbocharger 1, a high-pressure stage exhaust gas turbocharger 2, a first compressor 3, a low-pressure stage volute 4, a second compressor 5, and a high-pressure stage volute 6 , Air inlet 7, first air outlet 8, second air outlet 9, second middle shell 10, first middle shell 11, mounting bracket 12, etc.

如图1所示,本实用新型是一种两级涡轮增压器,包括固定连接在一起的低压级废气涡轮增压器1和高压级废气涡轮增压器2,所述低压级废气涡轮增压器1包括依次安装在一起的第一压气机3、第一中间壳11、低压级涡壳4,所述高压级废气涡轮增压器2包括依次安装在一起的第二压气机5、第二中间壳10、高压级涡壳6,所述低压级涡壳4的进气口7直接密封连接高压级涡壳6的第一出气口8,所述第二压气机5的第二出气口9朝向与第二压气机5轴向平行,指向第二中间壳10一侧。 As shown in Figure 1, the utility model is a two-stage turbocharger, comprising a low-pressure stage exhaust gas turbocharger 1 and a high-pressure stage exhaust gas turbocharger 2 fixedly connected together, the low-pressure stage exhaust gas turbocharger The compressor 1 includes a first compressor 3, a first intermediate shell 11, and a low-pressure stage volute 4 installed together in sequence, and the high-pressure stage exhaust gas turbocharger 2 includes a second compressor 5, a second compressor installed in sequence Two intermediate casings 10, high-pressure stage volute 6, the air inlet 7 of the low-pressure stage volute 4 is directly sealed and connected to the first air outlet 8 of the high-pressure stage volute 6, and the second air outlet of the second compressor 5 9 is oriented parallel to the axial direction of the second compressor 5 and directed to the side of the second intermediate shell 10 .

所述低压级涡壳4上设置有一个以上的安装支架12。 More than one mounting bracket 12 is arranged on the low-pressure stage volute 4 .

所述低压级涡壳4的进气口7与所述高压级涡壳6的第一出气口8通过螺栓固定连接。 The air inlet 7 of the low-pressure stage volute 4 is fixedly connected with the first air outlet 8 of the high-pressure stage volute 6 through bolts.

所述低压级涡壳4的进气口7与所述高压级涡壳6的第一出气口8通过V型卡箍固定连接。 The air inlet 7 of the low-pressure stage volute 4 is fixedly connected with the first air outlet 8 of the high-pressure stage volute 6 through a V-shaped clamp.

本实用新型的工作过程如下:汽车发动机废气首先通过排气歧管进入高压级废气涡轮增压器2,经过高压级涡壳6导流进入高压级涡轮膨胀做功,废气膨胀后通过第一出气口8直接进入低压级涡壳4,经过低压级涡壳4流道的导流进入低压级涡轮进行二次膨胀做功,然后经低压级涡壳4出气口流出。在压气机端,经过空气滤清器的新鲜空气首先进入第一压气机3,被低压级涡轮带动的同轴压叶轮压缩空气,使空气被压缩,压力提高,第一次压缩后空气,进入到第二压气机5,再次被压缩,最后进入到发动机参与燃烧。 The working process of the utility model is as follows: the exhaust gas of the automobile engine first enters the high-pressure exhaust gas turbocharger 2 through the exhaust manifold, and then enters the high-pressure turbine through the high-pressure volute 6 to expand and perform work. After the exhaust gas expands, it passes through the first gas outlet. 8 directly enters the volute 4 of the low pressure stage, and enters the turbine of the low pressure stage through the diversion of the flow channel of the volute 4 of the low pressure stage to perform secondary expansion work, and then flows out through the gas outlet of the volute 4 of the low pressure stage. At the compressor end, the fresh air passing through the air filter first enters the first compressor 3, and the coaxial impeller driven by the low-pressure stage turbine compresses the air, so that the air is compressed and the pressure increases. After the first compression, the air enters To the second compressor 5, it is compressed again, and finally enters the engine to participate in combustion.

本实用新型通过将高、低压级废气涡轮增压器直接连接,减少了高、低压级涡壳间连接的零件数量,此结构具有较少的密封面和连接件,从而提高了系统的可靠性;同时低压级蜗壳上设置通安装支架,可以直接与发动机连接固定,减少了增压器系统的零件数量,系统结构更紧凑,要求的安装空间更小;高压级压气机出口走向做了优化设计,可以减少压气机端管路安装所需的空间,使整个两级涡轮增压器结构更紧凑,使得在发动机布置上有更好的空间布置优势。 The utility model reduces the number of parts connected between the high and low pressure stage volutes by directly connecting the high and low pressure stage exhaust gas turbochargers. This structure has fewer sealing surfaces and connecting parts, thereby improving the reliability of the system At the same time, the low-pressure stage volute is equipped with a through-mounting bracket, which can be directly connected to the engine, reducing the number of parts in the supercharger system, making the system more compact and requiring less installation space; the outlet direction of the high-pressure stage compressor has been optimized. The design can reduce the space required for the installation of the pipeline at the compressor end, and make the structure of the entire two-stage turbocharger more compact, so that there is a better space arrangement advantage in the engine layout.

Claims (4)

1.一种应用于重型柴油机的两级涡轮增压器,包括固定连接在一起的低压级废气涡轮增压器(1)和高压级废气涡轮增压器(2),所述低压级废气涡轮增压器(1)包括依次安装在一起的第一压气机(3)、第一中间壳(11)、低压级涡壳(4),所述高压级废气涡轮增压器(2)包括依次安装在一起的第二压气机(5)、第二中间壳(10)、高压级涡壳(6),其特征是:所述低压级涡壳(4)的进气口(7)直接密封连接高压级涡壳(6)的第一出气口(8),所述第二压气机(5)的第二出气口(9)朝向与第二压气机(5)轴向平行,指向第二中间壳(10)一侧。 1. A two-stage turbocharger applied to a heavy-duty diesel engine, comprising a low-pressure stage exhaust gas turbocharger (1) and a high-pressure stage exhaust gas turbocharger (2) fixedly connected together, the low-pressure stage exhaust gas turbocharger (2) The supercharger (1) includes a first compressor (3), a first intermediate casing (11), and a low-pressure stage volute (4) installed together in sequence, and the high-pressure stage exhaust gas turbocharger (2) includes sequentially The second compressor (5), the second intermediate casing (10), and the high-pressure stage volute (6) installed together are characterized in that the air inlet (7) of the low-pressure stage volute (4) is directly sealed The first air outlet (8) connected to the high-pressure stage volute (6), the second air outlet (9) of the second compressor (5) is oriented parallel to the axial direction of the second compressor (5), pointing to the second One side of the middle shell (10). 2.按照权利要求1所述的一种应用于重型柴油机的两级涡轮增压器,其特征是:所述低压级涡壳(4)上设置有一个以上的安装支架(12)。 2. A two-stage turbocharger applied to a heavy-duty diesel engine according to claim 1, characterized in that: the low-pressure stage volute (4) is provided with more than one mounting bracket (12). 3.按照权利要求1所述的一种应用于重型柴油机的两级涡轮增压器,其特征是:所述低压级涡壳(4)的进气口(7)与所述高压级涡壳(6)的第一出气口(8)通过螺栓固定连接。 3. A two-stage turbocharger applied to heavy-duty diesel engines according to claim 1, characterized in that: the air inlet (7) of the low-pressure stage volute (4) is connected to the high-pressure stage volute The first air outlet (8) of (6) is fixedly connected by bolts. 4.按照权利要求1所述的一种应用于重型柴油机的两级涡轮增压器,其特征是:所述低压级涡壳(4)的进气口(7)与所述高压级涡壳(6)的第一出气口(8)通过V型卡箍固定连接。 4. A two-stage turbocharger applied to heavy-duty diesel engines according to claim 1, characterized in that: the air inlet (7) of the low-pressure stage volute (4) is connected to the high-pressure stage volute The first air outlet (8) of (6) is fixedly connected by a V-shaped clamp.
CN2012207114103U 2012-12-20 2012-12-20 Two-stage turbocharger applicable to heavy-duty diesel engine Expired - Lifetime CN203098039U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2012207114103U CN203098039U (en) 2012-12-20 2012-12-20 Two-stage turbocharger applicable to heavy-duty diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2012207114103U CN203098039U (en) 2012-12-20 2012-12-20 Two-stage turbocharger applicable to heavy-duty diesel engine

Publications (1)

Publication Number Publication Date
CN203098039U true CN203098039U (en) 2013-07-31

Family

ID=48849446

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2012207114103U Expired - Lifetime CN203098039U (en) 2012-12-20 2012-12-20 Two-stage turbocharger applicable to heavy-duty diesel engine

Country Status (1)

Country Link
CN (1) CN203098039U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102979616A (en) * 2012-12-20 2013-03-20 无锡康明斯涡轮增压技术有限公司 Two-stage turbocharger applied to heavy-duty diesel engine
CN104847695A (en) * 2015-05-13 2015-08-19 张澄宇 Stage-middle air bleeding type air compressor based on micro-turbine jet engine
CN110284958A (en) * 2019-05-31 2019-09-27 北京理工大学 A two-stage supercharging system for a V-shaped internal combustion engine
CN113374548A (en) * 2021-06-02 2021-09-10 东风康明斯发动机有限公司 Two-stage supercharger system of V-shaped diesel engine
US11448118B2 (en) 2018-09-04 2022-09-20 Caterpillar Motoren Gmbh & Co. Kg Two-stage turbocharged internal combustion engine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102979616A (en) * 2012-12-20 2013-03-20 无锡康明斯涡轮增压技术有限公司 Two-stage turbocharger applied to heavy-duty diesel engine
CN104847695A (en) * 2015-05-13 2015-08-19 张澄宇 Stage-middle air bleeding type air compressor based on micro-turbine jet engine
US11448118B2 (en) 2018-09-04 2022-09-20 Caterpillar Motoren Gmbh & Co. Kg Two-stage turbocharged internal combustion engine
CN110284958A (en) * 2019-05-31 2019-09-27 北京理工大学 A two-stage supercharging system for a V-shaped internal combustion engine
CN113374548A (en) * 2021-06-02 2021-09-10 东风康明斯发动机有限公司 Two-stage supercharger system of V-shaped diesel engine

Similar Documents

Publication Publication Date Title
SU609484A3 (en) Internal combustion engine
JP4387411B2 (en) Turbo compressor system for an internal combustion engine having two in-line turbo units with a coaxial rotation axis
CN203098039U (en) Two-stage turbocharger applicable to heavy-duty diesel engine
CN102840169B (en) Centrifugal compressor used for generating two different pressure ratios
CN113123854B (en) Supercharging system and serial two-stage turbocharging structure thereof
CN102434268A (en) Double-turbine double-air-compressor turbocharging system
CN102979616A (en) Two-stage turbocharger applied to heavy-duty diesel engine
CN101027473A (en) Pipe line for a turbocharger system for an internal combustion engine
CN102400777B (en) Single-vortex double-air compressor turbine pressurizing system with air escape valves
CN102418593B (en) Single-vortex double-pressure turbocharging system
CN105508035A (en) Supercharged diesel engine multi-mode switch supercharging structure and method
CN206158836U (en) Exhaust system and vehicle of engine
CN111946444A (en) Three-stage variable-section turbine two-stage sequential supercharging system and control method
CN101027459A (en) Turbo charger unit for IC engine
CN102444464A (en) Twin-scroll single-pressure turbo system
CN104520550B (en) Exhaust module and reciprocating engine
US9581079B2 (en) Two-stage turbocharger apparatus
CN102434283A (en) Integrated low-pressure stage turbine shell structure of two-stage supercharging exhaust gas turbocharger
CN215520988U (en) Two-stage supercharger system of V-shaped diesel engine
CN106368800B (en) A kind of supercharger structure that single shaft dual-air compressor is controllable
CN215213678U (en) Supercharging system and serial two-stage turbocharging structure thereof
CN104100360A (en) Supercharged internal combustion engine and combined member system for the supercharged internal combustion engine and a supercharged device
CN110284958B (en) A two-stage supercharging system for V-type internal combustion engine
CN111878234A (en) A gas turbine system
CN218030313U (en) Integrated serial two-stage supercharging structure for realizing high-low pressure stage pressure ratio distribution

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20130731

CX01 Expiry of patent term