CN202140163U - Turbocharger and engine - Google Patents

Turbocharger and engine Download PDF

Info

Publication number
CN202140163U
CN202140163U CN201120193318U CN201120193318U CN202140163U CN 202140163 U CN202140163 U CN 202140163U CN 201120193318 U CN201120193318 U CN 201120193318U CN 201120193318 U CN201120193318 U CN 201120193318U CN 202140163 U CN202140163 U CN 202140163U
Authority
CN
China
Prior art keywords
compressor
turbine
turbocharger
intermediate body
thrust
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
CN201120193318U
Other languages
Chinese (zh)
Inventor
晁鑫
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.)
SAIC General Motors Corp Ltd
Pan Asia Technical Automotive Center Co Ltd
Original Assignee
Pan Asia Technical Automotive Center Co Ltd
Shanghai General Motors 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 Pan Asia Technical Automotive Center Co Ltd, Shanghai General Motors Co Ltd filed Critical Pan Asia Technical Automotive Center Co Ltd
Priority to CN201120193318U priority Critical patent/CN202140163U/en
Application granted granted Critical
Publication of CN202140163U publication Critical patent/CN202140163U/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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

本实用新型涉及一种涡轮增压器以及发动机,涡轮增压器包括有涡轮机、压缩机、中间体、电磁阀、电子进气旁通阀、废气旁通阀执行器,其中涡轮机与中间体的一端相连接,压缩机与中间体的另一端相连接,电磁阀设置在所述压缩机的壳体上,其中所述电磁阀分别连通到压缩机的进气口和排气口,电磁阀进一步与中央电子控制模块电性连接,所述废气旁通阀执行器与所述涡轮机相连接,所述电子进气旁通阀固定在压缩机的壳体上,并且所述电子进气旁通阀同样与中央电子控制模块电性连接。

Figure 201120193318

The utility model relates to a turbocharger and an engine. The turbocharger includes a turbine, a compressor, an intermediate body, a solenoid valve, an electronic intake bypass valve, and a waste gas bypass valve actuator, wherein the turbine and the intermediate body One end is connected, the compressor is connected with the other end of the intermediate body, and the solenoid valve is arranged on the shell of the compressor, wherein the solenoid valve is connected to the air inlet and the exhaust port of the compressor respectively, and the solenoid valve further It is electrically connected with the central electronic control module, the actuator of the wastegate valve is connected with the turbine, the electronic intake bypass valve is fixed on the casing of the compressor, and the electronic intake bypass valve It is also electrically connected with the central electronic control module.

Figure 201120193318

Description

Turbosupercharger and motor
[technical field]
The utility model relates to a kind of turbosupercharger, and especially, the utility model relates to a kind of Motor Vehicle supercharging turbosupercharger of starting and motor that is provided with this turbosupercharger of being used for.
[background technique]
Well-known motor does work at combustor inner cylinder by fuel and produces power, sucks air quantitative limitation in the cylinder because the fuel quantity of input receives, and the power that motor produced thus also is restricted.If the ride quality of motor has been in the optimum state, further increases output power and can only increase burning capacity, thereby improve the work by combustion ability through compression more air entering cylinder.Thus, produced turbosupercharger, it increases output power under the constant situation of engine operation efficient.Turbo charging installation increases the air inflow of motor through pressurized air.
Turbo charging installation mainly is made up of turbine chamber and pressurized machine; Wherein the suction port of turbine chamber links to each other with enmgine exhaust and relief opening then is connected on the outlet pipe; The suction port of pressurized machine links to each other with the air-strainer pipeline and its relief opening is connected on the intake manifold; Turbine and impeller are contained in respectively in turbine chamber and the pressurized machine, the two coaxial rigid connection.Generally, the waste gas inertia impulsive force that turbosupercharging utilizes motor to discharge promotes the turbine in the turbine chamber, makes turbine drive coaxial impeller, and the air that the impeller force feed is sent here by the air-strainer pipeline makes it supercharging and gets into cylinder.When engine speed speeds; The waste gas velocity of discharge and secondary speed also speed synchronously; Impeller just compresses more air and gets into cylinder; The pressure of air and density increase the more fuel that can burn, corresponding increase fuel quantity with adjust the rotating speed of motor, thereby increase the output power of motor.
One Chinese patent application discloses a kind of exhaust gas turbocharger internal combustion engine CN200680005485.7 number, and it has at least one cylinder, is compressed machine 10 precompressed fuel one air mixtures and in cylinder, is compressed and burns; Produced waste gas in this course; Waste gas from cylinder, discharge and in turbo machine 19 by step-down, wherein the part waste gas of discharging from cylinder turbo machine 19 by step-down before or after, be recovered through high pressure or low pressure exhaust gas recirculating line; Said pipeline is equipped with exhaust gas cooling device; It comprises that one or at least two cooling circuits, these loops pass along the heat exchanger core of the flow direction series connection of waste gas, wherein is arranged in as far as possible the heat exchanger core in downstream along exhaust gas flow direction and arranges with the mode of erectting; Like this; Heat exchanger core is just parallel or be basically parallel to the line of action of gravity, from percolation down or from top to bottom, is provided with that condensed fluid compiles and/or tapping equipment by waste gas simultaneously in the underpart of heat exchanger core.
One Chinese patent application also discloses a kind of turbosupercharger CN200580017214.9 number; It has the turbine shroud that has a turbine wheel, has to be arranged in the sleeve that is used for variable turbine geometry in the turbine shroud, has the bearing housing between the compressor housing that is arranged in this turbine shroud and compressor impeller; And wherein arrange to be useful on the axle that carries this turbine wheel and this compressor impeller; And have the dish arrangement that is arranged between housing and this bearing housing, and wherein should dish arrangement form by at least two material layers, air gap is arranged between these material layers; A material layer is designed to conical disc, and another material layer is provided with bending.
[ The model utility content]
A purpose of the utility model is, a kind of technological scheme of new turbosupercharger is provided, its compact structure, arrangement convenience.
The above-mentioned purpose of the utility model solves through following technological scheme with other purposes:
The utility model provides a kind of turbosupercharger; Wherein said turbosupercharger includes turbo machine, compressor, intermediate, solenoid valve, electronics air inlet bypass valve, exhaust gas bypass valve actuator; Wherein said turbo machine is connected with an end of said intermediate; Said compressor is connected with the other end of said intermediate
Said solenoid valve is arranged on the housing of said compressor, and wherein said solenoid valve is communicated to the suction port and the relief opening of said compressor respectively, and said solenoid valve further electrically connects with central eletronics,
Said exhaust gas bypass valve actuator is connected with said turbo machine,
Said electronics air inlet bypass valve is fixed on the housing of compressor, and said electronics air inlet bypass valve is same and central eletronics electrically connects.
The turbosupercharger that the utility model provided, preferably, said turbo machine passes through the V-type clip connected to an end of said intermediate, and said compressor is connected on the other end of said intermediate through bolt.
The turbosupercharger that the utility model provided, preferably, the inlet flange of said turbo machine is the triangle flange with the flange of giving vent to anger.
The turbosupercharger that the utility model provided preferably, is integrated with the crankcase ventilation pipeline at the suction port place of said compressor.
The turbosupercharger that the utility model provided, preferably, the axial almost parallel of the air outlet of the axial and said compressor of the turnover oil duct of said intermediate; The inlet flange approximate vertical of the axial and said turbo machine of the turnover oil duct of said intermediate.
The turbosupercharger that the utility model provided, preferably, the inside that a coupling shaft 20 is supported on said intermediate through spring bearing and the support sleeve that is arranged on this coupling shaft.
The turbosupercharger that the utility model provided preferably, is equipped with the turbine assembly of turbo machine at an end of said coupling shaft, and the impeller of said compressor is installed at the other end of said coupling shaft.
The turbosupercharger that the utility model provided, preferably, said turbine assembly and said coupling shaft are whole to be constituted, and the impeller of said compressor perhaps radially is fixed on the other end of said coupling shaft through lock screw through the key connection.
The turbosupercharger that the utility model provided preferably, is provided with screw thread at the other end of said coupling shaft, and locking nut is spun on the said screw thread and the impeller of said compressor is resisted against on the said locking nut.
The turbosupercharger that the utility model provided; Preferably; On said coupling shaft, also be provided with thrust bush, thrust bearing and thrust plate; One end of wherein said thrust bearing is resisted against on the thrust plate, and the other end is resisted against an end of said thrust bush, and the other end of said thrust bush is against the opposite side of the impeller of said compressor.
The turbosupercharger that the utility model provided, preferably, said thrust bush is supported by the intermediate backboard of intermediate diametrically.
The turbosupercharger that the utility model provided preferably, is provided with at least one seal ring on said thrust bush.
The turbosupercharger that the utility model provided preferably, is provided with thermal shield between said turbo machine and said intermediate.
Understand easily, any reasonable combination of technique scheme is obviously also within the protection domain of the utility model.
In addition, another purpose of the utility model is to provide a kind of motor that comprises aforementioned arbitrary said turbosupercharger.
[description of drawings]
Below in conjunction with accompanying drawing, the preferred implementation of the utility model is carried out in detail or preferred the description, wherein,
Fig. 1 is the stereogram of an angle of the turbosupercharger of the utility model.
Fig. 2 is the stereogram of another angle of the turbosupercharger of the utility model.
Fig. 3 is the sectional view of the turbosupercharger of the utility model.
[embodiment]
Understand easily, according to the technological scheme of the utility model, under the connotation that does not change the utility model, one of ordinary skill in the art can propose a plurality of mode of structure of the utility model.Therefore following embodiment and accompanying drawing only are to the specifying of the technological scheme of the utility model, and should not be regarded as the utility model all perhaps be regarded as qualification or restriction to the utility model technological scheme.
Below with reference to figure 1 and Fig. 2; The turbosupercharger of the utility model mainly includes turbo machine 1, compressor 2, intermediate 3, solenoid valve 4, electronics air inlet bypass valve 5, exhaust gas bypass valve actuator 6; Wherein, Said turbo machine 1 is connected with an end of said intermediate 3, and the other end of said intermediate 3 is connected with said compressor 2.Preferably, said turbo machine 1 passes through the V-type clip connected to an end of said intermediate 3, and said compressor 2 is fastenedly connected on the other end of said intermediate through bolt connection ground mode.Further preferably, the inlet flange of turbo machine 1 is the triangle flange, can be connected with gas exhaust manifold by three fastening pieces during use; The flange of giving vent to anger is similarly the triangle flange, is connected with ternary catalyzing unit by other three fastening pieces during use.Suction port place at said compressor 2 preferably is integrated with the crankcase ventilation pipeline.Said solenoid valve 4 is arranged on the housing of compressor 2, and preferably is fixed on the housing of compressor 2 through bolt connection ground mode.Wherein, said solenoid valve 4 preferably is connected respectively to the suction port and the relief opening of compressor 2 through the connection flexible pipe, and said solenoid valve 4 further electrically connects with central eletronics.Said solenoid valve 4 is mainly used in control exhaust gas bypass valve actuator 6, be used under the different operating modes of motor, regulating the exhaust flow flux through turbo machine, thereby the rotating speed of control turbosupercharger realizes controlling suction pressure.Said exhaust gas bypass valve actuator 6 is connected with said turbo machine 1.Said electronics air inlet bypass valve 5 is fixed on the housing of compressor 2, its role is to the air pressure after the compression is remained within the setting range, thus the device damage of avoiding overvoltage to cause.The 5 same and central eletronics electric connections of electronics air inlet bypass valve.
Further preferably, the axial almost parallel of the air outlet of the axial and said compressor 2 of the turnover oil duct of said intermediate 3; The inlet flange approximate vertical of the axial and turbo machine 1 of the turnover oil duct of intermediate 3 preferably is 84 ° of angles.
Further with reference to accompanying drawing 3, it schematically shows the sectional view of the turbosupercharger of the utility model.As shown in the figure, coupling shaft 20 is through being arranged on the inside that spring bearing 15 and support sleeve 16 on the coupling shaft 20 is supported on intermediate 2.At an end of coupling shaft 20 the turbine assembly 7 of turbo machine 1 is installed, preferably, said turbine assembly 7 and coupling shaft 20 are whole to be constituted.At the other end of coupling shaft 20 impeller 8 of compressor 2 is installed, the impeller of said compressor 2 for example can connect or radially be fastened on the other end of coupling shaft 20 through lock screw through key.Said coupling shaft 20 axially on, be provided with screw thread at the other end of coupling shaft 20, make the side of impeller of compressor 20 against the locking nut 17 that is spun on this screw thread.On said coupling shaft 20, also be provided with thrust bush 12, thrust bearing 13 and thrust plate 14; One end of wherein said thrust bearing 13 is resisted against on the thrust plate 14; The other end is resisted against an end of said thrust bush 12, and the other end of said thrust bush 12 is against the opposite side of the impeller 8 of said compressor 20.Said thrust bush 12 is supported by the intermediate backboard 10 of intermediate 2 diametrically.In addition, on said thrust bush 12, also be provided with at least one seal ring 18, said seal ring 18 is used for preventing that lubricant oil from flowing into impeller 8.As shown in Figure 3, turbo machine 1 preferably is connected with said intermediate 3 through V-type clip 9.And, between said turbo machine 1 and said intermediate 3, also be provided with thermal shield 11, in order to prevent the heat circulation between turbo machine 1 and the intermediate 3.
Obviously, the turbocharger arrangement of the utility model is simple, and connection and reasonable arrangement can be widely used in the motor of multiple vehicle.

Claims (14)

1.一种涡轮增压器,其特征在于,所述涡轮增压器包括有涡轮机、压缩机、中间体、电磁阀、电子进气旁通阀、废气旁通阀执行器,其中所述涡轮机与所述中间体的一端相连接,所述压缩机与所述中间体的另一端相连接,1. A turbocharger, characterized in that, the turbocharger includes a turbine, a compressor, an intermediate, a solenoid valve, an electronic intake bypass valve, and a wastegate actuator, wherein the turbine connected to one end of the intermediate body, the compressor is connected to the other end of the intermediate body, 所述电磁阀设置在所述压缩机的壳体上,其中所述电磁阀分别连通到所述压缩机的进气口和排气口,并且所述电磁阀进一步与中央电子控制模块电性连接,The solenoid valve is arranged on the casing of the compressor, wherein the solenoid valve is connected to the air inlet and the exhaust port of the compressor respectively, and the solenoid valve is further electrically connected with the central electronic control module , 所述废气旁通阀执行器与所述涡轮机相连接,the wastegate actuator is coupled to the turbine, 所述电子进气旁通阀固定在压缩机的壳体上,并且所述电子进气旁通阀同样与中央电子控制模块电性连接。The electronic intake bypass valve is fixed on the casing of the compressor, and the electronic intake bypass valve is also electrically connected to the central electronic control module. 2.如权利要求1所述的涡轮增压器,其特征在于,所述涡轮机通过V型卡箍连接到所述中间体的一端上,并且所述压缩机通过螺栓连接到所述中间体的另一端上。2. The turbocharger according to claim 1, wherein the turbine is connected to one end of the intermediate body by a V-clamp, and the compressor is connected to an end of the intermediate body by bolts. on the other end. 3.如权利要求1所述的涡轮增压器,其特征在于,所述涡轮机的进气法兰和出气法兰均为三角法兰。3. The turbocharger according to claim 1, wherein the inlet flange and the outlet flange of the turbine are triangular flanges. 4.如权利要求1所述的涡轮增压器,其特征在于,在所述压缩机的进气口处集成有曲轴箱通风管路。4. The turbocharger of claim 1, wherein a crankcase ventilation line is integrated at the air inlet of the compressor. 5.如权利要求1所述的涡轮增压器,其特征在于,所述中间体的进出油道的轴向与所述压缩机的出气口的轴向大致平行;所述中间体的进出油道的轴向与所述涡轮机的进气法兰大致垂直。5. The turbocharger according to claim 1, wherein the axial direction of the oil inlet and outlet of the intermediate body is approximately parallel to the axial direction of the air outlet of the compressor; the oil inlet and outlet of the intermediate body The axial direction of the duct is approximately perpendicular to the intake flange of the turbine. 6.如权利要求1所述的涡轮增压器,其特征在于,一连接轴通过设置在该连接轴上的支撑轴承和支撑轴套支撑在所述中间体的内部。6. The turbocharger according to claim 1, wherein a connecting shaft is supported inside the intermediate body through a supporting bearing and a supporting bush provided on the connecting shaft. 7.如权利要求6所述的涡轮增压器,其特征在于,在所述连接轴的一端安装有涡轮机的涡轮总成,在所述连接轴的另一端安装有所述压缩机的叶轮。7. The turbocharger according to claim 6, wherein a turbine assembly of a turbine is mounted on one end of the connecting shaft, and an impeller of the compressor is mounted on the other end of the connecting shaft. 8.如权利要求7所述的涡轮增压器,其特征在于,所述涡轮总成与所述连接轴整体构成,并且所述压缩机的叶轮通过键连接或者通过锁紧螺钉径向固定在所述连接轴的另一端上。8. The turbocharger according to claim 7, wherein the turbine assembly is formed integrally with the connecting shaft, and the impeller of the compressor is fixed radially on the shaft through a key connection or through locking screws. on the other end of the connecting shaft. 9.如权利要求7所述的涡轮增压器,其特征在于,在所述连接轴的另一端设有螺纹,锁紧螺母旋在所述螺纹上并且所述压缩机的叶轮抵靠在所述锁紧螺母上。9. The turbocharger according to claim 7, wherein a screw thread is provided at the other end of the connecting shaft, a lock nut is screwed on the screw thread and the impeller of the compressor abuts against the screw thread. on the locknut described above. 10.如权利要求9所述的涡轮增压器,其特征在于,在所述连接轴上还设有止推轴套、止推轴承和止推板,其中所述止推轴承的一端抵靠在止推板上,另一端抵靠在所述止推轴套的一端,所述止推轴套的另一端抵靠所述压缩机的叶轮的另一侧。10. The turbocharger according to claim 9, wherein a thrust bushing, a thrust bearing and a thrust plate are also provided on the connecting shaft, wherein one end of the thrust bearing abuts against On the thrust plate, the other end abuts against one end of the thrust sleeve, and the other end of the thrust sleeve abuts against the other side of the impeller of the compressor. 11.如权利要求10所述的涡轮增压器,其特征在于,所述止推轴套在径向上由中间体的中间体背板支撑。11. The turbocharger of claim 10, wherein the thrust bushing is radially supported by an intermediate body back plate of the intermediate body. 12.如权利要求10所述的涡轮增压器,其特征在于,在所述止推轴套上设有至少一个密封环。12. The turbocharger of claim 10, wherein at least one sealing ring is provided on the thrust bush. 13.如权利要求7所述的涡轮增压器,其特征在于,在所述涡轮机和所述中间体之间设有隔热罩。13. The turbocharger of claim 7, wherein a heat shield is provided between the turbine and the intermediate body. 14.一种发动机,所述发动机包括前述任一权利要求所述的涡轮增压器。14. An engine comprising a turbocharger as claimed in any preceding claim.
CN201120193318U 2011-06-09 2011-06-09 Turbocharger and engine Expired - Fee Related CN202140163U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201120193318U CN202140163U (en) 2011-06-09 2011-06-09 Turbocharger and engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201120193318U CN202140163U (en) 2011-06-09 2011-06-09 Turbocharger and engine

Publications (1)

Publication Number Publication Date
CN202140163U true CN202140163U (en) 2012-02-08

Family

ID=45551223

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201120193318U Expired - Fee Related CN202140163U (en) 2011-06-09 2011-06-09 Turbocharger and engine

Country Status (1)

Country Link
CN (1) CN202140163U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105626236A (en) * 2014-11-26 2016-06-01 上海通用汽车有限公司 Turbosupercharged engine assembly for vehicle
CN106285916A (en) * 2016-09-13 2017-01-04 中国北方发动机研究所(天津) A kind of Novel supercharger structure
CN119222031A (en) * 2023-06-30 2024-12-31 浙江春风动力股份有限公司 All Terrain Vehicles

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105626236A (en) * 2014-11-26 2016-06-01 上海通用汽车有限公司 Turbosupercharged engine assembly for vehicle
CN105626236B (en) * 2014-11-26 2019-03-29 上海通用汽车有限公司 Vehicle turbocharged engine assembly
CN106285916A (en) * 2016-09-13 2017-01-04 中国北方发动机研究所(天津) A kind of Novel supercharger structure
CN119222031A (en) * 2023-06-30 2024-12-31 浙江春风动力股份有限公司 All Terrain Vehicles

Similar Documents

Publication Publication Date Title
CN103370511B (en) Internal-combustion engine
JP4875654B2 (en) Supercharger
CN101782015B (en) Internal combustion engine with exhaust-gas turbocharging
CN104088702A (en) Compact micro gas turbine
CN103282619A (en) Multi-stage supercharging device
CN107810315B (en) Internal combustion engine system
GB2500192A (en) Compact Multi-Stage Turbo Pump
CN106321240A (en) Centrifugal compression reactive radial-flow internal combustion engine
US20120152214A1 (en) Turbocharger system
CN202140163U (en) Turbocharger and engine
JP2012149588A (en) Controller for internal combustion engine
CN104314669B (en) Variable indexing turbocharger
CN101182805A (en) Internal Combustion Engine Exhaust Gas Turbine Electric Compressor System
CN105298633A (en) Adjustable type exhaust gas turbocharger
CN202431358U (en) Turbocharger of gasoline engine
CN110080830A (en) A kind of radial-flow type supercharging device of included back disk impinging cooling
CN203476492U (en) Twin-turbocharger arrangement for large internal combustion engines
CN213016540U (en) Turbocharged engine assembly
CN202391493U (en) Gasoline engine turbocharger turbine casing integrated with exhaust pipe manifold
CN207813733U (en) A kind of two-stage turbocharger of the double membranous cochleas of twin turbines
CN103109057A (en) Exhaust module and internal combustion engine
CN202402178U (en) Air damper turbocharging mixed flow device
CN102155287B (en) Structure capable of exhaust emission
CN2661934Y (en) Exhaust gas turbo charger
CN203559981U (en) Electronic-control turbofan supercharger

Legal Events

Date Code Title Description
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: 20120208

Termination date: 20200609