CN102003272A - Double-channel air exhausting device of double-flow channel turbocharger - Google Patents
Double-channel air exhausting device of double-flow channel turbocharger Download PDFInfo
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- CN102003272A CN102003272A CN201010529253XA CN201010529253A CN102003272A CN 102003272 A CN102003272 A CN 102003272A CN 201010529253X A CN201010529253X A CN 201010529253XA CN 201010529253 A CN201010529253 A CN 201010529253A CN 102003272 A CN102003272 A CN 102003272A
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- bleed passage
- air exhausting
- double
- turbine volute
- flow channel
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Abstract
The invention discloses a double-channel air exhausting device of a double-flow channel turbocharger. The air exhausting device comprises a turbine volute, wherein two air inlet flow channels are formed in the turbine volute; the turbine volute is provided with an air exhausting channel which is communicated with the two air inlet flow channels respectively; and an air exhausting valve is arranged at the outlet of the air exhausting channel and is in transmission connection with an execution mechanism on the turbine volute. Mutual influence of exhaust pulses of the two air inlet flow channels of the double-flow channel turbine volute is restrained by a simple device and energy loss caused by the entrance of waste gas into the air exhausting channel when an engine runs at a low speed is reduced. The air exhausting device has a simple structure; an air exhausting port is molded in the casting process of the turbine volute; and compared with a double-air exhausting channel double-air exhausting valve device, the air exhausting device can effectively lower processing and assembly difficulty and cost and contributes to enhancing the sealing performance of the air exhausting valve and the reliability of a bypass air exhausting device of the turbocharger.
Description
Technical field
The present invention relates to a kind of exhaust gas bypass device of turbosupercharger, specifically, relate to a kind of bypass means of deflation that is used for the double flow channel turbosupercharger.
Background technique
During the vehicular engine turbocharger operation, the waste gas that motor is discharged enters the turbine volute of turbosupercharger, promoting turbine wheel rotation acting back discharges, turbine wheel drives coaxial mounted compressor impeller high speed rotating, the extraneous air that sucks is also sent into engine cylinder combustion after the compression, thereby improve the density of the induced air of motor, reach the purpose that improves engine power and reduce discharging.
Tight and people are to the improving constantly of engine performance requirement along with adding of Abgasgesetz, and turbosupercharger is widely used in diesel engine, and develops into the exhaust gas bypass device by original constant cross-section device.Adopt the pressurized machine of exhaust gas bypass device that the match point of pressurized machine and motor is moved to maximum torque point by rated point, help improving the low-speed torque characteristic and the accelerating performance of motor, solved the discharging that diesel engine quickens the problem of over-emitting black exhaust and reduced motor effectively.When the low engine speed low-load, the waste gas that motor is discharged all enters the turbine acting; When the high engine speeds high load, for avoiding too high boost pressure and supercharger speed, exhaust gas by-pass valve is opened, and a part of waste gas that enters turbine volute directly is bypassed to the turbine volute outlet without turbine wheel, thereby boost pressure is controlled in the safe scope.The bypass means of deflation has become the device that generally adopts on the turbosupercharger at present.
Be to improve the low speed torque and the accelerating performance of motor, multicylinder engine is generally adopted the pressurization system of ram charging, correspondingly turbosupercharger has also adopted double flow channel air inlet turbine device.High operating mode is that the exhaust pressure of each cylinder of motor is consistent when exitting, and avoids the difference cylinder of motor to be operated under the different conditions, and the turbosupercharger of double flow channel air inlet generally adopts Twin channel bypass means of deflation.
As shown in Figure 1, the turbine volute 1 of traditional double flow channel turbosupercharger is provided with air inlet runner 2a and air inlet runner 2b, air inlet runner 2a is communicated with bleed passage 14a, air inlet runner 2b is communicated with bleed passage 14b, venting valve 15a is installed on bleed passage 14a, venting valve 15b is installed on bleed passage 14b, venting valve 15a and venting valve 15b control the venting of bleed passage 14a and bleed passage 14b respectively, the device relative complex, discharge quantity identical and avoid the exit valve 15a of while in order to guarantee air inlet runner 2a and air inlet runner 2b, venting valve 15b does not leak gas when closing, the assembly precision of the machining accuracy of two valve seats and valve assembly is required very high, this brings difficulty to production and processing.
And this turbosupercharger is under the low engine speed operating mode, its venting valve is in closed condition, adopt two air inlet runners to be in airtight connected state this moment, after the exhaust pulses of motor enters one of them air inlet runner, part waste gas pours another air inlet runner from bleed passage under the effect of flow differential pressure, cause each cylinder exhaust phase mutual interference of motor and be unfavorable for that turbo operating state keeps stable.
Summary of the invention
The problem to be solved in the present invention is in order to overcome the defective that traditional double flow channel bypass means of deflation exists, provide a kind of install simple, easy to process, take up room little and can effectively control the bypass means of deflation of the double flow channel turbosupercharger of bypass discharge quantity.
In order to address the above problem, the technical solution used in the present invention is:
A kind of Twin channel means of deflation of double flow channel turbosupercharger, comprise turbine volute, be provided with two air inlet runners in the described turbine volute, described turbine volute is provided with the bleed passage that is communicated with respectively with two air inlet runners, in the outlet port of bleed passage the venting valve is installed, described venting valve is in transmission connection with the actuator that is installed on the turbine volute.
Below be further improvement of these options of the present invention:
Described bleed passage comprises bleed passage front portion, bleed passage fluidic junction, bleed passage middle part and the bleed passage rear portion that is communicated with successively.
Further improve:
Position on the described turbine volute between bleed passage middle part and bleed passage rear portion is provided with the boss shape valve seat, and the valve gap of described venting valve and boss shape valve seat are connected.
Further improve:
Described two air inlet runners are respectively equipped with air vent, and one of them air vent is communicated with bleed passage is anterior, and another air vent is communicated with the bleed passage fluidic junction.
Further improve:
The axial cross section of described air vent is shaped as the gradually-reducing shape structure shape, and the inlet area of described air vent is greater than discharge area.
Further improve:
The sectional area of described bleed passage front portion is greater than the discharge area of air vent, less than the sectional area in the middle part of the bleed passage.
Further improve:
The axial cross section of described bleed passage fluidic junction is shaped as flaring type structure shape.
The present invention adopts such scheme, when motor is in low-speed running, for improving low speed torque, obtain bigger running moment of torsion, the venting valve is in closed state under the control of actuator, thereby will close, thereby provide sufficiently high boost pressure to motor with the bleed passage of the turbosupercharger of bypass means of deflation.
The axial cross section of described air vent and air vent is shaped as the gradually-reducing shape structure shape, after the engine exhaust pulse of one of them air inlet runner enters, because waste gas enters bleed passage from an air inlet runner and enters the process of another air inlet runner again, its pressure descends earlier and afterwards rises, flow velocity increases afterwards earlier and descends, it is a kind of flow process that quickens the back diffusion earlier, enter another air inlet runner exhaust pulses and decay to zero substantially, flow and be subjected to very big obstruction, suppressed waste gas effectively and entered another air inlet runner, thereby avoided the exhaust pulses between two groups of cylinders of motor to disturb effectively from an air inlet runner.
Motor is in middle and high when running speed, the exhaust energy abundance that motor is discharged, for in allowed limits with boost pressure and maximum explosive pressure and supercharger speed restriction, the venting valve is in open mode under the control of actuator, two runners of the turbine volute of double flow channel device are in the open communication state.The a part of waste gas that enters turbo machine is drained by bleed passage without turbine wheel, makes the travel line of motor under the high loaded process state approach horizontal line, thereby reduces boost pressure.Because the longitudinal cross-section of air vent and air vent is shaped as the gradually-reducing shape structure shape, the waste gas that enters the venting runner is that step-down is quickened to flow, and because exhaust shortening blanking time, the internal pressure of two runners was more or less the same in engine exhaust interim, and its internal pressure all is higher than the pressure in the bleed passage, guaranteed that waste gas can not enter the turbine volute runner from bleed passage, no matter engine operation is in which kind of working state, can both effectively avoid two runners of double flow channel turbine volute to produce the exhaust pulses interference, waste gas enters bleed passage and causes too much energy loss when effectively being suppressed at low engine speed.
The present invention regulates the rotating speed of turbosupercharger by the switching of regulating bleed passage, reaches the control engine output, improves the purpose of engine operation efficient, and the power character of motor, Economy are significantly improved, and satisfies various emission standards.
The present invention adopts simple device to suppress the influencing each other of exhaust pulses of two air inlet runners of double flow channel turbine volute, and waste gas enters the energy loss that bleed passage causes when having reduced low engine speed.The present invention is simple in structure, the moulding in the turbine volute casting process of its air vent, with respect to the two bleed valve door devices of two bleed passages, can effectively reduce the difficulty and the cost of processing and assembling, the reliability that helps improving the sealability of venting valve and improve turbosupercharger bypass means of deflation.
The invention will be further described below in conjunction with the drawings and specific embodiments:
Description of drawings
Accompanying drawing 1 is the two bleed passage double valve device schematic representation that are used for the double flow channel turbosupercharger in the background technique;
Accompanying drawing 2 is the device schematic representation that are used for two bleed passage single valve door device valve closes states of double flow channel turbosupercharger in the embodiment of the invention;
Accompanying drawing 3 is structural representations of air inlet runner and bleed passage in the embodiment of the invention;
Among the figure: the 1-turbine volute; 2a, 2b-air inlet runner; 3a, 3b-air vent; 4,14a, 14b-bleed passage; 5-bleed passage front portion; 6-actuator; 7-bleed passage fluidic junction; 8-bleed passage middle part; The 9-transmission device; The 10-rocking arm; 11,15a, 15b-venting valve; 12-bleed passage rear portion; 13-boss shape valve seat; The F1-inlet area; The F2-discharge area; F3, F4-sectional area.
Embodiment
Embodiment, as shown in Figure 2, a kind of Twin channel means of deflation of double flow channel turbosupercharger, comprise turbine volute 1, be provided with two air inlet runners in the described turbine volute 1: air inlet runner 2a and air inlet runner 2b, described turbine volute 1 is provided with the bleed passage 4 that is communicated with respectively with air inlet runner 2a and air inlet runner 2b, and venting valve 11 is installed in the outlet port of bleed passage 4, and described venting valve 11 is in transmission connection with the actuator 6 that is installed on the turbine volute 1.
Described bleed passage 4 comprises bleed passage front portion 5, bleed passage fluidic junction 7, bleed passage middle part 8 and the bleed passage rear portion 12 that is communicated with successively.
Position on the described turbine volute 1 between bleed passage middle part 8 and bleed passage rear portion 12 is provided with boss shape valve seat 13, and described venting valve 11 is connected with boss shape valve seat 13.
Described air inlet runner 2a is provided with air vent 3a, and air inlet runner 2b is provided with air vent 3b, and described air vent 3a is communicated with bleed passage anterior 5, and described air vent 3b is communicated with bleed passage fluidic junction 7.
Be in transmission connection by transmission device 9 and rocking arm 10 between described venting valve 11 and the actuator 6, driven by actuator 6 and transmission device 9, around the rotation of A1 axle, thereby open or close bleed passage, its aperture is by actuator's 6 controls.
When motor is in low-speed running, for improving low speed torque, obtain bigger running moment of torsion, venting valve 11 is in closed state under the control of actuator 6, thereby bleed passage 4 is closed, thereby provides sufficiently high boost pressure to motor.
As shown in Figure 3, for producing exhaust pulses, disturb two runners effectively avoiding the double flow channel turbine volute, waste gas enters bleed passage 4 and causes too much energy loss when effectively being suppressed at low engine speed, the axial cross section of described air vent 3a and air vent 3b is shaped as the gradually-reducing shape structure shape, and the inlet area F1 of described air vent 3a and air vent 3b is greater than discharge area F2.
After the engine exhaust pulse of one of them air inlet runner enters, because waste gas enters bleed passage from an air inlet runner and enters the process of another air inlet runner again, its pressure descends earlier and afterwards rises, flow velocity increases afterwards earlier and descends, it is a kind of flow process that quickens the back diffusion earlier, enter another air inlet runner exhaust pulses and decay to zero substantially, flow and be subjected to very big obstruction, suppressed waste gas effectively and entered another air inlet runner, thereby avoided the exhaust pulses between two groups of cylinders of motor to disturb effectively from an air inlet runner.
The sectional area F3 of described bleed passage front portion 5 is greater than the discharge area F2 of air vent 3b, and less than the sectional area F4 at bleed passage middle part 8; The axial cross section of bleed passage fluidic junction 7 is shaped as flaring type structure shape.
As shown in Figure 4, motor is in middle and high when running speed, the exhaust energy abundance that motor is discharged, for in allowed limits with boost pressure and maximum explosive pressure and supercharger speed restriction, venting valve 11 is in open mode under the control of actuator 6, two runners of the turbine volute of double flow channel device are in the open communication state.The a part of waste gas that enters turbo machine is drained by bleed passage 4 without turbine wheel, makes the travel line of motor under the high loaded process state approach horizontal line, thereby reduces boost pressure.Because the longitudinal cross-section of air vent 3a and air vent 3b is shaped as the gradually-reducing shape structure shape, the waste gas that enters venting runner 4 is that step-down is quickened to flow, and because exhaust shortening blanking time, the internal pressure of two runners was more or less the same in engine exhaust interim, and its internal pressure all is higher than the pressure in the bleed passage 4, has guaranteed that waste gas can not enter the turbine volute runner from bleed passage.
The present invention regulates the rotating speed of turbosupercharger by the switching of regulating bleed passage, reaches the control engine output, improves the purpose of engine operation efficient, and the power character of motor, Economy are significantly improved, and satisfies various emission standards.
In the foregoing description, the radial cross section shape of described air vent 3a, air vent 3b can be circle or rectangle, and the sectional shape at described bleed passage front portion 5, bleed passage fluidic junction 7, bleed passage middle part 8 is designed to circle or rectangle accordingly.
We have been described in detail invention according to the national patent method now, can discern the improvement or the replacement of specific embodiment disclosed herein for those skilled in the art.These modifications are within the spirit and scope of the present invention.
Claims (7)
1. the Twin channel means of deflation of a double flow channel turbosupercharger, comprise turbine volute (1), be provided with two air inlet runners (2a, 2b) in the described turbine volute (1), it is characterized in that: described turbine volute (1) is provided with the bleed passage that is communicated with respectively with two air inlet runners (2a, 2b), venting valve (11) is installed in the outlet port of bleed passage, and described venting valve (11) is in transmission connection with the actuator (6) that is installed on the turbine volute (1).
2. the Twin channel means of deflation of double flow channel turbosupercharger according to claim 1 is characterized in that: described bleed passage comprises bleed passage front portion (5), bleed passage fluidic junction (7), the bleed passage middle part (8) and bleed passage rear portion (12) that is communicated with successively.
3. the Twin channel means of deflation of double flow channel turbosupercharger according to claim 2, it is characterized in that: the position that is positioned on the described turbine volute (1) between the bleed passage middle part (8) and bleed passage rear portion (12) is provided with boss shape valve seat (13), and the valve gap of described venting valve (11) and boss shape valve seat (13) are connected.
4. the Twin channel means of deflation of double flow channel turbosupercharger according to claim 3, it is characterized in that: described two air inlet runners (2a, 2b) are respectively equipped with air vent (3a, 3b), one of them air vent (3a) is communicated with bleed passage front portion (5), and another air vent (3b) is communicated with bleed passage fluidic junction (7).
5. the Twin channel means of deflation of double flow channel turbosupercharger according to claim 4, it is characterized in that: the axial cross section of described air vent (3a, 3b) is shaped as the gradually-reducing shape structure shape, and the inlet area (F1) of described air vent (3a3b) is greater than discharge area (F2).
6. the Twin channel means of deflation of double flow channel turbosupercharger according to claim 4 is characterized in that: the sectional area (F3) of described bleed passage front portion (5) is greater than the discharge area (F2) of air vent (3a, 3b), less than the sectional area (F4) at bleed passage middle part (8).
7. the Twin channel means of deflation of double flow channel turbosupercharger according to claim 4 is characterized in that: the axial cross section of described bleed passage fluidic junction (7) is shaped as flaring type structure shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010529253XA CN102003272B (en) | 2010-11-03 | 2010-11-03 | Double-channel air exhausting device of double-flow channel turbocharger |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201010529253XA CN102003272B (en) | 2010-11-03 | 2010-11-03 | Double-channel air exhausting device of double-flow channel turbocharger |
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| CN102003272A true CN102003272A (en) | 2011-04-06 |
| CN102003272B CN102003272B (en) | 2012-06-06 |
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| CN201010529253XA Active CN102003272B (en) | 2010-11-03 | 2010-11-03 | Double-channel air exhausting device of double-flow channel turbocharger |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102383877A (en) * | 2011-10-08 | 2012-03-21 | 康跃科技股份有限公司 | Volute device of variable geometry pulse gas inlet turbine |
| CN104005837A (en) * | 2013-02-20 | 2014-08-27 | 福特环球技术公司 | Supercharged internal combustion engine with two-channel turbine and method for operating an internal combustion engine of said type |
| CN104302889A (en) * | 2012-05-29 | 2015-01-21 | 博格华纳公司 | Exhaust-gas turbocharger |
| CN104879211A (en) * | 2015-06-16 | 2015-09-02 | 潍柴动力股份有限公司 | Device and method for controlling turbocharger with asymmetric runners |
| CN107956521A (en) * | 2017-12-21 | 2018-04-24 | 湖南天雁机械有限责任公司 | A kind of supercharger worm-gear case for improving engine EGR rate |
| CN109154229A (en) * | 2016-05-12 | 2019-01-04 | 大陆汽车有限公司 | The turbine with double volute turbine cylinder and with the valve gear for improving outflow for exhaust-driven turbo-charger exhaust-gas turbo charger |
| CN110735673A (en) * | 2019-11-18 | 2020-01-31 | 大连海事大学 | kinds of double-channel volute |
| CN113931706A (en) * | 2021-10-20 | 2022-01-14 | 无锡康明斯涡轮增压技术有限公司 | Turbine shell assembly for double-runner turbocharger and turbocharger |
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| CN101460710A (en) * | 2006-05-31 | 2009-06-17 | 康明斯涡轮增压技术有限公司 | Turbocharger with dual wastegate |
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| US4355503A (en) * | 1979-01-12 | 1982-10-26 | Daimler-Benz Aktiengesellschaft | Exhaust gas turbocharger |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102383877A (en) * | 2011-10-08 | 2012-03-21 | 康跃科技股份有限公司 | Volute device of variable geometry pulse gas inlet turbine |
| CN104302889A (en) * | 2012-05-29 | 2015-01-21 | 博格华纳公司 | Exhaust-gas turbocharger |
| CN104302889B (en) * | 2012-05-29 | 2016-12-21 | 博格华纳公司 | Exhaust turbine supercharger |
| CN104005837A (en) * | 2013-02-20 | 2014-08-27 | 福特环球技术公司 | Supercharged internal combustion engine with two-channel turbine and method for operating an internal combustion engine of said type |
| CN104879211A (en) * | 2015-06-16 | 2015-09-02 | 潍柴动力股份有限公司 | Device and method for controlling turbocharger with asymmetric runners |
| CN104879211B (en) * | 2015-06-16 | 2017-12-05 | 潍柴动力股份有限公司 | The control device and control method of asymmetric path turbocharger |
| US10767554B2 (en) | 2016-05-12 | 2020-09-08 | Continental Automotive Gmbh | Turbine for an exhaust gas turbocharger with a two-volute turbine housing and a valve arrangement having improved outflow |
| CN109154229A (en) * | 2016-05-12 | 2019-01-04 | 大陆汽车有限公司 | The turbine with double volute turbine cylinder and with the valve gear for improving outflow for exhaust-driven turbo-charger exhaust-gas turbo charger |
| CN109154229B (en) * | 2016-05-12 | 2021-01-15 | 大陆汽车有限公司 | Turbine for an exhaust-gas turbocharger |
| CN107956521A (en) * | 2017-12-21 | 2018-04-24 | 湖南天雁机械有限责任公司 | A kind of supercharger worm-gear case for improving engine EGR rate |
| CN107956521B (en) * | 2017-12-21 | 2024-03-19 | 湖南天雁机械有限责任公司 | Supercharger turbine box capable of improving EGR rate of engine |
| CN110735673A (en) * | 2019-11-18 | 2020-01-31 | 大连海事大学 | kinds of double-channel volute |
| CN113931706A (en) * | 2021-10-20 | 2022-01-14 | 无锡康明斯涡轮增压技术有限公司 | Turbine shell assembly for double-runner turbocharger and turbocharger |
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| CN102003272B (en) | 2012-06-06 |
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Effective date of registration: 20201228 Address after: No.1 luoqian street, Gucheng street, Shouguang City, Weifang City, Shandong Province Patentee after: Kangyue Technology (Shandong) Co.,Ltd. Address before: 262700 science and Technology Industrial Zone, Shouguang Development Zone, Shandong Patentee before: KANGYUE TECHNOLOGY Co.,Ltd. |
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Denomination of invention: Dual channel bleeding device of dual channel turbocharger Effective date of registration: 20220516 Granted publication date: 20120606 Pledgee: Shandong Shouguang Rural Commercial Bank Co.,Ltd. Pledgor: Kangyue Technology (Shandong) Co.,Ltd. Registration number: Y2022980005594 |
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