CN102536439A - Electrically controlled variable geometrical turbocharger - Google Patents
Electrically controlled variable geometrical turbocharger Download PDFInfo
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- CN102536439A CN102536439A CN2012100159339A CN201210015933A CN102536439A CN 102536439 A CN102536439 A CN 102536439A CN 2012100159339 A CN2012100159339 A CN 2012100159339A CN 201210015933 A CN201210015933 A CN 201210015933A CN 102536439 A CN102536439 A CN 102536439A
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- turbine
- automatically controlled
- controlled variable
- drive link
- variable geometry
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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 an electrically controlled variable geometrical turbocharger which comprises a turbine shell, a middle body and a compressor shell which are connected together; the middle body is internally and rotatably provided with a turbine shaft; one end of the turbine shaft is fixedly provided with a turbine; the turbine is arranged in the turbine shell; the other end of the turbine shaft is fixedly provided with a compressor impeller; the compressor impeller is arranged in the compressor shell; the turbine shell is internally fixedly provided with a turbine sleeve; an air inlet cavity for facilitating rotation of the turbine is formed between the turbine shell and the turbine sleeve; a plurality of nozzle ring blades are fixedly arranged between the air inlet cavity and the turbine; a regulating device for regulating the angles of the nozzle ring blades is arranged between the middle body and the turbine sleeve; the regulating device comprises an installing disk and a driving disk; the nozzle ring blades are installed on the installing disk; the driving disk is connected with an electrically controlled actuator for driving the driving disk through a linkage mechanism; and the turbine sleeve is fixedly provided with a rib for guiding the direction of an air flow. The electrically controlled variable geometrical turbocharger has the advantages of wide flow range, precise flow control, good low-speed response, non-excessive pressurization and the like.
Description
Technical field
The present invention relates to the engine component field, relate in particular to a kind of automatically controlled variable geometry turbocharger.
Background technique
Turbocharging technology is to realize that combustion engine energy-saving reduces discharging, satisfies the key technology of increasingly stringent emission regulation demands, and turbocharging technology is crossed over to the variable geometry turbine supercharging technology from traditional exhaust gas bypass turbocharging technology at present.Supercharging technology utilizes the waste heat overbottom pressure ability drive pressure mechanism of qi in the exhaust gases of internal combustion engines, improves the density of the induced air of motor, thereby increases substantially the specific power of motor; Reduce fuel consume, and significantly reduce the discharging of pollutant, the exhaust gas bypass turbosupercharger makes moderate progress to low engine speed performance and mapping aspect; But when the high operating mode of motor, because bleed valve splitter section high-pressure gas has lost expendable-limited-recoverable energy; Thereby influenced the high speed performance of motor, can not solve the slow problem of discharging of variable working condition speed of response simultaneously fully, therefore with reduction; Present exhaust gas bypass turbosupercharger can only satisfy state 2 and state's 3 Abgasgesetzs; Can't satisfy state 4 and above emission regulation demands, variable geometry turbocharger turns down the nozzle actual internal area when low engine speed, increases the acting ability of motor; Air demand when improving low speed; Thereby obviously improve the low engine speed torque characteristics and improve the engine acceleration ability, when high engine speeds, amplify the nozzle actual internal area, avoid pressurized machine hypervelocity and cylinder-firing pressure superpressure.
The development course of variable geometry turbine supercharging technology is a hydraulic pressure, pneumatic, automatically controlled; The present invention provides a kind of automatically controlled variable geometry turbocharger; Can solve the fixed turbosupercharger variable working condition low-response of band bleed valve, defective such as oil consumption high, low speed torque characteristics is poor, the low velocity discharge smoke intensity is big; Having the degree of regulation height, respond advantages such as fast, is the high-end of variable geometry turbine supercharging technology, satisfies the requirement of state 4 and above Abgasgesetz.
Summary of the invention
The technical problem that the present invention solved is to provide a kind of automatically controlled variable geometry turbocharger, and it is narrow to have solved range of flow, and bad response during low speed is prone to the problem that breaks down during high speed.
The technological scheme of the technical problem that the present invention solved is: a kind of automatically controlled variable geometry turbocharger, comprise the turbine case, intermediate and the compressor casing that link together, and be rotatablely equipped with turbine shaft in the intermediate; One end of turbine shaft is fixed with turbine; Turbine is arranged in the turbine case, and the other end of turbine shaft is fixed with compressor impeller, and compressor impeller is arranged in the compressor casing; The turbine case internal fixation is equipped with the turbine cover; Form the air-inlet cavity that impels the turbine rotation between turbine case and the turbine cover, be installed with several nozzle blades between air-inlet cavity and the turbine, be provided with the controlling device that is used to adjust the nozzle blade angle between intermediate and the turbine cover.
As optimized technical scheme; Controlling device comprises mounting disc, is coaxially installed with drive plate in the mounting disc, and nozzle blade is installed in the mounting disc; Crank is installed on the drive plate; The other end of crank connects nozzle blade, and drive plate connects the automatically controlled final controlling element that is used to drive drive plate through linkage mechanism, and automatically controlled final controlling element is installed on the compressor casing.
As optimized technical scheme, linkage mechanism comprises first drive link and second drive link, and first drive link and second drive link are hinged, and first drive link connects automatically controlled final controlling element, and second drive link connects drive plate.
As optimized technical scheme, automatically controlled final controlling element comprises the ECU of motor and control motor, and motor and ECU are installed in the final controlling element housing, and motor drives first drive link through turbine and worm mechanism.
As optimized technical scheme, turbine puts the rib that is fixed with the steering flow direction.
Owing to adopted the automatically controlled variable geometry turbocharger of technique scheme; Waste gas in the air-inlet cavity of turbosupercharger impels the turbine rotation, adopts the angle of automatically controlled final controlling element regulating and controlling device adjustment nozzle blade, and utilize automatically controlled final controlling element to accomplish like this: variable geometry turbocharger turns down the nozzle actual internal area when low engine speed; Increase the acting ability of motor; Air demand when improving low speed, thus obviously improve the low engine speed torque characteristics and improve the engine acceleration ability, when high engine speeds, amplify the nozzle actual internal area; Avoid pressurized machine hypervelocity and cylinder-firing pressure superpressure, thereby solved the narrow problem of range of flow.
Owing to adopted automatically controlled final controlling element to come the regulating and controlling device; According to the electronic signal regulating and controlling device of motor feedback, and then the angle of swing of change nozzle blade, make the angle of regulating nozzle blade more accurate; The control of being convenient to become more meticulous; When low speed and high speed, can in time adjust the angle of swing of nozzle blade according to operating mode, thereby the control exit area of nozzle reaches the purpose of controlling pressurized machine flow and rotating speed.
Owing to adopted the turbine that is fixed in the turbine case to put the rib that is provided with the steering flow direction, airflow direction that can direct exhaust reduces windage loss.
This invention is simple in structure, has advantages such as range of flow is wide, flow control accurate, low speed response property is good, and supercharging is inexcessive.
Description of drawings
Fig. 1 is the structural representation of the automatically controlled variable geometry turbocharger of the present invention;
Fig. 2 is the side-looking structural representation of Fig. 1;
Fig. 3 is the structural representation of controlling device of the nozzle blade of the automatically controlled variable geometry turbocharger of the present invention;
Fig. 4 is the automatically controlled actuator structure schematic representation of the automatically controlled variable geometry turbocharger of the present invention;
Fig. 5 is the turbine nested structure wind direction guiding schematic representation of the automatically controlled variable geometry turbocharger of the present invention;
Among the figure: 1. turbine case, 2. intermediate, 3. compressor casing, 4. turbine shaft, 5. turbine, 6. compressor impeller; 7. turbine cover, 8. air-inlet cavity, 9. nozzle blade, 10. automatically controlled final controlling element, 101. ECUs, 102. motor; 103. the turbine and worm output mechanism, 104. final controlling element housings, 11. controlling devices, 111. mounting discs, 112. drive plates; 113. crank, 12. linkage mechanisms, 121. first drive link, 122. second drive link, 13. ribs.
Embodiment
Below in conjunction with accompanying drawing and embodiment, further set forth the present invention, should be understood that these embodiments only be used to the present invention is described and be not used in the restriction scope of the present invention.Should be understood that in addition those skilled in the art can do various changes or modification to the present invention after the content of having read the present invention's instruction, these equivalent form of values fall within the application's appended claims institute restricted portion equally.
Shown in Fig. 1, a kind of automatically controlled variable geometry turbocharger comprises the turbine case 1, intermediate 2 and the compressor casing 3 that link together; Be rotatablely equipped with turbine shaft 4 in the intermediate 2, an end of turbine shaft 4 is fixed with turbine 5, and turbine 5 is arranged in the turbine case 1; The other end of turbine shaft 4 is fixed with compressor impeller 6; Compressor impeller 6 is arranged in the compressor casing 3, and turbine case 1 internal fixation is equipped with turbine cover 7, forms the air-inlet cavity 8 that impels turbine 5 rotations between turbine case 1 and the turbine cover 7; Be installed with several nozzle blades 9 between air-inlet cavity 8 and the turbine 5, be provided with the controlling device 11 that is used to adjust nozzle blade 9 angles between intermediate 2 and the turbine cover 1.
Like Fig. 1, Fig. 2, shown in Figure 3; Controlling device 11 comprises mounting disc 111, is coaxially installed with drive plate 112 in the mounting disc 111, and nozzle blade 9 is installed in the mounting disc 111; Crank 113 is installed on the drive plate 112; The other end of crank 113 connects nozzle blade 9, and drive plate 112 connects the automatically controlled final controlling element 10 that is used to drive drive plate 112 through linkage mechanism 12, and automatically controlled final controlling element 10 is installed on the compressor casing 3.
Like Fig. 1, Fig. 2, shown in Figure 3; Linkage mechanism 12 comprises first drive link 121 and second drive link 122; First drive link 121 and second drive link 122 are hinged, and first drive link 121 connects automatically controlled final controlling element 10, the second drive link 122 and connects drive plate 112.
Like Fig. 1, Fig. 2, shown in Figure 4; Automatically controlled final controlling element 10 comprises the ECU 101 of motor 102 and control motor 102; Motor 102 is installed in the final controlling element housing 104 with ECU 101, and motor 102 drives first drive link 121 through turbine and worm mechanism 103.
Like Fig. 1, shown in Figure 5, be fixed with the rib 13 of steering flow direction on the turbine cover 7.
Air-inlet cavity 8 is the waste gas air-inlet cavitys that cooperated the confession exhaust-gas flow that forms by turbine case 1 with turbine cover 7; Turbine 5 utilizes the energy of waste gas to rotate; The signal drive electric motor 102 that ECU 101 sends is rotated, and the rotation of motor 102 is ordered about the rotation of turbine and worm mechanism 103 and ordered about the motion of first drive link 121, because of first drive link 121 and 122 splicing of second drive link; Then second drive link 122 is stirred drive plate 112 rotations; Through the angle of crank 113 and then adjusting nozzle blade 9, turbine cover 2 can compress mounting disc 111, prevents to rotate.
When automatically controlled variable geometry turbocharger was worked, automatically controlled final controlling element 10 received the state signal of motors, handles; Adopt the high automatically controlled final controlling element 10 of reliability of signal adaptive, contactless differential capacitance type angle transducer is adopted in the angle measurement of automatically controlled variable geometry turbocharger, can effectively avoid mechanical failure; Interface circuit can be communicated by letter with any engine signal Adaptive matching, has avoided automatically controlled variable geometry turbocharger and motor to have the unmatched possibility of signal, controls the rotation of motor 102 then; Drive 121 motions of first drive link through turbine and worm mechanism 103, turbine and worm mechanism 103 adopts the turbine and worm transmission design with auto-lock function, effectively reduces motor load; Improve working life, second drive link 122 drives drive plate 112 rotations, is that signal source is sent instruction to automatically controlled final controlling element 10 according to the required nozzle angle of control unit of engine; It is the signal source drive transmission part that the ECU 101 of automatically controlled final controlling element 10 adopts current angle and the difference of intending the angle that turns to, thereby realizes mouth ring blade 9 adjustable angle, has realized the rotation of control nozzle blade 9; Change the airflow area and the flow outlet angle of waste gas, when low engine speed, reduce the nozzle ring discharge area; Make the waste gas flow velocity improve, supercharger speed rises, and air demand strengthens; When high engine speeds; The reverse change reduces supercharger speed, reduces air demand.
Owing to adopted the automatically controlled variable geometry turbocharger of technique scheme, be fixed in the rib 13 that turbine cover 7 in the turbine case 1 is provided with the steering flow direction, airflow direction that can direct exhaust; Reduce windage loss; The circumference side of the turbine 5 in turbine case 1 is provided with air-inlet cavity 8, impels turbine 5 rotations, and 5 of air-inlet cavity 8 and turbines are provided with plurality of nozzles ring blade 9 that is uniformly distributed along the circumference around turbine 5 and the controlling device 11 of controlling nozzle blade 9 angle of swing; Controlling device 11 is connected on the automatically controlled final controlling element 10 that places on the pressurized machine support through linkage mechanism 12; Pass through automatically controlled final controlling element 10 during use, according to the electronic signal regulating and controlling device 11 of motor feedback, and then the angle of swing of change nozzle blade 9; Thereby the control exit area of nozzle reaches the purpose of controlling pressurized machine flow and rotating speed.This invention is simple in structure, has advantages such as range of flow is wide, flow control accurate, low speed response property is good, and supercharging is inexcessive.
More than show and described basic principle of the present invention, major character and advantage of the present invention.
The technician of the industry should understand; The present invention is not restricted to the described embodiments; That describes in the foregoing description and the specification just explains principle of the present invention; Under the prerequisite that does not break away from spirit and scope of the invention, the present invention also has various changes and modifications, and these variations and improvement all fall in the scope of the invention that requires protection.The present invention requires protection domain to be defined by appending claims and equivalent thereof.
All are from design of the present invention, and the structure conversion of having done without creative work all drops within the protection domain of the present invention.
Claims (5)
1. automatically controlled variable geometry turbocharger; Comprise the turbine case, intermediate and the compressor casing that link together; Be rotatablely equipped with turbine shaft in the said intermediate, an end of said turbine shaft is fixed with turbine, and said turbine is arranged in the said turbine case; The other end of said turbine shaft is fixed with compressor impeller; Said compressor impeller is arranged in the said compressor casing, it is characterized in that: said turbine case internal fixation is equipped with the turbine cover, forms the air-inlet cavity that impels said turbine rotation between said turbine case and the said turbine cover; Be installed with several nozzle blades between said air-inlet cavity and the said turbine, be provided with the controlling device that is used to adjust said nozzle blade angle between said intermediate and the turbine cover.
2. automatically controlled variable geometry turbocharger according to claim 1; It is characterized in that: said controlling device comprises mounting disc, is coaxially installed with drive plate in the said mounting disc, and said nozzle blade is installed in the said mounting disc; On the said drive plate crank is installed; The other end of said crank connects said nozzle blade, and said drive plate connects the automatically controlled final controlling element that is used to drive said drive plate through linkage mechanism, and said automatically controlled final controlling element is installed on the said compressor casing.
3. automatically controlled variable geometry turbocharger according to claim 2; It is characterized in that: said linkage mechanism comprises first drive link and second drive link; Said first drive link and second drive link are hinged; Said first drive link connects said automatically controlled final controlling element, and said second drive link connects said drive plate.
4. automatically controlled variable geometry turbocharger according to claim 3; It is characterized in that: said automatically controlled final controlling element comprises the ECU of motor and the said motor of control; Motor and ECU are installed in the final controlling element housing, and said motor drives said first drive link through turbine and worm mechanism.
5. automatically controlled variable geometry turbocharger according to claim 1 is characterized in that: said turbine puts the rib that is fixed with the steering flow direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012100159339A CN102536439A (en) | 2012-01-18 | 2012-01-18 | Electrically controlled variable geometrical turbocharger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012100159339A CN102536439A (en) | 2012-01-18 | 2012-01-18 | Electrically controlled variable geometrical turbocharger |
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| Publication Number | Publication Date |
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| CN102536439A true CN102536439A (en) | 2012-07-04 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN2012100159339A Pending CN102536439A (en) | 2012-01-18 | 2012-01-18 | Electrically controlled variable geometrical turbocharger |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103485905A (en) * | 2013-06-29 | 2014-01-01 | 哈尔滨安龙迪环保科技有限公司 | Intelligent, quick and accurate electric control system for turbo-charging adjustment |
| CN114017393A (en) * | 2021-11-25 | 2022-02-08 | 重庆江增船舶重工有限公司 | Electrically-controlled adjustable blade diffuser device of turbocharger and control method thereof |
| CN115789703A (en) * | 2022-12-02 | 2023-03-14 | 苏州达储能源科技有限公司 | Device capable of adjusting jet flow angle to control thermoacoustic vibration and NOx emission |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| JPH11343857A (en) * | 1998-06-01 | 1999-12-14 | Toyota Motor Corp | Actuator for turbocharger |
| CN2763536Y (en) * | 2005-01-18 | 2006-03-08 | 潍坊富源增压器有限公司 | Variable cross-section pressure booster |
| CN2864100Y (en) * | 2005-10-21 | 2007-01-31 | 中国燃气涡轮研究院 | Actuating mechanism for control of turbine booster nozzle ring |
| CN101255814A (en) * | 2007-02-28 | 2008-09-03 | 三菱重工业株式会社 | Mounting structure for variable nozzle mechanism |
| US20110123316A1 (en) * | 2008-07-25 | 2011-05-26 | Roberts Tom J | Variable geometry turbine |
| CN202417696U (en) * | 2012-01-18 | 2012-09-05 | 潍坊富源增压器有限公司 | Electric control variable geometry turbocharger |
-
2012
- 2012-01-18 CN CN2012100159339A patent/CN102536439A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH11343857A (en) * | 1998-06-01 | 1999-12-14 | Toyota Motor Corp | Actuator for turbocharger |
| CN2763536Y (en) * | 2005-01-18 | 2006-03-08 | 潍坊富源增压器有限公司 | Variable cross-section pressure booster |
| CN2864100Y (en) * | 2005-10-21 | 2007-01-31 | 中国燃气涡轮研究院 | Actuating mechanism for control of turbine booster nozzle ring |
| CN101255814A (en) * | 2007-02-28 | 2008-09-03 | 三菱重工业株式会社 | Mounting structure for variable nozzle mechanism |
| US20110123316A1 (en) * | 2008-07-25 | 2011-05-26 | Roberts Tom J | Variable geometry turbine |
| CN202417696U (en) * | 2012-01-18 | 2012-09-05 | 潍坊富源增压器有限公司 | Electric control variable geometry turbocharger |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103485905A (en) * | 2013-06-29 | 2014-01-01 | 哈尔滨安龙迪环保科技有限公司 | Intelligent, quick and accurate electric control system for turbo-charging adjustment |
| CN114017393A (en) * | 2021-11-25 | 2022-02-08 | 重庆江增船舶重工有限公司 | Electrically-controlled adjustable blade diffuser device of turbocharger and control method thereof |
| CN114017393B (en) * | 2021-11-25 | 2024-02-09 | 重庆江增船舶重工有限公司 | Electric control adjustable vane diffuser device of turbocharger and control method thereof |
| CN115789703A (en) * | 2022-12-02 | 2023-03-14 | 苏州达储能源科技有限公司 | Device capable of adjusting jet flow angle to control thermoacoustic vibration and NOx emission |
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Application publication date: 20120704 |