CN201474729U - Compact Disc Drive Variable Area Nozzle Ring Assemblies - Google Patents
Compact Disc Drive Variable Area Nozzle Ring Assemblies Download PDFInfo
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- CN201474729U CN201474729U CN2009201584601U CN200920158460U CN201474729U CN 201474729 U CN201474729 U CN 201474729U CN 2009201584601 U CN2009201584601 U CN 2009201584601U CN 200920158460 U CN200920158460 U CN 200920158460U CN 201474729 U CN201474729 U CN 201474729U
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- 230000000712 assembly Effects 0.000 title 1
- 238000000429 assembly Methods 0.000 title 1
- 239000007787 solid Substances 0.000 claims 1
- 238000003466 welding Methods 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 2
- 230000001052 transient effect Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
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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
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Abstract
本实用新型公开了一种传动更紧凑,叶片动作一致性更好,组件的高温可靠性更高的紧凑盘形驱动可变截面喷嘴环组件,它包括叶片4、安装盘5、驱动盘6、拨叉7、套环9、驱动片10和驱动柱11,其中,叶片4装在安装盘5中,与拨叉7焊固共同组成喷嘴环焊件13;驱动盘6直接套在安装盘5上,驱动柱11插入驱动片10中,套环9焊接在驱动柱11上。工作时套环9和驱动柱11被拨动,从而带动驱动片10和驱动盘6,驱动盘6与拨叉7间为滑动配合,因此驱动盘6旋转时,带动拨叉7旋转,拨叉7带动叶片4旋转,从而改变叶片角度、调节气流截面,使发动机在增压器的支持下在各个功率段都能较高效地工作。
The utility model discloses a compact disk-shaped driving variable section nozzle ring assembly with more compact transmission, better consistency of blade action and higher high-temperature reliability of the assembly, which includes blades 4, mounting disks 5, driving disks 6, Shift fork 7, collar 9, drive piece 10 and drive column 11, wherein blade 4 is installed in mounting plate 5, and welded together with shift fork 7 to form nozzle ring weldment 13; drive plate 6 is directly set on mounting plate 5 Above, the driving column 11 is inserted into the driving piece 10, and the collar 9 is welded on the driving column 11. During work, the collar 9 and the driving column 11 are moved, thereby driving the driving piece 10 and the driving plate 6, and the driving plate 6 and the shift fork 7 are in a sliding fit, so when the driving plate 6 rotates, it drives the shift fork 7 to rotate, and the shift fork 7 rotates. 7 drives the blades 4 to rotate, thereby changing the angle of the blades and adjusting the cross-section of the airflow, so that the engine can work more efficiently at each power stage with the support of the supercharger.
Description
技术领域technical field
本实用新型涉及一种汽车零部件,应用于发动机增压器,尤其是一种紧凑盘形驱动可变截面喷嘴环组件。The utility model relates to an automobile part, which is applied to an engine supercharger, in particular to a compact disk-shaped driving variable section nozzle ring assembly.
背景技术Background technique
涡轮增压是世界内燃机技术的发展方向之一,涡轮增压技术能大幅度提高发动机输出功率,节约能源,减少发动机废气污染。而可变截面喷嘴环组件是当今先进的可变几何涡轮增压器中的关键部件。之前用于发动机增压器喷嘴环组件的叶片角度固定、叶片不可调,增压器只能使发动机在某一个功率区间高效工作。我公司在国内率先将喷嘴环组件结构改进为叶片角度可调,叶片与拨叉焊合件靠驱动盘带动旋转从而改变叶片角度、调节气流截面,使发动机在增压器的支持下在各个功率段都能较高效地工作(专利申请号:200610163404.8)。但改进初期的喷嘴环组件结构为:叶片插在安装盘上,拨叉焊在叶片末端,然后拨叉套在驱动盘中,驱动盘上再套一个主动拨叉,靠外力带动主动拨叉从而带动驱动盘,再通过驱动盘驱动拨叉,拨叉带动叶片转动,从而改变燃气通道的截面。驱动盘与组件间的联接较为松懈、高温下有走位或叶片滑出、叶片不协调动作等缺点。Turbocharging is one of the development directions of internal combustion engine technology in the world. Turbocharging technology can greatly increase engine output power, save energy, and reduce engine exhaust pollution. The variable section nozzle ring assembly is a key component in today's advanced variable geometry turbocharger. Previously, the angle of the blades used in the engine supercharger nozzle ring assembly was fixed and the blades were not adjustable. The supercharger can only make the engine work efficiently in a certain power range. Our company is the first in China to improve the structure of the nozzle ring assembly so that the angle of the blade can be adjusted. All segments can work more efficiently (patent application number: 200610163404.8). However, the structure of the nozzle ring assembly in the early stage of improvement is: the blade is inserted on the mounting plate, the shift fork is welded to the end of the blade, and then the shift fork is set in the driving disc, and an active shift fork is placed on the driving disc, and the active shift fork is driven by external force to achieve Drive the drive plate, and then drive the shift fork through the drive plate, and the shift fork drives the blade to rotate, thereby changing the cross section of the gas channel. The connection between the drive plate and the components is relatively loose, and there are disadvantages such as displacement or blade slipping out under high temperature, and uncoordinated action of the blades.
发明内容Contents of the invention
针对上述技术的不足,本实用新型提出了一种传动更紧凑,叶片动作一致性更好,组件的高温可靠性更高的紧凑盘形驱动可变截面喷嘴环组件。Aiming at the deficiencies of the above-mentioned technologies, the utility model proposes a compact disc-driven variable-section nozzle ring assembly with more compact transmission, better blade action consistency, and higher high-temperature reliability of the assembly.
本实用新型解决的技术问题采取的技术方案是:所述喷嘴环组件包括定距螺栓、螺母、后盖、叶片、安装盘、驱动盘、拨叉、垫片、套环、驱动片、驱动柱和螺钉,其中,叶片装在安装盘中,与拨叉焊固共同组成喷嘴环焊件;驱动盘直接套在安装盘上,当叶片与拨叉焊固后,驱动盘的位置在焊件中得到固定;后盖通过定距螺栓和螺母固定在安装盘上,至此,后盖、安装盘和叶片组成了可变截面流道;垫片和驱动片通过螺钉固定在驱动盘上;驱动柱插入驱动片中,套环焊接在驱动柱上。The technical solution to the technical problem solved by the utility model is: the nozzle ring assembly includes a distance bolt, a nut, a back cover, a blade, a mounting plate, a drive plate, a shift fork, a gasket, a collar, a drive plate, and a drive column. and screws, wherein the blades are installed in the mounting plate, and welded together with the shift fork to form a nozzle ring weldment; the drive plate is directly set on the mounting plate, when the blade and the shift fork are welded, the position of the drive plate is in the weldment fixed; the rear cover is fixed on the mounting plate by distance bolts and nuts, so far, the rear cover, mounting plate and blades form a variable cross-section flow channel; the gasket and the driving plate are fixed on the driving plate by screws; the driving column is inserted into the In the drive piece, the collar is welded to the drive post.
可变几何涡轮增压器的工作原理是:通过改变涡轮的流通截面来实现与发动机在各个转速下的最佳匹配。发动机低转速运转时,旋转喷嘴环叶片,调节涡轮进口截面积,涡轮转速上升,增压压力增加,保证了低转速时的增压压力和进气量,提高了空燃比,使燃料充分燃烧,防止了冒黑烟问题的产生;发动机高转速运转时,反方向旋转喷嘴环叶片,增大喷嘴环截面积,涡轮转速下降,防止增压器超速。发动机加速时,旋转喷嘴环叶片以减小喷嘴环截面积,迅速提高增压器转速,从而改善了增压器的瞬态响应性。喷嘴环组件中的喷嘴环叶片能够根据发动机的工况要求,接受发动机电子控制系统的指令(或根据增压压力)调节叶片的旋转角度,保持最佳的燃气流道面积,使涡轮始终处于高效率区工作,从而保证增压器及时响应发动机的工况变化、提高发动机的瞬态性能,确保发动机的技术经济指标与排放性能。The working principle of the variable geometry turbocharger is to achieve the best match with the engine at each speed by changing the flow section of the turbine. When the engine is running at low speed, the nozzle ring blades are rotated to adjust the cross-sectional area of the turbine inlet, the turbine speed rises, and the boost pressure increases, ensuring the boost pressure and intake air volume at low speed, increasing the air-fuel ratio, and fully burning the fuel. The problem of black smoke is prevented; when the engine is running at high speed, the blades of the nozzle ring are rotated in the opposite direction to increase the cross-sectional area of the nozzle ring, and the speed of the turbine is reduced to prevent the supercharger from overspeeding. When the engine accelerates, the blades of the nozzle ring are rotated to reduce the cross-sectional area of the nozzle ring and rapidly increase the speed of the supercharger, thereby improving the transient response of the supercharger. The nozzle ring blades in the nozzle ring assembly can adjust the rotation angle of the blades according to the requirements of the engine's working conditions, and accept the instructions of the engine electronic control system (or according to the boost pressure), so as to maintain the best gas flow path area and keep the turbine at a high level all the time. Work in the efficiency zone, so as to ensure that the turbocharger responds to the change of the engine's working conditions in a timely manner, improves the transient performance of the engine, and ensures the technical and economic indicators and emission performance of the engine.
附图说明Description of drawings
图1是本实用新型剖视结构示意图Fig. 1 is the utility model sectional structure schematic diagram
图2是图1的俯视图Figure 2 is a top view of Figure 1
图中1、定距螺栓2、螺母3、后盖4、叶片5、安装盘6、驱动盘7、拨叉8、垫片9、套环10、驱动片11、驱动柱12、螺钉13、喷嘴环焊件In the figure 1,
具体实施方式Detailed ways
在图1和图2中:叶片4装在安装盘5中,与拨叉7焊固共同组成喷嘴环焊件13;驱动盘6直接套在安装盘5上,当叶片4与拨叉7焊固后,驱动盘6的位置在焊件中得到固定;后盖3通过定距螺栓1和螺母2固定在安装盘5上,至此,后盖3、安装盘5和叶片4组成了可变截面流道;垫片8和驱动片10通过螺钉12固定在驱动盘6上;驱动柱11插入驱动片10中,套环9焊接在驱动柱11上。工作时,发动机控制系统通过一个主动拨叉同时拨动套环9和驱动柱11,从而带动驱动片10和驱动盘6,驱动盘6与拨叉7间为滑动配合,因此驱动盘6旋转时,就会带动拨叉7旋转,拨叉7带动叶片4旋转,从而改变叶片4的角度、调节气流截面,使发动机在增压器的支持下在各个功率段都能较高效地工作。In Fig. 1 and Fig. 2: the blade 4 is installed in the
Claims (3)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201584601U CN201474729U (en) | 2009-05-26 | 2009-05-26 | Compact Disc Drive Variable Area Nozzle Ring Assemblies |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201584601U CN201474729U (en) | 2009-05-26 | 2009-05-26 | Compact Disc Drive Variable Area Nozzle Ring Assemblies |
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| CN201474729U true CN201474729U (en) | 2010-05-19 |
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| CN2009201584601U Expired - Fee Related CN201474729U (en) | 2009-05-26 | 2009-05-26 | Compact Disc Drive Variable Area Nozzle Ring Assemblies |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104100301A (en) * | 2013-04-02 | 2014-10-15 | 成都盛航动力设备有限公司 | Multi-stage differential pressure radial flow turbine capable of adjusting nozzle ring opening |
| CN104295325A (en) * | 2014-09-16 | 2015-01-21 | 萍乡市德博科技发展有限公司 | Variable section nozzle ring for turbocharger |
| CN104819014A (en) * | 2015-05-06 | 2015-08-05 | 重庆江增船舶重工有限公司 | Adjustable nozzle ring structure for ship mixed-flow turbo-superchager |
| WO2019200950A1 (en) * | 2018-04-19 | 2019-10-24 | 萍乡德博科技股份有限公司 | Section-variable nozzle ring for supercharger |
| US11092032B2 (en) | 2018-08-28 | 2021-08-17 | Pratt & Whitney Canada Corp. | Variable vane actuating system |
| US11092167B2 (en) | 2018-08-28 | 2021-08-17 | Pratt & Whitney Canada Corp. | Variable vane actuating system |
| CN114251134A (en) * | 2021-12-07 | 2022-03-29 | 萍乡德博科技股份有限公司 | Turbocharging variable-section nozzle ring of gasoline engine |
| US11371380B2 (en) | 2020-12-01 | 2022-06-28 | Pratt & Whitney Canada Corp. | Variable guide vane assembly and vane arms therefor |
-
2009
- 2009-05-26 CN CN2009201584601U patent/CN201474729U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104100301A (en) * | 2013-04-02 | 2014-10-15 | 成都盛航动力设备有限公司 | Multi-stage differential pressure radial flow turbine capable of adjusting nozzle ring opening |
| CN104100301B (en) * | 2013-04-02 | 2015-12-02 | 成都盛航动力设备有限公司 | The multistage differential pressure radial-flow turbine of nozzle ring aperture can be regulated |
| CN104295325A (en) * | 2014-09-16 | 2015-01-21 | 萍乡市德博科技发展有限公司 | Variable section nozzle ring for turbocharger |
| CN104295325B (en) * | 2014-09-16 | 2016-02-03 | 萍乡德博科技股份有限公司 | A kind of turbosupercharger nozzle ring capable of changing cross sections |
| CN104819014A (en) * | 2015-05-06 | 2015-08-05 | 重庆江增船舶重工有限公司 | Adjustable nozzle ring structure for ship mixed-flow turbo-superchager |
| WO2019200950A1 (en) * | 2018-04-19 | 2019-10-24 | 萍乡德博科技股份有限公司 | Section-variable nozzle ring for supercharger |
| US11092032B2 (en) | 2018-08-28 | 2021-08-17 | Pratt & Whitney Canada Corp. | Variable vane actuating system |
| US11092167B2 (en) | 2018-08-28 | 2021-08-17 | Pratt & Whitney Canada Corp. | Variable vane actuating system |
| US11371380B2 (en) | 2020-12-01 | 2022-06-28 | Pratt & Whitney Canada Corp. | Variable guide vane assembly and vane arms therefor |
| CN114251134A (en) * | 2021-12-07 | 2022-03-29 | 萍乡德博科技股份有限公司 | Turbocharging variable-section nozzle ring of gasoline engine |
| CN114251134B (en) * | 2021-12-07 | 2024-01-26 | 萍乡德博科技股份有限公司 | A gasoline engine turbocharger variable section nozzle ring |
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Address after: 337000 North Zone, Pingxiang Development Zone, Jiangxi, China Patentee after: PINGXIANG DEBO TECHNOLOGY DEVELOPMENT CO., LTD. Address before: 337000 No. 6 Zheng He road, North Zone, Pingxiang Economic Development Zone, Jiangxi, China Patentee before: Pingxiang Debo Technology Development Co.,Ltd. |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100519 Termination date: 20170526 |
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| CF01 | Termination of patent right due to non-payment of annual fee |
