CN201884075U - Plate-driven nozzle ring component with variable cross section - Google Patents
Plate-driven nozzle ring component with variable cross section Download PDFInfo
- Publication number
- CN201884075U CN201884075U CN201020698394XU CN201020698394U CN201884075U CN 201884075 U CN201884075 U CN 201884075U CN 201020698394X U CN201020698394X U CN 201020698394XU CN 201020698394 U CN201020698394 U CN 201020698394U CN 201884075 U CN201884075 U CN 201884075U
- Authority
- CN
- China
- Prior art keywords
- driving
- drive plate
- shift fork
- blade
- weldment
- 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
Links
- 238000003466 welding Methods 0.000 claims abstract description 7
- 238000012856 packing Methods 0.000 claims description 12
- 239000007787 solid Substances 0.000 claims description 3
- 230000033001 locomotion Effects 0.000 abstract description 5
- 230000009471 action Effects 0.000 abstract description 3
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 230000001052 transient effect Effects 0.000 description 1
Images
Classifications
-
- 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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- Supercharger (AREA)
Abstract
本实用新型公开了一种高温下高速运动时可靠性更高、运动阻力更小、叶片动作一致性更好的盘方驱动型可变截面喷嘴环组件。它由后盖1、叶片2、定距螺钉3、安装盘4、拨叉5、驱动方6、垫圈7、从动销钉8、驱动盘9、主动销钉11、主动方12和主动垫圈13组成，其中：叶片2装在安装盘4中，与拨叉5焊固组成喷嘴环焊件10；驱动方6、垫圈7通过从动销钉8串联后焊在驱动盘9上，主动方12、主动垫圈13通过主动销钉11串联焊在驱动盘9上，焊接后组成驱动盘焊件14；驱动盘焊件14直接套在安装盘4上；驱动方6放在拨叉5中，两者为滑动配合；后盖1通过定距螺钉3固定在安装盘4上。工作时，控制系统通过驱动盘焊件之主动方12拨动驱动盘焊件14，驱动盘焊件14上的驱动方6与拨叉5间为滑动配合，因此驱动盘焊件14旋转时，就会通过驱动方6带动拨叉5旋转，拨叉5带动叶片1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地工作。
The utility model discloses a disc drive type variable section nozzle ring assembly with higher reliability, smaller movement resistance and better blade action consistency when moving at high temperature and at high speed. It consists of rear cover 1, blade 2, distance screw 3, mounting plate 4, shift fork 5, driving side 6, washer 7, driven pin 8, driving plate 9, driving pin 11, driving side 12 and driving washer 13 , wherein: the blade 2 is installed in the mounting plate 4, and welded with the shift fork 5 to form a nozzle ring weldment 10; the driving side 6 and the washer 7 are welded on the driving plate 9 after being connected in series through the driven pin 8, and the driving side 12, the driving The washer 13 is welded in series on the drive plate 9 through the active pin 11, and forms the drive plate weldment 14 after welding; the drive plate weldment 14 is directly set on the mounting plate 4; the driver 6 is placed in the shift fork 5, and the two are sliding Cooperate; the back cover 1 is fixed on the mounting plate 4 by the distance screw 3 . During work, the control system moves the drive plate weldment 14 through the active side 12 of the drive plate weldment, and the driving side 6 on the drive plate weldment 14 is in sliding fit with the shift fork 5, so when the drive plate weldment 14 rotates, The driving side 6 will drive the shift fork 5 to rotate, and the shift fork 5 will drive the blade 1 to rotate, thereby changing the angle of the blade and adjusting the airflow section, so that the engine can work at a higher level in each power section with the support of the supercharger.
Description
Technical field
The utility model relates to a kind of auto parts and components, is applied to engine supercharger, the driving variable-area nozzle ring member in especially a kind of dish side
Background technique
Turbosupercharging is one of developing direction of world's internal-combustion engine technology, is the main approach that current internal-combustion engine is strengthened, and turbocharging technology can increase substantially engine output, and energy saving reduces engine exhaust and pollutes.And the variable-area nozzle ring member is the critical component in the current advanced variable geometry turbocharger, the blade angle that before is used for engine supercharger nozzle ring assembly is fixed, blade is non-adjustable, pressurized machine can only make motor in the interval efficient operation of some power, it is adjustable that my company takes the lead in that at home the nozzle ring modular construction is improved to blade angle, thereby blade and shift fork soldering member change blade angle by the drive plate driven rotary, regulate flow area, make the motor can both more efficient ground work (number of patent application: 200610163404.8) under the support of pressurized machine in each power section.But the nozzle ring assembly type of belt drive at the initial stage of improvement is conventional driving, drive plate was relaxed with connecting comparatively of inter-module, walk or hidden danger such as blade skids off, blade incoordinate movement under the high temperature, and the energy loss of airflow strikes on blade is bigger, and efficient is not high enough.
Summary of the invention
At the deficiency of above-mentioned technology, reliability is higher when the utility model proposes under a kind of high temperature high-speed motion, resistance to motion is littler, the better driving variable-area nozzle ring member in the side of coiling of blade action consistency.
The technological scheme that the technical problem that the utility model solves is taked is: it is made up of bonnet, blade, distance screws, mounting disc, shift fork, driving side, packing ring, driven pin, drive plate, active pin, masters and active packing ring, wherein: blade is contained in the mounting disc, forms the nozzle ring weldment with the shift fork solid welding; Driving side, packing ring are welded on the drive plate after connecting by driven pin, and masters, active packing ring are welded on the drive plate after connecting by the active pin, welding back composition drive plate weldment; The drive plate weldment directly is enclosed within the mounting disc, can freely rotate; Driving side is placed in the shift fork, and both are for being slidingly matched; Bonnet is fixed in the mounting disc by distance screws.
The working principle of variable geometry turbocharger is: realize and the optimum Match of motor under each rotating speed by the flow area that changes turbine.During the running of engine low rotation speed, swivel nozzle ring blade is regulated the turbine inlet sectional area, secondary speed rises, and boost pressure increases, boost pressure when having guaranteed the slow-speed of revolution and air inflow, improve air fuel ratio, made full combustion of fuel, prevented the generation of over-emitting black exhaust problem; During the high rotation speed operation of motor, the opposite spin nozzle blade, it is long-pending to increase nozzle ring cross-sectional, and secondary speed descends, and prevents the pressurized machine hypervelocity.When motor quickened, swivel nozzle ring blade was long-pending to reduce nozzle ring cross-sectional, improves supercharger speed rapidly, thereby has improved the transient response of pressurized machine.Nozzle blade in the nozzle ring assembly can be according to the working condition requirement of motor, accept the angle of swing of instruction (or according to boost pressure) adjusting vane of electronic engine management system, keep best combustion gas Flow area, make turbine be in high efficient area work all the time, thereby guarantee the working conditions change of the timely responding engine of pressurized machine, improve the mapping of motor, guarantee the technical-economic index and the emission performance of motor.
The utility model has the advantages that: resistance to motion is littler, the compacter blade action consistency of transmission is better, and the assembly high-temperature reliability is higher, has reduced the relative friction forces between drive plate and shift fork, required driving is littler, helps nozzle ring assembly stable operation and improves speed of response.
Description of drawings
Fig. 1 is the utility model sectional structure schematic representation
Fig. 2 is the plan view of Fig. 1
Among the figure 1, bonnet 2, blade 3, distance screws 4, mounting disc 5, shift fork 6, driving side, 7, packing ring 8, driven pin 9, drive plate 10, nozzle ring weldment 11, initiatively pin 12, masters 13, initiatively packing ring 14, drive plate weldment
Embodiment
In Fig. 1 and Fig. 2: blade 2 is contained in the mounting disc 4, forms nozzle ring weldment 10 with shift fork 5 solid weldings; Driving side 6, packing ring 7 are welded on the drive plate 9 after connecting by driven pin 8, and masters 12, active packing ring 13 are welded on the drive plate 9 after connecting by active pin 11, welding back composition drive plate weldment 14; Drive plate weldment 14 directly is enclosed within the mounting disc 4, can freely rotate; Driving side 6 is placed in the shift fork 5, and both are for being slidingly matched, and bonnet 1 is fixed in the mounting disc 4 by distance screws 3, and so far, bonnet 1, mounting disc 4 and blade 2 have been formed the variable cross section runner.During work, control system is stirred drive plate weldment 14 by the masters 12 of drive plate weldment, 5 of driving side 6 on the drive plate weldment 14 and shift forks are for being slidingly matched, when therefore drive plate weldment 14 rotates, will drive shift fork 5 rotations by driving side 6, shift fork 5 drives blade 1 rotation, thereby changes blade angle, adjusting flow area, and motor can both be worked than the highland in each power section under the support of pressurized machine.
Claims (2)
1. driving variable-area nozzle ring member in dish side, comprise bonnet (1), blade (2), distance screws (3), mounting disc (4), shift fork (5), driving side (6), packing ring (7), driven pin (8), drive plate (9), active pin (11), masters (12) and active packing ring (13), it is characterized in that: blade (2) is contained in the mounting disc (4), forms nozzle ring weldment (10) with shift fork (5) solid welding; Driving side (6), packing ring (7) are welded on the drive plate (9) after connecting by driven pin (8), and masters (12), active packing ring (13) are gone up composition drive plate weldment (14) jointly by the series welding of active pin (11) at drive plate (9); Drive plate weldment (14) directly is enclosed within the mounting disc (4); Driving side (6) is placed in the shift fork (5), and both are for being slidingly matched; Bonnet (1) is fixed in the mounting disc (4).
2. the driving variable-area nozzle ring member in dish side according to claim 1 is characterized in that: bonnet (1) is fixed in the mounting disc (4) by distance screws (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201020698394XU CN201884075U (en) | 2010-12-19 | 2010-12-19 | Plate-driven nozzle ring component with variable cross section |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201020698394XU CN201884075U (en) | 2010-12-19 | 2010-12-19 | Plate-driven nozzle ring component with variable cross section |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201884075U true CN201884075U (en) | 2011-06-29 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201020698394XU Expired - Lifetime CN201884075U (en) | 2010-12-19 | 2010-12-19 | Plate-driven nozzle ring component with variable cross section |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201884075U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN106437870A (en) * | 2016-08-31 | 2017-02-22 | 中车大连机车研究所有限公司 | Adjustable nozzle device of axial flow turbocharger |
| CN107905850A (en) * | 2017-11-02 | 2018-04-13 | 江西省萍乡市三善机电有限公司 | A kind of nozzle ring for turbocharger |
| 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 |
-
2010
- 2010-12-19 CN CN201020698394XU patent/CN201884075U/en not_active Expired - Lifetime
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN106437870A (en) * | 2016-08-31 | 2017-02-22 | 中车大连机车研究所有限公司 | Adjustable nozzle device of axial flow turbocharger |
| CN106437870B (en) * | 2016-08-31 | 2018-09-11 | 中车大连机车研究所有限公司 | Axial flow turbine booster adjustable nozzle assembly |
| CN107905850A (en) * | 2017-11-02 | 2018-04-13 | 江西省萍乡市三善机电有限公司 | A kind of nozzle ring for turbocharger |
| 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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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP03 | Change of name, title or address |
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. |
|
| CX01 | Expiry of patent term |
Granted publication date: 20110629 |
|
| CX01 | Expiry of patent term |