CN107905850B - A kind of nozzle ring for turbocharger - Google Patents

A kind of nozzle ring for turbocharger Download PDF

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Publication number
CN107905850B
CN107905850B CN201711062333.7A CN201711062333A CN107905850B CN 107905850 B CN107905850 B CN 107905850B CN 201711062333 A CN201711062333 A CN 201711062333A CN 107905850 B CN107905850 B CN 107905850B
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CN
China
Prior art keywords
disc
mounting disc
shifting fork
shift fork
blade
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.)
Active
Application number
CN201711062333.7A
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Chinese (zh)
Other versions
CN107905850A (en
Inventor
欧阳鹏志
潘保良
黎书珍
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.)
Pingxiang Sunshine Machinery & Electronic Co Ltd
Original Assignee
Pingxiang Sunshine Machinery & Electronic 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.)
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Publication date
Application filed by Pingxiang Sunshine Machinery & Electronic Co Ltd filed Critical Pingxiang Sunshine Machinery & Electronic Co Ltd
Priority to CN201711062333.7A priority Critical patent/CN107905850B/en
Publication of CN107905850A publication Critical patent/CN107905850A/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/24Control of the pumps by using pumps or turbines with adjustable guide vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers
    • 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

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)

Abstract

The invention discloses a kind of nozzle rings for turbocharger, it includes liner plate, mounting disc and shifting fork disc, it is arranged at intervals with spacing axis between the liner plate and mounting disc and is arranged at intervals with blade, shifting fork disc is sleeved in mounting disc outer circle and can make rotation with one heart around mounting disc, shifting fork disc is movably connected by pin shaft interval with one end of the connection board, the other end of connecting plate is movably connected by pin shaft and shift fork one end, the shift fork other end is fixedly linked with sharf one end, and the sharf other end passes through mounting disc and blade is fixedly linked and is fixed on liner plate.The present invention provides a kind of shifting disc rotation radial positionings directly to carry out radial positioning with mounting disc outer circle, it does not need to open up cylindrical groove on shifting disc with shift fork one end to cooperate yet, but come shift fork in the form of riveting plate, its structure is more compact, it processes more simple and convenient, machining accuracy is higher, the more consistent nozzle ring of blade synchronization.

Description

A kind of nozzle ring for turbocharger
Technical field
The present invention relates to turbocharger, more particularly, to a kind of nozzle ring in turbocharger.
Background technique
It is well known that turbocharger is pressurized for air-intake of combustion engine, the product of working efficiency of internal combustion engine is promoted, it is The turbo blade of exhaust end on exhaust pipe is installed on by the exhaust-driven turbocharger that internal combustion engine is discharged, then is driven on coaxial The air end of booster blade rotating inlet of the turbocharger for being installed on intake lines of combustion engines be pressurized, mention admission pressure It rises, improving engine conditions to promote blade of the power of internal combustion engine wherein in nozzle ring capable of changing cross sections is by certain angle Rotation changes exhaust cross-sectional sizes, to adjust turbocharger exhaust pressure, controls turbo charger speed, and then control The components of boost pressure since nozzle ring work is under about 600 DEG C ~ 1200 DEG C of high temperature and high pressure environment, thus require spray Mouth ring has high mechanical performance and machining accuracy.
There is also have following problems at work for existing turbocharger nozzle ring capable of changing cross sections: shifting fork disc, which drives, to be dialled Fork, shift fork drive blade oscillating, are fixed at peace by arc groove thereon and with guide wheel pin interval when shifting fork disc rotates The mutually embedding of guide wheel in sabot is slidably matched to realize the radial positioning of shifting fork disc rotation, first is that due to guide wheel pin installation error and The mismachining tolerance and shifting fork disc of arc groove work after a certain period of time, the wearing clearance of every group of arc groove and guide wheel cooperation Increase, the circular runout of shifting fork disc rotation increases, and the blade rotation angular error for causing shifting fork disc that shift fork is driven to swing increases, leaf The initial time of piece rotation and the rate of angular turn are inconsistent, and the synchronism for causing blade to rotate reduces;It is shift fork one end again It is fixedly linked with blade, and the shift fork other end is built-in in the cylindrical groove on shifting fork disc, when shifting fork disc rotates, due to cylindricality Groove and shift fork other end cooperation contact gap are less uniform, work after a certain period of time, the swing of shift fork will faster or slower, make It cannot be rotated synchronously at blade.It is uneven that the presence of both problems will cause air inflow in the unit time, to influence to start The working performance of machine.
Summary of the invention
For above-mentioned the problems of nozzle ring in the prior art, it is radial fixed that the present invention provides a kind of rotations of shifting fork disc Position does not need the guide wheel phase scarf conjunction for opening up arc groove on it with being fixed in mounting disc, but directly makes shifting fork disc and peace The cooperation of sabot outer circle carries out radial positioning, does not also need to open up cylindrical groove on shifting fork disc with shift fork one end to cooperate, but Come shift fork in the form of riveting plate, structure is more compact, and processing is more simple and convenient, and machining accuracy is higher, leaf The more consistent nozzle ring of piece synchronism.
The technical problem to be solved in the present invention is adopted the technical scheme that: the nozzle ring packet for turbocharger Liner plate, mounting disc and shifting fork disc are included, spacing axis is arranged at intervals between the liner plate and mounting disc and is arranged at intervals with blade, institute It states shifting fork disc to be fitted in mounting disc outer circle and rotation with one heart can be made around mounting disc, the shifting fork disc passes through pin shaft I and connecting plate One end is movably connected, and the other end of connecting plate is movably connected by pin shaft II and shift fork one end, the shift fork other end and sharf one End is fixedly linked, and the sharf other end passes through mounting disc and blade is fixedly linked and is fixed on liner plate.
The course of work of the invention is: additionaling power, which acts on shifting fork disc, rotates shifting fork disc around mounting disc, shifting fork disc All connecting plate synchronous huntings are driven by pin shaft, connecting plate swings by pin shaft and drives what is be connected with one end of the connection board to own Shift fork synchronous hunting, shift fork swing by sharf and blade synchronization are driven to swing, and realize that air inlet synchronizes together by blade oscillating Air inlet is measured, the synchronous same amount air inlet of air inlet in different time is realized by the variation of shifting fork disc rotational angle, to reach raising The purpose of working efficiency of internal combustion engine.
Nozzle ring of the present invention in turbocharger has the following characteristics that compared with existing nozzle ring
1, shifting fork disc rotation radial positioning of the present invention does not need to open up arc groove on it and in mounting disc Cooperation is mutually moved with the guide wheel that guide wheel pin is fixed, but uses and the shifting fork disc of original plate is designed to axle sleeve in T shape, i.e., will Originally the T-shaped shifting fork disc (as shown in Figure 4) of unitary tape flange sleeve is made in the shifting fork disc of plate, thus increase shifting fork disc with The axial distance of mounting disc increases be engaged length and the area of shifting fork disc and mounting disc outer round surface, makes shifting fork disc with most Small―gap suture rotates the technical measures one for carrying out radial positioning around mounting disc, has both eliminated the parts such as guide pin and guide wheel, and be not required to If arc groove simplifies processing and assembly technology, processing cost is reduced, and improves the radial essence that shifting fork disc swings Degree, shifting fork disc location structure is compact simple, positions more acurrate.
2, the present invention does not need to open up cylindrical groove and shift fork one end on shifting fork disc to cooperate, but pin shaft is used to rivet Form one end of the connection board is connected with shift fork, the other end be connected with shifting fork disc comes shift fork rotation, thus drive and shift fork The technical measures two for the blade rotation being fixedly linked, not only simplify shift fork processing and assembly technology, shift fork one end do not need to process At the spheroid form matched with cylindrical groove, keep shift fork shape simpler, reduce costs, shifting fork structure is compact simple, passes Move more reliable stabilization.
3, blade rotation consistency and synchronism are more preferable, and more preferably, reliability and wearability are higher for transmission effect.
4, shifting fork disc, shift fork, between connecting plate be not in catching phenomenon, mutually arrive transmitting flexible movements, harmony is high, saves Power.
5, that the processing is simple is convenient for the nozzle ring of the present invention for turbocharger, and using reliable, durability is strong, can mention High working efficiency of internal combustion engine.
Shifting fork disc of the present invention is mounted below shift fork, is directly riveted with shift fork by pin shaft and connecting plate, on the blade Sharf stretch out both ends of the blade, one end is riveted with mounting disc and shift fork is passed through, and the other end is fixedly linked with liner plate, and the present invention creates New feature is the kind of drive that traditional shifting fork disc rotational positioning mode and shift fork are changed by two technical measures, not only So that its structure is more compact simple, and solves and asked in the prior art due to assembly mismachining tolerance and using abrasion bring Topic keeps blade opening and closing consistency and synchronism more accurate.
Detailed description of the invention
Fig. 1 is the schematic view of the front view of part cutting of the present invention,
Fig. 2 is the B of Fig. 1 to structural schematic diagram,
Fig. 3 is that Fig. 2 dismantles the partial structural diagram after pin shaft and shift fork release,
Fig. 4 is the A-A broken section structural schematic diagram of Fig. 3.
1, shifting fork disc 2, pin shaft I 3, sharf 4, blade 5, mounting disc 6, connecting plate 7, pin in the figure Axis II 8, liner plate 9, shift fork 10, axial limiting set 11, spacing axis.
Specific embodiment
In Fig. 1, Fig. 2, Fig. 3 and Fig. 4, a kind of nozzle ring for turbocharger includes liner plate 8, mounting disc 5 and dials Disk 1 is pitched, five spacing axis 11 are arranged at intervals between the liner plate and mounting disc, if being arranged at intervals between liner plate and mounting disc Blade is 15 pieces in dry block blade 4(the present embodiment), the blade is sharp pears shape shape, and the shifting fork disc is fitted in outside mounting disc On circle, shifting fork disc can make rotation (swinging) with one heart around mounting disc under external force, using by the shifting fork disc of original plate It is designed to axle sleeve in T shape, i.e., the T-shaped shifting fork disc of unitary tape flange sleeve is made (such as in the shifting fork disc of original plate Shown in Fig. 4), to increase the distance that axially engages of shifting fork disc and mounting disc, increase connecing for shifting fork disc and mounting disc outer round surface Length of fit and area are touched, keeps shifting fork disc rotational stability high (circular runout very little), makes shifting fork disc with minimum clearance around peace Sabot rotation carries out the technical measures one of radial positioning, and the shifting fork disc is movably connected by pin shaft I 2 and 6 one end of connecting plate, dials It pitches disk and pin shaft I 2 rivets, rivet layer height 1.2-1.4 millimeters, the other end of connecting plate is living by pin shaft II 7 and 9 one end of shift fork Dynamic to be connected, connecting plate and pin shaft II 7 rivet, and the shift fork other end is fixedly linked with the riveting of 3 one end of sharf, and the sharf is another End activity passes through mounting disc and blade is fixedly linked and rivets and is fixed on liner plate 8.Gap between blade and liner plate is 0.13- 0.18 millimeter, axial limiting set 10, the shift fork and connecting plate are provided on the pin shaft I 2 between the shifting fork disc and connecting plate Between pin shaft II 7 on be provided with axial limiting set 10, to prevent connecting plate from moving axially.

Claims (1)

1. a kind of nozzle ring for turbocharger, it includes liner plate (8), mounting disc (5) and shifting fork disc (1), the liner plate It is arranged at intervals with spacing axis (11) between mounting disc and is arranged at intervals with blade (4), the shifting fork disc is fitted in outside mounting disc It can make on circle and around mounting disc to rotate with one heart, the shifting fork disc is movably connected by pin shaft I (2) and connecting plate (6) one end, is connected The other end of plate is movably connected by pin shaft II (7) and shift fork (9) one end, the shift fork other end and sharf (3) one end stationary phase Even, the sharf other end passes through mounting disc and blade and is fixedly linked and is fixed on liner plate (8), the shift fork (9) and even Axial limiting set (10) are provided in pin shaft II (7) between fishplate bar, it is characterized in that: the shifting fork disc and pin shaft I (2) rivet, Connecting plate and pin shaft II (7) rivet, and the riveting height is 1.2-1.4 millimeters.
CN201711062333.7A 2017-11-02 2017-11-02 A kind of nozzle ring for turbocharger Active CN107905850B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711062333.7A CN107905850B (en) 2017-11-02 2017-11-02 A kind of nozzle ring for turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711062333.7A CN107905850B (en) 2017-11-02 2017-11-02 A kind of nozzle ring for turbocharger

Publications (2)

Publication Number Publication Date
CN107905850A CN107905850A (en) 2018-04-13
CN107905850B true CN107905850B (en) 2019-09-20

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Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3411822B2 (en) * 1998-06-25 2003-06-03 株式会社アキタファインブランキング Variable nozzle drive for variable capacity turbine
CN201884075U (en) * 2010-12-19 2011-06-29 萍乡市德博科技发展有限公司 Plate-driven nozzle ring component with variable cross section
CN202810969U (en) * 2012-09-20 2013-03-20 江西省萍乡市三善机电有限公司 Square shift block driving type nozzle ring with variable cross section
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
CN204386673U (en) * 2014-12-30 2015-06-10 江西汇宏科技发展有限公司 A kind of turbosupercharger nozzle ring
CN206655719U (en) * 2017-04-20 2017-11-21 江西凯格新材料科技有限公司 A kind of chain type nozzle ring

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