EP2209969A2 - Supercharger device - Google Patents
Supercharger deviceInfo
- Publication number
- EP2209969A2 EP2209969A2 EP08851470A EP08851470A EP2209969A2 EP 2209969 A2 EP2209969 A2 EP 2209969A2 EP 08851470 A EP08851470 A EP 08851470A EP 08851470 A EP08851470 A EP 08851470A EP 2209969 A2 EP2209969 A2 EP 2209969A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- bearing
- ring
- dowel pin
- roller
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/12—Control of the pumps
- F02B37/24—Control of the pumps by using pumps or turbines with adjustable guide vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/50—Building or constructing in particular ways
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
Definitions
- the present invention relates to a charging device, in particular an exhaust gas turbocharger for a motor vehicle.
- the invention also relates to a combustion engine equipped with such a charging device for a motor vehicle.
- Exhaust gas turbochargers are usually used to increase the performance of piston engines, in which they increase an air and fuel flow rate per stroke.
- the exhaust gas turbocharger driven by the exhaust gas flow of the piston engine compresses the air supplied to the combustion chamber, whereby it may be advantageous to decouple the compressed air flow supplied to the combustion chamber from the exhaust gas flow due to different engine operating conditions, thus improving in particular an efficiency, a response or an operating range of the exhaust gas turbocharger can be.
- Such an intervention for controlling the exhaust-gas turbocharger can be achieved, for example, by a variable geometry of the nozzle channels leading to the turbine wheel.
- an exhaust gas turbocharger with a variable turbine geometry is known, which is realized via a blade bearing ring with rotatably mounted thereon guide vanes, wherein the guide vanes together via a coaxial with the blade bearing ring and with respect to this ro tierbar mounted adjusting ring are adjustable.
- the adjusting ring overlapping roller bearings can be stored exclusively in the blade bearing ring or additionally in a housing part, which indeed improves the storage, the installation, that is, the assembly, but much more difficult.
- the present invention addresses the problem of providing a generic charging device an improved embodiment, which is characterized in particular by an improved storage of an adjusting ring.
- the invention is based on the general idea of supporting an adjusting ring coupled to the guide vanes of a vane device via sliding or roller bearings, these sliding or roller bearings being provided on a respective locating pin which penetrates a vane bearing ring carrying the vanes and whose distance from a housing or defined to an arranged in this insert / cover disk element.
- the adjusting ring is there arranged at coaxial with the blade bearing ring and mounted on the mentioned roller or slide bearing on this. About a rotation of the adjusting ring with respect to the blade bearing ring, the setting of the bearing blades mounted on the blade bearing ring is effected.
- the storage of the adjusting can on the one hand simplifies and on the other hand, the variety of parts of the charging device according to the invention can be reduced because the roller or plain bearings now no longer need to be mounted separately from the dowel pins on the vane ring, but can be set via the dowel pins on the vane ring.
- the dowel pins thus fulfill two tasks simultaneously, namely on the one hand to define an axial distance between the blade bearing ring and a housing or arranged in this insert / cover disk element and on the other hand to act as a carrier for the sliding or roller bearings.
- the charging device can be made structurally simpler, which helps to keep maintenance and repair costs low and at the same time to reduce the production costs for the charging device according to the invention.
- the supported by the dowel pins roller or plain bearings also ensure a particularly smooth-running storage of the adjusting ring and thus for a particularly high storage quality.
- the high bearing quality is also responsible for the high positioning accuracy of the vane. lent, so that the charging device according to the invention can be adapted particularly precisely to the respective operating situation.
- a roller bearing with a rotatably mounted bearing roller is provided on each dowel pin.
- a rotatably mounted bearing roller can also be easily and therefore produced inexpensively and also ensures a particularly smooth mounting of the adjusting ring.
- the adjusting ring can be guided via an annular groove, which is embedded in the respective bearing roller on the circumferential side and into which the adjusting ring engages.
- At least one dowel pin on its end bearing the roller bearing on a collar which forms an axial stop for the bearing roller is conceivable, in particular, for example, clamping pins or locknuts.
- At least one dowel pin expediently has a first radial step, via which it is supported on the vane bearing ring, wherein an axial distance between the first radial level and the collar of the dowel pin is greater than an axial extent of the roller bearing or the bearing roller, so that it is arranged with play between the blade bearing ring and the collar of the dowel pin.
- the first radial stage By means of the first radial stage according to the invention, it is possible to predetermine an axial distance or an exact position of the dowel pin to the blade bearing ring, the axial distance between the blade bearing ring and the collar of the dowel pin still remaining for the bearing roller being greater than the axial longitudinal extent of the bearing Bearing roller, so that it can always be stored smoothly and without jamming over the dowel pin on the blade bearing ring. Another measure to secure the jam-free storage of the bearing roller is therefore not required, the first radial stage manufacturing technology is easy to manufacture and thus does not burden the charger with additional, for example, separately manufactured spacers.
- FIGS. 1 to 9 each show a loading device with a roller or slide bearing arranged on a dowel pin according to the invention for supporting an adjusting ring on the blade bearing ring.
- a charging device 1 which is only partially shown, which is designed, for example, as an exhaust-gas turbocharger for a motor vehicle, has a vane device 2 with which a variable turbine and / or compressor geometry can be realized.
- the vane device 2 comprises at least one vane bearing ring 3 with guide vanes 4 rotatably mounted thereon / and an adjusting ring 5 arranged coaxially with the vane ring 3, via which the vanes 4 are jointly adjustable.
- the guide vanes 4 are rotatably mounted on the blade bearing ring 3 by means of blade pins 6, wherein the blade pins 6 pass through the blade bearing ring 3 axially and are connected to the guide blade 4 at one end and to a blade lever 7 at one end , which each carries a radially outwardly directed lever head 8 and thus engages in a corresponding, not shown recess on the adjusting ring 5.
- a rotational movement of the adjusting ring 5 with respect to the blade bearing ring 3 thus causes a uniform rotational movement of all vanes 4 about the blade pin. 6
- the invention provides that a bearing of the adjusting 5 on the blade bearing ring 3 via sliding or roller bearings, each arranged on a, the blade bearing ring 3 penetrating dowel pin 9 are.
- the dowel pin 9 has the task of defining an axial spacing of the blade bearing ring 3 with respect to a housing or with an insert part / cover disk element 10 arranged in the latter. 1, there is a radial gap between the dowel pin 9 and the blade bearing ring 3, whereby an at least certain radial and axial displaceability of the blade bearing ring 3 with respect to the housing 10 is given.
- This mobility makes it possible to compensate for strains and / or tolerances better and at least reduces the risk of jamming of the guide vanes. 4
- the roller bearing has a rotatably mounted bearing roller 11 which is arranged in the axial direction on the one hand adjacent to the blade bearing ring 3 and on the other hand to an axial stop 12, for example a nut.
- the distance between the blade bearing ring 3 of a on the other hand, in the embodiment according to FIG. 1, two radial stages, namely a second radial stage 13 and a third radial stage 14 are delimited.
- the dowel pin 9 is supported on the insert part / cover disk element 10, while it is supported on the blade bearing ring 3 via the third radial step 14.
- Such radial stages 13, 14 can be produced particularly simply, for example by a turning process, and thus do not require a spacer sleeve 15 to be provided in this area, as proposed for example in FIGS. 5, 6, 8 and 9.
- a further, namely a fourth radial step 16 may be provided, against which the axial stop 12 rests in the assembled state.
- the bearing roller 11 is shown in FIG. 1 mounted smoothly on the dowel pin 9, wherein the predetermined by the radial stages 14 and 16 axial distance between the axial stop 12 and the blade bearing ring 3 is greater than the axial longitudinal extent of the bearing roller 11, so that this can be stored without jamming in any case.
- the dowel pin 9 may also have a collar 17 at its end bearing the bearing roller 11, as shown for example in FIGS. 6 and 9.
- This collar 17 forms another embodiment for an axial stop 12.
- Another possibility for an axial stop 12 is a bearing sleeve 18 having a collar, as shown for example in accordance with FIG. 2.
- the bearing sleeve 18 is between the dowel pin 9 and the associated roller bearing, that is, the bearing roller 11, arranged, wherein the bearing sleeve 18 has a greater axial extent than the bearing roller 11 so that they play with between the blade bearing ring 3 and the collar of the bearing sleeve 18 is arranged.
- the bearing rollers 11 shown in FIGS. 1 to 7 and 9 may also be formed as sliding bearings, so that they are not rotatably mounted with respect to the dowel pin 9, but the adjusting 5 mounted in a circumferential groove 19 of the bearing roller 11 designed as a sliding bearing, in particular is guided.
- the dowel pin 9 is formed without radial stages, which is why in this case for reliable definition of the axial distance between the blade bearing ring 3 on the one hand and the insert / cover plate member 10 on the other hand, the dowel pin 9 both with the insert / cover plate member 10 as well firmly connected to the blade bearing ring 3, in particular is pressed.
- the bearing roller 11 may be formed as a sliding bearing. Looking at the embodiment of FIG.
- the dowel pin 9 has a first radial step 20, via which it is supported on the blade bearing ring 3 and wherein an axial distance between the first radial step 20 and the collar 17 of the dowel pin 9 is greater as the axial extent of the bearing roller 11, so that it can be arranged with play between the blade bearing ring 3 and the collar 17 of the dowel pin 9. Also in this case, a jam-free storage of the bearing roller 11 is given.
- an attachment of the dowel pin 9 on the insert / cover disk element 10 or on the housing by means of rivets, screws or welding is provided.
- Figs. 1-4 and 7 of the dowel pin 9 is shown in not riveted state.
- Figs. 5 and 8 and 9 the Pass pin 9 are also screwed into the insert / cover plate member 10.
- a bearing head 21 with a circumferential groove 19 is provided on an adjusting ring 5 facing the end of the dowel pin 9, in which the adjusting ring 5 is slidably guided.
- at least three bearing rollers 11 or three bearing heads 21 are provided with a lying between two bearing rollers 11 / bearing heads 21 angle range of 120 °.
- four or more bearing rollers 11 are provided.
- the charging device 1 makes it possible to realize a particularly simple and highly functional mounting of the adjusting ring 5 on the blade bearing ring 3, since the dowel pins 9 which define an axial spacing between the blade bearing ring 3 and the insert part / cover disk element 10 also act as supports for the adjusting ring 5 stock bearing rollers 11 and bearing heads 21 act. This also achieves a reduction in the variety of parts, which can also reduce storage and logistics costs.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200710056154 DE102007056154A1 (en) | 2007-11-21 | 2007-11-21 | loader |
PCT/EP2008/065453 WO2009065763A2 (en) | 2007-11-21 | 2008-11-13 | Supercharger device |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2209969A2 true EP2209969A2 (en) | 2010-07-28 |
EP2209969B1 EP2209969B1 (en) | 2016-06-29 |
Family
ID=40576897
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08851470.8A Not-in-force EP2209969B1 (en) | 2007-11-21 | 2008-11-13 | Supercharger device |
Country Status (4)
Country | Link |
---|---|
US (1) | US8845279B2 (en) |
EP (1) | EP2209969B1 (en) |
DE (1) | DE102007056154A1 (en) |
WO (1) | WO2009065763A2 (en) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008000776B4 (en) * | 2008-01-21 | 2022-04-14 | BMTS Technology GmbH & Co. KG | Turbine with variable turbine geometry, in particular for an exhaust gas turbocharger, and exhaust gas turbocharger |
DE102008005658A1 (en) | 2008-01-23 | 2009-07-30 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | loader |
DE102008014678B4 (en) | 2008-03-18 | 2014-08-14 | Continental Automotive Gmbh | Turbocharger with a variable turbine geometry VTG |
DE102009009129B4 (en) | 2009-02-17 | 2022-11-03 | BMTS Technology GmbH & Co. KG | Turbocharger with variable turbine geometry |
DE102009032452A1 (en) * | 2009-07-09 | 2011-01-13 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Loading device i.e. exhaust gas turbocharger, for motor vehicle, has rotatably supported guide vanes, and adjusting ring e.g. translationally supported adjusting slider, for adjusting guide vanes orthogonal to axis of device |
DE102009052982A1 (en) * | 2009-10-31 | 2011-05-05 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Variable turbine and / or compressor geometry |
US8668443B2 (en) * | 2010-01-08 | 2014-03-11 | Honeywell International Inc. | Variable-vane assembly having unison ring guided radially by rollers and fixed members, and restrained axially by one or more fixed axial stops |
DE102010004622B8 (en) * | 2010-01-14 | 2014-04-17 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Variable turbine and / or compressor geometry |
DE102011083990A1 (en) | 2010-10-08 | 2012-07-05 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Variable turbine- and/or compressor geometry for charging device i.e. exhaust gas turbocharger, has pin cylindrically formed and fixed at blade bearing ring via press fit, and axial fixation unit for guide rollers provided at pin |
DE102010042181A1 (en) | 2010-10-08 | 2012-04-12 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Variable turbine and / or compressor geometry |
JP5934786B2 (en) * | 2011-05-10 | 2016-06-15 | ボーグワーナー インコーポレーテッド | Turbocharger with variable turbine shape |
US20150110608A1 (en) * | 2012-04-03 | 2015-04-23 | Borgwarner Inc. | Retention system and method for vane ring assembly |
US9651053B2 (en) | 2014-01-24 | 2017-05-16 | Pratt & Whitney Canada Corp. | Bleed valve |
US10087774B2 (en) * | 2014-09-29 | 2018-10-02 | Honeywell International Inc. | Turbocharger variable-vane cartridge with nozzle ring and pipe secured by two-piece self-centering spacers |
DE102015209813A1 (en) * | 2015-05-28 | 2016-12-01 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Variable turbine or compressor geometry for an exhaust gas turbocharger |
DE102016207698A1 (en) * | 2016-05-04 | 2017-11-09 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | loader |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6145313A (en) | 1997-03-03 | 2000-11-14 | Allied Signal Inc. | Turbocharger incorporating an integral pump for exhaust gas recirculation |
US5947681A (en) | 1997-03-17 | 1999-09-07 | Alliedsignal Inc. | Pressure balanced dual axle variable nozzle turbocharger |
DE10262006B4 (en) | 2002-03-05 | 2005-09-22 | Borgwarner Turbo Systems Gmbh | Turbocharger for vehicles with improved suspension for the actuating mechanism of the variable nozzles |
US6679057B2 (en) | 2002-03-05 | 2004-01-20 | Honeywell-International Inc. | Variable geometry turbocharger |
DE10213897A1 (en) | 2002-03-28 | 2003-10-09 | Daimler Chrysler Ag | Variable turbocharger |
JP4008404B2 (en) * | 2002-10-18 | 2007-11-14 | 三菱重工業株式会社 | Variable displacement exhaust turbocharger |
DE10337491A1 (en) | 2003-08-14 | 2005-03-17 | Volkswagen Ag | Exhaust gas turbocharger for IC engines esp. for motor vehicles has flow channel component fastened by bolts, with one bolt passing through turbine guide blade to form pivot axis |
DE10337495B4 (en) | 2003-08-14 | 2016-09-22 | Volkswagen Ag | Exhaust gas turbocharger for an internal combustion engine |
DE102004023209A1 (en) | 2004-05-11 | 2005-12-08 | Volkswagen Ag | Exhaust gas turbocharger with variable turbine geometry for internal combustion engine has at least one adjusting ring guiding element formed with cut away section so that bearing surface protrudes radially beyond guide element |
DE102004023279A1 (en) | 2004-05-11 | 2005-12-01 | Volkswagen Ag | Exhaust gas turbocharger for internal combustion engine, has turbine casings with two wall sections, in which one section is designed and arranged such that low-pass area is extended over entire length of section of flow channel unit |
DE102004037082A1 (en) | 2004-07-30 | 2006-03-23 | Volkswagen Ag | Exhaust gas turbocharger for internal combustion engine of especially motor vehicle has first slide surface formed on bearing housing and axially guides adjustment ring on side facing away from guide vane carrier |
DE102004057864A1 (en) | 2004-11-30 | 2006-06-01 | Borgwarner Inc.(N.D.Ges.D.Staates Delaware), Auburn Hills | Exhaust gas turbocharger, distributor for an exhaust gas turbocharger and blade lever for a distributor |
DE102005019938A1 (en) | 2005-04-29 | 2006-11-09 | Daimlerchrysler Ag | Exhaust gas turbocharger for an internal combustion engine |
DE102006048514B3 (en) | 2005-12-01 | 2007-05-10 | Mtu Friedrichshafen Gmbh | Guidance device for VTG-exhaust gas turbocharger, has fixing element on side, which is turned away from blade lever, is designed as stopper for following spring element |
DE102006007347A1 (en) | 2006-02-17 | 2007-08-30 | Daimlerchrysler Ag | Compressor for an internal combustion engine |
DE102008014678B4 (en) | 2008-03-18 | 2014-08-14 | Continental Automotive Gmbh | Turbocharger with a variable turbine geometry VTG |
DE102008020932B4 (en) | 2008-04-25 | 2010-09-23 | Continental Automotive Gmbh | Turbocharger with a variable turbine geometry device |
-
2007
- 2007-11-21 DE DE200710056154 patent/DE102007056154A1/en not_active Withdrawn
-
2008
- 2008-11-13 US US12/744,143 patent/US8845279B2/en not_active Expired - Fee Related
- 2008-11-13 WO PCT/EP2008/065453 patent/WO2009065763A2/en active Application Filing
- 2008-11-13 EP EP08851470.8A patent/EP2209969B1/en not_active Not-in-force
Non-Patent Citations (1)
Title |
---|
See references of WO2009065763A3 * |
Also Published As
Publication number | Publication date |
---|---|
WO2009065763A2 (en) | 2009-05-28 |
DE102007056154A1 (en) | 2009-05-28 |
EP2209969B1 (en) | 2016-06-29 |
WO2009065763A3 (en) | 2010-01-14 |
US8845279B2 (en) | 2014-09-30 |
US20100316489A1 (en) | 2010-12-16 |
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