EP2553275B1 - Turbocharger casing including valve housing and manufacturing process of such a casing - Google Patents

Turbocharger casing including valve housing and manufacturing process of such a casing Download PDF

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Publication number
EP2553275B1
EP2553275B1 EP11710461.2A EP11710461A EP2553275B1 EP 2553275 B1 EP2553275 B1 EP 2553275B1 EP 11710461 A EP11710461 A EP 11710461A EP 2553275 B1 EP2553275 B1 EP 2553275B1
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EP
European Patent Office
Prior art keywords
valve
housing
passage section
slide element
turbocharger housing
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
EP11710461.2A
Other languages
German (de)
French (fr)
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EP2553275A1 (en
Inventor
Robert Vetter
Alexandre Pfister
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.)
Continental Automotive GmbH
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Continental Automotive GmbH
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Publication date
Application filed by Continental Automotive GmbH filed Critical Continental Automotive GmbH
Publication of EP2553275A1 publication Critical patent/EP2553275A1/en
Application granted granted Critical
Publication of EP2553275B1 publication Critical patent/EP2553275B1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/009Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids by bleeding, by passing or recycling fluid
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • B22D17/20Accessories: Details
    • B22D17/22Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
    • B22D17/24Accessories for locating and holding cores or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • 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
    • F01D17/105Final actuators by passing part of the fluid
    • 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
    • F01D9/026Scrolls for radial machines or engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0207Surge control by bleeding, bypassing or recycling fluids
    • F04D27/0215Arrangements therefor, e.g. bleed or by-pass valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • 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
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/21Manufacture essentially without removing material by casting
    • 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
    • F05D2250/00Geometry
    • F05D2250/30Arrangement of components
    • F05D2250/31Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/312Arrangement of components according to the direction of their main axis or their axis of rotation the axes being parallel to each other

Definitions

  • the invention relates to a turbocharger housing with at least one valve device, for example a compressor housing with a diverter valve. Furthermore, the invention relates to a method for producing such a turbocharger housing.
  • Turbochargers usually have a turbine which is arranged in an exhaust gas flow and is connected via a shaft to a compressor in the intake tract.
  • a turbine wheel and a compressor wheel are arranged on the shaft.
  • the turbine wheel drives the compressor wheel of the compressor.
  • the compressor can increase the pressure in the intake tract of the engine, so that a larger amount of air enters the cylinder during the intake stroke. This has the consequence that more oxygen is available and a correspondingly larger amount of fuel can be burned.
  • turbocharger In order to largely prevent or reduce the falling of the speed of the turbocharger, for example, in an engine thrust operation modern turbocharger have diverter valves. These diverter valves are located on the turbocharger in the compressor housing, which is made of aluminum. The function of the diverter valve is realized via channels between an inlet side and an outlet side and a valve seat, which represents the sealing plane. These overflow channels and also the valve seat usually have complex geometries.
  • a compressor housing of a turbocharger which is a diverter valve or recirculation valve having.
  • the compressor housing in this case has a valve flange to which the recirculation valve can be fastened.
  • the valve flange has a flange surface, in which an inlet opening is arranged, to which a connecting channel connects to the compressor inlet.
  • the valve flange has a valve seat for the closing element of the recirculation valve.
  • a channel axis of the connecting channel is arranged at an angle ⁇ to the valve seat.
  • the flange surface is disposed at an angle ⁇ to a reference surface which is perpendicular to the turbocharger axis and axially bounds the volute of the compressor housing toward the bearing housing side.
  • the compressor housing has the disadvantage that it has a complex shape and the predetermined angle ⁇ , ⁇ are difficult to realize with sufficient accuracy.
  • a compressor which comprises a compressor housing rotatably mounted compressor wheel.
  • the compressor housing is connected to the housing of an external control valve, via which a recirculation path connects the discharge opening of the compressor housing with the inlet opening of the compressor housing to regulate the flow through the compressor wheel.
  • a wastegate device which has a first housing and an external second housing which is bolted to the first housing.
  • a first bypass line and a second bypass line are provided in the first housing.
  • a membrane made of rubber is provided in the second housing, in which a valve disc is integrated. The position of the valve disc may be changed to connect or disconnect the two bypass conduits and the first housing.
  • the invention provides a turbocharger housing having a valve means formed in the turbocharger housing, the valve means having at least a first passage portion and a second passage portion, and wherein the valve means further comprises a valve space formed in the turbocharger housing and a valve seat formed in the turbocharger housing.
  • the first channel section connects a main channel of a suction side in the compressor housing with the valve chamber.
  • the second channel section connects a volute housing a pressure side in the compressor housing with the valve chamber.
  • Essential for the invention is that the two channel sections are formed without undercuts over their entire extent and are arranged parallel to each other with their longitudinal axes.
  • the turbocharger housing has the advantage that it is formed by means of a simply designed and inexpensive slide element with a valve device in the die-cast can.
  • the tool slide element can be designed simply because the valve device has two mutually parallel channel sections, which are formed without undercuts. As a result, the slide element can also very easily be introduced into the diecasting tool in the die casting process and easily removed again from the latter and the turbocharger housing.
  • Fig. 1 is a sectional view of a finished turbocharger housing 10 with at least one valve device 12 according to the invention shown.
  • the turbocharger housing 10 is in the Die casting process produced, for example as aluminum die casting or from another suitable for the die casting material or material combination.
  • a die-casting tool 14 is provided, in which a tool slide element 16 is arranged, as shown by way of example in FIG Fig. 1 is shown to form a valve device 12 in the turbocharger housing 10.
  • the die-cast tool can be formed, for example, in a horizontal or substantially horizontal plane divided into two mold halves 18, 20, as in Fig. 1 is indicated by a dashed line.
  • the die casting tool and its two mold halves are in Fig.
  • a mold half 18 can in this case, for example, the inner channel 22 and the volute casing 24 and the other mold half 20, the outer contour of the turbocharger housing 10, as in Fig. 1 is indicated.
  • the die casting tool 14 may be formed such that the tool slide element 16 is received in a mold half of the die casting tool or in both mold halves 18, 20 of the diecasting tool.
  • Fig. 1 Completely manufactured turbocharger housing 10, the tool slide element 16 is shown partially inserted, with which the valve means 12, here for example a diverter valve, has been formed in the turbocharger housing 10.
  • the valve means 12 here for example a diverter valve
  • the turbocharger housing 10 is designed in the present example as a separate compressor housing which can be fastened, for example, to a bearing housing of the turbocharger.
  • a compressor housing section of a turbocharger housing which is integrally formed, for example, with a bearing housing, may also be formed with a valve device 12 according to the invention (not shown).
  • valve device 12 is formed in the turbocharger housing 10.
  • the tool slide element 16 is designed such that the valve chamber 26, preferably the entire valve chamber, the valve seat 28 and one or more channels 30, 32 of the valve device 12 in the turbocharger housing 10 form or form.
  • a diverter valve is provided as a valve device 12.
  • the corresponding tool slide member 16 has two channel section projections 34, 36, i. a first channel section projection 34 of e.g. is disposed outside and a second channel section projection 36 of the e.g. is arranged inside.
  • the first outer channel section projection 34 forms the outflow or outlet channel 38, which is connected, for example, to an inlet region of the suction side or the intake channel of the compressor.
  • the second inner channel portion projection 36 in turn forms e.g. the inlet or inlet channel 40, which is connected to the input area of the pressure side of the compressor.
  • the two channel section projections 34, 36 of the tool slide element 16 are arranged in such a way to each other, so that the tool slide element 16 can be easily pulled out or removed from the die-cast tool 14 and the turbocharger housing 10 following a die-casting process for forming the turbocharger housing 10.
  • the tool slide element 16 is designed for this purpose without undercuts or has no undercut.
  • the two channel section projections 34, 36 of the tool slide element 16 are arranged in the longitudinal direction parallel to each other, wherein the two channel section projections 34, 36 with their longitudinal axes 42 while parallel and offset from each other or parallel and can be provided with their longitudinal axes 42 in a vertical or vertical plane lying or coaxial with each other, as in the following 3 and 4 is shown.
  • the tool slide member 16 has a valve space portion 44, wherein the valve space portion 44 is formed so as to form the complete valve space 26 or substantially the entire valve space 26 in the turbocharger housing 10.
  • the tool slide element 16 has a valve seat portion 46 for forming the valve seat 28 in the turbocharger housing 10.
  • the valve seat 28 is formed on the tool slide element 16 in the form of a valve seat projection 48, for example, a circumferential projection.
  • the projection 48 for the valve seat 28 may also be formed in the outer first channel portion projection 34 temporarily.
  • the valve seat projection 48 also has no undercut, so that the tool slide member 16 can be easily pulled out of the die casting tool 14 and the finished shaped turbocharger housing 10.
  • Fig. 2 is the sectional view of the finished turbocharger housing 10 according to Fig. 1 shown without the tool slide element.
  • the compressor housing 10 has a diverter valve 12 as a valve device.
  • the two channels 30, 32 of the diverter valve 12 are formed parallel to each other.
  • the inlet channel 40 of the diverter valve 12 is connected to the pressure side or in this case the spiral 24 of the compressor housing 10 and the outlet channel 38 to the inlet regions of the suction side of the compressor.
  • the diverter valve 10 has a valve seat 28 and a valve space 26 which is completely formed by the tool slide element 16.
  • the two channel section projections 34, 36 are arranged parallel to each other and not offset from each other or the longitudinal axes 42 of the two channel section projections 34, 36 are both in a common vertical plane 50th .
  • the two channel section projections 34, 36 but also be arranged in parallel and offset from each other.
  • the longitudinal axes 42 of the two channel section projections 34, 36 are provided in two mutually offset vertical planes 50, 51.
  • the two channel section projections 34, 36 may have an arbitrary cross-sectional shape, as long as the channel section projections 34, 36 do not form or have undercuts.
  • one or both of the channel section projections 34, 36 may have a constant cross section, for example, a cylindrical cross section flattened on one side.
  • one or both of the channel section projections 34, 36 may be longitudinally tapered or have a longitudinally tapered cross section, as in the first outer channel section projection 34 Fig. 3
  • the valve seat projection 48 may be provided, for example, with a flat 52 on one or both sides, depending on the function and intended use.
  • Fig. 4 shows the tool slide element 16 according to Fig. 3 in a side view. The transition between the valve seat projection 48 and the first outer channel section projection 34 is shown.
  • Fig. 5 shows a perspective view of the tool slide element 16 from behind.
  • the valve seat projection 48 and the portion 44 for forming the valve space, and the outer channel section projection 34 can be seen.
  • the formation of the end 54 of the tool slide element 16 as a flat surface is greatly simplified and purely exemplary. Depending on how For example, the connection between the die casting tool and the tool slide element 16 is provided, the tool slide element 16 and its end 54 may be designed accordingly.
  • Fig. 6 shows a perspective view of the tool slide element 16 from the front.
  • the first and second channel portion projection 34, 36 are shown, which are parallel to each other with their longitudinal axes 42 and also not offset from each other or without an offset to each other.
  • the valve seat projection 48 is shown, which merges into the outer channel section projection 34.
  • FIGS. 7 and 8 a sectional perspective view of the compressor housing 10 is shown according to the invention.
  • the tool slide element 16 is shown, with which a diverter valve 12 is formed in the compressor housing 10.
  • the tool slide element 16 is partially pulled out of the diverter valve 12 out.
  • the tool slide element 16 is in this case designed such that in the fully inserted state, the first and second channel section projections 34, 36 of the tool slide element 16, as previously in Fig. 1 is indicated, extend into the spiral or spiral housing 24 and the main channel 22 of the compressor housing 10, which are formed for example by one of the two mold halves of the die-casting tool.
  • Fig. 9 shows the compressor housing 10 and the tool slide element 16 in a sectional view.
  • the diverter valve 12 is shown with its inlet channel 40 and outlet channel 42, the valve seat 28 and the valve chamber 26.
  • imported State fits the tool slide element 16 with its contour exactly in the contour of the diverter valve 12th
  • Fig. 10 the compressor housing 10 and the tool slide element 16 is shown in a perspective sectional view.
  • the valve chamber 26 and the valve seat 28, and the inlet channel 40 and the outlet channel 42 of the diverter valve 12 are shown.
  • the valve seat 28 forms a section of the outlet channel or outer channel section 30.
  • FIG. 11 a perspective view of the compressor housing 10 and the tool slide element 16 is shown.
  • the turbocharger housing 10 or here the compressor housing 10 is produced by die casting.
  • the tool slide element 16 is, for example, made of metal or another suitable solid or resistant material, which preferably allows multiple use of the tool slide element 16.
  • Fig. 12 shows the compressor housing 10 in a perspective view, wherein the compressor housing 10 thereof is shown from the side of the diverter valve 12.
  • the valve chamber 26 and the valve seat 28 of the diverter valve 12 is shown, as well as its outer outlet channel 38 and the inner inlet channel 40.
  • the outer periphery of the valve seat 26 is flattened in the region of the outer channel 28, here the outlet channel, to a part of the Channel 28 to form.
  • the portion of the valve seat 28 which forms part of the channel 28 is suitably adapted with its contour to the channel 28 to allow optimum flow through the channel.
  • the turbocharger housing with valve device described above for example in the form of a compressor housing with a diverter valve, has the advantage that the housing with valve can be easily produced by die-casting.
  • the compressor housing can be produced for example in aluminum die-cast or another suitable die-cast.
  • the entire valve chamber, the valve seat and also the overflow channels of the diverter valve can be represented in a die-cast tool slide element. This allows either a livelihood without any additional mechanical processing, or only a minimal amount of processing, which can affect the sealing and mounting geometry, i. the sealing seat and the mounting holes of the diverter valve, limited.
  • the arrangement and location of the tool slide element in the die casting tool can reduce the number and complexity of moving parts. This manufacturing costs can be reduced because the feasibility of a pressure-castable compressor housing is improved with a diverter valve. Furthermore, the complexity of the tool slide element can be reduced and the tool slide element can be simplified. Another advantage is that the processing of the compressor housing or its diverter valve can be reduced or even allows geometries that require no additional mechanical processing, resulting in a further reduction in manufacturing costs.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Supercharger (AREA)

Description

Die Erfindung betrifft ein Turboladergehäuse mit wenigstens einer Ventileinrichtung, beispielsweise ein Verdichtergehäuse mit einem Schubumluftventil. Des Weiteren betrifft die Erfindung ein Verfahren zur Herstellung eines solchen Turboladergehäuses.The invention relates to a turbocharger housing with at least one valve device, for example a compressor housing with a diverter valve. Furthermore, the invention relates to a method for producing such a turbocharger housing.

Turbolader weisen normalerweise eine Turbine auf, die in einem Abgasstrom angeordnet ist und über eine Welle mit einem Verdichter im Ansaugtrakt verbunden ist. Auf der Welle sind dabei im Allgemeinen ein Turbinenrad und ein Verdichterrad angeordnet. Über den Abgasstrom eines angeschlossenen Motors wird das Turbinenrad der Turbine angetrieben. Das Turbinenrad treibt dabei wiederum das Verdichterrad des Verdichters an. Hierdurch kann der Verdichter den Druck im Ansaugtrakt des Motors erhöhen, so dass während des Ansaugtaktes eine größere Menge Luft in den Zylinder gelangt. Dies hat zur Folge, dass mehr Sauerstoff zur Verfügung steht und eine entsprechend größere Kraftstoffmenge verbrannt werden kann.Turbochargers usually have a turbine which is arranged in an exhaust gas flow and is connected via a shaft to a compressor in the intake tract. In general, a turbine wheel and a compressor wheel are arranged on the shaft. About the exhaust gas flow of a connected engine, the turbine wheel of the turbine is driven. The turbine wheel in turn drives the compressor wheel of the compressor. As a result, the compressor can increase the pressure in the intake tract of the engine, so that a larger amount of air enters the cylinder during the intake stroke. This has the consequence that more oxygen is available and a correspondingly larger amount of fuel can be burned.

Um nun das Abfallen der Drehzahl des Turboladers beispielsweise in einem Motorschubbetrieb weitestgehend zu verhindern bzw. zu verringern besitzen moderne Turbolader Schubumluftventile. Diese Schubumluftventile sitzen am Turbolader im Verdichtergehäuse, welches aus Aluminium gefertigt ist. Die Funktion des Schubumluftventils wird über Kanäle zwischen einer Eintrittsseite und einer Austrittsseite und einem Ventilsitz, welcher die Dichtebene darstellt, realisiert. Diese Überströmkanäle und auch der Ventilsitz weisen üblicherweise komplexe Geometrien auf.In order to largely prevent or reduce the falling of the speed of the turbocharger, for example, in an engine thrust operation modern turbocharger have diverter valves. These diverter valves are located on the turbocharger in the compressor housing, which is made of aluminum. The function of the diverter valve is realized via channels between an inlet side and an outlet side and a valve seat, which represents the sealing plane. These overflow channels and also the valve seat usually have complex geometries.

Aus der WO 2008/055588 ist ein Verdichtergehäuse eines Turboladers bekannt, welches ein Schubumluftventil bzw. Umluftventil aufweist. Das Verdichtergehäuse weist dabei einen Ventilflansch auf, an dem das Umluftventil befestigbar ist. Der Ventilflansch weist dazu eine Flanschfläche auf, in der eine Eintrittsöffnung angeordnet ist, an die sich ein Verbindungskanal zu dem Verdichtereintritt anschließt. Des Weiteren weist der Ventilflansch einen Ventilsitz für das Schließelement des Umluftventils auf. Eine Kanalachse des Verbindungskanals ist dabei in einem Winkel β zu dem Ventilsitz angeordnet. Des Weiteren ist die Flanschfläche in einem Winkel α zu einer Bezugsfläche angeordnet, welche senkrecht zu der Turboladerachse vorgesehen ist und die Spirale des Verdichtergehäuses zur Lagergehäuseseite hin axial begrenzt. Das Verdichtergehäuse hat dabei den Nachteil, dass es eine komplexe Form aufweist und die vorgegebenen Winkel α, β nur schwer mit einer ausreichenden Genauigkeit zu realisieren sind.From the WO 2008/055588 a compressor housing of a turbocharger is known, which is a diverter valve or recirculation valve having. The compressor housing in this case has a valve flange to which the recirculation valve can be fastened. For this purpose, the valve flange has a flange surface, in which an inlet opening is arranged, to which a connecting channel connects to the compressor inlet. Furthermore, the valve flange has a valve seat for the closing element of the recirculation valve. A channel axis of the connecting channel is arranged at an angle β to the valve seat. Furthermore, the flange surface is disposed at an angle α to a reference surface which is perpendicular to the turbocharger axis and axially bounds the volute of the compressor housing toward the bearing housing side. The compressor housing has the disadvantage that it has a complex shape and the predetermined angle α, β are difficult to realize with sufficient accuracy.

Aus der EP 0 468 676 A1 ist ein Verdichter bekannt, der ein in einem Verdichtergehäuse drehbar angeordnetes Verdichterrad aufweist. Das Verdichtergehäuse ist mit dem Gehäuse eines externen Steuerventils verbunden, über welches ein Wiederumlaufweg die Abgabeöffnung des Verdichtergehäuses mit der Eintrittsöffnung des Verdichtergehäuses verbindet, um die Strömung durch das Verdichterrad zu regeln.From the EP 0 468 676 A1 a compressor is known which comprises a compressor housing rotatably mounted compressor wheel. The compressor housing is connected to the housing of an external control valve, via which a recirculation path connects the discharge opening of the compressor housing with the inlet opening of the compressor housing to regulate the flow through the compressor wheel.

Aus der nicht vorveröffentlichten DE 10 2009 012 732 A1 ist ebenfalls ein Verdichtergehäuse bekannt, welches mit einem externen Taktventil verbunden ist.From the not pre-published DE 10 2009 012 732 A1 is also known a compressor housing, which is connected to an external clock valve.

Aus der DE 690 05 357 T2 ist eine Ladedruckregelvorrichtung bekannt, die ein erstes Gehäuse und ein externes zweites Gehäuse aufweist, welches mit dem ersten Gehäuse verschraubt ist. Im ersten Gehäuse sind eine erste Bypassleitung und eine zweite Bypassleitung vorgesehen. Im zweiten Gehäuse ist eine Membran aus Kautschuk vorgesehene, in welche ein Ventilteller integriert ist. Die Position des Ventiltellers kann verändert werden, um die beiden Bypassleitungen und des ersten Gehäuses miteinander zu verbinden oder voneinander zu trennen. Demnach ist es die Aufgabe der vorliegenden Erfindung, ein vereinfacht herzustellendes Turboladergehäuse mit einer Ventileinrichtung und ein Verfahren zum Herstellen eines solchen Turboladergehäuses bereitzustellen.From the DE 690 05 357 T2 For example, a wastegate device is known which has a first housing and an external second housing which is bolted to the first housing. In the first housing, a first bypass line and a second bypass line are provided. In the second housing a membrane made of rubber is provided, in which a valve disc is integrated. The position of the valve disc may be changed to connect or disconnect the two bypass conduits and the first housing. Accordingly, it is the object of the present invention to provide a simplified manufacture turbocharger housing with a valve device and a method for producing such a turbocharger housing.

Diese Aufgabe wird durch ein Turboladergehäuse mit einer Ventileinrichtung mit den Merkmalen des Patentanspruchs 1 und ein Verfahren zur Herstellung eines Turboladergehäuses mit einer Ventileinrichtung mit den Merkmalen des Patentanspruchs 8 gelöst.This object is achieved by a turbocharger housing having a valve device with the features of patent claim 1 and a method for producing a turbocharger housing having a valve device having the features of patent claim 8.

Demgemäß wird erfindungsgemäß ein Turboladergehäuse mit einer im Turboladergehäuse ausgebildeten Ventileinrichtung bereitgestellt, wobei die Ventileinrichtung wenigstens einen ersten Kanalabschnitt und einen zweiten Kanalabschnitt aufweist, und wobei die Ventileinrichtung des Weiteren einen im Turboladergehäuse ausgeformten Ventilraum und einen im Turboladergehäuse ausgeformten Ventilsitz aufweist. Der erste Kanalabschnitt verbindet einen Hauptkanal einer Ansaugseite im Verdichtergehäuse mit dem Ventilraum. Der zweite Kanalabschnitt verbindet ein Spiralgehäuse einer Druckseite im Verdichtergehäuse mit dem Ventilraum. Wesentlich für die Erfindung ist, dass die beiden Kanalabschnitte über ihre gesamte Erstreckung hinterschneidungsfrei ausgebildet und mit ihren Längsachsen zueinander parallel angeordnet sind.Accordingly, the invention provides a turbocharger housing having a valve means formed in the turbocharger housing, the valve means having at least a first passage portion and a second passage portion, and wherein the valve means further comprises a valve space formed in the turbocharger housing and a valve seat formed in the turbocharger housing. The first channel section connects a main channel of a suction side in the compressor housing with the valve chamber. The second channel section connects a volute housing a pressure side in the compressor housing with the valve chamber. Essential for the invention is that the two channel sections are formed without undercuts over their entire extent and are arranged parallel to each other with their longitudinal axes.

Das Turboladergehäuse hat dabei den Vorteil, dass es mittels eines einfach gestalteten und preiswerten Schieberelements mit einer Ventileinrichtung im Druckguss ausgebildet werden kann. Das Werkzeugschieberelement kann einfach gestaltet werden, da die Ventileinrichtung zwei zueinander parallele Kanalabschnitte aufweist, welche hinterschneidungsfrei ausgebildet sind. Dadurch kann das Schieberelement außerdem sehr einfach im Druckgussverfahren in das Druckgusswerkzeug eingeführt und aus diesem und dem Turboladergehäuse wieder leicht entfernt werden.The turbocharger housing has the advantage that it is formed by means of a simply designed and inexpensive slide element with a valve device in the die-cast can. The tool slide element can be designed simply because the valve device has two mutually parallel channel sections, which are formed without undercuts. As a result, the slide element can also very easily be introduced into the diecasting tool in the die casting process and easily removed again from the latter and the turbocharger housing.

Vorteilhafte Ausgestaltungen und Weiterbildungen der Erfindung ergeben sich aus den Unteransprüchen sowie der Beschreibung unter Bezugnahme auf die Zeichnungen.Advantageous embodiments and modifications of the invention will become apparent from the dependent claims and the description with reference to the drawings.

Die Erfindung wird nachfolgend anhand der in den schematischen Figuren der Zeichnungen angegebenen Ausführungsbeispiele näher erläutert. Es zeigen:

Fig. 1
eine Schnittansicht eines Turboladergehäuses mit einer Ventileinrichtung gemäß der Erfindung, wobei zur Ausbildung der Ventileinrichtung in das Turboladergehäuse ein Werkzeugschieberelement teilweise eingeführt ist;
Fig. 2
die Schnittansicht des Turboladergehäuses gemäß Fig. 1, ohne das Werkzeugschieberelement;
Fig. 3
eine Vorderansicht des Werkzeugschieberelement gemäß Fig. 1;
Fig. 4
eine Seitenansicht der Werkzeugschieberelements gemäß Fig. 1 und 3;
Fig. 5
eine Perspektivansicht des Werkzeugschieberelements gemäß Fig. 1, 3 und 4;
Fig. 6
eine weitere Perspektivansicht des Werkzeugschieberelements gemäß Fig. 1, 3, 4 und 5;
Fig. 7
eine perspektivische Schnittansicht des Turboladergehäuses mit der Ventileinrichtung gemäß Fig. 1, wobei das Werkzeugschieberelement teilweise aus dem Turboladergehäuse entfernt ist;
Fig. 8
die perspektivische Schnittansicht des Turboladergehäuses mit der Ventileinrichtung gemäß Fig. 7, aus Sicht der Ventileinrichtung;
Fig. 9
eine Schnittansicht des Turboladergehäuses und des Werkzeugschiebelements, wobei das Werkzeugschieberelement vollständig aus dem Turboladergehäuse entfernt ist;
Fig. 10
eine perspektivische Schnittansicht des Turboladergehäuses und des Werkzeugschieberelements gemäß Fig. 1 , wobei das Werkzeugschieberelement vollständig aus dem Turboladergehäuse entfernt ist und das Turboladergehäuse aus Sicht der Ventileinrichtung gezeigt ist;
Fig. 11
eine weitere Perspektivansicht des Turboladergehäuses und des Werkzeugschieberelements gemäß Fig. 1 , wobei das Werkzeugschieberelement vollständig aus dem Turboladergehäuse entfernt ist; und
Fig. 12
eine andere Perspektivansicht des Turboladergehäuses aus Richtung der Ventileinrichtung.
The invention will be explained in more detail with reference to the exemplary embodiments indicated in the schematic figures of the drawings. Show it:
Fig. 1
a sectional view of a turbocharger housing with a valve device according to the invention, wherein a tool slide element is partially inserted to form the valve means in the turbocharger housing;
Fig. 2
the sectional view of the turbocharger housing according to Fig. 1 without the tool slide element;
Fig. 3
a front view of the tool slide element according to Fig. 1 ;
Fig. 4
a side view of the tool slide element according to Fig. 1 and 3 ;
Fig. 5
a perspective view of the tool slide element according to Fig. 1 . 3 and 4 ;
Fig. 6
a further perspective view of the tool slide element according to Fig. 1 . 3, 4 and 5 ;
Fig. 7
a perspective sectional view of the turbocharger housing with the valve device according to Fig. 1 wherein the tool slide element is partially removed from the turbocharger housing;
Fig. 8
the perspective sectional view of the turbocharger housing with the valve device according to Fig. 7 , from the perspective of the valve device;
Fig. 9
a sectional view of the turbocharger housing and the Werkzeugschiebelements, wherein the tool slide element is completely removed from the turbocharger housing;
Fig. 10
a perspective sectional view of the turbocharger housing and the tool slide element according to Fig. 1 wherein the tool slide element is completely removed from the turbocharger housing and the turbocharger housing is shown from the perspective of the valve device;
Fig. 11
another perspective view of the turbocharger housing and the tool slide element according to Fig. 1 wherein the tool slide element is completely removed from the turbocharger housing; and
Fig. 12
another perspective view of the turbocharger housing from the direction of the valve device.

In allen Figuren sind gleiche bzw. funktionsgleiche Elemente und Vorrichtungen - sofern nichts anderes angegeben ist - mit denselben Bezugszeichen versehen worden.In all figures, identical or functionally identical elements and devices have been provided with the same reference numerals, unless stated otherwise.

In Fig. 1 ist eine Schnittansicht eines fertigen Turboladergehäuses 10 mit wenigstens einer Ventileinrichtung 12 gemäß der Erfindung gezeigt. Das Turboladergehäuse 10 wird dabei im Druckgussverfahren hergestellt, beispielsweise als Aluminiumdruckguss oder aus einem anderen für das Druckgussverfahren geeigneten Material oder Materialkombination. Dazu ist ein Druckgusswerkzeug 14 vorgesehen, in welchem ein Werkzeugschieberelement 16 angeordnet ist, wie es beispielhaft in Fig. 1 gezeigt ist, um eine Ventileinrichtung 12 in dem Turboladergehäuse 10 auszubilden. Dabei kann das Druckgusswerkzeug beispielsweise in einer waagerechten oder im Wesentlichen waagerechten Ebene in zwei Formhälften 18, 20 geteilt ausgebildet sein, wie in Fig. 1 mit einer gestrichelten Linie angedeutet ist. Das Druckgusswerkzeug und seine beiden Formhälften sind in Fig. 1 nur angedeutet und stark vereinfacht und rein schematisch dargestellt. Eine Formhälfte 18 kann hierbei beispielsweise den inneren Kanal 22 und das Spiralgehäuse 24 bilden und die andere Formhälfte 20 die Außenkontur des Turboladergehäuses 10, wie in Fig. 1 angedeutet ist. Dabei kann das Druckgusswerkzeug 14 derart ausgebildet sein, dass das Werkzeugschieberelement 16 in einer Formhälfte des Druckgusswerkzeugs oder in beiden Formhälften 18, 20 des Druckgusswerkzeugs aufgenommen ist.In Fig. 1 is a sectional view of a finished turbocharger housing 10 with at least one valve device 12 according to the invention shown. The turbocharger housing 10 is in the Die casting process produced, for example as aluminum die casting or from another suitable for the die casting material or material combination. For this purpose, a die-casting tool 14 is provided, in which a tool slide element 16 is arranged, as shown by way of example in FIG Fig. 1 is shown to form a valve device 12 in the turbocharger housing 10. In this case, the die-cast tool can be formed, for example, in a horizontal or substantially horizontal plane divided into two mold halves 18, 20, as in Fig. 1 is indicated by a dashed line. The die casting tool and its two mold halves are in Fig. 1 only indicated and greatly simplified and shown purely schematically. A mold half 18 can in this case, for example, the inner channel 22 and the volute casing 24 and the other mold half 20, the outer contour of the turbocharger housing 10, as in Fig. 1 is indicated. In this case, the die casting tool 14 may be formed such that the tool slide element 16 is received in a mold half of the die casting tool or in both mold halves 18, 20 of the diecasting tool.

In dem in Fig. 1 fertig hergestellten Turboladergehäuse 10 ist das Werkzeugschieberelement 16 teilweise eingeführt gezeigt, mit welchem die Ventileinrichtung 12, hier beispielsweise ein Schubumluftventil, in dem Turboladergehäuse 10 ausgebildet worden ist.In the in Fig. 1 Completely manufactured turbocharger housing 10, the tool slide element 16 is shown partially inserted, with which the valve means 12, here for example a diverter valve, has been formed in the turbocharger housing 10.

Das erfindungsgemäße Turboladergehäuse 10 ist in dem vorliegenden Beispiel als ein separates Verdichtergehäuse ausgebildet, welches z.B. an einem Lagergehäuse des Turboladers befestigbar ist. Ebenso kann aber auch ein Verdichtergehäuseabschnitt eines Turboladergehäuses, welches beispielsweise mit einem Lagergehäuse einteilig ausgebildet ist, mit einer Ventileinrichtung 12 gemäß der Erfindung ausgebildet werden (nicht dargestellt).The turbocharger housing 10 according to the invention is designed in the present example as a separate compressor housing which can be fastened, for example, to a bearing housing of the turbocharger. Likewise, however, a compressor housing section of a turbocharger housing, which is integrally formed, for example, with a bearing housing, may also be formed with a valve device 12 according to the invention (not shown).

Wie in dem Beispiel in Fig. 1 gezeigt ist, wird in dem Turboladergehäuse 10 wenigstens eine Ventileinrichtung 12 ausgebildet. Dabei ist das Werkzeugschieberelement 16 derart ausgebildet, um den Ventilraum 26, vorzugsweise den gesamten Ventilraum, den Ventilsitz 28 und einen oder mehrere Kanäle 30, 32 der Ventileinrichtung 12 in dem Turboladergehäuse 10 auszubilden oder auszuformen.As in the example in Fig. 1 is shown, at least one valve device 12 is formed in the turbocharger housing 10. In this case, the tool slide element 16 is designed such that the valve chamber 26, preferably the entire valve chamber, the valve seat 28 and one or more channels 30, 32 of the valve device 12 in the turbocharger housing 10 form or form.

In dem in Fig. 1 und den nachfolgenden Figuren 2 bis 12 gezeigten Beispiel wird als Ventileinrichtung 12 ein Schubumluftventil vorgesehen.In the in Fig. 1 and the following ones FIGS. 2 to 12 As shown, a diverter valve is provided as a valve device 12.

Zur Ausbildung des Schubumluftventils 12 als Ventileinrichtung 12 weist das entsprechende Werkzeugschieberelement 16 zwei Kanalabschnittsvorsprünge 34, 36 auf, d.h. einen ersten Kanalabschnittsvorsprung 34 der z.B. außen angeordnet ist und einen zweiten Kanalabschnittsvorsprung 36 der z.B. innen angeordnet ist. Der erste äußere Kanalabschnittsvorsprung 34 bildet dabei den Ausström- oder Auslasskanal 38, welcher beispielsweise mit einem Eintrittsbereich der Ansaugseite oder des Ansaugkanals des Verdichters verbunden ist. Der zweite innere Kanalabschnittsvorsprung 36 bildet wiederum z.B. den Einström- oder Einlasskanal 40, welcher mit dem Eingangsbereich der Druckseite des Verdichters verbunden ist.To form the diverter valve 12 as a valve means 12, the corresponding tool slide member 16 has two channel section projections 34, 36, i. a first channel section projection 34 of e.g. is disposed outside and a second channel section projection 36 of the e.g. is arranged inside. The first outer channel section projection 34 forms the outflow or outlet channel 38, which is connected, for example, to an inlet region of the suction side or the intake channel of the compressor. The second inner channel portion projection 36 in turn forms e.g. the inlet or inlet channel 40, which is connected to the input area of the pressure side of the compressor.

Die beiden Kanalabschnittsvorsprünge 34, 36 des Werkzeugschieberelements 16 sind dabei derart zueinander angeordnet, so dass das Werkzeugschieberelement 16 im Anschluss an ein Druckgussverfahren zum Ausbilden des Turboladergehäuses 10 leicht aus dem Druckgusswerkzeug 14 und dem Turboladergehäuse 10 wieder herausgezogen oder entnommen werden kann. Das Werkzeugschieberelement 16 ist hierzu ohne Hinterschneidungen ausgebildet bzw. weist keine Hinterschneidung auf. Die beiden Kanalabschnittsvorsprünge 34, 36 des Werkzeugschieberelements 16 sind in Längsrichtung parallel zueinander angeordnet, wobei die beiden Kanalabschnittsvorsprünge 34, 36 mit ihren Längsachsen 42 dabei parallel und zueinander versetzt oder parallel und mit ihren Längsachsen 42 in einer vertikalen bzw. senkrechten Ebene liegend oder koaxial zueinander vorgesehen werden können, wie in nachfolgender Fig. 3 und 4 gezeigt ist.The two channel section projections 34, 36 of the tool slide element 16 are arranged in such a way to each other, so that the tool slide element 16 can be easily pulled out or removed from the die-cast tool 14 and the turbocharger housing 10 following a die-casting process for forming the turbocharger housing 10. The tool slide element 16 is designed for this purpose without undercuts or has no undercut. The two channel section projections 34, 36 of the tool slide element 16 are arranged in the longitudinal direction parallel to each other, wherein the two channel section projections 34, 36 with their longitudinal axes 42 while parallel and offset from each other or parallel and can be provided with their longitudinal axes 42 in a vertical or vertical plane lying or coaxial with each other, as in the following 3 and 4 is shown.

Des Weiteren weist das Werkzeugschieberelement 16 einen Ventilraumabschnitt 44 auf, wobei der Ventilraumabschnitt 44 derart ausgebildet ist, so dass er den vollständigen Ventilraum 26 oder im Wesentlichen den vollständigen Ventilraum 26 in dem Turboladergehäuse 10 ausbildet. Außerdem weist das Werkzeugschieberelement 16 einen Ventilsitzabschnitt 46 auf, zum Ausbilden des Ventilsitzes 28 in dem Turboladergehäuse 10. Der Ventilsitz 28 ist dabei an dem Werkzeugschieberelement 16 in Form eines Ventilsitzvorsprungs 48 ausgebildet, beispielsweise eines umlaufenden Vorsprungs. Der Vorsprung 48 für den Ventilsitz 28 kann dabei außerdem in den äußeren ersten Kanalabschnittsvorsprung 34 übergehend ausgebildet sein. Der Ventilsitzvorsprung 48 weist ebenfalls keine Hinterschneidung auf, so dass das Werkzeugschieberelement 16 leicht aus dem Druckgusswerkzeug 14 und dem fertig geformten Turboladergehäuse 10 herausgezogen werden kann.Furthermore, the tool slide member 16 has a valve space portion 44, wherein the valve space portion 44 is formed so as to form the complete valve space 26 or substantially the entire valve space 26 in the turbocharger housing 10. In addition, the tool slide element 16 has a valve seat portion 46 for forming the valve seat 28 in the turbocharger housing 10. The valve seat 28 is formed on the tool slide element 16 in the form of a valve seat projection 48, for example, a circumferential projection. The projection 48 for the valve seat 28 may also be formed in the outer first channel portion projection 34 temporarily. The valve seat projection 48 also has no undercut, so that the tool slide member 16 can be easily pulled out of the die casting tool 14 and the finished shaped turbocharger housing 10.

In Fig. 2 ist die Schnittansicht des fertigen Turboladergehäuses 10 gemäß Fig. 1 gezeigt, ohne das Werkzeugschieberelement. Wie aus Fig. 2 entnommen werden kann, weist das Verdichtergehäuse 10 ein Schubumluftventil 12 als Ventileinrichtung auf. Die beiden Kanäle 30, 32 des Schubumluftventils 12 sind dabei parallel zueinander ausgebildet. Der Einlasskanal 40 des Schubumluftventils 12 ist dabei mit der Druckseite oder hier der Spirale 24 des Verdichtergehäuses 10 verbunden und der Auslasskanal 38 mit dem Eintrittsbereiche der Ansaugseite des Verdichters. Des Weiteren weist das Schubumluftventil 10 einen Ventilsitz 28 und einen durch das Werkzeugschieberelement 16 vollständig ausgebildeten Ventilraum 26 auf. Die Fig. 3 bis 6 zeigen mehrere Ansichten des Werkzeugschieberelements 16. Wie in der Vorderansicht des Werkzeugschieberelements 16 gezeigt ist, sind die beiden Kanalabschnittsvorsprünge 34, 36 parallel zueinander angeordnet und nicht zueinander versetzt bzw. die Längsachsen 42 der beiden Kanalabschnittsvorsprünge 34, 36 liegen beide in einer gemeinsamen senkrechten Ebene 50. Wie in Fig. 3 mit einer strichpunktierten Linie angedeutet ist, können die beiden Kanalabschnittsvorsprünge 34, 36 aber auch parallel und zueinander versetzt angeordnet sein. In diesem Fall sind die Längsachsen 42 der beiden Kanalabschnittsvorsprünge 34, 36 in jeweils zwei zu einander versetzten senkrechten Ebenen 50, 51 vorgesehen. Die beiden Kanalabschnittsvorsprünge 34, 36 können eine beliebige Querschnittsform aufweisen, sofern die Kanalabschnittsvorsprünge 34, 36 keine Hinterschneidungen bilden oder aufweisen. Ein oder beide Kanalabschnittsvorsprünge 34, 36 können beispielsweise einen konstanten Querschnitt aufweisen, beispielsweise einen an einer Seite abgeflachten zylindrischen Querschnitt. Ebenso können eine oder beide Kanalabschnittsvorsprünge 34, 36 sich in Längsrichtung verjüngen bzw. einen sich in Längsrichtung verjüngenden Querschnitt aufweisen, wie der erste äußere Kanalabschnittsvorsprung 34. In dem in Fig. 3 gezeigten Beispiel kann außerdem der Ventilsitzvorsprung 48 z.B. an einer oder beiden Seiten mit einer Abflachung 52 versehen sein, je nach Funktion und Einsatzzweck.In Fig. 2 is the sectional view of the finished turbocharger housing 10 according to Fig. 1 shown without the tool slide element. How out Fig. 2 can be removed, the compressor housing 10 has a diverter valve 12 as a valve device. The two channels 30, 32 of the diverter valve 12 are formed parallel to each other. The inlet channel 40 of the diverter valve 12 is connected to the pressure side or in this case the spiral 24 of the compressor housing 10 and the outlet channel 38 to the inlet regions of the suction side of the compressor. Furthermore, the diverter valve 10 has a valve seat 28 and a valve space 26 which is completely formed by the tool slide element 16. The Fig. 3 to 6 As shown in the front view of the tool slide element 16, the two channel section projections 34, 36 are arranged parallel to each other and not offset from each other or the longitudinal axes 42 of the two channel section projections 34, 36 are both in a common vertical plane 50th . As in Fig. 3 is indicated by a dot-dash line, the two channel section projections 34, 36 but also be arranged in parallel and offset from each other. In this case, the longitudinal axes 42 of the two channel section projections 34, 36 are provided in two mutually offset vertical planes 50, 51. The two channel section projections 34, 36 may have an arbitrary cross-sectional shape, as long as the channel section projections 34, 36 do not form or have undercuts. For example, one or both of the channel section projections 34, 36 may have a constant cross section, for example, a cylindrical cross section flattened on one side. Likewise, one or both of the channel section projections 34, 36 may be longitudinally tapered or have a longitudinally tapered cross section, as in the first outer channel section projection 34 Fig. 3 In addition, the valve seat projection 48 may be provided, for example, with a flat 52 on one or both sides, depending on the function and intended use.

Fig. 4 zeigt das Werkzeugschieberelement 16 gemäß Fig. 3 in einer Seitenansicht. Dabei ist der Übergang zwischen dem Ventilsitzvorsprung 48 und dem ersten äußeren Kanalabschnittsvorsprung 34 gezeigt. Fig. 4 shows the tool slide element 16 according to Fig. 3 in a side view. The transition between the valve seat projection 48 and the first outer channel section projection 34 is shown.

Fig. 5 zeigt eine Perspektivansicht des Werkzeugschieberelements 16 von hinten. Dabei sind der Ventilsitzvorsprung 48 und der Abschnitt 44 zum Ausbilden des Ventilraums, sowie der äußere Kanalabschnittsvorsprung 34 zu sehen. Das Ausbilden des Endes 54 des Werkzeugschieberelements 16 als ebene Fläche ist stark vereinfacht und rein beispielhaft. Je nachdem wie beispielsweise die Verbindung zwischen dem Druckgusswerkzeug und dem Werkzeugschieberelement 16 vorgesehen ist, kann das Werkzeugschieberelement 16 und sein Ende 54 entsprechend gestaltet sein. Fig. 5 shows a perspective view of the tool slide element 16 from behind. In this case, the valve seat projection 48 and the portion 44 for forming the valve space, and the outer channel section projection 34 can be seen. The formation of the end 54 of the tool slide element 16 as a flat surface is greatly simplified and purely exemplary. Depending on how For example, the connection between the die casting tool and the tool slide element 16 is provided, the tool slide element 16 and its end 54 may be designed accordingly.

Fig. 6 zeigt eine Perspektivansicht des Werkzeugschieberelements 16 von vorne. Dabei sind der erste und zweite Kanalabschnittsvorsprung 34, 36 gezeigt, welche mit ihren Längsachsen 42 zueinander parallel und außerdem nicht zueinander versetzt bzw. ohne einen Versatz zu einander angeordnet sind. Des Weiteren ist der Ventilsitzvorsprung 48 gezeigt, welcher in den äußeren Kanalabschnittsvorsprung 34 übergeht. Fig. 6 shows a perspective view of the tool slide element 16 from the front. In this case, the first and second channel portion projection 34, 36 are shown, which are parallel to each other with their longitudinal axes 42 and also not offset from each other or without an offset to each other. Further, the valve seat projection 48 is shown, which merges into the outer channel section projection 34.

In den Fig. 7 und 8 ist eine perspektivische Schnittansicht des Verdichtergehäuses 10 gemäß der Erfindung gezeigt. Dabei ist auch das Werkzeugschieberelement 16 gezeigt, mit welchem ein Schubumluftventil 12 in dem Verdichtergehäuse 10 ausgebildet ist. Das Werkzeugschieberelement 16 ist dabei teilweise aus dem Schubumluftventil 12 heraus gezogen. Das Werkzeugschieberelement 16 ist hierbei derart ausgebildet, dass in vollständig eingeführtem Zustand der erste und zweite Kanalabschnittsvorsprung 34, 36 des Werkzeugschieberelements 16, wie zuvor in Fig. 1 angedeutet ist, bis in die Spirale bzw. das Spiralgehäuse 24 und den Hauptkanal 22 des Verdichtergehäuses 10 reichen, welche beispielsweise durch eine der beiden Formhälften des Druckgusswerkzeugs gebildet werden.In the FIGS. 7 and 8 a sectional perspective view of the compressor housing 10 is shown according to the invention. In this case, the tool slide element 16 is shown, with which a diverter valve 12 is formed in the compressor housing 10. The tool slide element 16 is partially pulled out of the diverter valve 12 out. The tool slide element 16 is in this case designed such that in the fully inserted state, the first and second channel section projections 34, 36 of the tool slide element 16, as previously in Fig. 1 is indicated, extend into the spiral or spiral housing 24 and the main channel 22 of the compressor housing 10, which are formed for example by one of the two mold halves of the die-casting tool.

Fig. 9 zeigt das Verdichtergehäuse 10 und das Werkzeugschieberelement 16 in einer Schnittansicht. Dabei ist das Schubumluftventil 12 mit seinem Einlasskanal 40 und Auslasskanal 42, dem Ventilsitz 28 und dem Ventilraum 26 gezeigt. In eingeführtem Zustand passt das Werkzeugschieberelement 16 mit seiner Kontur exakt in die Kontur des Schubumluftventils 12. Fig. 9 shows the compressor housing 10 and the tool slide element 16 in a sectional view. In this case, the diverter valve 12 is shown with its inlet channel 40 and outlet channel 42, the valve seat 28 and the valve chamber 26. In imported State fits the tool slide element 16 with its contour exactly in the contour of the diverter valve 12th

In Fig. 10 ist das Verdichtergehäuse 10 und das Werkzeugschieberelement 16 in einer perspektivischen Schnittansicht gezeigt. Dabei sind der Ventilraum 26 und der Ventilsitz 28, sowie der Einlasskanal 40 und der Auslasskanal 42 des Schubumluftventils 12 gezeigt. Der Ventilsitz 28 bildet dabei einen Abschnitt des Auslasskanals bzw. äußeren Kanalabschnitts 30.In Fig. 10 the compressor housing 10 and the tool slide element 16 is shown in a perspective sectional view. In this case, the valve chamber 26 and the valve seat 28, and the inlet channel 40 and the outlet channel 42 of the diverter valve 12 are shown. The valve seat 28 forms a section of the outlet channel or outer channel section 30.

Weiter ist in Fig. 11 eine Perspektivansicht des Verdichtergehäuses 10 und des Werkzeugschieberelements 16 gezeigt. Wie zuvor beschrieben wird das Turboladergehäuse 10 bzw. hier das Verdichtergehäuse 10 im Druckguss hergestellt. Das Werkzeugschieberelement 16 ist dabei beispielsweise aus Metall oder einem anderen geeigneten festen oder beständigen Material, das vorzugsweise eine Mehrfachverwendung des Werkzeugschieberelements 16 zulässt.Next is in Fig. 11 a perspective view of the compressor housing 10 and the tool slide element 16 is shown. As described above, the turbocharger housing 10 or here the compressor housing 10 is produced by die casting. The tool slide element 16 is, for example, made of metal or another suitable solid or resistant material, which preferably allows multiple use of the tool slide element 16.

Fig. 12 zeigt das Verdichtergehäuse 10 in einer Perspektivansicht, wobei das Verdichtergehäuse 10 davon von der Seite des Schubumluftventils 12 gezeigt ist. Dabei ist der Ventilraum 26 und der Ventilsitz 28 des Schubumluftventils 12 gezeigt, sowie dessen äußerer Auslasskanal 38 und der innere Einlasskanal 40. Der Außenumfang des Ventilsitzes 26 ist dabei im Bereich des äußeren Kanals 28, hier des Auslasskanals, abgeflacht ausgebildet, um einen Teil des Kanals 28 zu bilden. Mit anderen Worten, der Abschnitt des Ventilsitzes 28 welcher einen Teil des Kanals 28 bildet ist mit seiner Kontur an den Kanal 28 geeignet angepasst, um eine optimale Strömung durch den Kanal zu ermöglichen. Fig. 12 shows the compressor housing 10 in a perspective view, wherein the compressor housing 10 thereof is shown from the side of the diverter valve 12. In this case, the valve chamber 26 and the valve seat 28 of the diverter valve 12 is shown, as well as its outer outlet channel 38 and the inner inlet channel 40. The outer periphery of the valve seat 26 is flattened in the region of the outer channel 28, here the outlet channel, to a part of the Channel 28 to form. In other words, the portion of the valve seat 28 which forms part of the channel 28 is suitably adapted with its contour to the channel 28 to allow optimum flow through the channel.

Das zuvor beschriebene Turboladergehäuse mit Ventileinrichtung, beispielsweise in Form eines Verdichtergehäuses mit einem Schubumluftventil, hat den Vorteil, dass das Gehäuse mit Ventil leicht im Druckgussverfahren hergestellt werden kann. Dabei kann das Verdichtergehäuse beispielsweise im Aluminiumdruckguss oder einem anderen geeigneten Druckguss hergestellt werden.The turbocharger housing with valve device described above, for example in the form of a compressor housing with a diverter valve, has the advantage that the housing with valve can be easily produced by die-casting. In this case, the compressor housing can be produced for example in aluminum die-cast or another suitable die-cast.

Durch die parallelaxiale und beispielsweise koaxiale Anordnung der Kanäle des Schubumluftventils in Werkzeugschieberrichtung im Druckgusswerkzeug, können der gesamte Ventilraum, der Ventilsitz und auch die Überströmkanäle des Schubumluftventils in einem Druckgusswerkzeugschieberelement dargestellt werden. Dies ermöglicht entweder ein Auskommen ohne jegliche zusätzliche mechanische Bearbeitung oder lediglich einen minimalen Bearbeitungsaufwand, der sich auf die Dicht- und Befestigungsgeometrie, d.h. den Dichtsitz und die Befestigungsbohrungen des Schubumluftventils, beschränkt.Due to the parallel axial and, for example, coaxial arrangement of the channels of the diverter valve in the tool slide direction in the die casting tool, the entire valve chamber, the valve seat and also the overflow channels of the diverter valve can be represented in a die-cast tool slide element. This allows either a livelihood without any additional mechanical processing, or only a minimal amount of processing, which can affect the sealing and mounting geometry, i. the sealing seat and the mounting holes of the diverter valve, limited.

Durch die Anordnung und die Lage des Werkzeugschieberelements im Druckgusswerkzeug kann die Anzahl und Komplexität der beweglichen Teile reduziert werden. Damit können Herstellungskosten reduziert werden, da die Machbarkeit eines druckgussfähigen Verdichtergehäuses mit einem Schubumluftventil verbessert wird. Des Weiteren kann die Komplexität des Werkzeugschieberelements reduziert und das Werkzeugschieberelement vereinfacht werden. Ein weiterer Vorteil ist dabei, dass die Bearbeitung des Verdichtergehäuses bzw. dessen Schubumluftventils reduziert werden kann oder sogar Geometrien erlaubt, die keiner zusätzlichen mechanischen Bearbeitung bedürfen, was zu einer weiteren Reduzierung der Herstellungskosten führt.The arrangement and location of the tool slide element in the die casting tool can reduce the number and complexity of moving parts. This manufacturing costs can be reduced because the feasibility of a pressure-castable compressor housing is improved with a diverter valve. Furthermore, the complexity of the tool slide element can be reduced and the tool slide element can be simplified. Another advantage is that the processing of the compressor housing or its diverter valve can be reduced or even allows geometries that require no additional mechanical processing, resulting in a further reduction in manufacturing costs.

Obwohl die vorliegende Erfindung vorstehend anhand der bevorzugten Ausführungsbeispiele beschrieben wurde, ist sie darauf nicht beschränkt, sondern im Rahmen ihrer Definition durch die beiliegenden Ansprüche auf vielfältige Art und Weise modifixierbar. Although the present invention has been described above with reference to the preferred embodiments, it is not limited thereto but can be modified in a variety of ways within the scope of its definition by the appended claims.

Claims (6)

  1. Turbocharger housing (10) with a valve device (12) formed in the turbocharger housing,
    wherein the turbocharger housing is a compressor housing, wherein the valve device (12) is an overrun air recirculation valve,
    wherein the valve device has a valve chamber (26) formed in the compressor housing and a valve seat (28) formed in the valve chamber,
    wherein the valve device has at least a first passage section (30) and a second passage section (32),
    wherein the first passage section (30) forms an outlet passage (38), which is connected to a main passage (22) of an intake side in the compressor housing and opens into the valve chamber (26),
    wherein the second passage section (32) forms an inlet passage (40), which is connected to a spiral housing (24) of a pressure side in the compressor housing and likewise opens into the valve chamber (26),
    characterized
    in that the first passage section (30) and the second passage section (32), over their entire extent, are formed free of an undercut and are arranged with their longitudinal axes (42) parallel to one another.
  2. Turbocharger housing according to Claim 1,
    characterized
    in that at least one out of the first passage section (30) and the second passage section (32) tapers proceeding from its end in the valve chamber (26) towards its respectively opposite end.
  3. Turbocharger housing according to either of Claims 1 and 2,
    characterized
    in that the valve seat (28) of the valve device (12) forms a section of the second passage section (32).
  4. Method for producing a turbocharger housing (10) with a valve device (12) formed in the turbocharger housing, according to Claim 1, wherein the method features the steps:
    - making available a pressure diecasting mold (14) for forming the turbocharger housing (10),
    - providing a mold slide element (16) formed free of an undercut in the pressure diecasting mold (14) for forming the valve device (12) in the turbocharger housing (10), wherein the mold slide element (16) has a first passage section projection (34), which forms the first passage section (30), and a second passage section projection (36), which forms the second passage section (32), wherein the first passage section projection (34) and the second passage section projection (36) are arranged with their longitudinal axes (42) parallel to one another, and wherein the mold slide element furthermore has a valve chamber section (44) and a valve seat section (46),
    - introducing a pressure diecasting material into the pressure diecasting mold (14) and forming the turbocharger housing (10) with the valve device (12) formed in the turbocharger housing (10) as a pressure diecasting part.
  5. Method according to Claim 4,
    characterized in that
    the mold slide element (16) is formed so as to form the valve seat (28), the valve chamber (26), the first passage section (30) and the second passage section (32) of the valve device (12) of an overrun air recirculation valve in a compressor housing.
  6. Method according to Claim 4 or 5,
    characterized in that
    the pressure diecasting mold (14) has a first mold half (18) and a second mold half (20), wherein the mold slide element (16) can be connected to at least one mold half (18, 20) or can be brought into engagement therewith.
EP11710461.2A 2010-03-29 2011-03-18 Turbocharger casing including valve housing and manufacturing process of such a casing Active EP2553275B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010013264A DE102010013264A1 (en) 2010-03-29 2010-03-29 Turbocharger housing with a valve device and method for producing such a turbocharger housing
PCT/EP2011/054146 WO2011120825A1 (en) 2010-03-29 2011-03-18 Turbocharger housing having a valve device, and method for manufacturing a turbocharger housing of said type

Publications (2)

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EP2553275A1 EP2553275A1 (en) 2013-02-06
EP2553275B1 true EP2553275B1 (en) 2018-01-24

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US (1) US9677568B2 (en)
EP (1) EP2553275B1 (en)
CN (1) CN102812255B (en)
DE (1) DE102010013264A1 (en)
WO (1) WO2011120825A1 (en)

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US11136997B2 (en) * 2019-07-23 2021-10-05 Ford Global Technologies, Llc Methods and systems for a compressor housing

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Also Published As

Publication number Publication date
WO2011120825A1 (en) 2011-10-06
US9677568B2 (en) 2017-06-13
DE102010013264A1 (en) 2011-09-29
CN102812255A (en) 2012-12-05
CN102812255B (en) 2016-03-02
EP2553275A1 (en) 2013-02-06
US20130136578A1 (en) 2013-05-30

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