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EP1722073B1 - Variable geometry turbocharger unison ring - Google Patents

Variable geometry turbocharger unison ring Download PDF

Info

Publication number
EP1722073B1
EP1722073B1 EP05010523A EP05010523A EP1722073B1 EP 1722073 B1 EP1722073 B1 EP 1722073B1 EP 05010523 A EP05010523 A EP 05010523A EP 05010523 A EP05010523 A EP 05010523A EP 1722073 B1 EP1722073 B1 EP 1722073B1
Authority
EP
European Patent Office
Prior art keywords
ring
adjusting
lever engagement
bearing
bearing ring
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.)
Not-in-force
Application number
EP05010523A
Other languages
German (de)
French (fr)
Other versions
EP1722073A1 (en
Inventor
Holger Fäth
Ralf Böning
Dirk Frankenstein
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.)
BorgWarner Inc
Original Assignee
BorgWarner Inc
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.)
Filing date
Publication date
Application filed by BorgWarner Inc filed Critical BorgWarner Inc
Priority to EP05010523A priority Critical patent/EP1722073B1/en
Priority to CNA2006800165718A priority patent/CN101175897A/en
Priority to US11/913,896 priority patent/US8459938B2/en
Priority to KR1020077023545A priority patent/KR20080005923A/en
Priority to PCT/EP2006/002233 priority patent/WO2006122596A1/en
Priority to JP2008510423A priority patent/JP2008540907A/en
Publication of EP1722073A1 publication Critical patent/EP1722073A1/en
Application granted granted Critical
Publication of EP1722073B1 publication Critical patent/EP1722073B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
    • 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
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/22—Manufacture essentially without removing material by sintering
    • 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
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles

Definitions

  • the invention relates to an adjusting ring for adjusting the blades of the VTG diffuser of exhaust gas turbochargers, according to the preamble of claim 1.
  • VTG diffuser is understood to mean an arrangement which serves to provide exhaust gas turbochargers with a variable turbine geometry.
  • an adjusting ring specified in the preamble of claim 1, which has a bearing ring for receiving bearing bodies and a lever engagement ring.
  • the lever engagement ring is provided with grooves in which the levers of the VTG blades engage.
  • Such known adjusting rings for example, from the EP-A-1 398 463 are known, are constructed as fully machined components, which are usually produced in turning or milling operations or combined operations.
  • the adjusting ring is formed with its bearing ring and a lever engaging ring as a one-piece part of a solid material.
  • this represents a relatively time-consuming and costly production process.
  • the adjusting ring is made of several, at least two, separately manufactured individual parts, which are connected to one another by means of a suitable connecting device.
  • the individual parts can in this case by Urform- (investment casting or sintering), forming (pressing) or separation processes, preferably stamping, be made completely or require a small machining finishing, such as turning or milling.
  • the items may consist of different materials, which are adapted to the specific function of the bearing of the bearing ring or bearing portion of the adjusting and the leadership of the blade lever of the lever engagement ring or lever engagement portion.
  • bearing ring and the lever engagement ring can be adapted in terms of their geometry in a simple manner to the said functions. For example, a specific hardening of the surface according to the required properties is possible.
  • the bearing ring and the lever engagement ring are each made in a separate manufacturing step as separate items.
  • connecting device can be used in principle all suitable material or positive connections.
  • crimping or edging operations as well as welding or soldering are particularly preferably suitable for connecting the bearing ring and the manufacturing ring according to the method according to the invention. .
  • FIG. 1 an inventive adjusting ring 1 for adjusting the blades of a VTG diffuser of exhaust gas turbochargers is shown.
  • the adjusting ring 1 has a bearing ring 2, which is provided for guiding suitable bearing bodies (rolling elements).
  • the adjusting ring 1 has a lever engagement ring 3, which has a plurality of circumferentially arranged grooves, one of which is designated by the reference numeral 5.
  • Fig. 1 clarifies, the adjusting ring with its two components bearing ring and lever engagement ring 3 is a circular Component in Fig. 2 is again illustrated along the section line AA.
  • Fig. 2 illustrates here that the bearing ring 2 and the lever engagement ring 3 are connected via a connecting device 4 with each other after their preparation as individual parts to form the adjusting ring 1 in its entirety.
  • the connecting device 4 is in this case illustrated by the dividing line between the bearing ring 2 and the lever engagement ring 3 and can be generated by one of the above-explained methods of production.

Landscapes

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

Description

Die Erfindung betrifft einen Verstellring zum Verstellen der Schaufeln des VTG-Leitapparates von Abgasturboladern, gemäss dem Oberbegriff des Anspruchs 1.The invention relates to an adjusting ring for adjusting the blades of the VTG diffuser of exhaust gas turbochargers, according to the preamble of claim 1.

Unter dem Begriff "VTG-Leitapparat" versteht man eine Anordnung, die dazu dient, Abgasturbolader mit einer variablen Turbinengeometrie zu versehen. Zur Verstellung dieser variablen Turbinengeometrie dient ein Verstellring der im Oberbegriff des Anspruches 1 angegebenen Art, der einen Lagerring zur Aufnahme von Lagerkörpern und einen Hebeleingriffsring aufweist. Der Hebeleingriffsring ist mit Nuten versehen, in die die Hebel der VTG-Schaufeln eingreifen.The term "VTG diffuser" is understood to mean an arrangement which serves to provide exhaust gas turbochargers with a variable turbine geometry. To adjust this variable turbine geometry is an adjusting ring specified in the preamble of claim 1, which has a bearing ring for receiving bearing bodies and a lever engagement ring. The lever engagement ring is provided with grooves in which the levers of the VTG blades engage.

Derartige bekannte Verstellringe, die z.B. aus der EP-A-1 398 463 bekannt sind, sind als voll zerspante Bauteile aufgebaut, die üblicherweise in Dreh- oder Fräsvorgängen oder kombinierten Arbeitsgängen hergestellt werden. Hierzu wird aus einem Vollmaterial der Verstellring mit seinem Lagerring und einem Hebeleingriffsring als einstückiges Teil ausgebildet. Dies stellt jedoch ein relativ zeit- und kostenaufwendiges Herstellungsverfahren dar.Such known adjusting rings, for example, from the EP-A-1 398 463 are known, are constructed as fully machined components, which are usually produced in turning or milling operations or combined operations. For this purpose, the adjusting ring is formed with its bearing ring and a lever engaging ring as a one-piece part of a solid material. However, this represents a relatively time-consuming and costly production process.

Auch das Gießen eines kompletten Verstellringrohteils mit anschließender spanender Bearbeitung führt nicht zu deutlichen Kostenvorteilen.The casting of a complete Verstellringrohteils with subsequent machining does not lead to significant cost advantages.

Aus der EP-A- 1 422 385 ist ein Verfahren zur Hestellung eines Turbinenrahmen bekannt.From the EP-A-1 422 385 a method for the production of a turbine frame is known.

Es ist daher Aufgabe der vorliegenden Erfindung, einen Verstellring der im Oberbegriff des Anspruches 1 angegebenen Art zu schaffen, der auf einfache und kostengünstige Art und Weise herstellbar ist.It is therefore an object of the present invention to provide an adjusting ring specified in the preamble of claim 1 way, which can be produced in a simple and cost-effective manner.

Es ist ferner Aufgabe der Erfindung, ein Verfahren zur Herstellung eines derartigen Verstellringes zu schaffen.It is a further object of the invention to provide a method for producing such an adjusting ring.

Die Lösung dieser Aufgabe erfolgt durch die Merkmale des Anspruchs 1 bzw. des Anspruches 9.The solution of this object is achieved by the features of claim 1 and claim 9.

Erfindungsgemäß ist der Verstellring aus mehreren, zumindest zwei, separat hergestellten Einzelteilen gefertigt, die mittels einer geeigneten Verbindungseinrichtung miteinander verbunden werden. Die Einzelteile können hierbei durch Urform-(Feingießen oder Sintern), Umform- (Pressen) oder Trennverfahren, vorzugsweise Stanzen, komplett hergestellt werden oder erfordern eine geringe spanende Nachbearbeitung, wie Drehen oder Fräsen.According to the invention, the adjusting ring is made of several, at least two, separately manufactured individual parts, which are connected to one another by means of a suitable connecting device. The individual parts can in this case by Urform- (investment casting or sintering), forming (pressing) or separation processes, preferably stamping, be made completely or require a small machining finishing, such as turning or milling.

Die Einzelteile können aus verschiedenen Werkstoffen bestehen, die an die spezifische Funktion der Lagerung des Lagerrings bzw. Lagerabschnitts des Verstellringes und an die Führung der Schaufelhebel des Hebeleingriffsringes bzw. Hebeleingriffabschnittes angepasst sind.The items may consist of different materials, which are adapted to the specific function of the bearing of the bearing ring or bearing portion of the adjusting and the leadership of the blade lever of the lever engagement ring or lever engagement portion.

Ferner ergibt sich der Vorteil, dass der Lagerring und der Hebeleingriffsring hinsichtlich ihrer Geometrie auf einfache Art und Weise an die genannten Funktionen angepasst werden können.
So ist beispielsweise eine gezielte Härtung der Oberfläche gemäß der geforderten Eigenschaften möglich.Furthermore, there is the advantage that the bearing ring and the lever engagement ring can be adapted in terms of their geometry in a simple manner to the said functions.
For example, a specific hardening of the surface according to the required properties is possible.

Die Unteransprüche 2 bis 6 haben vorteilhafte Weiterbildungen des erfindungsgemäßen Verstellrings zum Inhalt.The dependent claims 2 to 6 have advantageous developments of the adjusting ring according to the invention to the content.

In den Ansprüchen 8 bis 11 ist ein erfindungsgemäßes Verfahren zur Herstellung eines zuvor erläuterten Verstellringes definiert.In claims 8 to 11, a method according to the invention for the production of a previously described adjusting ring is defined.

Demgemäß werden der Lagerring und der Hebeleingriffsring jeweils in einem separaten Herstellungsschritt als separate Einzelteile gefertigt.Accordingly, the bearing ring and the lever engagement ring are each made in a separate manufacturing step as separate items.

Danach werden die beiden Ringe durch eine geeignete Verbindungseinrichtung miteinander verbunden.Thereafter, the two rings are connected together by a suitable connecting device.

Als Verbindungseinrichtung können vom Prinzip her alle geeigneten stoff- oder formschlüssigen Verbindungen herangezogen werden.As a connecting device can be used in principle all suitable material or positive connections.

Besonders bevorzugt sind zur Verbindung des Lagerrings und des Herstellungsrings gemäß dem erfindungsgemäßen Verfahren jedoch Bördel- oder Umkantvorgänge sowie Schweißen oder Löten geeignet. ,However, crimping or edging operations as well as welding or soldering are particularly preferably suitable for connecting the bearing ring and the manufacturing ring according to the method according to the invention. .

Vom Prinzip her wäre auch eine Verschraubung oder eine Nietung denkbar.In principle, a screw or a riveting would be conceivable.

Weitere Einzelheiten, Vorteile und Merkmale der Erfindung ergeben sich aus nachfolgender Beschreibung eines Ausführungsbeispiels anhand der Zeichnung. Es zeigt:

Fig. 1
eine Frontansicht eines erfindungsgemäßen Verstellrings, und
Fig. 2
eine Schnittdarstellung des Verstellrings gemäß Fig. 1 entlang der Linie A-A in Fig. 1.
Further details, advantages and features of the invention will become apparent from the following description of an embodiment with reference to the drawing. It shows:
Fig. 1
a front view of an adjusting ring according to the invention, and
Fig. 2
a sectional view of the adjusting ring according to Fig. 1 along the line AA in Fig. 1 ,

Gemäß Fig. 1 ist ein erfindungsgemäßer Verstellring 1 zum Verstellen der Schaufeln eines VTG-Leitapparates von Abgasturboladern dargestellt.According to Fig. 1 an inventive adjusting ring 1 for adjusting the blades of a VTG diffuser of exhaust gas turbochargers is shown.

Der Verstellring 1 weist einen Lagerring 2 auf, der zum Führen von geeigneten Lagerkörpern (Wälzkörpern) vorgesehen ist.The adjusting ring 1 has a bearing ring 2, which is provided for guiding suitable bearing bodies (rolling elements).

Ferner weist der Verstellring 1 einen Hebeleingriffsring 3 auf, der eine Mehrzahl von am Umfang angeordneten Nuten aufweist, von denen eine mit der Bezugsziffer 5 gekennzeichnet ist.Furthermore, the adjusting ring 1 has a lever engagement ring 3, which has a plurality of circumferentially arranged grooves, one of which is designated by the reference numeral 5.

Wie Fig. 1 verdeutlicht, ist der Verstellring mit seinen beiden Bauteilen Lagerring und Hebeleingriffsring 3 ein kreisrundes Bauteil, das in Fig. 2 entlang der Schnittlinie A-A nochmals verdeutlicht ist.As Fig. 1 clarifies, the adjusting ring with its two components bearing ring and lever engagement ring 3 is a circular Component in Fig. 2 is again illustrated along the section line AA.

Fig. 2 verdeutlicht hierbei, dass der Lagerring 2 und der Hebeleingriffsring 3 über eine Verbindungseinrichtung 4 miteinander nach ihrer Herstellung als Einzelteile verbunden sind, um den Verstellring 1 in seiner Gesamtheit zu bilden. Die Verbindungseinrichtung 4 ist hierbei durch die Trennlinie zwischen dem Lagerring 2 und dem Hebeleingriffsring 3 verdeutlicht und kann durch eine der eingangs erläuterten Herstellungsweisen erzeugt werden. Fig. 2 illustrates here that the bearing ring 2 and the lever engagement ring 3 are connected via a connecting device 4 with each other after their preparation as individual parts to form the adjusting ring 1 in its entirety. The connecting device 4 is in this case illustrated by the dividing line between the bearing ring 2 and the lever engagement ring 3 and can be generated by one of the above-explained methods of production.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
Verstellringadjusting
22
Lagerringbearing ring
33
HebeleingriffsringLever engagement ring
44
Verbindungseinrichtungconnecting device
55
Nutgroove

Claims (12)

  1. Adjusting ring (1) for adjusting the blades of the VTG distributor of exhaust gas turbochargers
    - having a bearing ring (2); and
    - having a lever engagement ring (3) which is connected to the bearing ring (2),
    characterized
    - in that the bearing ring (2) and the lever engagement ring (3) are separately-produced individual parts which are connected to one another by means of a separate connecting device (4).
  2. Adjusting ring according to Claim 1, characterized in that the bearing ring (2) is formed as a sheet metal part.
  3. Adjusting ring according to Claim 1 or 2, characterized in that the lever engagement ring (3) is formed as a sheet metal part.
  4. Adjusting ring according to one of Claims 1 to 3, characterized in that the bearing ring (2) and the lever engagement ring (3) are produced from the same or from different materials.
  5. Adjusting ring according to one of Claims 1 to 4, characterized in that the bearing ring (2) and/or the lever engagement ring (3) are produced as sintered parts.
  6. Adjusting ring according to one of Claims 1 to 5, characterized in that the geometry of the bearing ring (2) and/or of the lever engagement ring (3) is adapted to the bearing function and/or the guidance function.
  7. Adjusting ring according to one of Claims 1 to 6, characterized in that the connecting device (4) is formed as a flanged or overturned connection.
  8. Adjusting ring according to one of Claims 1 to 6, characterized in that the connecting device (4) is formed as a welded or soldered connection.
  9. Method for producing an adjusting ring for adjusting the blades of the VTG distributor of exhaust gas turbochargers, characterized by the following method steps:
    - producing a bearing ring (2) as a separate component;
    - producing a lever engagement ring (3) as a separate component in a separate production step; and
    - connecting the bearing ring (2) to the lever engagement ring (3).
  10. Method according to Claim 9, characterized in that the production of the bearing ring (2) and of the lever engagement ring (3) takes place by means of punching as separate sheet metal parts.
  11. Method according to Claim 9, characterized in that the production of the bearing ring (2) and of the lever engagement ring (3) takes place by means of sintering as separate sheet metal parts.
  12. Method according to Claim 9 or 10 or 11, characterized in that the connection of the bearing ring (2) and of the lever engagement ring (3) takes place by means of flanging, overturning, welding or soldering.
EP05010523A 2005-05-13 2005-05-13 Variable geometry turbocharger unison ring Not-in-force EP1722073B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
EP05010523A EP1722073B1 (en) 2005-05-13 2005-05-13 Variable geometry turbocharger unison ring
CNA2006800165718A CN101175897A (en) 2005-05-13 2006-03-10 Adjusting ring for adjusting the blades of teh VTG distributor of exhaust gas turbochargers
US11/913,896 US8459938B2 (en) 2005-05-13 2006-03-10 Adjusting ring for adjusting the blades of the VTG distributor of exhaust gas turbochargers
KR1020077023545A KR20080005923A (en) 2005-05-13 2006-03-10 Adjustment ring for adjusting the blades of the exhaust distributor of the exhaust turbochargers
PCT/EP2006/002233 WO2006122596A1 (en) 2005-05-13 2006-03-10 Adjusting ring for adjusting the blades of the vtg distributor of exhaust gas turbochargers
JP2008510423A JP2008540907A (en) 2005-05-13 2006-03-10 Adjustment ring for adjusting the blades of the VTG distributor of the exhaust gas turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP05010523A EP1722073B1 (en) 2005-05-13 2005-05-13 Variable geometry turbocharger unison ring

Publications (2)

Publication Number Publication Date
EP1722073A1 EP1722073A1 (en) 2006-11-15
EP1722073B1 true EP1722073B1 (en) 2013-01-23

Family

ID=35058291

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05010523A Not-in-force EP1722073B1 (en) 2005-05-13 2005-05-13 Variable geometry turbocharger unison ring

Country Status (6)

Country Link
US (1) US8459938B2 (en)
EP (1) EP1722073B1 (en)
JP (1) JP2008540907A (en)
KR (1) KR20080005923A (en)
CN (1) CN101175897A (en)
WO (1) WO2006122596A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4098821B1 (en) * 2007-06-07 2008-06-11 株式会社アキタファインブランキング Variable mechanism in VGS type turbocharger and exhaust guide assembly incorporating the same
DE102008014680A1 (en) * 2008-03-18 2010-09-23 Continental Automotive Gmbh Leitgitteranordnung an exhaust gas turbocharger, exhaust gas turbocharger and method for producing a Leitgitteranordnung
DE102008039093A1 (en) * 2008-08-21 2010-02-25 Bosch Mahle Turbo Systems Gmbh & Co. Kg Turbo-supercharger for internal combustion engine of motor vehicle, has turbine wheel and compressor wheel, which are mounted in bearing housing by common shaft
DE102009008531A1 (en) 2009-02-11 2010-08-12 Bosch Mahle Turbo Systems Gmbh & Co. Kg Adjusting ring for a charging device, in particular for an exhaust gas turbocharger of a motor vehicle
CN102597453B (en) * 2009-11-27 2014-12-10 博格华纳公司 Turbocharger with variable turbine geometry (VTG)
CN105804849B (en) * 2010-10-25 2019-02-15 博格华纳公司 Exhaust turbine supercharger
US8864449B2 (en) * 2010-11-02 2014-10-21 Hamilton Sundstrand Corporation Drive ring bearing for compressor diffuser assembly
DE112011103421T8 (en) * 2010-12-08 2013-12-24 Borgwarner Inc. turbocharger
DE102012106789B4 (en) * 2012-07-26 2022-10-27 Ihi Charging Systems International Gmbh Adjustable diffuser for a turbine, turbine for an exhaust gas turbocharger and exhaust gas turbocharger
GB2527297B (en) * 2014-06-16 2016-08-17 Rolls Royce Plc An assembly
DE202016103778U1 (en) * 2016-07-13 2016-07-27 Bosch Mahle Turbo Systems Gmbh & Co. Kg Adjustment ring of a variable turbine geometry

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE7904823L (en) * 1978-06-06 1979-12-07 Skf Kugellagerfabriken Gmbh BALL BEARINGS
US4373859A (en) * 1981-09-23 1983-02-15 General Motors Corporation Unison ring support system
US4654941A (en) * 1984-04-20 1987-04-07 The Garrett Corporation Method of assembling a variable nozzle turbocharger
JPS60175829U (en) * 1984-04-28 1985-11-21 三菱自動車工業株式会社 Stator vane drive device for variable displacement exhaust turbocharger
JPS6125512U (en) * 1984-07-20 1986-02-15 三菱自動車工業株式会社 Exhaust inlet variable turbo charger
DE3501883C1 (en) * 1985-01-22 1986-08-28 J.M. Voith Gmbh, 7920 Heidenheim Cover for turbines and pumps
DE3516738A1 (en) * 1985-05-09 1986-11-13 Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen FLOWING MACHINE
DE3541508C1 (en) 1985-11-23 1987-02-05 Kuehnle Kopp Kausch Ag Exhaust gas turbocharger
JPS6321331A (en) * 1986-07-15 1988-01-28 Toyota Motor Corp Variable nozzle turbocharger
US6710021B1 (en) * 1999-09-22 2004-03-23 Henkel Loctite Corporation Non-staining, active metal-working fluid
JP2001173681A (en) * 1999-12-22 2001-06-26 Mitsubishi Materials Corp Iron-base sintered alloy-made synchronizer ring excellent in seizure resistance
IT1320472B1 (en) * 2000-06-30 2003-11-26 Skf Ind Spa ROLLING BEARING FOR AN ELECTRIC MOTOR.
EP1234950B1 (en) * 2001-02-26 2006-01-18 Mitsubishi Heavy Industries, Ltd. Vane adjustment mechanism for a turbine and assembling method therefor
JP2003048029A (en) * 2001-08-03 2003-02-18 Sogi Kogyo Kk Method for manufacturing turbine frame capable of turnably holding variable blade in exhaust guide assembly of vgs type turbocharger
US20040205966A1 (en) * 2001-08-03 2004-10-21 Shinjiroh Ohishi Method of manufacturing turbine frame of vgs type turbo charger, turbine frame manufactured by the method, exhaust gas guide assembly of vgs type turbo charger using the turbine frame and vgs type turbo charger incorporating the exhaust gas guide assembly
DE50207509D1 (en) * 2002-09-10 2006-08-24 Borgwarner Inc Guiding gratings of variable geometry and turbocharger with such a guide grille
JP4008404B2 (en) * 2002-10-18 2007-11-14 三菱重工業株式会社 Variable displacement exhaust turbocharger
US6984104B2 (en) * 2002-12-16 2006-01-10 United Technologies Corporation Variable vane arm/unison ring attachment system
FR2866058B1 (en) * 2004-02-05 2006-06-02 Snecma Moteurs LEVER FOR CONTROLLING THE ANGULAR SETTING OF A DAWN IN A TURBOMACHINE
US6925806B1 (en) * 2004-04-21 2005-08-09 Honeywell International, Inc. Variable geometry assembly for turbochargers
GB2416194B (en) * 2004-07-15 2006-08-16 Rolls Royce Plc A spacer arrangement
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

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CN101175897A (en) 2008-05-07
US20090142185A1 (en) 2009-06-04
KR20080005923A (en) 2008-01-15
WO2006122596A1 (en) 2006-11-23
EP1722073A1 (en) 2006-11-15
US8459938B2 (en) 2013-06-11
JP2008540907A (en) 2008-11-20

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