WO2015023432A1 - Adjusting shaft arrangement of an exhaust-gas turbocharger - Google Patents

Adjusting shaft arrangement of an exhaust-gas turbocharger Download PDF

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Publication number
WO2015023432A1
WO2015023432A1 PCT/US2014/048799 US2014048799W WO2015023432A1 WO 2015023432 A1 WO2015023432 A1 WO 2015023432A1 US 2014048799 W US2014048799 W US 2014048799W WO 2015023432 A1 WO2015023432 A1 WO 2015023432A1
Authority
WO
WIPO (PCT)
Prior art keywords
adjusting shaft
bushing
bearing sleeve
region
shaft arrangement
Prior art date
Application number
PCT/US2014/048799
Other languages
French (fr)
Inventor
Thomas Ramb
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.
Publication of WO2015023432A1 publication Critical patent/WO2015023432A1/en

Links

Classifications

    • 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
    • F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • 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
    • F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • 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
    • F02B37/18—Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • F02B37/183—Arrangements of bypass valves or actuators therefor
    • F02B37/186—Arrangements of actuators or linkage for bypass valves
    • 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
    • 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
    • F02B37/18—Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • F02B37/183—Arrangements of bypass valves or actuators therefor
    • 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
    • F05D2240/00—Components
    • F05D2240/60—Shafts
    • 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
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/79—Bearing, support or actuation arrangements therefor
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Definitions

  • the invention relates to an adjusting shaft arrangement for an exhaust-gas turbocharger as per the preamble of claim 1.
  • An adjusting shaft arrangement of this type is known from EP 2 253 816 A1.
  • the known adjusting shaft arrangement has the disadvantage of a relatively large amount of axial play, and of the occurrence of a notch effect in the adjusting shaft.
  • the adjusting shaft has a smooth, that is to say non- stepped, cylindrical outer contour over its entire length, and as a result of the provision of a bearing sleeve, which is arranged on the adjusting shaft and has a stepped outer contour, and the provision of a bushing, which is arranged on said bearing sleeve and has a stepped inner contour matched to the outer contour, it is achieved firstly that the axial play of the adjusting shaft arrangement according to the invention is reduced considerably in relation to known arrangements.
  • the described design permits improved sealing, which is preferably effected through the provision of a labyrinth seal.
  • Figure 1 is a perspective sectional illustration of an exhaust-gas turbocharger according to the invention which is provided with an adjusting shaft arrangement according to the invention.
  • FIG 2 is a sectional illustration through an embodiment of an adjusting shaft arrangement according to the invention for use in the turbocharger as per Figure 1,
  • Figure 3 is an enlarged illustration in relation to Figure 1 of a longitudinal section through a bearing sleeve of the adjusting shaft arrangement
  • Figure 4 is an illustration, corresponding to Figure 3, of a bushing of the adjusting shaft arrangement according to the invention.
  • FIG 1 illustrates an exhaust-gas turbocharger 15 according to the invention which has a turbine housing 16, a bearing housing 9 and a compressor housing 17.
  • the exhaust-gas turbocharger 15 is furthermore equipped with a variable turbine geometry (VTG) that can be actuated by means of an adjusting shaft arrangement 1 according to the invention, which will hereinafter be explained in detail on the basis of Figures 2 to 4.
  • the exhaust-gas turbocharger 15 furthermore has an actuator 18 for the actuation of the adjusting shaft arrangement 1.
  • FIG. 2 is a sectional illustration of an embodiment of an adjusting shaft arrangement 1 according to the invention arranged in the bearing housing 9.
  • the adjusting shaft arrangement 1 has an adjusting shaft 2 which comprises a fixing section 3 to which an outer lever 4 is fastened, the latter being operatively connected to the actuator 18 via a connecting device that is not illustrated in detail in the figure.
  • the adjusting shaft arrangement 1 furthermore has a bearing sleeve 5 which is arranged on a main body 6 of the adjusting shaft 2.
  • the main body 6 is that region of the adjusting shaft 2 which is arranged between the fixing section 3 and a fixing section 8 to which an inner lever 7 is fastened.
  • the adjusting shaft 2 has a smooth cylindrical outer contour over its entire length LA, which means that the adjusting shaft 2 has no stepped sections.
  • the bearing sleeve 5 has a stepped outer contour 10 equipped with an abutment surface 11, as can be seen in particular from Figure 3.
  • a bushing 12 is arranged on the bearing sleeve 5, which bushing has an inner contour 13 which is matched to the outer contour 10 of the bearing sleeve 5, as shown in particular by the illustration of Figure 2.
  • the bushing 12 furthermore has an abutment surface 13 of complementary form which, as per the illustration of Figure 1, abuts against the abutment surface 11 of the bearing sleeve 5 in the installed state.
  • the detail illustration of Figure 3 shows that the bearing sleeve 5 has a sleeve region 5 A with an outer diameter Dl and has an adjoining sleeve region 5B with an outer diameter D2 that is smaller than the outer diameter Dl .
  • Said two sleeve regions 5 A and 5B form the stepped outer contour 10 of the bearing sleeve 5.
  • the inner contour 10' of the bearing sleeve 5 is cylindrical, and is thus matched to the outer contour of the adjusting shaft 2.
  • Figure 3 also shows that the abutment surface 11 is arranged preferably at an acute angle a with respect to the perpendicular LT to the longitudinal axis L of the bearing sleeve 5.
  • the longitudinal axis L of the bearing sleeve 5 corresponds to the longitudinal axis L of the adjusting shaft 2 and also to the longitudinal axis L of the bushing 12, such that said axes are each denoted by the same reference letter L in Figures 2 to 4.
  • Figure 3 shows that the sleeve region 5A has an axial length greater than the axial length of the sleeve region 5B.
  • the bushing 12 Since the bushing 12 is arranged on the bearing sleeve 5, said bushing has an inner contour 13 that is matched to the outer contour 10. Accordingly, the bushing 12 has a bushing region 12A with an inner diameter D'l and an adjoining bushing region 12B with an inner diameter D'2.
  • the bushing region 12A has a greater axial length than the bushing region 12B, wherein the juxtaposition of Figures 2 and 3 shows that the sleeve region 5 A and the bushing region 12A, and also the sleeve region 5B and the bushing region 12B, are in each case formed so as to be of equal length.
  • Figure 4 also shows that the abutment surface 14, against which the abutment surface 11 as per Figure 2 bears, is arranged at an angle ⁇ with respect to the longitudinal axis L, said angle being at least substantially a right angle, in particular exactly 90°.
  • the outer contour 13' of the bushing 12, via which said bushing bears against an inner circumferential surface of a receiving recess 20, is smooth and cylindrical, with a slight bevel 19 of the bushing region 12B at the end side.
  • the above-described design of the adjusting shaft arrangement 1 makes it possible to realize the advantages explained in the introduction, in particular the reduction of a degree of axial play, improved sealing through the preferable provision of a labyrinth seal 14 that is illustrated in Figure 1, the elimination of a notch effect in the adjusting shaft 2, and simplified installation of the assembly comprising the adjusting shaft 2 in a mass production context, because there is no need for the bearing sleeve 5 to be pressed in in stepwise fashion.

Landscapes

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

Abstract

The invention relates to an adjusting shaft arrangement (1) for an exhaust-gas turbocharger (15) that is equipped in particular with a variable turbine geometry (VTG) and/or a wastegate arrangement, having an adjusting shaft (2) that has a fixing section (3); having an outer lever (4) that is connected to the adjusting shaft (2) via the fixing section (3); and having a bearing sleeve (5) that is arranged on a main body (6) of the adjusting shaft (2); wherein the adjusting shaft (2) has a smooth cylindrical outer contour over its entire length (LA); the bearing sleeve (5) has a stepped outer contour (10) with a first abutment surface (11), and a bushing (12) is arranged on the bearing sleeve (5), the inner contour (13) of which bushing is matched to the outer contour (10) of the bearing sleeve (5) and which bushing has a second abutment surface (14) of complementary form which abuts against the abutment surface (11).

Description

ADJUSTING SHAFT ARRANGEMENT OF AN EXHAUST-GAS
TURBOCHARGER
DESCRIPTION
The invention relates to an adjusting shaft arrangement for an exhaust-gas turbocharger as per the preamble of claim 1.
An adjusting shaft arrangement of this type is known from EP 2 253 816 A1. The known adjusting shaft arrangement has the disadvantage of a relatively large amount of axial play, and of the occurrence of a notch effect in the adjusting shaft.
It is therefore an object of the present invention to provide an adjusting shaft arrangement of the type indicated in the preamble of claim 1, which adjusting shaft arrangement permits a reduction of the axial play and an elimination of the notch effect in the adjusting shaft.
This object is achieved by the features of claim 1.
By virtue of the fact that the adjusting shaft has a smooth, that is to say non- stepped, cylindrical outer contour over its entire length, and as a result of the provision of a bearing sleeve, which is arranged on the adjusting shaft and has a stepped outer contour, and the provision of a bushing, which is arranged on said bearing sleeve and has a stepped inner contour matched to the outer contour, it is achieved firstly that the axial play of the adjusting shaft arrangement according to the invention is reduced considerably in relation to known arrangements.
Furthermore, owing to the design explained above, there is no notch effect in the adjusting shaft because an improved transmission of torque is possible.
Furthermore, the described design permits improved sealing, which is preferably effected through the provision of a labyrinth seal.
Finally, simplified installation of the adjusting shaft assembly is advantageously made possible because, in particular, there is no need for the bearing sleeve to be pressed in in stepwise fashion onto the smooth outer contour of the adjusting shaft.
The dependent claims contain advantageous developments of the invention. Further details, features and advantages of the invention become apparent from the following description with reference to the drawing, in which: Figure 1 is a perspective sectional illustration of an exhaust-gas turbocharger according to the invention which is provided with an adjusting shaft arrangement according to the invention.
Figure 2 is a sectional illustration through an embodiment of an adjusting shaft arrangement according to the invention for use in the turbocharger as per Figure 1,
Figure 3 is an enlarged illustration in relation to Figure 1 of a longitudinal section through a bearing sleeve of the adjusting shaft arrangement, and
Figure 4 is an illustration, corresponding to Figure 3, of a bushing of the adjusting shaft arrangement according to the invention.
Figure 1 illustrates an exhaust-gas turbocharger 15 according to the invention which has a turbine housing 16, a bearing housing 9 and a compressor housing 17. The exhaust-gas turbocharger 15 is furthermore equipped with a variable turbine geometry (VTG) that can be actuated by means of an adjusting shaft arrangement 1 according to the invention, which will hereinafter be explained in detail on the basis of Figures 2 to 4. The exhaust-gas turbocharger 15 furthermore has an actuator 18 for the actuation of the adjusting shaft arrangement 1.
Figure 2 is a sectional illustration of an embodiment of an adjusting shaft arrangement 1 according to the invention arranged in the bearing housing 9. The adjusting shaft arrangement 1 has an adjusting shaft 2 which comprises a fixing section 3 to which an outer lever 4 is fastened, the latter being operatively connected to the actuator 18 via a connecting device that is not illustrated in detail in the figure.
The adjusting shaft arrangement 1 furthermore has a bearing sleeve 5 which is arranged on a main body 6 of the adjusting shaft 2. The main body 6 is that region of the adjusting shaft 2 which is arranged between the fixing section 3 and a fixing section 8 to which an inner lever 7 is fastened.
As can be seen from Figure 2, the adjusting shaft 2 has a smooth cylindrical outer contour over its entire length LA, which means that the adjusting shaft 2 has no stepped sections.
The bearing sleeve 5 has a stepped outer contour 10 equipped with an abutment surface 11, as can be seen in particular from Figure 3.
A bushing 12 is arranged on the bearing sleeve 5, which bushing has an inner contour 13 which is matched to the outer contour 10 of the bearing sleeve 5, as shown in particular by the illustration of Figure 2. The bushing 12 furthermore has an abutment surface 13 of complementary form which, as per the illustration of Figure 1, abuts against the abutment surface 11 of the bearing sleeve 5 in the installed state.
The detail illustration of Figure 3 shows that the bearing sleeve 5 has a sleeve region 5 A with an outer diameter Dl and has an adjoining sleeve region 5B with an outer diameter D2 that is smaller than the outer diameter Dl . Said two sleeve regions 5 A and 5B form the stepped outer contour 10 of the bearing sleeve 5. The inner contour 10' of the bearing sleeve 5 is cylindrical, and is thus matched to the outer contour of the adjusting shaft 2.
Figure 3 also shows that the abutment surface 11 is arranged preferably at an acute angle a with respect to the perpendicular LT to the longitudinal axis L of the bearing sleeve 5. The longitudinal axis L of the bearing sleeve 5 corresponds to the longitudinal axis L of the adjusting shaft 2 and also to the longitudinal axis L of the bushing 12, such that said axes are each denoted by the same reference letter L in Figures 2 to 4.
Finally, Figure 3 shows that the sleeve region 5A has an axial length greater than the axial length of the sleeve region 5B.
Since the bushing 12 is arranged on the bearing sleeve 5, said bushing has an inner contour 13 that is matched to the outer contour 10. Accordingly, the bushing 12 has a bushing region 12A with an inner diameter D'l and an adjoining bushing region 12B with an inner diameter D'2. The bushing region 12A has a greater axial length than the bushing region 12B, wherein the juxtaposition of Figures 2 and 3 shows that the sleeve region 5 A and the bushing region 12A, and also the sleeve region 5B and the bushing region 12B, are in each case formed so as to be of equal length.
Figure 4 also shows that the abutment surface 14, against which the abutment surface 11 as per Figure 2 bears, is arranged at an angle β with respect to the longitudinal axis L, said angle being at least substantially a right angle, in particular exactly 90°.
The outer contour 13' of the bushing 12, via which said bushing bears against an inner circumferential surface of a receiving recess 20, is smooth and cylindrical, with a slight bevel 19 of the bushing region 12B at the end side.
The above-described design of the adjusting shaft arrangement 1 makes it possible to realize the advantages explained in the introduction, in particular the reduction of a degree of axial play, improved sealing through the preferable provision of a labyrinth seal 14 that is illustrated in Figure 1, the elimination of a notch effect in the adjusting shaft 2, and simplified installation of the assembly comprising the adjusting shaft 2 in a mass production context, because there is no need for the bearing sleeve 5 to be pressed in in stepwise fashion.
In addition to the above written disclosure of the invention, reference is hereby explicitly made to the illustrative presentation thereof in Figures 1 to 4.
LIST OF REFERENCE SIGNS
1 Adjusting shaft arrangement
2 Adjusting shaft (cylindrical clamping axle)
3 Fixing section
4 Lever
5 Bearing sleeve
5A, 5B Sleeve regions
6 Main body
7 Inner lever
8 Fixing section
9 Bearing housing
10 Outer contour
11 First abutment surface
12 Bushing
12 A, 12B Bushing regions
13 Inner contour
13' Outer contour
14 Second abutment surface
15 Exhaust-gas turbocharger
16 Turbine housing
17 Compressor housing
18 Actuator
19 Bevel
20 Receiving recess of the bearing housing 9
VTG Variable turbine geometry
α, β Angles
D 1 , D2 Outer diameters
D'l, D'2 Inner diameters
L Longitudinal axis of the adjusting shaft 2, of the bearing sleeve 5 and of the bushing 12
LA Length of the adjusting shaft 2

Claims

1. An adjusting shaft arrangement (1) for an exhaust-gas turbocharger (15) that is equipped in particular with a variable turbine geometry (VTG) and/or a wastegate arrangement,
having an adjusting shaft (2) that has a fixing section (3); having an outer lever (4) that is connected to the adjusting shaft (2) via the fixing section (3); and
having a bearing sleeve (5) that is arranged on a main body (6) of the adjusting shaft (2); wherein
the adjusting shaft (2) has a smooth cylindrical outer contour over its entire length (LA);
the bearing sleeve (5) has a stepped outer contour (10) with a first abutment surface (11), and
- a bushing (12) is arranged on the bearing sleeve (5), the inner contour
(13) of which bushing is matched to the outer contour (10) of the bearing sleeve (5) and which bushing has a second abutment surface (14) of complementary form which abuts against the abutment surface (11).
2. The adjusting shaft arrangement as claimed in claim 1, wherein the first abutment surface (11) points toward the outer lever (4).
3. The adjusting shaft arrangement as claimed in claim 1 or 2, wherein the first abutment surface (11) is arranged at an acute angle (a) with respect to the perpendicular (LT) to the longitudinal axis (L) of the bearing sleeve (5).
4. The adjusting shaft arrangement as claimed in one of claims 1 to 3, wherein the second abutment surface (14) is arranged at least substantially at right angles (β) with respect to the longitudinal axis (L) of the bearing sleeve (5) or of the bushing (12).
5. The adjusting shaft arrangement as claimed in one of claims 1 to 4, wherein the bearing sleeve (5) has a sleeve region (5 A) with a first outer diameter (Dl) and has an adjoining sleeve region (5B) with a second outer diameter (D2) that is smaller than the first outer diameter (Dl).
6. The adjusting shaft arrangement as claimed in claim 5, wherein the sleeve region (5) is axially longer than the sleeve region (5B).
7. The adjusting shaft arrangement as claimed in one of claims 1 to 6, wherein the bushing (12) has a bushing region (12A) with an inner diameter (D'l) corresponding to the outer diameter (Dl) and has a bushing region (12B) with an inner diameter (D'2) corresponding to the outer diameter (D2).
8. The adjusting shaft arrangement as claimed in claim 7, wherein the bushing region (12A) is longer than the bushing region (12B).
9. The adjusting shaft arrangement as claimed in one of claims 5 to 8, wherein the relatively short sleeve region (5B) and the relatively short bushing region (12B) are arranged adjacent to the outer lever (4).
10. The adjusting shaft arrangement as claimed in one of claims 1 to 9, wherein a labyrinth seal (14) is arranged between the bearing sleeve (5) and the adjusting shaft (2).
PCT/US2014/048799 2013-08-14 2014-07-30 Adjusting shaft arrangement of an exhaust-gas turbocharger WO2015023432A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102013013618.0 2013-08-14
DE102013013618 2013-08-14

Publications (1)

Publication Number Publication Date
WO2015023432A1 true WO2015023432A1 (en) 2015-02-19

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ID=52468579

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Application Number Title Priority Date Filing Date
PCT/US2014/048799 WO2015023432A1 (en) 2013-08-14 2014-07-30 Adjusting shaft arrangement of an exhaust-gas turbocharger

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WO (1) WO2015023432A1 (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4838711A (en) * 1987-04-11 1989-06-13 Kuehnle, Kopp & Kausch Bearing for an exhaust-gas turbocharger
US20020098080A1 (en) * 2001-01-25 2002-07-25 Arnold Steven Don Actuator shaft seal for variable nozzle turbocharger
US20040057834A1 (en) * 2001-02-09 2004-03-25 Masami Shimizu Connection method for turbo charger turbine shaft
US20090226304A1 (en) * 2005-06-02 2009-09-10 Borgwarner Inc. Adjusting shaft arrangement of a turbocharger
US20130071243A1 (en) * 2011-09-20 2013-03-21 Honeywell International Inc. Turbocharger rotating assembly

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4838711A (en) * 1987-04-11 1989-06-13 Kuehnle, Kopp & Kausch Bearing for an exhaust-gas turbocharger
US20020098080A1 (en) * 2001-01-25 2002-07-25 Arnold Steven Don Actuator shaft seal for variable nozzle turbocharger
US20040057834A1 (en) * 2001-02-09 2004-03-25 Masami Shimizu Connection method for turbo charger turbine shaft
US20090226304A1 (en) * 2005-06-02 2009-09-10 Borgwarner Inc. Adjusting shaft arrangement of a turbocharger
US20130071243A1 (en) * 2011-09-20 2013-03-21 Honeywell International Inc. Turbocharger rotating assembly

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