WO2012018553A2 - Exhaust-gas turbocharger - Google Patents

Exhaust-gas turbocharger Download PDF

Info

Publication number
WO2012018553A2
WO2012018553A2 PCT/US2011/044954 US2011044954W WO2012018553A2 WO 2012018553 A2 WO2012018553 A2 WO 2012018553A2 US 2011044954 W US2011044954 W US 2011044954W WO 2012018553 A2 WO2012018553 A2 WO 2012018553A2
Authority
WO
WIPO (PCT)
Prior art keywords
housing
bearing housing
screws
exhaust
gas turbocharger
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.)
Ceased
Application number
PCT/US2011/044954
Other languages
French (fr)
Other versions
WO2012018553A3 (en
Inventor
Wolfram Schaefer
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 KR1020137004072A priority Critical patent/KR102077747B1/en
Priority to JP2013523187A priority patent/JP2013533429A/en
Priority to DE112011102593T priority patent/DE112011102593T5/en
Priority to US13/812,893 priority patent/US9695711B2/en
Priority to CN201180034233.8A priority patent/CN102985660B/en
Publication of WO2012018553A2 publication Critical patent/WO2012018553A2/en
Publication of WO2012018553A3 publication Critical patent/WO2012018553A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • 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
    • 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 exhaust-gas turbocharger according to the preamble of claim 1.
  • the screws of a connecting device for the purpose of a direct screw connection are arranged, perpendicular to the joining surface between the housings, on a hole circle. The screws thus generate c lamping of the components perpendicular to the joining surface.
  • screws can be mounted easily and that screws can be used which have a hexagon socket and a so-called torx socket, which is a specific embodiment of a hexagon socket.
  • the advantage is attained that the assembly of the exhaust-gas turbocharger housing can be automated when implemented on the compressor and turbine sides, because the same screw-in direction is possible.
  • Subclaims 2 to 4 relate to advantageous refinements of the exhaust-gas turbocharger according to the invention.
  • Claims 5 and 6 define a bearing housing according to the invention as an independently marketable object.
  • figure 1 shows a schematically slightly simplified illustration of an exhaust-gas turbocharger according to the invention
  • figure 2 shows an enlarged illustration o f the bearing housing of the exhaust-gas turbocharger, mounted on the turbine housing, in the region of a joining surface,
  • figure 3 shows a perspective illustration of a bearing housing according to the invention.
  • figure 4 shows a perspective illustration of the assembled exhaust-gas turbocharger according to the invention.
  • the exhaust-gas turbocharger 1 has, according to figure 1, a turbine housing 2, a compressor housing 3 and a bearing housing 4.
  • the exhaust-gas turbocharger 1 according to the invention self-evidently also has all the other conventional components of modern turbochargers, but these are not described below or illustrated in figure 1 because they are not required for explaining the principles of the present invention.
  • the bearing housing 4 may be connected either to the turbine housing 2 or to the compressor housing 3, or to both the turbine housing 2 and also to the compressor housing 3, by means of a connecting device 5 which has firstly a multiplicity of screws, of which one screw 6 is illustrated representatively in figure 1.
  • the connecting device 5 has in the bearing housing 4 a number of screw holes 7 corresponding to the number of screws 6 used, and in the turbine housing 2 and/or in the compressor housing 3 a number of threaded holes 8 corresponding to the number of screws 6 used.
  • the screw hole 7 and the threaded hole 8 are illustrated representatively of all the screw holes and threaded holes provided.
  • a joining surface 9 is arranged between the bearing housing 4 and the turbine housing 2, which joining surface is perpendicular to the charger axis L.
  • the screw holes 7 and the threaded holes 8 and consequently the screws 6 inserted into said holes are inclined, which means that they are arranged at an acute angle a with respect to the joining surface 9. They are therefore not perpendicular to the joining surface 9 or axially parallel to the charger axis L, as in the prior art, but rather are at an angle, wherein the resulting acute angle is denoted by the reference symbol a.
  • Figure 2 shows that said angle a is defined between the common longitudinal axis S of the screw holes 7 and threaded holes 8 and of the screws 6 and the charger axis or bearing housing axis L.
  • Preferred angle dimensions for the angle a are accordingly between 25° and 65°.
  • a particularly preferred angle range is 45° ⁇ 15°, that is to say between 30° and 60°.
  • Said angled arrangement results preferably in a symmetrical arrangement, provided on an imaginary conical surface, of the axes of the screw holes 7 and threaded holes 8 and of the screws 6. This in turn yields the facility, explained in the introduction, for the radial and axial clamping of the components, the magnitude and direction of which clamping is dependent on the angle of inclination a of the axis S relative to the joining surface 9.
  • Figure 3 shows the bearing housing 4 according to the invention, as an independently marketable object, in a perspective illustration.
  • the bearing housing 4 has a fastening flange 10 which is provided with the screw holes, of which the screw holes 7 and T are illustrated by w ay of example for all the screw holes.
  • the screw holes 7, 7' are arranged in the fastening flange 10 so as to be spaced apart from one another in the circumferential direction.
  • the reference numeral 9 again indicates the joining surface or the contact surface against which, in the assembled state, the associated flange of the turbine housing 2 or the associated flange of the bearing housing 3 bears if both housings 2 and 3 are connected to the bearing housing 4 by means of a screw connection.
  • the bearing housing 4 would be provided only for a connection to the turbine housing 2 by means of the described connecting device 5 with screws 6, because screw holes 7, 7' are provided only in the fastening flange 10. If the compressor housing 3 is also to be connected to the bearing housing 4 by means of the connecting device 5 with screws 6, it would be necessary for a suitable number of screw holes to be provided correspondingly in the opposite fastening flange 10'.
  • Figure 3 also shows that, as a result of the inclination of the screw holes 7, 7', the screw contact surfaces 1 1 and 1 ⁇ are easily accessible despite the opposite fastening flange 10', such that said screw contact surfaces 1 1, 1 1 ' can be produced, for example countersunk, in a simple manner.
  • Figure 4 additionally shows the assembled exhaust-gas turbocharger 1 in a perspective illustration. Aside from the above written disclosure of the invention, reference is hereby made explicitly to the diagrammatic illustration thereof in figures 1 to 4.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

The invention relates to an exhaust-gas turbocharger (1) having a turbine housing (2), having a compressor housing (3), having a bearing housing (4) which has a bearing housing axis (L), and having a connecting device (5) for connecting the bearing housing (4) to the turbine housing (2) and/or to the compressor housing (3), which connecting device has a multiplicity of screws (6), which connecting device has in the bearing housing (4) a number of screw holes (7, 7') corresponding to the number of screws (6), and which connecting device has in the turbine housing (2) and/or in the compressor housing (3) a number of threaded holes (8) corresponding to the number of screws (6), wherein the screw holes (7, 7'), the threaded holes (8) and the screws (6) are arranged at an acute angle (α) with respect to a joining surface (9) between the bearing housing (4) and the turbine housing (2) or between the bearing housing (4) and the compressor housing (3).

Description

EXHAUST-GAS TURBOCHARGER DESCRIPTION The invention relates to an exhaust-gas turbocharger according to the preamble of claim 1.
In a generic exhaust-gas turbocharger, for a direct connection of the bearing housing to the turbine housing and/or to the compressor housing, the screws of a connecting device for the purpose of a direct screw connection are arranged, perpendicular to the joining surface between the housings, on a hole circle. The screws thus generate c lamping of the components perpendicular to the joining surface.
However, such a direct screw connection often yields problems in practice on account of poor accessibility of the screws, wherein such a connecting device is not possible in particular in the case of small hole circle diameters.
It is therefore an object of the present invention to provide an exhaust-gas turbocharger of the type specified in the preamble of claim 1 which permits reduced assembly expenditure for the connection of the bearing housing to the compressor housing and/or to the turbine housing.
Said object is achieved by means of the features of claim 1.
As a result of the inclination of the screws and threaded holes, and in the final assembled state of the screws, an arrangement of the screw holes, of the threaded holes and of the screws at an angle and diametrically on an imaginary conical surface is obtained instead of the above-explained arrangement at right angles on a cylindrical surface, which not only achieves the object but also offers the advantage that the screw head contact surface can be easily machined on account of the improved accessibility.
Furthermore, it is achieved that the screws can be mounted easily and that screws can be used which have a hexagon socket and a so-called torx socket, which is a specific embodiment of a hexagon socket.
Furthermore, the advantage is attained that the assembly of the exhaust-gas turbocharger housing can be automated when implemented on the compressor and turbine sides, because the same screw-in direction is possible.
Furthermore, the inclination of the threaded holes in the turbine housing and compressor housing yields a reduction in axial installation space.
Finally, the inclination makes clamping of the components in the axial and radial directions possible.
Subclaims 2 to 4 relate to advantageous refinements of the exhaust-gas turbocharger according to the invention. Claims 5 and 6 define a bearing housing according to the invention as an independently marketable object.
Further details, advantages and features of the present invention will emerge from the following description of exemplary embodiments on the basis of the drawing, in which:
figure 1 shows a schematically slightly simplified illustration of an exhaust-gas turbocharger according to the invention,
figure 2 shows an enlarged illustration o f the bearing housing of the exhaust-gas turbocharger, mounted on the turbine housing, in the region of a joining surface,
figure 3 shows a perspective illustration of a bearing housing according to the invention, and
figure 4 shows a perspective illustration of the assembled exhaust-gas turbocharger according to the invention.
The exhaust-gas turbocharger 1 has, according to figure 1, a turbine housing 2, a compressor housing 3 and a bearing housing 4. The exhaust-gas turbocharger 1 according to the invention self-evidently also has all the other conventional components of modern turbochargers, but these are not described below or illustrated in figure 1 because they are not required for explaining the principles of the present invention.
The bearing housing 4 may be connected either to the turbine housing 2 or to the compressor housing 3, or to both the turbine housing 2 and also to the compressor housing 3, by means of a connecting device 5 which has firstly a multiplicity of screws, of which one screw 6 is illustrated representatively in figure 1.
Furthermore, the connecting device 5 has in the bearing housing 4 a number of screw holes 7 corresponding to the number of screws 6 used, and in the turbine housing 2 and/or in the compressor housing 3 a number of threaded holes 8 corresponding to the number of screws 6 used. In figure 1, again, the screw hole 7 and the threaded hole 8 are illustrated representatively of all the screw holes and threaded holes provided.
As shown in figure 1, in the assembled state in the illustrated example of figure 1, a joining surface 9 is arranged between the bearing housing 4 and the turbine housing 2, which joining surface is perpendicular to the charger axis L. As is also shown in particular by figure 2, the screw holes 7 and the threaded holes 8 and consequently the screws 6 inserted into said holes are inclined, which means that they are arranged at an acute angle a with respect to the joining surface 9. They are therefore not perpendicular to the joining surface 9 or axially parallel to the charger axis L, as in the prior art, but rather are at an angle, wherein the resulting acute angle is denoted by the reference symbol a. Figure 2 shows that said angle a is defined between the common longitudinal axis S of the screw holes 7 and threaded holes 8 and of the screws 6 and the charger axis or bearing housing axis L. Preferred angle dimensions for the angle a are accordingly between 25° and 65°. A particularly preferred angle range is 45° ± 15°, that is to say between 30° and 60°.
Said angled arrangement results preferably in a symmetrical arrangement, provided on an imaginary conical surface, of the axes of the screw holes 7 and threaded holes 8 and of the screws 6. This in turn yields the facility, explained in the introduction, for the radial and axial clamping of the components, the magnitude and direction of which clamping is dependent on the angle of inclination a of the axis S relative to the joining surface 9.
Figure 3 shows the bearing housing 4 according to the invention, as an independently marketable object, in a perspective illustration. In the example, the bearing housing 4 has a fastening flange 10 which is provided with the screw holes, of which the screw holes 7 and T are illustrated by w ay of example for all the screw holes. Here, figure 3 shows that the screw holes 7, 7' are arranged in the fastening flange 10 so as to be spaced apart from one another in the circumferential direction. The reference numeral 9 again indicates the joining surface or the contact surface against which, in the assembled state, the associated flange of the turbine housing 2 or the associated flange of the bearing housing 3 bears if both housings 2 and 3 are connected to the bearing housing 4 by means of a screw connection. In principle, it is consequently possible for both the compressor housing 3 and the turbine housing 2, or alternatively only one of the two housings 2 or 3, to be connected to the bearing housing 4 by means of the associated screw connection 5.
In the case of figure 3, the bearing housing 4 would be provided only for a connection to the turbine housing 2 by means of the described connecting device 5 with screws 6, because screw holes 7, 7' are provided only in the fastening flange 10. If the compressor housing 3 is also to be connected to the bearing housing 4 by means of the connecting device 5 with screws 6, it would be necessary for a suitable number of screw holes to be provided correspondingly in the opposite fastening flange 10'.
Figure 3 also shows that, as a result of the inclination of the screw holes 7, 7', the screw contact surfaces 1 1 and 1 Γ are easily accessible despite the opposite fastening flange 10', such that said screw contact surfaces 1 1, 1 1 ' can be produced, for example countersunk, in a simple manner.
Figure 4 additionally shows the assembled exhaust-gas turbocharger 1 in a perspective illustration. Aside from the above written disclosure of the invention, reference is hereby made explicitly to the diagrammatic illustration thereof in figures 1 to 4.
LIST OF REFERENCE SYMBOLS
1 Exhaust-gas turbocharger
2 Turbine housing
3 Compressor housing
4 Bearing housing
5 Connecting device
6, 6', 6" Screws
7, 7' Screw holes
8 Threaded holes
9 Joining surface
10, 10' Fastening flanges
11, I V Screw contact surface
a Angle of inclination between the axis S and the charger or bearmg housing axis L
S Axis
L Charger axis / bearing housing axis (longitudinal axis of the exhaust-gas turbocharger 1 or bearing housing 4)

Claims

1. An exhaust-gas turbocharger (1)
having a turbine housing (2),
- having a compressor housing (3),
having a bearing housing (4) which has a bearing housing axis (L), and having a connecting device (5)
• for connecting the bearing housing (4) to the turbine housing (2) and/or to the compressor housing (3),
· which has a multiplicity of screws (6),
• which has in the bearing housing (4) a number of screw holes (7, 7') corresponding to the number of screws (6), and
• which has in the turbine housing (2) and/or in the compressor housing (3) a number of threaded holes (8) corresponding to the number of screws (6),
wherein
the screw holes (7, 7'), the threaded holes (8) and the screws (6) are arranged at an acute angle (a) with respect to the bearing housing axis (L).
2. The exhaust-gas turbocharger as claimed in claim 1, wherein the axes (S) of the screws (6), of the screw holes (7, 7') and of the tlireaded holes (8) are arranged symmetrically on an imaginary conical surface.
3. The exhaust-gas turbocharger as claimed in claim 1 or 2, wherein the angle (a) is approximately 25° to 65°, in particular 30° to 60°.
4. The exhaust-gas turbocharger as claimed in one of claims 1 to 3, wherein the screw holes (7, 7') have a machined screw contact surface (1 1 , I V).
5. A bearing housing (4) of an exhaust-gas turbocharger ( 1 ),
having at least one fastening flange (10, 10') which has an outwardly pointing joining surface (9), and
having a multiplicity of screw holes (7, T) which are arranged, spaced apart from one another in the circumferential direction, on the fastening flange ( 10, 10'),
wherein
the screw holes (7, 7') are arranged at an acute angle (a) with respect to the bearing housing axis ( L).
6. The bearing housing as claimed in claim 5, wherein the angle (a) is approximately 25° to 65°, in particular 30° to 60°.
PCT/US2011/044954 2010-08-03 2011-07-22 Exhaust-gas turbocharger Ceased WO2012018553A2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
KR1020137004072A KR102077747B1 (en) 2010-08-03 2011-07-22 Exhaust-gas turbocharger
JP2013523187A JP2013533429A (en) 2010-08-03 2011-07-22 Exhaust gas turbocharger
DE112011102593T DE112011102593T5 (en) 2010-08-03 2011-07-22 turbocharger
US13/812,893 US9695711B2 (en) 2010-08-03 2011-07-22 Exhaust-gas turbocharger
CN201180034233.8A CN102985660B (en) 2010-08-03 2011-07-22 Exhaust turbine supercharger

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010033200 2010-08-03
DE102010033200.3 2010-08-03

Publications (2)

Publication Number Publication Date
WO2012018553A2 true WO2012018553A2 (en) 2012-02-09
WO2012018553A3 WO2012018553A3 (en) 2012-04-26

Family

ID=45559974

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2011/044954 Ceased WO2012018553A2 (en) 2010-08-03 2011-07-22 Exhaust-gas turbocharger

Country Status (6)

Country Link
US (1) US9695711B2 (en)
JP (1) JP2013533429A (en)
KR (1) KR102077747B1 (en)
CN (1) CN102985660B (en)
DE (1) DE112011102593T5 (en)
WO (1) WO2012018553A2 (en)

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US10570778B2 (en) * 2017-09-11 2020-02-25 Ford Global Technologies, Llc Coupling system for turbocharger and emission control device
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Also Published As

Publication number Publication date
WO2012018553A3 (en) 2012-04-26
CN102985660A (en) 2013-03-20
US20130129502A1 (en) 2013-05-23
US9695711B2 (en) 2017-07-04
JP2013533429A (en) 2013-08-22
KR102077747B1 (en) 2020-02-14
DE112011102593T5 (en) 2013-05-08
CN102985660B (en) 2015-12-09
KR20130096244A (en) 2013-08-29

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