US20050123417A1 - Turbocharger assembly and method - Google Patents

Turbocharger assembly and method Download PDF

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Publication number
US20050123417A1
US20050123417A1 US10/728,907 US72890703A US2005123417A1 US 20050123417 A1 US20050123417 A1 US 20050123417A1 US 72890703 A US72890703 A US 72890703A US 2005123417 A1 US2005123417 A1 US 2005123417A1
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United States
Prior art keywords
turbocharger
turbine
assembly
turbine wheel
threaded portion
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.)
Abandoned
Application number
US10/728,907
Inventor
Kerry Alan DelVecchio
Paul William Reisdorf
Ulrich Hopmann
Frank Gerke
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Caterpillar Inc
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Caterpillar Inc
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Filing date
Publication date
Application filed by Caterpillar Inc filed Critical Caterpillar Inc
Priority to US10/728,907 priority Critical patent/US20050123417A1/en
Assigned to CATERPILLAR INC. reassignment CATERPILLAR INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GERKE, FRANK GEORGE, DELVECCHIO, KERRY ALAN, HOPMANN, ULRICH, REISDORF, PAUL WILLIAM
Publication of US20050123417A1 publication Critical patent/US20050123417A1/en
Abandoned legal-status Critical Current

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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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/025—Fixing blade carrying members on shafts
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/026—Shaft to shaft connections
    • 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
    • F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
    • F02B37/10—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump at least one pump being alternatively or simultaneously driven by exhaust and other drive, e.g. by pressurised fluid from a reservoir or an engine-driven pump
    • 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
    • F02B39/02—Drives of pumps; Varying pump drive gear ratio
    • F02B39/08—Non-mechanical drives, e.g. fluid drives having variable gear ratio
    • F02B39/10—Non-mechanical drives, e.g. fluid drives having variable gear ratio electric
    • 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 present invention is directed to a turbocharger assembly and, more particularly, to a turbocharger assembly that provides for removably connecting a turbine wheel assembly to a turbocharger drive.
  • Internal combustion engines such as, for example, diesel engines, gasoline engines, or natural gas engines may be operated to generate a power output.
  • the engine may be equipped with a turbocharged air induction system.
  • a turbocharged air induction system may include a turbocharger that compresses the air flowing into the engine to thereby force more air into a combustion chamber.
  • the increased supply of air allows for increased fuelling, which may result in increased power.
  • a turbocharged engine typically produces more power than the same engine without turbocharging.
  • a turbocharger may include a turbine wheel that is connected to a compressor. The expansion of hot exhaust gases over the turbine wheel drives the compressor wheel to force compressed air into a combustion chamber.
  • a typical turbocharger includes a housing, a shaft, a turbine wheel attached to one end of the shaft, and a compressor connected by threaded fastening to the other end of the shaft.
  • the turbine, shaft, and compressor may be assembled into the housing as described in U.S. Pat. No. 5,193,989 issued to Fleury et al. on Mar. 16, 1993.
  • the '989 patent to Fleury et al. describes assembly of a turbocharger having the turbine wheel permanently attached to the shaft. The shaft and turbine wheel may be inserted from one side of the housing and the compressor wheel may be fastened to the other end of the shaft.
  • turbocharger of Fleury et al. does not allow for the design flexibility required for more complex turbocharging systems that require additional components. Adding the additional components to the turbocharger systems of Fluery et al. may be difficult because the turbocharger components may only be assembled from one end of the turbocharger shaft. Additionally, the turbocharger of Fleury et al. may be too expensive to maintain when combined with more complex air induction systems because the turbine wheel and shaft are inseparable.
  • the turbocharger assembly of the present invention solves one or more of the problems set forth above.
  • a first aspect of the present disclosure is directed to a turbine assembly.
  • the turbine assembly includes a turbocharger drive having a first threaded portion and a turbine wheel assembly.
  • the turbine wheel assembly includes a turbine wheel and a second threaded portion adapted to engage the first threaded portion of the turbocharger drive.
  • a second aspect of the present disclosure is directed to a method of assembling a turbocharger.
  • the method includes inserting a drive into a main housing, wherein the turbocharger drive includes a first end having a first threaded portion and a second end.
  • a second threaded portion of a turbine wheel assembly is engaged with the first threaded portion of the turbocharger drive.
  • a compressor is connected to the second end of the turbocharger drive.
  • FIG. 1 is a cross-sectional illustration of a turbine assembly in accordance with an exemplary embodiment of the present invention.
  • FIG. 2 is a cross-sectional illustration of a turbine assembly in accordance with an exemplary embodiment of the present invention.
  • FIG. 3 is a cross-sectional illustration of a turbocharger in accordance with an exemplary embodiment of the present invention.
  • FIG. 4 is a diagrammatic and schematic illustration of an engine system in accordance with an exemplary embodiment of the present invention.
  • FIG. 1 An exemplary embodiment of a turbine wheel assembly 10 is illustrated in FIG. 1 .
  • the turbine wheel assembly 10 includes a turbine wheel 11 having a turbine wheel base 12 and a plurality of turbine blades 13 .
  • the plurality of turbine blades 13 may be disposed on the outer periphery of the turbine wheel base 12 and may be adapted to rotate the turbine wheel base 12 when driven by the expansion of hot exhaust gases.
  • the plurality of turbine blades 13 may be rigidly fixed to the turbine wheel base 12 using conventional means or they may be movable with respect to the turbine wheel base 12 such as, for example, by providing variable pitch turbine blades or variable geometry turbine blades.
  • the plurality of turbine blades 13 may also be integral with the turbine wheel base 12 .
  • the turbine wheel assembly 10 may also include a connecting means such as for example, a threaded portion 14 .
  • the threaded portion 14 may be integral to turbine wheel base 12 or may be connected to the base through any means known in the art such as, for example, inertia welding.
  • the threaded portion 14 may be adapted to transmit power from the turbine wheel assembly 10 to a corresponding connecting member.
  • the threaded portion 14 of the turbine wheel assembly 10 is adapted to engage a corresponding connecting means of a turbocharger drive 18 .
  • the connecting means is a threaded portion 16 .
  • the threaded portion 14 of turbine wheel assembly 10 has male threads and the threaded portion 16 of the turbocharger drive 18 has female threads.
  • the male threads of the turbine wheel assembly 10 may be engaged with the female threads to connect the turbine wheel assembly 10 to the turbocharger drive 18 .
  • the turbine wheel assembly 10 may alternatively have a female threaded portion adapted to engage a male threaded portion of the turbocharger drive 18 .
  • FIG. 2 Another exemplary embodiment of a turbine wheel assembly 10 is illustrated in FIG. 2 .
  • the turbine wheel assembly 10 of this embodiment includes a turbine wheel 11 and a stub shaft 20 having a threaded portion 22 .
  • the stub shaft 20 may be integral to turbine wheel base 12 or may be connected to turbine wheel base 12 by any manner known in the art such as, for example, inertia welding.
  • the stub shaft 20 may include a female threaded portion 22 adapted to engage a male threaded portion 16 located on the turbocharger drive 18 (referring to FIG. 1 ), thereby connecting the turbine wheel assembly 10 to the turbocharger drive 18 .
  • the stub shaft 20 may include a male threaded portion adapted to engage a female threaded portion located on the turbocharger drive 18 .
  • the turbine wheel assembly 10 may be incorporated in a turbocharger assembly.
  • An exemplary embodiment of a turbocharger 23 is illustrated in FIG. 3 .
  • the turbocharger 23 includes a stator housing 24 in which a pre-assembled drive assembly 26 may be inserted.
  • the pre-assembled drive assembly 26 may have a stator 28 and a rotor 29 held by end plate retainers 34 between bearings 30 .
  • the stator 28 , rotor 29 , end plate retainers 34 , and bearings 30 are assembled to the turbocharger drive 18 .
  • the pre-assembled drive assembly 26 may be adapted to generate power when the turbocharger drive 18 is rotated and direct the power to a crankshaft of an engine 46 (referring to FIG. 4 ) to which the turbocharger 23 is attached.
  • a turbine housing 40 is assembled to stator housing 24 to enclose turbine wheel assembly 10 .
  • the turbine housing 40 is adapted to direct hot expanding exhaust gases through a turbine exhaust inlet 41 to the plurality of turbine blades 13 disposed on the turbine wheel base 12 to cause the turbine wheel assembly 10 and associated turbocharger drive 18 to rotate. After passing through the turbine wheel assembly 10 , the exhaust gases are released to the atmosphere through a turbine exhaust outlet 42 .
  • a compressor assembly 37 may be connected to the other end of the turbocharger drive 18 and be adapted to rotate with the turbocharger drive 18 .
  • the compressor assembly 37 may include a compressor wheel base 38 and a plurality of compressor blades 39 disposed around the outer periphery of the compressor wheel base 38 .
  • Compressor assembly 37 may also include a stub shaft (not shown) having a fastening means such as for example, threads, similar to stub shaft 20 connected to turbine wheel 11 .
  • the stub shaft of compressor assembly 37 may be adapted to connect the compressor assembly 37 to the turbocharger drive 18 .
  • a compressor housing 43 may be assembled to the stator housing 24 that encloses compressor assembly 37 .
  • Compressor housing 43 is adapted to direct ambient air from a compressor air inlet 44 to the plurality of compressor blades 39 attached to the rotating compressor wheel base 38 .
  • the plurality of compressor blades 39 may be operable to compress the air and force the compressed air out of the turbocharger 23 through a compressor air outlet 45 (referring to FIG. 4 ).
  • the turbocharger 23 of the present disclosure may be used with an engine 46 in an engine assembly 48 .
  • the engine 46 may be a diesel engine, a gasoline engine, a natural gas engine, or any other engine known in the art.
  • Hot exhaust gases from the engine 46 are directed into the turbine exhaust inlet 41 where the gases drive the rotation of the turbine assembly 10 resulting in a corresponding rotation of compressor assembly 37 .
  • the rotation of compressor assembly 37 compresses inlet air and forces the compressed air into the engine 46 through compressor air outlet 45 .
  • the present disclosure provides a system and method that allows for design flexibility and low cost maintenance of a turbocharger 23 .
  • the turbocharger 23 of the present disclosure may be assembled from both ends of the turbocharger drive 18 .
  • the pre-assembled drive assembly 26 (having stator 28 , rotor 29 , end plate retainers 34 , bearings 30 , and turbocharger drive 18 ) is balanced and then inserted into stator housing 24 .
  • Turbine wheel assembly 10 is connected to one end of the turbocharger drive 18 by engaging threaded portion 14 of the turbine wheel assembly 10 with threaded portion 16 of the turbocharger drive 18 .
  • Turbine housing 40 is assembled to one side of the stator housing 24 and encloses the turbine wheel assembly 10 .
  • Compressor assembly 37 may be connected to the other end of the turbocharger drive 18 and enclosed by compressor housing 43 assembled to the other side of the stator housing 24 .
  • turbocharger 23 can be assembled from both sides of the turbocharger drive 18 , design flexibility is expanded. Design is no longer limited to components capable of assembly from only one direction. Likewise, methods of assembly are no longer limited to only one direction of assembly.
  • turbocharger 23 may be reduced by the ability to remove both the turbine wheel assembly 10 and the compressor assembly 37 from the turbocharger drive 18 .
  • replacement of a damaged turbine wheel required the entire turbocharger be taken apart.
  • Both turbine and compressor housings had to be removed and the compressor assembly had to be disconnected from the turbocharger drive.
  • the pre-assembled drive assembly had to be removed from the stator housing along with the turbine wheel and the turbocharger drive.
  • the pre-assembled drive assembly had to be separated from the turbocharger drive. Finally the turbine wheel and turbocharger drive could be replaced.
  • the maintenance process is simplified. For example, when replacing a broken or damaged turbine wheel assembly 10 , the turbine housing 40 is removed and the turbine wheel assembly 10 is detached. Not only is the process simplified saving time and labor cost, but part cost is also reduced.

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

Abstract

A turbine assembly is provided. The turbine assembly includes a turbocharger drive having a first threaded portion and a turbine wheel assembly. The turbine wheel assembly includes a turbine wheel and a second threaded portion adapted to engage the first threaded portion of the turbocharger drive. The turbine assembly may be utilized in a turbocharger assembly, wherein a compressor is connected to a second end of the turbocharger drive.

Description

    U.S. GOVERNMENT RIGHTS
  • This invention was made with government support under the terms of Contract No. DE-SC05-00OR-22810 awarded by the Department of Energy. The government may have certain rights in this invention.
    • TECHNICAL FIELD
  • The present invention is directed to a turbocharger assembly and, more particularly, to a turbocharger assembly that provides for removably connecting a turbine wheel assembly to a turbocharger drive.
    • BACKGROUND
  • Internal combustion engines such as, for example, diesel engines, gasoline engines, or natural gas engines may be operated to generate a power output. In order to maximize the power generated by the internal combustion engine, the engine may be equipped with a turbocharged air induction system.
  • A turbocharged air induction system may include a turbocharger that compresses the air flowing into the engine to thereby force more air into a combustion chamber. The increased supply of air allows for increased fuelling, which may result in increased power. A turbocharged engine typically produces more power than the same engine without turbocharging.
  • A turbocharger may include a turbine wheel that is connected to a compressor. The expansion of hot exhaust gases over the turbine wheel drives the compressor wheel to force compressed air into a combustion chamber. A typical turbocharger includes a housing, a shaft, a turbine wheel attached to one end of the shaft, and a compressor connected by threaded fastening to the other end of the shaft. The turbine, shaft, and compressor may be assembled into the housing as described in U.S. Pat. No. 5,193,989 issued to Fleury et al. on Mar. 16, 1993. The '989 patent to Fleury et al. describes assembly of a turbocharger having the turbine wheel permanently attached to the shaft. The shaft and turbine wheel may be inserted from one side of the housing and the compressor wheel may be fastened to the other end of the shaft.
  • However, the turbocharger of Fleury et al. does not allow for the design flexibility required for more complex turbocharging systems that require additional components. Adding the additional components to the turbocharger systems of Fluery et al. may be difficult because the turbocharger components may only be assembled from one end of the turbocharger shaft. Additionally, the turbocharger of Fleury et al. may be too expensive to maintain when combined with more complex air induction systems because the turbine wheel and shaft are inseparable.
  • The turbocharger assembly of the present invention solves one or more of the problems set forth above.
    • SUMMARY OF THE INVENTION
  • A first aspect of the present disclosure is directed to a turbine assembly. The turbine assembly includes a turbocharger drive having a first threaded portion and a turbine wheel assembly. The turbine wheel assembly includes a turbine wheel and a second threaded portion adapted to engage the first threaded portion of the turbocharger drive.
  • A second aspect of the present disclosure is directed to a method of assembling a turbocharger. The method includes inserting a drive into a main housing, wherein the turbocharger drive includes a first end having a first threaded portion and a second end. A second threaded portion of a turbine wheel assembly is engaged with the first threaded portion of the turbocharger drive. A compressor is connected to the second end of the turbocharger drive.
    • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a cross-sectional illustration of a turbine assembly in accordance with an exemplary embodiment of the present invention.
  • FIG. 2 is a cross-sectional illustration of a turbine assembly in accordance with an exemplary embodiment of the present invention.
  • FIG. 3 is a cross-sectional illustration of a turbocharger in accordance with an exemplary embodiment of the present invention.
  • FIG. 4 is a diagrammatic and schematic illustration of an engine system in accordance with an exemplary embodiment of the present invention.
    • DETAILED DESCRIPTION
  • An exemplary embodiment of a turbine wheel assembly 10 is illustrated in FIG. 1. The turbine wheel assembly 10 includes a turbine wheel 11 having a turbine wheel base 12 and a plurality of turbine blades 13. The plurality of turbine blades 13 may be disposed on the outer periphery of the turbine wheel base 12 and may be adapted to rotate the turbine wheel base 12 when driven by the expansion of hot exhaust gases. The plurality of turbine blades 13 may be rigidly fixed to the turbine wheel base 12 using conventional means or they may be movable with respect to the turbine wheel base 12 such as, for example, by providing variable pitch turbine blades or variable geometry turbine blades. The plurality of turbine blades 13 may also be integral with the turbine wheel base 12.
  • The turbine wheel assembly 10 may also include a connecting means such as for example, a threaded portion 14. The threaded portion 14 may be integral to turbine wheel base 12 or may be connected to the base through any means known in the art such as, for example, inertia welding. The threaded portion 14 may be adapted to transmit power from the turbine wheel assembly 10 to a corresponding connecting member.
  • In the embodiment of FIG. 1, the threaded portion 14 of the turbine wheel assembly 10 is adapted to engage a corresponding connecting means of a turbocharger drive 18. In this embodiment, the connecting means is a threaded portion 16. When the threaded portion 14 of the turbine wheel assembly 10 is engaged with the threaded portion 16 of the turbocharger drive 18, the turbine wheel assembly 10 is connected to the turbocharger drive 18 so that a rotation of the turbine wheel assembly 10 will cause a corresponding rotation of the turbocharger drive 18.
  • In the exemplary embodiment of FIG. 1, the threaded portion 14 of turbine wheel assembly 10 has male threads and the threaded portion 16 of the turbocharger drive 18 has female threads. The male threads of the turbine wheel assembly 10 may be engaged with the female threads to connect the turbine wheel assembly 10 to the turbocharger drive 18. The turbine wheel assembly 10 may alternatively have a female threaded portion adapted to engage a male threaded portion of the turbocharger drive 18.
  • Another exemplary embodiment of a turbine wheel assembly 10 is illustrated in FIG. 2. The turbine wheel assembly 10 of this embodiment includes a turbine wheel 11 and a stub shaft 20 having a threaded portion 22. The stub shaft 20 may be integral to turbine wheel base 12 or may be connected to turbine wheel base 12 by any manner known in the art such as, for example, inertia welding. The stub shaft 20 may include a female threaded portion 22 adapted to engage a male threaded portion 16 located on the turbocharger drive 18 (referring to FIG. 1), thereby connecting the turbine wheel assembly 10 to the turbocharger drive 18. Alternatively, the stub shaft 20 may include a male threaded portion adapted to engage a female threaded portion located on the turbocharger drive 18.
  • It is contemplated that the turbine wheel assembly 10 may be incorporated in a turbocharger assembly. An exemplary embodiment of a turbocharger 23 is illustrated in FIG. 3. In this embodiment, the turbocharger 23 includes a stator housing 24 in which a pre-assembled drive assembly 26 may be inserted.
  • The pre-assembled drive assembly 26 may have a stator 28 and a rotor 29 held by end plate retainers 34 between bearings 30. The stator 28, rotor 29, end plate retainers 34, and bearings 30 are assembled to the turbocharger drive 18. The pre-assembled drive assembly 26 may be adapted to generate power when the turbocharger drive 18 is rotated and direct the power to a crankshaft of an engine 46 (referring to FIG. 4) to which the turbocharger 23 is attached.
  • A turbine housing 40 is assembled to stator housing 24 to enclose turbine wheel assembly 10. The turbine housing 40 is adapted to direct hot expanding exhaust gases through a turbine exhaust inlet 41 to the plurality of turbine blades 13 disposed on the turbine wheel base 12 to cause the turbine wheel assembly 10 and associated turbocharger drive 18 to rotate. After passing through the turbine wheel assembly 10, the exhaust gases are released to the atmosphere through a turbine exhaust outlet 42.
  • A compressor assembly 37 may be connected to the other end of the turbocharger drive 18 and be adapted to rotate with the turbocharger drive 18. The compressor assembly 37 may include a compressor wheel base 38 and a plurality of compressor blades 39 disposed around the outer periphery of the compressor wheel base 38. Compressor assembly 37 may also include a stub shaft (not shown) having a fastening means such as for example, threads, similar to stub shaft 20 connected to turbine wheel 11. The stub shaft of compressor assembly 37 may be adapted to connect the compressor assembly 37 to the turbocharger drive 18.
  • A compressor housing 43 may be assembled to the stator housing 24 that encloses compressor assembly 37. Compressor housing 43 is adapted to direct ambient air from a compressor air inlet 44 to the plurality of compressor blades 39 attached to the rotating compressor wheel base 38. The plurality of compressor blades 39 may be operable to compress the air and force the compressed air out of the turbocharger 23 through a compressor air outlet 45 (referring to FIG. 4).
  • As illustrated in FIG. 4, the turbocharger 23 of the present disclosure may be used with an engine 46 in an engine assembly 48. The engine 46 may be a diesel engine, a gasoline engine, a natural gas engine, or any other engine known in the art. Hot exhaust gases from the engine 46 are directed into the turbine exhaust inlet 41 where the gases drive the rotation of the turbine assembly 10 resulting in a corresponding rotation of compressor assembly 37. The rotation of compressor assembly 37 compresses inlet air and forces the compressed air into the engine 46 through compressor air outlet 45.
  • Industrial Applicability
  • As will be apparent from the foregoing description, the present disclosure provides a system and method that allows for design flexibility and low cost maintenance of a turbocharger 23.
  • The turbocharger 23 of the present disclosure may be assembled from both ends of the turbocharger drive 18. The pre-assembled drive assembly 26 (having stator 28, rotor 29, end plate retainers 34, bearings 30, and turbocharger drive 18) is balanced and then inserted into stator housing 24. Turbine wheel assembly 10 is connected to one end of the turbocharger drive 18 by engaging threaded portion 14 of the turbine wheel assembly 10 with threaded portion 16 of the turbocharger drive 18. Turbine housing 40 is assembled to one side of the stator housing 24 and encloses the turbine wheel assembly 10. Compressor assembly 37 may be connected to the other end of the turbocharger drive 18 and enclosed by compressor housing 43 assembled to the other side of the stator housing 24.
  • Because the turbocharger 23 can be assembled from both sides of the turbocharger drive 18, design flexibility is expanded. Design is no longer limited to components capable of assembly from only one direction. Likewise, methods of assembly are no longer limited to only one direction of assembly.
  • In addition to increased design flexibility, maintenance costs of the turbocharger 23 may be reduced by the ability to remove both the turbine wheel assembly 10 and the compressor assembly 37 from the turbocharger drive 18. For example, when maintaining a turbocharger having a turbine wheel permanently secured to a turbocharger drive, replacement of a damaged turbine wheel required the entire turbocharger be taken apart. Both turbine and compressor housings had to be removed and the compressor assembly had to be disconnected from the turbocharger drive. The pre-assembled drive assembly had to be removed from the stator housing along with the turbine wheel and the turbocharger drive. The pre-assembled drive assembly had to be separated from the turbocharger drive. Finally the turbine wheel and turbocharger drive could be replaced.
  • With the turbine wheel assembly 10 detachable from the turbocharger drive 18 as described in the present disclosure, the maintenance process is simplified. For example, when replacing a broken or damaged turbine wheel assembly 10, the turbine housing 40 is removed and the turbine wheel assembly 10 is detached. Not only is the process simplified saving time and labor cost, but part cost is also reduced.
  • It will be apparent to those skilled in the art that various modifications and variations can be made in the turbine wheel assembly 10 of the present disclosure without departing from the scope of the invention. Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. It is intended that the specification and examples be considered as exemplary only, with a true scope of the invention being indicated by the following claims and their equivalents.

Claims (21)

1. A turbine assembly, comprising:
a turbocharger drive having a first threaded portion; and
a turbine wheel assembly having a turbine wheel and a second threaded portion adapted to engage the first threaded portion of the turbocharger drive.
2. The turbine assembly of claim 1, wherein the turbine wheel assembly includes a turbine shaft having a first end and a second end, the first end of the turbine shaft having the second threaded portion and the second end of the turbine shaft being connected to the turbine wheel.
3. The turbine assembly of claim 1, wherein the second threaded portion of the turbine wheel assembly has male threads.
4. The turbine assembly of claim 1, wherein the second threaded portion of the turbine wheel assembly has female threads.
5. The turbine assembly of claim 1, further including a turbine housing enclosing the turbine wheel assembly.
6. The turbine assembly of claim 5, further including at least one bearing operatively connecting the turbocharger drive to the housing.
7. The turbine assembly of claim 2, wherein the second end of the turbine shaft is inertia welded to the turbine wheel.
8. The turbine assembly of claim 1, further including:
a turbine wheel base; and
a plurality of turbine blades disposed around the outer periphery of the turbine wheel base.
9. A method of assembling a turbocharger comprising:
inserting a turbocharger drive into a main housing, wherein the turbocharger drive includes a first end having a first threaded portion and a second end;
engaging a second threaded portion of a turbine wheel assembly with the first threaded portion of the turbocharger drive; and
connecting a compressor to the second end of the turbocharger drive.
10. The method of claim 9, further including:
pre-assembling the turbocharger drive before inserting the turbocharger drive into the main housing, wherein pre-assembling the turbocharger drive includes:
installing a shaft through a rotor; and
balancing the rotor.
11. The method of claim 9, further including:
attaching a turbine housing to the main housing thereby enclosing the turbine wheel assembly; and
attaching a compressor housing to the main housing thereby enclosing the compressor.
12. A turbocharger, comprising:
a housing assembly;
a turbocharger drive rotatingly disposed in the housing assembly, the turbocharger drive including a first end having a first threaded portion and a second end;
a turbine wheel assembly having a turbine wheel and a second threaded portion adapted to engage the first threaded portion on the turbocharger drive; and
a compressor connected to the second end of the turbocharger drive.
13. The turbocharger of claim 12, wherein the turbine wheel assembly includes a shaft having a first end and a second end, the first end of the shaft having the second threaded portion and the second end of the shaft being connected to the turbine wheel.
14. The turbocharger of claim 12, wherein the second threaded portion of the turbine wheel assembly has male threads.
15. The turbocharger of claim 12, wherein the second threaded portion of the turbine wheel assembly has female threads.
16. The turbocharger of claim 12, wherein the compressor includes a third threaded portion adapted to engage a fourth threaded portion disposed on the second end of the turbocharger drive.
17. The turbocharger of claim 13, wherein the compressor includes a shaft having a first end and a second end, the first end of the shaft having the third threaded portion and the second end connected to the compressor.
18. The turbocharger of claim 12, wherein the housing assembly includes:
a main housing enclosing the turbocharger drive;
a compressor housing enclosing the compressor; and
a turbine housing enclosing the turbine assembly.
19. The turbocharger of claim 12, wherein the turbocharger drive includes:
a shaft; and
a rotor operably connected to the shaft.
20. A turbocharger, comprising:
a housing assembly;
a turbocharger drive rotatingly disposed in the housing assembly;
a turbine wheel assembly having a turbine wheel and a means for removably connecting the turbine wheel to the turbocharger drive; and
a compressor connected to the second end.
21. The turbocharger of claim 20, wherein the turbine wheel assembly includes a shaft having a first end and a second end, the first end of the shaft having the connecting means and the second end of the shaft being connected to the turbine wheel.
US10/728,907 2003-12-08 2003-12-08 Turbocharger assembly and method Abandoned US20050123417A1 (en)

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US20060127242A1 (en) * 2004-12-09 2006-06-15 Martin Steve P Turbocharger with removable wheel shrouds and/or removable seals
GB2477564A (en) * 2010-02-09 2011-08-10 George Michael Morrell Turbine wheels with a female tool engagement member
WO2014016016A1 (en) * 2012-07-24 2014-01-30 Schaeffler Technologies AG & Co. KG Device and method for joining a shaft-hub connection of a rotor
WO2014032825A1 (en) * 2012-08-28 2014-03-06 Schaeffler Technologies AG & Co. KG Turbine rotor of an exhaust-gas turbocharger
US20140147306A1 (en) * 2011-06-08 2014-05-29 Mitsubishi Heavy Industries, Ltd. Structure and method for adjusting balance of turbocharging device incorporating electric motor
US20140186745A1 (en) * 2011-08-24 2014-07-03 Borgwarner Inc. Air feed device for a fuel cell
US20160003140A1 (en) * 2013-02-22 2016-01-07 Ecomotors, Inc. Electric rotor fit onto a turbomachine shaft
US20160115824A1 (en) * 2014-02-19 2016-04-28 Mitsubishi Heavy Industries Compressor Corporation Rotary system
EP3081746A4 (en) * 2013-12-11 2016-12-21 Mitsubishi Heavy Ind Ltd Rotating body and method for manufacturing rotating body
US20180094646A1 (en) * 2016-10-05 2018-04-05 Borgwarner Inc. Assembly method for the connection of a turbine wheel to a shaft
CN108020869A (en) * 2017-12-30 2018-05-11 无锡烨隆精密机械有限公司 A kind of volute threaded hole detection device
WO2020114662A1 (en) * 2018-12-06 2020-06-11 Robert Bosch Gmbh Rotor for an electric drive machine for driving a compressor, a turbine or a charger shaft of a turbocharger, and turbocharger comprising an electric drive machine and such a rotor

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Cited By (18)

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Publication number Priority date Publication date Assignee Title
US20060127242A1 (en) * 2004-12-09 2006-06-15 Martin Steve P Turbocharger with removable wheel shrouds and/or removable seals
GB2477564A (en) * 2010-02-09 2011-08-10 George Michael Morrell Turbine wheels with a female tool engagement member
US20140147306A1 (en) * 2011-06-08 2014-05-29 Mitsubishi Heavy Industries, Ltd. Structure and method for adjusting balance of turbocharging device incorporating electric motor
US10069154B2 (en) * 2011-08-24 2018-09-04 Borgwarner Inc. Air feed device for a fuel cell
US20140186745A1 (en) * 2011-08-24 2014-07-03 Borgwarner Inc. Air feed device for a fuel cell
WO2014016016A1 (en) * 2012-07-24 2014-01-30 Schaeffler Technologies AG & Co. KG Device and method for joining a shaft-hub connection of a rotor
WO2014032825A1 (en) * 2012-08-28 2014-03-06 Schaeffler Technologies AG & Co. KG Turbine rotor of an exhaust-gas turbocharger
US20160003140A1 (en) * 2013-02-22 2016-01-07 Ecomotors, Inc. Electric rotor fit onto a turbomachine shaft
US10309300B2 (en) * 2013-02-22 2019-06-04 Borgwarner Inc. Electric rotor fit onto a turbomachine shaft
EP3081746A4 (en) * 2013-12-11 2016-12-21 Mitsubishi Heavy Ind Ltd Rotating body and method for manufacturing rotating body
US10578116B2 (en) 2013-12-11 2020-03-03 Mitsubishi Heavy Industries, Ltd. Rotational body and method for manufacturing the same
US10227894B2 (en) * 2014-02-19 2019-03-12 Mitsubishi Heavy Industries Compressor Corporation Rotary system
US20160115824A1 (en) * 2014-02-19 2016-04-28 Mitsubishi Heavy Industries Compressor Corporation Rotary system
US20180094646A1 (en) * 2016-10-05 2018-04-05 Borgwarner Inc. Assembly method for the connection of a turbine wheel to a shaft
US10451085B2 (en) * 2016-10-05 2019-10-22 Borgwarner Inc. Assembly methods for the connection of a turbine wheel to a shaft
CN108020869A (en) * 2017-12-30 2018-05-11 无锡烨隆精密机械有限公司 A kind of volute threaded hole detection device
WO2020114662A1 (en) * 2018-12-06 2020-06-11 Robert Bosch Gmbh Rotor for an electric drive machine for driving a compressor, a turbine or a charger shaft of a turbocharger, and turbocharger comprising an electric drive machine and such a rotor
US11466610B2 (en) 2018-12-06 2022-10-11 Robert Bosch Gmbh Rotor for an electric drive machine for driving a compressor, a turbine or a charger shaft of a turbocharger, and turbocharger comprising an electric drive machine and such a rotor

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