EP1500788A1 - Volute à double flux - Google Patents

Volute à double flux Download PDF

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Publication number
EP1500788A1
EP1500788A1 EP03016529A EP03016529A EP1500788A1 EP 1500788 A1 EP1500788 A1 EP 1500788A1 EP 03016529 A EP03016529 A EP 03016529A EP 03016529 A EP03016529 A EP 03016529A EP 1500788 A1 EP1500788 A1 EP 1500788A1
Authority
EP
European Patent Office
Prior art keywords
twin
turbine housing
shells
housing according
partition wall
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.)
Withdrawn
Application number
EP03016529A
Other languages
German (de)
English (en)
Inventor
Hartmut Claus
Michael Mayer
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 EP03016529A priority Critical patent/EP1500788A1/fr
Priority to US10/897,727 priority patent/US20050019158A1/en
Publication of EP1500788A1 publication Critical patent/EP1500788A1/fr
Withdrawn legal-status Critical Current

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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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/026—Scrolls for radial machines or engines
    • 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

Definitions

  • the present invention relates to a twin-flow turbine housing according to the preamble of claim 1.
  • turbines such as the turbine part of a turbocharger for Motor vehicles to use turbine housing of various kinds.
  • turbine housings made of cast iron have a helical inlet space for the combustion gases from the engine be supplied via a manifold to the turbine part of a turbocharger, from where they then For example, by an annular gap, which has a mechanism for varying the Flow geometry may be supplied to the turbine wheel.
  • the helical inlet space surrounds the actual turbine chamber and forms with this together the turbine housing in which the turbine wheel and the mechanism are housed for geometry variation.
  • the turbine housing made of sheet metal, advantageously in double-walled construction, on the one hand to save weight, but above all, what It is more important to over-cool the exhaust gases of the engine when the turbocharger is cold Prevent, as the downstream catalyst through the exhaust gases as soon as possible Operating temperature must be heated to achieve its full effect.
  • the present invention is therefore the object of a twin turbine housing Manufacture with reasonable effort and at reasonable cost from sheet metal.
  • a twin flow turbine housing according to the present invention may Have half shells, which consist of sheet metal.
  • a twin flow turbine housing according to the present invention may Furthermore, have a partition made of sheet metal
  • twin-flow turbine casing In a twin-flow turbine casing according to the present invention the two half-shells and optionally the partition wall are welded together.
  • the Partition and the half shells matched outer contours.
  • the outer contours of the half-shells lying in the parting plane bent edges have, which are welded together.
  • the half-shells have circular inner contours, at which lying in the parting plane bent edges are formed, which like the outer contours by means of notches and Fortroisn and welding are connectable.
  • twin-flow turbine casing In a twin-flow turbine casing according to the present invention the two inlet channels to a bypass line leading bypass openings and have that this bypass line is divided by an extension of the partition into two partial bypasses is.
  • FIG 1 is a conventional twin turbine engine casing for a turbocharger shown. Such twin housings are used in relatively strong engines and This is done by the exhaust gases of one group of cylinders from the exhaust gases of another group to separate from cylinders.
  • a cylinder may have a plurality of valves and that these valves a certain, for example, controlled by the camshaft Subject opening and closing cycle, with different exhaust valves of the same Cylinders open at different times to gases under different pressure to let out.
  • Fig. 1 is a computer drawing of a known modern one Twin turbine housing 1 for the two separate inlet channels 2 and 3 to one single turbine wheel, not shown, which, as explained above, one Implementation of turbochargers for more powerful engines corresponds.
  • FIG. 2 shows a twin-flow turbine housing (the term “twin”) on the presence of two inlet channels, at which, seen from the outside, only a single inlet duct appears to be present, but in reality is, as in Fig. 2 and 3, the inlet channel of this housing through a partition wall 18 in two axially adjacent parts 13a and 14a divided, thereby two operationally from each other completely separate inlet channels arise.
  • twin twin-flow turbine housing
  • the twin turbine housing of Fig. 2 consists of a double-walled structure, wherein the division into two separate inlet channels only affects the inner housing.
  • the Outer housing consists of two parts 12 and 15 which are connected together at 21.
  • the inner housing consists of two half shells 13 and 14 whose outer edges 20 and 20 ' are bent parallel to the parting surface A (see Fig. 3) and thus welded together can be.
  • the housing of FIG. 2 also has two connection flanges 11 and 16 for connection the catalyst or to the central housing of the turbocharger.
  • said partition Before welding, however, between the two half-shells 13 and 14 a Dividing wall 18 placed, said partition has an outer contour 18 ', with the mutually congruent outer contours 13 'and 14' of the two half-shells 13 and 14th matches.
  • edge portions 31 of the half-shells 13 and 14 may also have notches and extensions be formed as in the outdoor areas.
  • openings 17 and 17 ' are formed on the half-shells 13 and 14'. intended to complement each other in a circle and to divide Bypasses are provided, these openings to one, through a with the openings 17, 17 'welded tube 17 "formed bypass line 22 lead, by means of a Folding valve 19 by means of a controllable from outside the housing lever 23rd is lockable.
  • the partition wall 18 has a continuation 18 ', which projects into the bypass line and this follows up to the seat of the valve 19.
  • the bypass pipe 17 "also of two Half shells and the continuation 18 'of the partition wall 18 further extensions 30th have in notches of bent, axially extending edges of the half-shells of Tube 17 "intervene and are welded.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
EP03016529A 2003-07-23 2003-07-23 Volute à double flux Withdrawn EP1500788A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP03016529A EP1500788A1 (fr) 2003-07-23 2003-07-23 Volute à double flux
US10/897,727 US20050019158A1 (en) 2003-07-23 2004-07-23 Twin flow turbine housing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03016529A EP1500788A1 (fr) 2003-07-23 2003-07-23 Volute à double flux

Publications (1)

Publication Number Publication Date
EP1500788A1 true EP1500788A1 (fr) 2005-01-26

Family

ID=33483922

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03016529A Withdrawn EP1500788A1 (fr) 2003-07-23 2003-07-23 Volute à double flux

Country Status (2)

Country Link
US (1) US20050019158A1 (fr)
EP (1) EP1500788A1 (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009015353A1 (de) * 2009-03-27 2010-09-30 Bosch Mahle Turbo Systems Gmbh & Co. Kg Ladeeinrichtung
US10436069B2 (en) 2017-01-30 2019-10-08 Garrett Transportation I Inc. Sheet metal turbine housing with biaxial volute configuration
US10472988B2 (en) 2017-01-30 2019-11-12 Garrett Transportation I Inc. Sheet metal turbine housing and related turbocharger systems
US10494955B2 (en) 2017-01-30 2019-12-03 Garrett Transportation I Inc. Sheet metal turbine housing with containment dampers
US10544703B2 (en) 2017-01-30 2020-01-28 Garrett Transportation I Inc. Sheet metal turbine housing with cast core
US10690144B2 (en) 2017-06-27 2020-06-23 Garrett Transportation I Inc. Compressor housings and fabrication methods
US11732729B2 (en) 2021-01-26 2023-08-22 Garrett Transportation I Inc Sheet metal turbine housing

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004042127B4 (de) * 2004-08-30 2006-07-13 Daimlerchrysler Ag Rotor-Stator-Vorrichtung mit Anstreifbelag, Verfahren zu deren Herstellung sowie Verwendung
JP2010025104A (ja) 2008-07-16 2010-02-04 Borgwarner Inc 後処理装置の受動的暖機制御用熱操作バイパス弁
CN102439269A (zh) * 2009-04-21 2012-05-02 博格华纳公司 用于改善车辆系统中的后处理装置的起燃或再生行为的方法
DE102010011375A1 (de) 2010-03-12 2011-09-15 Bosch Mahle Turbo Systems Gmbh & Co. Kg Turbinen-/Verdichtergehäuse
JP6126246B2 (ja) * 2013-12-27 2017-05-10 三菱重工業株式会社 タービンハウジング

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2801043A (en) * 1954-08-24 1957-07-30 Thompson Prod Inc Turbine supercharger
GB1199158A (en) * 1966-11-25 1970-07-15 Cav Ltd Casings for Radial Flow Fluid Turbines e.g. of Turbo-Superchargers for I.C. Engines
GB1263932A (en) * 1969-06-27 1972-02-16 Cav Ltd Turbo superchargers
DE3232925A1 (de) * 1981-10-14 1983-04-28 Wallace Murray Corp., 10171 New York, N.Y. Turbolader mit unterteiltem turbinengehaeuse
EP0204509A1 (fr) * 1985-05-29 1986-12-10 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Bâche spirale pour une turbosoufflante
EP0281345A1 (fr) * 1987-03-02 1988-09-07 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Carter de turbine pour turbocompresseur de suralimentation
DE10218436C1 (de) * 2002-04-25 2003-08-14 Benteler Automobiltechnik Gmbh Abgasturbine für einen Turbolader

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6267237A (ja) * 1985-09-18 1987-03-26 Hitachi Ltd 二流路型排気駆動タ−ボチヤ−ジヤ

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2801043A (en) * 1954-08-24 1957-07-30 Thompson Prod Inc Turbine supercharger
GB1199158A (en) * 1966-11-25 1970-07-15 Cav Ltd Casings for Radial Flow Fluid Turbines e.g. of Turbo-Superchargers for I.C. Engines
GB1263932A (en) * 1969-06-27 1972-02-16 Cav Ltd Turbo superchargers
DE3232925A1 (de) * 1981-10-14 1983-04-28 Wallace Murray Corp., 10171 New York, N.Y. Turbolader mit unterteiltem turbinengehaeuse
EP0204509A1 (fr) * 1985-05-29 1986-12-10 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Bâche spirale pour une turbosoufflante
EP0281345A1 (fr) * 1987-03-02 1988-09-07 Ishikawajima-Harima Jukogyo Kabushiki Kaisha Carter de turbine pour turbocompresseur de suralimentation
DE10218436C1 (de) * 2002-04-25 2003-08-14 Benteler Automobiltechnik Gmbh Abgasturbine für einen Turbolader

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009015353A1 (de) * 2009-03-27 2010-09-30 Bosch Mahle Turbo Systems Gmbh & Co. Kg Ladeeinrichtung
US10436069B2 (en) 2017-01-30 2019-10-08 Garrett Transportation I Inc. Sheet metal turbine housing with biaxial volute configuration
US10472988B2 (en) 2017-01-30 2019-11-12 Garrett Transportation I Inc. Sheet metal turbine housing and related turbocharger systems
US10494955B2 (en) 2017-01-30 2019-12-03 Garrett Transportation I Inc. Sheet metal turbine housing with containment dampers
US10544703B2 (en) 2017-01-30 2020-01-28 Garrett Transportation I Inc. Sheet metal turbine housing with cast core
US11035254B2 (en) 2017-01-30 2021-06-15 Garrett Transportation I Inc Sheet metal turbine housing with cast core
US10690144B2 (en) 2017-06-27 2020-06-23 Garrett Transportation I Inc. Compressor housings and fabrication methods
US11732729B2 (en) 2021-01-26 2023-08-22 Garrett Transportation I Inc Sheet metal turbine housing

Also Published As

Publication number Publication date
US20050019158A1 (en) 2005-01-27

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