WO2009068137A1 - Dispositif directeur pour une turbine d'un turbocompresseur - Google Patents

Dispositif directeur pour une turbine d'un turbocompresseur Download PDF

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Publication number
WO2009068137A1
WO2009068137A1 PCT/EP2008/008558 EP2008008558W WO2009068137A1 WO 2009068137 A1 WO2009068137 A1 WO 2009068137A1 EP 2008008558 W EP2008008558 W EP 2008008558W WO 2009068137 A1 WO2009068137 A1 WO 2009068137A1
Authority
WO
WIPO (PCT)
Prior art keywords
bearing housing
turbine
sliding wall
exhaust gas
housing
Prior art date
Application number
PCT/EP2008/008558
Other languages
German (de)
English (en)
Inventor
Stefan Ortmann
Original Assignee
Bayerische Motoren Werke Aktiengesellschaft
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 Bayerische Motoren Werke Aktiengesellschaft filed Critical Bayerische Motoren Werke Aktiengesellschaft
Priority to EP08802852A priority Critical patent/EP2212523A1/fr
Publication of WO2009068137A1 publication Critical patent/WO2009068137A1/fr

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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins

Definitions

  • the invention relates to a distributor for a turbine of an exhaust gas turbocharger with the features of the preamble of patent claim 1.
  • the operating behavior of the exhaust-gas turbocharger is determined via an adjustment unit, a so-called distributor, or a variable exhaust-gas throttle on the turbine side.
  • the adjustment basically consists of adjustable vanes, which are pivotally mounted between two sliding plates.
  • the diffuser is usually secured by a frictional connection between the bearing housing and the turbine housing in the axial direction.
  • the nozzle is positively connected against rotation by at least one circumferential Vermospin with the turbine housing.
  • a further embodiment is known, for example, from the European patent EP 1 574 673 B1.
  • the diffuser is screwed through a hollow, exhaust-carrying central screw assembly in the turbine housing.
  • pins are provided, which are inserted into corresponding holes in the nozzle and the turbine housing.
  • a spring element is arranged between the nozzle and the turbine housing.
  • a temperature-dependent deformation of the turbine housing causes a deformation of the nozzle, which can lead to a malfunction.
  • the axial improvement of the diffuser depends on the deformation of the bearing housing, turbine housing, diffuser and its tolerance chain.
  • the axial compression of the diffuser is deformation-dependent on the bearing housing, the turbine housing and the diffuser itself, as well as their different thermal expansion coefficients.
  • the object of the present invention is o. G. To avoid disadvantages.
  • the embodiment according to claim 2 corresponds to a first particularly preferred embodiment.
  • the embodiment according to claim 3 corresponds to a second particularly preferred embodiment.
  • the embodiment according to claim 4 is an advantageous development of the second particularly preferred embodiment.
  • Fig. 1 shows a plan view of an inventive, three-dimensional illustrated nozzle.
  • Fig. 2 shows a plan view of the nozzle according to the invention, installed in a turbine housing.
  • Fig. 3 shows a section through a first, particularly preferred
  • Fig. 4 shows a section through a second, particularly preferred
  • the guide apparatus 1 consists essentially of two, spaced over four spacer bolts 4, largely annular and mutually parallel sliding walls 5, 6, between which a plurality of guide vanes 7 (three are quantified ) are arranged pivotably.
  • the distributor 1 with four screws 8 can be screwed to a bearing housing 1 "of an exhaust gas turbocharger shown in FIG. 2.
  • Fig. 3 shows a section through a first particularly preferred embodiment of an inventively designed exhaust gas turbocharger 3. Since the exhaust gas turbocharger 3 is constructed largely rotationally symmetrical, only one half is shown.
  • the distributor 1 is arranged between the turbine housing 1 'and the bearing housing 1 ", and a guide vane 7 is pivotally arranged between the turbine housing-side sliding wall 5 and the bearing housing-side sliding wall 6.
  • the guide vane 7 can be pivoted by an adjusting mechanism 14.
  • the adjusting mechanism 14 does not become since it is known from the prior art, according to the invention, the bearing housing-side sliding wall 6 is screwed to the bearing housing 1 "with the screw 8.
  • the sliding wall 6 has a through hole 9, which corresponds to a threaded bore 10 in the bearing housing 1 "Since the diffuser 1 is screwed to the bearing housing 1", in this first particularly preferred embodiment, an anti-twist protection of the guide apparatus 1 can be dispensed with.
  • the diffuser 1 is installed biased in the region of the turbine 2 by a spring element 13.
  • the spring element 13 is particularly preferably a plate spring.
  • FIG. 4 shows a section through a second particularly preferred exemplary embodiment of an exhaust gas turbocharger 3 designed according to the invention.
  • Fig. 4 shows substantially the same geometric relationships as in Fig. 3, but in this second particularly preferred embodiment, the nozzle 1 is pressed against the bearing housing 1 "via a clamping ring 11.
  • the clamping ring 11 is in Fig. 4, on base the cutting position not visible screws to the bearing housing 1 "screwed.
  • a rotation of a clamping element 12 is provided for the distributor 1, in the present second embodiment, a pin.
  • the distributor 1 can be connected directly (first embodiment) or indirectly (second embodiment) to the bearing housing 1 ".

Landscapes

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

Abstract

L'invention concerne un dispositif directeur (1) pour une roue de turbine (2) d'un turbocompresseur (3) comportant une enveloppe de turbine (1') et un logement de palier (1'') entre lesquels peut être placé le dispositif directeur (1). Ce dernier comprend deux parois de glissement (5, 6) espacées par l'intermédiaire d'au moins deux boulons d'écartement (4), sensiblement annulaires et parallèles l'une à l'autre, entre lesquelles au moins une aube directrice (7) peut être placée de manière à pouvoir pivoter. La paroi de glissement (6) orientée vers le logement de palier (1'') peut être vissée directement ou non sur ce dernier. La conception selon l'invention permet d'éviter, dans une large mesure, une déformation thermique du dispositif directeur.
PCT/EP2008/008558 2007-11-28 2008-10-10 Dispositif directeur pour une turbine d'un turbocompresseur WO2009068137A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP08802852A EP2212523A1 (fr) 2007-11-28 2008-10-10 Dispositif directeur pour une turbine d'un turbocompresseur

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007057345.8 2007-11-28
DE102007057345A DE102007057345A1 (de) 2007-11-28 2007-11-28 Leitapparat für eine Turbine eines Abgasturboladers

Publications (1)

Publication Number Publication Date
WO2009068137A1 true WO2009068137A1 (fr) 2009-06-04

Family

ID=40165821

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2008/008558 WO2009068137A1 (fr) 2007-11-28 2008-10-10 Dispositif directeur pour une turbine d'un turbocompresseur

Country Status (3)

Country Link
EP (1) EP2212523A1 (fr)
DE (1) DE102007057345A1 (fr)
WO (1) WO2009068137A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009007663A1 (de) * 2009-02-05 2010-08-12 Bosch Mahle Turbo Systems Gmbh & Co. Kg Ladeeinrichtung

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009009129B4 (de) 2009-02-17 2022-11-03 BMTS Technology GmbH & Co. KG Turbolader mit variabler Turbinengeometrie
DE102011005151A1 (de) * 2011-03-04 2012-09-06 Bayerische Motoren Werke Aktiengesellschaft Abgasturbolader für eine Brennkraftmaschine
DE102017207540A1 (de) * 2017-05-04 2018-11-08 Man Diesel & Turbo Se Turbolader

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3844189A1 (de) * 1988-12-29 1990-07-12 Mtu Muenchen Gmbh Verstellbarer radialdiffusor fuer einen verdichter
EP0433560A1 (fr) * 1989-12-18 1991-06-26 Dr.Ing.h.c. F. Porsche Aktiengesellschaft Turbochargeur à gaz pour un moteur à combustion interne
DE19752534C1 (de) * 1997-11-27 1998-10-08 Daimler Benz Ag Radialdurchströmte Abgasturboladerturbine
WO2004035991A2 (fr) * 2002-10-18 2004-04-29 Mitsubishi Heavy Industries, Ltd. Mecanisme de tuyere variable, turbocompresseur d'echappement equipe de ce mecanisme, et procede de fabrication d'un turbocompresseur pourvu de ce mecanisme de tuyere variable
DE102004023279A1 (de) * 2004-05-11 2005-12-01 Volkswagen Ag Abgasturbolader für eine Brennkraftmaschine mit variabler Turbinengeometrie
DE102004030798A1 (de) * 2004-06-25 2006-01-19 Volkswagen Ag Abgasturbolader für eine Brennkraftmaschine mit variabler Turbinengeometrie
DE102004038748A1 (de) 2004-08-10 2006-02-23 Daimlerchrysler Ag Abgasturbolader für eine Brennkraftmaschine
EP1574673B1 (fr) 2004-03-10 2007-04-18 BorgWarner Inc. Aubes de guidage variables et turbosoufflante avec ces aubes

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3844189A1 (de) * 1988-12-29 1990-07-12 Mtu Muenchen Gmbh Verstellbarer radialdiffusor fuer einen verdichter
EP0433560A1 (fr) * 1989-12-18 1991-06-26 Dr.Ing.h.c. F. Porsche Aktiengesellschaft Turbochargeur à gaz pour un moteur à combustion interne
DE19752534C1 (de) * 1997-11-27 1998-10-08 Daimler Benz Ag Radialdurchströmte Abgasturboladerturbine
WO2004035991A2 (fr) * 2002-10-18 2004-04-29 Mitsubishi Heavy Industries, Ltd. Mecanisme de tuyere variable, turbocompresseur d'echappement equipe de ce mecanisme, et procede de fabrication d'un turbocompresseur pourvu de ce mecanisme de tuyere variable
EP1574673B1 (fr) 2004-03-10 2007-04-18 BorgWarner Inc. Aubes de guidage variables et turbosoufflante avec ces aubes
DE102004023279A1 (de) * 2004-05-11 2005-12-01 Volkswagen Ag Abgasturbolader für eine Brennkraftmaschine mit variabler Turbinengeometrie
DE102004030798A1 (de) * 2004-06-25 2006-01-19 Volkswagen Ag Abgasturbolader für eine Brennkraftmaschine mit variabler Turbinengeometrie
DE102004038748A1 (de) 2004-08-10 2006-02-23 Daimlerchrysler Ag Abgasturbolader für eine Brennkraftmaschine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009007663A1 (de) * 2009-02-05 2010-08-12 Bosch Mahle Turbo Systems Gmbh & Co. Kg Ladeeinrichtung

Also Published As

Publication number Publication date
EP2212523A1 (fr) 2010-08-04
DE102007057345A1 (de) 2009-06-04

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