EP1111196A3 - Variable guide vane system for the turbine of a turbocharger - Google Patents
Variable guide vane system for the turbine of a turbocharger Download PDFInfo
- Publication number
- EP1111196A3 EP1111196A3 EP00106218A EP00106218A EP1111196A3 EP 1111196 A3 EP1111196 A3 EP 1111196A3 EP 00106218 A EP00106218 A EP 00106218A EP 00106218 A EP00106218 A EP 00106218A EP 1111196 A3 EP1111196 A3 EP 1111196A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- guide
- impeller
- guide vane
- turbocharger
- turbine
- 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.)
- Granted
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
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
Eine Abgasturbine eines Abgasturboladers für eine Brennkraftmaschine ist mit einem in einem Gehäuse angeordneten Laufrad und mindestens einem das Laufrad umgebenden Strömungskanal versehen. Dieser umfaßt eine an das Laufrad mündende Ringdüse, in der mindestens ein variables Leitgitter mit leitschaufeln angeordnet ist. Durch das Leitgitter ist über eine Leitungsverstelleinrichtung der wirksame Strömungsquerschnitt einstellbar. Die Breite des Spaltes zwischen dem Leitgitter und den das Leitgitter umgebenden Gehäusewandteilen ist durch eine Einstelleinrichtung zwischen einem Maximalwert und einem Nullwert vertellbar. An exhaust gas turbine of an exhaust gas turbocharger for an internal combustion engine is provided with an impeller arranged in a housing and at least one flow channel surrounding the impeller. This comprises an annular nozzle opening onto the impeller, in which at least one variable guide vane with guide vanes is arranged. The effective flow cross section can be set by the guide grille via a line adjustment device. The width of the gap between the guide grid and the housing wall parts surrounding the guide grid can be adjusted between a maximum value and a zero value by means of an adjusting device.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19961613 | 1999-12-21 | ||
DE19961613A DE19961613A1 (en) | 1999-12-21 | 1999-12-21 | Exhaust gas turbine of an exhaust gas turbocharger for an internal combustion engine |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1111196A2 EP1111196A2 (en) | 2001-06-27 |
EP1111196A3 true EP1111196A3 (en) | 2002-07-24 |
EP1111196B1 EP1111196B1 (en) | 2004-04-28 |
Family
ID=7933528
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00106218A Expired - Lifetime EP1111196B1 (en) | 1999-12-21 | 2000-03-22 | Variable guide vane system for the turbine of a turbocharger |
Country Status (3)
Country | Link |
---|---|
US (1) | US6314736B1 (en) |
EP (1) | EP1111196B1 (en) |
DE (2) | DE19961613A1 (en) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10035762A1 (en) * | 2000-07-22 | 2002-01-31 | Daimler Chrysler Ag | Turbocharger for motor vehicle internal combustion engine has vanes to adjust flow through turbine and vary flow cross section |
US6729134B2 (en) | 2001-01-16 | 2004-05-04 | Honeywell International Inc. | Variable geometry turbocharger having internal bypass exhaust gas flow |
ITTO20010505A1 (en) * | 2001-05-25 | 2002-11-25 | Iveco Motorenforschung Ag | VARIABLE GEOMETRY TURBINE. |
US6665604B2 (en) | 2002-02-05 | 2003-12-16 | Honeywell International Inc. | Control method for variable geometry turbocharger and related system |
US6681573B2 (en) | 2002-02-05 | 2004-01-27 | Honeywell International Inc | Methods and systems for variable geometry turbocharger control |
DE10212675B4 (en) * | 2002-03-22 | 2006-05-18 | Daimlerchrysler Ag | Exhaust gas turbocharger in an internal combustion engine |
US6996986B2 (en) | 2002-07-19 | 2006-02-14 | Honeywell International, Inc. | Control system for variable geometry turbocharger |
US6647724B1 (en) | 2002-07-30 | 2003-11-18 | Honeywell International Inc. | Electric boost and/or generator |
US6637205B1 (en) | 2002-07-30 | 2003-10-28 | Honeywell International Inc. | Electric assist and variable geometry turbocharger |
DE60226784D1 (en) * | 2002-09-05 | 2008-07-03 | Honeywell Int Inc | TURBOCHARGER WITH ADJUSTABLE RODS |
EP1549826B1 (en) * | 2002-09-18 | 2008-09-17 | Honeywell International Inc. | Variable nozzle device for a turbocharger and method for operating the same |
AU2002334286A1 (en) * | 2002-09-18 | 2004-04-08 | Erbs, Eric | Turbocharger having variable nozzle device |
DE10253693B4 (en) * | 2002-11-18 | 2005-12-01 | Borgwarner Turbo Systems Gmbh | turbocharger |
DE10311205B3 (en) * | 2003-03-14 | 2004-09-16 | Man B & W Diesel Ag | Guiding device for a radial turbine of a turbocharger of a lifting piston I.C. engine operating with heavy oil has blades with shafts positioned in a housing part of the device facing a compressor of the turbocharger |
AU2003215784A1 (en) * | 2003-03-21 | 2004-10-11 | Honeywell International Inc. | Swinging vane concept for vnt turbochargers |
WO2004099573A1 (en) * | 2003-05-08 | 2004-11-18 | Honeywell International Inc. | Turbocharger with a variable nozzle device |
EP1536103B1 (en) * | 2003-11-28 | 2013-09-04 | BorgWarner, Inc. | Turbo machine having inlet guide vanes and attachment arrangement therefor |
DE102004030798B4 (en) * | 2004-06-25 | 2014-12-24 | Volkswagen Ag | Exhaust gas turbocharger for an internal combustion engine with variable turbine geometry |
FR2921100B1 (en) * | 2007-09-13 | 2009-12-04 | Snecma | ROTATIONAL DRIVE LEVER AROUND A VARIABLE TURBOMACHINE STATOR VANE PIVOT |
JP4952558B2 (en) * | 2007-12-12 | 2012-06-13 | 株式会社Ihi | Turbocharger |
DE102008060251B4 (en) | 2008-12-03 | 2021-08-12 | BMTS Technology GmbH & Co. KG | Exhaust gas turbocharger with variable turbine geometry |
JP5402682B2 (en) * | 2010-01-29 | 2014-01-29 | 株式会社Ihi | Turbocharger sealing device |
JP5136701B2 (en) * | 2010-12-02 | 2013-02-06 | トヨタ自動車株式会社 | Control device for an internal combustion engine with a supercharger |
ITCO20110038A1 (en) * | 2011-09-28 | 2013-03-29 | Nuovo Pignone Spa | INTEGRATED IMPLEMENTATION SYSTEM IN A COMPRESSOR |
JP5710452B2 (en) * | 2011-11-16 | 2015-04-30 | トヨタ自動車株式会社 | Turbocharger |
DE102011121394A1 (en) | 2011-12-17 | 2013-06-20 | Ihi Charging Systems International Gmbh | Adjustable control device for use in turbine of turbo-supercharger in combustion engine, has carrier ring axially positionable by rotary ring along symmetry axis, where carrier ring and rotary ring are arranged in force-transferable manner |
DE102012001237A1 (en) * | 2012-01-18 | 2013-07-18 | Ihi Charging Systems International Gmbh | Turbine for supercharger, has flow channel that is limited partly by one of the housing portions and partly by the insert element |
DE102012103412A1 (en) | 2012-04-19 | 2013-10-24 | Ihi Charging Systems International Gmbh | Turbine for supercharger formed as internal combustion engine of motor vehicle, has spring element that is positioned in wall of exhaust gas guide portion, in order to maintain minimal gap between support ring and contour ring |
DE102013220036A1 (en) * | 2013-10-02 | 2015-04-02 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Method for filling a pressure accumulator of an exhaust gas turbocharger |
DE102014214915B3 (en) * | 2014-07-30 | 2015-12-10 | MTU Aero Engines AG | Housing for a gas turbine, aircraft engine and a method for operating a gas turbine |
DE112017005661T5 (en) * | 2016-11-10 | 2019-08-29 | Ihi Corporation | Variable nozzle unit and turbocharger |
PL3542033T3 (en) | 2016-11-18 | 2024-02-05 | L'Air Liquide, Société Anonyme pour l'Etude et l'Exploitation des Procédés Georges Claude | Low-friction inlet nozzle for a turboexpander |
DE102019125823B4 (en) * | 2019-09-25 | 2023-05-11 | Rolls-Royce Solutions GmbH | Turbine housing and exhaust gas turbocharger with pre-guide blades and an internal combustion engine with an exhaust gas turbocharger |
EP3929407A1 (en) * | 2020-06-23 | 2021-12-29 | ABB Schweiz AG | Modular nozzle ring for a turbine stage of a flow engine |
CN111963470A (en) * | 2020-08-07 | 2020-11-20 | 中国北方发动机研究所(天津) | Turbocharger compressor clearance control device |
DE102022128618A1 (en) | 2022-10-28 | 2024-05-08 | Atlas Copco Energas Gmbh | Turbomachines and methods for operating a turbomachine |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2341974A (en) * | 1941-05-14 | 1944-02-15 | Wright Aeronautical Corp | Supercharger control |
US4242040A (en) * | 1979-03-21 | 1980-12-30 | Rotoflow Corporation | Thrust adjusting means for nozzle clamp ring |
US4502836A (en) * | 1982-07-02 | 1985-03-05 | Swearingen Judson S | Method for nozzle clamping force control |
JPS60175707A (en) * | 1984-02-22 | 1985-09-09 | Nissan Motor Co Ltd | Variable nozzle of radial turbine |
JPH01130002A (en) * | 1987-11-12 | 1989-05-23 | Mitsubishi Heavy Ind Ltd | Variable nozzle device for radial turbine |
US5769602A (en) * | 1995-04-26 | 1998-06-23 | Rotoflow Corporation | Active automatic clamping control |
DE19838928C1 (en) * | 1998-08-27 | 1999-04-22 | Daimler Chrysler Ag | Variably adjustable guide grid of turbine |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2931766C2 (en) * | 1979-08-04 | 1982-08-05 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Sealing device for the free blade ends of an adjustable diffuser of a gas turbine |
DE3541508C1 (en) * | 1985-11-23 | 1987-02-05 | Kuehnle Kopp Kausch Ag | Exhaust gas turbocharger |
DE3941715A1 (en) * | 1989-12-18 | 1991-06-20 | Porsche Ag | EXHAUST TURBOCHARGER FOR AN INTERNAL COMBUSTION ENGINE |
US5214920A (en) * | 1990-11-27 | 1993-06-01 | Leavesley Malcolm G | Turbocharger apparatus |
SE501488C2 (en) * | 1993-07-08 | 1995-02-27 | Mecel Ab | Arrangement and procedure for idle control and charge pressure control in a supercharged internal combustion engine |
DE19543190C2 (en) | 1995-11-20 | 1998-01-29 | Daimler Benz Ag | Engine brake for a supercharged internal combustion engine |
DE19615237C2 (en) * | 1996-04-18 | 1999-10-28 | Daimler Chrysler Ag | Exhaust gas turbocharger for an internal combustion engine |
JPH10130002A (en) | 1996-10-28 | 1998-05-19 | Unitika Ltd | Three dimensional mesh like metal oxide and its production |
DE19651498C1 (en) * | 1996-12-11 | 1998-04-16 | Daimler Benz Ag | Exhaust turbocharger for IC engine |
-
1999
- 1999-12-21 DE DE19961613A patent/DE19961613A1/en not_active Ceased
-
2000
- 2000-03-22 DE DE50006238T patent/DE50006238D1/en not_active Expired - Fee Related
- 2000-03-22 EP EP00106218A patent/EP1111196B1/en not_active Expired - Lifetime
- 2000-04-26 US US09/558,834 patent/US6314736B1/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2341974A (en) * | 1941-05-14 | 1944-02-15 | Wright Aeronautical Corp | Supercharger control |
US4242040A (en) * | 1979-03-21 | 1980-12-30 | Rotoflow Corporation | Thrust adjusting means for nozzle clamp ring |
US4502836A (en) * | 1982-07-02 | 1985-03-05 | Swearingen Judson S | Method for nozzle clamping force control |
JPS60175707A (en) * | 1984-02-22 | 1985-09-09 | Nissan Motor Co Ltd | Variable nozzle of radial turbine |
JPH01130002A (en) * | 1987-11-12 | 1989-05-23 | Mitsubishi Heavy Ind Ltd | Variable nozzle device for radial turbine |
US5769602A (en) * | 1995-04-26 | 1998-06-23 | Rotoflow Corporation | Active automatic clamping control |
DE19838928C1 (en) * | 1998-08-27 | 1999-04-22 | Daimler Chrysler Ag | Variably adjustable guide grid of turbine |
Non-Patent Citations (2)
Title |
---|
PATENT ABSTRACTS OF JAPAN vol. 010, no. 014 (M - 447) 21 January 1986 (1986-01-21) * |
PATENT ABSTRACTS OF JAPAN vol. 013, no. 376 (M - 862) 21 August 1989 (1989-08-21) * |
Also Published As
Publication number | Publication date |
---|---|
DE19961613A1 (en) | 2001-07-19 |
DE50006238D1 (en) | 2004-06-03 |
EP1111196B1 (en) | 2004-04-28 |
US6314736B1 (en) | 2001-11-13 |
EP1111196A2 (en) | 2001-06-27 |
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