DE112012006245A5 - Turbine für einen Abgasturbolader - Google Patents
Turbine für einen Abgasturbolader Download PDFInfo
- Publication number
- DE112012006245A5 DE112012006245A5 DE112012006245.0T DE112012006245T DE112012006245A5 DE 112012006245 A5 DE112012006245 A5 DE 112012006245A5 DE 112012006245 T DE112012006245 T DE 112012006245T DE 112012006245 A5 DE112012006245 A5 DE 112012006245A5
- Authority
- DE
- Germany
- Prior art keywords
- turbine
- exhaust gas
- gas turbocharger
- turbocharger
- exhaust
- 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- Withdrawn
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
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
-
- 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
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
- F01D17/143—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path the shiftable member being a wall, or part thereof of a radial diffuser
-
- 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
- F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
-
- 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
- F02B37/12—Control of the pumps
- F02B37/18—Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
- F02B37/183—Arrangements of bypass valves or actuators therefor
-
- 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
- F02B37/12—Control of the pumps
- F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
- F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
-
- 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
- F02B37/12—Control of the pumps
- F02B37/24—Control of the pumps by using pumps or turbines with adjustable guide vanes
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Supercharger (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102012103411A DE102012103411A1 (de) | 2012-04-19 | 2012-04-19 | Turbine für einen Abgasturbolader |
DE102012103411.7 | 2012-04-19 | ||
PCT/EP2012/002217 WO2013156047A2 (de) | 2012-04-19 | 2012-05-24 | Turbine für einen abgasturbolader |
Publications (1)
Publication Number | Publication Date |
---|---|
DE112012006245A5 true DE112012006245A5 (de) | 2015-03-05 |
Family
ID=46458411
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102012103411A Withdrawn DE102012103411A1 (de) | 2012-04-19 | 2012-04-19 | Turbine für einen Abgasturbolader |
DE112012006245.0T Withdrawn DE112012006245A5 (de) | 2012-04-19 | 2012-05-24 | Turbine für einen Abgasturbolader |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102012103411A Withdrawn DE102012103411A1 (de) | 2012-04-19 | 2012-04-19 | Turbine für einen Abgasturbolader |
Country Status (2)
Country | Link |
---|---|
DE (2) | DE102012103411A1 (de) |
WO (3) | WO2013156047A2 (de) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170350417A1 (en) * | 2016-06-03 | 2017-12-07 | Dresser-Rand Company | Variable area diffuser |
US9739166B1 (en) * | 2016-08-31 | 2017-08-22 | Borgwarner Inc. | VTG internal by-pass |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2861774A (en) * | 1950-02-16 | 1958-11-25 | Alfred J Buchi | Inlet control for radial flow turbines |
NL270226A (de) * | 1961-10-13 | |||
SU478957A2 (ru) * | 1973-10-05 | 1975-07-30 | Предприятие П/Я В-2504 | Центробежный компрессор |
EP0093462B1 (de) | 1982-04-29 | 1988-01-20 | BBC Brown Boveri AG | Abgasturbolader mit verstellbarem Ringschieber |
US5214920A (en) * | 1990-11-27 | 1993-06-01 | Leavesley Malcolm G | Turbocharger apparatus |
DE19918232C2 (de) * | 1999-04-22 | 2001-03-01 | Daimler Chrysler Ag | Mehrzylindriger Verbrennungsmotor mit einem Abgasturbolader |
DE10028732A1 (de) * | 2000-06-09 | 2001-12-13 | Daimler Chrysler Ag | Abgasturbine |
DE10212032A1 (de) * | 2002-03-19 | 2003-10-02 | Daimler Chrysler Ag | Abgasturbolader für eine Brennkraftmaschine |
GB0227473D0 (en) * | 2002-11-25 | 2002-12-31 | Leavesley Malcolm G | Variable turbocharger apparatus with bypass apertures |
WO2004074643A1 (en) * | 2003-02-19 | 2004-09-02 | Honeywell International Inc. | Nozzle device for a turbocharger and associated control method |
DE102004038903A1 (de) * | 2004-08-11 | 2006-02-23 | Daimlerchrysler Ag | Abgasturbolader für eine Brennkraftmaschine |
US20090301082A1 (en) * | 2005-11-16 | 2009-12-10 | Alain Lombard | Turbocharger having piston-type variable nozzle with integrated actuation system |
US7338254B2 (en) * | 2005-11-29 | 2008-03-04 | Honeywell International, Inc. | Turbocharger with sliding piston assembly |
JP2009228479A (ja) * | 2008-03-19 | 2009-10-08 | Toyota Motor Corp | ターボチャージャ |
DE102008000848A1 (de) * | 2008-03-27 | 2009-10-01 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Abgasturbolader für eine Brennkraftmaschine eines Kraftfahrzeugs |
US8070425B2 (en) * | 2008-03-28 | 2011-12-06 | Honeywell International Inc. | Turbocharger with sliding piston, and having vanes and leakage dams |
DE102008032492A1 (de) * | 2008-07-05 | 2010-01-07 | Daimler Ag | Turbinengehäuse für einen Abgasturbolader einer Brennkraftmaschine |
US8702381B2 (en) * | 2008-12-11 | 2014-04-22 | Borgwarner Inc. | Simplified variable geometry turbocharger with vane rings |
DE102008063656A1 (de) * | 2008-12-18 | 2010-06-24 | Daimler Ag | Abgasturbolader |
US8113770B2 (en) * | 2009-02-03 | 2012-02-14 | Honeywell International Inc. | Turbine assembly for an exhaust gas-driven turbocharger having a variable nozzle |
DE102009050975A1 (de) | 2009-10-28 | 2011-05-05 | Daimler Ag | Leitvorrichtung für einen Abgasturbolader mit verstellbarer Turbinengeometrie sowie Abgasturbolader für eine Brennkraftmaschine |
DE102009050951A1 (de) | 2009-10-28 | 2011-05-05 | Daimler Ag | Turbine für einen Abgasturbolader |
-
2012
- 2012-04-19 DE DE102012103411A patent/DE102012103411A1/de not_active Withdrawn
- 2012-05-24 DE DE112012006245.0T patent/DE112012006245A5/de not_active Withdrawn
- 2012-05-24 WO PCT/EP2012/002217 patent/WO2013156047A2/de active Application Filing
- 2012-06-20 WO PCT/EP2012/002585 patent/WO2013156048A1/de active Application Filing
-
2013
- 2013-04-10 WO PCT/EP2013/001052 patent/WO2013156121A1/de active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2013156121A1 (de) | 2013-10-24 |
DE102012103411A1 (de) | 2013-10-24 |
WO2013156048A1 (de) | 2013-10-24 |
WO2013156047A3 (de) | 2014-02-20 |
WO2013156047A2 (de) | 2013-10-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
R012 | Request for examination validly filed | ||
R082 | Change of representative |
Representative=s name: HEEB-KELLER, ANNETTE, DR., DE |
|
R016 | Response to examination communication | ||
R081 | Change of applicant/patentee |
Owner name: IHI CHARGING SYSTEMS INTERNATIONAL GMBH, DE Free format text: FORMER OWNER: IHI CHARGING SYSTEMS INTERNATIONAL GMBH, 69126 HEIDELBERG, DE |
|
R082 | Change of representative |
Representative=s name: HEEB-KELLER, ANNETTE, DR., DE |
|
R016 | Response to examination communication | ||
R120 | Application withdrawn or ip right abandoned |