EP0856639A3 - Nozzle ring for a radial turbine - Google Patents
Nozzle ring for a radial turbine Download PDFInfo
- Publication number
- EP0856639A3 EP0856639A3 EP98810023A EP98810023A EP0856639A3 EP 0856639 A3 EP0856639 A3 EP 0856639A3 EP 98810023 A EP98810023 A EP 98810023A EP 98810023 A EP98810023 A EP 98810023A EP 0856639 A3 EP0856639 A3 EP 0856639A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- nozzle ring
- radial turbine
- seal
- fastening elements
- expansion gap
- 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- Withdrawn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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/048—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector for radial admission
-
- 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
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
-
- 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
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/045—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector for radial flow 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
Aufgabe der Erfindung ist es, einen Düsenring für die Abgasturbine eines Turboladers zu schaffen, welcher neben einer verbesserter Lebensdauer auch einen konstanten Wirkungsgrad garantiert.The object of the invention is to provide a nozzle ring for the exhaust gas turbine of a turbocharger to create, which in addition to an improved lifespan also a constant efficiency guaranteed.
Erfindungsgemäss wird dies dadurch erreicht, dass zwischen dem Turbinengehäuse (2) und dem Düsenring (11) ein radialer Dehnungsspalt (20) ausgebildet und im Dehnungsspalt (20) zumindest eine Dichtung (22) angeordnet ist. Dazu ist in zumindest einem der Befestigungselemente (16, 17) des Düsenrings (11) oder in zumindest einem der die Befestigungselemente (16, 17) umgebenden Bauteile (3, 4, 5) des Turbinengehäuses (2) eine die Dichtung (22) aufnehmende, umlaufende Nut (21) ausgebildet. According to the invention, this is achieved in that a radial expansion gap (20) is formed between the turbine housing (2) and the nozzle ring (11) and at least one seal (22) is arranged in the expansion gap (20). For this purpose, at least one of the fastening elements (16, 17) of the nozzle ring (11) or in at least one of the components (3, 4, 5) of the turbine housing (2) surrounding the fastening elements (16, 17) has a seal (22) , circumferential groove (21) formed.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19703033A DE19703033A1 (en) | 1997-01-29 | 1997-01-29 | Exhaust gas turbine of a turbocharger |
DE19703033 | 1997-01-29 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0856639A2 EP0856639A2 (en) | 1998-08-05 |
EP0856639A3 true EP0856639A3 (en) | 2000-04-19 |
Family
ID=7818574
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP98810023A Withdrawn EP0856639A3 (en) | 1997-01-29 | 1998-01-20 | Nozzle ring for a radial turbine |
Country Status (7)
Country | Link |
---|---|
US (1) | US5964574A (en) |
EP (1) | EP0856639A3 (en) |
JP (1) | JP3004616B2 (en) |
KR (1) | KR19980070758A (en) |
CN (1) | CN1192513A (en) |
CZ (1) | CZ292035B6 (en) |
DE (1) | DE19703033A1 (en) |
Families Citing this family (54)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6565468B2 (en) | 1999-12-21 | 2003-05-20 | The Gates Corporation | Tensioner with damping mechanism |
JP4370662B2 (en) * | 2000-03-17 | 2009-11-25 | アイシン精機株式会社 | Variable capacity turbocharger |
US6287091B1 (en) * | 2000-05-10 | 2001-09-11 | General Motors Corporation | Turbocharger with nozzle ring coupling |
EP1180632A1 (en) * | 2000-08-07 | 2002-02-20 | ABB Turbo Systems AG | Axial securing system |
DE10051223A1 (en) | 2000-10-16 | 2002-04-25 | Alstom Switzerland Ltd | Connectable stator elements |
JP2003184563A (en) * | 2001-12-14 | 2003-07-03 | Aisin Seiki Co Ltd | Variable displacement turbocharger |
EP1394363B1 (en) * | 2002-08-26 | 2006-03-01 | BorgWarner Inc. | Variable guide vane system for a turbine unit |
DE10256418A1 (en) | 2002-12-02 | 2004-06-09 | Abb Turbo Systems Ag | Exhaust turbine housing |
EP1536103B1 (en) | 2003-11-28 | 2013-09-04 | BorgWarner, Inc. | Turbo machine having inlet guide vanes and attachment arrangement therefor |
JP4729901B2 (en) * | 2004-11-01 | 2011-07-20 | 株式会社Ihi | Turbocharger and sealing device |
US8047772B2 (en) * | 2005-03-30 | 2011-11-01 | Honeywell International Inc. | Variable geometry turbine for a turbocharger and method of controlling the turbine |
KR20090039770A (en) * | 2006-08-18 | 2009-04-22 | 가부시키가이샤 아이에이치아이 | Electric supercharger |
US7559199B2 (en) * | 2006-09-22 | 2009-07-14 | Honeywell International Inc. | Variable-nozzle cartridge for a turbocharger |
JP5045304B2 (en) * | 2007-08-16 | 2012-10-10 | 株式会社Ihi | Turbocharger |
JP4952558B2 (en) * | 2007-12-12 | 2012-06-13 | 株式会社Ihi | Turbocharger |
JP2009197633A (en) * | 2008-02-20 | 2009-09-03 | Ihi Corp | Turbo charger |
DE102008057878A1 (en) * | 2008-11-18 | 2010-05-20 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Supercharger device, particularly exhaust gas turbocharger for combustion engine of motor vehicle, has turbine wheel and compressor carrying shaft, where turbine wheel is partially surrounded by turbine housing |
JP5402061B2 (en) * | 2009-02-17 | 2014-01-29 | 株式会社Ihi | Turbocharger |
JP5402682B2 (en) * | 2010-01-29 | 2014-01-29 | 株式会社Ihi | Turbocharger sealing device |
US8857178B2 (en) * | 2011-06-28 | 2014-10-14 | Caterpillar Inc. | Nozzled turbocharger turbine and associated engine and method |
DE112012003266T5 (en) * | 2011-09-27 | 2014-05-22 | Borgwarner Inc. | Semi-permeable medium for sealing an actuating shaft |
JP5710452B2 (en) * | 2011-11-16 | 2015-04-30 | トヨタ自動車株式会社 | Turbocharger |
CN104246170B (en) * | 2012-03-30 | 2018-09-21 | 博格华纳公司 | Turbo-charger bearing shell with integrated heat screen |
JP5949164B2 (en) * | 2012-05-29 | 2016-07-06 | 株式会社Ihi | Variable nozzle unit and variable capacity turbocharger |
JP6051791B2 (en) * | 2012-11-06 | 2016-12-27 | トヨタ自動車株式会社 | Turbocharger |
EP2733311B1 (en) * | 2012-11-16 | 2019-01-02 | ABB Turbo Systems AG | Nozzle ring |
JP6331423B2 (en) * | 2014-01-29 | 2018-05-30 | 株式会社Ihi | Variable capacity turbocharger |
JP6542246B2 (en) * | 2014-10-02 | 2019-07-10 | 株式会社Ihi | Variable displacement turbocharger |
CN104564174B (en) * | 2014-12-29 | 2017-01-18 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | Elastic sealing structure for turbine fixed blades of gas turbine |
US9739238B2 (en) | 2015-03-09 | 2017-08-22 | Caterpillar Inc. | Turbocharger and method |
US10006341B2 (en) | 2015-03-09 | 2018-06-26 | Caterpillar Inc. | Compressor assembly having a diffuser ring with tabs |
US9732633B2 (en) | 2015-03-09 | 2017-08-15 | Caterpillar Inc. | Turbocharger turbine assembly |
US9879594B2 (en) | 2015-03-09 | 2018-01-30 | Caterpillar Inc. | Turbocharger turbine nozzle and containment structure |
US9650913B2 (en) | 2015-03-09 | 2017-05-16 | Caterpillar Inc. | Turbocharger turbine containment structure |
US9822700B2 (en) | 2015-03-09 | 2017-11-21 | Caterpillar Inc. | Turbocharger with oil containment arrangement |
US9915172B2 (en) | 2015-03-09 | 2018-03-13 | Caterpillar Inc. | Turbocharger with bearing piloted compressor wheel |
US9903225B2 (en) | 2015-03-09 | 2018-02-27 | Caterpillar Inc. | Turbocharger with low carbon steel shaft |
US10066639B2 (en) | 2015-03-09 | 2018-09-04 | Caterpillar Inc. | Compressor assembly having a vaneless space |
US9777747B2 (en) | 2015-03-09 | 2017-10-03 | Caterpillar Inc. | Turbocharger with dual-use mounting holes |
US9890788B2 (en) | 2015-03-09 | 2018-02-13 | Caterpillar Inc. | Turbocharger and method |
US9810238B2 (en) | 2015-03-09 | 2017-11-07 | Caterpillar Inc. | Turbocharger with turbine shroud |
US9638138B2 (en) | 2015-03-09 | 2017-05-02 | Caterpillar Inc. | Turbocharger and method |
US9752536B2 (en) | 2015-03-09 | 2017-09-05 | Caterpillar Inc. | Turbocharger and method |
US9683520B2 (en) | 2015-03-09 | 2017-06-20 | Caterpillar Inc. | Turbocharger and method |
CN106337697B (en) * | 2016-09-13 | 2019-02-01 | 中国北方发动机研究所(天津) | A kind of nozzle ring seal arrangement |
US10731546B2 (en) * | 2017-02-06 | 2020-08-04 | Borgwarner Inc. | Diffuser in wastegate turbine housings |
DE102017114397A1 (en) * | 2017-06-28 | 2019-01-03 | 2G Energy AG | Method for adapting a turbocharger and a stationary engine system as well as turbocharger and stationary engine system |
WO2019044777A1 (en) * | 2017-08-28 | 2019-03-07 | 株式会社豊田自動織機 | Turbocharger |
DE102017127628A1 (en) * | 2017-11-22 | 2019-05-23 | Man Energy Solutions Se | Turbine and turbocharger |
US10612418B2 (en) * | 2018-03-22 | 2020-04-07 | GM Global Technology Operations LLC | Nested flange joint |
EP3929407A1 (en) * | 2020-06-23 | 2021-12-29 | ABB Schweiz AG | Modular nozzle ring for a turbine stage of a flow engine |
WO2023180071A1 (en) * | 2022-03-22 | 2023-09-28 | Turbo Systems Switzerland Ltd. | Nozzle ring for a radial turbine, exhaust turbine, and turbocharger |
WO2023228467A1 (en) * | 2022-05-25 | 2023-11-30 | 株式会社Ihi | Turbine and supercharger |
DE102022118731A1 (en) | 2022-07-26 | 2024-02-01 | Rolls-Royce Solutions GmbH | Turbine arrangements, turbochargers and internal combustion engines |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447942A (en) * | 1944-12-05 | 1948-08-24 | Rateau Soc | Turbine distributor and nozzle |
US2668006A (en) * | 1949-11-08 | 1954-02-02 | Baldwin Lima Hamilton Corp | Turbocharger |
EP0024275A1 (en) * | 1979-08-15 | 1981-03-04 | BBC Aktiengesellschaft Brown, Boveri & Cie. | Arresting of nozzle rings |
US4311432A (en) * | 1979-11-20 | 1982-01-19 | United Technologies Corporation | Radial seal |
US4687412A (en) * | 1985-07-03 | 1987-08-18 | Pratt & Whitney Canada Inc. | Impeller shroud |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE111098C (en) * | ||||
US1154777A (en) * | 1914-02-21 | 1915-09-28 | Gen Electric | Attaching means for nozzles. |
US1922017A (en) * | 1931-10-27 | 1933-08-08 | Gen Electric | Elastic fluid turbine |
US3068638A (en) * | 1953-06-09 | 1962-12-18 | Laval Steam Turbine Inc De | Turbocharger for internal com. bustion engines |
DE1040569B (en) * | 1954-07-08 | 1958-10-09 | Westinghouse Electric Corp | Attachment of the nozzle segments in the housing of a steam turbine |
US3737247A (en) * | 1971-04-12 | 1973-06-05 | Garrett Corp | Composite nozzle |
JPS5257410A (en) * | 1975-11-07 | 1977-05-11 | Hitachi Ltd | Leakage sealing mechanism for axial fluid machine |
US4242040A (en) * | 1979-03-21 | 1980-12-30 | Rotoflow Corporation | Thrust adjusting means for nozzle clamp ring |
DE3541508C1 (en) * | 1985-11-23 | 1987-02-05 | Kuehnle Kopp Kausch Ag | Exhaust gas turbocharger |
US4679984A (en) * | 1985-12-11 | 1987-07-14 | The Garrett Corporation | Actuation system for variable nozzle turbine |
GB2234295B (en) * | 1989-07-21 | 1993-07-21 | Rolls Royce Plc | Gas turbine engine compressor assembly |
US5249920A (en) * | 1992-07-09 | 1993-10-05 | General Electric Company | Turbine nozzle seal arrangement |
-
1997
- 1997-01-29 DE DE19703033A patent/DE19703033A1/en not_active Withdrawn
-
1998
- 1998-01-20 EP EP98810023A patent/EP0856639A3/en not_active Withdrawn
- 1998-01-22 US US09/012,035 patent/US5964574A/en not_active Expired - Lifetime
- 1998-01-23 KR KR1019980002038A patent/KR19980070758A/en not_active Application Discontinuation
- 1998-01-27 JP JP10013696A patent/JP3004616B2/en not_active Expired - Fee Related
- 1998-01-27 CN CN98105958A patent/CN1192513A/en active Pending
- 1998-01-28 CZ CZ1998263A patent/CZ292035B6/en not_active IP Right Cessation
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447942A (en) * | 1944-12-05 | 1948-08-24 | Rateau Soc | Turbine distributor and nozzle |
US2668006A (en) * | 1949-11-08 | 1954-02-02 | Baldwin Lima Hamilton Corp | Turbocharger |
EP0024275A1 (en) * | 1979-08-15 | 1981-03-04 | BBC Aktiengesellschaft Brown, Boveri & Cie. | Arresting of nozzle rings |
US4311432A (en) * | 1979-11-20 | 1982-01-19 | United Technologies Corporation | Radial seal |
US4687412A (en) * | 1985-07-03 | 1987-08-18 | Pratt & Whitney Canada Inc. | Impeller shroud |
Also Published As
Publication number | Publication date |
---|---|
CN1192513A (en) | 1998-09-09 |
DE19703033A1 (en) | 1998-07-30 |
EP0856639A2 (en) | 1998-08-05 |
US5964574A (en) | 1999-10-12 |
CZ26398A3 (en) | 1998-08-12 |
KR19980070758A (en) | 1998-10-26 |
JP3004616B2 (en) | 2000-01-31 |
CZ292035B6 (en) | 2003-07-16 |
JPH10220235A (en) | 1998-08-18 |
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Legal Events
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PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
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RIC1 | Information provided on ipc code assigned before grant |
Free format text: 7F 01D 9/04 A, 7F 01D 11/00 B, 7F 01D 25/24 B |
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RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ABB TURBO SYSTEMS AG |
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Effective date: 20000913 |
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17Q | First examination report despatched |
Effective date: 20021028 |
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Effective date: 20040130 |