EP0856639A3 - Nozzle ring for a radial turbine - Google Patents

Nozzle ring for a radial turbine Download PDF

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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Withdrawn
Application number
EP98810023A
Other languages
German (de)
French (fr)
Other versions
EP0856639A2 (en
Inventor
Marcel Meier
Martin Seiler
Claus Weisheit
Marcel Zehnder
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.)
Accelleron Industries AG
Original Assignee
ABB Asea Brown Boveri Ltd
Asea Brown Boveri AB
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 ABB Asea Brown Boveri Ltd, Asea Brown Boveri AB filed Critical ABB Asea Brown Boveri Ltd
Publication of EP0856639A2 publication Critical patent/EP0856639A2/en
Publication of EP0856639A3 publication Critical patent/EP0856639A3/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/048Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector for radial admission
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/045Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector for radial flow machines or engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application 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.

Figure 00000001
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.
Figure 00000001

EP98810023A 1997-01-29 1998-01-20 Nozzle ring for a radial turbine Withdrawn EP0856639A3 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
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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