EP0834646A1 - Dispositif de rétention pour la turbine radiale d'un turbocompresseur - Google Patents

Dispositif de rétention pour la turbine radiale d'un turbocompresseur Download PDF

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Publication number
EP0834646A1
EP0834646A1 EP97810657A EP97810657A EP0834646A1 EP 0834646 A1 EP0834646 A1 EP 0834646A1 EP 97810657 A EP97810657 A EP 97810657A EP 97810657 A EP97810657 A EP 97810657A EP 0834646 A1 EP0834646 A1 EP 0834646A1
Authority
EP
European Patent Office
Prior art keywords
burst protection
protection device
housing
burst
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.)
Withdrawn
Application number
EP97810657A
Other languages
German (de)
English (en)
Inventor
Josef Bättig
Wolfgang Diebold
Reto Meier
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.)
ABB Asea Brown Boveri Ltd
ABB AB
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 EP0834646A1 publication Critical patent/EP0834646A1/fr
Withdrawn legal-status Critical Current

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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
    • F01D9/026—Scrolls for radial machines or engines
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • 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

Definitions

  • the invention relates to a burst protection device for radial turbines of turbochargers, according to the preamble of the claim 1.
  • DE-A1-42 23 496 describes a device for reduction the kinetic energy of bursting parts for those with high Speed revolving machines known.
  • This inside An axial turbine device consists of several interconnected guard rings between which each a crumple zone made of ductile material is trained.
  • Such a solution is for radial turbines not suitable because of their radial gas entry no burst protection devices in the radial area of the turbine can be used.
  • the invention tries to avoid all of these disadvantages. It is based on the task of being simple and safe Burst protection device for radial turbines of turbochargers create and thus the stability of the turbine, respectively the availability of the internal combustion engine connected to it to increase.
  • the first burst protection device is internal, i.e. arranged radially between the gas inlet and gas outlet housing and designed as a circumferential burst protection ring, wherein however, the guide vane channel is excluded.
  • the second burst protection device is external, i.e. Outside arranged on the gas inlet housing. It is as a spiral Formed sheet metal shell and extends at least over the axial expansion of the turbine wheel. Gas outlet side The burst protection ring also covers at least the axial extent of the turbine wheel.
  • burst protection device This creates a relatively simple and safe burst protection device created for radial turbocharger turbines.
  • the loose arrangement of the burst protection ring facilitates its assembly and thus leads to lower assembly costs. It comes to When the turbine wheel bursts, the burst protection ring takes one Most of the burst energy. Since the burst protection ring with Except for the guide vane duct, the entire length of the turbine wheel covers, can through the relatively narrow guide vane channel only smaller turbine fragments in the gas inlet casing to be flung. The big fragments which have a large kinetic energy are from Burst protection ring stopped. When smaller fragments Knock through the wall of the gas inlet housing, so these caught by the external burst protection device. Consequently can be achieved by combining internal and external burst protection devices even with very large released energies prevents turbine parts from being thrown out into the environment will.
  • a third burst protection device arranged and designed as a steel wire rope package.
  • the steel wire rope package is also in the cavity of Gas inlet housing and gas inlet housing, namely on the gas outlet housing side the burst protection ring arranged. It exists from several steel wire ropes, which are parallel to the direction of rotation of the turbine wheel and in at least one row are arranged side by side.
  • the exhaust gas turbocharger mainly consists of one shown compressor and designed as a radial turbine Exhaust gas turbine 1.
  • the radial turbine 1 has a turbine housing 2, with a spiral gas inlet housing 3 and a gas outlet housing designed as a gas outlet flange 4.
  • Turbine wheel 6 with blades 7 rotatably mounted.
  • shaft 5 is also not shown Compressor wheel arranged.
  • the gas inlet housing 3 goes downstream into a guide vane duct 8 over, in which a nozzle ring 9 between form Gas inlet housing 3 and gas outlet flange 4 is arranged.
  • the shaft 5 is in a bearing housing 11 by means of bearings 10 rotatably mounted.
  • the gas inlet housing 3 and the bearing housing 11 are via a clamping band arranged in the circumferential direction 12 connected to each other (Fig. 1).
  • the gas inlet housing 3 and the gas outlet housing 4 are releasably connected by screws 13. Both parts of the turbine housing 2 each have in their connection area a recess 14.
  • the recesses 14 form one common cavity 15, which is a first, as a circumferential Burst protection ring designed burst protection device 16, takes up loosely.
  • the burst protection ring 16 is thus radial between the gas inlet housing 3 and the gas outlet flange 4 arranged, however, the area of the guide vane channel 8 is excluded.
  • the burst protection ring covers the gas outlet side 16 the turbine wheel 6 in its axial extent completely from. Of course, he can the turbine wheel 6 on this Tower over the side.
  • Second burst protection device 17 arranged and detachable via a plurality of screws 18 with the Gas inlet housing 3 connected.
  • 17 becomes a high quality material, such as Hastelloy used. This can further increase the protective effect be improved.
  • the first and the second burst protection device 16, 17 a third burst protection device 19 gas outlet housing side of the Burst protection ring 16 arranged in the cavity 15.
  • This third Burst protection device 19 is designed as a steel wire rope package, which consists of several parallel to the direction of rotation of the Turbine wheel 6 and arranged side by side in a row Steel wire ropes 20 exists (Fig. 2).
  • the gas outlet flange 4 has four in its recess 14 parallel to the axis of rotation 21 of the turbine wheel 6 arranged ribs 22 with which the steel wire rope package 19 is positively connected (Fig. 3). These ribs are stiffening, so that an additional Burst protection is achieved.
  • a third burst protection device 19 is reduced the likelihood of turbine part leakage out of the turbine housing 2 and thus increases safety of the exhaust gas turbocharger.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
EP97810657A 1996-10-02 1997-09-15 Dispositif de rétention pour la turbine radiale d'un turbocompresseur Withdrawn EP0834646A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19640654 1996-10-02
DE19640654A DE19640654A1 (de) 1996-10-02 1996-10-02 Berstschutzvorrichtung für Radialturbinen von Turboladern

Publications (1)

Publication Number Publication Date
EP0834646A1 true EP0834646A1 (fr) 1998-04-08

Family

ID=7807677

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97810657A Withdrawn EP0834646A1 (fr) 1996-10-02 1997-09-15 Dispositif de rétention pour la turbine radiale d'un turbocompresseur

Country Status (6)

Country Link
EP (1) EP0834646A1 (fr)
JP (1) JPH10110622A (fr)
KR (1) KR19980032381A (fr)
CZ (1) CZ309997A3 (fr)
DE (1) DE19640654A1 (fr)
PL (1) PL322377A1 (fr)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000034628A1 (fr) * 1998-12-07 2000-06-15 Pratt & Whitney Canada Corp. Systeme de confinement pour turbine
GB2357120A (en) * 1999-12-09 2001-06-13 Alexander Cameron Henderson Catalyst coated turbocharger turbine
EP1233190A1 (fr) * 2001-02-20 2002-08-21 MAN B&W Diesel AG Turbomachine avec une roue à aubes radiale
GB2414769A (en) * 2004-06-05 2005-12-07 Man B & W Diesel Ag Turbo-machine with impeller containment assembly.
WO2007075532A2 (fr) * 2005-12-23 2007-07-05 Honeywell International Inc. Boîtier de compresseur à pièces multiples
WO2007124559A1 (fr) * 2006-04-27 2007-11-08 Pratt & Whitney Canada Corp. Élément de confinement de rotor ayant des connections cassantes
US20120263584A1 (en) * 2011-04-14 2012-10-18 Mann+Hummel Gmbh Compressor Housing of a Radial Compressor
US9021802B2 (en) 2010-08-26 2015-05-05 Honeywell International Inc. Turbine housing assembly with wastegate
US9091208B2 (en) 2010-07-16 2015-07-28 Honeywell International Inc. Turbocharger bearing housing assembly
US9097120B2 (en) 2010-08-26 2015-08-04 Honeywell International Inc. Turbine housing assembly
WO2015132616A1 (fr) * 2014-03-07 2015-09-11 Cummins Ltd Turbine
DE102014212926A1 (de) * 2014-07-03 2016-01-07 Siemens Aktiengesellschaft Spiralgehäuse für einen Radialverdichter
KR20160088922A (ko) * 2014-03-31 2016-07-26 미츠비시 쥬고교 가부시키가이샤 원심 압축기, 과급기, 및 원심 압축기의 제조 방법
EP3009634A4 (fr) * 2013-09-25 2016-09-14 Mitsubishi Heavy Ind Ltd Compresseur et compresseur à suralimentation
US9702266B2 (en) 2014-06-30 2017-07-11 Honeywell International Inc. Turbocharger turbine housing
DE102017109594A1 (de) * 2017-05-04 2018-11-08 Abb Turbo Systems Ag Verdichtergehäuse eines Radialverdichters
US20190301304A1 (en) * 2018-03-27 2019-10-03 Man Energy Solutions Se Turbocharger
EP1783343B1 (fr) * 2005-11-07 2019-10-09 Garrett Transportation I Inc. Structure de rétention pour turbocompresseur

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10014810A1 (de) * 2000-03-27 2001-10-11 Abb Turbo Systems Ag Baden Radialturbine eines Abgasturboladers
DE10050931C5 (de) * 2000-10-13 2007-03-29 Man Diesel Se Turbomaschine mit radial durchströmten Laufrad
TW576886B (en) 2001-05-04 2004-02-21 Abb Turbo Systems Ag Turbocharger having a radial-flow compressor and burst-protection arrangement for a radial-flow compressor of a turbocharger
DE10220573C1 (de) 2002-05-08 2003-07-03 Mtu Friedrichshafen Gmbh Abgasturbolader
EP1719879B1 (fr) * 2005-05-03 2008-01-30 ABB Turbo Systems AG Dispositif de protection en cas d'éclatement pour compresseur radial
DE102006041321A1 (de) * 2006-09-01 2008-03-06 Rolls-Royce Deutschland Ltd & Co Kg Gehäuseabschnitt, insbesondere Fangehäuse, für ein Gasturbinentriebwerk
JP4876959B2 (ja) * 2007-02-19 2012-02-15 株式会社Ｉｈｉ 過給機
DE102008061398A1 (de) 2008-12-10 2010-06-17 Man Diesel Se Berstschutz für eine Strömungsmaschine
DE102008062363A1 (de) 2008-12-17 2010-06-24 Rolls-Royce Deutschland Ltd & Co Kg Fangehäuse für ein Strahltriebwerk
DE102009009129B4 (de) 2009-02-17 2022-11-03 BMTS Technology GmbH & Co. KG Turbolader mit variabler Turbinengeometrie
DE102009049841B4 (de) 2009-10-14 2015-01-15 Mtu Friedrichshafen Gmbh Gasturbomaschine und Brennkraftmaschine
JP4905565B2 (ja) 2010-02-04 2012-03-28 トヨタ自動車株式会社 ターボチャージャおよびそのホイールハウジング
JP5511725B2 (ja) * 2011-03-31 2014-06-04 三菱重工業株式会社 板金タービンハウジング
JP6456596B2 (ja) * 2014-03-31 2019-01-23 三菱重工業株式会社 遠心圧縮機、過給機、および遠心圧縮機の製造方法
JP6541956B2 (ja) * 2014-10-17 2019-07-10 三菱重工業株式会社 遠心圧縮機およびそれを備えた過給機
DE102014012123A1 (de) * 2014-08-14 2016-02-18 Man Diesel & Turbo Se Abgasturbolader
DE102016012317A1 (de) 2016-10-15 2018-04-19 Daimler Ag Radialturbine für einen Abgasturbolader
JP6624338B2 (ja) 2017-03-17 2019-12-25 株式会社Ihi 可変ノズルユニットのシール構造および可変容量型過給機
DE102018101066A1 (de) 2018-01-18 2019-07-18 Man Energy Solutions Se Berstschutzvorrichtung für eine Gasturbomaschine
DE102018110235A1 (de) * 2018-04-27 2019-10-31 Man Energy Solutions Se Turbolader
DE102018114093A1 (de) * 2018-06-13 2019-12-19 Man Energy Solutions Se Berstschutzvorrichtung für eine Gasturbomaschine
DE102018129128A1 (de) 2018-11-20 2020-05-20 Man Energy Solutions Se Einsatzstück für einen Turbolader
DE102020213708A1 (de) 2020-10-30 2022-05-05 Mtu Friedrichshafen Gmbh Turbinen-Anordnung für einen Abgasturbolader
DE102020213709A1 (de) 2020-10-30 2022-05-05 Mtu Friedrichshafen Gmbh Turbinen-Anordnung für einen Abgasturbolader
DE102021113581A1 (de) 2021-05-26 2022-12-01 Rolls-Royce Solutions GmbH Turbinenanordnung für einen Abgasturbolader

Citations (4)

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US2935294A (en) * 1957-01-22 1960-05-03 Thompson Ramo Wooldridge Inc Double wall turbine shroud
DE2706110A1 (de) * 1977-02-14 1978-08-17 Kuehnle Kopp Kausch Ag Verdichtergehaeuse vorzugsweise fuer abgasturbolader
US5271220A (en) * 1992-10-16 1993-12-21 Sundstrand Corporation Combustor heat shield for a turbine containment ring
DE4223496A1 (de) 1992-07-17 1994-01-20 Asea Brown Boveri Vorrichtung zum Reduzieren der kinetischen Energie von berstenden Teilen

Family Cites Families (4)

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FR2448626A1 (fr) * 1979-02-08 1980-09-05 Snecma Perfectionnement aux rotors de machines tournantes
FR2467978A1 (fr) * 1979-10-23 1981-04-30 Snecma Dispositif de retention pour carter de compresseur d'une turbomachine
US4534698A (en) * 1983-04-25 1985-08-13 General Electric Company Blade containment structure
DE3704197C1 (de) * 1987-02-11 1987-08-20 Mtu Muenchen Gmbh Demontierbarer Berstschutzring

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2935294A (en) * 1957-01-22 1960-05-03 Thompson Ramo Wooldridge Inc Double wall turbine shroud
DE2706110A1 (de) * 1977-02-14 1978-08-17 Kuehnle Kopp Kausch Ag Verdichtergehaeuse vorzugsweise fuer abgasturbolader
DE4223496A1 (de) 1992-07-17 1994-01-20 Asea Brown Boveri Vorrichtung zum Reduzieren der kinetischen Energie von berstenden Teilen
US5271220A (en) * 1992-10-16 1993-12-21 Sundstrand Corporation Combustor heat shield for a turbine containment ring

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000034628A1 (fr) * 1998-12-07 2000-06-15 Pratt & Whitney Canada Corp. Systeme de confinement pour turbine
US6224321B1 (en) 1998-12-07 2001-05-01 Pratt & Whitney Canada Inc. Impeller containment system
GB2357120A (en) * 1999-12-09 2001-06-13 Alexander Cameron Henderson Catalyst coated turbocharger turbine
KR100794974B1 (ko) * 2001-02-20 2008-01-15 만 디젤 에스이 반경류 컴프레서 임펠러를 구비한 터보머신
US6638007B2 (en) 2001-02-20 2003-10-28 Man B&W Diesel Aktiengesellschaft Turbomachine with radial-flow compressor impeller
EP1233190A1 (fr) * 2001-02-20 2002-08-21 MAN B&W Diesel AG Turbomachine avec une roue à aubes radiale
GB2414769A (en) * 2004-06-05 2005-12-07 Man B & W Diesel Ag Turbo-machine with impeller containment assembly.
GB2414769B (en) * 2004-06-05 2009-11-04 Man B & W Diesel Ag Turbo-machine having a compressor wheel with radial flow
EP1783343B1 (fr) * 2005-11-07 2019-10-09 Garrett Transportation I Inc. Structure de rétention pour turbocompresseur
WO2007075532A2 (fr) * 2005-12-23 2007-07-05 Honeywell International Inc. Boîtier de compresseur à pièces multiples
WO2007075532A3 (fr) * 2005-12-23 2007-09-13 Honeywell Int Inc Boîtier de compresseur à pièces multiples
US7568338B2 (en) 2005-12-23 2009-08-04 Honeywell International Inc. Multi-piece compressor housing
WO2007124559A1 (fr) * 2006-04-27 2007-11-08 Pratt & Whitney Canada Corp. Élément de confinement de rotor ayant des connections cassantes
US7874136B2 (en) 2006-04-27 2011-01-25 Pratt & Whitney Canada Corp. Rotor containment element with frangible connections
US9091208B2 (en) 2010-07-16 2015-07-28 Honeywell International Inc. Turbocharger bearing housing assembly
US9021802B2 (en) 2010-08-26 2015-05-05 Honeywell International Inc. Turbine housing assembly with wastegate
US9097120B2 (en) 2010-08-26 2015-08-04 Honeywell International Inc. Turbine housing assembly
US20120263584A1 (en) * 2011-04-14 2012-10-18 Mann+Hummel Gmbh Compressor Housing of a Radial Compressor
EP3009634A4 (fr) * 2013-09-25 2016-09-14 Mitsubishi Heavy Ind Ltd Compresseur et compresseur à suralimentation
WO2015132616A1 (fr) * 2014-03-07 2015-09-11 Cummins Ltd Turbine
EP3067569A4 (fr) * 2014-03-31 2016-12-21 Mitsubishi Heavy Ind Ltd Compresseur centrifuge, compresseur de suralimentation et procédé de fabrication de compresseur centrifuge
CN106164497A (zh) * 2014-03-31 2016-11-23 三菱重工业株式会社 离心压缩机、增压器及离心压缩机的制造方法
KR20160088922A (ko) * 2014-03-31 2016-07-26 미츠비시 쥬고교 가부시키가이샤 원심 압축기, 과급기, 및 원심 압축기의 제조 방법
CN106164497B (zh) * 2014-03-31 2019-06-28 三菱重工业株式会社 离心压缩机、增压器及离心压缩机的制造方法
US9702266B2 (en) 2014-06-30 2017-07-11 Honeywell International Inc. Turbocharger turbine housing
DE102014212926A1 (de) * 2014-07-03 2016-01-07 Siemens Aktiengesellschaft Spiralgehäuse für einen Radialverdichter
DE102017109594A1 (de) * 2017-05-04 2018-11-08 Abb Turbo Systems Ag Verdichtergehäuse eines Radialverdichters
US20190301304A1 (en) * 2018-03-27 2019-10-03 Man Energy Solutions Se Turbocharger
CN110307048A (zh) * 2018-03-27 2019-10-08 曼恩能源方案有限公司 涡轮增压器
US11041408B2 (en) * 2018-03-27 2021-06-22 Man Energy Solutions Se Turbocharger

Also Published As

Publication number Publication date
KR19980032381A (ko) 1998-07-25
JPH10110622A (ja) 1998-04-28
PL322377A1 (en) 1998-04-14
CZ309997A3 (cs) 1998-04-15
DE19640654A1 (de) 1998-04-09

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