EP2092174B1 - Turbocompresseur - Google Patents
Turbocompresseur Download PDFInfo
- Publication number
- EP2092174B1 EP2092174B1 EP07819254.9A EP07819254A EP2092174B1 EP 2092174 B1 EP2092174 B1 EP 2092174B1 EP 07819254 A EP07819254 A EP 07819254A EP 2092174 B1 EP2092174 B1 EP 2092174B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- turbine
- rotor shaft
- rotor
- turbine wheel
- wheel
- 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.)
- Not-in-force
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/266—Rotors specially for elastic fluids mounting compressor rotors on shafts
-
- 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
- F02B37/16—Control of the pumps by bypassing charging air
-
- 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
- F01D25/18—Lubricating arrangements
- F01D25/183—Sealing means
- F01D25/186—Sealing means for sliding contact bearing
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/025—Fixing blade carrying members on shafts
-
- 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
-
- 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
-
- 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
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/16—Other safety measures for, or other control of, pumps
-
- 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 turbocharger according to the preamble of claim 1.
- a generic turbocharger is from the US 5 176 497 A .
- EP 1 394 387 A US 2000/001522 A1 or the WO 99/07982 A known.
- the piston ring recesses or grooves were always arranged in the rotor shaft.
- one respective groove is provided per piston ring or that two piston rings are arranged in a groove.
- the turbinenradnahe Kolbenringnut requires a constructive minimum distance from the turbine and the connection pin is kept axially as short as possible at the Turbinenraapp, it is not yet possible to introduce two grooves in the shaft area without weakening the shaft in cross section or without axially extending the shaft, which is very negative Effects on rotor bearing stability. If the turbine wheel and the rotor shaft connected by a weld, it was not possible, the Kolbenringnuten arbitrary
- the area of the weld is not suitable for the attachment of the grooves.
- turbocharger for an internal combustion engine according to the preamble of claim 1, which has a turbine rotor, which allows without increasing the axial rotor length to avoid deterioration of the arrangement by the attachment of piston ring grooves.
- Fig. 1 an inventive turbocharger 1 is illustrated in a partially broken view.
- the turbocharger 1 has a turbine 2 which comprises an exhaust gas inlet opening 3 and an exhaust gas outlet opening 4.
- a turbine wheel 5 is disposed in the turbine housing of the turbine 2, which is fixed to one end of a rotor shaft 6.
- a plurality of blades is arranged in the turbine housing between the exhaust gas inlet opening 3 and the turbine wheel 5.
- the turbocharger 1 has a compressor 8, which comprises a compressor wheel 9, which is fastened on the other end of the rotor shaft 6 and arranged in the compressor housing 8 of the compressor.
- turbocharger 1 also includes all other conventional components of a turbocharger, such as a bearing housing with a bearing housing unit, etc., which, however, will not be described below since they are not necessary for the explanation of the principles of the present invention.
- FIG. 2 is a part of a turbine rotor 10 shown in section, the rotor shaft 6 and the turbine wheel 5 with the inventive arrangement of Kolbenringeinsstichen 11, 11 ' on an extended, one-piece connecting pin 17 of the turbine wheel 5 shows.
- this shaping of the turbine wheel 5 it is achieved that all structurally required piston ring punctures 11, 11 'are formed in the heat-resistant material of the turbine wheel 5 which is more heat-resistant than the material alloy of the rotor shaft 6.
- This arrangement of Kolbenringeinsstiche 11, 11 'in identical material creates identical tribological conditions for the piston rings to be installed therein (which are not shown in this figure).
- the turbine wheel 5 has a cylindrical cavity 15 whose depth L, measured from the axial shaft-side end face 14 of the connecting pin 17 to a wheel back 13 of the turbine wheel 5, is smaller than a length B of the connecting pin 17.
- the rotor shaft 6 and the turbine wheel 5 can be connected to each other at the connection plane A either by friction welding or electron beam welding.
- the rotor shaft 6 has a short stub shaft 16.
- the inventive design of the connecting pin 17 of the turbine wheel 5 has the advantage that it can be easily pressed onto the stub shaft 16 and the risks of the occurrence of stresses during the welding process and possible resulting cracking can be minimized by the existing at the connection level A on both components material or wall thicknesses.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Supercharger (AREA)
Claims (3)
- Turbocompresseur (1)- comportant un compresseur (8) qui comprend une roue de compresseur (9) qui est fixée sur une extrémité d'un arbre de rotor (6) ;- comportant une turbine (2) qui comprend un rotor de turbine (10) qui comporte une roue de turbine (5) qui comprend un tourillon de connexion (17) qui peut être relié à une partie de raccordement (12) de l'arbre de rotor (6), et- comportant au moins une gorge d'anneau de piston (11, 11') qui est prévue sur le rotor de turbine (10) ; caractérisé- en ce que deux gorges d'anneau de piston (11, 11') sont disposées sur le tourillon de connexion (17), et- en ce que le tourillon de connexion (17) de la roue de turbine (5) comprend une cavité cylindrique (15) dont la profondeur (L) est inférieure à une longueur (B) du tourillon de connexion (17), mesurée à partir d'une surface d'extrémité (14) axiale côté arbre de l'arbre de rotor (6) jusqu'à un dos de roue (13) de la roue de turbine (5).
- Turbocompresseur selon la revendication 1, caractérisé en ce qu'un plan de liaison (A) entre l'arbre de rotor (6) et la roue de turbine (5) est disposé de manière espacée par rapport à la gorge d'anneau de piston (11, 11') la plus proche.
- Turbocompresseur selon la revendication 1, caractérisé en ce que la roue de turbine (5) et l'arbre de rotor (6) sont reliés par une soudure par friction ou par une soudure par faisceau d'électrons.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006058339 | 2006-12-11 | ||
PCT/EP2007/009193 WO2008071253A1 (fr) | 2006-12-11 | 2007-10-23 | Turbocompresseur |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2092174A1 EP2092174A1 (fr) | 2009-08-26 |
EP2092174B1 true EP2092174B1 (fr) | 2015-09-09 |
Family
ID=39015735
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07819254.9A Not-in-force EP2092174B1 (fr) | 2006-12-11 | 2007-10-23 | Turbocompresseur |
Country Status (6)
Country | Link |
---|---|
US (1) | US8465261B2 (fr) |
EP (1) | EP2092174B1 (fr) |
JP (1) | JP2010512481A (fr) |
KR (1) | KR20090087885A (fr) |
CN (1) | CN101542088A (fr) |
WO (1) | WO2008071253A1 (fr) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20090087885A (ko) * | 2006-12-11 | 2009-08-18 | 보르그워너 인코퍼레이티드 | 터보차저 |
DE102008038007A1 (de) | 2008-08-16 | 2010-02-18 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Abgasturbolader |
JP5157813B2 (ja) * | 2008-10-17 | 2013-03-06 | トヨタ自動車株式会社 | ターボ過給機 |
DE102009030042A1 (de) | 2009-06-23 | 2011-01-05 | Continental Automotive Gmbh | Turbinenläufer für einen Turbolader und Verfahren zur Herstellung eines Turbinenläufers |
JP5538569B2 (ja) * | 2010-02-19 | 2014-07-02 | ボーグワーナー インコーポレーテッド | タービンホイール、およびタービンホイールを製造するための方法 |
US20120076639A1 (en) * | 2010-09-27 | 2012-03-29 | Nicolas Vazeille | Shaft and Turbine Wheel Assembly |
DE102010054905A1 (de) | 2010-12-17 | 2012-06-21 | Schaeffler Technologies Gmbh & Co. Kg | Lagereinheit für einen Turbolader |
DE102010054939A1 (de) * | 2010-12-17 | 2012-06-21 | Schaeffler Technologies Gmbh & Co. Kg | Lageranordnung für einen Turbolader und Turbolader |
KR101940588B1 (ko) * | 2011-11-15 | 2019-01-21 | 보르그워너 인코퍼레이티드 | 유동 로터, 특히 터빈 휠 |
DE102012202272B4 (de) * | 2012-02-15 | 2021-05-12 | BMTS Technology GmbH & Co. KG | Rotor einer Ladeeinrichtung und Ladeeinrichtung |
JP5966417B2 (ja) * | 2012-02-20 | 2016-08-10 | 株式会社Ihi | 過給機 |
DE112013000971B4 (de) * | 2012-03-15 | 2022-12-15 | Borgwarner Inc. | Abgasturbolader |
JP5408283B2 (ja) * | 2012-04-20 | 2014-02-05 | トヨタ自動車株式会社 | ターボ過給機 |
US9624776B2 (en) | 2012-05-03 | 2017-04-18 | Borgwarner Inc. | Reduced stress superback wheel |
DE102014213641A1 (de) * | 2014-01-17 | 2015-08-06 | Borgwarner Inc. | Verfahren zur Verbindung eines Verdichterrades mit einer Welle einer Aufladeeinrichtung |
US9827631B2 (en) | 2014-09-16 | 2017-11-28 | Honeywell International Inc. | Turbocharger shaft and wheel assembly |
US9821410B2 (en) | 2014-09-16 | 2017-11-21 | Honeywell International Inc. | Turbocharger shaft and wheel assembly |
US10041351B2 (en) | 2014-09-16 | 2018-08-07 | Honeywell International Inc. | Turbocharger shaft and wheel assembly |
US10024166B2 (en) | 2014-09-16 | 2018-07-17 | Honeywell International Inc. | Turbocharger shaft and wheel assembly |
CN104500268A (zh) * | 2014-12-12 | 2015-04-08 | 常州环能涡轮动力股份有限公司 | 具有双面离心压轮的微型涡轮喷气发动机 |
US10603740B2 (en) * | 2015-02-09 | 2020-03-31 | Borgwarner Inc. | Method of joining by electron beam or laser welding a turbocharger turbine wheel to a shaft; corresponding turbocharger turbine wheel |
US9915172B2 (en) | 2015-03-09 | 2018-03-13 | Caterpillar Inc. | Turbocharger with bearing piloted compressor wheel |
US9810238B2 (en) | 2015-03-09 | 2017-11-07 | Caterpillar Inc. | Turbocharger with turbine shroud |
US9822700B2 (en) | 2015-03-09 | 2017-11-21 | Caterpillar Inc. | Turbocharger with oil containment arrangement |
US9650913B2 (en) | 2015-03-09 | 2017-05-16 | Caterpillar Inc. | Turbocharger turbine containment structure |
US9903225B2 (en) | 2015-03-09 | 2018-02-27 | Caterpillar Inc. | Turbocharger with low carbon steel shaft |
US10006341B2 (en) | 2015-03-09 | 2018-06-26 | Caterpillar Inc. | Compressor assembly having a diffuser ring with tabs |
US9890788B2 (en) | 2015-03-09 | 2018-02-13 | Caterpillar Inc. | Turbocharger and method |
US9638138B2 (en) | 2015-03-09 | 2017-05-02 | Caterpillar Inc. | Turbocharger and method |
US9739238B2 (en) | 2015-03-09 | 2017-08-22 | Caterpillar Inc. | Turbocharger and method |
US9752536B2 (en) | 2015-03-09 | 2017-09-05 | Caterpillar Inc. | Turbocharger and method |
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 |
US9683520B2 (en) | 2015-03-09 | 2017-06-20 | Caterpillar Inc. | Turbocharger and method |
US9777747B2 (en) | 2015-03-09 | 2017-10-03 | Caterpillar Inc. | Turbocharger with dual-use mounting holes |
US10066639B2 (en) | 2015-03-09 | 2018-09-04 | Caterpillar Inc. | Compressor assembly having a vaneless space |
US9267441B1 (en) | 2015-03-17 | 2016-02-23 | Borgwarner Inc. | Multi-piece piston ring for a turbocharger shaft assembly |
US10024228B2 (en) * | 2015-10-08 | 2018-07-17 | Honeywell International Inc. | Compressor recirculation valve with noise-suppressing muffler |
JP6705266B2 (ja) * | 2016-04-07 | 2020-06-03 | オムロン株式会社 | 制御装置、制御方法およびプログラム |
US20190112927A1 (en) | 2017-10-12 | 2019-04-18 | Borgwarner Inc. | Turbocharger having improved turbine wheel |
CN108626167A (zh) * | 2018-04-28 | 2018-10-09 | 江苏锡宇汽车有限公司 | 加固型涡轮增压器转子总成 |
TWI745771B (zh) * | 2019-10-23 | 2021-11-11 | 峰安車業股份有限公司 | 渦輪轉子頭與軸身之接合方式及渦輪轉子 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
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GB1430308A (en) * | 1973-04-06 | 1976-03-31 | Woollenweber W E | Rotatable assembly |
US4408959A (en) * | 1980-07-03 | 1983-10-11 | Kennecott Corporation | Ceramic radial turbine wheel |
JPS5793606A (en) * | 1980-12-02 | 1982-06-10 | Mitsubishi Heavy Ind Ltd | Impeller and manufacturing method thereof |
EP0138516A1 (fr) * | 1983-10-07 | 1985-04-24 | Household Manufacturing, Inc. | Roue de compresseur centrifuge et son montage sur l'arbre |
JPS60120201U (ja) * | 1984-01-21 | 1985-08-14 | 日本特殊陶業株式会社 | タ−ボ過給機の軸 |
DE3535511A1 (de) * | 1984-10-06 | 1986-04-17 | Ngk Spark Plug Co., Ltd., Nagoya, Aichi | Verbindungsanordnung zwischen einer keramik- und einer metallwelle |
JPS61167128A (ja) * | 1985-01-18 | 1986-07-28 | Nissan Motor Co Ltd | タ−ボチヤ−ジヤの潤滑油流出防止装置 |
JPS61215270A (ja) * | 1985-03-15 | 1986-09-25 | 日本特殊陶業株式会社 | タ−ビンロ−ター |
US5176497A (en) * | 1991-01-22 | 1993-01-05 | Allied-Signal Inc. | Boreless hub compressor wheel assembly for a turbocharger |
US6017184A (en) * | 1997-08-06 | 2000-01-25 | Allied Signal Inc. | Turbocharger integrated bearing system |
US6481970B2 (en) * | 2000-06-28 | 2002-11-19 | Honeywell International Inc. | Compressor wheel with prestressed hub and interference fit insert |
JP2002235547A (ja) * | 2001-02-09 | 2002-08-23 | Shozo Shimizu | ターボチャージャ用タービン軸の接合方法 |
GB2392477A (en) * | 2002-08-24 | 2004-03-03 | Alstom | Turbocharger |
GB0425088D0 (en) * | 2004-11-13 | 2004-12-15 | Holset Engineering Co | Compressor wheel |
KR20090087885A (ko) * | 2006-12-11 | 2009-08-18 | 보르그워너 인코퍼레이티드 | 터보차저 |
-
2007
- 2007-10-23 KR KR1020097009850A patent/KR20090087885A/ko not_active Application Discontinuation
- 2007-10-23 EP EP07819254.9A patent/EP2092174B1/fr not_active Not-in-force
- 2007-10-23 JP JP2009539622A patent/JP2010512481A/ja active Pending
- 2007-10-23 US US12/517,389 patent/US8465261B2/en not_active Expired - Fee Related
- 2007-10-23 WO PCT/EP2007/009193 patent/WO2008071253A1/fr active Application Filing
- 2007-10-23 CN CNA2007800432959A patent/CN101542088A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
US8465261B2 (en) | 2013-06-18 |
KR20090087885A (ko) | 2009-08-18 |
WO2008071253A1 (fr) | 2008-06-19 |
US20100003132A1 (en) | 2010-01-07 |
CN101542088A (zh) | 2009-09-23 |
JP2010512481A (ja) | 2010-04-22 |
EP2092174A1 (fr) | 2009-08-26 |
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