DE102013002605A1 - Turbocharger and thrust bearing for a turbocharger - Google Patents
Turbocharger and thrust bearing for a turbocharger Download PDFInfo
- Publication number
- DE102013002605A1 DE102013002605A1 DE102013002605.9A DE102013002605A DE102013002605A1 DE 102013002605 A1 DE102013002605 A1 DE 102013002605A1 DE 102013002605 A DE102013002605 A DE 102013002605A DE 102013002605 A1 DE102013002605 A1 DE 102013002605A1
- Authority
- DE
- Germany
- Prior art keywords
- turbocharger
- turbine
- compressor
- rotor
- axial bearing
- 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.)
- Pending
Links
- 239000002131 composite material Substances 0.000 claims abstract description 6
- 239000000835 fiber Substances 0.000 claims abstract description 6
- 235000013929 Psidium pyriferum Nutrition 0.000 claims abstract 2
- 244000236580 Psidium pyriferum Species 0.000 claims abstract 2
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 9
- 239000004917 carbon fiber Substances 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 8
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 7
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 7
- 239000003921 oil Substances 0.000 claims description 5
- 229910010293 ceramic material Inorganic materials 0.000 claims description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 4
- 230000006835 compression Effects 0.000 claims description 2
- 238000007906 compression Methods 0.000 claims description 2
- 238000013022 venting Methods 0.000 abstract 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000002040 relaxant effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Images
Classifications
-
- 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
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/166—Sliding contact bearing
- F01D25/168—Sliding contact bearing for axial load mainly
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/043—Sliding surface consisting mainly of ceramics, cermets or hard carbon, e.g. diamond like carbon [DLC]
-
- 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
- F05D2240/00—Components
- F05D2240/50—Bearings
- F05D2240/52—Axial thrust bearings
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/226—Carbides
- F05D2300/2261—Carbides of silicon
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
- F16C2360/24—Turbochargers
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Supercharger (AREA)
- Sliding-Contact Bearings (AREA)
Abstract
Turbolader, mit einer einen beschaufelten Turbinenrotor (19) und ein Turbinengehäuse (18) aufweisenden Turbine (11) zur Entspannung von Abas und mit einem einen beschaufelten Verdichterrotor (20) und ein Verdichtergehäuse (17) aufweisen Verdichter (12) zur Verdichtung von Ladeluft, wobei der Verdichterrotor (20) ausgehend vom Turbinenrotor (19) antreibbar und hierzu mit dem Turbinenrotor (19) über eine ein Axiallager (25) aufweisende Welle (21) gekoppelt ist, wobei das Axiallager (25) eine Axiallagerscheibe aufweist, und wobei die Axiallagerscheibe aus einem Faserverbundwerkstoff gefertigt ist.A turbocharger comprising a bladed turbine rotor (19) and a turbine housing (18) for venting abas and having a bladed compressor rotor (20) and a compressor housing (17) for compressing charge air compressor (12), wherein the compressor rotor (20), starting from the turbine rotor (19) drivable and this with the turbine rotor (19) via a thrust bearing (25) having a shaft (21) is coupled, wherein the thrust bearing (25) has a thrust washer, and wherein the thrust washer is made of a fiber composite material.
Description
Die Erfindung betrifft einen Turbolader nach dem Oberbegriff des Anspruchs 1. Des Weiteren betrifft die Erfindung eine Axiallagerscheibe für einen Turbolader.The invention relates to a turbocharger according to the preamble of claim 1. Furthermore, the invention relates to a thrust bearing for a turbocharger.
Der grundsätzliche Aufbau eines Turboladers ist hinlänglich bekannt. So verfügt ein Turbolader über eine Turbine zur Entspannung von Abgas und über einen Verdichter zur Verdichtung der Ladeluft. Die Turbine eines Turboladers verfügt über einen beschaufelten Turbinenrotor und ein Turbinengehäuse. Der Verdichter verfügt über einen beschaufelten Verdichterrotor und ein Verdichtergehäuse. Der Verdichterrotor des Verdichters ist ausgehend vom Turbinenrotor der Turbine antreibbar und hierzu mit dem Turbinenrotor über eine ein Axiallager aufweisende Welle gekoppelt. Das Axiallager umfasst eine Axiallagerscheibe, die nach dem Stand der Technik aus Bronze oder einem anderen metallischen Werkstoff gefertigt ist.The basic structure of a turbocharger is well known. For example, a turbocharger has a turbine for the expansion of exhaust gas and a compressor for compressing the charge air. The turbine of a turbocharger has a bladed turbine rotor and a turbine housing. The compressor has a bladed compressor rotor and a compressor housing. The compressor rotor of the compressor can be driven starting from the turbine rotor of the turbine and for this purpose coupled to the turbine rotor via a shaft having a thrust bearing. The thrust bearing comprises a thrust washer, which is made in the prior art of bronze or other metallic material.
Hiervon ausgehend liegt der vorliegenden Erfindung die Aufgabe zugrunde, einen neuartigen Turbolader und eine neuartige Axiallagerscheibe für einen Turbolader zu schaffen.On this basis, the present invention has the object to provide a novel turbocharger and a new thrust bearing for a turbocharger.
Diese Aufgabe wird durch einen Turbolader nach Anspruch 1 gelöst. Erfindungsgemäß ist die Axiallagerscheibe aus einem Faserverbundwerkstoff gefertigt. Beim erfindungsgemäßen Turbolader ist die Axiallagerscheibe aus einem Faserverbundwerkstoff gefertigt. Hierdurch kann die Lebensdauer der Axiallagerscheibe des Axiallagers erhöht werden. Wartungsintervalle des Turboladers können verlängert werden.This object is achieved by a turbocharger according to claim 1. According to the invention the thrust washer is made of a fiber composite material. In the turbocharger invention, the thrust washer is made of a fiber composite material. As a result, the life of the thrust bearing of the thrust bearing can be increased. Maintenance intervals of the turbocharger can be extended.
Nach einer vorteilhaften Weiterbildung der Erfindung ist die Axiallagerscheibe aus einem mit Kohlestofffasern verstärkten, keramischen Werkstoff gefertigt. Vorzugsweise ist die Axiallagerscheibe aus einem mit Kohlenstofffasen verstärkten Siliziumcarbid Werkstoff gefertigt. Die Verwendung dieser Werkstoffe für die Axiallagerscheibe ist besonders bevorzugt, da dieselben besonders verschleißresistent sind.According to an advantageous embodiment of the invention, the thrust washer is made of a reinforced with carbon fibers, ceramic material. Preferably, the thrust washer is made of carbon fiber reinforced silicon carbide material. The use of these materials for the thrust washer is particularly preferred because they are particularly resistant to wear.
Nach einer weiteren vorteilhaften Weiterbildung der Erfindung sind in die Axiallagerscheibe Ölführnuten eingebracht. Über die Ölführnuten kann Kühlöl und/oder Schmieröl einfach und zuverlässig im Bereich des Axiallagers geführt werden.According to a further advantageous embodiment of the invention oil guide grooves are introduced into the thrust washer. Cooling oil and / or lubricating oil can be guided simply and reliably in the region of the axial bearing via the oil guide grooves.
Die erfindungsgemäße Axiallagerscheibe für einen Turbolader ist in Anspruch 5 definiert.The axial bearing washer for a turbocharger according to the invention is defined in claim 5.
Bevorzugte Weiterbildungen der Erfindung ergeben sich aus den Unteransprüchen und der nachfolgenden Beschreibung. Ausführungsbeispiele der Erfindung werden, ohne hierauf beschränkt zu sein, an Hand der Zeichnung näher erläutert. Dabei zeigt:Preferred embodiments of the invention will become apparent from the dependent claims and the description below. Embodiments of the invention will be described, without being limited thereto, with reference to the drawings. Showing:
Die hier vorliegende Erfindung betrifft einen Turbolader einer Brennkraftmaschine, insbesondere einen Turbolader einer Schiffsdieselbrennkraftmaschine.The present invention relates to a turbocharger of an internal combustion engine, in particular a turbocharger of a marine diesel engine.
Zu entspannendes Abgas ist der Turbine
Zu verdichtende Ladeluft ist dem Verdichter
Der Lufteinlass
Der Abgaseinlass
Die Turbine
Der Verdichter
Der Verdichterrotor
Die Lagerung für die Welle
Die Axiallagerscheibe
Ein solcher mit Kohlestofffasern verstärkter Siliziumcarbid Werkstoff verfügt über eine hohe Verschleißunanfälligkeit und eignet sich besonders bevorzugt zur Ausbildung der Axiallagerscheibe
Bevorzugt findet ein kohlestofffaserverstärkter Siliziumcarbid Werkstoff mit folgenden Eigenschaften Verwendung: Dichte: 1,8–2,8 g/cm3; Bruchdehnung: 0,05–0.8%; Hochtemperaturbeständigkeit bis 1350°C; Wärmedehnung: 1,5–3,8 10-6/K; Koeffizient der Thermoschockbeständigkeit: 46–83 kW/m; Spezifische Wärmekapazität: 0,6–1,7 J/g·K; Wärmeleitfähigkeit: 20–125 W/m·K.A carbon fiber-reinforced silicon carbide material preferably has the following properties: density: 1.8-2.8 g / cm3; Elongation at break: 0.05-0.8%; High temperature resistance up to 1350 ° C; Thermal expansion: 1.5-3.8 10-6 / K; Coefficient of thermal shock resistance: 46-83 kW / m; Specific heat capacity: 0.6-1.7 J / g · K; Thermal conductivity: 20-125 W / m · K.
Nach einer vorteilhaften Weiterbildung der Erfindung sind in die Axiallagerscheibe
Gemäß
In
BezugszeichenlisteLIST OF REFERENCE NUMBERS
- 1010
- Turboladerturbocharger
- 1111
- Turbineturbine
- 1212
- Verdichtercompressor
- 1313
- Abgaseinlassexhaust inlet
- 1414
- Abgasauslassexhaust outlet
- 1515
- Lufteinlassair intake
- 1616
- Ladeluftauslasscharge air outlet
- 1717
- Verdichtergehäusecompressor housing
- 1818
- Turbinengehäuseturbine housing
- 1919
- Turbinenrotorturbine rotor
- 2020
- Verdichterrotorcompressor rotor
- 2121
- Wellewave
- 2222
- Lagerbuchsebearing bush
- 2323
- Lagerbuchsebearing bush
- 2424
- Lagergehäusebearing housing
- 2525
- Axiallagerthrust
- 2626
- Widerlagerabutment
- 2727
- Axiallagerscheibeaxial bearing
- 2828
- Axiallagerringthrust bearing
- 2929
- ÖlführnutÖlführnut
Claims (8)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013002605.9A DE102013002605A1 (en) | 2013-02-15 | 2013-02-15 | Turbocharger and thrust bearing for a turbocharger |
CH00180/14A CH707584B1 (en) | 2013-02-15 | 2014-02-11 | Turbocharger and thrust washer for such a turbocharger. |
KR1020140015784A KR102008537B1 (en) | 2013-02-15 | 2014-02-12 | Turbocharger and axial bearing disc for a turbocharger |
JP2014026338A JP2014156859A (en) | 2013-02-15 | 2014-02-14 | Turbocharger and axial bearing disk for the same |
CN201410051142.0A CN103993918A (en) | 2013-02-15 | 2014-02-14 | Turbocharger and axial bearing disc applied in same |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013002605.9A DE102013002605A1 (en) | 2013-02-15 | 2013-02-15 | Turbocharger and thrust bearing for a turbocharger |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102013002605A1 true DE102013002605A1 (en) | 2014-08-21 |
Family
ID=51263608
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102013002605.9A Pending DE102013002605A1 (en) | 2013-02-15 | 2013-02-15 | Turbocharger and thrust bearing for a turbocharger |
Country Status (5)
Country | Link |
---|---|
JP (1) | JP2014156859A (en) |
KR (1) | KR102008537B1 (en) |
CN (1) | CN103993918A (en) |
CH (1) | CH707584B1 (en) |
DE (1) | DE102013002605A1 (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102016117960A1 (en) | 2016-09-23 | 2018-03-29 | Man Diesel & Turbo Se | turbocharger |
DE102016123249A1 (en) | 2016-12-01 | 2018-06-07 | Man Diesel & Turbo Se | turbocharger |
WO2018099619A1 (en) | 2016-12-01 | 2018-06-07 | Man Diesel & Turbo Se | Turbocharger |
DE102017107381A1 (en) | 2017-04-06 | 2018-10-11 | Man Diesel & Turbo Se | turbocharger |
DE102017215569A1 (en) | 2017-09-05 | 2019-03-07 | Man Diesel & Turbo Se | turbocharger |
DE102017215539A1 (en) | 2017-09-05 | 2019-03-07 | Man Diesel & Turbo Se | turbocharger |
DE102017126950A1 (en) | 2017-11-16 | 2019-05-16 | Man Energy Solutions Se | turbocharger |
DE102017126933A1 (en) | 2017-11-16 | 2019-05-16 | Man Energy Solutions Se | turbocharger |
DE102017126935A1 (en) | 2017-11-16 | 2019-05-16 | Man Energy Solutions Se | turbocharger |
DE102017126936A1 (en) | 2017-11-16 | 2019-05-16 | Man Energy Solutions Se | turbocharger |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6463640B2 (en) * | 2015-01-27 | 2019-02-06 | 川崎重工業株式会社 | Marine exhaust turbine |
DE102016207698A1 (en) * | 2016-05-04 | 2017-11-09 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | loader |
DE102017207173B4 (en) * | 2017-04-28 | 2022-12-22 | Vitesco Technologies GmbH | Turbocharger with predetermined breaking point for an internal combustion engine |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5884420U (en) * | 1981-12-03 | 1983-06-08 | 本田技研工業株式会社 | thrust bearing device |
DE19641673B4 (en) * | 1996-10-11 | 2005-09-01 | Abb Turbo Systems Ag | axial plain |
JP4331441B2 (en) * | 2002-05-30 | 2009-09-16 | 株式会社荏原製作所 | Plain bearings and rotating machinery |
JP4296292B2 (en) * | 2003-10-31 | 2009-07-15 | 株式会社豊田中央研究所 | Fluid bearing |
CN1945038A (en) * | 2006-06-05 | 2007-04-11 | 肖忠渊 | Oilless lubricating bearing made from carbon fibre composite material |
EP2006497A1 (en) * | 2007-06-21 | 2008-12-24 | Siemens Aktiengesellschaft | Axial disc for the rotor of a turbo engine and turbo machine rotor |
GB2453143A (en) * | 2007-09-27 | 2009-04-01 | Siemens Ag | A method of preventing damage to a bearing |
DE102008011258A1 (en) * | 2008-02-27 | 2009-09-10 | Continental Automotive Gmbh | Cooled housing consisting of a turbine housing and a bearing housing of a turbocharger |
DE102008031730A1 (en) * | 2008-07-04 | 2010-01-07 | Daimler Ag | Bearing housing for exhaust gas turbo charger of internal-combustion engine, has bearing surface for mounting shaft, by which turbine wheel and compressor wheel are coupled with one another |
DE102010027770B4 (en) * | 2010-04-15 | 2012-03-22 | Man Diesel & Turbo Se | turbocharger |
CN102817921A (en) * | 2012-08-30 | 2012-12-12 | 吉林省达美水利水电工程有限公司 | Bearing and outer ring thereof |
-
2013
- 2013-02-15 DE DE102013002605.9A patent/DE102013002605A1/en active Pending
-
2014
- 2014-02-11 CH CH00180/14A patent/CH707584B1/en unknown
- 2014-02-12 KR KR1020140015784A patent/KR102008537B1/en active IP Right Grant
- 2014-02-14 CN CN201410051142.0A patent/CN103993918A/en active Pending
- 2014-02-14 JP JP2014026338A patent/JP2014156859A/en active Pending
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10954963B2 (en) | 2016-09-23 | 2021-03-23 | Man Energy Solutions Se | Turbocharger |
DE102016117960A1 (en) | 2016-09-23 | 2018-03-29 | Man Diesel & Turbo Se | turbocharger |
DE102016123249A1 (en) | 2016-12-01 | 2018-06-07 | Man Diesel & Turbo Se | turbocharger |
WO2018099618A1 (en) | 2016-12-01 | 2018-06-07 | Man Diesel & Turbo Se | Turbocharger having sealing surfaces between a nozzle ring and a turbine housing |
WO2018099619A1 (en) | 2016-12-01 | 2018-06-07 | Man Diesel & Turbo Se | Turbocharger |
EP3548705B1 (en) * | 2016-12-01 | 2021-03-03 | MAN Energy Solutions SE | Turbocharger |
US10655497B2 (en) | 2017-04-06 | 2020-05-19 | Man Energy Solutions Se | Turbocharger |
DE102017107381A1 (en) | 2017-04-06 | 2018-10-11 | Man Diesel & Turbo Se | turbocharger |
DE102017215569A1 (en) | 2017-09-05 | 2019-03-07 | Man Diesel & Turbo Se | turbocharger |
DE102017215539A1 (en) | 2017-09-05 | 2019-03-07 | Man Diesel & Turbo Se | turbocharger |
US10746053B2 (en) | 2017-09-05 | 2020-08-18 | Man Energy Solutions Se | Turbocharger |
DE102017126933A1 (en) | 2017-11-16 | 2019-05-16 | Man Energy Solutions Se | turbocharger |
US10605306B2 (en) | 2017-11-16 | 2020-03-31 | Man Energy Solutions Se | Turbocharger |
US10648364B2 (en) | 2017-11-16 | 2020-05-12 | Man Energy Solutions Se | Turbocharger |
US10598043B2 (en) | 2017-11-16 | 2020-03-24 | Man Energy Solutions Se | Turbocharger |
DE102017126936A1 (en) | 2017-11-16 | 2019-05-16 | Man Energy Solutions Se | turbocharger |
DE102017126935A1 (en) | 2017-11-16 | 2019-05-16 | Man Energy Solutions Se | turbocharger |
DE102017126950A1 (en) | 2017-11-16 | 2019-05-16 | Man Energy Solutions Se | turbocharger |
Also Published As
Publication number | Publication date |
---|---|
KR20140103059A (en) | 2014-08-25 |
CH707584A2 (en) | 2014-08-15 |
CH707584B1 (en) | 2017-09-29 |
CN103993918A (en) | 2014-08-20 |
JP2014156859A (en) | 2014-08-28 |
KR102008537B1 (en) | 2019-08-07 |
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