DE102011086778A1 - Exhaust gas-turbo-loaded combustion engine i.e. diesel engine, has exhaust gas catalyst integrated in bypass strand behind high pressure turbine of supercharger, and bypass pipe in parallel connection to high pressure turbine - Google Patents

Exhaust gas-turbo-loaded combustion engine i.e. diesel engine, has exhaust gas catalyst integrated in bypass strand behind high pressure turbine of supercharger, and bypass pipe in parallel connection to high pressure turbine Download PDF

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DE102011086778A1
DE102011086778A1 DE102011086778A DE102011086778A DE102011086778A1 DE 102011086778 A1 DE102011086778 A1 DE 102011086778A1 DE 102011086778 A DE102011086778 A DE 102011086778A DE 102011086778 A DE102011086778 A DE 102011086778A DE 102011086778 A1 DE102011086778 A1 DE 102011086778A1
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exhaust gas
bypass
pressure turbine
high pressure
combustion engine
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German (de)
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Jens Tophoven
Andreas Mauch
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Robert Bosch GmbH
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Robert Bosch GmbH
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/18Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by methods of operation; Control
    • F01N3/20Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by methods of operation; Control specially adapted for catalytic conversion ; Methods of operation or control of catalytic converters
    • F01N3/2053By-passing catalytic reactors, e.g. to prevent overheating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/105General auxiliary catalysts, e.g. upstream or downstream of the main catalyst
    • F01N3/106Auxiliary oxidation catalysts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/004Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust drives arranged in series
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/013Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in series
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/18Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/18Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • F02B37/183Arrangements of bypass valves or actuators therefor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

The engine has an exhaust line (21) comprising an exhaust gas catalyst i.e. oxidation catalyst (15) such as pre-turbo catalyst, in a series arrangement with a high pressure turbine (14) and a low-pressure turbine (16) of first and second superchargers. A bypass pipe (22) is in a parallel connection to the high pressure turbine of the first supercharger. The exhaust gas catalyst is integrated in a bypass strand behind the high pressure turbine to a bypass flap (12), where the bypass strand and the bypass flap are integrated in a common bypass housing (13) adjacent to each other.

Description

Die Erfindung betrifft eine Brennkraftmaschine mit einem Abgastrang und mit zweistufiger Turboaufladung, wobei der Abgasstrang zwei Turbinen eines ersten und eines zweiten Abgasturboladers und mindestens einem Abgaskatalysator, insbesondere einem Oxidationskatalysator, in Reihenschaltung und eine Bypassleitung in Parallelschaltung zur Hochdruck-Turbine des ersten Abgasturboladers umfasst.The invention relates to an internal combustion engine with an exhaust line and two-stage turbocharging, wherein the exhaust system comprises two turbines of a first and a second exhaust gas turbocharger and at least one exhaust gas catalyst, in particular an oxidation catalyst in series and a bypass line in parallel to the high-pressure turbine of the first exhaust gas turbocharger.

Eine derartige Brennkraftmaschine ist aus der WO 2004/097195 A1 bekannt. Diese Brennkraftmaschine weist eine zweistufige Turboaufladung auf, wobei zwischen der Hochdruck-Turbine des ersten Turboladers und der Niederdruck-Turbine des zweiten Turboladers ein Oxidationskatalysator in die Verbindungsleitung eingesetzt ist. Um den Oxidationskatalysator in diese Verbindungsleitung einbauen zu können, ist eine Mindestdimensionierung dieser Verbindungsleitung erforderlich, um den Oxidationskatalysator unterbringen zu können. Zudem muss die Verbindungsleitung zur Aufnahme des Oxidationskatalysators ausgebildet sein, beispielsweise mit entsprechenden Flanschen zur Befestigung des in ein eigenes Gehäuse eingebauten Katalysators ausgebildet sein.Such an internal combustion engine is from the WO 2004/097195 A1 known. This internal combustion engine has a two-stage turbocharging, wherein an oxidation catalytic converter is inserted into the connecting line between the high-pressure turbine of the first turbocharger and the low-pressure turbine of the second turbocharger. In order to install the oxidation catalyst in this connection line, a minimum sizing of this connection line is required in order to accommodate the oxidation catalyst can. In addition, the connecting line for receiving the oxidation catalyst must be formed, for example, be formed with corresponding flanges for mounting the built-in a separate housing catalyst.

Der Erfindung liegt die Aufgabe zugrunde, eine abgasturboaufgeladene Brennkraftmaschine mit Abgaskatalysator bereit zu stellen, die hinsichtlich des Verbaus des Abgaskatalysator verbessert ist.The invention has for its object to provide a exhaust-gas-charged internal combustion engine with catalytic converter ready, which is improved in terms of the Verbaus the catalytic converter.

Offenbarung der ErfindungDisclosure of the invention

Vorteile der ErfindungAdvantages of the invention

Diese Aufgabe wird dadurch gelöst, dass der Abgaskatalysator, insbesondere ein Oxidationskatalysator, hinter der Hochdruck-Turbine des ersten Abgasturboladers in einen Bypassstrang einer Turbinenbypassklappe integriert ist, und dass der Bypassstrang und die Turbinenbypassklappe in einem gemeinsamen Bypassgehäuse integriert sind.This object is achieved in that the exhaust gas catalyst, in particular an oxidation catalyst, is integrated behind the high-pressure turbine of the first exhaust gas turbocharger in a bypass line of a turbine bypass valve, and that the bypass line and the turbine bypass valve are integrated in a common bypass housing.

Der Abgaskatalysator kann im Rahmen der Erfindung anstatt des Oxidationskatalysators auch ein 3-Wege-Katalysator für einen Ottomotor sein. Durch diese Ausgestaltung und Integration in das gemeinsame Bypassgehäuse ist keine zusätzliche Strecke oder Verbindungsleitung nach der Hochdruck-Turbine als Einbauort oder Einbauraum für den Oxidationskatalysator notwendig. Dadurch wird der Einfluss auf die Strömung und damit die zu erwartenden Druckverluste minimal. Bei der Integration des Oxidationskatalysators, der im Übrigen als sogenannter PTC (Pre Turbo Catalyst; Vorturbokatalysator) ausgebildet ist, in das Bypassgehäuse erfolgt keine Vergrößerung der Wandfläche und somit auch keine Steigerung der Wandwärmeverluste. Das Bypassgehäuse wird ohnehin im Betrieb der Brennkraftmaschine aufgeheizt, wobei das Gewicht und damit die Wärmekapazität des Katalysatormaterials vernachlässigbar sind. Zudem ist kein zusätzlicher Bauraum nötig; das System bleibt also kompakt. Ein genereller Vorteil eines Systems mit einem PTC gegenüber einem System ohne PTC ist die beschleunigte Einsatzbereitschaft des Oxidationskatalysators. Dadurch werden bei einem Kaltstart der entsprechend ausgerüsteten Brennkraftmaschine HC / CO-Emissionen früher konvertiert.In the context of the invention, the catalytic converter can also be a 3-way catalytic converter for a gasoline engine instead of the oxidation catalytic converter. Due to this configuration and integration in the common bypass housing no additional route or connection line to the high-pressure turbine as installation or installation space for the oxidation catalyst is necessary. As a result, the influence on the flow and thus the expected pressure losses is minimal. In the integration of the oxidation catalyst, which is otherwise designed as a so-called PTC (Pre Turbo Catalyst) in the bypass housing takes place no enlargement of the wall surface and thus no increase in wall heat losses. The bypass housing is in any case heated during operation of the internal combustion engine, wherein the weight and thus the heat capacity of the catalyst material are negligible. In addition, no additional space is needed; the system remains compact. A general advantage of a system with a PTC over a system without PTC is the accelerated readiness of the oxidation catalyst. As a result, HC / CO emissions are converted earlier in a cold start of the corresponding equipped engine.

Durch die erfindungsgemäße Ausgestaltung wird ein deutlich besseres Ansprechverhalten des Hochdruck-Verdichters des ersten Abgasturboladers im Vergleich mit einem System, das einen Oxidationskatalysator vor der Hochdruckturbine aufweist, erzielt, der seinerseits maßgeblich die Dynamik des Luftsystems bestimmt. Gegenüber einem System ohne Oxidationskatalysator ergeben sich keine Veränderungen beim Ansprechverhalten. Der Ladedruckaufbau zwischen dem System ohne und demjenigen mit einem Oxidationskatalysator zwischen der Hochdruck-Turbine des ersten Abgasturboladers und der Niederdruck-Turbine des zweiten Turboladers ist nahezu identisch. Der Temperaturverlust ist aber deutlich geringer im Vergleich zu einer Anordnung des Oxidationskatalysators beispielsweise vor der Hochdruck-Turbine des ersten Abgasturboladers. Zudem ist der Temperaturverlust von untergeordneter Bedeutung, da die Hauptarbeit bei einem Lastsprung ohnehin von dem Hochdruck-Lader des zweiten Abgasturboladers geleistet wird.As a result of the configuration according to the invention, a significantly better response of the high-pressure compressor of the first exhaust gas turbocharger is achieved in comparison with a system which has an oxidation catalytic converter in front of the high-pressure turbine, which in turn decisively determines the dynamics of the air system. Compared to a system without oxidation catalyst, there are no changes in the response. The supercharging pressure build-up between the system without and that with an oxidation catalyst between the high pressure turbine of the first exhaust gas turbocharger and the low pressure turbine of the second turbocharger is almost identical. The temperature loss is significantly lower compared to an arrangement of the oxidation catalyst, for example, in front of the high-pressure turbine of the first exhaust gas turbocharger. In addition, the temperature loss of minor importance, since the main work is done in a load jump anyway from the high pressure supercharger of the second exhaust gas turbocharger.

Das bessere Ansprechverhalten des Hochdruck-Laders bei Lastsprüngen führt zu einem Luftüberschuss in der Verbrennung. Dadurch kommt es insbesondere zu weniger Ruß- sowie HC-/ CO-Emissionen in den Dynamikphasen.The better response of the high-pressure loader with load jumps leads to an excess of air in the combustion. This results in particular in less soot and HC / CO emissions in the dynamic phases.

Durch die Anordnung des Oxidationskatalysators im Bypassstrang hinter der Hochdruckturbine des ersten Abgasturboladers werden die sehr hohen Abgastemperaturen (bis 800° Celsius) in vollastnahem Betriebspunkten der Brennkraftmaschine vermieden, weil in diesen Betriebspunkten die Bypassklappe geöffnet ist und das Abgas nicht durch den Oxidationskatalysator strömt. Der Abgasgegendruck wird verringert und somit der Wirkungsgrad der Brennkraftmaschine verbessert. Außerdem verringert sich die Wahrscheinlichkeit einer frühzeitigen Alterung des Oxidationskatalysators.The arrangement of the oxidation catalyst in the bypass line behind the high-pressure turbine of the first exhaust gas turbocharger, the very high exhaust gas temperatures (up to 800 ° C) are avoided in full-load operating points of the internal combustion engine, because in these operating points, the bypass valve is open and the exhaust gas does not flow through the oxidation catalyst. The exhaust backpressure is reduced, thus improving the efficiency of the internal combustion engine. In addition, the likelihood of premature aging of the oxidation catalyst is reduced.

Weitere vorteilhafte Ausgestaltungen der Erfindung sind der Zeichnungsbeschreibung zu entnehmen, in der ein in den Figuren dargestelltes Ausführungsbeispiel der Erfindung näher beschrieben ist:Further advantageous embodiments of the invention can be found in the drawing description, in which an illustrated in the figures embodiment of the invention is described in more detail:

Kurze Beschreibung der Zeichnungen Brief description of the drawings

Es zeigen:Show it:

1 ein Blockschaltbild einer Brennkraftmaschine mit zweistufiger Turboaufladung und erfindungsgemäß verbautem Oxidationskatalysator und 1 a block diagram of an internal combustion engine with two-stage turbocharging and inventively built oxidation catalyst and

2 eine stirnseitige Ansicht eines Bypassgehäuses des ersten Abgasturboladers mit integriertem Oxidationskatalysator. 2 an end view of a bypass housing of the first exhaust gas turbocharger with integrated oxidation catalyst.

Ausführungsform der ErfindungEmbodiment of the invention

Das Blockschaltbild gemäß 1 zeigt eine dreizylindrige Brennkraftmaschine 9 mit einem Frischluftstrang 20 und einem Abgasstrang 21. Dem Frischluftstrang 20 wird Frischluft 1 über einen Luftfilter 2 und einem Heißfilmluftmassenmesser 3, weiter über einen Niederdruck-Verdichter 4 eines zweiten Abgasturboladers und einen Hochdruck-Verdichter 6 eines ersten Abgasturboladers, weiter über einen Ladeluftkühler 7 und eine Drosselklappe 8 zugeführt. Der Hochdruck-Verdichter 6 ist über einen Verdichter-Bypass 5 umgehbar.The block diagram according to 1 shows a three-cylinder internal combustion engine nine with a fresh air line 20 and an exhaust system 21 , The fresh air line 20 gets fresh air 1 via an air filter 2 and a hot film air mass meter 3 , continue via a low-pressure compressor 4 a second exhaust gas turbocharger and a high pressure compressor 6 a first exhaust gas turbocharger, further via a charge air cooler 7 and a throttle 8th fed. The high pressure compressor 6 is via a compressor bypass 5 bypassed.

Die zusammen mit einem Kraftstoff, insbesondere Dieselkraftstoff, in den Brennräumen der Brennkraftmaschine zugeführte Frischluft 1 verlässt nach der Verbrennung die Brennkraftmaschine 9 und den Abgasstrang 21 als Abgas 19. Ein Teil des verbrannten Abgases wird über eine Abgasrückführleitung, in die ein Abgasrückführkühler 10 und ein Abgasrückführventil 11 zur Steuerung der zurückgeführten Abgasmenge eingebaut sind, in den Frischluftstrang 20 direkt vor dem Einlass in die Brennkraftmaschine 9 zurückgeführt. Der restliche Abgasstrom wird einer Hochdruck-Turbine 14 des ersten Abgasturboladers zugeführt und gelangt hinter der Hochdruck-Turbine 14 zu einem Abgaskatalysator in Form eines Oxidationskatalysators 15. Der Oxidationskatalysator 15 ist in ein Bypassgehäuse 13 der Hochdruck-Turbine 14 des ersten Abgasturboladers eingebaut, wobei der genaue Einbau der 2 zu entnehmen ist. Das Bypassgehäuse 13 weist eine Bypassleitung 22 mit einer Bypassklappe 12 auf, über die die Hochdruck-Turbine 14 umgehbar ist. Hinter dem Oxidationskatalysator 15 ist in den Abgasstrang 21 eine Niederdruck-Turbine 16 mit variabler Geometrie eingebaut, die Bestandteil des zweiten Abgasturboladers ist. Dieser Niederdruck-Turbine 16 schließen sich ein Diesel-Oxidationskatalysator 17 und ein Partikelfilter 18 an, bevor das gereinigte Abgas 19 in die Umgebung gelangt.The fresh air supplied together with a fuel, in particular diesel fuel, in the combustion chambers of the internal combustion engine 1 leaves after combustion the internal combustion engine nine and the exhaust system 21 as exhaust 19 , A portion of the burned exhaust gas is passed through an exhaust gas recirculation line into which an exhaust gas recirculation cooler 10 and an exhaust gas recirculation valve 11 are installed to control the amount of recirculated exhaust gas, in the fresh air line 20 directly in front of the inlet to the internal combustion engine nine recycled. The remaining exhaust gas flow becomes a high-pressure turbine 14 supplied to the first exhaust gas turbocharger and passes behind the high-pressure turbine 14 to an exhaust gas catalyst in the form of an oxidation catalyst 15 , The oxidation catalyst 15 is in a bypass housing 13 the high pressure turbine 14 installed the first exhaust gas turbocharger, the exact installation of the 2 can be seen. The bypass housing 13 has a bypass line 22 with a bypass flap 12 on top of that the high pressure turbine 14 is bypassable. Behind the oxidation catalyst 15 is in the exhaust system 21 a low pressure turbine 16 installed with variable geometry, which is part of the second exhaust gas turbocharger. This low pressure turbine 16 close a diesel oxidation catalyst 17 and a particle filter 18 before, the purified exhaust gas 19 gets into the environment.

2 zeigt eine Ansicht des Bypassgehäuses 13, wobei im oberen Bereich des Bypassgehäuses 13 die Bypassleitung 22 mit der Bypassklappe 12 angeordnet ist, während im unteren Bereich der Strömungsauslass die Hochdruck-Turbine 14 angeordnet ist. In diesen Strömungsauslass ist der Oxidationskatalysator 15 integriert. Ist die Bypassklappe 12 geschlossen, was insbesondere bei geringen Drehzahlen und Lasten der Brennkraftmaschine erfolgt, bei denen der HC-/ CO-Ausstoß der Brennkraftmaschine für die Emissionierung relevant ist, fließt der gesamte Abgasmassenstrom (ausgenommen des in den Frischluftstrang 20 zurückgeführten Abgases) über die Hochdruck-Turbine 14 und anschließend durch den in das Bypassgehäuse 13 integrierten Oxidationskatalysator 15. Bei geöffneter Bypassklappe 12 strömt das Abgas 19 durch den dann freigegebenen oberen Querschnitt der Bypassleitung 22 direkt auf die Niederdruck-Turbine 16. 2 shows a view of the bypass housing 13 , being in the upper part of the bypass housing 13 the bypass line 22 with the bypass flap 12 is arranged, while in the lower part of the flow outlet, the high-pressure turbine 14 is arranged. In this flow outlet is the oxidation catalyst 15 integrated. Is the bypass flap 12 closed, which takes place especially at low speeds and loads of the internal combustion engine, in which the HC / CO emissions of the engine is relevant for the emission, the entire exhaust gas mass flow flows (except that in the fresh air line 20 recirculated exhaust gas) via the high-pressure turbine 14 and then through the into the bypass housing 13 integrated oxidation catalyst 15 , With open bypass flap 12 the exhaust gas flows 19 through the then released upper cross section of the bypass line 22 directly on the low-pressure turbine 16 ,

ZITATE ENTHALTEN IN DER BESCHREIBUNG QUOTES INCLUDE IN THE DESCRIPTION

Diese Liste der vom Anmelder aufgeführten Dokumente wurde automatisiert erzeugt und ist ausschließlich zur besseren Information des Lesers aufgenommen. Die Liste ist nicht Bestandteil der deutschen Patent- bzw. Gebrauchsmusteranmeldung. Das DPMA übernimmt keinerlei Haftung für etwaige Fehler oder Auslassungen.This list of the documents listed by the applicant has been generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.

Zitierte PatentliteraturCited patent literature

  • WO 2004/097195 A1 [0002] WO 2004/097195 A1 [0002]

Claims (4)

Brennkraftmaschine mit einem Abgasstrang (21) und mit zweistufiger Turboaufladung, wobei der Abgasstrang (21) zwei Turbinen eines ersten und eines zweiten Abgasturboladers und mindestens einem Abgaskatalysator, insbesondere einem Oxidationskatalysator (15) in Reihenschaltung und eine Bypassleitung (22) in Parallelschaltung zur der Hochdruck-Turbine (14) des ersten Abgasturboladers umfasst, dadurch gekennzeichnet, dass der Abgaskatalysator (15) hinter der Hochdruck-Turbine (14) des ersten Abgasturboladers in einem Bypassstrang zu einer Bypassklappe (12) integriert ist, und dass der Bypassstrang und die Bypassklappe (12) in einem gemeinsamen Bypassgehäuse (13) integriert sind.Internal combustion engine with an exhaust gas line ( 21 ) and with two-stage turbocharging, wherein the exhaust gas line ( 21 ) two turbines of a first and a second exhaust gas turbocharger and at least one exhaust gas catalyst, in particular an oxidation catalyst ( 15 ) in series connection and a bypass line ( 22 ) in parallel with the high-pressure turbine ( 14 ) of the first exhaust gas turbocharger, characterized in that the exhaust gas catalytic converter ( 15 ) behind the high-pressure turbine ( 14 ) of the first exhaust gas turbocharger in a bypass line to a bypass flap ( 12 ) and that the bypass line and the bypass flap ( 12 ) in a common bypass housing ( 13 ) are integrated. Brennkraftmaschine (9) nach Anspruch 1, dadurch gekennzeichnet, dass der Bypassstrang und die Bypassklappe (12) nebeneinanderliegend in dem Bypassgehäuse (13) angeordnet sind.Internal combustion engine ( nine ) according to claim 1, characterized in that the bypass strand and the bypass flap ( 12 ) juxtaposed in the bypass housing ( 13 ) are arranged. Brennkraftmaschine (9) nach einem der vorherigen Ansprüche, dadurch gekennzeichnet, dass das Bypassgehäuse (13) mit dem Turbinengehäuse des ersten Abgasturboladers verbunden, insbesondere vereinigt ist.Internal combustion engine ( nine ) according to one of the preceding claims, characterized in that the bypass housing ( 13 ) is connected to the turbine housing of the first exhaust gas turbocharger, in particular united. Brennkraftmaschine (9) nach einem der vorherigen Ansprüche, dadurch gekennzeichnet, dass der Abgaskatalysator (15) gehäuselos in das Bypassgehäuse (13) eingesetzt ist.Internal combustion engine ( nine ) according to one of the preceding claims, characterized in that the catalytic converter ( 15 ) caseless in the bypass housing ( 13 ) is used.
DE102011086778A 2011-11-22 2011-11-22 Exhaust gas-turbo-loaded combustion engine i.e. diesel engine, has exhaust gas catalyst integrated in bypass strand behind high pressure turbine of supercharger, and bypass pipe in parallel connection to high pressure turbine Withdrawn DE102011086778A1 (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9771892B2 (en) 2014-05-20 2017-09-26 Ge Jenbacher Gmbh & Co Og Method of starting up a thermoreactor
US10801381B2 (en) 2015-09-04 2020-10-13 Innio Jenbacher Gmbh & Co Og Exhaust gas after treatment device

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004097195A1 (en) 2003-05-02 2004-11-11 Daimlerchrysler Ag Turbocharger device and method for operation of a turbocharger device

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004097195A1 (en) 2003-05-02 2004-11-11 Daimlerchrysler Ag Turbocharger device and method for operation of a turbocharger device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9771892B2 (en) 2014-05-20 2017-09-26 Ge Jenbacher Gmbh & Co Og Method of starting up a thermoreactor
US10801381B2 (en) 2015-09-04 2020-10-13 Innio Jenbacher Gmbh & Co Og Exhaust gas after treatment device

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