Exhaust system for combustion engine, has turbine housing of exhaust turbo charger and exhaust manifold, where turbine housing and exhaust manifold are connected with each other over connecting area

The exhaust system (10) has a turbine housing (14) of an exhaust turbo charger and an exhaust manifold (12), where the turbine housing and the exhaust manifold are connected with each other over a connecting area. The turbine housing and the exhaust manifold are connected with each other by a form-f...

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Bibliographische Detailangaben
Hauptverfasser:	RIEWERT, DIRK, ELFELDT, JAN-PETER
Format:	Patent
Sprache:	eng ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNALCOMBUSTION ENGINES GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES ORENGINES IN GENERAL GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	The exhaust system (10) has a turbine housing (14) of an exhaust turbo charger and an exhaust manifold (12), where the turbine housing and the exhaust manifold are connected with each other over a connecting area. The turbine housing and the exhaust manifold are connected with each other by a form-fit connection or by a bonded-adhesion connection in a simple manner. Die Erfindung betrifft eine Abgasanlage (10, 10') für eine Verbrennungskraftmaschine mit einem Turbinengehäuse (14, 14') eines Abgasturboladers und mit einem Abgaskrümmer (12), welche über zumindest einen Verbindungsbereich verbunden sind, wobei das Turbinengehäuse (14, 14') und der Abgaskrümmer (12) lediglich durch eine formschlüssige Verbindung und/oder durch eine stoffschlüssige Verbindung miteinander verbunden sind.