The invention relates to an exhaust-gas turbocharger.
Exhaust-gas-turbocharged internal combustion engines are nowadays often fitted with air-gap-insulated exhaust manifolds which are expediently produced in a two-shell design from thin-walled sheet-metal parts. The turbine housing is generally composed of cast materials with correspondingly greater wall thicknesses.
With air-gap-insulated manifold technology, the heat loss from the hot exhaust gas and likewise the surface temperature are reduced in relation to conventional cast manifolds on account of the lower masses. A greater amount of thermal energy is therefore made available to the downstream turbine of the exhaust-gas turbocharger for power conversion.
Air-gap-insulated manifolds are used in combination with both single-channel and also twin-channel turbine housings. Twin-channel turbine housings are used with so-called pulse supercharging, in which, for example in the case of a 4-cylinder or 6-cylinder engine, the exhaust-gas flows of in each case 2 or 3 cylinders are combined in groups and supplied in separate pipe lines to in each case one channel in the turbine housing. The individual channels in the turbine housing are separated from one another from the turbine housing inlet to the outlet from the spiral by a partition. In twin-channel turbine housings, the dynamic energy (pulsation) of the exhaust gases is additionally utilized for power conversion by means of the separation of individual exhaust gas flows.
With such complex components, however, the connecting technology between the thin-walled air-gap-insulated manifold and the comparatively thick-walled cast turbine housing has often proven to be relatively critical. On account of the available installation space, of the heat losses and leakage losses and on account of assembly requirements, the connection between the air-gap-insulated manifold and the cast turbine housing is often formed as a welded connection. With this type of connection in particular, problems arise on account of the materials, which are different for production reasons, of the air-gap-insulated manifold and of the cast turbine housing.
A further disadvantage, at least in the case of the twin-channel design of the turbine housing, is that the gas flows of the separate channels influence one another on account of leaks at the sliding connections within the air-gap-insulated manifold and in the region of the partition at the inlet into the turbine housing. The pulsation effect is therefore reduced as a result of the so-called “crosstalk” of the gas flows.
It is therefore an object of the present invention to create an exhaust-gas turbocharger which utilizes the advantages of an air-gap-insulated manifold and at the same time makes it possible to avoid the critical connecting technology between the air-gap-insulated manifold and the cast turbine housing.
This object is achieved by means of an exhaust-gas turbocharger in which the turbine housing and the manifold section, which is composed of the exhaust ducts of at least two cylinders, are formed as a single-piece cast part which can be referred to as a turbine-housing/manifold module.
The object is likewise achieved by means of an exhaust-gas turbocharger in which the turbine housing is formed as a cast part and the manifold section is formed as a separate cast part, which cast parts can be connected to one another after being produced by casting.
This embodiment is aimed at applications in which particular mounting conditions of the exhaust-gas turbocharger on the engine and the spatial conditions in the engine bay of the vehicle may result in such a complicated geometry of the manifold section that casting the manifold section together with the turbine housing would be made impossible. In this case, the manifold section and the turbine housing may be cast as separate individual parts that are subsequently connected to one another. The connection of the two individual parts to one another may take place by means of welding, a flange connection, a V-strap connection or similar suitable connecting methods.
The turbine housing may be of either single-channel or twin-channel design.
For a twin-channel turbine housing, the manifold section is designed such that, for the separation of the channels, each turbine housing duct extends separately up to the cylinder head and is acted on with exhaust gas from in each case one cylinder or from a plurality of cylinders combined in groups, and the dynamic energy (pulsation) of the exhaust gas is therefore additionally used for power conversion. To receive the exhaust-gas flows from the other cylinders, for example cylinders 1 and 4 in a 4-cylinder engine or cylinders 1, 2 and 5, 6 in a 6-cylinder engine, the manifold section is provided with openings at the sides, to which openings the exhaust lines of the cylinders are then connected by means of a plug-type connection or the like. The plug-type connections of the exhaust lines of further cylinders to one another and to the manifold section should be designed such that length variations as a result of thermal expansions can be compensated.
The turbine housing with the integrally cast manifold section is fastened to flanges, provided specifically for the purpose, on the cylinder head, for example at cylinders 2 and 3, and therefore serves as the main supporting element for the entire exhaust-gas turbocharger (turbine-housing/manifold module). The additional exhaust lines of the other cylinders are themselves fastened to corresponding flanges on the cylinder head.
Correspondingly shaped sheet-metal shells are arranged around the individual exhaust lines including the integrally cast manifold section, which sheet-metal shells form the so-called outer shell. The insulating air intermediate space is thereby formed between the hot lines which conduct exhaust gas and the outer shell. The outer shell is composed of at least two sheet-metal molded parts which are welded in a gas-tight fashion to one another and to the manifold section in the region of the transition to the turbine housing. It is also conceivable to use other connecting techniques, such as folding, brazing, riveting, screw connections etc. or combinations of the different types of connection, for the outer shell instead of welding. The at least two sheet-metal shells are not arranged around the turbine housing.
As a result of this design, specifically providing the channel separation directly at the cylinder head outlet in the case of a twin-channel turbine housing, it is ensured that the so-called “crosstalk” of the individual channels cannot take place and the pulsation effect of the exhaust gas is therefore utilized more effectively for power conversion. A further advantage is that the design-induced and functionally induced leakage flows at the plug-type connections of the exhaust pipe of the individual groups of cylinders likewise cannot influence one another.
In contrast to pulse supercharging in which a 2-channel turbine housing is imperatively necessary, no separation of the exhaust-gas flows takes place with so-called ram supercharging. Here, the exhaust-gas flows of all the cylinders are merged in a so-called collector and are supplied to the turbine wheel through the single-channel turbine housing. The teaching of the invention is expedient here too, specifically a turbine housing having an integrally cast manifold section which is designed in this case as a collector. The supply of the individual exhaust-gas flows to the collector and the fastenings of the turbine housing with “collector manifold” and of the individual exhaust lines take place in the same way as for a 2-channel design.
Further details, features and advantages of the invention can be gathered from the following description of an exemplary embodiment on the basis of the drawings, in which:
In the embodiment illustrated in
The design can also be seen from the enlarged illustration of
In the embodiment illustrated in
In addition to the above written disclosure of the invention, reference is hereby made to the graphic illustration of the invention in
Number | Date | Country | Kind |
---|---|---|---|
10 2008 047 448 | Sep 2008 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/US2009/056428 | 9/10/2009 | WO | 00 | 2/28/2011 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2010/033414 | 3/25/2010 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3930747 | Woollenweber | Jan 1976 | A |
3948052 | Merkle et al. | Apr 1976 | A |
4187678 | Herenius | Feb 1980 | A |
4294073 | Neff | Oct 1981 | A |
5463867 | Ruetz | Nov 1995 | A |
5761905 | Yamada et al. | Jun 1998 | A |
6062024 | Zander et al. | May 2000 | A |
6122911 | Maeda et al. | Sep 2000 | A |
6247552 | Kovar et al. | Jun 2001 | B1 |
6256990 | Itoh | Jul 2001 | B1 |
6343417 | Bonny et al. | Feb 2002 | B1 |
6892532 | Bruce et al. | May 2005 | B2 |
7089737 | Claus | Aug 2006 | B2 |
7234302 | Koerner | Jun 2007 | B2 |
7434390 | Nording et al. | Oct 2008 | B2 |
7610758 | Augstein et al. | Nov 2009 | B2 |
7731241 | Aoki et al. | Jun 2010 | B2 |
7836692 | Leroy | Nov 2010 | B2 |
8375707 | Muller | Feb 2013 | B2 |
8549851 | Grussmann et al. | Oct 2013 | B2 |
20020174650 | Durr et al. | Nov 2002 | A1 |
20040083730 | Wizgall et al. | May 2004 | A1 |
20050072143 | Diez | Apr 2005 | A1 |
20050126163 | Bjornsson, Sr. | Jun 2005 | A1 |
20050144946 | Claus | Jul 2005 | A1 |
20050183414 | Bien et al. | Aug 2005 | A1 |
20060131817 | Kerelchuk | Jun 2006 | A1 |
20070289954 | Bien et al. | Dec 2007 | A1 |
20080289323 | Diez et al. | Nov 2008 | A1 |
20090031722 | An et al. | Feb 2009 | A1 |
20090188247 | Phillips et al. | Jul 2009 | A1 |
20100038901 | Schmidt et al. | Feb 2010 | A1 |
20100047054 | Doerle et al. | Feb 2010 | A1 |
20100126156 | Diez et al. | May 2010 | A1 |
20100223911 | Gockel et al. | Sep 2010 | A1 |
20130014497 | Wu et al. | Jan 2013 | A1 |
Number | Date | Country |
---|---|---|
7372 | Feb 2005 | AT |
2252705 | May 1974 | DE |
3925802 | Feb 1991 | DE |
4342572 | Nov 1994 | DE |
102004054726 | Jun 2006 | DE |
69927233 | Jul 2006 | DE |
60312535 | Nov 2007 | DE |
102009030014 | Dec 2010 | DE |
1536141 | Jun 2005 | EP |
2060066 | Apr 1981 | GB |
63215809 | Sep 1988 | JP |
2000161056 | Jun 2000 | JP |
2003221639 | Aug 2003 | JP |
2008055588 | May 2008 | WO |
Number | Date | Country | |
---|---|---|---|
20110171017 A1 | Jul 2011 | US |