The invention relates to a multi-stage turbocharger arrangement.
Known multi-stage turbocharger arrangements have the disadvantage of a complex design, with flaps, sleeves and control capsules which are highly susceptible to wear, in particular as a result of a fragile crank drive. Furthermore, uniform and continuous cross-sectional openings, which contribute to the regulating accuracy or quality of the regulating characteristic, can only be realized to a limited extent.
It is therefore an object of the present invention to create a multi-stage turbocharger arrangement, the regulating system of which has improved regulating accuracy and a simplified and compact design.
This object is achieved by means of a multi-stage turbocharger arrangement for an internal combustion engine. The multi-stage turbocharger arrangement includes a high-pressure stage and a low-pressure stage. The low-pressure stage is operatively connected to the high-pressure stage by means of an openable and closable flow duct system. The multi-stage turbocharger arrangement includes a regulating unit for regulating the operative connection between the high-pressure stage and the low-pressure stage. The regulating unit and the flow duct system are integrated in an engine exhaust-gas manifold, which is arranged between the high-pressure stage and the low-pressure stage.
According to the invention, a simplified regulating unit for regulating the operative connection between the high-pressure turbocharger or the high-pressure stage and the low-pressure turbocharger or the low-pressure stage of the turbocharger, which regulating unit is arranged in the manifold between the high-pressure stage and the low-pressure stage and in which regulating unit are integrated all of the required flow ducts.
The subclaims relate to advantageous refinements of the invention.
Further details, advantages and features of the present invention can be gathered from the following description of exemplary embodiments on the basis of the drawing, in which:
The turbocharger arrangement 1 has a high-pressure stage 2 and a low-pressure stage 3, which are formed in each case by a correspondingly designed turbocharger, of which in each case the turbine housing of the turbine is illustrated in the figures.
The high-pressure stage 2 and the low-pressure stage 3 can be operatively connected to one another by means of an openable and closable flow duct system 4, for which purpose a regulating unit 5 is provided.
As can be seen in particular from
In the embodiment according to
In the abovementioned embodiment, the regulating unit 5 also has a bypass slide 9 which, in order to open and close a bypass duct 10, is arranged, like the regulating slide 7, in an axially slidable fashion in a housing 17 of the regulating unit 5. In the switching position which is illustrated by way of example in
In the first switching position, which can be seen in particular from
In the second switching position, as illustrated in
A corresponding switching position is illustrated in
A corresponding switching position of the variant according to
To complement the above written disclosure of the invention, reference is hereby explicitly made to the diagrammatic illustration of the invention in
Number | Date | Country | Kind |
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10 2006 060 743 | Dec 2006 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2007/009233 | 10/24/2007 | WO | 00 | 6/17/2009 |
Publishing Document | Publishing Date | Country | Kind |
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WO2008/083769 | 7/17/2008 | WO | A |
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