The invention relates to an exhaust-gas turbocharger.
In a generic exhaust-gas turbocharger, charge-pressure regulation is realized by means of a charge-pressure regulating device which has a compressor-side and/or turbine-side bypass that can be opened or closed by means of an actuator-operated flap plate. Said type of charge-pressure regulation can be used for single-stage, two-stage or twin-scroll turbocharger arrangements, or also in the case of turbochargers with a variable turbine geometry and wastegate.
Here, the charge-pressure regulation is realized in that a fraction of the exhaust gas is conducted so as to bypass the turbine by virtue of the flap plate being opened. In the case of two-stage regulation, one of the two turbochargers connected in parallel is regulated by means of a regulating flap.
A technical problem in the case of a single flap is however the leakage and the poor regulability, that is to say at a small stroke, a relatively large mass flow bypasses the turbine. At small strokes, however, small changes in the flap plate position result in relatively large changes in the bypass mass flow. If relatively small bore diameters were used for the bypass or the bypass opening, said problem would duly be alleviated, but this would result in the maximum possible bypass mass flow being reduced, such that, both at engine full load and also at engine part load, it would not be possible for the charge pressure to be regulated down, that is to say reduced, to an adequate extent.
It is therefore an object of the present invention to specify an exhaust-gas turbocharger capable of solving the above-mentioned technical problems of the prior art.
The solution according to the invention is based on the concept of providing not a single bypass opening or bore but two or multiple bores of said type, wherein each of said bores has a separate regulable flap plate assigned thereto.
Said concept may be used both on the turbine side and also on the compressor side.
It is thus made possible, with for example a given change in the stroke, to realize finer regulation of the exhaust-gas mass flow to be diverted. Furthermore, it is possible, when the two flap plates are open, to realize large opening cross sections which make it possible to realize high bypass rates.
The dependent claims contain advantageous developments of the invention.
It is thus possible for the bypass bores to be of equal diameter, or for bores of different diameter to be provided.
The actuation of the flap plates may be realized by means of suitable actuation elements (actuators), such as for example electric actuators or pneumatic control capsules.
It is also possible for the flap plates to be actuated simultaneously or with a time offset.
It is finally possible for the flap to be provided with a crank drive or to be formed as a charge-pressure valve.
Further details, advantages and features of the present invention will emerge from the following description of exemplary embodiments with reference to the drawing, in which:
In the illustrated embodiment of the exhaust-gas turbocharger 1, the turbine housing 5 is provided with a charge-pressure regulating device 6 according to the invention, which charge-pressure regulating device is merely symbolically indicated in
In the embodiment illustrated in
This illustration with two flap arrangements 7 and 8 is however to be understood merely as an example. It would theoretically likewise be possible for more than two such flap arrangements to be provided in order to attain the advantages explained in the introduction.
In the embodiment illustrated here, the flap arrangements 7 and 8 are provided in each case with a crank drive which comprises a respective inner flap lever 7B and 8B connected to the flap plate 7A, 8A. The flap lever 7B, 8B is connected to a respective spindle 7C and 8C which is mounted in the housing 5 by means of a respective bushing 7D and 8D. The spindle 7C and 8C is connected to a respective outer lever 7E and 8E which is connected via a respective connecting piece 7F and 8F to a respective regulating rod 7G and 8G of a respective associated actuator 11 and 12, wherein the actuators 11 and 12 are in each case indicated symbolically by the two hexagons.
In addition to the above written description of the invention, reference is hereby explicitly made, for additional disclosure thereof, to the diagrammatic illustration in
1 Exhaust-gas turbocharger
2 Compressor
3 Compressor housing
4 Turbine
5 Turbine housing
6 Charge-pressure regulating device
7, 8 Flap arrangement
7A, 8A Flap plate
7B, 8B Inner flap lever
7C, 8C Spindle
7D, 8D Bushing
7E, 8E Outer lever
7F, 8F Connecting piece
7G, 8G Regulating rod
9, 10 Bypass openings
11, 12 Actuators
13 Shaft
14 Bearing housing
L Longitudinal axis of the exhaust-gas turbocharger 1
Number | Date | Country | Kind |
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10 2012 023 805 | Dec 2012 | DE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/US2013/071131 | 11/21/2013 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2014/088818 | 6/12/2014 | WO | A |
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Entry |
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International Search Report in International Application No. PCT/US2013/071131, dated Feb. 27, 2014. |
Number | Date | Country | |
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20150300244 A1 | Oct 2015 | US |