DE202014103795U1 - Charged internal combustion engine with turbocharger - Google Patents

Abstract

Supercharged internal combustion engine with - an intake system (1) for supplying charge air, - an exhaust gas removal system for removing exhaust gas, - at least one exhaust gas turbocharger (2) which comprises a turbine arranged in the exhaust gas removal system and a compressor (3) arranged in the intake system (1), wherein the compressor (3) is equipped with at least one impeller (3d) mounted in a compressor housing (3e) on a rotatable shaft (3c), and - an exhaust gas recirculation system comprising a recirculation line system, the downstream of the turbine of the at least one exhaust gas turbocharger (2) from Exhaust gas discharge system branches off and opens upstream of the at least one compressor impeller (3d) into the intake system (1), characterized in that - the return line system comprises at least two ring channels (4, 5) which the intake system (1) upstream of the at least one compressor impeller (3d) Surrounded at least in sections in a spiral shape, with several channels (4a, 5a) from each ring channel (4, 5) which are fluidically connected to the intake system (1) on the intake side via the inlet opening (4b, 5b), - a first annular channel (4) has channels (4a) which, at least on the intake side, are essentially radial to the shaft (3c) of the compressor (3 ) are aligned and thus intersect the shaft (3c) in a virtual extension, and - a second annular channel (5) has channels (5a) which are aligned at least on the suction side in the manner of a secant and are thus spaced apart from the shaft in a virtual extension ( 3c) of the compressor (3) run.

Description

• – einem Ansaugsystem zum Zuführen von Ladeluft,
• – einem Abgasabführsystem zum Abführen von Abgas,
• – mindestens einem Abgasturbolader, der eine im Abgasabführsystem angeordnete Turbine und einen im Ansaugsystem angeordneten Verdichter umfasst, wobei der Verdichter mit mindestens einem in einem Verdichtergehäuse auf einer drehbaren Welle gelagerten Laufrad ausgestattet ist, und
• – einer Abgasrückführung umfassend ein Rückführleitungssystem, das stromabwärts der Turbine des mindestens einen Abgasturboladers vom Abgasabführsystem abzweigt und stromaufwärts des mindestens einen Verdichterlaufrades in das Ansaugsystem mündet.

The invention relates to a supercharged internal combustion engine with

• An intake system for supplying charge air,
• An exhaust gas removal system for removing exhaust gas,
• - At least one exhaust gas turbocharger, which comprises a turbine arranged in the Abgasabführsystem and a compressor arranged in the intake system, wherein the compressor is equipped with at least one mounted in a compressor housing on a rotatable shaft impeller, and
• An exhaust gas recirculation comprising a return line system, which branches off from the exhaust gas removal system downstream of the turbine of the at least one exhaust gas turbocharger and opens into the intake system upstream of the at least one compressor impeller.

An internal combustion engine of the type mentioned is used as a motor vehicle drive. In the context of the present invention, the term internal combustion engine includes diesel engines and gasoline engines, but also hybrid internal combustion engines, which use a hybrid combustion process, and hybrid drives, which in addition to the internal combustion engine comprise an electric motor which can be electrically connected to the internal combustion engine, which receives power from the internal combustion engine or as switchable auxiliary drive additionally delivers power.

In recent years, there has been a trend toward small, supercharged engines, with supercharging primarily a method of increasing performance by compressing the air needed for the engine combustion process. The economic importance of these engines for the automotive industry continues to increase.

Frequently, an exhaust gas turbocharger is used for charging, in which a compressor and a turbine are arranged on the same shaft. The hot exhaust stream is supplied to the turbine and relaxes with energy release in the turbine, causing the shaft to rotate. The energy emitted by the exhaust gas flow to the turbine and finally to the shaft is used to drive the compressor, which is also arranged on the shaft. The compressor conveys and compresses the charge air supplied to it, whereby a charging of the cylinder is achieved. Frequently, a charge air cooler is provided downstream of the compressor in the intake system, with which the compressed charge air is cooled before entering the at least one cylinder. The radiator lowers the temperature and thus increases the density of the charge air, so that the intercooler for a better filling of the cylinder, d. H. contributes to a larger air mass. There is a compaction by cooling.

The advantage of an exhaust gas turbocharger compared to a mechanical supercharger is that there is no mechanical connection to the power transmission between the supercharger and the internal combustion engine or is required. While a mechanical supercharger obtains the energy required for its drive completely from the internal combustion engine and thus reduces the power provided and thus adversely affects the efficiency, the exhaust gas turbocharger uses the exhaust gas energy of the hot exhaust gases.

The charge is - as already mentioned - the increase in performance. The air required for the combustion process is compressed, which allows each cylinder per working cycle, a larger air mass can be supplied. As a result, the fuel mass and thus the medium pressure can be increased.

The charge is a suitable means to increase the capacity of an internal combustion engine with unchanged displacement or to reduce the displacement at the same power. In any case, the charging leads to an increase in space performance and a lower power mass. If the displacement is reduced, then the load spectrum can be shifted to higher loads, where the specific fuel consumption is lower.

Charging thus supports the constant effort in the development of internal combustion engines to minimize fuel consumption, d. H. to improve the efficiency of the internal combustion engine.

Another fundamental goal is to reduce pollutant emissions. In the solution of this task, the charging can also be effective. With targeted design of the charge namely benefits in efficiency and in the exhaust emissions can be achieved. In order to comply with future limits for pollutant emissions in addition to the charge but further internal engine measures required.

Exhaust gas recirculation, for example, reduces nitrogen oxide emissions. In this case, the exhaust gas recirculation rate x _{AGR is} determined as x _AGR = m _AGR / (m _AGR + m _{fresh air} ), where m _{AGR designates} the mass of recirculated exhaust gas and m _{fresh air} the fresh air supplied.

The interpretation of the turbocharger turbocharger is difficult, with basically a noticeable increase in performance in all engine speed ranges is sought. In the prior art, however, a strong torque drop is observed when falling below a certain speed.

This torque drop becomes understandable if it is taken into account that the boost pressure ratio depends on the turbine pressure ratio. If the engine speed is reduced, this leads to a smaller exhaust gas mass flow and thus to a smaller turbine pressure ratio. Consequently, the boost pressure ratio also decreases toward lower speeds. This is equivalent to a boost pressure drop or torque drop.

In practice, the relationships described above often result in a small exhaust gas turbocharger, i. H. an exhaust gas turbocharger with a small turbine cross section is used, whereby the turbine pressure ratio can be increased. However, this degrades the charge at high speeds and shifts the torque drop only towards low speeds. In addition, this approach, d. H. the reduction of the turbine cross-section limits, since the desired charging and performance increase should be possible without restriction and to the desired extent, even at high speeds.

The torque characteristic of a supercharged internal combustion engine is tried to improve in the prior art by various measures.

For example, by a small design of the turbine cross-section and simultaneous Abgasabblasung, the Abgasabblasung can be controlled by means of boost pressure or by means of exhaust pressure. Such a turbine is also referred to as a waste gate turbine. If the exhaust gas mass flow exceeds a critical size, part of the exhaust gas flow is conducted past the turbine by means of a bypass line as part of the so-called exhaust gas blow-off. However, this approach has - as already mentioned above - the disadvantage that the charging behavior at higher speeds is insufficient.

The torque characteristic of a supercharged internal combustion engine may be further characterized by a plurality of turbochargers arranged in parallel, i. H. be improved by a plurality of parallel turbines of smaller turbine cross-section, with turbines are switched successively with increasing exhaust gas quantity.

The torque characteristic can also be advantageously influenced by means of a plurality of exhaust-gas turbochargers connected in series. By switching in series of two exhaust gas turbochargers, one of which is an exhaust gas turbocharger as a high-pressure stage and an exhaust gas turbocharger as a low-pressure stage, the engine map can be widened in an advantageous manner, both towards smaller compressor streams and towards larger compressor streams.

In particular, in the case of the exhaust gas turbocharger serving as a high-pressure stage, the pumping limit can be shifted towards smaller compressor flows, which means that high boost pressure ratios can be achieved even with small compressor flows, which significantly improves the torque characteristic in the lower rpm range. This is achieved by designing the high-pressure turbine for small exhaust gas mass flows and providing a bypass line, with which increasing exhaust gas mass flow increasingly exhaust gas is passed to the high-pressure turbine. For this purpose, the bypass line branches off the exhaust-gas removal system upstream of the high-pressure turbine and returns to the exhaust-gas removal system upstream of the low-pressure turbine. In the bypass line, a shut-off element is arranged to control the exhaust gas flow passed past the high-pressure turbine.

The pumping limit of the compressor of an exhaust turbocharger further or as far as possible to shift towards small compressor flows, is advantageous for other reasons.

With small compressor flows, the velocity of the charge air flow relative to the intake system decreases to such an extent that the flow of the rotating impeller blades is too large and the charge air flow separates from the airfoil-like blades. The resulting pressure fluctuations on the blades lead to an increased noise emission and possibly damage to the blades. Other negative effects that can occur are mass flow fluctuations and a high loss of efficiency.

With a variable compressor geometry, this effect can be counteracted. By adjusting the blades of an upstream stator provided on the flow of the rotating impeller blades, d. H. On the angle of attack, be influenced to a limited extent, whereby the pumping limit of the compressor in the compressor map is shifted towards small compressor flows.

The equipment of a compressor with a variable compressor geometry is costly. In addition, the influence by means of variable compressor geometry also limits, as an adjustment of the stator is possible only to a certain extent. In addition, a guide turns out to be a drag for larger compressor flows and thus more of a hindrance.

Against this background, it is the object of the present invention to provide a supercharged internal combustion engine according to the preamble of claim 1, with which the disadvantages known from the prior art are overcome and their charging behavior is significantly improved, especially at low compressor currents.

• – einem Ansaugsystem zum Zuführen von Ladeluft,
• – einem Abgasabführsystem zum Abführen von Abgas,
• – mindestens einem Abgasturbolader, der eine im Abgasabführsystem angeordnete Turbine und einen im Ansaugsystem angeordneten Verdichter umfasst, wobei der Verdichter mit mindestens einem in einem Verdichtergehäuse auf einer drehbaren Welle gelagerten Laufrad ausgestattet ist, und
• – einer Abgasrückführung umfassend ein Rückführleitungssystem, das stromabwärts der Turbine des mindestens einen Abgasturboladers vom Abgasabführsystem abzweigt und stromaufwärts des mindestens einen Verdichterlaufrades in das Ansaugsystem mündet, die dadurch gekennzeichnet ist, dass
• – das Rückführleitungssystem mindestens zwei Ringkanäle umfasst, die das Ansaugsystem stromaufwärts des mindestens einen Verdichterlaufrades zumindest abschnittsweise spiralförmig umgeben, wobei von jedem Ringkanal mehrere Kanäle ausgehen, die jeweils via Eintrittsöffnung ansaugseitig mit dem Ansaugsystem strömungstechnisch verbunden sind,
• – ein erster Ringkanal Kanäle aufweist, die zumindest ansaugseitig im Wesentlichen radial zur Welle des Verdichters ausgerichtet sind und damit die Welle in einer virtuellen Verlängerung schneiden, und
• – ein zweiter Ringkanal Kanäle aufweist, die zumindest ansaugseitig in der Art einer Sekante ausgerichtet sind und damit in einer virtuellen Verlängerung beabstandet zur Welle des Verdichters verlaufen.

This problem is solved by a supercharged internal combustion engine

• An intake system for supplying charge air,
• An exhaust gas removal system for removing exhaust gas,
• - At least one exhaust gas turbocharger, which comprises a turbine arranged in the Abgasabführsystem and a compressor arranged in the intake system, wherein the compressor is equipped with at least one mounted in a compressor housing on a rotatable shaft impeller, and
• An exhaust gas recirculation system comprising a return line system which branches off from the exhaust gas removal system downstream of the turbine of the at least one exhaust gas turbocharger and opens into the intake system upstream of the at least one compressor impeller, which is characterized in that
• The return line system comprises at least two annular channels which surround the intake system at least partially spirally upstream of the at least one compressor impeller, whereby several channels emanate from each annular channel, which are fluidly connected respectively to the intake system via the inlet opening,
• - A first annular channel has channels which are aligned at least on the suction side substantially radially to the shaft of the compressor and thus intersect the shaft in a virtual extension, and
• - A second annular channel has channels which are aligned at least on the suction side in the manner of a secant and thus extend in a virtual extension spaced from the shaft of the compressor.

The inventive supercharged by exhaust gas turbocharger internal combustion engine is equipped with an exhaust gas recirculation, namely with a low-pressure EGR. In contrast to a high pressure EGR, which introduces exhaust gas taken from the exhaust gas removal system upstream of the turbine into the intake system downstream of the compressor, at a low pressure EGR, exhaust gas is returned to the inlet side which has already passed through the turbine. For this purpose, the low-pressure EGR comprises a return line system, which branches off from the exhaust gas removal system downstream of the turbine and opens into the intake system upstream of the compressor.

The main advantage of the low-pressure EGR compared with the high-pressure EGR is that the exhaust gas flow introduced into the turbine is not reduced by the amount of recirculated exhaust gas in the case of exhaust gas recirculation. It is always the entire exhaust gas flow to the turbine to generate a sufficiently high boost pressure available.

The exhaust gas, which is returned to the inlet side by means of low-pressure EGR and is preferably cooled, is mixed with fresh air upstream of the compressor. The mixture of fresh air and recirculated exhaust gas produced in this way forms the charge air, which is supplied to the compressor and compressed.

It is harmless that exhaust gas is passed through the compressor in the context of low-pressure EGR, since preferably exhaust gas is used, which downstream of the turbine of an exhaust aftertreatment, in particular in a particulate filter was subjected. Deposits in the compressor, which change the geometry of the compressor, in particular the flow cross-sections, and thus worsen the efficiency of the compressor, are therefore not to be feared.

According to the invention, the return line system of the low-pressure EGR comprises at least two annular channels, each of which emanates a plurality of channels which are in fluid communication with the intake system.

The ring channels are formed differently. While the channels of the first annular channel are aligned substantially radially to the virtual extension of the shaft of the compressor and serve primarily to introduce exhaust gas into the intake system, the channels of the second annular channel are aligned in the manner of a secant or a tangent, so that from Radiantly exiting exhaust gas forms a vortex around the shaft of the compressor.

With the channels of the second annular channel, in particular in the case of small compressor flows, it is possible to influence the velocity of the charge air flow relative to the compressor impeller, ie the velocity vector of the inflow, wherein the extent of the influence can be adjusted by means of the exhaust gas quantity exiting the channels. The velocity vector of the charge air flow is replaced by the exhaust vortex an additional component, so that the angle of the flow to the rotating impeller blades of the compressor can be changed. In the context of the description of the figures, the corresponding speed triangles explained in detail, the effect of the invention is clearly visible.

Separation of the charge air flow from the airfoil-like blades of the compressor impeller can be counteracted, whereby an increased noise emission and damage to the blades can be avoided or reduced.

The surge limit of the compressor in the compressor map can be further shifted towards smaller compressor flows. The inventive measure is inexpensive compared to the equipment of the compressor with a variable compressor geometry, especially when it is considered that modern internal combustion engines usually already have an exhaust gas recirculation, which is still to be provided with the features of the return piping system according to the invention. In addition, the ring channels do not represent a flow resistance in the case of larger compressor flows, in contrast to a guide device.

Thus, the object underlying the invention is achieved, namely provided a supercharged internal combustion engine, with which the known from the prior art disadvantages are overcome and their charging behavior is significantly improved, especially at low compressor currents.

The orientation of the channels of the second annular channel in the manner of a secant in the context of the present invention means that the virtual extension of each channel intersects the curve-like inner wall of the intake system and in particular includes the limiting case that the virtual extension of a channel tangent to the outer periphery of the compressor wheel , d. H. in the projection represents a tangent to the compressor wheel, d. H. forms.

Further advantageous embodiments of the internal combustion engine are discussed in connection with the subclaims.

Embodiments of the internal combustion engine in which the compressor of the at least one exhaust-gas turbocharger is a radial compressor are advantageous. This embodiment allows a tight packaging of the exhaust gas turbocharger and thus the overall charge. The compressor housing can be designed as a spiral or worm housing, wherein the deflection of the charge air flow in the compressor of the exhaust gas turbocharger can be used advantageously to the compressed charge air on the shortest route from the outlet side, on which the turbine of the exhaust gas turbocharger is arranged on the inlet side respectively.

In this context, embodiments of the internal combustion engine in which the turbine of the at least one exhaust-gas turbocharger is a radial turbine are advantageous. This embodiment also allows a tight packaging of the exhaust gas turbocharger and thus the overall charge.

Unlike the turbines, compressors are defined by their outflow. A radial compressor is thus a compressor whose outflow from the blades takes place substantially radially. In the context of the present invention, essentially radial means that the velocity component in the radial direction is greater than the axial velocity component.

Embodiments of the internal combustion engine in which the compressor of the at least one exhaust gas turbocharger is an axial compressor can also be advantageous. The outflow from the impeller blades of an axial compressor takes place substantially axially.

Embodiments of the internal combustion engine in which the compressor of the at least one exhaust-gas turbocharger has an inlet region which runs coaxially to the shaft of the compressor and is designed so that the flow of the charge air to the compressor takes place essentially axially are advantageous.

In an axial flow of the compressor often eliminates a deflection or change in direction of the charge air flow in the intake upstream of the compressor impeller, whereby unnecessary pressure losses in the charge air flow due to flow deflection can be avoided and the pressure of the charge air is increased at the inlet to the compressor of the exhaust gas turbocharger.

Embodiments of the internal combustion engine in which the at least two annular channels are arranged adjacent to one another and at least partially separated from one another by means of a wall are advantageous. A neighborhood of the at least two annular channels provides for compact packaging and provides the ability to adjust the amounts of exhaust gas introduced into the annular channels with only one control, i. H. to dose.

Embodiments of the internal combustion engine in which the return line system comprises a metering device with which exhaust gas removed downstream of the turbine of the at least one exhaust gas turbocharger can be divided into the at least two annular channels are advantageous.

In this connection, embodiments of the internal combustion engine in which the metering device has a control with which the first annular channel can be closed on the exhaust side in a first operating position are advantageous.

The channels of the first annular channel essentially serve to introduce exhaust gas for realizing a predetermined exhaust gas recirculation rate. In this respect, it may be useful to close these channels, especially at low return rates and bring the entire recirculated exhaust gas via the second annular channel in the intake system. Then, even with small recirculation rates or small amounts of exhaust gas to recirculate, it is possible to create a vortex around the shaft of the compressor upstream of the compressor impeller.

Nevertheless, the channels of the first annular channel also provide for a charge air movement in the intake system and thus for a thorough mixing of the recirculated exhaust gas with the fresh air, d. H. for a homogenization of the charge air with respect to composition and temperature. This is advantageous in view of the running in the cylinders combustion, especially in a multi-cylinder internal combustion engine.

Embodiments of the internal combustion engine in which the metering device has a control with which the second annular channel can be closed on the exhaust side in a second operating position are also advantageous in this connection.

With the channels of the second annular channel, it is possible to exert influence on the velocity vector of the flow, in particular in the case of small compressor flows. But as long as such influence is not required to optimize the flow, it may be useful to close these channels and bring the entire recirculated exhaust gas via the first annular channel in the intake system.

Embodiments of the internal combustion engine in which the metering device has a control with which the first annular channel and the second annular channel can be connected to the exhaust gas removal system in a third working position and / or can be separated from the exhaust gas removal system in a further working position are also advantageous. In the former case, the control of the metering device is used to divide the downstream of the turbine of the at least one exhaust gas turbocharger removed and recirculated exhaust gas to the ring channels. In the latter case, the exhaust gas recirculation is deactivated by means of control, d. H. off. In this respect, the control element can basically also function as an EGR valve.

Embodiments of the internal combustion engine in which the metering device has a flap serving as a control, which can be pivoted, are advantageous.

A flap has already proved to be advantageous as an EGR valve, is less prone to failure and cost.

Embodiments of the internal combustion engine in which the first annular channel is arranged upstream of the second annular channel are advantageous. This arrangement is advantageous because the second annular channel, which serves to generate the vortex upstream of the compressor impeller, the compressor near, d. H. the closest to the compressor ring channel. Therefore, the formed vortex can not be disturbed or redissolved by another downstream annular channel.

Advantageous embodiments of the internal combustion engine, in which the channels of the first annular channel and / or the second annular channel are arranged regularly spaced from each other.

Embodiments of the internal combustion engine in which the at least two annular channels completely surround the intake system are advantageous.

The two above embodiments support both the formation of a regular vortex and the mixing of the recirculated exhaust gas with the fresh air, d. H. the homogenization of the charge air in the intake system.

Advantageous embodiments of the internal combustion engine, in which the channels of the second annular channel at least on the suction side - in a projection in the direction of the shaft - tangential to the at least one compressor wheel. The virtual extensions of the channels affect the outer circumference of the compressor impeller in the projection.

Advantageous embodiments of the internal combustion engine, in which the channels of the second annular channel are aligned according to the direction of rotation of the at least one compressor impeller.

Embodiments of the internal combustion engine in which at least the inlet openings of the channels of the first annular channel are circular are advantageous.

In order to achieve a significant reduction in nitrogen oxide emissions, high exhaust gas recirculation rates are required. Therefore can also be advantageous Be embodiments in which an additional exhaust gas recirculation is provided, which includes a line which branches off from the Abgasabführsystem upstream of the turbine and opens again downstream of the compressor in the intake system.

In contrast to the low-pressure EGR already mentioned, exhaust gas is taken from the exhaust system at a high-pressure EGR upstream of the turbine and introduced into the intake system downstream of the compressor, i. H. Exhaust gas recirculated, which has not yet passed through the turbine. One advantage of the high-pressure EGR is that there is a sufficiently high pressure gradient for conveying the exhaust gas and the exhaust gas does not have to undergo any exhaust gas aftertreatment.

For operating an internal combustion engine of the type described above, in which the return line system comprises a metering device with which exhaust gas removed downstream of the turbine of the at least one exhaust gas turbocharger can be divided to the at least two annular channels, starting from an operating mode of the internal combustion engine, the exhaust gas is returned via the return line system is, preferably increased via a second annular channel in the intake system recirculated exhaust gas fraction when a charge air to be supplied to the compressor decreases.

The surge line of the compressor can be moved in this way further towards small compressor streams. In the case of small compressor flows, the second annular channel influences the flow of the compressor impeller, d. H. on the velocity vector of the charge air flow. A more or less strong exhaust vortex is generated by more or less recirculated exhaust gas. A separation of the charge air flow from the blades of the compressor impeller is avoided.

In the following the invention is based on an embodiment according to the 1a . 1b . 1c . 2a and 2 B described in more detail. Hereby shows:

1a schematically the compressor arranged in the intake system of a first embodiment of the internal combustion engine, partially cut,

1b the speed triangle without EGR,

1c the speed triangle with EGR via second ring channel,

2a schematically the in 1a illustrated embodiment, cut perpendicular to the shaft of the compressor along the first annular channel, and

2 B schematically the in 1a illustrated embodiment, cut perpendicular to the shaft of the compressor along the second annular channel.

1a schematically shows the intake system 1 arranged compressor 3 a first embodiment of the internal combustion engine, partially cut.

For supplying the charge air to the cylinders, the internal combustion engine has an intake system 1 and for the purpose of charging the cylinders, there is provided an exhaust gas turbocharger having a turbine (not shown) disposed in the exhaust gas discharge system and one in the intake system 1 arranged compressor 3 includes. The compressor 3 is a centrifugal compressor 3b in its case 3e an impeller 3d on a rotatable shaft 3c is stored.

The compressor 3 the exhaust gas turbocharger 2 has an entrance area 3a on, coaxial with the shaft 3c of the compressor 3 runs and is formed so that the flow of charge air to the compressor 3 the exhaust gas turbocharger 2 essentially axially and the section of the intake system 1 upstream of the compressor 3 has no direction changes.

The internal combustion engine is further provided with exhaust gas recirculation, which includes a return piping system that branches off the exhaust gas removal system downstream of the turbine and upstream of the compressor 3 or compressor impeller 3d into the intake system 1 empties.

The return line system has two ring channels 4 . 5 that the intake system 1 upstream of the compressor impeller 3d Surround spirally and fully enclose, with each annular channel 4 . 5 several channels go out, each via the entrance opening 4b . 5b suction side with the intake system 1 are fluidically connected.

The second ring channel 5 serves to create a vortex around the shaft 3c of the compressor 3 or the virtual extension of the wave 3c namely in the direction of rotation of the shaft 3c (see double arrow). 1b shows the speed triangle without EGR, ie without vortex, and 1c the speed triangle with EGR via second ring channel, ie with vortex.

Like from the 1b and 1c it can be seen that the velocity vector v _{wheel of} the flow to the compressor impeller is composed of the velocity vector v _{charge of} the charge air in the intake system and the vector v _{c of} the peripheral speed of the rotating compressor impeller.

While according to 1b an exactly axial charge air flow v _charge is present, the velocity vector v _charge receives the _charge air in the intake system according to 1c as a result of the return of exhaust gas via a second annular channel, a component in the circumferential direction of the compressor impeller. This increases the angle α of the flow to the compressor wheel. This is advantageous in terms of the flow of the blades of the compressor impeller.

2a shows a section perpendicular to the shaft 3c of the compressor impeller 3d and along the first ring channel 4 the in 1a illustrated embodiment. The first ring channel 4 has channels 4a that are essentially radial to the shaft 3c the compressor are aligned and thus the shaft 3c cut in a virtual extension.

2 B shows a section perpendicular to the shaft 3c of the compressor impeller 3d and along the second ring channel 5 the in 1a illustrated embodiment. The second ring channel 5 has channels 5a , which are aligned in the manner of a secant and thus in a virtual extension spaced from the shaft 3c of the compressor run. The virtual extension of each channel 5a cuts the curvy inner wall of the intake system and in the present case touches the outer circumference of the compressor impeller 3d in the projection.

LIST OF REFERENCE NUMBERS

1

 intake system

2

 turbocharger

3

 Compressor of the exhaust gas turbocharger

3a

 Entry area of the compressor of the exhaust gas turbocharger

3b

 centrifugal compressors

3c

 Shaft of the compressor of the exhaust gas turbocharger

3d

 Impeller of the compressor of the exhaust gas turbocharger

3e

 Compressor housing of the exhaust gas turbocharger

4

 first ring channel

4a

 Channel of the first ring channel

4b

 inlet opening

5

 second ring channel

5a

 Channel of the second ring channel

5b

 inlet opening

AGR

 Exhaust gas recirculation

α

 Angle of the flow to the compressor impeller

m _AGR

 Mass of recirculated exhaust gas

_{Fresh air}

 Mass of supplied fresh air or charge air

v _C

 Vector of the peripheral speed of the rotating compressor impeller

v _charge

 Speed vector of the charge air in the intake system

v _wheel

 Velocity vector of the flow to the compressor impeller

x _AGR

 Exhaust gas recirculation rate

Claims (16)

Charged internal combustion engine with - an intake system ( 1 ) for supplying charge air, - an exhaust gas removal system for discharging exhaust gas, - at least one exhaust gas turbocharger ( 2 ), which has a turbine arranged in the exhaust-gas removal system and one in the intake system ( 1 ) arranged compressors ( 3 ), wherein the compressor ( 3 ) with at least one in a compressor housing ( 3e ) on a rotatable shaft ( 3c ) mounted impeller ( 3d ), and an exhaust gas recirculation system comprising a return line system which is located downstream of the turbine of the at least one exhaust gas turbocharger (FIG. 2 ) branches off the Abgasabführsystem and upstream of the at least one compressor impeller ( 3d ) into the intake system ( 1 ), characterized in that - the return line system has at least two ring channels ( 4 . 5 ), which is the intake system ( 1 ) upstream of the at least one compressor impeller ( 3d ) at least partially surrounded in a spiral shape, wherein of each annular channel ( 4 . 5 ) several channels ( 4a . 5a ), each via the inlet opening ( 4b . 5b ) on the intake side with the intake system ( 1 ) are fluidically connected, - a first annular channel ( 4 ) Channels ( 4a ), which at least on the intake side substantially radially to the shaft ( 3c ) of the compressor ( 3 ) and thus the shaft ( 3c ) in a virtual extension, and - a second annular channel ( 5 ) Channels ( 5a ), which are aligned at least on the suction side in the manner of a secant and thus in a virtual extension spaced from the shaft ( 3c ) of the compressor ( 3 ). Supercharged internal combustion engine according to claim 1, characterized in that the compressor ( 3 ) of the at least one exhaust gas turbocharger ( 2 ) a radial compressor ( 3b ). Supercharged internal combustion engine according to claim 1, characterized in that the compressor ( 3 ) of the at least one exhaust gas turbocharger ( 2 ) is an axial compressor. Supercharged internal combustion engine according to one of the preceding claims, characterized in that the compressor ( 3 ) of the at least one exhaust gas turbocharger ( 2 ) an entrance area ( 3a ) coaxial with the shaft ( 3c ) of the compressor ( 3 ) and is formed so that the flow of charge air to the compressor ( 3 ) is effected substantially axially. Supercharged internal combustion engine according to one of the preceding claims, characterized in that the at least two annular channels ( 4 . 5 ) are arranged adjacent to each other and at least partially separated by a wall from each other. Supercharged internal combustion engine according to one of the preceding claims, characterized in that the return line system comprises a metering device, with the downstream of the turbine of the at least one exhaust gas turbocharger ( 2 ) removed exhaust gas to the at least two annular channels ( 4 . 5 ) is divisible. Supercharged internal combustion engine according to claim 6, characterized in that the metering device has a control with which the first annular channel ( 4 ) is closable in a first working position on the exhaust side. Supercharged internal combustion engine according to claim 6 or 7, characterized in that the metering device has a control, with which the second annular channel ( 5 ) can be closed off in a second working position on the exhaust side. Supercharged internal combustion engine according to one of claims 6 to 8, characterized in that the metering device has a control with which the first annular channel ( 4 ) and the second ring channel ( 5 ) are connectable in a third working position with the Abgasabführsystem. Supercharged internal combustion engine according to one of claims 6 to 9, characterized in that the metering device has a serving as a control flap, which is pivotable. Supercharged internal combustion engine according to one of the preceding claims, characterized in that the first annular channel ( 4 ) upstream of the second ring channel ( 5 ) is arranged. Supercharged internal combustion engine according to one of the preceding claims, characterized in that the channels ( 4a . 5a ) of the first ring channel ( 4 ) and / or the second ring channel ( 5 ) are arranged regularly spaced from each other. Supercharged internal combustion engine according to one of the preceding claims, characterized in that the at least two annular channels ( 4 . 5 ) the intake system ( 1 ) completely enclose. Supercharged internal combustion engine according to one of the preceding claims, characterized in that the channels ( 5a ) of the second ring channel ( 5 ) at least on the suction side in a projection in the direction of the shaft ( 3c ) tangentially to the at least one compressor impeller ( 3d ). Supercharged internal combustion engine according to one of the preceding claims, characterized in that the channels ( 5a ) of the second ring channel ( 5 ) according to the direction of rotation of the at least one compressor impeller ( 3d ) are aligned. Supercharged internal combustion engine according to one of the preceding claims, characterized in that at least the inlet openings ( 4b ) of the channels ( 4a ) of the first ring channel ( 4 ) are circular.

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