Turbocharger for an internal combustion engine of a motor vehicle
In a turbocharger for an internal combustion engine of a motor vehicle, comprising a turbine housing having first and second spiral passages, each of which is connected to at least one exhaust gas line of an exhaust train of the internal combustion engine and a turbine wheel disposed within a rotor chamber of the turbine housing and connected to a compressor impeller via a drive shaft for rotation with the impeller, the exhaust gas of the internal combustion engine can be routed through the spiral passages for admission to the turbine wheel via the first and second spiral passages which have different wrap angles around the turbine wheel.
1. A turbocharger for an internal combustion engine ( 10 ) of a motor vehicle, comprising a turbine housing ( 12 ) having at least one first and one second spiral inlet passage ( 14 a , 14 b ), each of which can be coupled to at least one of several exhaust gas lines ( 16 a , 16 b ) of an exhaust train ( 18 ) of the internal combustion engine ( 10 ), and through each of which exhaust gas can flow independently, and further comprising a turbine wheel ( 22 ) located within a rotor chamber ( 20 ) of the turbine housing ( 12 ), which is provided for driving a compressor impeller ( 25 ) coupled to the turbine wheel ( 22 ) for rotation therewith via a support shaft ( 24 ), wherein the exhaust gas of the internal combustion engine, which can be routed through the at least two spiral passages ( 14 a , 14 b ), can be admitted to the turbine wheel ( 22 ), the first and second spiral passages ( 14 a , 14 b ) having different wrap angles (φs) around the turbine wheel ( 22 ) at least one of the first and the second spiral passages ( 14 a , 14 b ) comprising in the region leading to the rotor chamber ( 20 ) a nozzle ( 28 a , 28 b ) with an effective cross-section (A D ) chosen according to the formula
A D =r D *2 *π*b D *sin(α D )*(φ S /360),
wherein:
A D denotes the effective cross-section of the nozzle ( 28 a );
r D a radius of the nozzle ( 28 a ) with respect to an axis of rotation (I) of the turbine wheel ( 22 );
b D the cross-sectional width of the nozzle ( 28 a );
α D an angle between a circumferential speed vector and a radial speed vector of the exhaust gas flow in the cross-section of the nozzle ( 28 a ); and
φ s the wrap angle of the respective spiral passage ( 14 a ).
2. The turbocharger according to claim 1 , wherein the first spiral passage ( 14 a ) has a wrap angle (φ s ) of less than 300°.
3. The turbocharger according to claim 2 , wherein the second spiral passage ( 14 b ) has a wrap angle (φ s ) of at least 280°.
4. The turbocharger according to claim 3 , wherein the first spiral passage ( 14 a ) is located in the region of a shaft bearing ( 24 ) of the turbocharger and the second spiral passage ( 14 b ) is located in the region of an exhaust gas outlet ( 26 ) of the turbine housing ( 12 ).
5. The turbocharger according to claim 1 , wherein the cross-sectional width (b D ) of the nozzle ( 28 a ) is chosen in dependence on a limit width defined by production engineering considerations.
6. The turbocharger according to claim 1 , wherein an inlet region (E 14 a ) of the first spiral passage ( 14 a ) corresponds to an inlet region (E 14 b ) of the second spiral passage ( 14 b ).
7. The turbocharger according to claim 6 , wherein the turbine housing ( 12 ) comprises a third spiral passage ( 14 c ) located adjacent to the first spiral passage ( 14 a ) and the second spiral passage ( 14 b ), the wrap angle (φ s ) of the third spiral passage ( 14 c ) corresponding to the wrap angle (φ s ) of a full volute.
8. The turbocharger according to claim 1 , wherein a guide grid element (30, 30′) with guide vanes is provided in the region of at least one of the first and the second spiral passage ( 14 a , 14 b ) which leads into the rotor chamber ( 20 ).
9. The turbocharger according to claim 8 , wherein the guide grid element ( 30 ) is mounted movably in the turbine housing ( 12 ).
10. The turbocharger according to claim 8 , wherein a matrix ( 32 ) for the adjustment of a blade height of the guide grid element ( 30 ) is mounted movably in the turbine housing ( 12 ).
11. The turbocharger according to claim 1 , wherein a blow-off valve ( 42 ) is provided upstream of the turbine wheel ( 22 ) for guiding the exhaust gas past the turbine wheel ( 22 ).
12. An internal combustion engine ( 10 ) for a motor vehicle, comprising at least two cylinders ( 11 a - f ) or two cylinder groups ( 34 a , 34 b ) to which are assigned at least two exhaust gas lines ( 16 a , 16 b ), and further comprising a turbocharger with a compressor ( 27 ) located in an intake train ( 40 ) of the internal combustion engine ( 10 ) and a turbine ( 23 ) located in a exhaust train ( 18 ) of the internal combustion engine ( 10 ), wherein the turbine ( 23 ) comprises a turbine housing ( 12 ) with at least one first and one second spiral passage ( 14 a , 14 b ), each of which is coupled to at least one of the two exhaust gas lines ( 16 a , 16 b ) of the exhaust train ( 18 ) and through each of which exhaust gas can flow independently, and with a turbine wheel ( 22 ) located within a locating chamber ( 20 ) of the turbine housing ( 12 ), to which the exhaust gas of the internal combustion engine ( 10 ), which can be routed through the first and second spiral passages ( 14 a , 14 b ), can be admitted to drive a compressor impeller ( 25 ) of the compressor ( 27 ) which is coupled thereto for rotation therewith via a drive shaft ( 24 ), the first and second spiral passages ( 14 a , 14 b ) having different wrap angles (φ s ) the first and the second spiral passages ( 14 a , 14 b ) comprising in the region leading to the rotor chamber ( 20 ) nozzles ( 28 a , 28 b ) with effective cross-sections (A D ) chosen according to the formula
A D =r D *2 *π*b D *sin(α D )*(φ S /360),
wherein:
A D denotes the effective cross-section of the respective nozzle ( 28 a , 28 b );
r D a radius of the respective nozzle ( 28 a , 28 b ) with respect to an axis of rotation (I) of the turbine wheel ( 22 );
b D the cross-sectional width of the respective nozzle ( 28 a , 28 b );
α D an angle between a circumferential speed vector and a radial speed vector of the exhaust gas flow in the cross-section of the respective nozzle ( 28 a , 28 b ); and
φ s the wrap angle of the respective spiral passage ( 14 a , 14 b ).
13. The internal combustion engine according to claim 12 , wherein an exhaust gas recirculation system ( 38 ) is provided in the exhaust train ( 18 ) upstream of the turbine ( 23 ), by means of which at least a part of the exhaust gas from at least one of the exhaust gas lines ( 16 a ) can be recirculated to the intake train ( 40 ).
14. The internal combustion engine according to claim 12 , wherein an exhaust treatment system ( 44 ), including at least one of a particulate filter, a catalytic converter and an SCR system, is provided in the exhaust train ( 18 ) downstream of an exhaust gas outlet ( 26 ) of the turbine housing ( 12 ).