초록 ▼

A method for controlling a variable geometry turbine of a turbocharger to increase the temperature of the exhaust gas delivered to an after-treatment system. In one form the method includes reducing a fluid flow area to the turbine below a normal size and bypassing a portion of the exhaust gas aroun

A method for controlling a variable geometry turbine of a turbocharger to increase the temperature of the exhaust gas delivered to an after-treatment system. In one form the method includes reducing a fluid flow area to the turbine below a normal size and bypassing a portion of the exhaust gas around a plurality of guide vanes.

대표청구항 ▼

The invention claimed is: 1. A method comprising: operating a turbocharger including a variable geometry turbine having an inlet passage to the turbine with a fluid flow area, the fluid flow area having a normal size for an internal combustion engine operating in a normal operating range; reducing

The invention claimed is: 1. A method comprising: operating a turbocharger including a variable geometry turbine having an inlet passage to the turbine with a fluid flow area, the fluid flow area having a normal size for an internal combustion engine operating in a normal operating range; reducing the size of the fluid flow area from the normal size to a reduced size for exhaust gas heating, wherein the reduced size comprises a width between about zero and 4 millimeters; bypassing a portion of the exhaust gas entering the inlet passage around the guide vanes of the variable geometry turbine; and wherein said reducing exposes a bypass fluid flow path to the exhaust gas within the inlet passage, and wherein the bypass fluid flow path is normally blocked when the fluid flow area is of the normal size. 2. The method of claim 1, wherein in said bypassing the portion of the exhaust gas flows internally within the turbocharger. 3. The method of claim 1, wherein said reducing includes moving a portion of the variable geometry turbine. 4. The method of claim 1, wherein the fluid flow area has a maximum flow area, and wherein the flow area corresponding to said reduced size is within a range of about zero percent to about twenty-five percent of the maximum flow area. 5. The method of claim 1, which further includes determining the temperature of the exhaust gas passing from an outlet of the variable geometry turbine, and further includes operatively controlling said reducing based upon whether the temperature of the exhaust gas passing from the outlet of the variable geometry turbine satisfies a threshold temperature condition. 6. The method of claim 1, which further includes passing the exhaust gas from the variable geometry turbine to an after-treatment system; and which further includes determining the temperature of the exhaust gas in the after-treatment system, and operatively controlling said reducing based upon whether the temperature of the exhaust gas in the after-treatment system satisfies a threshold temperature condition. 7. A method for treating an exhaust gas, comprising: determining that an after-treatment system temperature is below a threshold temperature; operating a turbocharger including a variable geometry turbine having an inlet passage to the turbine with a fluid flow area, the fluid flow area having a normal size for an internal combustion engine operating in a normal operating range; in response to determining the after-treatment system temperature is below the threshold temperature, reducing the size of the fluid flow area from the normal size to a reduced size; and bypassing a portion of the exhaust gas entering the inlet passage around the guide vanes of the variable geometry turbine, wherein said reducing exposes a bypass fluid flow path to the exhaust gas within the inlet passage, and wherein the bypass fluid flow path is normally blocked when the fluid flow area is of the normal size. 8. The method of claim 7, wherein in said bypassing the portion of the exhaust gas flows internally within the turbocharger. 9. The method of claim 7, wherein said reducing includes moving a portion of the variable geometry turbine. 10. The method of claim 7, wherein the fluid flow area has a maximum flow area, and wherein the flow area corresponding to said reduced size is within a range of about zero percent to about twenty-five percent of the maximum flow area. 11. The method of claim 7, wherein the portion of the exhaust gas from said bypassing reenters the rest of the exhaust gas flowing to the turbine wheel from the inlet passage at a steep angle or substantially perpendicular thereto. 12. The method of claim 7, which further includes passing the exhaust gas from the variable geometry turbine to an after-treatment system; and which further includes determining the temperature of the exhaust gas in the after-treatment system, and operatively controlling said reducing based upon whether the temperature of the exhaust gas in the after-treatment system satisfies a threshold temperature condition. 13. A method comprising: operating a turbocharger including a variable geometry turbine having an inlet passage to the turbine with a fluid flow area, the fluid flow area having a normal size for an internal combustion engine operating in a normal operating range; reducing the size of the fluid flow area from the normal size to a reduced size for exhaust gas heating, wherein the reduced size comprises a width between about zero and 4 millimeters; bypassing a portion of the exhaust gas entering the inlet passage around the guide vanes of the variable geometry turbine, wherein said reducing exposes a bypass fluid flow path to the exhaust gas within the inlet passage, and wherein the bypass fluid flow path is normally blocked when the fluid flow area is of the normal size; and wherein the portion of the exhaust gas from said bypassing reenters the rest of the exhaust gas flowing to the turbine wheel from the inlet passage at a steep angle or substantially perpendicular thereto.