초록 ▼

The disclosure relates to a method for controlling a turbocharger system of an internal combustion engine. The method comprises controlling a first bypass valve of a high pressure exhaust gas turbine and a second bypass valve of a low pressure gas turbine on the basis of a turbine model, the first a

The disclosure relates to a method for controlling a turbocharger system of an internal combustion engine. The method comprises controlling a first bypass valve of a high pressure exhaust gas turbine and a second bypass valve of a low pressure gas turbine on the basis of a turbine model, the first and second bypass valves continuously variable. In this way, turbocharger system efficiency may be maximized.

대표청구항 ▼

1. A method for controlling a turbocharger system of an internal combustion engine, comprising: controlling a first bypass valve of a high pressure exhaust gas turbine and a second bypass valve of a low pressure gas turbine based on a turbine model, the model determining set positions of the first a

1. A method for controlling a turbocharger system of an internal combustion engine, comprising: controlling a first bypass valve of a high pressure exhaust gas turbine and a second bypass valve of a low pressure gas turbine based on a turbine model, the model determining set positions of the first and second bypass valves, and the first and second bypass valves continuously variable; andadjusting one of the first or second bypass valve while maintaining the set position of the other of the first or second bypass valve to maintain charge pressure and engine load. 2. The method as claimed in claim 1, wherein the first and second bypass valves are controlled in such a manner that turbine efficiency is at a maximum. 3. The method as claimed in claim 2, wherein a product of turbine efficiencies of the high pressure (ηHP) and of the low pressure exhaust gas turbine (ηLP) is at a maximum. 4. The method as claimed claim 1, wherein the first and second bypass valves are controlled as a function of a working point of the internal combustion engine, of a ratio of an inlet pressure to an outlet pressure of the high pressure and/or of the low pressure exhaust gas turbine, and/or of a rotational speed of the high pressure and/or of the low pressure exhaust gas turbine. 5. The method as claimed in claim 1, wherein the first or the second bypass valve is adjusted as a function of a charge pressure of the internal combustion engine. 6. The method as claimed in claim 5, wherein the first bypass valve is adjusted as a function of the charge pressure at low speed and/or low load of the internal combustion engine, and the second bypass valve is adjusted as a function of the charge pressure at relatively high speed and/or relatively high load of the internal combustion engine. 7. A turbocharger method, comprising: determining respective set positions of a first bypass valve of a high pressure turbine and a second bypass valve of a low pressure turbine;determining a set-point error comprising a difference between a desired set-point charge pressure and a measured charge pressure;under a first condition, maintaining the first bypass valve at the set position for the first bypass valve and adjusting a position of the second bypass valve away from the set position according to the set-point error to maintain charge pressure and engine load; andunder a second condition, maintaining the second bypass valve at the set position for the second bypass valve and adjusting a position of the first bypass valve away from the set position according to the set-point error to maintain charge pressure and engine load. 8. The method of claim 7, wherein the first condition comprises a third bypass valve of a high pressure compressor being open, and wherein the second condition comprises the third bypass valve being closed. 9. The method of claim 8, wherein the third bypass valve is open during high speed and high load conditions and is closed during low speed and low load conditions. 10. The method of claim 8, wherein the third bypass valve is passively controlled based on charge pressure. 11. The method of claim 7, wherein the set positions of the first and second bypass valves are determined as a function of engine speed and load. 12. A turbocharger system of an internal combustion engine, comprising: at least one high pressure exhaust gas turbine with a continuously variable position first bypass valve;at least one low pressure exhaust gas turbine with a continuously variable position second bypass valve, the low pressure exhaust gas turbine connected downstream of the high pressure exhaust gas turbine in an exhaust gas flow, the high pressure exhaust gas turbine driving a high pressure compressor and the low pressure exhaust gas turbine driving a low pressure compressor connected upstream of the high pressure compressor in a charge air flow; anda control system including a processor storing a non-transitory computer readable code executable to control a set position of the first and second bypass valve and adjust one of the first or second bypass valve while maintaining the set position of the other of the first or second bypass valve to maintain charge pressure and engine load. 13. The turbocharger system as claimed in claim 12, wherein the high pressure compressor has a third bypass valve. 14. The turbocharger system as claimed in claim 13, wherein the third bypass valve is controlled as a function of charge pressure. 15. The turbocharger system as claimed in claim 12, wherein the high pressure and/or the low pressure exhaust gas turbine have a rotational speed sensor. 16. The turbocharger system as claimed in claim 12, wherein the internal combustion engine has an exhaust gas recirculation system. 17. The turbocharger system as claimed in claim 12, wherein the control system controls the set position of the first and second bypass valves as a function of one or more of engine speed, engine load, pressure ratio across the high pressure and/or low pressure turbine, and rotation speed of the high pressure and/or low pressure turbine. 18. The turbocharger system as claimed in claim 17, wherein the control system adjusts the first bypass valve as a function of charge pressure at low speed and/or low load of the internal combustion engine, and adjusts the second bypass valve as a function of charge pressure at relatively high speed and/or relatively high load of the internal combustion engine.