Method and control unit for adjusting a variable turbocharger turbine flow cross section
In a method for actuating an actuating member for adjusting a turbine flow cross section of a turbocharger of an internal combustion engine in a motor vehicle in the event of a change of the load of the internal combustion engine from a relatively low load value to a relatively high load value, the adjustment takes place at least at times by use of the closed-loop control of a scavenging gradient of the internal combustion engine. The method is characterized in that the turbine flow cross section, in the case of a spark-ignition engine as the internal combustion engine, is not fixedly held at a minimum turbine flow cross section between the change of the load and a beginning of an adjustment which is dependent on the scavenging gradient. A control unit is set up and controls the process of such a method.
1 . A method for actuating an actuating member for adjusting a turbine flow cross section of a turbocharger of an internal combustion engine in a motor vehicle in an event of a change of a load of the internal combustion engine from a relatively low load value to a relatively high load value, which comprises the steps of:
performing the adjusting at least at times by closed-loop control of a scavenging gradient of the internal combustion engine; and
not fixedly holding the turbine flow cross section at a minimum turbine flow cross section between a change of the load and a beginning of an adjustment being dependent on the scavenging gradient if the internal combustion engine is a spark-ignition engine.
2 . The method according to claim 1 , which further comprises determining an actual value of the scavenging gradient as a difference of a measured charge pressure value and an exhaust gas back pressure prevailing upstream of the turbine flow cross section as viewed in a flow direction of exhaust gases of the spark-ignition engine.
3 . The method according to claim 2 , which further comprises modeling the exhaust gas back pressure from operating parameters of the spark-ignition engine.
4 . The method according to claim 3 , which further comprises measuring the exhaust gas back pressure.
5 . The method according to claim 3 , which further comprises:
measuring the exhaust gas back pressure; and
using measured values of the exhaust gas back pressure for adapting modeled values of the exhaust gas back pressure.
6 . The method according to claim 1 , which further comprises performing the actuation, which is dependent on the scavenging gradient, of the actuating member with a delay in relation to a change of the load.
7 . The method according to claim 6 , which further comprises predefining a magnitude of the delay as a function of at least one operating parameter of the spark-ignition engine.
8 . The method according to claim 1 , which further comprises in steady-state operating states of the spark-ignition engine, adjusting the turbine flow cross section by use of a closed-loop control circuit and a charge pressure as a variable to be controlled.
9 . A control system for an internal combustion engine in a motor vehicle, the control system comprising:
a control unit for actuating an actuating member for adjusting a turbine flow cross section of a turbocharger of the internal combustion engine in an event of a change of a load of the internal combustion engine from a relatively low load value to a relatively high load value, the adjusting taking place at least at times by closed-loop control of a scavenging gradient of the internal combustion engine, said control unit being set up so as not to fixedly hold the turbine flow cross section, in a case of a spark-ignition engine as the internal combustion engine, at a minimum turbine flow cross section between a change of the load and a beginning of an adjustment being dependent on the scavenging gradient.
10 . The control system according to claim 9 , wherein said control unit determines an actual value of the scavenging gradient as a difference of a measured charge pressure value and an exhaust gas back pressure prevailing upstream of the turbine flow cross section as viewed in a flow direction of exhaust gases of the spark-ignition engine.