Method and control device for a turbocharger having a variable turbine flow cross section
View Patent ↗An actual value of a turbine flow cross section of a turbocharger of an internal combustion engine in a motor vehicle is set for a change in the load on the internal combustion engine from a larger load value to a smaller load value. The actual value setting of the smaller load value is delayed to a setpoint value that is specified for the smaller load value under stationary conditions. A device controls the progression of the method.
1. A method for setting a value of a turbine flow cross section of a turbocharger of an internal combustion engine in a motor vehicle comprising:
changing a load on the internal combustion engine from a larger load value to a smaller load value as occurs after an acceleration and a subsequent heavy reduction of a torque requirement;
determining an actual value of the turbine flow cross section; and
transitioning from actual value of the turbine flow cross section to a setpoint value set for the smaller load value in a delayed manner to avoid a critical combination of hot guide blades and guide blades in an opened guide blade position, wherein said critical combination tends to jam the guide blades.
2. The method according to claim 1 , wherein the setpoint value to be specified under stationary conditions is set by specifying a progression of setpoint values that results in the setpoint value which is to be specified under stationary conditions.
3. The method according to claim 2 , wherein the progression is specified as a function of operating parameters of the internal combustion engine.
4. The method according to claim 3 , wherein the progression is a function of at least one of: combustion chamber fuel charge, rotational speed, exhaust gas temperature, and cumulative mass air flow rate.
5. The method according to claim 3 , wherein the operating parameters are dependent on the surroundings in which the internal combustion engine is operated.
6. The method according to claim 5 , wherein the operating parameters include at least one operating parameter which indicates a pressure or a temperature in the intake system of the internal combustion engine.
7. The method according to claim 2 , wherein the progression has at least one intermediate value of the turbine flow cross section larger than the turbine flow cross section set for the larger load value and is smaller than the turbine flow cross section to be set for the smaller load value under stationary conditions.
8. The method according to claim 1 , wherein the delayed manner has a time duration of the delay being limited to a predetermined maximum value of time.
9. The method according to claim 1 , further comprising making a check as to whether a guide blade adjustment mechanism is jammed, and activating a breakaway function in the event of a jam.
10. The method according to claim 9 , wherein the breakaway function is periodically repeated.
11. The method according to claim 9 , further comprising determining a frequency of occurrence of a jamming guide blade adjustment mechanism, and activating an emergency program when the frequency exceeds a predetermined threshold value.
12. The method according to claim 11 , wherein the breakaway function is periodically repeated.
13. A controller for setting a value of a turbine flow cross section of a turbocharger of an internal combustion engine in a motor vehicle comprising:
a control device, said control device is configured to receive a change in a load on the internal combustion engine from a larger load value to a smaller load value as occurs after an acceleration and a subsequent heavy reduction of a torque requirement;
said control device is configured to determine an actual value of the turbine flow cross section; and
said control device is configured to control a transition from said actual value of the turbine flow cross section to a setpoint value set for the smaller load value in a delayed manner to avoid a critical combination of hot guide blades and guide blades in an opened guide blade position, wherein said critical combination tends to jam the guide blades.
14. The controller according to claim 13 , wherein the control device is configured to control a progression of setpoint values that results in the setpoint value to be specified under stationary conditions.
15. The controller according to claim 14 , wherein the progression is specified as a function of operating parameters of the internal combustion engine.
16. The controller according to claim 15 , wherein the progression is a function of at least one of: combustion chamber fuel charge, rotational speed, exhaust gas temperature, and cumulative mass air flow rate.
17. The controller according to claim 14 , wherein the operating parameters are dependent on the surroundings in which the internal combustion engine is operated.
18. The controller according to claim 17 , wherein the operating parameters include at least one operating parameter which indicates a pressure or temperature in the intake system of the internal combustion engine.
19. The controller according to claim 14 , wherein the progression has at least one intermediate value of the turbine flow cross section larger than the turbine flow cross section set for the larger load value and is smaller than the turbine flow cross section to be set for the smaller load value under stationary conditions.
20. The controller according to claim 13 , further comprising making a check as to whether a guide blade adjustment mechanism is jammed, and activating a breakaway function in the event of a jam.