Charging device and associated operating method

1. A method for adjusting a charging device for an exhaust gas turbocharger of an internal combustion engine, comprising:

providing at least one of a variable turbine and compressor geometry;

measuring at least one of an aerodynamic minimum set flow and an aerodynamic maximum set flow through the at least one variable turbine and compressor geometry in different positions of an adjusting device, the adjusting device configured for adjusting the at least one variable turbine and compressor geometry;

determining an adjusting value of the adjusting device corresponding to a target value of the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow;

wherein the adjusting value is determined by one of an engine control unit after the installation of the charging device in an internal combustion engine in the case of a self-locking adjusting device, and a marking in the case of a non-self-locking adjusting device;

performing a set-actual value comparison with respect to the adjusting value corresponding to the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow during operation of the internal combustion engine;

upon a predefined set-actual value deviation, adjusting the adjusting device in response to the predefined set-actual value deviation; and

changing at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry in response to characteristics of at least one of the internal combustion engine and the charging device, the characteristics of the internal combustion engine including at least a charging pressure of the air to be fed to the internal combustion engine and the characteristics of the charging device including at least a rotational speed of a turbine.

2. The method according to claim 1 , wherein the characteristics of the at least one of the internal combustion engine and the charging device are represented by one of a characteristic curve and a characteristic diagram.

3. The method according to claim 2 , wherein the one of the characteristic curve and the characteristic diagram is defined on passing through predetermined parameters of at least one of the internal combustion engine and the charging device thereby defining corresponding minimum set flows and maximum set flows of at least one of the variable turbine and compressor geometry.

4. The method according to claim 1 , wherein the adjusting value in the case of the non-self-locking adjusting device is determined via one of a colour marking and a data matrix code (DMC).

5. The method according to claim 1 , wherein the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry is changed in response to the characteristics of the charging device, the characteristics of the charging device including at least the rotational speed of the turbine.

6. The method according to claim 5 , wherein the characteristics of the charging device and the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry is represented by one of a characteristic curve and a characteristic diagram.

7. The method according to claim 6 , wherein the one of the characteristic curve and the characteristic diagram is defined on passing through predetermined parameters of the charging device, thereby defining corresponding minimum set flows and maximum set flows of the at least one of the variable turbine and compressor geometry.

8. The method according to claim 1 , wherein the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry is changed in response to the characteristics of the internal combustion engine, the characteristics of the internal combustion engine include a charging pressure of air to be fed to the internal combustion engine.

9. The method according to claim 8 , wherein the characteristics of the internal combustion engine and the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry is represented by one of a characteristic curve and a characteristic diagram.

10. The method according to claim 9 , wherein the one of the characteristic curve and the characteristic diagram is defined on passing through predetermined parameters of the internal combustion engine, thereby defining corresponding minimum set flows and maximum set flows of the at least one of the variable turbine and compressor geometry.

11. The method according to claim 1 , wherein performing the set-actual value comparison includes comparing a measured aerodynamic flow of the at least one of the variable turbine and compressor geometry to the target valve of the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow corresponding to the adjusting value of the adjusting device.

12. The method according to claim 1 , wherein the predefined set-actual value deviation is represented by a deviation of a measured aerodynamic flow of the at least one of the variable turbine and compressor geometry from the target valve of the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow corresponding to the adjusting value of the adjusting device.

13. A charging device for an exhaust gas turbocharger of an internal combustion engine programmed to realize the method of claim 1 .

14. A method for adjusting a charging device for an exhaust gas turbocharger of an internal combustion engine, comprising:

providing at least one of a variable turbine and compressor geometry;

measuring at least one of an aerodynamic minimum set flow and an aerodynamic maximum set flow through the at least one variable turbine and compressor geometry in different positions of an adjusting device, the adjusting device configured for adjusting the at least one variable turbine and compressor geometry;

determining an adjusting value of the adjusting device corresponding to a target value of the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow;

wherein the adjusting value is determined by one of an engine control unit after the installation of the charging device in an internal combustion engine in the case of a self-locking adjusting device, and a marking in the case of a non-self-locking adjusting device;

performing a set-actual value comparison with respect to the adjusting value corresponding to the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow during operation of the internal combustion engine; and

upon a predefined set-actual value deviation, adjusting the adjusting device in response to the predefined set-actual value deviation;

wherein the adjusting value in the case of the non-self-locking adjusting device is determined via one of a colour marking and a data matrix code (DMC).

15. The method according to claim 14 , changing at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry in response to characteristics of at least one of the internal combustion engine and the charging device.

16. The method according to claim 15 , wherein the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry is changed in response to characteristics of the charging device, the characteristics of the charging device including at least a rotational speed of a turbine.

17. The method according to claim 15 , wherein the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry is changed in response to characteristics of the internal combustion engine, the characteristics of the internal combustion engine include a charging pressure of air to be fed to the internal combustion engine.

18. A charging device for an exhaust gas turbocharger of an internal combustion engine programmed to realize the method of claim 14 .

19. A method for adjusting a charging device for an exhaust gas turbocharger of an internal combustion engine, comprising:

providing at least one of a variable turbine and compressor geometry;

measuring at least one of an aerodynamic minimum set flow and an aerodynamic maximum set flow through the at least one variable turbine and compressor geometry in different positions of an adjusting device, the adjusting device configured for adjusting the at least one variable turbine and compressor geometry;

determining an adjusting value of the adjusting device corresponding to a target value of the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow;

wherein the adjusting value is determined by one of an engine control unit after the installation of the charging device in an internal combustion engine in the case of a self-locking adjusting device, and a marking in the case of a non-self-locking adjusting device;

performing a set-actual value comparison with respect to the adjusting value corresponding to the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow during operation of the internal combustion engine;

upon a predefined set-actual value deviation, adjusting the adjusting device in response to the predefined set-actual value deviation;

changing at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry in response to characteristics of at least one of the internal combustion engine and the charging device; and

wherein the characteristics of the at least one of the internal combustion engine and the charging device and the at least one of the aerodynamic minimum set flow and the aerodynamic maximum set flow of the at least one of the variable turbine and compressor geometry is represented by one of a characteristic curve and a characteristic diagram.