Granted Patent B2

US 8,276,378 · App. 12/507,455 · Granted Oct 2, 2012

Abstract

Claims (43)

1. A method for controlling an engine including a turbocharging system with a high pressure turbocharger and a low pressure turbocharger, comprising:

in a first load-engine speed region, operating a variable nozzle turbine of the high pressure turbocharger in a transient position by performing closed loop control of the variable nozzle turbine based on boost pressure, and operating a high pressure turbine bypass valve in a closed position;

in a second load-engine speed region between the first load-engine speed region and a third load-engine speed region, operating the variable nozzle turbine in a maximum open position, and operating the high pressure turbine bypass valve in a transient position by performing closed loop control of the high pressure turbine bypass valve based on a position of the high pressure turbine bypass valve and a measured current flowing to the high pressure turbine bypass valve; and

in the third load-engine speed region, operating the variable nozzle turbine in a transient position by performing open loop control of the variable nozzle turbine based on boost pressure, and operating the high pressure turbine bypass valve in a transient position by performing closed loop control of the high pressure turbine bypass valve based on the position of the high pressure turbine bypass valve.

2. A method as recited in claim 1 further comprising determining a target exhaust flow from a target boost pressure.

3. A method as recited in claim 2 further comprising determining the target boost pressure from an engine load and an engine speed.

4. A method as recited in claim 3 further comprising operating in the first load-engine speed region when a high pressure turbocharger maximum flow capacity is greater than the target exhaust flow.

5. A method as recited in claim 3 further comprising operating in the third load-engine speed region when the target exhaust flow is less than a control limit flow.

6. A method as recited in claim 3 further comprising operating in the second load-engine speed region when a high pressure turbocharger maximum flow capacity is less than the target exhaust flow and when the target exhaust flow is greater than a control limit flow.

7. A method as recited in claim 1 further comprising controlling the current to the high pressure turbine bypass valve based on a target boost pressure and a sensed boost pressure in the second load-engine speed region.

8. A method as recited in claim 1 further comprising controlling the current to the high pressure turbine bypass valve to control leakage through the bypass valve in the second load-engine speed region.

9. A method as recited in claim 1 wherein in the second load-engine speed region, operating the high pressure turbine bypass valve in the transient position by performing closed loop control of the high pressure turbine bypass valve based on the current flowing to the high pressure turbine bypass valve comprises generating current to force the high pressure turbine bypass valve to the closed position.

10. A method as recited in claim 1 wherein in the second load-engine speed region, operating the high pressure turbine bypass valve in the transient position by performing closed loop control of the high pressure turbine bypass valve comprises modulating the high pressure turbine bypass valve using a negative pulse width modulated signal.

11. A method as recited in claim 1 wherein in the second load-engine speed region, controlling the position of the high pressure turbine bypass valve comprises controlling the position based on a target opening signal and a valve sensor signal.

12. A control system for controlling an engine including a turbocharging system with a high pressure turbocharger and a low pressure turbocharger, comprising:

a variable nozzle turbine control module that operates a variable nozzle turbine of the high pressure turbocharger in a transient position by performing closed loop control of the variable nozzle turbine based on boost pressure in a first load-engine speed region; and

a high pressure turbine bypass valve control module that operates a high pressure turbine bypass valve in a closed position in the first load-engine speed region,

wherein the variable nozzle turbine control module operates the variable nozzle turbine in a maximum open position in a second load-engine speed region between the first load-engine speed region and a third load-engine speed region,

wherein the high pressure turbine bypass valve control module operates the high pressure turbine bypass valve in a transient position by performing closed loop control of the high pressure turbine bypass valve based on a position of the high pressure turbine bypass valve and a measured current flowing to the high pressure turbine bypass valve in the second load-engine speed region,

wherein the variable nozzle turbine control module operates the variable nozzle turbine in a transient position by performing open loop control of the variable nozzle turbine based on boost pressure in the third load-engine speed region, and

wherein the high pressure turbine bypass valve control module operates the high pressure turbine bypass valve in a transient position by performing closed loop control of the high pressure turbine bypass valve based on the position of the high pressure turbine bypass valve in the third load-engine speed region.

13. A control system as recited in claim 12 wherein during the second load-engine speed region, the high pressure turbine bypass valve control module controls the current to the high pressure turbine bypass valve to control leakage through the bypass valve.

14. A control system as recited in claim 12 further comprising:

a first comparison module that generates a first comparison signal when a high pressure turbocharger maximum flow capacity is less than a target exhaust flow, wherein the target exhaust flow is determined based on engine speed and engine load; and

a second comparison module that generates a second comparison signal when the target exhaust flow is greater than a control limit flow,

wherein the variable nozzle turbine control module commands operation in the second load-engine speed region in response to the first comparison signal and the second comparison signal.

15. A system comprising:

an engine;

the high pressure turbocharger having a high pressure variable geometry turbine and a high pressure compressor;

the low pressure turbocharger in series with the high pressure turbocharger having a low pressure turbine and a low pressure compressor;

the high pressure turbine bypass valve bypassing the high pressure turbine; and

the control system as recited in claim 12 .

16. A method for controlling an engine system comprising a variable-geometry turbocharger (VGT), the method comprising:

determining a target boost pressure for the VGT based on an engine load and an engine speed;

determining a target exhaust flow based on the target boost pressure;

comparing the target exhaust flow to each of a predetermined limit and a maximum flow capacity of the VGT, wherein the predetermined limit is based on characteristics of at least one of the engine and the VGT, and wherein the predetermined limit is greater than the maximum flow capacity of the VGT; and

when the target exhaust flow is less than or equal to the predetermined limit and greater than the maximum flow capacity of the VGT:

(i) commanding the VGT to a maximum open position, and

(ii) performing closed loop control of a current flowing to a bypass valve for the VGT based on a difference between the target boost pressure and a measured boost pressure, wherein the bypass valve is configured to redirect exhaust gas from the engine to bypass the VGT.

17. The method of claim 16 , further comprising when the target exhaust flow is less than or equal to the predetermined limit and less than or equal to the maximum flow capacity of the VGT, performing closed loop control of a position of the bypass valve based on the difference between the target boost pressure and the measured boost pressure.

18. The method of claim 16 , further comprising when the target exhaust flow is greater than the predetermined limit, performing open loop control of the bypass valve based on the target boost pressure.

19. The method of claim 16 , wherein performing closed loop control of the current flowing to the bypass valve includes fully closing the bypass valve by supplying a maximum current to the bypass valve.

20. The method of claim 16 , wherein performing closed loop control of the current flowing to the bypass valve includes supplying a negative pulse width modulated (PWM) current to the bypass valve.

Assignments (8)

Continuity (1)