System for controlling an air handling system including an electric motor assisted variable geometry turbocharger

Patent metadata

Field	Value
Publication number	US-9528432-B2
Application number	US-201113244551-A
Country	US
Kind code	B2
Filing date	Sep 25, 2011
Priority date	Sep 25, 2011
Publication date	Dec 27, 2016
Grant date	Dec 27, 2016

Abstract

A system and method are provided for controlling an air handling system for an internal combustion engine including a turbocharger having a variable geometry turbine fluidly coupled to an exhaust manifold of the engine and a compressor fluidly coupled to an intake manifold of the engine, and an electric motor coupled to a rotatable shaft connected between the compressor and the variable geometry turbine. A target torque required to drive the compressor to achieve target compressor operating parameters is determined, a maximum available torque that can be supplied by the variable geometry turbine in response to a target exhaust gas flow through the variable geometry turbine is determined, and the electric motor is enabled to supply supplemental torque to the rotatable shaft if the target torque is greater than the maximum available torque.

First claim

What is claimed is:

1. An air handling system for an internal combustion engine, comprising:
a turbocharger having a variable geometry turbine fluidly coupled to an exhaust manifold of the engine and a compressor fluidly coupled to an intake manifold of the engine, the variable geometry turbine rotatably connected to the compressor via a rotatable shaft such that the variable geometry turbine rotatably drives the compressor via the rotatable shaft in response to exhaust gas passing through the variable geometry turbine,
an electric motor coupled to the rotatable shaft of the turbocharger, and a control circuit having executable instructions stored in a non-transitory memory to:
determine a total target torque required to drive the compressor to achieve target compressor operating parameters;
determine a peak available turbine torque being supplied by a variable geometry turbine rack position in response to target exhaust gas conditions;
generate a supplemental torque via activating the electric motor on the rotatable shaft of the turbocharger if the total target torque is greater than the peak available turbine torque, wherein the supplemental torque being generated by the electric motor in combining with the peak available turbine torque is to achieve the total target torque; and
adjusting at least one of an exhaust gas flow and an exhaust gas recirculation flow via changing the variable geometry turbine rack position.

2. The system of claim 1 wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to control the variable geometry turbine to a geometry in which the turbine produces torque in an amount of a difference between the total target torque and the supplemental torque when the electric motor is enabled to supply the supplemental torque.

3. The system of claim 2 wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to control the variable geometry turbine to an over-opened geometry to produce the torque in the amount of the difference between the total target torque and the supplemental torque when it is desirable to optimize at least one of brake specific fuel consumption or fuel economy.

4. The system of claim 2 wherein the air handling system further includes an exhaust gas recirculation (EGR) fluid passageway fluidly coupled between the exhaust manifold and the intake manifold, and
wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to control the variable geometry turbine to an over-closed geometry to produce the torque in the amount of the difference between the total target torque and the supplemental torque when it is desirable to maximize exhaust gas flow through the EGR fluid passageway.

5. The system of claim 1 wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to disable the electric motor such that the electric motor does not supply the supplemental torque to the rotatable shaft if the peak available turbine torque is greater than or equal to the total target torque.

6. The system of claim 1 wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to determine the total target torque required to drive the compressor to achieve target compressor operating parameters by determining a target compressor torque corresponding to a target torque required to drive the compressor alone to achieve the target compressor operating conditions, determining an inertia torque as a function of a target rotational speed of the rotatable shaft, the inertia torque corresponding to torque associated with rotation of the rotatable shaft and of the electric motor, determining a bearing housing torque as a function of the target rotational speed of the rotatable shaft, the bearing housing torque corresponding to a friction torque associated with at least one bearing of a bearing housing of the turbocharger, and determining the target torque as a sum of the target compressor torque, the inertia torque and the bearing housing torque.

7. The system of claim 6 wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to determine the target rotational speed of the rotatatable shaft based on the target compressor operating parameters.

8. The system of claim 6 wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to determine the target compressor torque as a function of a target compressor outlet pressure and a target compressor flow rate.

9. The system of claim 1 wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to determine the target exhaust gas conditions based on target charge parameters and target engine fueling parameters.

10. The system of claim 9 wherein the air handling system further includes an exhaust gas recirculation (EGR) fluid passageway fluidly coupled between the exhaust manifold and the intake manifold, and
wherein the executable instructions stored in the non-transitory memory further include instructions that are executable by the control circuit to determine the target exhaust gas conditions based on a target EGR flow rate.

11. A method of controlling an air handling system, carried out by a control circuit, for an internal combustion engine including a turbocharger having a variable geometry turbine fluidly coupled to an exhaust manifold of the engine and a compressor fluidly coupled to an intake manifold of the engine, and an electric motor coupled to a rotatable shaft of the turbocharger connected between the compressor and the variable geometry turbine, the method comprising:
determining a total target torque required to drive the compressor to achieve target compressor operating parameters;
determining a peak available turbine torque being supplied by a variable geometry turbine rack position in response to a target exhaust gas conditions;
generating a supplemental torque via activating an electric motor on the rotatable shaft of the turbocharger if the total target torque is greater than the peak available turbine torque, wherein the supplemental torque being generated by the electric motor in combining with the peak available turbine torque is to achieve the total target torque; and
adjusting at least one of an exhaust gas flow and an exhaust gas recirculation flow via changing the variable geometry turbine rack position.

12. The method of claim 11 further comprising controlling the variable geometry turbine to a geometry in which the turbine produces torque in an amount of a difference between the total target torque and the supplemental torque when the electric motor is enabled to supply the supplemental torque.

13. The method of claim 12 further comprising controlling the variable geometry turbine to an over-opened geometry to produce the torque in the amount of the difference between the total target torque and the supplemental torque when it is desirable to optimize at least one of brake specific fuel consumption or fuel economy.

14. The method of claim 12 wherein the air handling system further includes an exhaust gas recirculation (EGR) fluid passageway fluidly coupled between the exhaust mani

Assignees

• Chi John N
• Mulloy John M
• Popuri Sriram S
• Frazier Timothy R
• Books Martin T
• Rajamohan Divakar
• Brahma Indranil
• Cummins Inc

Inventors

• Chi John N
• Mulloy John M
• Popuri Sriram S
• Frazier Timothy R
• Books Martin T
• Rajamohan Divakar
• Brahma Indranil

Classifications

• Y02T10/144

  Cross-Sectional Technologies · mapped topic

• F02B37/14

  {Control} of the alternation between {or the operation of} exhaust drive and other drive of a pump, e.g. dependent on speed · CPC title

• F02D41/1467

  with determination means using an estimation · CPC title

• F02M26/23

  Layout, e.g. schematics · CPC title

• F02D41/0052

  Feedback control of engine parameters, e.g. for control of air/fuel ratio or intake air amount · CPC title