Method of operating an engine assembly

Patent metadata

Field	Value
Publication number	US-10895207-B2
Application number	US-201816222818-A
Country	US
Kind code	B2
Filing date	Dec 17, 2018
Priority date	Jan 4, 2018
Publication date	Jan 19, 2021
Grant date	Jan 19, 2021

Abstract

A method of operating an engine assembly is provided. The engine assembly comprises an engine and a turbocharger assembly, wherein a control parameter of the turbocharger assembly is controllable in order to control a level of boost provided by the turbocharger assembly. The method comprises determining a desirable pressure limit of exhaust gases upstream of a turbine of the turbocharger assembly, predicting a desirable limit value of the control parameter to be applied to the turbocharger assembly in order to achieve the desirable pressure limit, determining an error in the desirable limit value of the control parameter, adjusting the desirable limit value of the control parameter based on the error, and controlling the operation of the turbocharger assembly such that the adjusted limit value is not exceeded.

First claim

The invention claimed is:

1. A method of operating an engine assembly, the engine assembly comprising:
an engine; and
a turbocharger assembly, wherein a control parameter of the turbocharger assembly is controllable in order to control a level of boost provided by the turbocharger assembly, and wherein the method comprises:
determining a desirable pressure limit of exhaust gases upstream of a turbine of the turbocharger assembly;
predicting a desirable limit value of the control parameter to be applied to the turbocharger assembly in order to achieve the desirable pressure limit;
determining an error in the desirable limit value of the control parameter; predicting a current value of the control parameter based on a current pressure of exhaust gases upstream of the turbine; determining a current value of the control parameter; and determining the error in the desirable limit value of the control parameter as being between the predicted current value of the control parameter and the current value of the control parameter;
adjusting the desirable limit value of the control parameter based on the error; and
controlling operation of the turbocharger assembly such that the adjusted desirable limit value is not exceeded.

2. The method of claim 1 , wherein determining the current value of the control parameter comprises calculating the control parameter based on a predicted current exhaust manifold pressure.

3. The method of claim 1 , wherein the desirable pressure limit is determined according to one or more of:
a maximum inlet pressure limit of the turbocharger assembly;
a maximum pressure ratio limit between an inlet and an outlet of the turbocharger assembly; and
a maximum permitted rate of increase of a pressure of exhaust gases upstream of the turbine.

4. The method of claim 3 , wherein the engine assembly further comprises an Exhaust Gas Recirculation (EGR) system configured to recirculate exhaust gases from a position upstream of the turbine of the turbocharger assembly, to an inlet of the engine, wherein the maximum permitted rate of increase of the pressure of exhaust gases upstream of the turbine is determined at least partially according to the operation of the EGR system.

5. The method of claim 4 , wherein the method further comprises:
varying the operation of the EGR system such that a flow rate of recirculated exhaust gases remains substantially constant as the turbocharger assembly is controlled.

6. The method of claim 1 , wherein the operation of the turbocharger assembly is controlled according to a minimum of:
a desired value of the control parameter; and
the adjusted desirable limit value of the control parameter.

7. The method of claim 1 , wherein the method further comprises controlling the operation of the turbocharger assembly using a closed feedback loop if a pressure of the exhaust gases upstream of the turbine exceeds the desirable pressure limit of the exhaust gases upstream of the turbine.

8. The method of claim 1 , further comprising detecting a request for an increased amount of torque to be supplied by the engine assembly.

9. The method of claim 8 , wherein the method is performed for a predetermined period of time following the request for an increased amount of torque being detected.

10. The method of claim 1 , wherein the turbocharger assembly comprises a Variable Geometry Turbine (VGT) and wherein the control parameter of the turbocharger assembly corresponds to the geometry of the VGT.

11. The method of claim 1 , wherein the turbocharger assembly comprises a turbocharger assembly bypass duct, configured to permit exhaust gases to bypass a turbine of the turbocharger assembly, wherein a flow of exhaust gases through the bypass duct is controlled by a bypass valve; and wherein the control parameter of the turbocharger assembly corresponds to a position of the bypass valve.

12. The method of claim 1 , where the method is performed by software which, when executed by a computing device, causes the computing device to perform the method.

13. An engine assembly comprising:
an engine;
a turbocharger assembly, a control parameter of the turbocharger assembly being controllable in order to control a level of boost provided by the turbocharger assembly; and
one or more controllers configured to;
determine a desirable pressure limit of exhaust gases upstream of a turbine of the turbocharger assembly;
predict a desirable limit value of the control parameter to be applied to the turbocharger assembly in order to achieve the desirable pressure limit; predicting a current value of the control parameter based on a current pressure of exhaust gases upstream of the turbine; determining a current value of the control parameter; and determining the error in the desirable limit value of the control parameter as being between the predicted current value of the control parameter and the current value of the control parameter;
determine an error in the desirable limit value of the control parameter;
adjust the desirable limit value of the control parameter based on the error; and
control operation of the turbocharger assembly such that the adjusted desirable limit value is not exceeded.

14. The engine assembly of claim 13 , wherein the engine assembly is included in a motor vehicle.

15. A method of operating an engine assembly, the engine assembly comprising:
an engine; and
a turbocharger assembly, a control parameter of the turbocharger assembly being controllable in order to control a level of boost provided by the turbocharger assembly, wherein the method comprises:
determining a desirable pressure limit of exhaust gases upstream of a turbine of the turbocharger assembly;
predicting a desirable limit value of the control parameter to be applied to the turbocharger assembly in order to achieve the desirable pressure limit;
determining an error in the desirable limit value of the control parameter; predicting a current value of the control parameter based on a current pressure of exhaust gases upstream of the turbine; determining a current value of the control parameter; and determining the error in the desirable limit value of the control parameter as being between the predicted current value of the control parameter and the current value of the control parameter;
adjusting the desirable limit value of the control parameter based on the error; and
controlling the operation of the turbocharger assembly such that the adjusted limit value is not exceeded;
wherein the operation of the turbocharger assembly is controlled according to a minimum of:
a desired value of the control parameter; and
the adjusted desirable limit value of the control parameter.

16. The method of claim 15 , further comprising detecting a request for an increased amount of torque to be supplied by the engine assembly;
wherein the method is performed for a predetermined period of time following the request for an increased amount of torque being detected.

17. The method of claim 15 , wherein determining the current value of the control parameter comprises calculating the control parameter based on a predicted current exhaust manifold pressure.

18. The method of claim 15 , wherein the method further comprises controlling the operation of the turbocharger assembly using a closed feedback loop if a pressure of the exhaust gases upstream of the turbine exceeds the desirable pressure limit of the exhaust gases upstream of the turbine.

Assignees

• Ford Global Tech Llc

Inventors

• Dixon Jon
• Parisi Nicholas Michael
• Schneyer Jeffrey B

Classifications

• F02B37/24

  by using pumps or turbines with adjustable guide vanes · CPC title

• F02M26/02

  EGR systems specially adapted for supercharged engines · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F02B2039/166

  the fluid pressure in the pump or exhaust drive being limited · CPC title

• F02B37/12 Primary

  Control of the pumps · CPC title