Method and device for ascertaining a modeling value for a physical variable in an engine system having an internal combustion engine

Patent metadata

Field	Value
Publication number	US-9309826-B2
Application number	US-201213710864-A
Country	US
Kind code	B2
Filing date	Dec 11, 2012
Priority date	Dec 15, 2011
Publication date	Apr 12, 2016
Grant date	Apr 12, 2016

Abstract

A method for determining a modeling value of a physical variable in a gas guiding section of an engine system including an internal combustion engine, includes the following steps: operating the engine system in such a way that an air mass flow is present in the gas guiding section; determining instantaneous values of other physical variables; and determining the modeling value of the physical variable by solving a differential equation, which results as the discretization of a differential equation, with the aid of the previously ascertained instantaneous values of the other physical variables.

First claim

What is claimed is:

1. An automated method for determining a modeling value of at least one physical variable at a specific point in an exhaust gas discharge section of an engine system including an internal combustion engine which is supplied with air via an air supply section, the method comprising:
operating the engine system to produce an exhaust gas mass flow in the exhaust gas discharge section;
determining instantaneous values of other physical variables; and
determining the modeling value of the at least one physical variable by solving a differential equation, which results as a discretization of a differential equation, with aid of the previously ascertained instantaneous values of the other physical variables, wherein the at least one physical variable corresponds to at least one of a pressure and an exhaust gas mass flow at a branching point of the exhaust gas discharge section downstream from a turbine of an exhaust-gas-driven turbocharger, wherein (i) a first branch from the branching point leads to a discharge point for the exhaust gas, and (ii) a second branch from the branching point forms a part of an exhaust gas recirculation line connecting the branching point to an intake point of the air supply section.

2. The method according to claim 1 , wherein the differential equation is formed based on an equation system employing at least one of a throttle model, ideal gas equation and law of conservation of mass.

3. The method according to claim 1 , wherein the other physical variables include a position of an exhaust gas recirculation valve, which is situated in a low-pressure-side exhaust gas recirculation line, a position of an exhaust gas valve, which is situated downstream from a branching point for the exhaust gas recirculation line, ambient pressure, an exhaust gas flow flowing to the branching point, a temperature of the exhaust gas at the branching point, and a pressure at an intake point of the exhaust gas recirculation line upstream from a compressor of an exhaust-gas-driven turbocharger.

4. The method according to claim 1 , wherein the discretization of the differential equation is carried out according to an implicit method.

5. The method according to claim 1 , wherein the modeling value of the at least one physical variable is used in one of an exhaust gas recirculation rate regulation and an air flow regulation.

6. The method according to claim 1 , wherein the differential equation is solved by an iterative method to determine the at least one physical variable.

7. The method according to claim 6 , wherein the iterative method is carried out between a first limiting value and a second limiting value for the at least one physical variable.

8. The method according to claim 7 , wherein the other physical variables include a first pressure in a first volume portion of the exhaust gas discharge section and a second pressure in a second volume portion of the exhaust gas discharge section, the first volume portion and the second volume portion being separated from one another by a flow resistance, the first limiting value for the at least one physical variable being determined in that the first pressure is set equal to the second pressure, and the second limiting value for the at least one physical variable being determined in that the second pressure is set equal to the first pressure.

9. The method according to claim 1 , wherein the modeling value of the at least one physical variable is determined for a plausibility check of the at least one physical variable.

10. The method according to claim 1 , wherein the at least one physical variable corresponds to the pressure and the exhaust gas mass flow at the branching point.

11. A control device of an engine system for determining a modeling value of at least one physical variable at a specific point in an exhaust gas discharge section of the engine system including an internal combustion engine which is supplied with air via an air supply section, the control device comprising:
a control unit including a processor configured to:
operate the engine system to produce an exhaust gas mass flow in the exhaust gas discharge section;
determine instantaneous values of other physical variables; and
determine the modeling value of the at least one physical variable by solving a differential equation, which results as a discretization of a differential equation, with aid of the previously ascertained instantaneous values of the other physical variables, wherein the at least one physical variable corresponds to at least one of a pressure and an exhaust gas mass flow at a branching point of the exhaust gas discharge section downstream from a turbine of an exhaust-gas-driven turbocharger, wherein (i) a first branch from the branching point leads to a discharge point for the exhaust gas, and (ii) a second branch from the branching point forms a part of an exhaust gas recirculation line connecting the branching point to an intake point of the air supply section.

12. The control device according to claim 11 , wherein the at least one physical variable corresponds to the pressure and the exhaust gas mass flow at the branching point.

13. A non-transitory computer-readable medium having stored thereon a computer program having program codes which, when executed on a computer, perform an automated method for determining a modeling value of at least one physical variable at a specific point in an exhaust gas discharge section of an engine system including an internal combustion engine which is supplied with air via an air supply section, the method comprising:
operating the engine system to produce an exhaust gas mass flow in the exhaust gas discharge section;
determining instantaneous values of other physical variables; and
determining the modeling value of the at least one physical variable by solving a differential equation, which results as a discretization of a differential equation, with aid of the previously ascertained instantaneous values of the other physical variables, wherein the at least one physical variable corresponds to at least one of a pressure and an exhaust gas mass flow at a branching point of the exhaust gas discharge section downstream from a turbine of an exhaust-gas-driven turbocharger, wherein (i) a first branch from the branching point leads to a discharge point for the exhaust gas, and (ii) a second branch from the branching point forms a part of an exhaust gas recirculation line connecting the branching point to an intake point of the air supply section.

14. The non-transitory computer-readable medium according to claim 13 , wherein the at least one physical variable corresponds to the pressure and the exhaust gas mass flow at the branching point.

Assignees

• Wagner Alexandre
• Bleile Thomas
• Lux Slobodanka
• Fleck Christian
• Bosch Gmbh Robert

Inventors

• Wagner Alexandre
• Bleile Thomas
• Lux Slobodanka
• Fleck Christian

Classifications

• F02M25/0728

  Mechanical Engineering · mapped topic

• F02D41/263 Primary

  the program execution being modifiable by physical parameters · CPC title

• F02M25/0707

  Mechanical Engineering · mapped topic

• F02D41/1446

  the characteristics being exhaust temperatures · CPC title

• Y02T10/47

  Cross-Sectional Technologies · mapped topic