Fuel injection control of a turbocharged internal combustion engine

Patent metadata

Field	Value
Publication number	US-10260405-B2
Application number	US-201715496819-A
Country	US
Kind code	B2
Filing date	Apr 25, 2017
Priority date	Apr 25, 2017
Publication date	Apr 16, 2019
Grant date	Apr 16, 2019

Abstract

An internal combustion engine has a cylinder configured to combust an air-fuel mixture and expel an exhaust gas and a turbocharger for generating a pressurized airflow to the cylinder. The turbocharger includes a turbine scroll defining an inlet and an outlet, an exhaust gas driven rotating assembly having a turbine wheel disposed inside the turbine scroll, and a waste-gate defining an opening. A first sensor detects turbine outlet pressure. A second sensor detects turbine inlet temperature. A controller determines an effective area of the waste-gate opening and an exhaust gas mass flow-rate. The controller also determines a turbine inlet pressure in response to the detected turbine outlet pressure and the turbine inlet temperature, and the determined waste-gate opening effective area and the exhaust gas mass flow-rate. The controller additionally regulates a supply of fuel to the cylinder corresponding to the pressurized airflow affected by the determined turbine inlet pressure.

First claim

What is claimed is:

1. An internal combustion engine comprising:
a cylinder configured to receive a mixture of air and fuel for combustion therein and expel an exhaust gas following the combustion;
a fuel injector configured to supply the fuel;
a turbocharger configured to receive ambient air and generate a pressurized airflow for delivery to the cylinder, wherein the turbocharger includes: a compressor scroll;
a turbine scroll defining a turbine inlet and a turbine outlet;
a rotating assembly driven by the exhaust gas and having a turbine wheel disposed inside the turbine scroll and a compressor wheel disposed inside the compressor scroll; and
a waste-gate defining an opening configured to selectively redirect at least a portion of the exhaust gas to the turbine outlet bypassing the turbine wheel;
a first sensor configured to detect a pressure at the turbine outlet;
a second sensor configured to detect a temperature at the turbine inlet; and
a controller configured to determine the pressure at the turbine inlet using a second order polynomial function configured to:
determine an effective area of the waste-gate opening and a mass flow-rate of the exhaust gas;
determine a pressure at the turbine inlet in response to the detected pressure at the turbine outlet and temperature at the turbine inlet, and the determined effective area of the waste-gate opening and mass flow-rate of the exhaust gas; and
command the fuel injector to supply an amount of fuel to the cylinder corresponding to the pressurized airflow as affected by the determined pressure at the turbine inlet.

2. The engine of claim 1 , wherein the controller is programmed with a first lookup table correlating the turbine inlet pressure to the detected pressure at the turbine outlet and temperature at the turbine inlet, and the determined effective area of the waste-gate
opening and mass flow-rate of the exhaust gas, and wherein the controller is further configured to determine the pressure at the turbine inlet via the first lookup table.

3. The engine of claim 1 , wherein the second order polynomial function includes a factor indicative of the determined effective area of the waste-gate opening.

4. The engine of claim 3 , wherein the waste-gate includes a variable position valve configured to regulate the effective area of the waste-gate opening, and wherein the factor indicative of the determined effective area of the waste-gate opening is defined by a current position of the valve.

5. The engine of claim 1 , wherein the rotating assembly is driven by the exhaust gas at a rotational speed, and wherein the second order polynomial function includes a factor indicative of the rotational speed of the rotating assembly.

6. The engine of claim 5 , wherein the controller is programmed with a second lookup table correlating the rotational speed of the rotating assembly to a mass flow-rate of air through the compressor and a compressor pressure ratio, and wherein the controller is further configured to determine a current rotational speed of the rotating assembly via the second lookup table.

7. The engine of claim 1 , wherein the compressor scroll defines a compressor inlet and a compressor outlet, the engine further comprising:
a third sensor configured to detect a temperature at the compressor outlet; a fourth sensor configured to detect a pressure at the compressor outlet; a fifth sensor configured to detect a pressure at the compressor inlet; and wherein the controller is further configured to determine the pressure at the turbine inlet in response to the detected temperature and pressure at the compressor outlet, and the detected pressure at the compressor inlet.

8. The engine of claim 1 , wherein the compressor scroll defines a compressor inlet and a compressor outlet, and wherein the controller is further configured to:
determine a power of the compressor wheel; and determine the pressure at the turbine inlet in response to the determined power of the compressor wheel.

9. The engine of claim 8 , wherein the controller is programmed with a third lookup table correlating the power of the compressor wheel to a corrected rotational speed of the rotating assembly and a corrected mass flow-rate of air through the compressor, and wherein the controller is further configured to determine the power of the compressor wheel via the third lookup table.

10. A method of controlling an internal combustion engine having a cylinder configured to receive a mixture of air and fuel for combustion therein and expel an exhaust gas following the combustion, a fuel injector configured to supply the fuel, and a turbocharger configured to receive ambient air and generate a pressurized airflow for delivery to the cylinder, wherein the turbocharger includes:
a compressor scroll;
a turbine scroll defining a turbine inlet and a turbine outlet;
a rotating assembly driven by the exhaust gas and having a turbine wheel disposed inside the turbine scroll and a compressor wheel disposed inside the compressor scroll; and
a waste-gate defining an opening configured to selectively redirect at least a portion of the exhaust gas to the turbine outlet bypassing the turbine wheel;
the method comprising:
detecting, via a first sensor, a pressure at the turbine outlet;
detecting, via a second sensor, a temperature at the turbine inlet;
determining, via a controller, an effective area of the waste-gate opening and a mass flow-rate of the exhaust gas;
determining, via the controller using a second order polynomial function, a pressure at the turbine inlet in response to the detected pressure at the turbine outlet and temperature at the turbine inlet, and the determined effective area of the waste-gate opening and mass flow-rate of the exhaust gas; and
commanding, via the controller, the fuel injector to supply an amount of fuel to the cylinder corresponding to the pressurized airflow as affected by the determined pressure at the turbine inlet.

11. The method of claim 10 , wherein the controller is programmed with a first lookup table correlating the turbine inlet pressure to the detected pressure at the turbine outlet and temperature at the turbine inlet, and the determined effective area of the waste-gate opening and mass flow-rate of the exhaust gas, the method further comprising accomplishing said determining the pressure at the turbine inlet via the first lookup table.

12. The method of claim 1 , further comprising using a factor indicative of the determined effective area of the waste-gate opening in the second order polynomial function.

13. The method of claim 12 , wherein the waste-gate includes a variable position valve configured to regulate the effective area of the waste-gate opening, and wherein the factor indicative of the determined effective area of the waste-gate opening is defined by a current position of the valve.

14. The method of claim 1 , wherein the rotating assembly is driven by the exhaust gas at a rotational speed, further comprising using a factor indicative of the rotational speed of the rotating assembly in the second order polynomial function.

15. The method of claim 14 , wherein the controller is programmed with a second lookup table correlating the rotational speed of the rotating assembly to a mass flow-rate of air through the compressor and a compressor pressure ratio, the method further comprising
determining, via the controller, a current rotational speed of the rotating assembly via the second lookup table.

16. The method of claim 10 , wherein the compressor scroll defines a compressor inlet and a compressor outlet, the met

Assignees

• Gm Global Tech Operations Llc

Inventors

• Wang Yue-Yun
• Suchy Martin
• Bernards Joerg

Classifications

• F02B37/186 Primary

  Arrangements of actuators or linkage for bypass valves · CPC title

• F02B37/22

  by varying cross-section of exhaust passages or air passages {, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits} (F02B37/24 takes precedence) · CPC title

• F05B2220/40

  in turbochargers · CPC title

• F02B37/18

  by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title

• Y02T10/144

  Cross-Sectional Technologies · mapped topic