Position based air/fuel ratio calculation in an internal combustion engine
View Patent ↗Some embodiments relate to an internal combustion engine that includes a combustion chamber and a rotating component. The internal combustion engine further includes a sensing system that detects an angular position of the rotating component. A controller calculates a ratio between air and fuel in the combustion chamber based on the detected position of the rotating component. As an example, the rotating component may be a crankshaft where the controller calculates a speed of the crankshaft and an acceleration of the crankshaft based on the detected position of the crankshaft.
1. An internal combustion engine comprising:
a combustion chamber that includes air and fuel;
a rotating component;
a sensing system that detects an angular position of the rotating component; and
a controller that determines a burn rate of the air and the fuel in the combustion chamber based on the angular position of the rotating component and calculates a ratio between air and fuel in the combustion chamber based on the burn rate.
2. The internal combustion engine of claim 1 , wherein the rotating component is a crankshaft.
3. The internal combustion engine of claim 1 , wherein the controller calculates a speed of the rotating component and an acceleration of the rotating component based on the detected position of the rotating component.
4. The internal combustion engine of claim 1 , wherein the engine operates in a lean burn condition.
5. The internal combustion engine of claim 1 , wherein the controller calculates the ratio between the air and the fuel within the combustion chamber based on changes in the burn rate when the controller initiates specific changes in a quantity of the fuel provided to the combustion chamber.
6. The internal combustion engine of claim 1 , wherein the controller adjusts a quantity of the fuel provided to the combustion chamber based on the ratio between the air and the fuel in the combustion chamber.
7. The internal combustion engine of claim 6 , further comprising a plurality of combustion chambers, wherein the controller calculates the ratio between the air and the fuel in each of the plurality of combustion chambers and individually adjusts a quantity of the fuel provided to each combustion chamber.
8. The internal combustion engine of claim 1 , further comprising a gear that includes teeth, the gear attached to the rotating component; and
wherein the gear has teeth omitted to provide a position reference to the controller,
wherein the sensing system detects a position of the rotating component by detecting the teeth on the gear.
9. The internal combustion engine of claim 1 , wherein the controller calculates the ratio between the air and the fuel within the combustion chamber based on the position of the rotating component and a pressure of the air entering the combustion chamber.
10. The internal combustion engine of claim 1 , wherein the controller calculates the ratio between air and fuel within the combustion chamber based on the position of the rotating component and a time of initiation of combustion of the air and fuel within the combustion chamber.
11. The internal combustion engine of claim 1 , wherein the fuel comprises diesel fuel.
12. The internal combustion engine of claim 1 , wherein the fuel comprises gasoline.
13. A method comprising:
receiving data indicating a volume of a combustion chamber;
determining a burn rate based on the volume of the combustion chamber and an amount of heat released from the combustion chamber; and
calculating, with a processor, a ratio between air and fuel in the combustion chamber based on the volume of the combustion chamber and the burn rate.
14. The method of claim 13 , wherein receiving data indicating the volume of the combustion chamber comprises sensing an angular position of a crankshaft that moves a piston, the piston partially defining the volume of the combustion chamber.
15. The method of claim 13 , further comprising calculating a temperature of the air and the fuel in the combustion chamber; and
adjusting the fuel supplied to the combustion chamber to control the temperature of the air and fuel in the combustion chamber.
16. The method of claim 13 , further comprising adjusting the fuel supplied to the combustion chamber to control the ratio between the air and the fuel in the combustion chamber.
17. The method of claim 13 , further comprising calculating a pressure of the air and the fuel in the combustion chamber; and
adjusting the fuel supplied to the combustion chamber to control the pressure of the air and the fuel in the combustion chamber.
18. A method comprising:
calculating momentary expansion acceleration of an air and fuel mixture in a combustion chamber;
estimating a burn rate based on an amount of heat released from the air and fuel mixture in the combustion chamber based on the momentary expansion acceleration of the air and fuel mixture; and
calculating a ratio between air and fuel in the combustion chamber based on the burn rate.