초록 ▼

A method for a multi-fuel vehicle includes: determining a first target amount of fuel to be injected for a combustion event of a combustion chamber of an engine; determining first and second fractions for the combustion event based on at least one of engine speed, engine load, and engine temperature

A method for a multi-fuel vehicle includes: determining a first target amount of fuel to be injected for a combustion event of a combustion chamber of an engine; determining first and second fractions for the combustion event based on at least one of engine speed, engine load, and engine temperature; determining a second target amount of liquid fuel for the combustion event based on the first target amount and the first fraction; determining a third target amount of gaseous fuel for the combustion event based on the first target amount and the second fraction; selectively injecting a liquid fuel directly into the combustion chamber for the combustion event based on the second target amount and using a first fuel injector; and selectively injecting a gaseous fuel into a port of the combustion chamber for the combustion event based on the third target amount and using a second fuel injector.

대표청구항 ▼

1. A system for a multi-fuel vehicle, comprising: a target fueling module that determines a first target amount of fuel to be injected for a combustion event of a combustion chamber of an engine;a first and second fraction modules that determine first and second fractions for the combustion event ba

1. A system for a multi-fuel vehicle, comprising: a target fueling module that determines a first target amount of fuel to be injected for a combustion event of a combustion chamber of an engine;a first and second fraction modules that determine first and second fractions for the combustion event based on an engine temperature,wherein the second fraction module determines the second fraction using interpolation based on the engine temperature relative to a predetermined minimum value of the engine temperature and a predetermined maximum value of the engine temperature, andwherein the first fraction module determines the first fraction as a function of the second fraction;a liquid fueling determination module that sets a second target amount of liquid fuel for the combustion event based on a first product of the first target amount and the first fraction;a gaseous fueling determination module that sets a third target amount of gaseous fuel for the combustion event based on a second product of the first target amount and the second fraction;a liquid injection control module that selectively injects a liquid fuel directly into the combustion chamber for the combustion event based on the second target amount and using a first fuel injector; anda gaseous injection control module that selectively injects a gaseous fuel into a port of the combustion chamber for the combustion event based on the third target amount and using a second fuel injector. 2. The system of claim 1 wherein the first and second fraction modules determine the first and second fractions for the combustion event further based on an engine speed and an engine load. 3. The system of claim 1 wherein: the second fraction module increases the second fraction as the engine temperature decreases; andthe first fraction module decreases the first fraction as the engine temperature decreases. 4. The system of claim 1 further comprising an engine temperature determination module that determines the engine temperature as a function of a coolant temperature measured using a coolant temperature sensor. 5. The system of claim 1 wherein the engine temperature is a coolant temperature measured using a coolant temperature sensor. 6. The system of claim 1 wherein the liquid fuel is one of gasoline and diesel fuel. 7. The system of claim 6 wherein the gaseous fuel is one of compressed natural gas and liquefied petroleum gas. 8. The system of claim 1 wherein: the first and second fractions are values between 0.0 and 1.0, inclusive; andthe first fraction module sets the first fraction equal to 1.0 minus the second fraction. 9. A method for a multi-fuel vehicle, comprising: determining a first target amount of fuel to be injected for a combustion event of a combustion chamber of an engine;determining first and second fractions for the combustion event based on an engine temperature,wherein determining the second fraction includes determining the second fraction using interpolation based on the engine temperature relative to a predetermined minimum value of the engine temperature and a predetermined maximum value of the engine temperature, andwherein determining the first fraction includes determining the first fraction as a function of the second fraction;setting a second target amount of liquid fuel for the combustion event based on a first product of the first target amount and the first fraction;setting a third target amount of gaseous fuel for the combustion event based on to a second product of the first target amount and the second fraction;selectively injecting a liquid fuel directly into the combustion chamber for the combustion event based on the second target amount and using a first fuel injector; andselectively injecting a gaseous fuel into a port of the combustion chamber for the combustion event based on the third target amount and using a second fuel injector. 10. The method of claim 9 further comprising determining the first and second fractions for the combustion event further based on an engine speed and an engine load. 11. The method of claim 9 further comprising: increasing the second fraction as the engine temperature decreases; anddecreasing the first fraction as the engine temperature decreases. 12. The method of claim 9 further comprising determining the engine temperature as a function of a coolant temperature measured using a coolant temperature sensor. 13. The method of claim 9 wherein the engine temperature is a coolant temperature measured using a coolant temperature sensor. 14. The method of claim 9 wherein the liquid fuel is one of gasoline and diesel fuel. 15. The method of claim 14 wherein the gaseous fuel is one of compressed natural gas and liquefied petroleum gas. 16. The method of claim 9 further comprising setting the first fraction equal to 1.0 minus the second fraction, wherein the first and second fractions are values between 0.0 and 1.0, inclusive.