Method for controlling ignition in internal combustion engine and pre-chamber assembly thereof
US-2018003132-A1 · Jan 4, 2018 · US
US11674464B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11674464-B2 |
| Application number | US-202117443941-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 28, 2021 |
| Priority date | Jul 28, 2021 |
| Publication date | Jun 13, 2023 |
| Grant date | Jun 13, 2023 |
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Methods and systems are provided for injecting gaseous fuel during an engine start. In one example, a method comprises generating gaseous fuel via a fuel gasification device and injecting the gaseous fuel via a fuel injector. The fuel injector is configured to inject adjacent to an ignition device.
Opening claim text (preview).
The invention claimed is: 1. A method, comprising: operating a reformer to generate a gaseous fuel; and injecting the gaseous fuel through an injector directly adjacent to an ignition device arranged in a prechamber of a combustion chamber having a piston, the combustion chamber fluidly coupled to the prechamber, the injector positioned at a central axis along which the piston oscillates in the combustion chamber and the injector injecting the gaseous fuel directly into the prechamber in a direction parallel to the central axis, wherein the injector is a low-pressure injector; and injecting the gaseous fuel through a high-pressure injector, wherein the high-pressure injector injects distally to the ignition device with a cylinder positioned between the high-pressure injector and the injector, the high-pressure injector being more outboard from the central axis than a cylinder valve. 2. The method of claim 1 , further comprising injecting the gaseous fuel within a threshold crank angle of top-dead center of a compression stroke, the high-pressure injector positioned to inject directly to the combustion chamber at an angle between 0 and 180 degrees. 3. The method of claim 1 , further comprising injecting the gaseous fuel directly into a volume of the prechamber separate from a volume of a combustion chamber to which the prechamber is coupled. 4. The method of claim 1 , wherein the high-pressure injector provides first and second compression stroke injection to inject the gaseous fuel, and the injector provides a top-dead-center injection to inject the gaseous fuel, followed by an ignition event by the ignition device during an expansion stroke to ignite the injected gaseous fuel. 5. The method of claim 1 , wherein operating the reformer occurs in response to a cold-start. 6. The method of claim 1 , wherein operating the reformer occurs in response to an engine start request signaled by one or more of an ignition key being turned, an ignition button being depressed, and a vehicle door being opened. 7. The method of claim 1 , further comprising flowing the gaseous fuel from the reformer to a reservoir, wherein the reservoir is fluidly coupled to the injector. 8. A system, comprising: an engine; a gaseous fuel reservoir fluidly coupled to a first fuel injector and a second fuel injector, the first fuel injector positioned to inject adjacent to an intake valve of a combustion chamber and the second fuel injector positioned to inject into a prechamber adjacent to an ignition device, the second fuel injector positioned at a central axis along which a piston oscillates in the combustion chamber and the first fuel injector injecting gaseous fuel directly into the prechamber, the first fuel injector positioned outboard of the intake valve relative to the central axis; and a controller with computer-readable instructions stored on non-transitory memory thereof that when executed cause the controller to: generate the gaseous fuel in response to a cold-start of the engine and a pressure of the gaseous fuel reservoir being less than a threshold pressure; flow the gaseous fuel to the first fuel injector and the second fuel injector; and execute first and second injections of a combustion cycle via the first fuel injector before top-dead center and further execute a final injection of the combustion cycle via the second fuel injector at the top-dead center of a compression stroke. 9. The system of claim 8 , wherein the instructions further cause the controller to flow fuel to a fuel reformer device via a fuel pump coupled to a fuel tank, wherein the fuel reformer device is configured to gasify the fuel. 10. The system of claim 8 , wherein the instructions further cause the controller to flow fuel to a fuel evaporation chamber via a fuel pump coupled to a fuel tank, wherein fuel is injected into the fuel evaporation chamber via a third fuel injector. 11. The system of claim 8 , wherein the instructions further cause the controller to activate the ignition device after the top-dead center of the compression stroke. 12. The system of claim 8 , wherein the first fuel injector is a high pressure injector and the second fuel injector is a low pressure injector. 13. The system of claim 8 , wherein an interior volume of the prechamber is separated from a combustion chamber volume via prechamber walls. 14. The system of claim 8 , wherein the instructions further cause the controller to determine an engine start is requested in response to a vehicle door being opened. 15. The system of claim 8 , wherein the first fuel injector injects at an angle between 0 and 180 degrees and the second fuel injector injects at an angle parallel to the central axis. 16. An engine system, comprising: a fuel system comprising a fuel tank, a pump, a fuel gasification device, and a reservoir; a first fuel injector and a second fuel injector fluidly coupled to the reservoir, wherein the first fuel injector is positioned to inject at an angle relative to a central axis of a combustion chamber and the second fuel injector is positioned to inject parallel to the central axis of the combustion chamber; and a controller with computer-readable instructions stored on non-transitory memory thereof that when executed cause the controller to: flow fuel to the fuel gasification device in response to a pressure of the reservoir being less than a threshold pressure and an engine start being requested; inject a final fuel injection via the second fuel injector following one or more injections via the first and second fuel injectors; and provide a spark via an ignition device during or after the final fuel injection. 17. The engine system of claim 16 , wherein the engine start further comprises where the engine start is a cold-start, the second fuel injector positioned at the central axis along which a piston oscillates in the combustion chamber and the first fuel injector injecting gaseous fuel directly into a prechamber, the first fuel injector positioned outboard of an intake valve relative to the central axis, the instructions further including instructions to execute first and second injections of a combustion cycle via the first fuel injector before top-dead center and further execute the final injection of the combustion cycle via the second fuel injector. 18. The engine system of claim 16 , wherein the second fuel injector and the ignition device are arranged in a prechamber, wherein a volume of the prechamber is separated from a volume of the combustion chamber via prechamber walls. 19. The engine system of claim 16 , wherein a piston of the combustion chamber is configured to oscillate in a direction parallel to the central axis. 20. The engine system of claim 16 , wherein the fuel gasification device comprises a third fuel injector configured to inject directly therein.
Feeding by means of driven pumps · CPC title
at least one fuel being gaseous, the other fuels being gaseous or liquid at standard conditions · CPC title
at cold start (F02D41/067 takes precedence) · CPC title
Improving ICE efficiencies · CPC title
Tanks, e.g. multiple tanks · CPC title
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