Fuel bypass system for gaseous-fueled engine
US-11939906-B2 · Mar 26, 2024 · US
US10047688B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10047688-B2 |
| Application number | US-201515509697-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 10, 2015 |
| Priority date | Sep 19, 2014 |
| Publication date | Aug 14, 2018 |
| Grant date | Aug 14, 2018 |
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A method for operating a spark ignited gaseous fuel internal combustion engine is disclosed. The engine may have at least one main combustion chamber and at least one ignition device configured to initiate an ignition event within an ignition region. The method may include supplying pressurized fuel to the ignition region at times between about 30° to about 0° crank angle before the ignition event is initiated by the ignition device for enriching the ignition region with fuel. The method may also include initiating an ignition event in the ignition region for combusting an enriched air/fuel mixture within the ignition region.
Opening claim text (preview).
The invention claimed is: 1. A spark ignited gaseous fuel internal combustion engine comprising: at least one cylinder movably accommodating an associated piston, the at least one cylinder and the associated piston defining a main combustion chamber for combusting an air/fuel mixture therein; and at least one ignition system, comprising: an ignition device having an igniting portion defining an ignition region, the ignition device being configured to initiate an ignition event in the ignition region for initiating a combustion process in the main combustion chamber; and at least one fuel supply channel configured to supply pressurized fuel into the ignition region for enriching the ignition region with fuel, wherein the pressurized fuel is supplied to the ignition region at crank angles between about 30° and about 0° before the ignition event is initiated by the ignition device. 2. The spark ignited gaseous fuel internal combustion engine of claim 1 , wherein the at least one fuel supply channel at least partially extends through the ignition device. 3. The spark ignited gaseous fuel internal combustion engine of claim 1 , further comprising a pre-chamber assembly including a pre-chamber, the pre-chamber accommodating the ignition device, and the pre-chamber being configured to be fluidly connected to the main combustion chamber. 4. The spark ignited gaseous fuel internal combustion engine of claim 1 , wherein the preset pressure is greater than a maximum pressure of the air/fuel mixture within the main combustion chamber at an end of a compression stroke of the internal combustion engine. 5. The spark ignited gaseous fuel internal combustion engine of claim 1 , wherein the preset pressure ranges from about 50 bar to about 170 bar. 6. The spark ignited gaseous fuel internal combustion engine of claim 1 , wherein the ignition device is a spark plug configured to generate a spark at a spark gap, the ignition region surrounds the spark gap and extends from the spark gap to a distance ranging from about 0.1 mm to about 15 mm. 7. The spark ignited gaseous fuel internal combustion engine of claim 1 , further including at least one control valve installed in or fluidly connected upstream of the at least one fuel supply channel to control an amount of the pressurized fuel supplied to the ignition region. 8. The spark ignited gaseous fuel internal combustion engine of claim 1 , further including at least one check valve installed in or fluidly connected upstream of the at least one fuel supply channel to selectively allow or disallow a flow of fuel to and from the ignition region. 9. An ignition system for a spark ignited gaseous fuel internal combustion engine including at least one main combustion chamber, the ignition system comprising: an ignition device having an igniting portion defining an ignition region, the ignition device being configured to initiate an ignition event in the ignition region for initiating a combustion process in the at least one main combustion chamber; and at least one fuel supply channel configured to supply pressurized fuel into the ignition region for enriching the ignition region with fuel, wherein the pressurized fuel is supplied to the ignition region at times between about 30° and about 0° crank angle before the ignition event is initiated by the ignition device. 10. The ignition system of claim 9 , wherein the at least one fuel supply channel ( 146 ) at least partially extends through the ignition device. 11. The ignition system of claim 9 , further comprising a pre-chamber assembly including a pre-chamber and accommodating the ignition device, the pre-chamber being configured to be fluidly connected to the main combustion chamber. 12. The ignition system of claim 9 , wherein the at least one fuel supply channel at least partially extends through a cylinder head of the internal combustion engine. 13. The ignition system of claim 9 , wherein the pressurized fuel is supplied to the ignition region under a preset pressure greater than a maximum pressure of the air/fuel mixture within the at least one main combustion chamber at an end of a compression stroke of the internal combustion engine. 14. The ignition system of claim 9 , wherein the preset pressure ranges from about 70 bar to about 120 bar. 15. The ignition system of claim 9 , wherein the ignition device is a spark plug configured to generate a spark at a spark gap, wherein the ignition region surrounds the spark gap and extends to a distance from the spark gap ranging from about 0.1 mm to about 15 mm. 16. The ignition system of claim 9 , further comprising: at least one control valve installed in or fluidly connected upstream of the at least one fuel supply channel to control an amount of the pressurized fuel supplied to the ignition region; and at least one check valve installed in or fluidly connected upstream of the at least one fuel supply channel to selectively allow or disallow a flow of fuel to and from the ignition region. 17. A method for operating a spark ignited gaseous fuel internal combustion engine including at least one main combustion chamber and at least one ignition device configured to initiate an ignition event within an ignition region, the method comprising: supplying pressurized fuel to the ignition region at times between about 30° to about 0° crank angle before the ignition event is initiated by the ignition device for enriching the ignition region with fuel; and initiating the ignition event in the ignition region for combusting an enriched air/fuel mixture within the ignition region. 18. The method of claim 1 , wherein the pressurized fuel is supplied to the ignition region under a preset pressure greater than an actual pressure of an air/fuel mixture within the at least one main combustion chamber. 19. The method of claim 18 , wherein the preset pressure of the pressurized fuel supplied to the ignition region is in a range between about 60% to about 140% of a maximum compressing pressure of the air/fuel mixture within the main combustion chamber. 20. The method of claim 18 , wherein the preset pressure ranges from about 50 bar to about 170 bar.
with only one pre-combustion chamber (F02B19/1004 take precedence) · CPC title
Fuel pressure · CPC title
the fuel being gaseous (non-electrical control F02D19/02) · CPC title
one of the functions being ignition · CPC title
using one central computing unit · CPC title
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