Method for operating an internal combustion engine system using hydrogen fuel

Patent metadata

Field	Value
Publication number	US-12188422-B2
Application number	US-202418584268-A
Country	US
Kind code	B2
Filing date	Feb 22, 2024
Priority date	Mar 3, 2023
Publication date	Jan 7, 2025
Grant date	Jan 7, 2025

Abstract

A method for operating an internal combustion engine system using gaseous fuel is disclosed. The method includes injecting, by activating a fuel injector to generate a first injection in association with a compression stroke, a first amount of gaseous fuel into a pre-combustion chamber, wherein the first injection and the first amount of gaseous fuel are adapted so that an ignitable fuel-air mix is formed in the pre-combustion chamber but not in a main combustion chamber; igniting, by activating an igniter, the ignitable fuel-air mix in the pre-combustion chamber formed by the first injection; and injecting, by activating the fuel injector to generate a second injection after ignition of the first amount of fuel, a second amount of gaseous fuel into the pre-combustion chamber, wherein the second injection and the second amount of gaseous fuel are adapted so that fuel is forced through the orifices into the main combustion chamber.

First claim

What is claimed is:

1. A method for operating an internal combustion engine system using gaseous fuel, wherein the internal combustion engine system comprises:
a piston arranged to reciprocate in a cylinder between a bottom dead center (BDC) and a top dead center (TDC), wherein a position of the piston during a compression stroke when the piston moves towards the TDC can be represented by −180° crank angle degrees (CAD) at the BDC and 00 CAD at the TDC;
a main combustion chamber arranged at an end portion of the cylinder so that an upper surface of the piston defines a lower side of the main combustion chamber;
an inlet valve and an exhaust valve arranged to regulate flow of air and exhaust gas to and from the main combustion chamber;
a pre-combustion chamber arranged in association with the main combustion chamber, wherein the pre-combustion chamber is provided with one or more orifices allowing fluid communication between the pre-combustion chamber and the main combustion chamber;
a fuel injector arranged to inject gaseous fuel into the pre-combustion chamber; and
an igniter arranged to ignite a fuel-air mix present in the pre-combustion chamber, the method comprising:
injecting, by activating the fuel injector to generate a first injection in association with a compression stroke, a first amount of gaseous fuel into the pre-combustion chamber, wherein the first injection and the first amount of gaseous fuel are adapted so that an ignitable fuel-air mix is formed in the pre-combustion chamber but not in the main combustion chamber,
igniting, by activating the igniter, the ignitable fuel-air mix in the pre-combustion chamber formed by the first injection,
injecting, by activating the fuel injector to generate a second injection after ignition of the first amount of gaseous fuel, a second amount of gaseous fuel into the pre-combustion chamber, wherein the second injection and the second amount of gaseous fuel ( 3 A) are adapted so that fuel is forced through the orifices into the main combustion chamber.

2. The method of claim 1 , wherein the second amount of gaseous fuel is larger than the first amount of gaseous fuel.

3. The method of claim 2 , wherein the second amount of gaseous fuel is at least 50% larger, or at least 100% larger, or at least 500% larger, than the first amount of gaseous fuel.

4. The method of claim 1 , wherein a duration of the first injection is less than 5° CAD.

5. The method of claim 4 , wherein the duration of the first injection is 0.5-2° CAD.

6. The method of claim 1 , wherein a duration of the second injection ( 3 ) is >0.5° CAD, or >1° CAD.

7. The method of claim 6 , wherein the duration of the second injection is <20° CAD, or <15° CAD.

8. The method of claim 1 , wherein the first injection is initiated somewhere between −160° and −10° CAD.

9. The method of claim 1 , wherein the first injection is initiated somewhere between −160° and −45° CAD.

10. The method of claim 9 , wherein the first injection is initiated after −110° CAD.

11. The method of claim 9 , wherein the first injection is initiated before −10° CAD, or before −45° CAD.

12. The method of claim 1 , wherein the ignition is initiated somewhere between −45° and +10° CAD, or between −20° and −10° CAD.

13. The method of claim 1 , wherein the second injection is initiated somewhere between −10° and +10° CAD.

14. The method of claim 13 , wherein the second injection is initiated at or after −5° CAD.

15. The method of claim 13 , wherein the first injection is initiated at or before 0° CAD.

16. The method of claim 1 , wherein the gaseous fuel is hydrogen gas.

17. An internal combustion engine system comprising:
a piston arranged to reciprocate in a cylinder between a bottom dead center (BDC) and a top dead center (TDC), wherein a position of the piston during a compression stroke when the piston moves towards the TDC can be represented by −180° crank angel degrees (CAD) at the BDC and 0° CAD at the TDC;
a main combustion chamber arranged at an end portion of the cylinder so that an upper surface of the piston defines a lower side of the main combustion chamber;
an inlet valve and an exhaust valve arranged to regulate flow of air and exhaust gas to and from the main combustion chamber;
a pre-combustion chamber arranged in association with the main combustion chamber, wherein the pre-combustion chamber is provided with one or more orifices allowing fluid communication between the pre-combustion chamber and the main combustion chamber;
a fuel injector arranged to inject gaseous fuel into the pre-combustion chamber; and
an igniter arranged to ignite a fuel-air mix present in the pre-combustion chamber, and
wherein the fuel injector is adapted to generate a first injection in association with a compression stroke, and to inject a first amount of gaseous fuel into the pre-combustion chamber, wherein the first injection and the first amount of gaseous fuel are adapted so that an ignitable fuel-air mix is formed in the pre-combustion chamber but not in the main combustion chamber,
wherein the igniter is adapted to ignite the ignitable fuel-air mix in the pre-combustion chamber formed by the first injection, and
wherein the fuel injector is adapted to generate a second injection after ignition of the first amount of gaseous fuel, and to inject a second amount of gaseous fuel into the pre-combustion chamber, wherein the second injection and the second amount of gaseous fuel are adapted so that fuel is forced through the orifices into the main combustion chamber.

18. A vehicle provided with an internal combustion engine system according to claim 17 .

Assignees

• Volvo Truck Corp

Inventors

• Persson Håkan
• Rohrssen Karsten

Classifications

• F02M45/02

  with each cyclic delivery being separated into two or more parts · CPC title

• F02D41/38

  of the high pressure type · CPC title

• F02M21/0206

  Non-hydrocarbon fuels, e.g. hydrogen, ammonia or carbon monoxide · CPC title

• F02B19/12

  with positive ignition (engines with non-timed positive ignition, and with incandescent chambers F02B9/08) · CPC title

• F02D41/402

  Multiple injections · CPC title