Pre-chamber arrangement for a gas engine and a gas engine

Patent metadata

Field	Value
Publication number	US-11608772-B2
Application number	US-202217683205-A
Country	US
Kind code	B2
Filing date	Feb 28, 2022
Priority date	Oct 11, 2018
Publication date	Mar 21, 2023
Grant date	Mar 21, 2023

Abstract

A pre-chamber arrangement (100) for a gas engine (1), including a pre-chamber body (20) accommodating a volume (30); and a supply device (50) for supplying a gaseous medium (52) into the pre-chamber volume (30); wherein the pre-chamber body (20) has a bottom portion (22) with channels (40) for allowing gas to flow between the pre-chamber volume (30) and a main combustion chamber (10) of the gas engine (1). Each channel (40) extends along a channel axis (C) from an inner opening (42) facing the pre-chamber volume (30) to an outer opening (44) configured to face the main combustion chamber (10). The bottom portion (22) has a curved outer surface (24). The channels (40) are obliquely arranged in relation to a radius (r) of the bottom portion (22). The bottom portion has flat surfaces (46) surrounding the outer openings of the channels.

First claim

We claim:

1. A pre-chamber arrangement for a gas engine, the arrangement comprising:
a pre-chamber body accommodating a pre-chamber volume extending longitudinally along a centre axis,
the pre-chamber body comprises:
a bottom portion comprising a curved outer surface that extends into a main combustion chamber, and
channels in the bottom portion for allowing gas to flow between the pre-chamber volume and the main combustion chamber of the gas engine, each channel extends along a respective channel axis from an inner opening facing the pre-chamber volume to an outer opening of the channel configured to face the main combustion chamber,

wherein the channels are arranged such that the respective channel axis of each channel does not intersect the centre axis of the pre-chamber volume, and in that the bottom portion comprises flat surfaces surrounding the outer openings of the channels.

2. The arrangement according to claim 1 , wherein the bottom portion comprises at least six channels.

3. The arrangement according to claim 1 , wherein the channels are arranged with the respective channel axis extending at an angle in a range of 5-15 degrees in relation to a radius of the bottom portion, the radius of the bottom portion extending from where the channel axis intersects the outer opening of the channel.

4. The arrangement according to claim 1 , wherein the inner opening has an oval or elliptical shape.

5. The arrangement according to claim 1 , wherein each channel has a constant cross-sectional diameter.

6. The arrangement according to claim 1 , wherein the outer opening of each channel comprises a rounding or a chamfer.

7. The arrangement according to claim 1 , wherein each channel extends obliquely downwards from the pre-chamber volume towards the main combustion chamber.

8. A gas engine, comprising at least one cylinder, wherein the gas engine further comprises a pre-chamber arrangement according to claim 1 .

9. A pre-chamber arrangement for a gas engine, the arrangement comprising:
a pre-chamber body accommodating a pre-chamber volume extending longitudinally along a centre axis;
a supply device for supplying a gaseous medium into the pre-chamber volume; and
a valve device arranged upstream of the supply device, wherein the valve device is configured to open and close depending on a pressure inside the pre-chamber body,
wherein the pre-chamber body comprises:
a bottom portion comprising a curved outer surface that extends into a main combustion chamber, and
channels in the bottom portion for allowing gas to flow between the pre-chamber volume and the main combustion chamber of the gas engine, each channel extends along a respective channel axis from an inner opening facing the pre-chamber volume to an outer opening of the channel configured to face the main combustion chamber,

wherein the channels are arranged such that the respective channel axis of each channel does not intersect the centre axis of the pre-chamber volume, and in that the bottom portion comprises flat surfaces surrounding the outer openings of the channels.

10. The arrangement according to claim 9 , wherein the bottom portion comprises at least six channels.

11. The arrangement according to claim 9 , wherein the channels are arranged with the respective channel axis extending at an angle in a range of 5-15 degrees in relation to a radius of the bottom portion, the radius of the bottom portion extending from where the channel axis intersects the outer opening of the channel.

12. The arrangement according to claim 9 , wherein the inner opening has an oval or elliptical shape.

13. The arrangement according to claim 9 , wherein each channel has a constant cross-sectional diameter.

14. The arrangement according to claim 9 , wherein the outer opening of each channel comprises a rounding or a chamfer.

15. The arrangement according to claim 9 , wherein each channel extends obliquely downwards from the pre-chamber volume towards the main combustion chamber.

16. A gas engine, comprising at least one cylinder, wherein the gas engine further comprises a pre-chamber arrangement according to claim 9 .

17. A method for combustion in a pre-chamber arrangement of a gas engine according to claim 1 or 9 , the method comprising:
supplying gaseous medium into the pre-chamber volume by the supply device;
ensuring the gas from the main combustion chamber enters the pre-chamber volume via the channels; and
igniting a gaseous mixture of the supplied gaseous medium and the gas from the main combustion chamber.

18. The method according to claim 17 , wherein the bottom portion comprises at least six channels.

19. The method according to claim 17 , wherein the inner opening has an oval or elliptical shape.

20. The method according to claim 17 , wherein each channel extends obliquely downwards from the pre-chamber volume towards the main combustion chamber.

Assignees

• Scania Cv Ab

Inventors

• Lejon Svante
• Axelsson Pål

Classifications

• F02B43/00

  Engines characterised by operating on gaseous fuels; Plants including such engines (engines characterised by the gas-air charge being ignited by compression ignition of an additional fuel F02B7/06; engines convertible from gas to other fuel consumption F02B69/04) · CPC title

• F02B19/18 Primary

  Transfer passages between chamber and cylinder · CPC title

• F02B19/08

  the chamber being of air-swirl type · CPC title

• F02B19/1023

  pre-combustion chamber and cylinder being fed with fuel-air mixture(s) · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title