IP Library › Granted Patent US 10,208,652
Granted Patent B2
US 10,208,652 · App. 15/374,083 · Granted Feb 19, 2019

Pre-chamber of internal combustion engine

Inventors: Thomas Maier (Ladenburg, DE); Enrico Drehobl (Reilingen, DE)
Assignee: Caterpillar Energy Solutions GmbH
F02B19/1019F02B19/12F02B19/18F02B19/108F02B19/1014F02D19/0642F02M21/0275Y02T10/125Y02T10/36
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Quick Facts
Patent No.
US 10,208,652
App. No.
15/374,083
Granted
Feb 19, 2019
Kind
B2
Abstract

A pre-chamber body for an internal combustion engine is disclosed. The pre-chamber body may have a pre-chamber. The pre-chamber body may also have a flow transfer passage, which may fluidly connect the pre-chamber and an exterior of the pre-chamber body. In addition, the pre-chamber body may have at least one backflow channel, which may fluidly connect the pre-chamber and the flow transfer passage.

Claims (33)

1. A pre-chamber body for an internal combustion engine, the pre-chamber body comprising:

a wall having a thickness extending from an internal surface of the pre-chamber body to an external surface of the pre-chamber body,

the internal surface defining a pre-chamber and a flow transfer passage within the pre-chamber body, the flow transfer passage including a venturi constriction,

the external surface defining a flow transfer outlet aperture therethrough, the pre-chamber being in fluid communication with the flow transfer outlet aperture via the flow transfer passage,

the wall defining at least one backflow channel extending from a first backflow aperture to a second backflow aperture, the first backflow aperture and the second backflow aperture each being defined by the internal surface,

the first backflow aperture being located in the pre-chamber, and the second backflow aperture being located in the venturi constriction, such that a fluid flow from the flow transfer outlet aperture toward the pre-chamber generates a pressure at the second backflow aperture that is less than a pressure at the first backflow aperture, thereby effecting a flow of fluid from the pre-chamber to the venturi constriction via the at least one backflow channel.

2. The pre-chamber body of claim 1 , wherein the at least one backflow channel comprises a plurality of backflow channels disposed in a circumferential direction about a pre-chamber longitudinal axis (A).

3. The pre-chamber body of claim 1 , wherein the flow transfer passage further includes a riser channel and a plurality of flow transfer channels, the riser channel opening in the pre-chamber, and the plurality of flow transfer channels fluidly connecting the riser channel with the external surface of the pre-chamber body.

4. The pre-chamber body of claim 3 , wherein the pre-chamber has a pre-chamber diameter, and the riser channel has a riser channel diameter, and the riser channel diameter is smaller than the pre-chamber diameter.

5. The pre-chamber body of claim 1 , wherein the flow transfer passage further includes a flow transfer channel extending from a flow transfer inlet aperture to the flow transfer outlet aperture, the flow transfer inlet aperture being defined by the internal surface, and

the flow transfer channel includes the venturi constriction.

6. The pre-chamber body of claim 5 , wherein the pre-chamber has a pre-chamber diameter, and the flow transfer channel has a flow transfer channel diameter, and the flow transfer channel diameter is smaller than the pre-chamber diameter.

7. The pre-chamber body of claim 1 , wherein the pre-chamber has a tapered section that tapers in a direction toward the flow transfer passage, and

the first backflow aperture is located along the tapered section of the pre-chamber.

8. The pre-chamber body of claim 1 , further comprising a fuel supply channel opening in the pre-chamber, the fuel supply channel being in fluid communication with the flow transfer passage via the pre-chamber.

9. The pre-chamber body of claim 1 , wherein the pre-chamber body is manufactured by a three-dimensional (3D) printing process.

10. A method for operating an internal combustion engine including a main combustion chamber and a pre-chamber, the method comprising:

flowing a mixture of main fuel and air from the main combustion chamber into the pre-chamber via a flow transfer passage fluidly connecting the pre-chamber and the main combustion chamber, the flow transfer passage including a venturi constriction;

supplying an enrichment fuel into the pre-chamber to generate an enriched mixture in the pre-chamber by mixing the mixture of main fuel and air from the main combustion chamber and the enrichment fuel;

generating a static pressure in the venturi constriction that is less than a static pressure in the pre-chamber, as a result of a venturi effect in the venturi constriction, by the flowing the mixture of main fuel and air through the venturi constriction toward the pre-chamber;

drawing a flow of the enriched mixture from the pre-chamber into the flow transfer passage via at least one backflow channel by the venturi effect in the venturi constriction, the at least one backflow channel extending from a first backflow aperture through an internal surface of the pre-chamber to a second backflow aperture through an internal surface of the venturi constriction; and

enriching a fuel concentration in the flow transfer passage by mixing the mixture of main fuel and air from the main combustion chamber and the enriched mixture from the pre-chamber drawn through the at least one backflow channel by the venturi effect.

11. An engine comprising:

a piston disposed in sliding contact with a cylinder wall, the piston and the cylinder wall at least partly defining a main combustion chamber;

a pre-chamber body including a wall having a thickness extending from an internal surface of the pre-chamber body to an external surface of the pre-chamber body,

the internal surface defining a pre-chamber and a flow transfer passage within the pre-chamber body,

the wall defining a flow transfer channel extending from a flow transfer inlet aperture to a flow transfer outlet aperture, the flow transfer inlet aperture being defined by the internal surface, the flow transfer outlet aperture being defined by the external surface, the pre-chamber being in fluid communication with the main combustion chamber via the flow transfer outlet aperture,

the wall further defining at least one backflow channel extending from a first backflow aperture to a second backflow aperture, the first backflow aperture being defined by the internal surface and being located in the pre-chamber, the second backflow aperture being located along the flow transfer channel;

an ignition device operably coupled to the pre-chamber to ignite a mixture therein; and

a fuel supply device fluidly connected to the pre-chamber to supply fuel, the fuel supply device being in fluid communication with the flow transfer passage via the pre-chamber.

12. The engine of claim 11 , wherein the at least one backflow channel comprises a plurality of backflow channels disposed in a circumferential direction about a pre-chamber longitudinal axis.

13. The engine of claim 11 , wherein the flow transfer passage further includes a riser channel and a plurality of flow transfer channels, the riser channel opening in the pre-chamber, and the plurality of flow transfer channels fluidly connecting the riser channel with the external surface of the pre-chamber body.

14. The engine of claim 13 , wherein the pre-chamber has a pre-chamber diameter, and the riser channel has a riser channel diameter, and the riser channel diameter is smaller than the pre-chamber diameter.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 9, 2016
From: MAIER, THOMAS; DREHOBL, ENRICO
To: CATERPILLAR ENERGY SOLUTIONS GMBH
Reel/Frame 040876/0060 →
Priority Claims (1)
EP 15199883 · Dec 14, 2015 · regional
Continuity (1)
Related Publication 20170167358A1 · Jun 15, 2017