GASEOUS FUEL MIXER FOR INTERNAL COMBUSTION ENGINE

• US 20140053815A1
• Filed: 08/27/2012
• Published: 02/27/2014
• Est. Priority Date: 08/27/2012
• Status: Active Grant

• Current Assignee: Cummins Intellectual Property, Inc. (Cummins Incorporated)
• Original Assignee: Cummins Intellectual Property, Inc. (Cummins Incorporated)
• Inventors: SPERRY, Robert G.
• Granted Patent: US 8,950,383 B2
• Time in Patent Office: Days
• US Class Current: 123/527
• CPC Class Codes: F02M 21/042 Mixer comprising a plurality of bores or flow passages
• CPC Class Codes: Y02T 10/30 Use of alternative fuels, e.g. biofuels

Abstract

A gaseous fuel mixer for an internal combustion engine includes a frustoconical cone and an outlet element extending from the frustoconical cone at an interior portion of the frustoconical cone. The outlet element and the frustoconical cone are located within a mixer passage of an intake system. The mixer passage has an internal diameter. The outlet element includes a plurality of transverse openings that connect a fuel passage formed within the outlet element to the interior portion of the frustoconical cone. The height and diameter of the frustoconical cone and the internal diameter of the passage form specific ratios that provide for uniform mixing of intake air and gaseous fuel prior to the mixture flowing into an intake manifold of the engine.

Claims

1. An internal combustion engine, comprising:

an intake circuit including a mixer passage having a mixer passage axis and a gaseous fuel mixer positioned within the mixer passage and extending along the mixer passage axis, the gaseous fuel mixer including a frustoconical cone and an outlet element;

the frustoconical cone including a first end, an open second end having a diameter D and positioned downstream from the first end, an interior portion, and a height H, the outlet element being positioned in the interior portion and including a fuel passage and a plurality of transverse openings connecting the fuel passage to the interior portion, the plurality of transverse openings positioned in the interior portion to direct gaseous fuel into the interior portion; and

a gaseous fuel system connected to the intake circuit.

2. The internal combustion engine of claim 1, further including a connection portion and an outer portion, wherein the mixer passage is formed within the outer portion, the outer portion includes a port, the gaseous fuel system is connected to the port, and the connection portion connects the port to the outlet element.

3. The internal combustion engine of claim 2, wherein an annular gap is formed between the frustoconical cone second end and the outer portion.

4. The internal combustion engine of claim 1, wherein a ratio of D/H is in the range 1.00 to 1.67.

5. The internal combustion engine of claim 1, wherein a ratio of D/H is in the range 1.29 to 1.39.

6. The internal combustion engine of claim 1, wherein the frustoconical cone has a concave shape.

7. The internal combustion engine of claim 1, wherein the frustoconical cone has a convex shape.

8. The internal combustion engine of claim 1, wherein the outlet portion includes a distal end and the distal end is offset from the frustoconical cone second end toward the frustoconical cone first end.

9. The internal combustion engine of claim 1, wherein the mixer passage has an internal diameter ID and a ratio of ID/D is in the range 1.07 to 1.45.

10. The internal combustion engine of claim 1, wherein the mixer passage has an internal diameter ID and a ratio of ID/D is in the range 1.23 to 1.33.

11. The internal combustion engine of claim 1, the gaseous fuel mixer further including a gas spreader plate extending radially outward from the outlet element toward the frustoconical cone at the frustoconical cone second end.

12. The internal combustion engine of claim 11, wherein a cone annular gap is formed between the gas spreader plate and the frustoconical cone.

13. The internal combustion engine of claim 12, wherein the cone annular gap is in the range 1.0 to 4.5 millimeters.

15. The internal combustion engine of claim 11, further including a connection portion and an outer portion, wherein the mixer passage is formed within the outer portion, the outer portion includes a port, the gaseous fuel system is connected to the port, and the connection portion connects the port to the outlet element.

14. An internal combustion engine, comprising:

an intake circuit including a mixer passage having a mixer passage axis and a gaseous fuel mixer positioned within the mixer passage and extending along the mixer passage axis, the mixer passage having an internal diameter ID, the gaseous fuel mixer including a frustoconical cone and an outlet element;

the frustoconical cone including a first end, an open second end having a diameter D and positioned downstream from the first end, an interior portion, a height H, and a cone axis coaxial with the mixer passage, the outlet element being positioned in the interior portion and including a fuel passage and a plurality of transverse openings connecting the fuel passage to the interior portion, the outlet element and the first end of the frustoconical cone attached or formed to prevent air flow from flowing into the interior portion from the mixer passage upstream from the frustoconical cone; and

a gaseous fuel system connected to the intake circuit.

16. The internal combustion engine of claim 14, wherein a ratio of ID/D is in the range 1.07 to 1.45.

17. The internal combustion engine of claim 14, wherein a ratio of ID/D is in the range 1.23 to 1.33.

18. The internal combustion engine of claim 14, wherein a ratio of D/H is in the range 1.00 to 1.67.

19. The internal combustion engine of claim 14, wherein a ratio of D/H is in the range 1.29 to 1.39.

20. The internal combustion engine of claim 14, wherein the frustoconical cone has a concave shape.

21. The internal combustion engine of claim 14, wherein the frustoconical cone has a convex shape.

22. The internal combustion engine of claim 14, the gaseous fuel mixer further including a gas spreader plate extending radially outward from the outlet element toward the frustoconical cone at the frustoconical cone second end.

23. The internal combustion engine of claim 22, wherein a cone annular gap is formed between the gas spreader plate and the frustoconical cone.

24. The internal combustion engine of claim 23, wherein the cone annular gap is in the range 1.0 to 4.5 millimeters.