Flow guiding structure for an internal combustion engine

• US 20050011488A1
• Filed: 07/19/2004
• Published: 01/20/2005
• Est. Priority Date: 07/19/2003
• Status: Active Grant

• Current Assignee: Rejean Doucet
• Original Assignee: Rejean Doucet
• Inventors: Doucet, Rejean
• Granted Patent: US 7,128,049 B2
• Time in Patent Office: Days
• US Class Current: 123/306
• CPC Class Codes: F02M 29/06 generating whirling motion of mixture
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A flow guiding structure for guiding into a clockwise swirling flow pattern gas flowing into a gas passageway leading toward a combustion chamber of an internal combustion engine. The structure includes a tubular peripheral wall having a base section for securing the structure to the gas passageway and an integrally extending guiding section. A plurality of guiding vanes extend radially inward from the guiding section each about a corresponding vane first edge. Each guiding vane includes a vane second edge extending in a geometrical plane perpendicular to the structure longitudinal axis. Each guiding vane further includes a substantially convex vane third edge. The guiding section is provided with a plurality of guiding bents formed therein and extending radially inwardly. The guiding bents are adapted to act as an auxiliary guide and as reinforcement for the structure.

Claims

1. A flow guiding structure for guiding into a predetermined flow pattern a flow of gas flowing into a gas passageway leading towards a combustion chamber of an internal combustion engine, said gas passageway including a passageway delimiting wall and defining a passageway axis, said structure comprising:

a substantially tubular peripheral wall delimiting a structure passage, said peripheral wall defining a peripheral wall first edge, an opposed peripheral wall second edge and a passage longitudinal axis;

said peripheral wall having a base section extending from said peripheral wall first edge for allowing said structure to be secured to said gas passageway;

said peripheral wall also having a guiding section extending substantially from said base section to said peripheral wall second edge for allowing said flow of gas to be guided into said predetermined flow pattern;

a plurality of guiding vanes, each extending substantially radially inward from said guiding section about a corresponding vane first edge;

each of said vane first edges extending from a first edge proximal end located substantially adjacent said base section to a first edge distal end located substantially adjacent said peripheral wall second edge;

at least one of said guiding vanes including a vane second edge extending in a second edge geometrical plane substantially perpendicular to said structure longitudinal axis from said first edge distal end to a second edge distal end;

said at least one of said guiding vanes also including a vane third edge extending from said second edge distal end to said first edge proximal end.

2. A structure as recited in claim 1, wherein the length of said vane second edge is approximately between ¼

and ¾

that of said vane first edge.

3. A structure as recited in claim 1, wherein the length of said vane second edge is approximately {fraction (1/3)} that of said vane first edge.

4. A structure as recited in claim 1, wherein said vane third edge has a substantially convex configuration.

5. A structure as recited in claim 4, wherein said vane third edge includes a substantially rectilinear third edge first segment extending from said second edge distal end.

6. A structure as recited in claim 5, wherein said third edge first segment extends at an angle relative to said vane second edge generally radially inward and away from said second edge geometrical plane.

7. A structure as recited in claim 6, wherein said third edge first segment and said vane second edge form a first segment-to-second edge angle therebetween, said first segment-to-second edge angle being obtuse.

8. A structure as recited in claim 7, wherein said first segment-to-second edge angle has a value of approximately 135 degrees.

9. A structure as recited in claim 5, wherein the length of said third edge first segment is approximately 2.5 times that of said vane second edge.

10. A structure as recited in claim 5, wherein said vane third edge also includes a substantially arcuate third edge second segment extending from said third edge first segment to said first edge proximal end.

11. A structure as recited in claim 1, wherein each of said vanes is oriented in a vane plane extending radially inward, slanted at a vane-to-axis angle relative to said structure longitudinal axis, said vane-to-axis angle being selected from a range of between 25 and 75 degrees.

12. A structure as recited in claim 1, wherein said guiding section is also provided with an auxiliary guiding means for further guiding said flow of gas into said predetermined flow pattern, said auxiliary guiding means also acting as a reinforcement means for structurally reinforcing said structure.

13. A structure as recited in claim 1, wherein said guiding section includes at least one guiding bent formed therein.

14. A structure as recited in claim 13, wherein said at least one guiding bent extends along a bent line substantially parallel to a corresponding vane first edge.

15. A structure as recited in claim 1, wherein said guiding section includes a plurality of radial apertures formed therein, each of said radial apertures being in fluid communication with a corresponding guiding vane for allowing radially flowing gas to penetrate through said radial apertures into said structure passage and to be guided by said guiding vane into said predetermined flow pattern.

16. A structure as recited in claim 15, wherein said radial apertures are formed by substantially V-shaped notches extending substantially from said peripheral wall second edge to said base section;

wherein said guiding section includes substantially triangular guiding section segments separated from each other by said substantially V-shaped notches;

each of said substantially triangular guiding section segments including a segment base and a substantially opposed segment apex located respectively substantially adjacent the interface between said base and guiding sections and said peripheral wall second edge;

said vane first edge extending from said segment apex to said segment base;

each of said substantially triangular guiding section segment also including a segment auxiliary edge also extending from said segment apex to said segment base in a substantially divergent relationship relative to said vane first edge;

at least one of said guiding section segments being provided with a guiding bents formed therein, said at least one guiding bent being configured, sized and positioned so as to act as an auxiliary guide for guiding said flow of gas into said predetermined flow pattern.

17. A structure as recited in claim 16, wherein said at least one guiding bent extends substantially inwardly into said structure passage, said at least one guiding bent extending in a direction substantially parallel to said vane first edge from a position substantially midway along said segment auxiliary edge to a position substantially midway along said segment base.

18. A flow guiding structure for guiding into a predetermined flow pattern a flow of gas flowing into a gas passageway leading towards a combustion chamber of an internal combustion engine, said gas passageway including a passageway delimiting wall and defining a passageway axis, said structure comprising:

a plurality of guiding vanes, each extending substantially radially inward from said guiding section about a corresponding vane first edge;

each of said vane first edges extending from a first edge proximal end located substantially adjacent said base section to a first edge distal end located substantially adjacent said peripheral wall second edge;

each of said guiding vanes including a vane second edge extending in a second edge geometrical plane substantially perpendicular to said structure longitudinal axis from said first edge distal end to a second edge distal end;

each of said guiding vanes also including a vane third edge extending from said second edge distal end to said first edge proximal end.

19. A flow guiding structure for guiding into a predetermined flow pattern a flow of gas flowing into a gas passageway leading towards a combustion chamber of an internal combustion engine, said gas passageway including a passageway delimiting wall and defining a passageway axis, said structure comprising:

a substantially tubular peripheral wall delimiting a structure passage, said peripheral wall defining a peripheral wall first edge, an opposed peripheral wall second edge and a passage longitudinal axis;

said peripheral wall having a base section extending from said peripheral wall first edge for allowing said structure to be secured to said gas passageway;

said peripheral wall also having a guiding section extending substantially from said base section to said peripheral wall second edge for allowing said flow of gas to be guided into said predetermined flow pattern;

a plurality of guiding vanes, each extending radially inward from said guiding section, said guiding vanes being configured, sized and positioned so as to guide said flow of gas into said predetermined flow pattern;

said guiding section being provided with at least one guiding bent formed therein and extending substantially inward into said structure passage, said at least one guiding bent being configured, positioned and sized so as to act as an auxiliary guide and cooperate with said guiding vanes for guiding said flow of gas into said predetermined flow pattern.

20. A structure as recited in claim 19, wherein said at least one guiding bent is configured, positioned and sized so as to bias said flow of gas substantially radially outward towards said peripheral wall.

21. A flow guiding structure for guiding into a predetermined flow pattern a flow of gas flowing into a gas passageway leading towards a combustion chamber of an internal combustion engine, said gas passageway including a passageway delimiting wall and defining a passageway axis, said structure comprising:

a substantially tubular peripheral wall delimiting a structure passage, said peripheral wall defining a peripheral wall first edge, an opposed peripheral wall second edge and a passage longitudinal axis;

said peripheral wall having a base section extending from said peripheral wall first edge for allowing said structure to be secured to said gas passageway;

said peripheral wall also having a guiding section extending substantially from said base section to said peripheral wall second edge for allowing said flow of gas to be guided into said predetermined flow pattern;

a plurality of guiding vanes, each extending substantially radially inward from said guiding section, said guiding vane being configured, sized and positioned so as to guide said flow of gas into a substantially clockwise swirling flow pattern.

22. A structure as recited in claim 21, wherein said flow structure guides said flow of gas into a substantially radially outwardly directed clockwise swirling flow pattern.