Claims
- 1. An air flow twisting device for an internal combustion engine for providing air for combustion to a combustion chamber of an engine, the device comprising:
a tubular body having a length and an inner surface; and a groove on the inner surface and twisting along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein the groove spans only an arcuate portion of the body and begins at an end of the body and extends along a length of about two-thirds the length of the body.
- 2. The air flow twisting device of claim 1, comprising a plurality of grooves on the inner surface and twisting along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein each groove spans only an arcuate portion of the body and begins at an end of the body and extends along a length of about two-thirds the length of the body.
- 3. An air inlet system for an internal combustion engine comprising:
a manifold coupled to an air source for providing air from the air source; and an air flow twisting device comprising,
a tubular body having a length and an inner surface, wherein the body is coupled at a first end to the manifold and at a second end to the engine combustion chamber, and a groove on the inner surface and twisting along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein the groove spans only an arcuate portion of the body and begins at an end of the body and extends along a length of about two-thirds the length of the body.
- 4. The air inlet system of claim 3, further comprising an air filter coupled to the air source for filtering the air provided to the manifold.
- 5. The air inlet system of claim 3, wherein the manifold is a rubber boot.
- 6. The air inlet system of claim 3, comprising a plurality of grooves on the inner surface and twisting along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein each groove spans only an arcuate portion of the body and begins at an end of the body and extends along a length of about two-thirds the length of the body.
- 7. The air inlet system of claim 6, wherein the plurality of grooves are spaced apart.
- 8. The air inlet system of claim 3, wherein the second end of the body is coupled to an air intake manifold for providing twisted air flow to the air intake manifold.
- 9. The air inlet system of claim 3, wherein the second end of the body is coupled to a carburetor for providing twisted air flow to the carburetor.
- 10. The air inlet system of claim 3, wherein the second end of the body is coupled to a mixing chamber for providing twisted air flow to the mixing chamber.
- 11. An air flow twisting device for an internal combustion engine for providing air for combustion to a combustion chamber of an engine, the device comprising:
a tubular body having a length and an inner surface; and a groove on the inner surface that twists along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein the groove spans only an arcuate portion of the inner surface, and wherein the groove comprises a first side, a second side and a base, wherein a concave surface defines the first side and the base, a convex surface defines the second side and a junction between the concave and convex surfaces is a point.
- 12. The air flow twisting device of claim 11, wherein the concave surface is longer than the convex surface.
- 13. The air flow twisting device of claim 11, wherein the groove begins at an end of the body and extends along a length of about two-thirds the length of the body.
- 14. The air flow twisting device of claim 11, comprising a plurality of grooves on the inner surface that each twist along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein each groove spans only an arcuate portion of the inner surface, and wherein each groove comprises a first side, a second side and a base, wherein a concave surface defines the first side and the base of each groove, a convex surface defines the second side of each groove and a junction between the concave and convex surfaces of each groove is a point.
- 15. The air flow twisting device of claim 14, wherein the concave surface of each groove is longer than the convex surface of each groove.
- 16. The air flow twisting device of claim 14, wherein each groove begins at an end of the body and extends along a length of about two-thirds the length of the body.
- 17. The air flow twisting device of claim 14, comprising four grooves.
- 18. The air flow twisting device of claim 14, wherein the inner surface has diagonal symmetry about any plane that extends through the longitudinal axis of the body.
- 19. An air flow twisting device for an internal combustion engine for providing air for combustion to a combustion chamber of an engine, the device comprising:
a tubular body having a length and an inner surface; and a groove on the inner surface that twists along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein the groove spans only an arcuate portion of the inner surface, and wherein the inner surface has diagonal symmetry about any plane that extends through the longitudinal axis of the body.
- 20. The air flow twisting device of claim 19, wherein the groove comprises a first side, a second side and a base, wherein a concave surface defines the first side and the base, a convex surface defines the second side and a junction between the concave and convex surfaces is a point.
- 21. The air flow twisting device of claim 19, wherein the groove begins at an end of the body and extends along a length of about two-thirds the length of the body.
- 22. The air flow twisting device of claim 19, comprising a plurality of grooves on the inner surface that each twist along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein each groove spans only an arcuate portion of the inner surface, and wherein the inner surface has diagonal symmetry about any plane that extends through the longitudinal axis of the body.
- 23. The air flow twisting device of claim 22, wherein each groove comprises a first side, a second side and a base, wherein a concave surface defines the first side and the base of each groove, a convex surface defines the second side of each groove and a junction between the concave and convex surfaces of each groove is a point.
- 24. The air flow twisting device of claim 22, wherein each groove begins at an end of the body and extends along a length of about two-thirds the length of the body.
- 25. The air flow twisting device of claim 22, comprising four grooves.
- 26. An air flow twisting device for an internal combustion engine for providing air for combustion to a combustion chamber of an engine, the device comprising:
a tubular body having a length and an inner surface; and a inner surface consisting of four identical grooves that twists along at least a portion of the length of the body such that air flowing through the body is caused to twist and thus have a twisting motion as it exits the body, wherein each groove spans only an arcuate portion of the inner surface.
- 27. The air flow twisting device of claim 25, wherein each groove comprises a first side, a second side and a base, wherein a concave surface defines the first side and the base of each groove, and a convex surface defines the second side of each groove.
- 28. The air flow twisting device of claim 26, wherein each groove further comprises a junction between the concave and convex surfaces that is a point.
- 29. The air flow twisting device of claim 26, wherein the inner surface has diagonal symmetry about any plane that extends through the longitudinal axis of the body.
Priority Claims (1)
Number |
Date |
Country |
Kind |
S 980077 |
Jul 1998 |
ID |
|
CROSS-REFERENCE TO RELATED APPLICATION(S)
[0001] This application is a continuation-in-part of U.S. Pat. application Ser. No. 09/509,439, filed on Mar. 27, 2000.
Continuation in Parts (1)
|
Number |
Date |
Country |
Parent |
09509439 |
Mar 2000 |
US |
Child |
10376134 |
Feb 2003 |
US |