Claims
- 1. A watercraft comprising:a hull with a keel; and a jet drive power source disposed within the hull, the jet drive power source being configured to (i) produce power along a predetermined direction and (ii) form a drive line based upon the predetermined direction, wherein the drive line intersects a plane of the keel at a predetermined angle that is less than about 4 degrees; an output shaft driven by the jet drive power source; a drive shaft with a first end and a second end, the drive shaft defining a central axis; and a nozzle connected to the hull, the nozzle defining a central axis aligned along a common centerline with the drive shaft central axis, wherein the first end of the drive shaft is rotationally coupled with the output shaft, and wherein the output shaft and the drive shaft are not substantially parallel.
- 2. The watercraft according to claim 1, wherein the predetermined angle is about −5 degrees to about +2 degrees.
- 3. The watercraft according to claim 2, wherein the predetermined angle is about −3 degrees to about +1 degree.
- 4. The watercraft according to claim 3, wherein the predetermined angle is about −2 degrees to about 0 degrees.
- 5. The watercraft according to claim 4, wherein the predetermined angle is about 0 degrees.
- 6. The watercraft according to claim 1, wherein an angle formed between the output shaft and the drive shaft is about 5 degrees to about 175 degrees.
- 7. The watercraft according to claim 6, wherein the angle is about 45 degrees to about 135 degrees.
- 8. The watercraft according to claim 7, wherein the angle is about 90 degrees.
- 9. The watercraft according to claim 1, wherein the jet drive power source is disposed above the drive shaft.
- 10. The watercraft according to claim 9, wherein a substantial portion of the jet drive power source extends over the drive shaft.
- 11. A watercraft comprising:a hull with a keel; a jet drive power source disposed within the hull, the jet drive power source being operatively connected to a drive shaft defining a central axis, the jet drive power source being configured (i) to produce power along the central axis of the drive shaft and (ii) to form a drive line based upon the central axis of the drive shaft, wherein the drive line intersects a plane of the keel at a predetermined angle that is less than about 4 degrees; a nozzle connected to the hull, the nozzle defining a central axis aligned along a common centerline with the drive shaft central axis; and an output shaft driven by the jet drive power source, wherein the drive shaft has a first and a second end, wherein the first end of the drive shaft is rotationally coupled with the output shaft, and wherein the output shaft and the drive shaft are not substantially parallel.
- 12. The watercraft according to claim 11, wherein the predetermined angle is about −5 degrees to about +2 degrees.
- 13. The watercraft according to claim 12, wherein the predetermined angle is about −3 degrees to about +1 degree.
- 14. The watercraft according to claim 13, wherein the predetermined angle is about −2 degrees to about 0 degrees.
- 15. The watercraft according to claim 14, wherein the predetermined angle is about 0 degrees.
- 16. The watercraft according to claim 11, wherein an angle formed between the output shaft and the drive shaft is about 5 degrees to about 175 degrees.
- 17. The watercraft according to claim 16, wherein the angle is about 45 degrees to about 135 degrees.
- 18. The watercraft according to claim 17, wherein the angle is about 90 degrees.
- 19. The watercraft according to claim 11, wherein the jet drive power source is disposed above the drive shaft.
- 20. The watercraft according to claim 19, wherein a substantial portion of the jet drive power source extends over the drive shaft.
- 21. A watercraft comprising:a hull with a keel; a jet drive power source disposed within the hull, the jet drive power source being configured to (i) produce power along a predetermined direction and (ii) form a drive line based upon the predetermined direction; a drive shaft operatively connected to the jet power source, the drive shaft defining a central axis; and a nozzle connected to the hull, the nozzle defining a central axis aligned alone a common centerline with the drive shaft central axis, wherein the drive line intersects a plane of the keel at a predetermined angle that is less than about 4 degrees.
- 22. The watercraft according to claim 21, wherein the predetermined angle is about −5 degrees to about +2 degrees.
- 23. The watercraft according to claim 22, wherein the predetermined angle is about −3 degrees to about +1 degree.
- 24. The watercraft according to claim 23, wherein the predetermined angle is about −2 degrees to about 0 degrees.
- 25. The watercraft according to claim 24, wherein the predetermined angle is about 0 degrees.
- 26. The watercraft according to claim 21, wherein the jet drive power source is disposed above the drive shaft.
- 27. The watercraft according to claim 26, wherein a substantial portion of the jet drive power source extends over the drive shaft.
- 28. The watercraft according to claim 1, further comprising a jet port defining a central axis also aligned along the common centerline with the drive shaft central axis.
- 29. The watercraft according to claim 11, further comprising a jet port defining a central axis also aligned along the common centerline with the drive shaft central axis.
- 30. The watercraft according to claim 21, further comprising a jet port defining a central axis also aligned along the common centerline with the drive shaft central axis.
Priority Claims (1)
Number |
Date |
Country |
Kind |
2279804 |
Aug 1999 |
CA |
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Parent Case Info
This application is a continuation-in-part of U.S. Non-provisional Patent Application Ser. No. 09/635,262, filed on Aug. 9, 2000, now pending, which is incorporated herein by reference. This application also claims the benefit of U.S. Provisional Patent Application Ser. No. 60/168,676, filed Dec. 3, 1999, and Canadian Application No. 2,279,804, filed Aug. 9, 1999, both of which are incorporated herein by reference. The parent application (Ser. No. 09/635,262) relies on these two applications for priority. In addition, this application relies for priority on U.S. Provisional Patent Application Ser. No. 60/308,836, filed on Aug. 1, 2001, the contents of which are incorporated herein by reference.
US Referenced Citations (35)
Foreign Referenced Citations (1)
Number |
Date |
Country |
4-133894 |
May 1992 |
JP |
Provisional Applications (2)
|
Number |
Date |
Country |
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60/168676 |
Dec 1999 |
US |
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60/308836 |
Aug 2001 |
US |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
09/635262 |
Aug 2000 |
US |
Child |
10/207004 |
|
US |