Watercraft with improved stability

Information

  • Patent Grant
  • 6702629
  • Patent Number
    6,702,629
  • Date Filed
    Tuesday, July 30, 2002
    22 years ago
  • Date Issued
    Tuesday, March 9, 2004
    20 years ago
Abstract
A watercraft, equipped with a jet drive power source, with improved stability is disclosed. The jet drive power source is configured to produce power along a predetermined direction and form a drive line based upon the predetermined direction. The drive line bisects a plane of the keel at a predetermined angle that is less than about 4 degrees. The drive shaft and the output shaft are not substantially parallel.
Description




FIELD OF THE INVENTION




This invention relates to watercraft and more particularly to watercraft with improved stability.




DESCRIPTION OF THE RELATED ART




Various types of watercraft exist, each being suited for different types of activities. For example, a pontoon-type watercraft is designed for slower speeds and general recreational use and is typically powered by an outboard engine. In contrast, sport boats and personal watercraft are designed for higher speeds and superior handling and are powered typically by inboard jet drive systems, which consist of an inboard engine and a jet propulsion unit.




In a conventional sport boat, the engine is mounted above a jet propulsion unit. The intake for the jet propulsion unit is located beneath the watercraft and the exhaust, or jet port, is located at the rear of the watercraft.




There are several parameters that are engineered into a sport boat that may affect its performance. One of those parameters is the “drive line angle,” which is the angle measured between the primary drive shaft (attached to the impeller) and the keel line of the watercraft.




Due to the physical characteristics of conventional jet drive systems in sport boats in the prior art, the drive line angle is typically about 4 degrees or greater. In a conventional watercraft, the positive angle of the drive line translates into an angle of thrust that is directed slightly upward toward the surface of the water, as illustrated in FIG.


2


. The upward thrust angle has a tendency to push the bow of the watercraft out of the water. In other words, the positive drive line angle tends to lift the bow of the sport boat during operation.




U.S. Pat. No. 5,984,740 (the '740 patent) describes and illustrates a personal watercraft


10


, which incorporates a jet propulsion drive configured according to the teachings of the prior art. As illustrated in FIG. 3 of the '740 patent, the impeller shaft 56 is angled upwardly from the keel line. The exact angle α of the impeller shaft 56, however, is not disclosed. The '740 patent only discusses the advantages of a positive angle α for operation of the personal watercraft


10


described. (See. e.g. the '740 patent at col. 5, lines 36-48.)




While those skilled in art may appreciate the benefits of a positive drive angle, a phenomenon known as “porpoising” may be detected, at certain speeds, by occupants of certain boats. “Porpoising” refers to a condition where the boat tends to move up and down in the water like the movement of a porpoise when it jumps out of the water. This can create an unpleasant ride for the occupants of the boat.




Conventionally, sport boats powered by jet propulsion units have all had positive drive line angles. In fact, conventional wisdom suggests that anything less than a positive drive line angle will so adversely affect vehicle performance that manufacturers of marine engines have specifically discouraged the incorporation of neutral (0°) or negative drive line angles in boats.




“Porpoising,” however, remains a problem with certain boat designs.




Accordingly, a need exists for a watercraft that utilizes a jet drive system with improved stability and reduced “porpoising” to ensure that the occupants of the boat will experience a more comfortable and enjoyable ride.




SUMMARY OF THE INVENTION




It is, therefore, an object of the present invention to provide a watercraft, which provides the advantages of a jet propulsion system, with increased stability and reduced “porpoising,” by controlling the angle of thrust of the propulsion unit relative to the keel line.




One embodiment of the present invention provides a watercraft including a hull with a keel and a jet drive power source. The jet drive power source includes an engine, an engine output shaft, and a jet propulsion unit. The jet propulsion unit includes a water passage, a drive shaft, an impeller, and a jet port. The engine output shaft is operationally connected to the drive shaft. The jet drive power source is configured to produce power along a predetermined direction and form a drive line based upon the predetermined direction. The drive line bisects a plane of the keel at a predetermined, preferably negative, angle.




Other embodiments of the present invention will be discussed in or will be made apparent from the description that follows.











BRIEF DESCRIPTION OF THE DRAWINGS




The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate embodiments of the invention and, together with the general description given above and the detailed description of the embodiments given below, serve to explain the principles of the present invention. In the figures:





FIG. 1

is a cross-sectional side view of the watercraft of the present invention;





FIG. 2

is a detailed cross-sectional view of the jet drive system of the prior art;





FIG. 3

is a detailed cross-sectional view of one embodiment of the jet drive system of the present invention; and





FIG. 4

is a detailed cross-sectional view of an alternate embodiment of the jet drive system of the present invention as illustrated in FIG.


3


.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Throughout the description of the several embodiments of the present invention, reference will be made to various elements, the construction of which is readily known to those skilled in the art. Accordingly, an exhaustive description of each and every component is not provided, only a description of those elements required for an understanding of the present invention.





FIG. 1

is a side view of a watercraft


10


of the present invention. In the preferred embodiment, the watercraft


10


is a jet boat that includes a hull


20


, with a bow


21


, a stern


22


, and a keel


23


. The watercraft illustrated in

FIG. 1

is a sport boat. The details of the sport boat have been omitted because they are not relevant to the present invention. As those of ordinary skill in the art will appreciate after reading the description set forth below, the present invention may be employed on any style jet-propelled boat, regardless of the size, style, or configuration.




In the preferred embodiment, the watercraft


10


of the present invention is powered by a jet drive power source


30


. The jet drive power source


30


of the present invention provides for an improved boat ride by comparison with a conventional, propeller-driven watercraft.




As shown in general detail in

FIG. 1

, and in greater detail in

FIGS. 3 and 4

, the jet drive power source


30


includes an engine


40


with an output shaft


45


and a jet propulsion unit


50


. The engine


40


may be, but is not limited to, a two-stroke or a four-stroke, inboard, internal combustion engine.




Referring to

FIGS. 3 and 4

, the jet propulsion unit


50


comprises a housing


51


with a water passage


52


defined by the housing


51


, an intake


90


, an drive shaft


55


, an impeller


56


, and a jet port


80


. Although the housing


51


can be a separate piece that is mounted to the hull


20


, the housing


51


is preferably integrally formed as part of the hull


20


.




The engine


40


is operatively connected to a jet propulsion unit


50


through its output shaft


45


. The output shaft


45


is rotationally connected to the drive shaft


55


, located within the jet propulsion unit


50


, such that the output shaft


45


and the drive shaft


55


are not substantially parallel. That is, an angle


60


is formed between the longitudinal axis of the output shaft


45


and the longitudinal axis of the drive shaft


55


such that the angle


60


is greater than zero. As would be appreciated by those skilled in the art, however, the output shaft


45


and the drive shaft


55


could be disposed so that they are substantially parallel (either coaxial or coplanar) to one another.




As defined herein, in the preferred embodiment, the angle


60


formed between the longitudinal axis of the output shaft


45


and the longitudinal axis of the drive shaft


55


will, by definition, be between about 5 degrees to about 175 degrees, no matter the configuration between the engine


40


and the jet propulsion unit


50


. Preferably, the angle


60


will be between about 45 degrees to about 135 degrees. Most preferably, the angle


60


will be about 90 degrees and the output shaft


45


will have a generally vertical orientation.




In the embodiments illustrated, the output shaft


45


and the drive shaft


55


are located in the same longitudinal plane that bisects the hull


20


from the bow


21


to the stern


22


. Alternatively, the output shaft


45


and the drive shaft


55


may be located in a plane that is either parallel to, or intersects with the longitudinal plane that bisects the hull


20


from the bow


21


to the stern


22


.




Disposed within the jet propulsion unit


50


is a water passage


52


. During normal operation of the watercraft


10


, water enters the passage


52


at an intake


90


located at the bottom of the hull


20


. The water enters the passage


52


, passes by an impeller


56


and exits the passage


52


through a nozzle


78


and then through a jet port


80


. Depending on the speed of the watercraft


10


, the jet port


80


may or may not operate below the waterline


70


of the watercraft


10


. Normally, at slow speeds, the jet port


80


usually operates beneath the waterline


70


.




The jet port


80


typically is a steerable nozzle connected, usually via cables, to the helm of the watercraft


10


. As the operator changes the helm direction, so, too; does he/she change the direction of jet port


80


. In this manner, the operator changes the travel direction of the watercraft


10


.




As illustrated in

FIGS. 3 and 4

, the nozzle


78


and the jet port


80


for the jet drive power source


30


generate a force along the drive line


85


in a rearward direction


86


. The drive line


85


forms an angle


87


with the keel


23


of the watercraft


10


. In

FIGS. 3 and 4

, a plane


25


defined by the keel


23


is shown at the keel


23


as a solid line and above the keel


23


(for reference) as a dotted line. The plane


25


is laterally oriented, parallel to the keel


23


.




In the illustrated embodiments, the central axes of the drive shaft


55


, the impeller


56


, the nozzle


78


, and the jet port


80


are aligned along a common centerline. So aligned, the centerline, which is an extension of the central axis of the drive shaft


55


, defines the drive line


85


of the jet propulsion unit


50


.




In the illustrated embodiments, the nozzle


78


and the jet port


80


are substantially oriented along the same direction. In other words, both are oriented to direct the force of the jet power source


30


along the drive line


85


, which corresponds to the axis of the drive shaft


55


. It is possible, however, that the jet port


80


and the nozzle


78


may be oriented with respect to one another so that they are not substantially oriented along the same direction. Regardless, the combined effect of the nozzle


78


and the jet port


80


will establish a drive line


85


with an angular orientation to the plane


25


defined by the keel


23


. That drive line


85


typically corresponds to the axis of the drive shaft


55


.




As shown in

FIGS. 3 and 4

, the drive line


85


intersects with the plane


25


of the keel


23


at an angle


87


. In the conventional embodiment illustrated in

FIG. 2

, the drive line


85


forms a positive angle


87


of more than about 4 degrees with the plane


25


of the keel


23


.




As discussed above, prior to the present invention, those skilled in the art (in particular the jet drive engine manufacturers) believed that the drive line angle must be positive in order for the watercraft to operate properly, as shown in FIG.


2


. Anything less than about a 4 degree drive line angle


87


was strongly discouraged.




In certain watercraft designs, however, the positive drive line angle


87


of 4 degrees may create the “porpoising” effect. This problem is acknowledged in the '740 patent, which is discussed above. The reason for this is believed to be as follows. The positive drive line angle


87


has a tendency to push the bow


21


of the watercraft


10


up out of the water. When the watercraft


10


reaches a sufficient speed, enough of the bow


21


of the watercraft


10


extends above the water that the water cannot support the bow


21


. In other words, the weight of the bow


21


exceeds the upward buoyant force of the water. This causes the bow


21


to fall into the water until the flow of the water pushes the bow


21


up again to the point where it no longer is in equilibrium with the buoyant force of the water. The repetitive rise and fall of the bow


21


results in “porpoising.”




To address the problem of “porpoising,” the inventors decided to contravene conventional knowledge and decrease the drive line angle


87


to less than the traditionally-required 4 degrees. After reducing the drive line angle


87


to less than 4 degrees, the inventors discovered that “porpoising” can be reduced significantly or eliminated altogether without affecting the performance of the watercraft


10


. This creates a more stable, less bumpy, boat ride. The present invention is intended to encompass watercraft


10


with an angle


87


of less than 4 degrees. Preferably, the predetermined angle


87


is about −5 degrees to about 2 degrees. More preferably, the predetermined angle


87


is about −3 degrees to about 1 degree. Most preferably, the predetermined angle


87


is about −2 degrees to about 0 degrees.




In addition, one skilled in the art would understand that the predetermined angle


87


can be altered in a number of different ways without deviating from the scope of the present invention.




The embodiment illustrated in

FIG. 4

differs from the embodiment illustrated in

FIG. 3

in that the power source


30


is disposed above the drive shaft


55


. In particular, the jet drive power source


30


is positioned above the drive shaft


55


such that a substantial portion of the power source


30


extends over the drive shaft


55


toward the rear of the watercraft


10


. In the embodiment illustrated in

FIG. 3

, the power source


30


is positioned in front of the drive shaft


55


. In that embodiment, a substantial portion of the power source


30


extends forwardly of the end of the drive shaft


55


(toward the front of the watercraft


10


). The embodiment illustrated in

FIG. 4

permits a more compact construction for the jet propulsion unit


50


than the embodiment illustrated in FIG.


3


. Accordingly, the jet propulsion unit


50


illustrated in

FIG. 4

may be employed in a watercraft


10


where space is more of a concern than the watercraft


10


illustrated in FIG.


3


.




From the invention just described, it will be obvious that the invention may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modifications as would be obvious to one skilled in the art are intended for inclusion within the scope of the following claims.



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
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.

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Number Date Country
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Continuation in Parts (1)
Number Date Country
Parent 09/635262 Aug 2000 US
Child 10/207004 US