Abstract
A jet pump assembly includes a marine engine, a jet drive and a shield adapted to be secured to a transom of a watercraft. The shield has arms to which the marine engine is secured and legs to which the jet drive is secured, the arms and legs extending in opposite directions. The shield has a flange adapted to be secured to the transom of the watercraft. The shield covers an opening in the transom through which the jet pump assembly is passed during assembly. A gasket between the shield and transom prevents water from entering the watercraft.
Claims
1. A jet pump assembly for attachment to a transom of a watercraft, the jet pump assembly comprising: a marine engine; a jet drive including a rotatable shaft configured to receive torque from the marine engine; and a shield adapted to be secured to the transom of the watercraft, wherein the shield has parallel arms to which the marine engine is secured and parallel legs to which the jet drive is secured, the arms and legs of the shield extending in opposite directions, wherein the rotatable shaft extends through an opening in the shield.
2. The jet pump assembly of claim 1, wherein the shield has two arms to which the marine engine is secured and two legs to which the jet drive is secured.
3. The jet pump assembly of claim 2, wherein the arms and legs of the shield are hollow.
4. The jet pump assembly of claim 1, wherein a portion of the marine engine is behind a plane defined by the transom of the watercraft when the jet pump assembly is secured to the transom of the watercraft.
5. The jet pump assembly of claim 1, wherein the shield is large enough to cover an opening in the transom of the watercraft, the opening in the transom of the watercraft being large enough so the marine engine may pass through the opening in the transom of the watercraft.
6. The jet pump assembly of claim 1, wherein the shield has a removable cover.
7. The jet pump assembly of claim 1, wherein the shield has a flange which has openings through which fasteners extend to secure the shield to the transom.
8. In combination, a watercraft and a jet pump assembly, the combination comprising: a watercraft having a transom with an opening therein, a jet pump assembly comprising: a marine engine; a jet drive including a rotatable shaft configured to receive torque from the marine engine; and a shield secured to the transom of the watercraft and located behind the transom of the watercraft, the shield having two hollow parallel legs to which the jet drive is secured and two hollow parallel arms to which the marine engine is secured, wherein the rotatable shaft extends through an opening in the shield and the shield covers the opening in the transom of the watercraft.
9. The combination of claim 8, wherein the shield has a flange coupled to an exterior surface of the transom of the watercraft and a gasket is located between the flange and the exterior surface of the transom of the watercraft.
10. The combination of claim 8, wherein the shield has an interior cavity and a portion of the marine engine is located inside the interior cavity of the shield.
11. The combination of claim 8, wherein a grate of the jet drive is secured to the hollow parallel legs of the shield.
12. A method of installing a jet pump assembly to a watercraft, the method comprising: securing a jet drive and a marine engine to a shield; passing the marine engine at least partially through an opening in a transom of the watercraft; and securing a flange of the shield to a transom of the watercraft.
13. The method of claim 12, further comprising: sandwiching a gasket between the flange of the shield and the transom of the watercraft.
14. The method of claim 12, wherein securing the jet drive to the shield comprises securing the jet drive to two hollow parallel legs of the shield.
15. The method of claim 12, wherein securing the marine engine to the shield comprises securing the marine engine to two hollow parallel arms of the shield.
16. A method of installing a jet pump assembly to a watercraft, the method comprising: building a jet pump assembly by securing a jet drive and a marine engine to a shield, the shield having an opening through which a portion of the jet drive extends, the marine engine being coupled to the jet drive to power the jet drive; passing a portion of the jet pump assembly through an opening in a transom of the watercraft; and securing the shield to the transom of the watercraft.
17. The method of claim 16, wherein securing the shield to the transom of the watercraft comprises securing a flange of the shield to the transom of the watercraft.
18. The method of claim 17, further comprising securing a gasket between the flange of the shield and the transom of the watercraft.
19. The method of claim 16, wherein securing the jet drive to the shield comprises securing the jet drive to two hollow parallel legs of the shield.
20. The method of claim 16, wherein passing a portion of the jet pump assembly through the opening in the transom of the watercraft comprising passing at least a portion of the marine engine through the opening in the transom of the watercraft.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and, together with the general description given above and the detailed description given below, explain the embodiments of the invention.
(2) FIG. 1 is a perspective view of a watercraft including an exemplary jet pump assembly in accordance with the invention.
(3) FIG. 2 is a magnified bottom perspective view of a portion of the jet pump assembly of FIG. 1, showing the shield of the jet pump assembly secured to the transom of the watercraft.
(4) FIG. 3 is a top view of the jet pump assembly secured to the transom of the watercraft.
(5) FIG. 4 is a perspective view of the jet pump assembly prior to assembly.
(6) FIG. 4A is a perspective view of the assembled jet pump assembly prior to the shield of the jet pump assembly being secured to the transom of the watercraft.
(7) FIG. 5 is a side view showing the jet pump assembly secured to the transom of the watercraft.
(8) FIG. 5A is an enlarged view of the encircled area 5A of FIG. 5, showing a gasket sandwiched between the shield and the transom of the watercraft.
(9) FIG. 6 is a rear perspective view of the shield of the jet pump assembly.
(10) FIG. 7 is a front perspective view of the shield of the jet pump assembly.
(11) FIG. 8 is a side view of the shield of the jet pump assembly.
(12) FIG. 9 is a side view of the jet pump assembly secured to the transom of the watercraft.
(13) FIG. 10 is a perspective view of a portion of a pontoon boat having three toons, the middle toon having a jet pump assembly installed according to a method disclosed herein.
(14) FIG. 11 is a perspective view of the jet pump assembly being put into the middle toon of the pontoon boat of FIG. 10.
DETAILED DESCRIPTION
(15) Referring now to FIG. 1, an exemplary jet pump assembly 10 according to an aspect of the invention is shown mounted to a watercraft 12. The watercraft 12 includes a hull 14 which has a bottom 16, a bow (not shown), a stern 17, a transom 18, a port side 20, and a starboard side 22, which collectively define an interior 25 of the watercraft. The jet pump assembly 10 may be operatively coupled to a transom 18 of the hull 14 as shown in FIG. 1 for supplying power to the jet pump assembly 10 to propel the watercraft 12 through the water.
(16) As discussed in greater detail below, the jet pump assembly 10 may have a compact modular “plug and play” configuration for installation onto the transom 18 of the watercraft 12 with a substantial portion of the jet pump assembly 10 positioned external to the hull 14. The features of the jet pump assembly 10 are set forth in further detail below to clarify each of these functional advantages and other benefits provided in this disclosure.
(17) As best shown in FIG. 4, the jet pump assembly 10 comprises a marine engine 24, a shield 26 and a jet drive 28. Although one configuration of marine engine 24 is illustrated, any known marine engine may be used. The drawings are not intended to be limiting. Similarly, although one configuration of jet drive 28 is illustrated, any known jet drive may be used. Exemplary jet drives are disclosed in U.S. Pat. Nos. 10,486,786 and 10,787,237 which are fully incorporated herein.
(18) As best illustrated in FIGS. 6-8, one embodiment of shield 26 of the jet pump assembly 10 comprises a central portion 30, two arms 32 extending forwardly from the central portion 30 and two legs 34 extending rearwardly from the central portion 30. The central portion 30 of shield 26 includes a top 36, two sides 38, a bottom 40 and a rear 42 which define a hollow interior 41.
(19) As best shown in FIG. 8, the top 36 of the shield 26 is bent downwardly along bend 35 to make the rear 42 of the shield 26. The rear 42 of the shield 26 has an upper portion 44 which is generally vertically oriented, a middle portion 46 which is sloped or inclined downwardly from bend 48 to bend 50, and a lower portion 52. The lower portion 52 of rear 42 of the shield 26 is slightly sloped or declined from bend 50 to bend 53. As best shown in FIGS. 6 and 7, a circular opening 70 is cut from the lower portion 52 of the rear 42 of the shield 26.
(20) As best shown in FIGS. 7 and 8, the bottom 40 of the shield 26 has a front portion 54, a sloped portion 56 and a stub portion 62. The front portion 54 is generally horizontally oriented in the drawings extending from bend 53 to bend 58. The sloped portion 56 extends downwardly and forwardly from bend 58 to bend 60. As best shown in 8, from bend 60, the stub portion 62 is generally vertically oriented in the drawings. A stabilizer 64 having a hollow interior 66 is secured to the stub portion 62 of the bottom 40 of the shield 26. As best shown in FIG. 8, a bracket 68 is secured to the stabilizer 64.
(21) As best shown in FIG. 8, the top 36 and bottom 40 of the shield 26 are illustrated as being made from the same piece of metal as the rear 42 of the shield 26. However, the top and/or bottom 40 of the shield 26 may be made from one or more different pieces of metal than the rear 42 of the shield 26. The portions of the shield including the sides 38 of the shield 26 may be made of any number of different pieces.
(22) As best shown in FIG. 6, each leg 34 of the shield 26 is secured to the lower portion 52 of the rear 42 of the shield 30 with a triangular wedge 72 for stability and strength. Each wedge 72 is welded to the lower portion 52 of the rear 42 of the shield 26 and to an upper wall 74 of one of the legs 34 of the shield 26. As best shown in FIG. 6, each leg 34 of the shield 26 has an upper wall 74, a bottom wall 76 and two side walls 78 which define a hollow interior 80 and define a rectangular cross-sectional configuration. Each end of each leg 34 of the shield 26 has a cap 81 to prevent water from entering the hollow interior 80 of the leg 34 of the shield 26.
(23) As best shown in FIG. 7, each arm 32 of the shield 26 has an upper wall 84, a bottom wall 86 and two side walls 88 which define a hollow interior 90 and define a rectangular cross-sectional configuration. As best illustrated in FIG. 8, each of the arms 32 of the shield 26 extends from the central portion 30 of the shield 26 in a direction opposite the direction of the legs 34 of the shield 26. As best shown in FIG. 8, the length L of each of the arms 34 of the shield 26 is identical. Similarly, the length LL of each of the legs 32 of the shield is identical. However, the length L of the arms 34 is greater than the length L of the legs 32 of the shield 26.
(24) As seen in the drawings, the top 36 of the shield 26 has an opening 92 cut out therefrom. The opening 92 is covered with a removable cover 94 to allow access to the interior 41 of the shield 26 for purposes of replacing or repairing portions of the marine engine 24.
(25) The shield 26 of the jet pump assembly 10 may be constructed of aluminum, fiberglass and/or composite. For example, certain components of the shield 26 of jet pump assembly 10 may be constructed of cast aluminum. It will be appreciated that the shield 26 of the jet pump assembly 10 may be constructed of any suitable material which is waterproof.
(26) As best shown in FIG. 6, the shield 26 of the jet pump assembly 10 has a flange 96 extending around its perimeter. More particularly, the flange 96 extends upwardly from the top 36 of the shield 26, outwardly from the sides 34 of the shield 26 and downwardly from the bottom 40 of the shield 26. Holes 98 are formed through the flange 96 at select spaced locations and sized to allow bolts 100 to pass therethrough. As best shown in FIG. 2, the bolts 100 extend through the holes 98 in the flange 96 of the shield 26, through openings 116 in the gasket 114, through openings 118 in the transom 18 of the watercraft 12 and are tightened using nuts 120 with washers 122 between the nuts 120 and bolts 100 to secure the jet pump assembly 10 to the watercraft 12.
(27) As shown in FIG. 2, when the jet pump assembly is fully assembled, the jet drive 28 is secured to the two legs 34 of the shield 28. More specifically, a grate 102 of the jet drive 28 is secured with fasteners 104 to the bottom walls 76 of the legs 34 of the shield 28. However, any other portion(s) of any known jet drive may be secured to the legs 34 of the shield 28 to secure the jet drive 28 to the shield.
(28) As shown in FIG. 9, when the jet pump assembly is fully assembled, the marine engine 24 is secured to the two arms 32 of the shield 28. More specifically, the marine engine 24 is secured with bushings (only one shown) 106 to the arms 32 of the shield 28. However, any other portion(s) of any known marine engine may be secured to the arms 32 of the shield 28 to secure the jet drive 28 to the shield 28.
(29) Referring now to FIGS. 4-5, a method of constructing a jet pump assembly and installing the jet pump assembly 10 onto the transom 18 of the watercraft 12 is provided. Initially, as shown in FIG. 4, the jet drive 28 is secured to the shield 26 and more specifically to the two parallel legs 34 of the shield 26. The marine engine 24 is secured to two parallel arms 32 of the shield 26. Additionally, as shown in FIG. 5, a drive shaft 108 of the jet drive 28 is passed through circular opening 70 in the shield 26 and coupled to the marine engine 24 to provide power to the jet drive 28 upon operation.
(30) After the jet pump assembly 10 is fully assembled, the assembled jet pump assembly 10 is passed partially through an opening 110 in the transom 18 of the hull 14 of the watercraft 12. See FIG. 4A. As shown in FIG. 4A, the assembled jet pump assembly 10 is oriented as shown and moved in the direction of arrow 112 such that a portion of the marine engine 24 extends through the opening 110 in the transom 18 of the hull 14 of the watercraft 12. The opening 110 is cut out of the transom 18 of the hull 14 of the watercraft 12 prior to installation of the jet pump assembly 10. The opening 110 is large enough to enable at least a portion of the marine engine 24 of the assembled jet pump assembly 10 to pass therethrough. The assembled jet pump assembly 10 does not need to be lifted over the transom 18 for assembly. In addition, the presence of the opening 110 enables the jet pump assembly 10 to be constructed prior to securement to the hull 14 of the watercraft 12.
(31) As shown in FIG. 4A, the assembled jet pump assembly 10 is moved towards the bow of the watercraft or forwardly in the direction of arrow 112 such that a portion of the marine engine 24 extends through the opening 110 in the transom 18 of the hull 14 of the watercraft 12. The assembled jet pump assembly 10 is moved further forwardly until a gasket 114 is sandwiched between the transom 18 of the hull 14 of the watercraft 12 and the flange 96 of the shield 26 contacts the exterior surface of the transom 18 of the hull 14 of the watercraft 12. As shown in FIGS. 5 and 5A, the gasket 114 sandwiched between the transom 18 of the watercraft 12 and the flange 96 of the shield 26 prevents water from leaking inside the shield 26 and into the watercraft 12.
(32) As shown in FIGS. 5 and 5A, after the assembled jet pump assembly 10 is properly located with the shield 26 covering the opening 110 in the transom 18 of the watercraft 12, fasteners 100 are passed through the openings 98 in the flange 96 of the shield 26, through openings 118 in the gasket 114 and through openings 118 in the transom 18 of the watercraft 12. The fasteners 100 pass through washers 122 and nuts 120 are threaded onto the fasteners 100.
(33) Although the drawings show one size and shape of opening 110 in the transom 18 of the hull 14, the drawings are not intended to be limiting. The opening 110 in the transom 18 of the hull 14 may be any desired shape such that the opening 110 allows at least a portion of the marine engine 24 of the assembled jet pump assembly 10 to fit through the opening 110 in the transom 18 of the watercraft 12.
(34) FIGS. 10 and 11 illustrate one type of watercraft in the form of a tritoon boat 12a. As shown in FIG. 10, the tritoon boat 12a has two outer toons 125 and a middle toon 124. A deck 126 may be secured to some or all three of the toons 124, 125 in any known manner. Although one type of outer toon 125 is illustrated, any known outer toon may be used. The drawings are not intended to be limiting. Similarly, although one type of middle toon 124 is illustrated, any known middle toon may be used. The drawings are not intended to be limiting. The deck 126 is shown generally and not intended to be limited in any way. Any known deck 126 may be used.
(35) Middle toon 124 has a cavity 128 adapted to receive a gasoline tank (not shown) at the rear thereof. As shown in FIG. 11, the cavity 128 has a transom 130 in which an opening 132 is formed (like opening 110 formed in the transom 18 of watercraft 12 shown in FIG. 4). A jet pump assembly 10 is attached to the middle toon 124 through the opening 132 in the transom 130 of middle toon 124 in the same manner described above.
(36) Although FIGS. 10 and 11 illustrate a tritoon watercraft 12a, the present invention may be used to manufacture a pontoon watercraft as well. Any watercraft incorporating floats or toons may have a jet pump assembly as described and shown herein. The jet pump assembly or assemblies may be installed in any such watercraft in accordance with any of the methods described and/or shown herein.
(37) Accordingly, complete installation of the jet pump assembly 10 may be accomplished in a relatively short time as compared to conventional installation techniques. Moreover, by assembling the jet pump assembly 10 prior to securement to the transom 18 of the hull 14 of the watercraft 12, many of the difficulties associated with the current method of securing a jet pump to a watercraft are avoided. The jet pump assembly 10 may be assembled more easily and more quickly than the current method of assembling a portion of the jet pump assembly inside the watercraft including one having toons. As shown in FIGS. 1 and 3 when fully installed the marine engine 24 inside the interior 25 of the watercraft 12 may be covered with a cover shown in dashed lines for safety.
(38) While the present invention has been illustrated by the description of specific embodiments thereof, and while the embodiments have been described in considerable detail, it is not intended to restrict or in any way limit the scope of the appended claims to such detail. The various features discussed herein may be used alone or in any combination. Additional advantages and modifications will readily appear to those skilled in the art. The invention in its broader aspects is therefore not limited to the specific details, representative apparatus and methods and illustrative examples shown and described. Accordingly, departures may be made from such details without departing from the scope of the general inventive concept.
