This invention relates generally to watercraft lifts and more particularly concerns the structural components connecting the lift floatation tanks to the watercraft support frame.
In connecting lift floatation tanks to a watercraft support frame, the frame is fixed to the floatation tanks by bolts through flanges on the tanks, by metal belts tautly pulled around the cross-sections of the tanks or by use of welded assemblies of metal tubes and brackets with the tubes fitted into grooves in the sidewalls of the tanks. The bolts, surrounding belts and side mounted tube assemblies are continuously exposed to water. The integrity of the tank is eventually compromised by the reciprocating forces exerted at the bolt holes on the tank plastic while the lift is in use. The connections to the frame are typically located proximate the front and rear ends of the tanks. As a result, the weight of the watercraft is applied to the front and rear ends of the floatation tanks. The buoyancy force of the water, however, is applied to the entire length of the tanks. Therefore, the presence of the watercraft on the lift causes the hollow plastic tanks to bow downwardly at the ends, distorting the watercraft support frame. The use of side-of-tank tube assemblies may reduce the distortion to some extent, but the constant exposure of the metal tubes to the water far outweighs any such benefit. The deflection problem is most often resolved by the use of more plastic in the tank walls than would otherwise be necessary so as to strengthen the resistance of the tanks to deflection. Unfortunately, added plastic means a heavier and more expensive tank. In addition to these unique deficiencies, all of these known connecting systems are troublesome to install.
It is, therefore, an object of this invention to provide an improved watercraft lift. Another object of this invention is to provide a watercraft lift with a connecting assembly which does not use metal components below the waterline of a floatation tank. A further object of this invention is to provide a watercraft lift with a connecting assembly which does not compromise the structural integrity of the floatation tanks. Yet another object of this invention is to provide a watercraft lift with a connecting assembly which does not require the insertion of bolts through the floatation tank plastic. It is also an object of this invention to provide a watercraft lift with a connecting assembly which does not require the use of belts to girt the floatation tanks. Still another object of this invention is to provide a watercraft lift with a connecting assembly which does not require the engagement of welded tube and bracket assemblies in the side walls of the floatation tanks. An additional object of this invention is to provide a watercraft lift with a connecting assembly which does not place unnecessary stress on the floatation tank walls. Another object of this invention is to provide a watercraft lift with a connecting assembly which resists buoyancy-caused deflection of the floatation tanks. A further object of this invention is to provide a watercraft lift with a connecting assembly which enables use of thin-walled plastic floatation tanks. Yet another object of this invention is to provide a lightweight watercraft lift. And it is object of this invention to provide a watercraft lift with a connecting assembly which is easily installed.
In accordance with the invention, an improved connecting structure is provided for use in mounting a watercraft support frame on the floatation tanks of a watercraft lift.
A pair of pockets are spaced fore and aft in an upper longitudinal corner of the floatation tank A pair of pads have bottom surfaces sized and contoured to overlap their respective pockets and abut the top wall of the floatation tank. A pair of brackets are contoured for insertion into their respective pockets. Each bracket has a flange with a top surface contoured to abut the bottom surface of its respective pad when the bracket is disposed in its respective pocket. Upward and outward motion of each bracket relative to the floatation tank is limited by engagement of the bracket on the tank. The bracket flanges are fastened to their respective pads with the pads overlapping the pockets and abutting the floatation tank. Thus, the pads are secured in place on top of the tank without being fastened directly to the tank and the watercraft support structure can be mounted on the pads. The pockets are preferably sized for fore and aft tolerance of the brackets so as to compensate for the normal expansion and contraction of the components and forces exerted on the lifts in turbulent conditions without stressing the tank plastic.
In a preferred embodiment, a trough extends in the top of the floatation tank from approximately the fore to the aft pocket. The bottom of the trough slopes upwardly from the pockets to a crest. A reinforcing member extends from end to end in the trough. The pads abut the tops of the fore and aft ends of the reinforcing member and the crest abuts the bottom of the mid-portion of the reinforcing member when the pads are fastened to the brackets. This configuration of components resists buoyancy-induced bowing of the plastic tank. The reinforcing member may, for example, be a length of approximately 2″ inch square steel tubing.
Preferably, the top surface of the floatation tank is flat in the area of the pocket. The pocket is in the side wall of the floatation tank and opens into the flat surface on the top of the floatation tank and the pad has a flat bottom surface for juxtaposition against the flat surface on top of the floatation tank. Preferably, the bracket is engaged to the tank by use of one or more downwardly depending lugs on the side wall of the floatation tank below the pocket. In its preferred embodiment, the bracket has a lower portion contoured for engagement on the lug and an upper portion contoured for insertion into the pocket with the top surface of the bracket in the plane of the flat surface on the top of the floatation tank when the bracket lower portion is engaged on its respective lug. One or more holes through the pad open into its respective pocket and aligns with one or more holes through the bracket flange when the pad is seated on the bracket. Nuts co-operable with bolts extending through the aligned holes complete the connection.
In its preferred embodiment, the bracket is S-shaped with a lower portion contoured for hinging on the lug and an upper portion contoured for insertion into the pocket. The downwardly depending lug is bifurcated and respective pad and bracket holes are aligned above respective lugs. The S-shaped bracket may have a vertical reinforcing rib dividing its lower portion into fore and aft segments and contoured for disposition between the spaced-apart lugs resulting from the bifurcation. The rib may also extend to the upper portion of the S-shaped bracket.
Other objects and advantages of the invention will become apparent upon reading the following detailed description and upon reference to the drawings in which:
While the invention will be described in connection with preferred embodiments of its components, it will be understood that it is not intended to limit the invention to those embodiments or to the details of the construction or arrangement of parts illustrated in the accompanying drawings.
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Pads 70, preferably of cast iron, overlap each of the pockets 50 and abut the top walls 35 of the floatation tanks 30. The pads 70 are seated on, but not directly connected to, the tanks 30. Rather, the pads 70 are connected directly to plastic brackets 90. Each of the brackets 90 has a flange 91 with a top surface 93 which is contoured to abut the bottom surface 71 of a pad 70 when the bracket 90 is disposed in a pocket 50. The plastic bracket 90 is engaged on a lug 37 on the plastic tank 30 and rotated on the lug 37 into the pocket 50 for abutment of the flange 91 with the bottom surface 71 of the pad 70. The bracket flange 91 is fastened to its pad 70 after the bracket 90 is engaged on the lug 37 and the pad 70 has been positioned to overlap the pocket 50 and abut the floatation tank 30. In this position the bracket 90 cannot be rotated on its lug 37. As a result, the pads 70 are secured in place on top of the tank 30 without being fastened directly to the tank 30 and the watercraft support frame 10 can be mounted to vertical flanges 73 on the pads.
The particular watercraft lift L illustrated in
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The brackets 90 are engaged on, but not fastened to, the tank 30. Therefore, the brackets 90 can be made of substantially sturdier plastic while the tanks 30 can be of relatively thin-walled plastic. Thus, the overall weight of the lift L is reduced. The cast iron pads 70 are secured by steel, but the steel is entirely above the lift water line and not immersed in water. No welding need be involved in the assembly. No mounting holes need be provided in the tank plastic. No stresses are applied to the plastic walls of the tanks 30 by components fixed directly to the tanks 30. The use of the pads 70 facilitates the incorporation of the anti-buoyancy-deflection reinforcing structure 120, though the reinforcing structure 120 need not necessarily be incorporated into the lift L. Furthermore, the reinforcing system 120 herein described may be incorporated into lifts which do not incorporate the tank-to-watercraft support structure herein described.
Thus, there has been provided, in accordance with the invention, a watercraft lift that fully satisfies the objects, aims and advantages set forth above. While the invention has been described in conjunction with specific embodiments of the invention and its component parts, many alternatives, modifications and variations will be apparent to those skilled in the art in light of the foregoing description. Accordingly, it is intended to embrace all such alternatives, modifications and variations as fall within the spirit of the appended claims.
| Number | Name | Date | Kind |
|---|---|---|---|
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| 4557210 | Gerwin | Dec 1985 | A |
| 4875426 | Soga et al. | Oct 1989 | A |
| 4993350 | Pepper | Feb 1991 | A |
| 5016551 | Peck et al. | May 1991 | A |
| 5394814 | Rutter et al. | Mar 1995 | A |
| 6547485 | Elson | Apr 2003 | B2 |
| 6752096 | Elson et al. | Jun 2004 | B2 |
| 6755142 | Rice | Jun 2004 | B2 |