The present invention relates to watercraft lifts and, more particularly, to bunk mounting systems for watercraft lifts.
Boat lifts are often arranged in a body of water to raise the boat out of the water when not in use. Boat lifts may be supported on the bed of the body of water or by rafts, pontoons, or other floating structures.
Boat lifts may take many different configurations, but mechanical boat lifts typically comprise one or more bunk structures or bunk rails, often referred to simply as bunks, that engage the bottom of the boat when the boat is lifted. The bunks typically comprise a structural portion capable of transferring the weight of the boat to the boat lift and a cushioning portion that protects the bottom of the boat during lifting.
The need exists for bunks that may be reconfigured to accommodate a particular boat lift and a particular boat.
The present invention may be embodied as a bunk mounting system for a watercraft lift comprising a first support defining first and second legs, a second support defining third and fourth legs, and first and second bunks. The bunk mounting system comprises first and second crossbeams, a plurality of pivot connectors, and a plurality of rail connectors. The plurality of pivot connectors pivotably connect the first crossbeam to the first and second legs and the second crossbeam to the third and fourth legs. The plurality of rail connectors detachably connect the first bunk to the first and second crossbeams and the second bunk to the first and second crossbeams.
The present invention may also be embodied as a method of supporting first and second bunks to a watercraft lift comprising a first support defining first and second legs, a second support defining third and fourth legs, and first and second bunks, the method comprising the following steps. First and second crossbeams are provided. The first crossbeam is pivotably connected to the first and second legs, and the second crossbeam is pivotably connected to the third and fourth legs. The first bunk is detachably attached to the first and second crossbeams, and the second bunk is detachably attached to the first and second crossbeams.
The present invention may also be embodied as a bunk mounting system for a watercraft lift comprising first, second, third, and fourth mounting locations, the bunk mounting system comprising first and second crossbeams, first, second, third, and fourth pivot connectors, and first, second, third, and fourth rail connectors. The first pivot connector pivotably connects the first crossbeam to the first mounting location. The second pivot connector pivotably connects the second crossbeam to the second mounting location. The third pivot connector pivotably connects the third crossbeam to the third mounting location. The fourth pivot connector pivotably connects the fourth crossbeam to the fourth mounting location. The first rail connector rigidly connects the first bunk to the first crossbeam. The second rail connector rigidly connects the first bunk to the second crossbeam. The third rail connector rigidly connects the second bunk to the first crossbeam. The fourth rail connector rigidly connects the second bunk to the second crossbeam.
Referring initially to
The example watercraft lift 20 comprises a frame 30 defining first and second pivot axes 32 and 34. The example pivot axes 32 and 34 are parallel to each other, and a frame reference plane F extends through the pivot axes 32 and 34. During normal use of the watercraft lift 20, the example frame reference plane is substantially horizontal.
The example frame 30 supports first and second support assemblies 40 and 42 for rotation about the first and second pivot axes 32 and 34, respectively. The example first support assembly 40 comprises first and second leg assemblies 50 and 52, and the example second support assembly 42 comprises third and fourth leg assemblies 54 and 56. The example leg assemblies 50, 52, 54, and 56 are adjustable in length, but the present invention may be implemented using different configurations of the support assemblies and non-adjustable leg assemblies.
An actuator assembly 60 is operatively connected between the first and second support assemblies 40 and 42. In the example watercraft lift 20, operation of the actuator assembly 60 causes the first and second support assemblies 40 and 42 to pivot about the first and second pivot axes 32 and 34. In particular, a piston rod 62 of the actuator assembly 60 is connected to the first support assembly 40 above the reference plane, and a cylinder 64 of the actuator assembly 60 is connected to the second support assembly 42 below the reference plane.
The frame 30 is configured to rest on a bed (not shown) of a body of water (not shown). Extension of the rod 62 out of the cylinder 64 causes the support assemblies 40 and 42 to pivot away the frame 30, and retraction of the rod 62 into the cylinder 64 causes the support assemblies 40 and 42 to pivot towards the frame 30.
The example watercraft lift 20 comprises first and second bunk assemblies 70 and 72. Each of the bunk assemblies 70 and 72 comprises a rail 80 and a pad 82. The rails 80 are sized, dimensioned, and configured to extend between the first and second support assemblies 40 and 42 and to support a watercraft (not shown). The pads 82 are supported by the rails 80 to define a resilient surface that comes into contact with the supported watercraft to reduce the likelihood of damage to the watercraft lift 20 and/or watercraft when the watercraft is loaded onto, unloaded from, or supported by the watercraft lift 20.
Accordingly, when the support assemblies 40 and 42 are pivoted away from the frame 30 (e.g.,
As perhaps best shown in
The example rail connecting assemblies 126 rigidly support the rails 80 such that the bunk assemblies 70 and 72 extend between the crossbeams 120 and 122. In particular, the rail connecting assemblies 126 rigidly connect the rails 80 to the first and second crossbeams 120 and 122. The pivot connecting assemblies 124 allow the first and second crossbeams 120 and 122 to pivot relative to the support assemblies 40 and 42 as the actuator assembly 60 rotates the support assemblies 40 and 42 between the fully raised (
Referring now to
The example crossbeams 120 and 122 are the same, and only the example crossbeam 120 will be described herein in detail. However, it should be understood that the crossbeams 120 and 122 need not be the same to implement the principles of the present invention.
The inner sections 134 and 136 of the crossbeams 120 and 122 thus take the form of a V, with the outer sections 130 and 132 extending laterally outwardly from the outer ends of the V formed by the inner sections 134 and 136. In use, the inner sections 134 and 136 are arranged to provide clearance for a V-shaped hull of the watercraft, and the outer sections 130 and 132 extend laterally from the centerline of the watercraft to accommodate a desired configuration of bunk assemblies 70 and 72. The outer sections 130 and 132, which extend laterally from the centerline of the watercraft, are further configured to accommodate a desired configuration of accessories as will be described in further detail below.
Referring now to
In use, the pivot openings 146 and 148 are aligned with support openings not visible in one of the leg assemblies 50, 52, 54, and 56 (the leg assembly 50 is shown in
More specifically, the pivot pin 144 allows the crossbeams 120 and 122 to remain such that the V defined by the inner portions 134 and 136 is pointed down during movement of the support assemblies 40 and 42 between the fully raised and fully lowered positions. When the support assemblies 40 and 42 are in the lower positions and during movement of the support assemblies 40 and 42 from the lower position to the upper position as shown in
Other pivot connecting assemblies may be used in addition to or instead of the example connecting assemblies 124 when implementing the principles of the present invention.
Referring now to
With the U-bolt 160 extending around the crossbeam 120 and through the holes in the connecting plate 162, the nuts 164 are engaged with the U-bolt 160 and tightened such that the U-bolt 160 clamps the crossbeam 120 to the underside of the rail 80. This clamping force inhibits relative movement of the rail 180 relative to the crossbeam 120 during normal use of the example watercraft lift 20. To adjust a location of the rails 80 relative to the crossbeams 120 and 122, the nuts 164 may be loosened to release the clamping force, the rails 80 are slid into the desired position relative to the crossbeams 120 and 122, and the nuts 164 are tightened reapply the clamping force. For certain adjustments (e.g., one side of the leg assembly to the other), it may be necessary to remove the U-bolt 160 from the connecting plate 162.
In place of the U-bolt 160, a straight bolt may be used, in which case the straight bolt would be inserted through holes holes formed in the crossbeams 120 and 122 and the rails 80. The holes in the crossbeams 120 and 122 would define the positions at which the rails 80 may be fixed relative to the crossbeams 120 and 122.
In addition, the connecting plate 162 may be rigidly attached to the rail 80 at any one of a continuum or a plurality of locations along the rail channel 166. The example rail connecting assemblies 126 thus allows the rail 80 to be moved forward and aft relative to the crossbeams 120 and 122 such that the rails 80 are in a desired position relative to the crossbeams 120 and 122 based on a configuration of the boat (not shown) supported by the watercraft lift 20. Based on the characteristics of the load (e.g., boat), a desired position of the rails 80 relative to the crossbeams 120 and 122 is determined. The desired forward/aft position of the rails 80 relative to the crossbeams 120 and 122 thus allows further adjustment of the position of the load (e.g., boat) on the rails 80 relative to the crossbeams 120 and 122.
Further, as shown in
Other rail connecting assemblies may be used in addition to or instead of the example rail assemblies 126 when implementing the principles of the present invention.
Turning now to
This application claims benefit of U.S. Provisional Application Ser. No. 62/449,100 filed Jan. 22, 2017, the contents of which are incorporated herein by reference.
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