Floating watercraft lift apparatus and method

Information

  • Patent Grant
  • 6823809
  • Patent Number
    6,823,809
  • Date Filed
    Monday, March 18, 2002
    22 years ago
  • Date Issued
    Tuesday, November 30, 2004
    19 years ago
Abstract
The present invention is generally directed to a floating watercraft lift capable of raising and lowering a watercraft, and more particularly to a floating watercraft lift. In one embodiment, the watercraft lift includes a pair of longitudinally extending and approximately parallel floats with an apparatus for supporting and lifting the watercraft positioned between the floats. When the watercraft lift is positioned in a lowered position, the apparatus is submerged and each of the floats is in a first orientation and partially submerged. The apparatus may then be activated to move the watercraft lift to a raised position by moving the floats downwardly and inwardly towards the watercraft, so that the floats become further submerged in the water. The buoyancy of the submerging floats thus lifts the lift apparatus and the watercraft above the water surface.
Description




TECHNICAL FIELD




This invention generally relates to lifts for watercraft, and more particularly, to floating watercraft lifts capable of raising and lowering a watercraft.




BACKGROUND OF THE INVENTION




A watercraft may encounter a variety of problems when a hull of the watercraft remains submerged in a lake, or other body of water, for a protracted period of time. For example, the watercraft may be subjected to significant physical damage when the hull is exposed to strong wave activity resulting from weather conditions or the wakes of passing watercraft. This damage generally occurs where the hull of the watercraft repeatedly contacts a stationary object such as a portion of a dock, floating debris, or even another watercraft that is docked nearby. Further, while the watercraft hull remains in the water, the exterior hull surfaces of the watercraft may acquire significant amounts of marine growth that may impair the performance of the watercraft, and superficially damage the hull surfaces if not frequently removed.




In response to these difficulties, watercraft lifting devices have been developed that generally include a user-actuated mechanical lifting mechanism that is positioned below the watercraft to lift it from the water and support it above the surface of the water when the watercraft is not in use. When it is desired to refloat the watercraft, the user is able to release the mechanical lifting mechanism to lower the watercraft into the water. The watercraft lift is therefore a particularly convenient solution to the foregoing difficulties, since the watercraft may be quickly removed from the water during periods of non-use, and refloated when desired, with minimal human effort.




One category of known watercraft lifts include a mechanical lifting mechanism that is attached to a support platform having columns, or other supports, that that extend downwardly from the platform to the bottom of a body of water. When the watercraft is supported by the lifting mechanism, the resulting load is transferred from the lifting mechanism to the bottom by the columns attached to the support platform. U.S. Pat. No. 4,895,479, for example, describes a watercraft lift that includes a lifting mechanism that is positioned below the water surface that is supported by a plurality of posts that are anchored to the bottom. Similarly, U.S. Pat. No. 5,184,914 also describes a lift having a submerged lifting mechanism supported above the bottom by a plurality of posts that are attached to the bottom.




One disadvantage present in this category of watercraft lifts is that they require that the watercraft lift be maintained in a fixed location, since the column supports are driven into the bottom of the body of water, or are otherwise attached to fixed anchor positions located on the bottom. Further, watercraft lifts that are attached to the bottom generally cannot accommodate significant water level variations that may exist in the body of water. Such variations in water level may be due, for example, to tidal activity if the water craft is maintained in a marine environment, or due to the storage or release of water from a nearby dam if the watercraft is maintained in a lake or river adjacent to the dam.




Another category of watercraft lifts includes one or more enclosed chambers that may be selectively inflated to lift the watercraft from the water surface. For example, U.S. Pat. No. 5,860,379 describes a watercraft lift having air chambers fabricated from a flexible, impermeable fabric that are positioned beneath the watercraft. A network of hoses and valves connects an air inflation device to the enclosed chambers. As inflation air is provided to the enclosed chambers, water is expelled from the chambers thus lifting the watercraft from the water surface. A similar watercraft lift is described in U.S. Pat. No. 4,750,444, which includes a platform for supporting the watercraft that has a downwardly extending lifting skirt having an open bottom that is connected to an air inflation device. By providing inflation air to the skirt, the platform that supports the watercraft may be raised above the water surface.




Although the operation of the foregoing watercraft devices is not generally limited by water level variations, other disadvantages nevertheless exist. For example, in order to provide sustained support for the watercraft, the inflation chambers must be capable of sealably containing the inflation air for prolonged periods of time. If the inflation chambers or the inflation system cannot sealably contain the inflation air, the watercraft will not be maintained in an elevated position above the water surface.




Still another category of watercraft lifts include one or more sealed floatation chambers that are moveable relative to the watercraft to raise and lower the watercraft. For example, U.S. Pat. No. 5,131,342 discloses a watercraft lift having a pair of spaced-apart floatation chambers with watercraft support beams positioned between the floatation chambers. The floatation chambers are translated in a vertical direction to partially raise and lower the watercraft. In order to fully submerge the support beams to receive the watercraft, however, the floatation chambers must be at least partially flooded with water. Correspondingly, when the watercraft lift is to raise the watercraft, water must be pumped from the floatation chambers to establish sufficient buoyancy to lift the watercraft from the water. Since the foregoing device is unable to effect a sufficient change in buoyancy by mechanically re-positioning the floats, it is therefore subject to the shortcomings described above since it relies on sealably containing inflation air within floatation chambers.




Accordingly, there is a need in the art for a watercraft lift to support a watercraft that is not limited by variations in water depth, and does not require support from the bottom of a body of water. Further, there is a need for a watercraft lift that does not require floatation chambers that must be inflated with air and/or flooded with water in order to develop sufficient changes in buoyancy to raise and lower the watercraft.




SUMMARY OF THE INVENTION




The present invention is generally directed to a floating watercraft lift capable of raising and lowering a watercraft, and more particularly to a floating watercraft lift that does require support from a bottom of a body of water and is capable of operation in water that may vary in depth. The watercraft lift may be positioned in a standard-sized boat slip, as well as in double-wide slips, where two such lifts may be used side by side, or only one lift may be used without impeding the berthing of a second watercraft in the slip. The watercraft lift may also be used separate from a slip or fixed dock, and may be anchored to a buoy, or other mooring devices, and may be conveniently and easily relocated to different locations when desired.




In one aspect of the invention, the watercraft lift includes a pair of longitudinally extending and approximately parallel floats with an apparatus for supporting and lifting a watercraft extending between the floats. When the watercraft lift is positioned in a lowered position, the apparatus is submerged and each of the floats is in a first orientation and partially submerged. When the watercraft enters the watercraft lift, it may be guided onto the lift by a pair of at least partially submerged and longitudinally extending bunks that extend lengthwise on either side of the watercraft. When the watercraft has moved a sufficient distance along the length of the lift, the watercraft contacts the bunks. The apparatus may then be activated to move the watercraft lift to a raised position. The apparatus moves the floats downwardly and inwardly towards the watercraft, so that the floats become further submerged in the water. The buoyancy of the submerging floats thus lifts the lift apparatus and the watercraft above the water surface.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is an isometric view of a watercraft lift according to an embodiment of the invention.





FIG. 2

is a partial isometric view of an under side of a watercraft lift according to an embodiment of the invention.





FIG. 3

is an end view of a watercraft lift according to an embodiment of the invention.





FIG. 4

is another end view of a watercraft lift according to an embodiment of the invention.





FIG. 5

is still another end view of a watercraft lift according to an embodiment of the invention.





FIGS. 6A through 6C

are partial cross sectional views of a watercraft lift according to an embodiment of the invention.





FIG. 7

is a block diagram of a power supply system for a watercraft lift according to another embodiment of the invention.





FIG. 8

is an isometric view of a power module according to still another embodiment of the invention.











DETAILED DESCRIPTION OF THE INVENTION




The present invention is directed to lifts for watercraft, and more particularly, to a floating watercraft lift capable of raising and lowering a watercraft. Many of the specific details of certain embodiments of the invention are set forth in the following description and in

FIGS. 1 through 8

to provide a thorough understanding of such embodiments. One skilled in the art will understand, however, that the present invention may be practiced without several of the details described in the following description. In the following description of the embodiments, it is understood that a watercraft includes any vehicle that is at least partially waterborne, which may include boats or like vessels, and may also include amphibious vehicles including various amphibious automobiles or aircraft. Moreover, in the description that follows, it is understood that the figures related to the various embodiments are not to be interpreted as conveying any specific or relative dimension, and that specific or relative dimensions, if stated, are not to be considered limiting unless the claims expressly state otherwise.





FIG. 1

is an isometric view of a watercraft lift


10


according to an embodiment of the invention. The watercraft lift


10


includes a pair of spaced apart, longitudinally-extending floats


11


that are approximately parallel to a longitudinal axis


12


. The floats


11


may be comprised of a sealed and enclosed structure formed from a rigid and corrosion-resistant material, such as a rigid polymer, aluminum, or other like materials. The floats


11


may have a hollow interior volume to provide buoyancy when partially submerged in water. Alternatively, the floats


11


may include a material within the interior volume having a specific density less than that of water. For example, the internal volume of the floats may include a foamed polymeric material that at least partially occupies the internal volume of the floats


11


.




Still referring to

FIG. 1

, the floats


11


are further approximately rectangular in cross section, having a first cross sectional dimension


16


that extends along a first cross sectional axis “A” and a second cross sectional dimension


17


that extends along a second cross sectional axis “B” that is substantially perpendicular to the first cross sectional axis “A”, with the first dimension


16


being generally greater than a second dimension


17


. The cross-section of the floats


11


may also include reduced cross-section portions


18


that significantly reduce the buoyancy afforded by the floats


11


by reducing the interior volume of the floats


11


. Thus, when the floats


11


are moved from a position as shown in

FIG. 1

, where the floats


11


are oriented with the axis “A” in a horizontal position, to a vertical position where the axis “A” is oriented in a vertical position (not shown in FIG.


1


), the reduced cross-section portion


18


will generally be submerged below a water surface, and provide less buoyancy to the lift


10


, so that the lift


10


will generally extend further below the water surface due to the decreased buoyancy.




With reference still to

FIG. 1

, the watercraft lift


10


further includes a lifting structure


13


that is positioned between the floats


11


that is configured to receive and support a watercraft. The lifting structure


13


may include a pair of longitudinally-extending and spaced-apart bunks


14


that define support points for the watercraft. The bunks


14


may be angled upwardly and inwardly as they extend from a rear portion to a forward portion of the watercraft lift


10


to additionally provide a stop mechanism for the watercraft by contacting a hull portion of the watercraft once the watercraft is suitably positioned on the watercraft lift


10


. The floats


11


may further include inwardly projecting cut-out portions


6


where the lifting structure


13


is mechanically coupled to the floats


11


. A pair of generally upwardly-extending upright members


19


may also be attached to the lifting structure


13


. The upright members


19


present visually prominent features to an operator of the watercraft that may assist the operator in locating the lift


10


prior to positioning the watercraft in the watercraft lift


10


. Further, the upright members


19


may further assist the operator in guiding the watercraft into position between the floats


11


.




Turning now to

FIG. 2

, an isometric view of the underside of the watercraft lift


10


is shown. For clarity of illustration, the watercraft lift


10


as shown in

FIG. 2

depicts the watercraft lift


10


configured in a position to receive a watercraft


15


. Other positions for the watercraft lift


10


will be described in greater detail below. The lifting structure


13


includes a pair of longitudinally-extending side beams


20


that are generally parallel to the longitudinal axis


12


. One end of each of the side beams


20


are coupled to a laterally-extending front cross-beam


21


, with the opposing ends of the side beams


20


each coupled to a laterally-extending rear cross-beam


22


to form a substantially rectangular frame. One or more diagonal braces


9


may positioned within the rectangular frame to further reinforce the frame. A center beam


29


extends between the side beams


20


, and is positioned approximately at a mid-length between the front cross beam


21


and the rear cross beam


22


. The front cross beam


21


further includes a pair of opposing ends


25


that extend generally outwardly from the rectangular structure. The ends


25


each further include a rotatably-mounted rollers


26


. Similarly, the rear cross beam


22


includes a pair of opposing ends


27


that also extend generally outwardly from the rectangular structure that each include rotatably-mounted rollers


28


. The rollers


26


and


28


engage surface portions of the floats


11


during the operation of the watercraft lift


10


, as will be described in greater detail below. Accordingly, the surface portions of the floats


11


that are contacted by the rollers


26


and


28


may have roller plates (not shown in

FIG. 2

) positioned on the surface portions of the floats


11


to locally reinforce the affected surface portions of the floats


11


, and to generally guide the rollers


26


and


28


as they engage the floats


11


. A front V-beam


23


is positioned on the side beams


20


proximate to the front cross beam


21


, and a rear V-beam


24


is similarly positioned on the side beams


20


proximate to the rear cross beam


22


. The front V-beam


23


and the rear V-beam


24


may support a pair of longitudinally-extending bunks


14


, as earlier described. The front V-beam


23


and the rear V-beam


24


further include rotation points


39


positioned at opposing ends of the front V-beam


23


and the rear V-beam


24


.




Referring still to

FIG. 2

, a pair of lift arm structures


30


are rotatably coupled to the front V-beam


23


and the rear V-beam


24


at the rotation points


39


so that each lift arm structure


30


is rotatable relative to the front V-beam


23


and the rear V-beam


24


about an axis


38


that projects through the rotation points


39


. Each lift arm structure


30


includes a longitudinally extending beam


31


that is joined at one end to a forward lift arm cross beam


32


and at an opposing end to a rear lift arm cross beam


33


. The lift arm structure


30


may be rotatably coupled to the floats


11


at a forward float clevis


35


and a rear float clevis


36


so that the floats


11


are rotatable relative to the lift arm structure


30


about an axis


41


that projects through the forward clevis


35


and the rear clevis


36


. A pair of actuators, shown herein as a hydraulic cylinders


37


extend between the center beam


29


and a rotatable connection


34


proximate to the mid-length of the lift arm structure


30


. Alternatively, the cylinders


37


may extend between the center beam


29


and the floats


11


, with the cylinders


37


being rotatably coupled to the floats


11


. Each cylinder


37


provides a linear actuation force that rotates the lift arm structure


30


about the rotational axis


38


, so that the floats


11


may be positioned in an orientation where the cross-sectional axis “A” is oriented substantially vertically, as shown in

FIG. 2

, or to position the floats


11


in an orientation wherein the axis “A” is oriented substantially horizontally, as shown in FIG.


1


. Although hydraulic cylinders


37


are shown, other means for imparting linear actuation may also be used. For example, a screw jack or a pneumatic cylinder may be used instead of the hydraulic cylinders


37


. Still other devices may be used to controllably rotate the lift arm structure


30


about the axes


38


. For example, a winch system that employs cables attached to the floats


11


to position the floats


11


relative to the lifting structure


13


may also be used.




With reference now to

FIGS. 3 through 5

, the operation of the watercraft lift


10


will be described in detail.

FIG. 3

is an end view of the watercraft lift


10


that is configured in a fully lowered position to receive the watercraft


15


. As discussed previously, when the watercraft lift


10


is positioned in the lowered position, the floats


11


are positioned with the axis “A” oriented in a substantially vertical orientation, which provides generally reduced buoyancy for the watercraft lift


10


, due to the rectangular cross section of the floats


11


, and further due to the reduced cross-sectional portions


18


of the floats


11


. Consequently, the lifting structure


13


is positioned sufficiently below a waterline


40


so that the watercraft


15


may be positioned above the bunks


14


. As the watercraft


15


proceeds into the watercraft lift


10


, it may be guided by the floats


11


, which are generally partially visible above the water surface


40


. As the watercraft


15


continues to move forward, the hull of the watercraft


15


may contact a portion of the bunks


14


, since the bunks


14


may be angled upwardly and inwardly as they extend from a rear portion of the watercraft lift


10


to a forward portion of the lift


10


. The bunks


14


may thus assist a watercraft operator in positioning the watercraft


15


onto the lifting structure


13


by centering the hull of the watercraft


15


between the floats


11


and by at least partially arresting the forward motion of the watercraft


15


by providing resistance against the hull of the watercraft


15


. With the watercraft


15


is positioned over the lifting structure


13


and between the floats


11


as shown, the lift assemblies


30


generally extend outwardly from the lifting structure


13


, with the cylinders


37


in a filly extended position. The watercraft


15


may now be lifted by actuating a power supply system (not shown) that is coupled to the cylinders


37


. The power supply system will be described in greater detail below.




Referring now to

FIG. 4

, an end view of the watercraft lift


10


is shown that depicts the watercraft lift


10


configured in an intermediate position between a fully lowered position (as shown in

FIG. 3

) and a fully raised position (as shown in FIG.


1


). Actuation of the aforementioned power supply system (not shown) causes the cylinders


37


to linearly retract inwardly, thus causing the lift arm structures


30


to rotate about the axes


38


in a direction


42


. As the lift arm structures


30


are rotated, the floats


11


are moved downwardly and inwardly towards the lifting structure


13


through a combination of a rotational movement of the floats


11


relative to the lifting arm structure


30


about the axis


41


that extends through the clevis


36


and the clevis


35


(as shown in FIG.


2


), and a translation of the floats


11


relative to the lifting structure


13


so that the axis “A” progressively moves toward a horizontal orientation that is generally parallel to the waterline


40


, while the axis “B” moves progressively towards a vertical orientation. As the floats


11


are moved, a greater portion of the internal volume of each of the floats


11


is submerged below the waterline


40


, resulting in increased buoyancy for the watercraft lift


10


. Consequently, the front V-beam


23


(as shown in

FIG. 2

) and the rear V-beam


24


are elevated to position the bunks


14


against the hull of the watercraft


15


and lift the watercraft


15


above the waterline


40


.




Still referring to

FIG. 4

, the rollers


26


(as shown in

FIG. 2

) attached to the front cross-beam


21


(also as shown in

FIG. 2

) and the rollers


28


attached to the rear cross-beam


22


engage surface portions of the floats


11


. As described earlier, roller plates


44


may be positioned on the floats


11


to reinforce the area contacted by the rollers


26


and


28


, and to further guide the rollers


26


and


28


as they move across the floats


11


in a direction


8


. The rollers


26


and


28


thus generally assist in rotating the floats


11


about the axis


41


while the cross beam


33


of the lift arm structure


30


draws the floats


11


inwardly in a direction


7


. Although the present embodiment includes rollers


26


and


28


rotatably coupled to the front cross beam


21


and the rear cross beam


22


, respectively, other means are available for engaging the surface portions of the floats


11


. For example, the rollers


26


and


28


may be replaced by sliding members positioned on the front cross beam


21


and the rear cross beam


22


that slide across the surface portions of the floats


11


. Still further, rollers may be rotatably mounted in the surface portions of the floats


11


that allow the sliding members to smoothly translate across the surface portions of the floats


11


.




Turning now to

FIG. 5

, an end view of the watercraft lift


10


is shown with the watercraft lift


10


configured in the fully raised position. The lift arm structures


30


are fully rotated inwardly towards a center of the lifting structure


13


, and may abut a portion of the floats


11


. The rollers


26


attached to the front cross-beam


21


(as shown in

FIG. 2

) and the rollers


28


attached to the rear cross-beam


22


rest on the floats


11


to generally maintain the floats


11


in a horizontal position. Further, when the watercraft lift


10


is configured in the fully raised position, the axis “A” is oriented in a substantially horizontal direction that is parallel to the surface


40


, while the axis “B” is oriented in a substantially vertical direction that is perpendicular to the surface


40


. With the floats


11


positioned as shown, the floats


11


are more stable because a larger portion of the cross sectional area of the floats


11


is situated at the waterline when the axis “A” is oriented in the horizontal position.




The foregoing operating description of the watercraft lift


10


illustrates a significant advantage afforded by the watercraft lift


10


. When the watercraft lift


10


is configured in the fully lowered position, as best shown in

FIG. 3

, the axis “A” of each of the floats


11


is oriented in a substantially vertical direction. Since the longest cross sectional dimension of the float


11


generally exists along the axis “A”, the watercraft lift


10


has a relatively narrow overall width when positioned in the fully lowered position. Moreover, when the watercraft lift


10


is configured in the fully raised position, as best shown in

FIG. 5

, and the axis “A” of each of the floats


11


is oriented in a substantially horizontal direction, the floats


11


are positioned substantially beneath the watercraft


15


, so that the watercraft lift


10


still maintains a relatively narrow overall width. Accordingly, the watercraft lift


10


may be advantageously accommodated and operated in narrow locations, such as narrow single watercraft slips, or other narrow mooring locations.




Still other advantages are apparent in the foregoing embodiment. For example, and still referring to

FIG. 5

, the downwardly-sloping surface


100


of the floats


11


advantageously permits the watercraft lift


10


to develop an over-center locking feature when the rollers


26


and


28


rest on the surface


100


, as shown. With reference now to

FIGS. 6A

to


6


C, this feature will be described in greater detail.





FIG. 6A

is a partial cross sectional view of the floats


11


as the watercraft lift


10


is moved through an intermediate position between the fully lowered position (as shown in FIG.


3


), and a fully raised position (as shown in FIG.


5


). At the intermediate position shown, the axis “A” of the floats


11


are relatively steeply inclined relative to the horizontal, as determined by the surface


40


. At the position shown in

FIG. 6A

, the rollers


26


coupled to the front cross beam


21


, and the rollers


28


coupled to the rear cross beam


22


rotatably engage a portion of the surface


100


of the floats


11


, and move onto the surface


100


in the direction


8


, while the front clevis


35


and the rear clevis


36


move in the direction


7


due to the inwardly directed movement of the lift arm cross beams


32


and rear lift arm cross beams


33


. As previously described, roller plates


44


may be positioned on the floats


11


to guide the rollers


26


and


28


, and to reinforce the surface of the float


1


contacted by the rollers


26


and


28


.




Referring now to

FIG. 6B

, a partial cross sectional view of the floats


11


as the watercraft lift


10


is moved further towards the fully raised position is shown (as best seen in FIG.


5


). As shown, the rollers


26


and


28


continue to move onto and across the surface


100


in the direction


8


as the front clevis


35


and the rear clevis


36


continue to move inwardly in the direction


7


. As the floats


11


continue to move, the axis “A” is moved to a less steeply inclined angle relative to the surface


40


.




Turning now to

FIG. 6C

, a partial cross sectional view of the floats


11


is shown when the watercraft lift


10


is positioned in the fully raised position (as shown in FIG.


5


). The axis “A” is now oriented substantially in a horizontal direction relative to the surface


40


, and the surface


100


of the floats


11


extends downwardly at an angle


110


relative to the horizontal. A downwardly directed force vector


120


, which arises from the weight of the watercraft and the lifting structure is transferred from the rollers


26


and


28


to the floats


11


. As shown in

FIG. 6C

, the force vector


120


consists of a downwardly and inwardly directed first component


130


, and an outwardly and downwardly directed second component


140


that cooperatively act to maintain the floats


11


in a stable and locked horizontal position when the lift


10


is in the fully raised position. Accordingly, the over-center feature advantageously maintains the watercraft lift


10


in the raised position without the participation of a latching mechanism, or other similar devices. Still further, since the load applied by the watercraft to the watercraft lift is advantageously transferred to the floats


11


through both the rollers


26


and


28


and through the float devises


35


and


36


, greater stability is attained, which further advantageously permits the floats


11


to be utilized as a walkway for persons entering or leaving the watercraft.





FIG. 7

is a block diagram of a power supply system


50


according to another embodiment of the invention. The system


50


includes a power module


52


that may be remotely positioned on a dock that is adjacent to the watercraft lift


10


. An embodiment of a power module


52


that may be remotely positioned will be described in greater detail below. Although the system


50


depicted in

FIG. 7

shows the module


52


operatively coupled to hydraulic cylinders


37


, it is understood that other linear actuation devices may be employed, as discussed more fully above. The module


52


generally includes a hydraulic pump


54


that exchanges a hydraulic fluid with a reservoir


55


, and is capable of delivering the fluid under pressure to the cylinders


37


through a solenoid-actuated up valve


56


when the cylinders


37


are being extended. A solenoid-actuated down valve


57


may be actuated to release pressurized fluid from the cylinders


37


when the cylinders


37


are being retracted. A flow control valve


58


may be included to control the rate at which the cylinders


37


are extended or retracted. The pump


54


is further coupled to a direct current (DC) motor


59


that receives current from a DC power source, such as a battery


60


. The battery


60


may be electrically coupled to the DC motor through a solenoid relay


61


, or other power relay devices. The battery


60


may further be electrically coupled to a solar panel


62


that is capable of electrically replenishing the battery


60


when the panel


62


is exposed to solar radiation. Alternatively, the pump


54


may be coupled to an alternating current (AC) motor


63


that is electrically coupled to an AC power source


64


.




Still referring to

FIG. 7

, the module


52


further includes a control unit


65


that is operatively coupled to the up valve


56


, the down valve


57


, and the solenoid relay


61


to control the operation of these elements. The control unit is further coupled to a limit switch assembly


69


to provide a feedback signal to the control unit


65


that provides an indication signal to the control unit


65


that the watercraft lift is in the fully lowered position, or alternatively, in the fully raised position. The control unit


65


further includes a receiver portion (not shown) that is capable of receiving wireless signals from a remote transmitter


66


. The control unit


65


may optionally be coupled to other devices, such as underwater lights


67


that may assist the watercraft operator in positioning the watercraft in the lift


10


during periods of darkness or low visibility, or to power unit lights


68


that may be used to illuminate a portion of the dock supporting the module


52


.




With reference still to

FIG. 7

, the operation of the power system


50


will now be briefly described. When the watercraft operator approaches the watercraft lift, the operator actuates the remote transmitter


66


to emit a wireless signal that is received by the receiver portion of the control unit


65


to command the watercraft lift to move to the lowered position, and otherwise prepare the watercraft lift


10


to receive the watercraft, which may include, for example, energizing any of the lighting systems previously described, in addition to commanding the valves


56


and


57


to move to appropriate positions for lowering the watercraft. The control unit


65


may then command the DC motor


59


to operate by commanding the solenoid relay


61


to move to a closed position. Alternatively, the control unit


65


may cause the AC motor


63


to operate by electrically coupling the AC motor


63


to the AC source


64


. In either case, the pump


54


is able to generate sufficient fluid pressure to move the cylinders


51


to the extended position. When the watercraft lift is in the fully lowered position, the limit switch assembly


69


transfers a signal to the unit


65


that indicates that the watercraft lift is in the lowered position, and the unit


65


interrupts the current to the DC motor


59


(or alternatively, the AC motor


63


). After the watercraft is suitably positioned on the watercraft lift, the operator again actuates the remote transmitter


66


to emit a signal that is received by the receiver portion of the control unit


65


to command the watercraft lift to move to the raised position. The valves


56


and


57


are moved to positions appropriate for lifting the watercraft, and the DC motor


59


(or alternatively, the AC motor


63


) is again energized. When the watercraft lift is in the fully raised position, the limit switch assembly


69


again transfers a signal to the control unit


65


, which in turn, again interrupts the current to the DC motor


63


.





FIG. 8

is an isometric view of a power module


70


according to another embodiment of the invention. The power module


70


includes a hydraulic power unit


74


having an integral DC motor that is capable of exchanging hydraulic fluid with the cylinders


37


(as shown in

FIG. 7

) through a plurality of hydraulic hoses


72


. The unit


74


is electrically coupled to a battery


73


and to a control unit


75


. A receiver


74


is operatively coupled to the control unit


75


in order to receive wireless signals transmitted by a hand held unit


77


. The module


70


may be enclosed (with the exception of the unit


77


) in a substantially weather proof cabinet


76


.




The above description of illustrated embodiments of the invention is not intended to be exhaustive or to limit the invention to the precise form disclosed. While specific embodiments of, and examples of, the inventions are described in the foregoing for illustrative purposes, various equivalent modifications are possible within the scope of the invention as those skilled within the relevant art will recognize. Moreover, the various embodiments described above can be combined to provide further embodiments. Accordingly, the invention is not limited by the disclosure, but instead the scope of the invention is to be determined entirely by the following claims.



Claims
  • 1. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned vertically below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water, the second end portions of the first and second lifting arms being pivotally connected to the first and second floats, respectively, at a location on the first and second floats to cause the first and second floats to rotate about the second end portions relative to the first and second lifting arms under the buoyancy forces on the first and second floats as the first and second lifting arms move between the first and second positions thereof; and at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof.
  • 2. The watercraft lift of claim 1, wherein the first and second floats each have a non-symmetrical cross-sectional shape with a first cross-sectional axis longer than a transverse second cross-sectional axis such that as the first and second lifting arms move between the first and second positions thereof the first and second floats rotate between an orientation with the first cross-sectional axis extending upward when the first and second lifting arms are in the first position, and an orientation with the first cross-sectional axis extending laterally outward when the first and second lifting arms are in the second position.
  • 3. The watercraft lift of claim 1 further including first and second float guide arms extending laterally outward from the lifting structure, the first and second float guide arms each having a first end portion rigidly connected to the lifting structure and an opposite second end portion, the second end portions of the first and second float guide arms being positioned on opposite sides of the lifting structure to engage the first and second floats, respectively, as the first and second lifting arms are moved from the first position toward the second position to rotatably guide the first and second floats into a predetermined rotational orientation when in position below the lifting structure.
  • 4. The watercraft lift of claim 3 wherein the first and second floats each have a non-symmetrical cross-sectional shape with a first cross-sectional axis longer than a transverse second cross-sectional axis such that as the first and second lifting arms are moved from the second position toward the first position the first and second floats rotate into an orientation with the first cross-sectional axis extending upward when the first and second lifting arms are in the first position, and as the first and second lifting arms are moved from the first position toward the second position the second end portions of the first and second guide arms rotatably guide the first and second floats into the predetermined orientation, the predetermined orientation having the first cross-sectional axis of each of the first and second floats extending laterally outward.
  • 5. The watercraft lift of claim 3 further including rollers rotatably mounted on the second end portions of the first and second float guide arms and positioned to rollably engage an upper surface portion of the first and second floats as the first and second lifting arms are moved from the first position toward the second position to rotatably guide the first and second floats into the predetermined orientation when in position below the lifting structure.
  • 6. The watercraft lift of claim 3 wherein the first and second floats each have an engagement portion engaged by the second end portion of the first and second guide arms, respectively, the engagement portion being oriented such that the buoyancy forces on the first and second floats cause the second end portions of the first and second guide arms to apply forces on the first and second floats, respectively, tending to move the first and second lifting arms toward the second position to lockably retain the first and second lifting arms in the second position.
  • 7. The watercraft lift of claim 1 wherein the first and second drive members comprise first and second actuators.
  • 8. The watercraft lift of claim 7 wherein the first and second actuators comprise first and second hydraulic cylinders.
  • 9. The watercraft lift of claim 7 wherein the first and second actuators comprise first and second jackscrews.
  • 10. The watercraft lift of claim 7 wherein the first and second actuators comprise first and second pneumatic cylinders.
  • 11. The watercraft lift of claim 1, further comprising a power supply system having a source of power and a remotely operable power module capable of receiving wireless signals to actuate the power module, the source of power being operatively connected to the first and second drive members to move the first and second lifting arms between the first and second positions thereof upon actuation of the power module.
  • 12. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water; at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof; and first and second float lock arms extending laterally outward from the lifting structure, the first and second float lock arms each having a first end portion rigidly connected to the lifting structure and an opposite second end portion, the second end portions of the first and second float lock arms being positioned on opposite sides of the lifting structure to engage the first and second floats, respectively, when the first and second lifting arms are moved to the second position, the first and second floats each having an engagement portion engaged by the second end portion of the first and second float lock arms, respectively, the engagement portion being arranged such that the buoyancy forces on the first and second floats cause the second end portions of the first and second float lock arms to apply forces on the first and second floats, respectively, tending to move the first and second lifting arms toward the second position to lockably retain the first and second lifting arms in the second position.
  • 13. The watercraft lift of claim 12 further including rollers rotatably mounted on the second end portions of the first and second float lock arms and positioned to rollably engage an upper surface portion of the first and second floats as the first and second lifting arms are moved from the first position toward the second position.
  • 14. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure at a pivotal connection and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned vertically below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water, the pivotal connection of the first end portions of the first and second lifting arms to the lifting structure being at locations spaced apart from the first and second floats to provide a separation between the pivotal connection and the first and second floats as the first and second lifting arms move between the first and second positions, the first end portions of the first and second lifting arms being disconnected from the first and second floats; and at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second position thereof.
  • 15. The watercraft lift of claim 14 further including first and second float lock arms extending laterally outward from the lifting structure, the first and second float lock arms each having a first end portion rigidly connected to the lifting structure and an opposite second end portion, the second end portions of the first and second float lock arms being positioned on opposite sides of the lifting structure to engage the first and second floats, respectively, when the first and second lifting arms are moved to the second position, the first and second floats each having an engagement portion engaged by the second end portion of the first and second float lock arms, respectively, the engagement portion being arranged such that the buoyancy forces on the first and second floats cause the second end portions of the first and second float lock arms to apply forces on the first and second floats, respectively, tending to move the first and second lifting arms toward the second position to lockably retain the first and second lifting arms in the second position.
  • 16. The watercraft lift of claim 14 wherein the second end portion of the first and second lifting arms are pivotally connected to the first and second floats, respectively.
  • 17. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water; at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof; and a power supply system having a source of power and a remotely operable power module capable of receiving wireless signals to actuate the power module, the source of power being operatively connected to the first and second drive members to move the first and second lifting arms between the first and second positions thereof upon actuation of the power module.
  • 18. The watercraft lift of claim 17 wherein the power supply system includes solar panel to produce electrical energy, a battery to store the electrical energy produced by the solar panel, the battery being operatively coupled to the first and second drive members to power the first and second drive members to move the first and second lifting arms.
  • 19. The watercraft lift of claim 18 wherein the first and second drive members are hydraulic actuators, and the power supply system further includes a reservoir of hydraulic fluid, a hydraulic pump connected to the reservoir and to the first and second hydraulic actuators, and a motor, operatively connected to the hydraulic pump, the motor being connected to the battery and powered by the electrical energy stored in the battery to operate the motor and cause the hydraulic pump to provide hydraulic fluid from the reservoir to the first and second hydraulic actuators to move the first and second lifting arms, whereby a self contained power supply is provided for operation of the first and second hydraulic actuators.
  • 20. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure and each having a non-symmetrical cross-sectional shape with a first cross-sectional axis longer than a transverse second cross-sectional axis; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water, the second end portions of the first and second lifting arms being pivotally connected to the first and second floats, respectively, at a location on the first and second floats to cause the first and second floats to rotate about the second end portions relative to the first and second lifting arms under the buoyancy forces on the first and second floats as the first and second lifting arms move between the first and second positions thereof, such that as the first and second lifting arms move between the first and second positions thereof the first and second floats rotate between an orientation with the first cross-sectional axis extending upward when the first and second lifting arms are in the first position, and an orientation with the first cross-sectional axis extending laterally outward when the first and second lifting arms are in the second position; and at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof.
  • 21. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water, the second end portions of the first and second lifting arms being pivotally connected to the first and second floats, respectively, at a location on the first and second floats to cause the first and second floats to rotate about the second end portions relative to the first and second lifting arms under the buoyancy forces on the first and second floats as the first and second lifting arms move between the first and second positions thereof; at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof; and first and second float guide arms extending laterally outward from the lifting structure, the first and second float guide arms each having a first end portion rigidly connected to the lifting structure and an opposite second end portion, the second end portions of the first and second float guide arms being positioned on opposite sides of the lifting structure to engage the first and second floats, respectively, as the first and second lifting arms are moved from the first position toward the second position to rotatably guide the first and second floats into a predetermined rotational orientation when in position below the lifting structure.
  • 22. The watercraft lift of claim 21 wherein the first and second floats each have a non-symmetrical cross-sectional shape with a first cross-sectional axis longer than a transverse second cross-sectional axis such that as the first and second lifting arms are moved from the second position toward the first position the first and second floats rotate into an orientation with the first cross-sectional axis extending upward when the first and second lifting arms are in the first position, and as the first and second lifting arms are moved from the first position toward the second position the second end portions of the first and second guide arms rotatably guide the first and second floats into the predetermined orientation, the predetermined orientation having the first cross-sectional axis of each of the first and second floats extending laterally outward.
  • 23. The watercraft lift of claim 21 further including rollers rotatably mounted on the second end portions of the first and second float guide arms and positioned to rollably engage an upper surface portion of the first and second floats as the first and second lifting arms are moved from the first position toward the second position to rotatably guide the first and second floats into the predetermined orientation when in position below the lifting structure.
  • 24. The watercraft lift of claim 21 wherein the first and second floats each have an engagement portion engaged by the second end portion of the first and second guide arms, respectively, the engagement portion being oriented such that the buoyancy forces on the first and second floats cause the second end portions of the first and second guide arms to apply forces on the first and second floats, respectively, tending to move the first and second lifting arms toward the second position to lockably retain the first second lifting arms in the second position.
  • 25. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water, the second end portions of the first and second lifting arms being pivotally connected to the first and second floats, respectively, at a location on the first and second floats to cause the first and second floats to rotate about the second end portions relative to the first and second lifting arms under the buoyancy forces on the first and second floats as the first and second lifting arms move between the first and second positions thereof; and at least first and second actuators connected to the lifting structure, the first actuator being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second actuator being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof.
  • 26. The watercraft lift of claim 25, wherein the first and second actuators comprise and second hydraulic cylinders.
  • 27. The watercraft lift of claim 25, wherein the first and second actuators comprise first and second jackscrews.
  • 28. The watercraft lift of claim 25, wherein the first and second actuators comprise first and second pneumatic cylinders.
  • 29. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned vertically below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water, the second end portions of the first and second lifting arms being pivotally connected to the first and second floats, respectively, at a location on the first and second floats to cause the first and second floats to rotate about the second end portions relative to the first and second lifting arms under the buoyancy forces on the first and second floats as the first and second lifting arms move between the first and second positions thereof; at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof; and a power supply system having a source of power and a remotely operable power module capable of receiving wireless signals to actuate the power module, the source of power being operatively connected to the first and second drive members to move the first and second lifting arms between the first and second positions thereof upon actuation of the power module.
  • 30. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward whereat the first and second floats are positioned laterally outward of the lifting structure and the lifting structure is sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward whereat the first and second floats are positioned below the lifting structure and the lifting structure thereby sufficiently raised to lift the watercraft out of the water; at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof; first and second float lock arms extending laterally outward from the lifting structure, the first and second float lock arms each having a first end portion rigidly connected to the lifting structure and an opposite second end portion, the second end portions of the first and second float lock arms being positioned on opposite sides of the lifting structure to engage the first and second floats, respectively, when the first and second lifting arms are moved to the second position, the first and second floats each having an engagement portion engaged by the second end portion of the first and second float lock arms, respectively, the engagement portion being arranged such that the buoyancy forces on the first and second floats cause the second end portions of the first and second float lock arms to apply forces on the first and second floats, respectively, tending to move the first and second lifting arms toward the second position to lockably retain the first and second lifting arms in the second position; and rollers rotatably mounted on the second end portions of the first and second float lock arms and positioned to rollably engage an upper surface portion of the first and second floats as the first and second lifting arms are moved from the first position toward the second position.
  • 31. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second laterally movable floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward with the first and second floats at a first lateral position laterally outward of the lifting structure and the lifting structure sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward with the first and second floats at a second lateral position laterally inward of the first lateral position and below the lifting structure and the lifting structure sufficiently raised to lift the watercraft out of the water, the second end portions of the first and second lifting arms being pivotally connected to the first and second floats, respectively, at a location on the first and second floats to cause the first and second floats to rotate about the second end portions relative to the first and second lifting arms under the buoyancy forces on the first and second floats as the first and second lifting arms move between the first and second positions thereof; and at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting am, to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof.
  • 32. The watercraft lift of claim 31 wherein the first and second floats each have a non-symmetrical cross-sectional shape with a first cross-sectional axis longer than a transverse second cross-sectional axis such that as the first and second lifting arms move between the first and second positions thereof the first and second floats rotate between an orientation with the first cross-sectional axis extending upward when the first and second lifting arms are in the first position, and an orientation with the first cross-sectional axis extending laterally outward when the first and second lifting arms are in the second position.
  • 33. The watercraft lift of claim 31 further including first and second float guide arms extending laterally outward from the lifting structure, the first and second float guide arms each having a first end portion rigidly connected to the lifting structure and an opposite second end portion, the second end portions of the first and second float guide arms being positioned on opposite sides of the lifting structure to engage the first and second floats, respectively, as the first and second lifting arms are moved from the first position toward the second position to rotatably guide the first and second floats into a predetermined rotational orientation when in position below the lifting structure.
  • 34. The watercraft lift of claim 33 wherein the first and second floats each have a non-symmetrical cross-sectional shape with a first cross-sectional axis longer than a transverse second cross-sectional axis such that as the first and second lifting arms are moved from the second position toward the first position the first and second floats rotate into an orientation with the first cross-sectional axis extending upward when the first and second lifting arms are in the first position, and as the first and second lifting arms are moved from the first position toward the second position the second end portions of the first and second guide arms rotatably guide the first and second floats into the predetermined orientation, the predetermined orientation having the first cross-sectional axis of each of the first and second floats extending laterally outward.
  • 35. The watercraft lift of claim 33 further including rollers rotatably mounted on the second end portions of the first and second float guide arms and positioned to rollably engage an upper surface portion of the first and second floats as the first and second lifting arms are moved from the first position toward the second position to rotatably guide the first and second floats into the predetermined orientation when in position below the lifting structure.
  • 36. The watercraft lift of claim 33 wherein the first and second floats each have an engagement portion engaged by the second end portion of the first and second guide arms, respectively, the engagement portion being oriented such that the buoyancy forces on the first and second floats cause the second end portions of the first and second guide arms to apply forces on the first and second floats, respectively, tending to move the first and second lifting arms toward the second position to lockably retain the first and second lifting arms in the second position.
  • 37. The watercraft lift of claim 31 wherein the first and second drive member comprise first and second actuators.
  • 38. The watercraft lift of claim 37 wherein the first and second actuators comprise first and second hydraulic cylinders.
  • 39. The watercraft lift of claim 37 wherein the first and second actuators comprise first and second jackscrews.
  • 40. The watercraft lift of claim 37 wherein the first and second actuators comprise first and second pneumatic cylinders.
  • 41. The watercraft lift of claim 31, further comprising a power supply system having a source of power and a remotely operable power module capable of receiving wireless signals to actuate the power module, the source of power being operatively connected to the first and second drive members to move the first and second lifting arms between the first and second positions thereof upon actuation of the power module.
  • 42. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second laterally movable floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward with the first and second floats at a first lateral position laterally outward of the lifting structure and the lifting structure sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward with the first and second floats at a second lateral position laterally inward of the first lateral position and below the lifting structure and the lifting structure sufficiently raised to lift the watercraft out of the water; at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof; and first and second float lock arms extending laterally outward from the lifting structure, the first and second float lock arms each having a first end portion rigidly connected to the lifting structure and an opposite second end portion, the second end portions of the first and second float lock arms being positioned on opposite sides of the lifting structure to engage the first and second floats, respectively, when the first and second lifting arms are moved to the second position, the first and second floats each having an engagement portion engaged by the second end portion of the first and second float lock arms, respectively, the engagement portion being arranged such that the buoyancy forces on the first and second floats cause the second end portions of the first and second float lock arms to apply forces on the first and second floats, respectively, tending to move the first and second lifting arms toward the second position to lockably retain the first and second lifting arms in the second position.
  • 43. The watercraft lift of claim 42 further including rollers rotatably mounted on the second end portions of the first and second float lock arms and positioned to rollably engage an upper surface portion of the first and second floats as the first and second lifting arms are moved from the first position toward the second position.
  • 44. A watercraft lift for raising and lowering a watercraft, comprising of:a lifting structure configured to receive and support the watercraft; first and second laterally movable floats positioned on opposite sides of the lifting structure; at least first and second lifting arms each having a first end portion pivotally connected to the lifting structure at a pivotal connection and an opposite second end portion connected to one of the first and second floats, the first and second lifting arms being rotatable about the first end portion relative to the lifting structure between a raised first position extending laterally outward with the first and second floats at a first lateral position laterally outward of the lifting structure and the lifting structure sufficiently submerged to receive and deploy the watercraft, and a lowered second position extending downward with the first and second floats at a second lateral position laterally inward of the first lateral position and below the lifting structure and the lifting structure sufficiently raised to lift the watercraft out of the water, the pivotal connection of the first end portions of the first and second lifting arms to the lifting structure being at locations spaced apart from the first and second floats to provide a separation between the pivotal connection and the first and second floats as the first and second lifting arms move between the first and second positions, the first end portions of the first and second lifting arms being disconnected from the first and second floats; and at least first and second drive members connected to the lifting structure, the first drive member being connected to the first lifting arm to move the first lifting arm between the first and second positions thereof, and the second drive member being connected to the second lifting arm to move the second lifting arm between the first and second positions thereof.
  • 45. The watercraft lift of claim 44 further including first and second float lock arms extending laterally outward from the lifting structure, the first and second float lock arms each having a first end portion rigidly connected to the lifting structure and an opposite second end portion, the second end portions of the first and second float lock arms being positioned on opposite sides of the lifting structure to engage the first and second floats, respectively, when the first and second lifting arms are moved to the second position, the first and second floats each having an engagement portion engaged by the second end portion of the first and second guide arms, respectively, the engagement portion being arranged such that the buoyancy forces on the first and second floats cause the second end portions of the first and second guide arms to apply forces on the first and second floats, respectively, tending to move the first and second lifting arms toward the second position to lockably retain the first and second lifting arms in the second position.
  • 46. The watercraft lift of claim 44 wherein the second end portion of the first and second lifting arms are pivotally connected to the firstand second floats, respectively.
CROSS-REFERENCE TO RELATED APPLICATION

This application claims priority to U.S. Provisional Application No. 60/276,358 filed Mar. 16, 2001.

US Referenced Citations (29)
Number Name Date Kind
17892 Ponton Jul 1857 A
87291 Richardson Feb 1869 A
123402 Janicki Feb 1872 A
3114535 Burch Dec 1963 A
3412702 Mann Nov 1968 A
3415212 Hennig Dec 1968 A
3541987 Barkley Nov 1970 A
3610192 Mauritzen Oct 1971 A
3638437 Fukuda Feb 1972 A
3657751 Shaw Apr 1972 A
3782317 Kriedt Jan 1974 A
3860982 Rumsey Jan 1975 A
3895592 King Jul 1975 A
3981259 Harper, Jr. Sep 1976 A
4072119 Williams Feb 1978 A
4092790 Sonerud Jun 1978 A
4357890 Anderson Nov 1982 A
4732102 Holman et al. Mar 1988 A
4750444 Lemvig Jun 1988 A
4763592 Russ Aug 1988 A
4841896 Fury Jun 1989 A
4895479 Michaelsen et al. Jan 1990 A
5078071 Miura Jan 1992 A
5131342 Sackett Jul 1992 A
5184914 Basta Feb 1993 A
5860379 Moody Jan 1999 A
6032601 Gates Mar 2000 A
6131528 Meek et al. Oct 2000 A
6477968 Powell Nov 2002 B2
Foreign Referenced Citations (4)
Number Date Country
3403592 Aug 1985 DE
2005603 Apr 1979 GB
62128896 Jun 1987 JP
04317885 Nov 1992 JP
Provisional Applications (1)
Number Date Country
60/276358 Mar 2001 US