This invention relates to vessel propulsion systems, and in particular to a self-contained hydraulic thruster for vessel.
Marine thrusters typically mount on barges and flat boats, and are used as propulsion for these vessels. One type of marine thruster employs a prime mover such as a diesel engine driving a hydraulic pump, together known as a “power pack”, and the resultant pressurized hydraulic fluid may be employed to drive a propeller attached to a lower unit.
There are a number of problems associated with currently available marine thrusters. Where a centrally located tiltable lower unit has been retracted and tilted backwards for storage, maintenance, cleaning, etc., the protruding upper end of the lower unit interferes with the helm and helm platform, and prevents full upward tilting of the retracted lower unit. Therefore, it would be desirable to provide a marine thruster which may be retracted and then fully tilted.
Another problem with current designs is the lack of an effective extension and retraction mechanism for lower units. It is important to be able to retract the lower unit so as to be able to more easily tilt the lower unit upwards for maintenance, storage, or transportation. A number of practical problems must be overcome to provide for an effective retraction apparatus. These include maintaining the angular orientation between cooperating telescoping sections (such as the instant shaft and tube) to allow steering, after the lower unit is extended. Another problem is providing for power assist, so as to avoid the greater work of manually extending and retracting the lower unit. Still another extension/retraction problem lies in adequately supporting the lower end of an extended lower unit, given the long resultant length of the lower unit when extended, and the resultant longer moment arm between the lower unit's mounting point at its upper end, and the propeller's location at its lower end.
Another problem with existing designs: the hydraulic fluid reservoir is disposed on the base of the marine thruster, where it is incapable of supplying enough fluid head to self-prime the power pack, and to facilitate hydraulic fluid flow to the hydraulic power pack. Thus, it would be desirable to provide a hydraulic fluid reservoir which is elevated above the level of the power pack.
Still another problem is where a marine thruster's single lower unit propeller does not supply enough power to adequately propel a vessel upon which it is mounted. It would therefore be desirable to provide a marine thruster with more than one lower unit, for increased power.
Other problems with existing designs include insufficient reinforcement at the lower unit tilt actuator attach point on the base, inadequate bearing surface at the lower unit pivot point, and excess steering motor stress.
Existing Designs
In addition, the mounting of the hydraulic fluid reservoir on the base of this design provides inadequate flow from the hydraulic fluid tank for self-priming and gravitational flow from hydraulic fluid tank to power pack.
It an object of this invention to provide a self-contained hydraulic thruster for vessel which is capable of extension, and maintaining the angular orientation between its extension components when extended. Design features allowing this object to be achieved include a steering clamp key traveling within a shaft keyway, or in the alternative, a steering clamp keyway sized to slidably admit a shaft key. Benefits associated with reaching this objective include the ability to steer a shaft by means of a steering clamp being actuated by a steering assembly or a steering actuator and tie rod.
It is another object of this invention to provide a self-contained hydraulic thruster for vessel which is easily extended and retracted. Design features allowing this object to be achieved include a lower unit actuator attached at one end to a tube, and at the other to a shaft. Benefits associated with reaching this objective include decreased operator work load, and increased convenience of operation.
It is yet another object of this invention to provide a self-contained hydraulic thruster for vessel which provides adequate support along the length of the lower unit, especially when under full power. Design features allowing this object to be achieved include an extensible shaft traveling within a tube, the length of the tube being a substantial proportion of the shaft length; in the preferred embodiment, the ratio of the length of the tube to the length of the shaft was 0.24-0.32. In addition, an optional lower support is disclosed, attached at one end to a vessel, and at the other to the shaft. Benefits associated with reaching this objective include the ability to farther extend the lower unit to accommodate greater vessel drafts, and reduced stress and consequent longer life, of the thruster components at the upper attach point of the lower unit.
It is still another object of this invention to provide a self-contained hydraulic thruster for vessel whose lower unit can be securely locked into the fully down-tilted position. Design features allowing this object to be achieved include a docking tab bore sized to admit a locking probe, and a pin bore in the locking probe sized to admit a pin. Benefits associated with reaching this objective include greater security that the lower unit will remain tilted down throughout all operating regimes, including all steering angles, and the consequent increased control and safety in operation of a vessel to which the hydraulic thruster for vessel is mounted.
It is another object of the present invention to provide a self-contained hydraulic thruster for vessel whose lower unit(s) may be retracted and tilted up without interference from the helm platform. Design features allowing this object to be accomplished include at least one lower unit mounted at an end of a lower unit mounting tube, the lower unit being laterally offset from a steering platform. Advantages associated with the accomplishment of this object include more efficient lower unit stowing for storage and/or transportation, greater tilt achievable (close to 90 degrees), the ability to tilt the propellers and lower unit completely out of the water for servicing and cleaning, decreased corrosion due to the ability of getting the lower units and propellers completely out of the water when not in use to reduce corrosion, and greater retraction of the lower unit.
It is still another object of this invention to provide a self-contained hydraulic thruster for vessel whose lower units pivot smoothly and easily within respective lower unit bores in lower unit housings. Design features enabling the accomplishment of this object include at least one bushing inside a lower unit bore, and a lower unit bushing bore sized to slidably admit a lower unit. Advantages associated with the realization of this object include easier and smoother steering, and less force required to accomplish same.
It is another object of the present invention to provide a self-contained hydraulic thruster for vessel which is stable and well-supported on a vessel to which it is mounted. Design features allowing this object to be accomplished include a base having at least one base foot attached to a rear side of the base, with a base foot reinforcement plate and base foot center spar in the base foot. Benefits associated with the accomplishment of this object include better support for the self-contained hydraulic thruster for vessel, and greater operator security.
It is still another object of this invention to provide a self-contained hydraulic thruster for vessel whose steering is reliable and long-lived. Design features enabling the accomplishment of this object include a steering motor driving a drive gear through an overhung load adaptor. Advantages associated with the realization of this object include smoother steering function, longer-lived steering motor, and the associated reduced motor maintenance and replacement costs.
It is another object of the present invention to provide a self-contained hydraulic thruster for vessel with an elevated hydraulic fluid reservoir. Design features allowing this object to be accomplished include a hydraulic fluid reservoir mounted on a helm platform which is elevated a substantial height above a base to which a hydraulic power pack is mounted. Benefits associated with the accomplishment of this object include power pack self-priming, and facilitated hydraulic fluid flow from the hydraulic fluid reservoir to the hydraulic power pack.
It is yet another object of this invention to provide a self-contained hydraulic thruster for vessel which is economical to build. Design features allowing this object to be achieved include the use of components made of readily available materials, and commercially available components such as an existing steering motor, overhung load adapter, hydraulic actuator, hydraulic power pack, hydraulic fluid reservoir, lower unit, propeller, steering gear, drive gear, and hydraulic lines. Benefits associated with reaching this objective include reduced cost, and hence increased availability.
The invention, together with the other objects, features, aspects and advantages thereof will be more clearly understood from the following in conjunction with the accompanying drawings.
Twenty sheets of drawings are provided. Sheet one contains
Sheet eleven contains
This disclosure is based upon, and builds on, parent disclosure U.S. utility application Ser. No. 11/999,531 filed Dec. 6, 2007 entitled Self-Contained Hydraulic Thruster for Vessel, which is hereby incorporated by reference into this disclosure. Drawing sheets 1-10 containing
It is desirable to locate hydraulic fluid reservoir 28 above the level of hydraulic power pack 22 to render the hydraulic system self-priming, and to facilitate the flow of hydraulic fluid from hydraulic fluid reservoir 28 to the hydraulic fluid pump in hydraulic power pack 22. Hydraulic power pack 22 is a conventional, commercially available prime mover, such as a diesel engine, coupled to a hydraulic fluid pump, which supplies hydraulic fluid under pressure to power hydraulic thruster 20.
Base 30 may comprise one or more base feet 32 at its rear, each attached to a base side spar 33, to increase the stability of base 30 on the vessel 10 upon which hydraulic thruster 20 is mounted. One or more vessel stops 44 are mounted to base rear spar 34, and serve to help immobilize hydraulic thruster 20 atop a vessel 10 to which it is mounted, and also transmit force from propellers 39 to vessel 10.
One or more lower unit mounting tube supports 40 extend aft from base rear spar 34 and support lower unit mounting tube 36. One or more lower units 38 are mounted to lower unit mounting tube 36 by means of respective lower unit housings 42.
Each lower unit 38 is free to rotate within its respective lower unit housing 42 as indicated by arrow 18 in
Hydraulic fluid under pressure from hydraulic power pack 22 powers propeller(s) 39 on lower unit(s) 38, and may also serve as a power source for steering assembly 50.
Each lower unit housing 42 is free to rotate on lower unit mounting tube 36 as indicated by arrow 16 in
Due to the slidable attachment between mounting tube bore 14 and lower unit mounting tube 36, lower unit 38 is free to rotate on lower unit mounting tube 36 in order to tilt up and down, as indicated by arrow 16 in
Lower unit housing 42 can be re-mounted on lower unit mounting tube 36 simply by sliding lower unit mounting tube 36 into mounting tube bore 14 as indicated by arrow 70 in
Lower unit 38 can be re-inserted into lower unit housing 42 by sliding it into lower unit bore 12 as indicated by arrow 74. Steering gear 52 can then be attached to lower unit 38, and steering assembly 50 mounted on lower unit housing 42, as indicated by arrow 72.
An alternate embodiment hydraulic thruster 20 comprises lower unit bushings 46. As may be observed in
As may be observed in
Lower unit bushings 46 serve to cushion and reduce friction associated with the slidable attachment between lower unit housing 42 and lower unit 38. In the preferred embodiment, lower unit bushings 46 were made of nylon, synthetic, plastic, teflon, stainless steel or other metal or coated material, or other appropriate low-friction, corrosion-resistant material.
Base foot 32 comprises base foot rear spar 80, and base foot side spar 82 attached at one end to base foot rear spar 80, and at the other to base side spar 33. In the preferred embodiment, base foot rear spar 80 was an end of base rear spar 34. Base foot 32 further comprises base foot reinforcement plate 86 attached to base foot rear spar 80 at vessel stop 44, and base foot center spar 84 attached at one end to base foot reinforcement plate 86, and at an opposite end to base foot side spar 82. Base foot reinforcement plate 86 and base foot center spar 84 serve to reinforce the structurally critical attach point of vessel stop 44 to base foot 32. In the preferred embodiment, base 30, base foot rear spar 80, base foot reinforcement plate 86, base foot side spar 82, and base foot center spar 84 were of welded metal construction.
When tilt actuator 88 is extended or retracted as indicated by arrow 92 in
Due to the slidable attachment of lower unit 38 and lower unit housing 42, lower unit 38 is not only free to pivot, but can also be retracted as indicated by arrow 78 in
Lower unit(s) 38 may be then stowed for transportation, servicing, cleaning and/or storage by tilting up lower unit 38 as indicated by arrow 94 in
When mounted on a vessel 10, the alternate embodiment hydraulic thruster 20 depicted in
In the interest of saving material and cost, a single base foot 32 may be incorporated into the single lower unit hydraulic thruster 20 embodiment depicted in
In the embodiments lower unit 38 depicted in
In order to achieve this re-enforcing function, in the preferred embodiment, the overall length of tube 112 depended on the length of shaft 110 to be supported. For example, in the “short reach” model, the length of tube 112 was 24 inches, the length of shaft 110 was 88 inches, and the ratio of the length of tube 112 to the length of shaft 110 was 0.273. In the “long reach” model, the length of tube 112 was 36 inches, the length of shaft 110 was 126 inches, and the ratio of the length of tube 112 to the length of shaft 110 was 0.286. In both cases the height of lower unit housing 42, and therefore the length of tube 112 disposed within lower unit housing 42, was 13 inches.
Thus as a general rule, it was determined experimentally that the optimal ratio of the length of tube 112 to the length of shaft 110 is between 0.24 and 0.32. The weight of steering clamp 120 and steering gear 52 hold shaft 110 down in position, under the influence of gravity.
One end of lower unit actuator 102 is attached to tube 112; the opposite end of lower unit actuator 102 is rotatably attached to shaft 110 at actuator collar 114. Because shaft 110 is free to slidably reciprocate and rotate within tube 112, extension and retraction of lower unit actuator 102 extends and retracts shaft 110 within tube 112.
Actuator collar 114 is rotatably disposed between shaft clamps 116. Shaft clamps 116 are rigidly attached to shaft 110. Sufficient clearance is left between shaft clamps 116 and actuator collar 114 to permit actuator collar 114 to freely rotate on shaft 110 without appreciable frictional interference from shaft clamps 116. In the preferred embodiment, shaft clamps 116 were split-ring clamps, whose symmetrical halves were mutually attached at each end via conventional fasteners such as nuts and bolts.
Steering clamp 120 is releasably clamped to shaft 110 above lower unit housing 42. Steering gear 52 is rigidly attached to steering clamp 120. As explained previously, steering assembly 50 drives steering gear 52. Thus, because steering gear 52 is rigidly attached to steering clamp 120, which in turn is rigidly clamped to shaft 110, steering assembly 50 steers by rotating shaft 110 within tube 112, through steering gear 52 and steering clamp 120.
The angular orientation between shaft 110 and steering clamp 120 is further prevented from changing by means of steering clamp key 122 slidably traveling within shaft keyway 124. Steering clamp 120 comprises steering clamp aperture 121, through which shaft 110 extends. Steering clamp key 122 extends radially into steering clamp aperture 121 from steering clamp 120. Loosening steering clamp 120 permits shaft 110 to slide upwards and downwards within steering clamp aperture 121; tightening steering clamp 120 immobilizes steering clamp 120 on shaft 110.
Steering clamp 120 fulfills two principal functions: first, when tightened it locks into place an extended (or retracted) length of shaft 110, and second, due to its rigid attachment to steering gear 52, it steers shaft 110.
Steering clamp key 122 within shaft keyway 124 also serves to prevent steering clamp 120 from rotating relative to shaft 110, even when steering clamp 120 is loosened (such as when shaft 110 is to be extended or retracted, for example).
Thus, the procedure for extending or retracting shaft 110 relative to tube 112 is: first, loosen steering clamp 120; second, command lower unit actuator 102 to extend or retract shaft 110 as desired, and third, re-tighten steering clamp 120 on shaft 110 to lock the extended length of shaft 110. During extension and retraction of shaft 10, steering clamp key 122 traveling within shaft keyway 124 prevents shaft 110 from rotating relative to steering clamp 120.
In
Tube bushing 130 is shaped as lower unit bushing 46, as illustrated in
Above lower unit housing 42, steering clamp 120 is visible rigidly attached to steering gear 52. Steering clamp key 122 extends radially inward from steering clamp aperture 121, and travels within shaft keyway 124:
The embodiment lower unit 38 depicted in
In the manually extendable embodiment of lower unit 38 illustrated in
As depicted in
Note that shaft key 138 slides into steering clamp keyway 140 only at the very end of the extension travel of shaft 110. Therefore, it may be necessary to manually align shaft key 138 with steering clamp keyway 140 visually, by rotating shaft 110 relative to steering clamp 120, in order to be able to slide shaft key 138 into steering clamp keyway 140. This alignment can be easily accomplished visually.
The lower unit 38 embodiment depicted in
Referring now also to
Lower support collar 134 further comprises lower support collar insert 136 sized to fit into lower support collar inner face groove 137. Lower support collar insert 136 comprises lower support collar insert aperture 142 sized to slidably admit shaft 110. Both lower support collar 134 and lower support collar insert 136 are split-ring design, that is, they are each comprised of two symmetrical halves. Both split-ring halves of lower support collar 134 and lower support collar insert 136 can be assembled around shaft 110 using conventional fasteners, and then the complete lower support collar 134 can be attached to an end of lower support 132 opposite vessel 10. This structure provides lower support for shaft 110, especially useful when propeller 39 is turning at full power.
Docking tab 156 is rigidly attached to base 30 in an orientation substantially co-planar with the plane of base 30. Docking tab 156 incorporates docking tab bore 158 disposed in a location wherein locking probe 152 slides into docking tab bore 158 when lower unit 38 is tilted into the down position, as indicated by arrow 166 in
Docking probe 152 is sufficiently long so as to extend through docking tab bore 158 sufficiently to expose locking probe bore 154, the situation depicted in
Locking probe bore 154 is sized to slidably admit pin 160. After pin 160 has been slid through locking probe bore 154 as indicated by arrow 170, safety element 164 may be slid through pin bore 162 in pin 160 as indicated by arrow 172, thus securely holding pin 160 in locking probe bore 154. Pin 160 through locking probe bore 154 in turn holds locking probe 152 securely within docking tab bore 158, which in turn locks lower unit 38 in the down-tilted position.
When it is desired to tilt lower unit 38 into the up position, safety element 164 is removed from pin 160, and pin 160 is slid out of locking probe bore 154, thus releasing lower unit 38 to tilt upwards. In the preferred embodiment, safety element 164 was a cotter pin, bolt and nut, spring retainer pin, or any other appropriate safety element.
In the preferred embodiment, base 30, helm platform 26, helm 24, hydraulic fluid reservoir 28, base feet 32, lower unit mounting tube supports 40, lower unit housing(s) 42, steering gear 52, locking probe 152, locking probe tab 150, docking tab 156, shaft 110, tube 112, tube lip 115, lower support 132, lower support collar 134, steering clamp 120, steering clamp bellcrank 148, and shaft clamps 116 were made using metal, synthetic, corrosion resistant metal, corrosion resistant metal fasteners, welded construction, or other appropriate materials.
Base 30 structural members such as base side spars 33, base rear spar 34, base foot 32, and lower unit mounting tube support(s) 40 may be plates, C beams, I beams, or any other appropriate structural member shape. Steering motor 56, overhung load adaptor 58, drive gear 60, steering gear 52, and hydraulic power pack 22 were commercially available items.
In the preferred embodiment, tilt actuator 88, lower unit actuator 102, steering actuator 146, and steering clamp actuator 144 were hydraulic actuators powered by pressurized hydraulic fluid from hydraulic power pack 22, and controlled from helm 24, although it is intended to fall within the scope of this disclosure that these elements be any appropriate actuator, including but not limited to electrical actuators, solenoids, linear motors, rack-and-pinion gear arrangements, etc. In the preferred embodiment these elements were connected to hydraulic power pack 22 by any appropriate means, including hydraulic lines, which along with wiring, controls, and other existent elements well-known in the art are not shown in the figures in interest of clarity.
Lower unit bushings 46, tube bushings 130, and lower support collar insert 136 were made of ultra-high density polyethylene, nylon, plastic, synthetic, teflon, felt or other appropriate material.
While a preferred embodiment of the invention has been illustrated herein, it is to be understood that changes and variations may be made by those skilled in the art without departing from the spirit of the appending claims.
This utility patent application is a Continuation-In-Part of U.S. utility application Ser. No. 11/999,531 filed Dec. 6, 2007 now U.S. Pat. No. 7,654,875 entitled Self-Contained Hydraulic Thruster for Vessel, which was based upon U.S. provisional patent application Ser. No. 60/903,400 filed Feb. 26, 2007 entitled Self-Contained Hydraulic Thruster for Vessel; and claims the benefit of the earlier filing date of these applications.
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Number | Date | Country | |
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60903400 | Feb 2007 | US |
Number | Date | Country | |
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Parent | 11999531 | Dec 2007 | US |
Child | 12381245 | US |