Technical Field
The field of art to which the invention pertains comprises the art of material handling of the non gravity type.
Background of the Invention
Over the years many different devices and methods have been used in loading cargo into the holds of deep water vessels and other haulage vehicles. Conveyor belts and pipes are used for particulate and fluid matter. Loads consisting of larger discrete objects are often handled by means of large portable containers. Food products such as rice are usually bagged and loaded in pallet sized stacks. Whatever arrangement is utilized for delivering the cargo from dockside or deckside through the cargo hatch to within the hold, the problem remains of finally dispensing the delivered cargo into their assigned locations in the wings of the hold. Typically, the crane utilized for delivering the cargo to a central location beneath the hatch is unable or unsuitable for appropriate removal of the cargo from the hatch area into the wing areas.
Typically, a large proportion of cargo space within a deep water vessel is located in the wing areas. Commonly, stevedores in the cargo hold must manually remove the cargo units from the delivery location and utilize mobile equipment for transporting the removed units to a remote location under the wing. With the limited load capacities of the mobile carriers such as fork lifts, frequent trips are required to complete any sizeable loading. Moreover, fork lifts are unsuitable for handling bag type cargo. Furthermore, they are characterized by limited stacking height capabilities frequently requiring manual labor to fill the remaining volume. Alternatively, the otherwise available cargo volume goes unused. In the process of stacking the cargo units in their assigned locations in the hold, the cargo units are usually handled individually or remain on a space-consuming pallet. Such manual handling has been recognized as time consuming and labor intensive amounting to a significant cost factor in the shipping expense of the goods that are ultimately passed on to the end user of the products which the cargo represents.
There has therefore been a long felt need to improve the disposition of delivered cargo from the delivery site location in the ship's hold to the final location within the wings of the hold selected for transport. Portable cargo loading equipment for fulfilling that purpose is disclosed in my co-pending application Ser. No. 830,235 filed Feb. 14, 1986, now abandoned. While functioning well for the intended purpose the equipment disclosed therein is characterized by a limited loading capacity on the order of about 2-3 metric tons per loading cycle depending on the size of the equipment selected. It has recently been recognized that much higher loading capacities on the order of ten metric tons per loading cycle and above would be highly cost effective and therefore desirable for many of the larger ocean going ships currently utilized. However, not only must such apparatus be characterized by the higher loading capacities, but it must be portable for hold placement and retrieval. Furthermore, it should preferably be self sufficient for both cargo placement and incremental self displacement for loading successive sites after loading of a selected site has been completed. Despite recognition of the problem, apparatus suitable for the larger capacities in satisfaction of the above has previously been unknown.
Summary of the Invention
The invention relates to wing loader apparatus for cargo loading of cargo ships. More specifically, the invention relates to such cargo loading apparatus having significantly greater load handling capacity than heretofore so as to further reduce the labor intensity previously associated with the cargo loading of large ships. This is achieved in accordance with the invention by apparatus that is relatively portable for placement and retrieval within the ship's hold by means of a deckside or a dockside crane. Yet when placed in the hold in loading relation with the wing area selected for loading, the apparatus not only can place cargo centrally received wtihin the hold into the designated wing areas, but is capable of incremental lateral self displacement for positioning relative to the next successive wing site to be loaded.
To enable the foregoing to be achieved, the apparatus is comprised of three separate sections including a first section for cargo loading and unloading, a second section for effecting lateral self displacement and a third section including a power source, pumps, valves, controls, etc., for controllably operating the first and second sections. Forming the first section are a plurality of stacked and nested large area trays. The lowermost of the trays is stationary whereas the middle and upper trays can be selectively extended and retracted by a drive motor and hydraulic cylinders respectively for placement and push off of a delivered cargo at the wing storage site in the vessel for shipment.
The second section is comprised of horizontal elongated beams parallel and spaced apart and supported on upright columns extending transversely to the first section. The length of the beams are approximately twice the width of the first section and at each distal end support a downwardly depending hydraulic cylinder. When the hydraulic cylinders are retracted upward the entire main frame of the apparatus including the first and third sections rests on flooring of the hold. When the hydraulic cylinders are extended to and against the flooring, the main frame being intermediate the cylinders is caused to be elevated above the flooring. Via drive means actuated with the main frame in the latter relation, the main frame is laterally displaced incrementally along the beams relative to a successive location at which cargo is to be placed into the wings of the hold. On reaching the successive location, the hydraulic cylinders are retracted lowering the main frame onto the floor. The beams are then free to be transversely extended relative to the main frame preparatory for the next incremental displacement thereof.
The third section provides the power equipment to render the apparatus self sufficient and includes a power generator which may be omitted where sufficient local power is otherwise available.
It is therefore a first important aspect of the invention to provide a portable and yet self sufficient cargo loading apparatus for dispensing and retrieving cargo between a central hold location of a haulage vessel and the wing areas thereof.
It is a second important aspect of the invention to provide such cargo apparatus that is not only portable and self sufficient but at the same time is capable of handling significantly greater loading capacities for dispensing cargo into the wing areas of the hold than has been available heretofore.
It is a third important aspect of the invention to provide cargo handling apparatus as in the second aspect hereof capable of incremental lateral self displacement within the hold for dispensing cargo loads successively into juxtaposed wing sites of a cargo ship.
The above noted features and advantages of the invention as well as other superior aspects thereof will be further appreciated by those skilled in the art upon reading the detailed description which follows in conjunction with the drawings.
Brief Description of the Drawings
FIG. 1 is topside isometric view of the cargo loading apparatus hereof;
FIG. 2 is a sectional view as seen substantially from the position 2--2 of FIG. 1;
FIG. 3 is a sectional view through a cargo vessel showing the apparatus hereto receiving delivery of cargo from dockside;
FIG. 4 is a sectional view similar to FIG. 3 in which the delivered cargo of FIG. 3 is being dispensed by the apparatus hereto in its extended relation into a selected site within the wings of the hold;
FIG. 5 is a plan view of FIG. 4;
FIG. 6 is a plan view similar to FIG. 5 in the course of the loading section of the apparatus hereto being retracted;
FIG. 7 is an enlarged sectional elevation as taken substantially from the position 7--7 of FIG. 5;
FIG. 8 is a fragmentary sectional elevation as seen substantially from the position 8--8 of FIG. 7; and
FIGS. 9, 10 and 11 are enlarged sequential rear elevations taken substantially from the position 9--9 of FIG. 6 for the incremental self displacement function of the apparatus hereof.
Description of the Preferred Embodiment
In the description which follows, like parts are marked throughout the specification and drawings with the same reference numerals respectively. The drawing figures are not necessarily to scale and certain views may be drawn rotated into the plane of the drawing for purposes of clarity.
Referring now to the drawings, the apparatus hereof is designated 10 and is comprised of a first section 12 to effect cargo loading and onloading within the wing areas 15 in hold 17 of a ship 19. A second section 14 provides for lateral incremental displacement of the first section to successive cargo loading sites. A third section 16 is joined with the other sections and contains a power source such as a diesel generator, pumps and the various controls necessary to render the apparatus self sufficient for effecting operation hereof as will be described.
Providing the underlying support for the operative components hereof is an elongated rectangular base 18 extending from the forward end 21 to the rearward end 23 underlying power section 16. Upstanding from base 18 at the sides and at a relatively rearward location are four columns 20, 22, 24 and 26. Each column includes an I-hook 28 by which the entire apparatus 10 can be transferred from deckside or dockside through cargo hatch 23 to within hold 17 by means of a deck or dockside crane as would be available. For balancing purposes, additional columns (not shown) and I-hooks (not shown) may be provided in the vicinity of power section 16.
Comprising the first section 12 at the relatively forward end of base 18 are opposite upright elongated side channels 36 and 38 forming with base 18 a lowermost and stationary U-shaped tray 29. Slidably received within tray 29 is a middle U-shaped tray 30 having opposite side uprights 32 and 34 slidably contained for longitudinal displacement within channels 36 and 38. Overlying tray 30 and slidably supported and nested thereon is a U-shaped upper tray 40 that includes longitudinal side uprights 42 and 44. The overall width of tray 40 provides a clearance space 46 on either side relative to the side face of channels 36 and 38 thereat. When retracted, as illustrated in FIG. 1, each of the trays 29, 30 and 40 are in a nested relation with the latter two capably of being selectively and controllably extended as will be described. For accommodating the load capacities contemplated with the apparatus hereof, each of the trays 29, 30 and 40 are approximately 16 feet long and 9 feet wide able, for example, to receive approximately 4-6 pallet loads per loading cycle. In order to render the trays relatively slidable to each other, they are formed of stainless steel or other composition of similar strength and low friction properties at least along their slidable surfaces.
When the apparatus 10 is transferred by crane or the like from dockside or deckside through cargo hatch 23, both trays 30 and 40 are contained in their retracted relations as illustrated in FIG. 1. To extend tray 30 leftward as viewed in FIG. 1, there is provided an hydraulic motor 48 mounted on base 18 and which through a clutch 50 and a chain sprocket 52 drives chain 54. Chain 54, in turn, through idler sprocket 56 drives chain 58 extending about idler sprocket 60. A bolt 62 laterally secured to the upright 32 of tray 30 extends through longitudinal slot 64 in channel 36 and is secured to the underside of chain 58. When driven, chain 58 causes bolt 62 to incur concomitant forward movement therewith for effecting outward displacement of tray 30. Clutch 50 for these purposes, has one-way operation being a type having a helically wound spring as manufactured by Warner Electric Brake and Clutch Co. of South Beloit, Ill. Secured longitudinally along the upper surface of tray 30 are a plurality of spaced apart and parallel ribs 66 (FIG. 7). The ribs in this relation are longitudinally intervening between the trays so as to provide the relatively slidable surface therefor. Also, each of the ribs includes a plurality of longitudinally extending uniformly spaced vertical apertures 67 at least near the rearward end thereof to enable a coupled retraction of the trays 30 and 40 as will be explained.
Extending transversely upright and joined between side uprights 42 and 44 so as to define the rear of top tray 40 is a rear wall 68. Horizontally extending longitudinally rearward from a connection with wall 68 for mounting on a stationary wall 70 are two spaced hydraulic cylinders 72 and 74. As shown in FIG. 1, the hydraulic cylinders are in their retracted positions and when hydraulically actuated, the pistons thereof are operatively extended to displace tray 40 toward its extended position beyond front end 21. A hydraulic cylinder 76 located intermediate cylinders 72 and 74 is likewise mounted on wall 70 and extends through aperture 78 in rear wall 68 for engaging push bar 80. The push bar is dimensionally comparable with wall 68 and can be advanced and retracted in tray 40 independent of tray displacement. On the back side of wall 68 (FIG. 7) are a plurality of spaced apart vertically oriented hydraulic cylinders 82 each having a downwardly depending actuating pin 84 spring loaded upwardly by means of spring 86. Each cylinder 82 when actuated will cause pin 84 to extend downwardly for a latching engagement and interlock cooperation with one of the apertures 67 in ribs 66 in order to couple the trays and enable concomitant retraction of trays 30 and 40 as will be understood. During retraction, one way clutch 50 will free wheel. After a selected wing site has been completely loaded and it is desired to load the adjacent site, the entire loading section 12 is retracted into the relation of FIG. 1.
To effect lateral relocation of the apparatus, second section 14 includes a pair of parallel spaced apart elongated beams 88 and 90 supported for relative transverse displacement on column members 20, 22, 24 and 26. The length of the beams is preferably slightly greater than twice the overall width of the base 18 with a strength factor readily able to accommodate the entire static and dynamic weight of the unit 10. Supporting the beams 88 and 90 at each of the columns for displacement relative to the other structures hereof is a pair of vertically spaced guide rollers 92 and 94 framed and journaled for rotation between upstanding parallel plates 96 and 98 secured in turn to the respective columns.
At the distal end of each of the beams there is disposed a vertically oriented hydraulic power cylinder 100 the piston 102 of which extends downwardly depending for supporting at its distal end a round circular pad 104. Secured longitudinally and arranged on the top surface of each of the beams is a hydraulic cylinder 106 extending between a clevis connection 108 and a cross plate 110 mounted in turn against upright plates 96 and 98. It will be appreciated that extending and retracting the hydraulic cylinders 106 will cause beams 88 and 90 to be displaced in opposite directions relative to the main frame as will be explained.
In operation, the entire unit 10 can be lowered through cargo hatch 23 via a crane hook 112 for placement on flooring 114 of hold 17 at a location and in an orientation selected for cargo loading into an opposite and paired location representing a first cargo loading site in wing 15. At this point in time, the support pads 104 are elevated in the relation of FIG. 9 and the underside of base 18 rests on the flooring 114. With unit 10 in position on flooring 114, and all power components in section 16 operative, hydraulic cylinders 100 are simultaneously energized to extend their pistons 102 downwardly until their support pads 104 engage against flooring 114. Continuing to extend pistons 102 causes the main frame of the apparatus to become elevated above flooring 114 until achieving the relation illustrated in FIG. 10. While still elevated hydraulic motor 48 is actuated and through clutch 50 motor 48 causes middle tray 30 to be extended outwardly until approaching the proximity of wing wall 115 as illustrated in FIG. 3. Once tray 30 has been extended, hydraulic cylinders 100 are reversed causing their pistons 102 and pads 104 to be retracted upwardly until the main frame is again supported directly on the flooring 114 in the manner of FIG. 9. With the apparatus on flooring 114 a cargo load 116, which may be transported and handled by apparatus 118, such as disclosed in my U.S. Pat. No. 4,432,689, is lowered via hook 112 through cargo hatch 23 onto top tray 40 as illustrated in FIG. 3. After separating the cargo load 116 from the cargo handler 118, push cylinders 72, 74 and 76 are simultaneously actuated for extending top tray 40 and push bar 80 along with the cargo load 116 thereon until the upper tray 40 is positioned substantially coextensive with and is superimposed over the middle tray 30 as shown in FIG. 4.
With the cargo 116 having reached its destination site in wing 15, the middle and upper trays 30 and 40 are withdrawn concomitantly. This is effected by first coupling the trays via hydraulic cylinders 82 causing their pins 84 to extend into an interlock relation with one of the apertures 67 of ribs 66 extending along the topside of tray 30. On being coupled, the middle tray 30 and upper tray 40 are withdrawn or retracted concomitantly by reversing operation of the push cylinders 72 and 74 so as to retract and withdraw tray 40. During withdrawal of the trays, push bar 80 remains engaged against the cargo 116 until the trays are removed from under the cargo after which push bar 80 is per se retracted by reversing hydraulic cylinder 76. When fully retracted, the trays are uncoupled by reversing cylinders 82 to permit their subsequent relatively independent extension as previously described for dispensing additional cargo load 116.
After a first cargo loading has been loaded as described above and with all operating components of section 12 in their retracted starting relation, the main frame of the apparatus is incrementally displaced laterally, in the direction of arrow 120 by means of section 14. The main frame is first elevated by operation of hydraulic cylinders 100 as described above. With the main frame elevated, the hydraulic cylinders 106 are simultaneously energized so as to extend and cause the main frame to be conveyed by means of rollers 92 and 94 over parallel beams 88 and 90 in the direction 120 from left to right as viewed in the comparative illustrations of FIGS. 10 and 11. When the main frame arrives at its laterally displaced location corresponding and oriented to the second cargo loading site in which the next cargo loading is to be placed, tray 30 is extended as aforesaid before the main frame is lowered by reversal of hydraulic cylinders 100. After being lowered, the entire unit 10 is in position for receiving additional cargo 116 to be dispensed into the wing area adjacent to wall 115 and juxtaposed to the load previously placed in the first loading site thereat. During the cargo loading process, hydraulic cylinders 106 are reversed so as to retract and cause the beams 88 and 90 to be restored to the relation with the main frame shown in FIG. 9 in preparation for the next main frame displacement in the direction 120 as aforesaid.
The foregoing is continually repeated over and over until one side of the wing is completely loaded with cargo. At that point, apparatus 10 is positioned via crane hook 112 at right angles to similarly load the ends of the hold. On completion of end loading the apparatus is again turned to similarly load the opposite wing followed by the opposite end. After the entire wings and ends have been loaded, the square of the hold beneath the cargo hatch can, for example, be loaded by means of apparatus disclosed in my U.S. Pat. 4,432,689. On completion of one layer of loaded cargo throughout the hold 15, apparatus 10 is placed on top of the cargo and the operation is repeated as in the preceding. For unloading, the operation is similar except for retrieval of cargo from the wing site onto tray 40 which is then retracted to the square of the hold.
By the above description there is disclosed novel apparatus for cargo loading and unloading wing areas of cargo ships. The apparatus hereof can increase loading capability from about 40 tons per hour in accordance with past practices to in excess of 100 tons per hour. At the same time it represents a significant advance in the art in being able to handle not only greater load capacities but is operative with substantial reduction in labor force as compared to the loading apparatus previously utilized for the cargo loading of wing areas. Except for personel utilized in the delivery of the cargo onto tray 40, only one person is required to operate the apparatus per se. During loading, the remaining persons are then free to perform other chores in and about the hold. The economic savings resulting from the reduced time and labor associated with the enhanced loading efficiency afforded by the apparatus hereof is so significant as to contribute substantial cost savings in the overall loading of such ships destined for the many parts of the world. In some instances charges for ocean freight is based on a flat rate per container rather than weight of goods being shipped, such that any reduction in labor and time involvement can result in substantial monetary savings to the shipper. Consequently, the virtues of the apparatus hereof should be instantly apparent. While use of a power generator has been described as included with the preferred embodiment, it obviously can be eliminated on those models intended for applications where adequate sources of local power is otherwise available. Furthermore, whereas the apparatus has been described as principally useful in the dispensing of cargo into the wing areas of the hold, it should be apparent that it is similarly useful for retrieving cargo therefrom in the unloading process from the wing areas.
Since many changes could be made in the above construction and many apparently widely different embodiments of this invention could be made without departing from the scope thereof, it is intended that all matter contained in the drawings and specification shall be interpreted as illustrative and not in a limiting sense.