Skid assembly for freight containers
A skid assembly for securement to the underside of a freight container, in order to assist the slidable loading and unloading of the container relative to a loading platform. The container has upper and lower corner fittings to enable the container to be clamped to one or more adjacent container(s) and/or support surfaces. The skid assembly is arranged to be capable of extending between a pair of lower corner fittings and to be securable thereto in order to secure the skid assembly to the underside of the container. The skid assembly includes an elongate support having upper and lower support surfaces, the lower support surface being engageable with a loading platform, and the upper support surface being engageable with the underside of the container. A pair of clamping devices are mounted one adjacent to each end of the elongate support and each engageable with a respective one of the pair of lower corner fittings to secure the skid assembly to the underside of the container.
This invention relates to a skid assembly for securement to the underside of a freight container in order to assist the loading and unloading of the freight container relative to a load platform.
Freight containers usually are designed in different standard sizes, and are used widely to transport goods via road, rail, ship and in aircraft.
The present invention has been developed primarily, though not exclusively, in connection with freight containers for transportation by aircraft, and which typically are of smaller size, and usually referred to as “mini container”. However, it should be understood that a skid assembly according to invention is applicable to freight containers generally, to be secured to the underside thereof, and to assist the loading and unloading relative to a load platform.
With transport by aircraft, the loading constraints of an aircraft usually dictate that small containers only can be loaded and unloaded with respect to the load platform/floor of the aircraft. It is usual to transport mini containers to and/from an aircraft by other means of transport, and with the containers forming assembled modules of more than one mini container e.g. TRICON or QUADCON for three and four modules/mini containers respectively.
The modules are assembled by coupling together adjacent “corner fittings” of the containers using clamping devices, usually referred to as “twistlocks”.
Typically, aircraft intended for the transportation of cargo only are fitted with roller tracks and guides at set pitches within their decks, to allow palletted cargo to be rolled in and out with relative ease. Existing pallets typically have dimensions of 2590×2438×40 to 70 mm thick, and are usually manufactured from aluminium sections which are welded together. Along the two edges of the pallet which contact the guides on the aircraft deck, a castellated tooth formation is produced to allow locking pins slidably mounted on the aircraft deck to travel up through the guides and engage the castellations when the pallet has been advanced to the required location. The pallets are also equipped with lashing points to allow the cargo to be strapped down to the pallet, either by chains or nylon webbing.
In recent years, it has been desirable to be able to ship mini containers in such transport aircraft. Typically, mini containers are capable of being assembled in modules to form a container assembly of standard length of twenty foot. As referred to above, mini containers may be designed as individual modules of appropriate size, to make up a twenty foot assembly, comprising four modules in a QUADCON, three modules in a TRICON, or two modules when each mini container is half size.
Although such containers are fitted with lifting fittings usually, to standard ISO1161, there has been no provision to lock them to the floor of the aircraft, and when chain lashings are used, this has led to severe damage, and the use of excessive time to secure and unsecure. Given in particular the demands of military transport aircraft, it is highly desirable, and often essential, that the loading and unloading times be kept to an absolute minimum, given the hazardous environments in which the aircraft may be operating. Existing mini containers have great integral strength, and do not require the loading pallet to distribute the load. They do, however, require a flat area to contact the roller tracks and the provision of the castellated tooth system to provide the required locking of the pallet.
The present invention seeks to provide a skid assembly for securement to the underside of a freight container, in order to assist the loading and unloading of a freight container relative to a load platform e.g. on an aircraft floor, and which does not require use of pallets, while providing an arrangement which can be loaded and unloaded easily, and also be secured and unsecured readily in a shorter period of time than with existing palletting techniques.
According to the invention there is provided a skid assembly for securement to the underside of a freight container, in order to assist the slidable loading and unloading of the container relative to a loading platform, said container having upper and lower corner fittings to enable the container to be clamped to one or more adjacent container(s) and/or support surfaces, and the skid assembly being arranged to be capable of extending between a pair of lower corner fittings, and to be securable thereto in order to secure the skid assembly to the underside of the container, in which the skid assembly comprises:
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- an elongate support having upper and lower support surfaces, the lower support surface being engageable with a loading platform and the upper support surface being engageable with the underside of the container; and
- a pair of clamping devices mounted one adjacent to each end of the elongate support and engageable with a respective one of the pair of lower corner fittings to secure the skid assembly to the underside of the container.
Thus, the skid assembly of the invention can be readily secured to the underside of a freight container, and to be clamped securely to a pair of lower corner fittings of the container, and then the skid assembly can engage slidably with a load platform to load and unload the freight container.
In a particularly preferred application of the invention, the freight container is a mini container which is intended to be loaded and unloaded with respect to a support deck or platform of an aircraft intended for cargo transportation, and usually provided with a floor having roller supports, and with longitudinal guides and locking elements.
The skid assembly may be a simple metal fabrication, preferably made of hollow sections to reduce the weight. At least some of the hollow sections may be filled with structural foam to increase the strength of the sections and resistance to bending loads, and also to distribute loads whilst minimising overall weight.
The elongate support of the skid assembly preferably includes two longitudinally extending load-bearing surfaces, a first of which is intended to engage and to support the lower surface of the pair of lower corner fittings, and a second of which is laterally spaced from the first surface and which is intended to engage and to support the underside of the base of the container.
It is usual for the lower corner fittings of a container to project downwardly by a small amount relative to the base of the container, so that vertical loads applied by the container to an underlying support e.g. a lower container on which it is stacked, are transmitted via the corner fittings and suitably strengthened columns at each corner of the container.
The second load-bearing surface is therefore at a slightly raised level relative to the first load-bearing surface, so that it can engage with the base of the container.
To compensate for any manufacturing tolerances and/or damage to the underside of the base, it is preferred that a load transfer pad forms the second load-bearing surface. Conveniently, the pad comprises a longitudinal strip of resiliently deformable material e.g. a rubber pad, which is secured to the upper surface of the skid assembly.
For some customers, it may be acceptable to manufacture the skid assembly with a length to suit the spacing apart of the pair of lower corner fittings of the particular container with which it is to be used. However, to provide a common design of skid assembly for use with different containers, the elongate support may be fabricated in two parts which are longitudinally adjustable to vary the overall length of the skid assembly. In a preferred arrangement, the two parts are telescopically adjustable.
A locking mechanism may be provided to lock the two parts in any required position of lengthwise adjustment.
In a particularly preferred embodiment, the skid assembly comprises a main wide box section, and a pair of narrower hollow sections each running longitudinally along a respective one of the opposed longitudinal sides of the main section. One of the hollow sections preferably has a support section secured thereto, is generally triangular in cross-section, and of which an upper and horizontal side has the load-bearing pad secured thereto.
The other hollow section may have a number of lateral projections secured thereto, and spaced apart longitudinally to define locking spaces there-between, into which fastening bolts on the loading platform can engage to restrain the skid assembly longitudinally.
The lateral projections preferably comprise wear resistant sliding portions e.g. made of heavy duty plastics, to engage slidingly with the guides usually provided on the loading platform of an aircraft.
The clamping devices preferably comprise rotatable clamping heads which are biassed to a retaining position, but which are moveable against the biassing to an entry position in which the head can enter the respective corner fitting.
Preferably, the heads are shaped so as to be engageable by the edge of the entrance aperture to the corner fitting (when the heads are in the engaged position), and thereby to be moved to the entry position. The heads are then received by the corner fittings, and when properly located therein, the biassing returns the heads to the retaining position. This then securely fastens the skid assembly to a pair of lower corner fittings of the container.
Usually, a pair of skid assemblies will be provided, to support each container, and then enable the container readily to be loaded and unloaded by slidable movement of the skid assemblies over rollers built into the loading platform.
A preferred embodiment of skid assembly according to the invention will now be described in detail, by way of example only, with reference to the accompanying drawings, in which:
Referring now to the drawings, and particularly
The corner fittings are rigidly clamped together by any one of a number of different proprietary types of clamping heads and twistlocks, all of which will be well known to those of ordinary skill in the art, and which need not be described in detail herein. However, when the QUADCON assembly has been delivered to an aircraft, the assembly must then be broken up into individual modules, which are then loaded individually on to the loading deck of the aircraft. This is achieved by utilisation of a skid assembly according to the invention, which will be described in more detail, with reference to the remaining figures of drawings.
The skid assembly according to the invention which will be described is intended for securement to the underside of a freight container, in order to assist the slidable loading and unloading of the container relative to a loading platform. The container has upper and lower corner fittings 12, 13 to enable the container to be clamped to one or more adjacent container(s) and/or support services, and the skid assembly is arranged to be capable of extending between a pair of lower corner fittings, and to be securable thereto in order to secure the skid assembly to the underside of the container.
In general terms, the skid assembly comprises an elongate support having upper and lower support surfaces, the lower support surface being engageable with a loading platform and the upper support surface being engageable with the underside of the container.
The skid assembly also includes a pair of clamping devices mounted one adjacent to each end of the elongate support, and engageable with a respective one of the pair of lower corner fittings to secure the skid assembly to the underside of the container.
The skid assembly 16 essentially comprises an elongate support 20 having an upper surface which engages the lower bases of the corner fittings, and also the underside of the container, as will be described in more detail below. The skid assembly also has a lower surface (not shown in
A pair of clamping devices 21 are mounted one adjacent to each end of the elongate support 20, and engageable with a respective one of the pair of lower corner fittings 13 to secure the skid assembly to the underside of the container.
It will be noted from the detail of
There is also shown in
Referring briefly back to
The lateral projections 30 are triangular in cross-section, and made of hardwearing material, typically hard plastics, such as nylon.
Referring to
The outboard side 36 of the skid assembly is provided with the lateral projections 30, as referred to above with reference to
Claims
1. A skid assembly for securement to the underside of a freight container, in order to assist the slidable loading and unloading of the container relative to a loading platform, said container having upper and lower corner fittings to enable the container to be clamped to one or more adjacent container(s) and/or support surfaces, and the skid assembly being arranged to be capable of extending between a pair of lower corner fittings and to be securable thereto in order to secure the skid assembly to the underside of the container, in which the skid assembly comprises:
- an elongate support having upper and lower support surfaces, the lower support surface being engageable with a loading platform, and the upper support surface being engageable with the underside of the container; and
- a pair of clamping devices mounted one adjacent to each end of the elongate support and each engageable with a respective one of the pair of lower corner fittings to secure the skid assembly to the underside of the container.
2. A skid assembly according to claim 1, comprising a metal fabrication, including hollow sections.
3. A skid assembly according to claim 2, in which at least some of the hollow sections are filled with structural foam to increase the strength of the sections and resistance to bending loads, and also to distribute loads whilst minimising overall weight.
4. A skid assembly according to claim 1, and including two longitudinally extending load-bearing surfaces, a first of which is intended to engage and to support the lower surface of the pair of lower corner fittings and a second of which is laterally spaced from the first surface and which is intended to engage and to support the underside of the base of the container.
5. A skid assembly according to claim 4, in which the second load bearing surface is at a slightly raised level relative to the first load bearing surface so that it can engage with the base of the container.
6. A skid assembly according to claim 4, in which a load transfer pad forms the second load-bearing surface.
7. A skid assembly according to claim 6, in which the pad comprises a longitudinal strip of resiliently deformable material, e.g. a rubber pad, which is secured to the upper surface of the skid assembly.
8. A skid assembly according to claim 1, in which the elongate support is fabricated in two parts which are longitudinally adjustable to vary the overall length of the skid assembly.
9. A skid assembly according to claim 8, in which the two parts are telescopically adjustable.
10. A skid assembly according to claim 8, in which a locking mechanism is provided to lock the two parts in any required position of lengthwise adjustment.
11. A skid assembly according to claim 1, and comprising a main wide box section, and a pair of narrower hollow sections each running longitudinally along a respective one of the opposed longitudinal sides of the main section.
12. A skid assembly according to claim 11, in which one of the hollow sections has a support section secured thereto, which is generally triangular in cross section, and of which an upper and horizontal side has the load-bearing pad secured thereto.
13. A skid assembly according to claim 12, in which the other hollow section has a number of lateral projections secured thereto, and spaced apart longitudinally to define locking spaces therebetween, into which fastening bolts on the loading platform can engage to restrain the skid assembly longitudinally.
14. A skid assembly according to claim 13, in which the lateral projections comprise wear resistance sliding portions, engageable slidingly with guides provided on the loading platform of an aircraft.
15. A skid assembly according to claim 1, in which each clamping device has a rotatable clamping head which is biased to a retaining position, but which is moveable against the biasing to an entry position in which the head can enter the respective corner fitting.
16. A skid assembly according to claim 15, in which the heads are shaped so as to be engageable by the edge of the entrance aperture to the corner fitting (when the heads are in the engaged position), and thereby to be moved to the entry position.
17. A container supported by a pair of skid assemblies, to enable the container to be loaded and unloaded by slidable movement of the skid assemblies over rollers built into the loading platform.
Type: Application
Filed: Apr 22, 2003
Publication Date: Oct 20, 2005
Inventor: Kenneth Reynard (Thirsk)
Application Number: 10/511,889