The present invention relates generally to a support assembly, and more specifically to a layered or multi-tiered support system.
Items are transported in various containers, to include containers for specialized care, such as for example the extra care needed to protect sensitive equipment from damage during transport or storage. For example and without limitation, sensitive electronic equipment such as for example a gyroscope, may need to be handled using special care. It is known to use a single-tier support assembly for the specialized transport of a gyroscope and other such sensitive devices. Single-tier support assemblies generally consist of a top and bottom portion and are designed to transport one or two devices only. In addition, these two-piece support systems are known to use a polyurethane (P.U.) foam, similar to sofa padding (e.g., Stathane 8201-2SEH). Such polyurethane foam deteriorates from exposure to UV light and moisture, and the material flakes off when contacted. This type of foam is also deemed a hazardous material, and requires special precautions to mold the foam into the desired shape or form for use as a support system. In short, special processes and safety precautions must be used, and expensive molds have to be designed and built, to manufacture such polyurethane support systems. What is needed is an improved support system that is easier, safer and more economical to manufacture while supporting more devices in the same volume. It is also desired to use material that does not degrade with exposure to light, and does not flake off with contact. In addition, it is desired to eliminate the hazardous process of molding the support material.
The present invention may comprise one or more of the following features and combinations thereof.
An illustrative support assembly generally comprising: a main body, a first cover and a second cover is provided along with a method of use and manufacture. The main body illustratively defines a first main cavity and an opposing second cavity. The first cover defines a first cover cavity and the second cover defines a second cover cavity, wherein the first and second covers are configured to sandwich therebetween the main body such that the first cover cavity generally aligns with the first main cavity adjacent and opposite thereto and the second cover cavity generally aligns with the second main cavity adjacent and opposite thereto, the aligned cavities configured to cooperate to receive and nestle therein a device.
Also provided is a method of supporting a device comprising the steps of: providing a main body defining an upper main cavity and a lower main cavity, providing an upper cover defining an upper cover cavity, providing a lower cover defining a lower cover cavity, receiving and nestling a device partially within one of the main cavities and partially within one of the cover cavities complimentary thereto; and joining together the main body and the cover.
Further provided is a method of manufacturing a support assembly comprising the steps of: cutting a first thickness of material into a desired shape including a first cavity, cutting a second thickness of material into a desired shape including a second cavity generally complimentary to the first cavity if the first and second thicknesses of material are stacked together with the first and second cavities in opposing fashion, and conditioning the material.
These and other objects of the present invention will become more apparent from the following description of the illustrative embodiment.
For the purposes of promoting an understanding of the principles of the invention, reference will now be made to a number of illustrative embodiments illustrated in the drawings and specific language will be used to describe the same.
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It will be appreciated that in the illustrative embodiment, as few as one or as many as four gyroscopes or other device(s) may thus be received and nestled in the layered assembly 10. If desired, the assembly components 20, 30, 40 could be sized to define only a single, or more than two cavities per layer, component or tier. So, too, the illustrative cavities depicted in the drawings could be sized to allow for fewer or additional cavities per layer, component, or tier and to accommodate different size devices. Those skilled in the art will further appreciate that while the illustrative embodiment depicts two tiers, additional tiers may be added. For example and without limitation, upper cover 20 could define cavities in its outer face and another cover (not shown) could be added with corresponding cavities that would cooperate therewith to receive additional gyroscopes. A three-tier assembly would thus be formed. A four-tier assembly, and so on, could also be formed as desired.
Illustratively, the support assembly 10 is made from polyethylene foam, although other suitable material may be used. Suitable material illustratively will not produce significant off-gassing. One such suitable foam includes a polyethylene foam sold under the trademark EPERAN. EPERAN illustratively comprises a Class A, non-abrasive polyethylene, that has improved wear and environmental characteristics, and is readily available in various colors and densities. Like other polyethylene foams, EPERAN also maintains it surface texture, and does not flake off to any significant extent. Additionally, EPERAN is a non-abrasive material, so it will not scratch the equipment, device(s) or container(s) during use. Illustratively, while the material can be molded, it can also be cut to the desired specifications including the desired shape, size and dimensions. One suitable method of cutting material into the desired shape(s) includes water cutting. The ability to cut the material illustratively eliminates hazardous aspects of, and special safety equipment used in the heretofore used molding process. The cavities may also be cut to the desired shape and size. The components and their respective cavities may also be formed through a combination of cutting and joining together, for example with adhesives, heat, or other suitable joining means, various pieces. For example, one or more thicknesses of material may be cut into one or more desired shapes. These thicknesses or pieces may be joined together with an adhesive, for example and without limitation a pressure sensitive adhesive such as FT 8328, or other suitable means, to form the desired internal and external geometries of the support assembly components. The assembly illustratively may then be treated to condition the material. For example, the material may be baked at a suitable temperature, for example 140° F. to 150° F., for a suitable amount of time, for example, 20 to 40 hours, to condition the material. In one illustrative embodiment, it may be baked at 145° F. for 30 hours. One suitable means of cutting comprises water or water-jet cutting, although laser cutting, air cutting, chemical cutting, and blade cutting and the like may also be used. Illustratively, the cavities 23, 24, 33, 34, 43A, 43B, 44A, 44B, may comprise any shape, regular or irregular, and size suitable to receive, nestle, support and generally stabilize the device to be received therein through an interference fit. Similarly, although the illustrative embodiment is generally cylindrical, any suitable shape may be used. Because the material may be cut, rather than having to use a mold to form the components, which molding process may be expensive and which confines the support to shapes according to the mold, the illustrative support assembly illustratively may be relatively easily and cheaply manufactured. In addition, the support assembly may be modified relatively easily to accommodate supporting therein different devices, even within the same assembly, and/or being received within different containers. Unlike in the case of a molded material, which requires that a mold insert must be redone or fashioned anew to accommodate changes to the supporting assembly's structure, here, the cutting, which may for example be computer controlled, need only be changed. Thus, the illustrative device and methods of use and manufacture described herein can be utilized for other military gyroscopes and sensitive devices that require shipment in the same manner as described herein. The same material and process can be utilized, with revisions to the computer model to account for the different internal and/or external geometry.
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It will be appreciated that the components and their respective recesses or cavities, may be fashioned into any desired shape having any desired dimensions. Such sizes and shapes may be determined by the device to be supported. For example, the internal cavities may be strategically sized and placed to maximize protection and capacity in the volume of the support assembly. In addition, the support assembly may be fashioned to fit inside another container, in which case the outer geometry of the support assembly illustratively would be sized and shaped to fit within any such container. For example, the illustrative support assembly, which will receive and nestle, cradle or support one to four gyroscopes, may itself be received within another container, for example a heat exchanger or heater assembly. So, too, the support assembly could be received directly into a shipping or storage container. In one illustrative embodiment, the support assemble is received within a heater assembly or container, which in turn is received within a shipping or storage container. In any event, the support assembly, alone or in combination with one or more containers within which it may be received, illustratively provides any device received and nestled therein, support, insulation from the ambient environmental conditions (e.g., temperature, moisture, precipitation, wind, radiation, and the like), as well as shock and vibration mitigation during storage and/or transport. In one illustrative example, one or more gyroscopes may be received within the support assembly and held or fastened together in a layered or stacked relationship with a binding member, such as for example and without limitation a metal strap. The support assembly may then be inserted into or received within another container, such as for example a heat exchanger, which in turn may be inserted or received in another container, such as for example a shipping or storage container. The heater illustratively regulates the temperature of the device at some desired temperature. For example, the heater may keep the interior of the heat exchanger at a temperature of about 100° F. to about 160° F., or some other desired temperature such as for example 145° F. Illustratively, the improved support assembly is generally cylindrical to fit inside existing heat exchanger assemblies. It will be appreciated; however, that the support assembly may be fashioned into other shapes, both regular and irregular, as desired. As noted, the illustrative layered embodiment allows the improved support assembly to be received within existing heater assemblies and/or shipping containers. Although the improved support assembly may be received within existing heaters/containers, its layered design allows it to receive and support additional devices than can be received within the support assemblies currently being received within those same existing heater assemblies and/or shipping containers.
While the invention has been illustrated and described in detail in the foregoing drawings and description, the same is to be considered as illustrative and not restrictive in character, it being understood that only illustrative embodiments thereof have been shown and described and that all changes and modifications that come within the spirit of the invention are desired to be protected.
This application claims priority to and the benefit of U.S. Provisional Patent Application No. 61/082,609, filed 22 Jul. 2008, the disclosure of which is now expressly incorporated herein by reference.
The invention described herein was made in the performance of official duties by an employee of the Department of the Navy and may be manufactured, used, licensed by or for the United States Government for any governmental purpose without payment of any royalties thereon.
Number | Date | Country | |
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61082609 | Jul 2008 | US |