Many storage containers, such as mobile storage containers for box or van-type trailers, include side walls and a roof assembly formed by multiple panel members coupled together. The panel members can be made from various types of materials in different configurations.
Some embodiments of the invention can provide a panel for use on a trailer. The panel can include a panel member core with a length and can including a first segment of thermoplastic foam extending the length and a second segment of thermoplastic foam extending the length adjacent the first segment. The first segment can have a first density and the second segment can have a second density. The first density can be greater than the second density. A sheet can extend over the first and second segments and a can be laminated to the panel member core. The panel member core can be formed by extrusion.
Other embodiments of the invention can provide a method of forming a panel for use on a trailer. The method can include extruding a panel member core of thermoplastic foam with a first region that can have a first density and a second region, adjacent the first region, that can have a second density. The second density can be less than the first density. The panel member core can be cut at a predetermined length. A sheet can extend over the first and second regions and can be laminated to the panel member core.
Other embodiments of the invention can provide a method for forming a panel member core with a length for a panel that can be used in a trailer. The method can include extruding a first region, a second region, a third region, a fourth region, and a fifth to extend along the length in parallel. The first, third, and fifth region can be configured to have a greater density than the second region and the fourth region. The extruded first, second, third, fourth, and fifth regions can be cut to the length.
The accompanying drawings, which are incorporated in and form a part of this specification, illustrate embodiments of the invention and, together with the description, serve to explain the principles of embodiments of the invention:
Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of “including,” “comprising,” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Unless specified or limited otherwise, the terms “mounted,” “connected,” “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
The following discussion is presented to enable a person skilled in the art to make and use embodiments of the invention. Various modifications to the illustrated embodiments will be readily apparent to those skilled in the art, and the generic principles herein can be applied to other embodiments and applications without departing from embodiments of the invention. Thus, embodiments of the invention are not intended to be limited to embodiments shown, but are to be accorded the widest scope consistent with the principles and features disclosed herein. The following detailed description is to be read with reference to the figures, in which like elements in different figures have like reference numerals. The figures, which are not necessarily to scale, depict selected embodiments and are not intended to limit the scope of embodiments of the invention. Skilled artisans will recognize the examples provided herein have many useful alternatives and fall within the scope of embodiments of the invention.
For the purposes of promoting an understanding of the principles of the invention, reference will now be made to illustrative embodiments shown in the attached drawings and specific language will be used to describe the same. Some of the discussion below describes a laminated panel member core that can be sandwiched between sheets formed from metal, plastic, reinforced plastic, or high modulus materials such as carbon fiber or aramid fiber. The context and particulars of this discussion are presented as examples only. For example, embodiments of the disclosed invention can be configured in various ways, including with other shapes and arrangements of elements. Similarly, while the concepts of this disclosure are described in relation to a truck trailer, it will be understood that they are equally applicable to other mobile or stationary storage enclosures or containers, as well as refrigerated and un-refrigerated trailers, storage containers, or truck bodies that include wall and/or roof panels joined together.
As used herein, directional terms including “top,” “bottom,” “side,” “horizontal,” “vertical,” and so on are used to indicate directional relationships with respect to an arbitrary reference frame (e.g., a reference frame of a particular figure or figures). These directional terms are used consistently relative to a particular embodiment. For example, a “top” feature of an embodiment is opposite a corresponding “bottom” feature, and a “horizontal” feature generally extends perpendicularly to a “vertical” feature. However, unless otherwise defined or limited, these directional terms are not intended to indicate an absolute reference frame for a particular assembly.
In conventional arrangements, panel members can be made from various types of materials in different configurations. For example, panel members can be made with hexagonal honeycomb cores that have a uniform internal structure and in which the axis of each honeycomb cell extends perpendicular to the length and width of the adjacent sheets. Cargo securement elements or fasteners must therefore be located in areas at or near the seams of adjacent panels where additional overlapping material is provided. Another example includes panel members comprising a core partially formed from a foamed thermoplastic and include higher density foam blocks inserted manually in locations in areas needing additional structural support. Although these conventional arrangements of panels can provide adequate structural strength and support for fasteners, mounting and fastening options for cargo securement elements and fasteners are limited and labor can be fairly intensive to manufacture the panel members.
Embodiments of the invention can address these or other issues. For example, in some embodiments, a panel member core can include areas of different densities. Some areas may be formed with higher density foam, respectively, for securing mounting elements or fasteners thereto, while other areas may be formed with lower density foam to reduce the overall weight of the panel member. As another example, other regions within the panel core can have densities between the densities of the higher and lower density regions. An example of the process for making a panel member core can include the extrusion and combination of streams of thermoplastic foam having the same or different densities. In some examples, the thermoplastic can be high density polyethylene (HDPE) or polypropylene (PP).
As shown in
The first, third, and fifth streams 122, 124, 126 each have a first density, and the second and fourth streams 132, 134 each have a second density. In the example, the first density of the first, third, and fifth streams 122, 124, 126 extruded from the first extruder 120 can be greater than the second density of the second and fourth streams 132, 134 extruded from the second extruder 130. For example, the first density can be in the range of about 14 lb/ft3 to about 30 lb/ft3 and the second density can be in the range of about 1 lb/ft3 to about 13 lb/ft3. The streams 122, 124, 126, 132, 134 can be thermally welded together to form a single continuous panel member core stream 118, which can be cut to a predetermined dimension to form the panel member core 116 (
The first, third, and fifth segments 150, 152, 154 are shown with widths that are smaller than the widths of the second and fourth segments 156, 158. However, other configurations with segments of different widths are contemplated, including the inverse of the panel member core 116, and the figures should not be viewed as limiting.
In other embodiments, other configurations are possible. For example, more or fewer alternating extrusion streams of different or similar densities can be combined to form a panel member core as determined by the predetermined structural and weight requirements. For example, in some embodiments, the first, third, and fifth streams 122, 124, 126 can each have a different density. In some embodiments, two of the first, third, and fifth streams 122, 124, 126 can have the same density and the other of the first, third, and fifth streams 122, 124, 126 can have a lesser or a greater density. In some other embodiments, the densities of the second and fourth streams 132, 134 can be different. In some embodiments, at least two of the densities of the first, second, third, fourth, and fifth streams 122, 132, 124, 134, 126 can be the same.
A weld zone 138 can be formed between any two adjacent, thermally welded extrusion streams, for example, between the second stream 132 and the third stream 124 shown in
At least the first set of regions 240 of the panel member core stream 218 can be compressed to a third thickness 238 (
The compression of the first, third, and fifth regions 222, 224, 226 and the second and fourth regions 232, 234 to the third thickness 238 increases the density of the first, third, and fifth regions 222, 224, 226 relative to the second and fourth regions 232, 234. In the example provided, the density of the first, third, and fifth regions 222, 224, 226 is approximately double the density of the second and fourth regions 232, 234 because the first, third, and fifth regions 222, 224, 226 were about twice the thickness of the second and fourth regions 232, 234 in the panel member core extrusion 218 and were compressed to the same thickness of the second and fourth regions 232, 234 in the panel member core stream 218.
After compression, the first, third, and fifth regions 222, 224, 226 can have a first density and the second and fourth regions 232, 234 can have a second density. The first density can be in the range of about 14 lb/ft3 to about 30 lb/ft3 and the second density can be in the range of about 1 lb/ft3 to about 13 lb/ft3. The panel member core stream can be cut to a predetermined dimension to form the panel member core 216 (
Similar to the example method of forming the panel member core 116 described above, the panel member core stream 218 can be cut to a predetermined dimension to form the panel member core 216 (
The first, third, and fifth segments 250, 252, 254 are shown with widths that are smaller than the widths of the second and fourth segments 256, 258. However, other configurations with segments of different widths are contemplated, including the inverse of the panel member core 216, and the figures should not be viewed as limiting.
In other embodiments, other configurations are possible. For example, more or fewer alternating extrusion stream regions of different thicknesses and different or similar densities can be formed to provide a panel member core 216as determined by the predetermined structural and weight requirements.
Thus, the above-described methods for forming panel member cores can form panel member cores having different strength and weight characteristics. Areas within the panel member cores having a greater density can provide additional strength to reduce fastener tear out where hardware is bonded thereto or where panels are joined together. Areas within the panel member cores having a lower density, respectively, can reduce overall panel weight in areas in which additional strength is not required.
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. Furthermore, it will be understood that the embodiments discussed above are presented as examples only, and that other embodiments are possible. Moreover, it is intended and will be appreciated that embodiments may be variously combined or separated without parting from the invention. For example, it will be appreciated that all preferred features described herein are applicable to all aspects of the invention described herein.
The description herein of the disclosed embodiments is provided to enable any person skilled in the art to make or use the invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein can be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
This application claims priority under 35 U.S.C. § 119 to U.S. Provisional Patent Application No. 62/947,926, filed Dec. 13, 2019, the entire contents of which are incorporated herein by reference.
Number | Date | Country | |
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62947926 | Dec 2019 | US |