Not applicable.
1. Field of the Invention
The present invention relates to foldable, connectable panel assemblies for use in building structures and other structures where the panel assemblies may be utilized. More specifically, the present invention relates to a system for interconnecting panel assemblies, providing for rotatability of one panel assembly relative to another around an axis of rotation, and providing for securing the interconnection of one panel assembly with respect to another panel assembly in a fixed, lockable relationship. Additionally, this invention provides with a fastenerless connection between the construction panel its perimeter trims.
2. Description of the Related Art
Pre-fabricated, foldable, portable building structures have been developed to enable shipment of structures in a collapsed form while facilitating the erection of those buildings at their installation site. One objective in developing pre-fabricated, foldable, portable buildings is to provide for maximum square footage of erected structure while retaining a minimum volume and weight of the structure in its collapsed form for shipping purposes. This avoids the unnecessary transportation of air volume within the structure, resulting in more economical transportation of such structures. At the same time, hingedly joining components of the structure to fold when collapsed facilitates erection of these structures at the erection site by unskilled labor at considerable cost and time saving.
The successful development and introduction of containerized transportation, involving the loading of fixed-dimension containers aboard land, sea, and air modes of transportation specially adapted for standard container sizes, has provided considerable cost benefit and generally provides safer and quicker worldwide freight transportation. The I.S.O. freight containers have been universally adopted by most modern modes of transportation, and practically every country in the world is now capable of handling and delivering such containers, making it possible to economically ship I.S.O. freight containers to practically any destination in the world.
Given the benefits associated with containerized transportation, the development of a pre-fabricated, foldable, portable building that is collapsible to fit within the outside dimensions of shipping containers meeting I.S.O. standards is desirable. One problem associated with the development of a pre-fabricated, foldable, portable building is a sufficiently robust and maneuverable interconnection system for interconnection of panel assemblies that compose the foldable building.
Current designs for interconnection systems are not maximally efficient in terms of use of the available space, do not interconnect panel assemblies with adequate fixation, resulting in weak connections, create unwanted heat transfer at the connections of adjacent panel assemblies, and inadequately seal the space between sides of the panel assembly to prevent fluid flow therebetween. Accordingly, there exists a need for an optimized panel assembly that addresses such deficiencies.
The present invention system for interconnection multiple panel assemblies comprises a first bracketing body having a first bearing member and at least one planar member; a second bracketing body having a second bearing member pivotally engaged with the first bearing member and at least one planar member; a third bracketing body having at least one planar member; a fourth bracketing body having at least one planar member; a first panel receiving volume at least partially defined by the at least one planar member of the first and third bracketing bodies; a second panel receiving volume at least partially defined by the at least one planar members of the second and fourth bracketing bodies; and wherein the at least one planar members of the second and fourth bracketing bodies at least partially define a second panel receiving volume. According to another aspect of the present invention, a first thermal insulating body is positioned between and separates the first and third bracketing bodies, and a second thermal insulating body positioned between and separates the second and fourth bracketing bodies. According to yet another aspect of the present invention, a fastenerless connection is provided between surfaces of the system and the panel assemblies.
The first bracketing 32 body is preferably fixed to a panel assembly with fasteners, such as rivets 47. Alternative embodiments contemplate panel engaging members, in conjunction with or instead of fasteners, extending from the engaging surfaces. In one alternative embodiment of the first bracketing body 32, shown in
A first channel beam 51 having a generally C-shaped cross section is formed integrally with and extends from the free end 40 to the first planar member 34. A non-engaging surface 45 of the first planar member 34 opposite its engaging surface 44 and the channel beam 51 has a concave interior curved surface 52 which defines a first insulating volume 54. Still referring to
The hinge pin 59 has a convex first bearing surface 58 having a first radius R1 from a first axis 60. The bearing arm 57 has interior second bearing surfaces 62 having a second radius R2 from the first axis 60 and a convex exterior third bearing surface 64 having a third radius R3 from the first axis 60. The bearing arm 57 terminates at an end surface 76 extending between the second and third bearing surfaces 62, 64.
A stop member 65 extends from the exterior third bearing surface 64. This stop member 65 comprises two preferably parallel opposing first and second stopping surfaces 68, 70 extending between the third bearing surface 64 and a convex fourth bearing surface 66 having a fourth radius R4 from the first axis 60.
As shown jointly in
First and second inner stopping surfaces 72, 74 comprise the sides of the bridging member 61 and extend between the first and second bearing surfaces 58, 62. Each of the first and second inner stopping surfaces 72, 74 are coplanar with reference planes P1, P2 extending through the first axis 60. A first partially-toroidal slot 78 is defined by the first inner stopping surface 72 and the first and second bearing surfaces 58, 62. A second partially-toroidal slot 80 is defined by the second inner stopping surface 74 and the first and second bearing surfaces 58, 62. A planar first support surface 82 is positioned adjacent to the second bearing surface 62 and extends between the non-engaging surface 45 of the first planar member 34 and the second bearing surface 62.
Referring to
The second bracketing body 84 is preferably fixed to a panel assembly with fasteners, such as a row of rivets 99. Alternative embodiments contemplate panel engaging members, in conjunction with or instead of fasteners, extending from the engaging surfaces. In one alternative embodiment of the second bracketing body 84, shown in
A second channel beam 91 having a generally C-shaped cross section is formed integrally with and extends from a non-engaging surface 97 of the third planar member 86 adjacent its free end 92. The second channel beam 91 has a concave interior curved surface 104 which defines a second insulating volume 106.
Still referring to
As shown in
A first stopping surface 122 extends between the seventh and eighth bearing surfaces 116, 118 and is co-planar with a reference plane P3 extending radially through the second axis 112. The second stopping surface 124 extends between the eighth and ninth bearing surfaces 118, 120 and is co-planar with a reference plane P4 extending radially through the second axis 112. The third stopping surfaces 126 extends from the ninth bearing surface 120 and is positioned adjacent the second junction 90 of the third and fourth planar members 86, 88. The hinge barrel 129 has an outer end surface 128 which extends between the fifth and sixth bearing surfaces 110, 114, and an inner end surface 130 extends between the fifth and seventh bearing surfaces 110, 116. A planar second support surface 132 is positioned adjacent to the sixth bearing surface 114 forming a portion of the exterior surface of the second bearing arm 108.
The third bracketing body 134 is preferably fixed to a panel assembly with fasteners, such as a row of rivets 145. Alternative embodiments contemplate panel engaging members (i.e., ridges or individualized extruded teeth), in conjunction with or instead of fasteners, extending from the engaging surfaces, as shown and described with reference to the first and second bracketing bodies 32, 84 and
A third channel beam 153 having a generally C-shaped cross section is continuous and extends from and is formed integrally with the non-engaging surface 147 of the fifth planar member 136 proximal its free end 142. The third channel beam 153 has a concave interior curved surface 154 defining a third insulating volume 156.
First and second engagement fins 158, 160 extend generally perpendicular from the non-engaging surface 147 of the fifth planar member 136 to partially define therebetween a first sealing volume 162 proximal to the junction 140. Retaining members 161 are angle toward the fifth planar member 136 extend from the planar surfaces of the first and second engagement fins 158, 160 that define the sealing volume 162. In the preferred embodiment, the retaining members 161 are ridges. In alternative embodiments the retaining members 161 are a plurality of individualized extruded teeth.
The fourth bracketing body 164 is preferably fixed to a panel assembly with fasteners, such as a row of rivets 175. Alternative embodiments contemplate panel engaging members (i.e., ridges or individualized extruded teeth), in conjunction with or instead of fasteners, extending from the engaging surfaces, as shown and described with reference to the first and second bracketing bodies 32, 84 and
A fourth channel beam 183, having a C-shaped cross section, is continuous with and extends from the non-engaging surface 177 of the seventh planar member 166 proximal its free end 172. The fourth channel beam member 183 has a concave interior curved surface 184 defining a fourth insulation volume 186.
Third and fourth engaging fins 188, 190 extend generally perpendicular from the non-engaging surface 177 of the seventh planar member 166 to define a second sealing volume 192 therebetween. The third engaging fin 188 is coplanar with the eighth planar member 168 and has a free end 194 that curves toward the fourth engagement fin 190. Retaining members 196 angled toward the seventh member 166 extend from the planar surfaces of the third and fourth engagement fins 188, 190 that define the sealing volume 192. In the preferred embodiment, the retaining members 196 are ridges extending along the length of the planar surfaces. In alternative embodiments the retaining members 196 are a plurality of individualized extruded teeth.
The first and third channel beams 51, 153 of the first and third bodies 32, 134, respectively, are mechanically connected with a first insulating body 198 positioned in a space between the first and third channel beams 51, 153. The first insulating body 198 is rigid, made of an insulative material such as a thermally nonconductive resin, portions of which are shaped to fit within the first and third insulating volumes 54, 156. Preferably, such a resin is poured into the insulating volumes 54, 156 and the space therebetween in a liquid state and allowed to harden. The interior curved surface 52, 154 of the first and third channel beam members 51, 153, respectively, secure the first and third bracketing bodies 32, 134 to the first insulating body 198.
The planar engaging surfaces 44, 46, 146, 148 of the first bracketing body 32 and the third bracketing body 134 form an assembly having a square U-shaped cross section which defines a first panel receiving volume 200. As shown in
The first panel assembly 26 itself comprises a layer of insulative core material (e.g., polystyrene) 202 positioned between two reinforcing layers 204, 206 that provide structural rigidity to the intermediate layer 202. In the preferred embodiment, the first and second reinforcing layers are metallic.
In the same manner as described with regard to the first and third bracketing bodies 32, 134, the second and fourth bracketing bodies 84, 164 are mechanically connected with a thermally non-conductive second insulating body 207 wherein the second insulating body 207 is positioned between the second and fourth channel beams 91, 183 and secured with the second and fourth insulating volumes 106, 186. In this position, the third planar member 86 of the second body 84 is in co-planar alignment with the seventh planar member 166 with a space 37 between the respective free ends 92, 172. Also in this position, the fourth and eighth planar members 88, 168 of the second and fourth bracketing bodies 84, 164, respectively, extend in the same direction wherein the planar engaging surfaces 146, 148, 176, 178 of the second and fourth bracketing bodies 84, 164 form an assembly with a square U-shaped cross section defining a second panel receiving volume 208. One end of the second panel assembly 28, also comprising a layer of insulative core material 210 positioned between two preferably metallic reinforcing layers 212, 214, is positioned within the second panel receiving volume 208.
Still referring to
Use of the preferred embodiment of the hinge assembly 22 is initially described with reference to
As shown in
As shown in
Referring back to
When the panel assemblies 26, 28 are in the aligned position as shown in
The first bracketing body 230 comprises a base planar member 232 with a first end 234 and a second end 236. A first engagement fin 238 extends at a right angle from the first end 234 of the base planar member 232. A side planar member 240 extends at a right angle from the second end 236 of the base planar member 232. A second engagement fin 246 extends from the base member 232 at a position between the side planar member 240 and first engagement fin 238 at a right angle. The base planar member 232 and the side planar member 240 both have planar engaging surfaces 233, 241 and non-engaging surfaces 235, 243.
The first bracketing body 230 is preferably fixed to the panel assembly 328 with fasteners, such as a row of rivets 245. A first channel beam 247, having a generally C-shaped cross section, is positioned at and formed integrally with the free end of the second engagement fin 246. The first channel beam 247 has a curved concave interior surface 248 which defines a first insulating volume 250. The first engagement fin 238, the second engagement fin 246, and the base member 232 define a first sealing volume 252 having a generally square U-shaped cross section. Retaining members 226 are located within the first seal forming volume 252. In the preferred embodiment, the retaining members 196 are ridges. In alternative embodiments the retaining members 226 are a plurality of individualized extruded teeth.
As shown in
The second engagement fin 246 and the second bracketing body 254 are positioned with respect to each other such that the open ends of the first and second channel beams 247, 261 face each other with a space 267 between. The channel beams 247, 261 are mechanically connected by a rigid first insulating body 268 (i.e., a thermally-nonconductive, hardened resin) shaped to fit within the first and second insulating volumes 250, 264 and a portion of the space 267 between the channel beams 247, 261. In this manner, the second bracketing body 254 is fixed relative to, but not in direct contact with, the first bracketing body 230.
A third channel beam 281 having a generally C-shaped cross section is formed integrally with and positioned at the free end of the side planar member 278. The third channel beam 281 has a concave curved interior surface 282 which defines a third insulating volume 284.
A third engagement fin 280 is formed integrally with and extends from the third channel beam 281 in a direction generally toward the base planar member 272. The third engagement fin 280 is spaced from and generally parallel with the side planar member 278 forming a second sealing volume 289 defined by the third engagement fin 280, the third channel beam 281 and the side planar member 278.
As shown in
The fourth bracketing body 290 is preferably fixed to the panel assembly 330 with fasteners, such as a row of rivets 287. A fourth channel beam 292, having a generally C-shaped cross section, is formed integrally with and positioned at the free end of the side planar member 293. The fourth channel beam 292 has a concave curved interior surface 294 forming a fourth insulating volume 296. A partially-cylindrical bearing surface 300 is formed in the exterior surface 295 of the fourth channel beam 292, the non-engaging surface 301 of the side planar member 293 and a curved surface 203 of a bearing fin 298 extending from the non-engaging surface 301. The side planar member 278 of the third bracketing body 270 is positioned with respect to the side planar member 293 of the fourth bracketing body 290 such that the open ends of the third and fourth channel beams 281, 292 face each other with a space 303 therebetween. The channel beams 281, 292 are mechanically connected by a second insulating body 322 (i.e., a thermally-nonconductive, hardened resin) shaped to fit within the third and fourth insulating volumes 284, 296 and a portion of the space 303 between the channel beams 281, 292. In this manner, the third bracketing body 270 is fixed relative to, but not in direct contract with, the fourth bracketing body 290.
A locking member 308 having a hinge pin 310 at one end is rotatably connected to the third bracketing body 290 with the hinge pin 310 pivoting within the partially-cylindrical bearing surface 300 and occupying the corresponding partially-cylindrical volume 302 defined by the bearing surface 300. The locking member 308 includes a planar strut member 312 extending from the hinge pin 310 at one end and having a free second end 314. Ridges 316 are formed in the free second end 314 to correspond with the locking engagement surface 266 of the lock-engaging member 254 (see
In the configuration shown in
A rubber sealing element 324 is positioned in the first sealing volume and compressed therein by the third engagement fin 280. Sealing element 326 occupies the second sealing volume 289 and is compressed therein by the first engagement fin 238. In this manner, the sealing elements 324, 326 inhibit fluid flow into the interior space 330.
To use the connection assembly 24, the first and third panel assemblies 26, 30 are inserted into the fourth and third panel receiving volumes 330, 328, respectively, and fixed thereto with fasteners, such as rows of rivets 245, 277, 287.
As shown in
As described above, the sealing elements 324, 326 inhibit moisture and other fluids from passing through the connection assembly 24 between first and third panel assemblies 26, 30. In addition, the sealing elements 324, 326 create a biasing force that urges the first bracketing body 230 and the third bracketing body 270 apart and at the same time urges the ridges 316 of the locking member 308 into the ridges 365 of the locking engagement surface 266 of the second bracketing body 254. This inhibits inadvertent disengagement of the locking member 308 from the locking engagement surface 266. Retaining members 332 in the first and second sealing volumes 252, 289, respectively, inhibit egress of the sealing elements 324, 326 from those volumes.
As shown in
The present invention is described above in terms of preferred illustrative embodiments of a specifically described interconnection system. Those skilled in the art will recognize that alternative constructions of such a system can be used in carrying out the present invention. Other aspects, features, and advantages of the present invention may be obtained from a study of this disclosure and the drawings, along with the appended claims.
This divisional application is a division of and claims the benefit of U.S. patent application Ser. No. 14/475,218 filed Sep. 2, 2014, which is a continuation application and claims the benefit of and priority to PCT Application No. PCT/US2012/027597 filed Mar. 2, 2012 which is incorporated by reference herein.
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Moon, Kihwan “International Preliminary Report on Patentability (Chapter 1 of the Patent Cooperation Treaty),” dated Sep. 2, 2014, Applicant Name: Vantem Modular, LLC, Applicant File Ref: P-10214PCT; International Application No. PCT/US2012/027597; International Filing date Mar. 2, 2012. |
Number | Date | Country | |
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20150275558 A1 | Oct 2015 | US |
Number | Date | Country | |
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Parent | 14475218 | Sep 2014 | US |
Child | 14736168 | US |
Number | Date | Country | |
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Parent | PCT/US2012/027597 | Mar 2012 | US |
Child | 14475218 | US |