WO2016123038A1 - Expandable panel - Google Patents

Expandable panel Download PDF

Info

Publication number
WO2016123038A1
WO2016123038A1 PCT/US2016/014772 US2016014772W WO2016123038A1 WO 2016123038 A1 WO2016123038 A1 WO 2016123038A1 US 2016014772 W US2016014772 W US 2016014772W WO 2016123038 A1 WO2016123038 A1 WO 2016123038A1
Authority
WO
WIPO (PCT)
Prior art keywords
inner core
sections
outer facing
collapsible
panel structure
Prior art date
Application number
PCT/US2016/014772
Other languages
English (en)
French (fr)
Inventor
Michael M. STEVENSON
Original Assignee
Cordion Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Cordion Corporation filed Critical Cordion Corporation
Priority to EP16743918.1A priority Critical patent/EP3250773A4/en
Priority to JP2017558354A priority patent/JP2018503762A/ja
Priority to CA2974436A priority patent/CA2974436A1/en
Priority to AU2016211704A priority patent/AU2016211704A1/en
Publication of WO2016123038A1 publication Critical patent/WO2016123038A1/en

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/343Structures characterised by movable, separable, or collapsible parts, e.g. for transport
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B9/00Ceilings; Construction of ceilings, e.g. false ceilings; Ceiling construction with regard to insulation
    • E04B9/04Ceilings; Construction of ceilings, e.g. false ceilings; Ceiling construction with regard to insulation comprising slabs, panels, sheets or the like
    • E04B9/0414Ceilings; Construction of ceilings, e.g. false ceilings; Ceiling construction with regard to insulation comprising slabs, panels, sheets or the like being foldable, curvable or rollable
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/343Structures characterised by movable, separable, or collapsible parts, e.g. for transport
    • E04B1/34384Assembling details for foldable, separable, collapsible or retractable structures

Definitions

  • the subject matter described herein relates to an expandable panel structure that includes a collapsible portion and, in some implementations, can further include one or more longitudinal support structures.
  • aspects of the current subject matter can include a compressible panel that has a collapsible portion and, in some implementations, can further include one or more longitudinal support structures.
  • an apparatus in a first aspect, includes a collapsible panel structure configured to form an expanded configuration and a collapsed configuration.
  • the collapsible panel structure includes outer facing sections forming a first side and a second side of the collapsible panel structure, and inner core sections arranged in a zig-zag manner between the first side and the second side with vertex hinge points pivotally coupling adjoining inner core sections.
  • the first and second sides include facing pair hinge points that pivotally couple adjoining outer facing sections.
  • the inner core sections and the outer facing sections form a series of adjoining triangular prisms when the collapsible panel structure is in the expanded configuration, and the inner core sections and outer facing sections form a series of adjoining quadrilateral prisms when the collapsible panel structure is transitioning into the collapsed configuration.
  • an apparatus in a second, interrelated aspect, includes a collapsible panel structure configured to form an expanded configuration and a collapsed configuration.
  • the collapsible panel structure includes outer facing sections forming a first side and a second side of the collapsible panel structure, inner core sections arranged in a zig-zag manner between the first side and the second side with inner core hinge points that pivotally couple adjoining inner core sections, extensions that extend between each coupling of an inner core section and an inner core hinge point thereby offsetting the inner core hinge point from a longitudinal length of the inner core section, and supplemental hinge points that pivotally couple adjoining outer facing sections and inner core sections.
  • the first and second sides include facing pair hinge points that pivotally couple adjoining outer facing sections.
  • the inner core sections, the extensions, and the outer facing sections form a series of adjoining quadrilateral prisms when the collapsible panel structure is in the expanded configuration, and wherein the inner core sections, the extensions, and the outer facing sections form a series of adjoining six-sided prisms when the collapsible panel structure is transitioning into the collapsed configuration.
  • a method includes expanding a collapsible portion of a collapsible panel structure along an axis perpendicular to faces of a plurality of inner core sections of the collapsible panel structure; and completing the expanding of the collapsible portion upon planar alignment of two outer facing sections of the collapsible panel structure joined at a facing pair hinge point that is disposed opposite a vertex hinge point joining two of the inner core sections.
  • the inner core sections are arranged in a zig-zag manner between a first side of outer facing sections and a second side of outer facing sections with vertex hinge points pivotally coupling adjoining inner core sections.
  • a method can optionally include joining a longitudinal support structure to the expanded collapsible portion, subsequently removing the longitudinal support structures, and re-collapsing the collapsible portion.
  • a method includes expanding a collapsible portion of a collapsible panel structure along an axis perpendicular to faces of a plurality of inner core sections of the collapsible panel structure and completing the expanding of the collapsible portion upon planar alignment of two outer facing sections of the collapsible panel structure joined at a facing pair hinge point that is disposed opposite an inner core hinge point joining two of the inner core sections.
  • the inner core sections are arranged in a zig-zag manner between a first side of outer facing sections and a second side of outer facing sections with inner core hinge points pivotally coupling adjoining inner core sections and are offset from longitudinal lengths of the adjoining inner core sections by extensions.
  • Supplemental hinge points pivotally couple adjoining outer facing sections and inner core sections.
  • a method can optionally include joining a longitudinal support structure to the expanded collapsible portion, subsequently removing the longitudinal support structures, and re-collapsing the collapsible portion.
  • a support structure can be included to extend along a length of the collapsible panel structure in the expanded configuration.
  • the support structure can include one or more of an open channel that is configured to cap a first end of the collapsible panel structure, a telescoping segment that allows the support structure to at least partially collapse, and a plurality of joinable segments.
  • the support structure can extend through openings located along the inner core sections.
  • the support structure can be curved.
  • the vertex hinge points can optionally be located at an apex of each triangular prism of the series of adjoining triangular prisms when the collapsible portion is in the extended configuration.
  • Two outer facing sections jointed at a facing pair hinge point can be aligned with an opposite vertex hinge point joining two inner core sections.
  • a facing pair hinge point of the facing pair hinge points is located at a top or a bottom of each quadrilateral prism of the series of adjoining quadrilateral prisms.
  • two outer facing sections can optionally be in an alignment and jointed at a facing pair hinge point that is disposed opposite an inner core hinge point when the collapsible portion is in the extended configuration.
  • the facing pair hinge points and inner core hinge points can be alternately located at a top and a bottom of each hexagonal prism of the series of adjoining quadrilateral prisms.
  • FIG. 1 A is a front elevation view of a compactable, light-weight panel according to some embodiments
  • FIG. IB is a partially exploded perspective view of the compactable, light-weight panel of FIG. 1A;
  • FIG. 1C is a front elevation view of a compactable, light-weight panel with a collapsible portion that can slide onto longitudinal support structures, according to some embodiments;
  • FIG. ID is a partially exploded perspective view of the compactable, light-weight panel of FIG. 1C;
  • FIG. 2 is a cross-sectional view of the compressible portion of the panel of FIGs. 1A - ID;
  • FIG. 3 is a view of the compressible portion of the panel of FIG. 2 when it is compressed
  • FIGs. 4A-4C show a cross-sectional view of the compressible portion of a light-weight panel that is curved along its expansion length which is representative of some embodiments;
  • FIG. 5 shows a view of a compactable, light-weight panel that is expandable to form a curved structure
  • FIG. 6 shows a process flow chart illustrating features of a method consistent with implementation of the current subject matter
  • FIG. 7 shows a partially exploded perspective view of a compactable, light-weight panel including supplemental hinge points and inner core hinge points;
  • FIG. 8 shows a cross-sectional view of the compressible portion of the light-weight panel of FIG. 7;
  • FIG. 9 shows a partially exploded perspective view of a compactable, light-weight panel including vertex hinge links
  • FIG. 10 shows a cross-sectional view of the compressible portion of the light-weight panel of FIG. 9.
  • implementations of the current subject matter can include a compactable part and one or more support parts, which can also be referred to as longitudinal support parts. Implementations of the current subject matter can be useful in many applications, including but not limited to situations involving assembling structures in areas where it would be prohibitive or unwieldy to bring in conventional building materials, as well as where it may be time intensive to construct shelters using conventional materials. Convenience of assembly, disassembly, transportation, and storage can all be improved relative to existing approaches.
  • FIG. 1 A is a front elevation view of an exemplary construction panel
  • the panel 100 includes two types of components: a collapsible portion 110 and longitudinal support structures 130.
  • the collapsible portion 110 may be an accordion-like structure that can compress down to a small volume or expand out to span a length that is significantly longer than the height of the collapsible portion when it is compacted for transportation or storage.
  • the collapsible portion 110 in its collapsed configuration can have a length that is approximately one tenth the length of the expandable panel when fully expanded.
  • such structures can be lightweight and readily portable (e.g. when collapsed) while providing excellent rigidity.
  • the longitudinal support structures 130 can in some implementations of the current subject matter have a fixed geometry (e.g. they need not be collapsible like the collapsible portion 110).
  • a longitudinal support structure 130 can include one or more telescoping segments or segments that are combinable in other manners such that the longitudinal support structure 130 can be at least partially collapsed for transportation and storage.
  • a longitudinal support structure 130 can be formed of two or more segments that are joinable by any feasible mechanism (e.g. threaded connections, an insertable feature of a first segment that slides into a receiving feature of a second segment, etc.)
  • the collapsible portion 110 includes at least one inner core section 115 and outer facing sections 120 which are above and below the inner core sections 115.
  • the longitudinal support structures 130 can optionally be shaped like caps that fit over the ends of the collapsible portion 110. Other configurations of the longitudinal support structures 130 are also within the scope of the current subject matter, including but not limited to the other variations discussed below.
  • the length of the support structures 130 can correspond at least approximately to the length of the collapsible portion 110 when it is extended to an appropriate, load-bearing length, as seen in FIG. IB, but may extend further, depending upon the application.
  • FIG. IB is a perspective view of the panel 100 of FIG. 1 A.
  • the collapsible portion 110 can be seen to have multiple inner core sections 115 that are sections or strips of material that are arranged in a zig-zag manner, connecting at the edge of each core section 115 to an adjacent core section and/or to an outer facing section 120, either connecting directly by a simple hinge, or by means of an intermediary hinge assembly or other jointed assembly or combination thereof.
  • the hinge, intermediary hinge assembly, or other jointed assembly can include an assembly that is secured to one or more associated outer facing sections and/or inner core sections during assembly of a collapsible portion of a panel.
  • respective outer facing sections and/or inner core sections that join to form a hinge can be manufactured or otherwise formed to include appropriate parts of a structure that forms a hinge when joined with a complementary structure on another outer facing section and/or inner core section along a hinge point (e.g. a facing pair hinge point or a vertex hinge point as described below).
  • the hinges of a collapsible assembly can be separate assemblies attached to associated panel sections, or the hinges can be formed as an integral part of respective panels, or some combination of these approaches can be used.
  • the inner core sections 115 can be shaped as rectangles as in the example shown in FIGs. 1 A to ID or alternatively as other shapes as discussed in greater detail below.
  • the inner core sections 115 make up sides of similar size of a series of adjoining triangular prisms that, with the outer facing sections 120, make up the collapsible portion 110.
  • the outer facing sections 120 complete the triangular prisms of an extended collapsible portion 110.
  • the term "prism” refers to a three-dimensional volume having a cross section that is of a similar shape along an axis of the volume.
  • a triangular prism has a triangular cross-section along an axis passing from one end of an outer facing section to an opposite end of the outer facing section.
  • similar shape indicates that the relative dimensions of the sides of the cross-sectional shape are constant although the size of the cross-sectional shape can vary along the length of the axis.
  • the cross section of the resulting triangular prisms formed by one outer facing section 120 and two inner core sections 115 is a triangle of similar relative dimensions along an axis parallel to the plane of the outer facing section 120.
  • the pattern of inner core sections 115 can bear loads applied perpendicular to the outer facing sections 120 as well as provide some torsional rigidity to a completed panel 100.
  • the collapsible portion 120 extends out along a direction, labeled as the X-axis in FIG. IB.
  • the longitudinal support structures 130 attach to the extended collapsible portion 115 and outer facing sections 120 along the X-axis. It will be understood that the view of FIG. 1 A is effectively a cross- sectional or end view taken along the X-axis.
  • the collapsible portion 110 can slide onto the longitudinal support structures 130.
  • one or more longitudinal support structures 130 can be formed as members that pass through holes or the like formed in the inner core sections 115.
  • FIG. 1C is an elevation view of a collapsible panel with an inner core section 115 which can slide onto longitudinal support structures 130.
  • FIG. ID is a perspective view of the panel shown in FIG. 1C.
  • the panel shown in FIGs. 1C and ID has similar components to the panel 100 of FIGs. 1 A and IB.
  • the panel shown in FIGs. 1C and ID has the same two types of components: a collapsible portion (110 in FIG. 1 A) with an inner core section 115 and outer facing sections 120, as well as longitudinal support structures 130.
  • the longitudinal support structures 130 of FIGs. 1C and ID are shown as poles or tubes with a circular cross-section.
  • the longitudinal support structures 130 can have other cross-sections that can allow for greater flexibility in the overall configuration of the panel. Though the longitudinal support structures 130 in FIGs. 1C and ID are shown near the edges of the panel, the location of the longitudinal support structures 130 can vary. Additionally, though two longitudinal support structures 130 are shown, a panel can have more than two longitudinal support structures 130 or
  • a single longitudinal support structure 130 for example one that is positioned approximately near the horizontal center of the inner core sections 115.
  • the configuration of the panel shown in FIGs. 1C and ID, with longitudinal support structures 130 through the inner core section 115 of the collapsible portion, may allow for panels that have fan-like shapes, panels that are curved, and for panels that are otherwise not planar, as shown in FIG. 5 and described in greater detail below.
  • FIG. 2 shows a cross-sectional view 200 taken along a plane perpendicular to the X-axis of just the collapsible portion 110 of the panel seen in FIGs. 1A and IB.
  • the points at which each segment or section of material of the inner core sections 115 and outer facing sections 120 meet are shown as dots.
  • each vertex hinge point 240 on a first outer facing section 120 is directly across from a facing pair hinge point 235 on the opposite outer facing section 120.
  • each facing pair hinge point 235 becomes the top or bottom point of a collapsing quadrilateral (e.g. a four-sided polygon), and each vertex hinge point 240 becomes a side point of this quadrilateral.
  • a collapsing quadrilateral e.g. a four-sided polygon
  • FIG. 3 shows the collapsible portion 110 of FIGs. 1 A-2 when it is nearly or fully collapsed.
  • the facing pair hinge points 235 can be seen to be the outer most points, each of those points connected to a segment of the outer facing sections 120.
  • a vertex hinge point 240 is located between adjacent sections of outer facing section 120 and inner core sections 115.
  • the collapsible portion 410 includes inner core sections 115 and outer facing sections 420 A and 420B. Each segment of the first outer facing section 420A is slightly longer than each segment of the second outer facing section 420B.
  • each triangular cross-sectional sub-structure formed by two adjoining inner core sections 115 and two expanded, planarly oriented first outer facing sections 420 A opposite the vertex where the two adjoining inner core sections 115 meet has an at least slightly longer base than the adjacent and oppositely oriented triangular cross-sectional sub-structure formed by adjoining inner core sections 115 and two expanded, planarly oriented second outer facing sections 420B.
  • the inner core sections 115 provide the bracing to the collapsible portion 410 that greatly contributes to the rigidity and load-bearing abilities of the panel.
  • the longitudinal support structures 130 may have a suitable degree of curvature to correspond to that of the fully extended collapsible portion 410.
  • the collapsible portion 410 shown in FIGs. 4A-4C have hinge points that are illustrated as points or dots. Facing pair hinge points 235 are located at the interface of two portions of an outer facing section, either 420A or 420B, while vertex hinge points 240 are located at the interface of two portions or segments of the inner core sections 115.
  • FIG. 4B shows the collapsible portion 410 as it is being compressed or collapsed
  • FIG. 4C shows a fully or nearly fully collapsed collapsible portion 410.
  • the triangles of the fully extended view seen in FIG. 4 A are supplanted by the quadrilaterals of FIG. 4C.
  • FIG. 4C shows a fully or nearly fully collapsed collapsible portion 410.
  • these quadrilaterals at the top have the same dimensions as those at the bottom of collapsible portion 110.
  • the top-most quadrilaterals shown in FIG. 4C will have different dimension than the bottom-most shapes of the collapsible portion 410.
  • FIG. 5 is a view of a compactable, lightweight panel 500 that is expandable to form a curved structure.
  • the inner core sections 115 can slide onto the longitudinal support structures 130 (or alternatively, one longitudinal support structure), as in the panel shown in FIGs. 1C and ID.
  • the collapsible portion of the exemplary panel 500 is shown partially expanded along two longitudinal support structures 130.
  • the longitudinal support structures 130 are curved, and as the compressible portion is expanded along the support structures 130, the resulting panel 500 is curved.
  • the collapsible portion can be adapted for the curvature of the longitudinal support structures 130.
  • Adaptations of the compressible portion can include inner core sections 115 and outer facing sections 120 made of materials that can accommodate the curvature of the longitudinal support structures 130, which can have shapes and dimensions (as in FIGs. 4A-4C) that accommodate the curvature of the longitudinal support structures 130 in one or more axes, and the like.
  • Adaptations of the compressible portion can also include facing pair hinge points 235 and vertex hinge points 240 formed of materials that can accommodate the curvature of the longitudinal support structures 130, that are configured to expand and/or contract to accommodate the curvature of the longitudinal support structures 130, and the like.
  • the parts of a panel as described herein may be constructed of one or more materials, which can be selected according to the intended use and/or desired properties of the panel.
  • the outer facing sections of the collapsible portion may include a first material selected for compatibility with an external environment in which the panel will be placed as well as tensile strength, while the inner core sections may include a second material that is chosen for compressive strength with less concern for the external environment.
  • the longitudinal support structures may be formed of even another material that is perhaps more rigid than the outer facing sections.
  • any or all of the parts of a panel may be constructed of the same material.
  • FIG. 6 shows a process flow chart 600 illustrating features of a method consistent with implementations of the current subject matter.
  • a collapsible portion can be expanded along an axis (which can be a curved axis) that is approximately
  • the expanding can be completed when two outer facing sections joined at a facing pair hinge point disposed opposite a vertex hinge point joining two of the inner core sections are aligned in a plane.
  • at least one longitudinal support structure can be joined to the expanded collapsible portion.
  • the at least one longitudinal support structure can be removed, and the collapsible portion can be re-collapsed.
  • FIGs. 7 and 8 show perspective and side views, respectively, of another implementation of a collapsible panel structure 700 including a collapsible portion 110 having inner core hinge points 740 that link adjacent inner core sections 115 together.
  • the inner core hinge point 740 can include one or more extensions 745 that extend between the inner core hinge point 740 and a side of an adjacent inner core section 1 15. As such, each extension 745 can offset the inner core hinge point 740 from the longitudinal length of an inner core section 115 to which the inner core hinge point 740 is connected.
  • the collapsible portion 110 of the panel 700 can also include facing pair hinge points that link two outer facing sections, such as described above.
  • the collapsible portion 110 of the panel 700 can also include supplemental hinge points 710 that connect an outer facing section 120 to an adjacent inner core section 115.
  • a first inner core section 115 can be linked to a second inner core section 115 via an inner core hinge point 740, as well as linked to an outer facing section 120 via the supplemental hinge point 710. Therefore, an inner core section 115 can have a total of four linking points, with two separate links disposed near each end of the inner core section: one to an outer facing section 120 via a supplemental hinge point 710 and a second to another inner core section 115 via an inner core hinge point 740.
  • each facing pair hinge point 235 and inner core hinge point 740 becomes the top or bottom point of a collapsing six-sided polygon (when the collapsible portion of the expandable panel is viewed along an axis parallel to an outer facing section 120, and each supplemental hinge point 710 becomes a side point of this six-sided polygon.
  • the fully expanded configuration e.g. on the left side of FIG.
  • the inner core sections 115, outer facing sections 120, and extensions 745 form linked trapezoids (again, when viewed along an axis parallel to the outer facing sections 120) in which two inner core sections 115 form the angled sides of the trapezoid, while two outer facing sections 120 (including a facing pair hinge point 235) form a base of the trapezoid, and the oppositely disposed extensions 745 (including a inner core hinge point 740) form the top of the trapezoid.
  • the supplemental hinge points 710 can align such that the outer facing sections 120 form a substantially flat configuration (e.g., an extended wall).
  • the supplemental hinge points 710 can align such that a minimal gap is formed between adjacent supplemental hinge points 710.
  • minimal (or even zero) spacing or gaps can be formed between adjacent outer facing sections 120.
  • Such a structure can be useful in applications such as video displays, solar panels, touch screen input displays, optical components, antenna arrays, radiator panels, or the like, in which a continuous or nearly continuous surface without gaps is desirable.
  • FIGs. 9 and 10 show perspective and side views, respectively, of another implementation of a collapsible panel structure 900 including vertex hinge links 910 that include four joints 915a-915d, with each joint having its own axis of rotation.
  • each vertex hinge link 910 can include a first joint 915a and a second joint 915b that pivotally links a first outer facing section 120a and second outer facing section 120b, respectively, to the vertex hinge link 910.
  • the vertex hinge link 910 can include a third joint 915c and a fourth joint 915d that pivotally links a first inner core section 115a and second inner core section 115b, respectively, to the vertex hinge link 910.
  • Each of the joints 915a-915d can include an axis of rotation that allows each of the linked collapsible portion 110 sections (e.g., outer facing sections 120a, 120b and inner core sections 115a, 115b) to independently pivot relative to each other and/or to the vertex hinge link 910.
  • the vertex hinge link 910 can allow all of the linked collapsible portion 110 sections (e.g., outer facing sections 120a, 120b and inner core sections 115a, 115b) to all simultaneously pivot relative to each other and/or to the vertex hinge link 910.
  • the joints 915a-915d can be positioned relative to each other such that they allow the collapsible portion 110 to form a compact collapsed configuration.
  • at least the inner core sections 115 can be positioned approximately parallel to each other and spaced apart from each other by a distance defined by the space between two joints, such as the third joint 115c and fourth joint 115d of an adjacent vertex hinge link 910.
  • the collapsible portion 110 of the panel 900 can also include facing pair hinge points 235 that link two outer facing sections, such as described above.
  • each facing pair hinge point 235 becomes the top or bottom point of a collapsing quadrilateral and each vertex hinge link 910 becomes a side point of this quadrilateral (as above, references to the shapes taken on by the various components of the collapsible portion as it is expanded, collapsed, or is in transition between expanded and collapsed states or vice versa refer to the shapes as viewed "end-on" to the collapsible portion 110, which is also referred to herein as "along an exist parallel to the outer facings sections).
  • the inner core sections 115 and outer facing sections 120 form the sides of linked triangular shapes (e.g. three-sided polygons) where the outer facing sections 120 (including facing pair hinge points 235) form the bottom side of the triangular shapes, and the inner core sections 115 form the sides of the triangular shapes.
  • linked triangular shapes e.g. three-sided polygons
  • the vertex hinge links 910 can allow for improved simplicity in manufacturing and assembly. As discussed above, a single vertex hinge link 910 can allow for the independent pivoting of four separate sections of the collapsible portion 110. As such, reductions in materials use as well manufacturing and assembly complexity can be realized. Additionally, this implementation can allow for greater structural loads and larger applications such as bridges, ramps, temporary piers and docks, and other uses.
  • Non-limiting examples of materials that may be used for the outer facing sections 120 include carbon fiber, polymers, fiber reinforced polymers, plastics, metal, ceramics, polymer reinforced ceramics, metal reinforced ceramics, composite materials, platelet material, chain link or chain mail material, mesh, woven fabric, wood, cardboard, paper, woven natural materials, honeycombed and other cored composites, and the like, including any combination thereof.
  • Polymers may include natural polymers, such as rubber, cellulose, and silk, and synthetic polymers, such as polyethylene, polystyrene, phenol formaldehyde resin, nylon, polyvinyl chloride, polylactic acid, acrylonitrile butadiene styrene, polypropylene, polyacrylonitrile, and the like.
  • Fiber reinforced polymers may include polymers reinforced with glass fibers, aramid fibers, graphite fibers, carbon fibers, polymer fibers, boron fibers, hemp fibers, natural material fibers, and the like.
  • Metals may include aluminum, aluminum alloys, nickel, nickel alloys, steel, iron, titanium alloys, cobalt- chromium alloys, and any other metal or metal alloy sufficiently strong and/or resistant to the environment in which the panel will be used.
  • a treatment may be applied to the outer facing sections, particularly the portions of the outer facing sections that will be exposed to the environment. Exemplary treatments include paint or a coating that may allow the panel to blend in with its surroundings, a reflective coating, and the like.
  • one or more outer facing sections can include elements or the like applied or attached to the outer facing sections, such as for example, one or more electronic components (e.g. solar cells, antenna elements, LED screen components, lighting sources, sensor arrays, touch screens, sound generating devices, transducers, or the like), printed material (e.g. signs, fabrics, wall coverings, or the like), etc.
  • electronic components e.g. solar cells, antenna elements, LED screen components, lighting sources, sensor arrays, touch screens, sound generating devices, transducers, or the like
  • printed material e.g. signs, fabrics, wall coverings, or the like
  • an expandable panel consistent with implementations of the current subject matter can be rapidly deployable (e.g.
  • a display screen of a desired scale - which can vary from screens sized for personal computer displays or smaller to theater-sized or larger - merely by expanding panel structure as described herein from a fully collapsed configuration to a fully expanded configuration and affixing one or more longitudinal support structures 130).
  • Materials used for the inner core sections 115 may also include those used for the outer facing sections, described above.
  • the inner core sections may require that the material selected also be strong in compression, so that the inner core sections resist collapse, buckling, or other failure when the panel is fully extended and a load is applied perpendicular to the outer facing sections.
  • the longitudinal support structures may be made from the same materials as those listed above for the outer facing sections.
  • the longitudinal support structures may require additional characteristics, such as, for example, increased rigidity compared to the outer facing sections, increased friction against the ground, and/or malleability to enable the edges of the panel to conform to a roof or ceiling layer.
  • the outer facing sections, inner core sections, and longitudinal support structures may be made by conventional machining, hot-pressing, injection molding, extrusion, roller-pressing, conventional reinforced polymer composite lay-up, foaming, 3D printing, spraying, and the like.
  • the components of a panel may be made as lattices or as solid bodies with strategically placed openings (e.g. holes or voids) to reduce weight while maintaining strength.
  • the components may include foamed materials, including foamed polymers, ceramics, and/or metals.
  • Other possible materials can include honeycomb core composites, foam core composites, and optionally "built-up" structures for larger assemblies.
  • a welded truss assembly can be used for the inner core components for larger-scale panels (e.g. for use in temporary bridges, ramps, or the like).
  • the outer facing sections, inner core sections, and longitudinal support structures may or may not have reinforcing shapes to provide additional stiffness as required by applications (e.g. ribbed or corrugated sections, or the like).
  • the vertices of the panel sections may be of any suitably strong and pliable material.
  • thin flexible hinges such as fabric or living hinges may be used at the hinge points or hinge links to connect inner core and/or outer facing sections depending on application loads.
  • the hinge points or hinge links can be joined by molded or machined polymer hinges, machined metal hinges, metal injection molded hinge components, combinations thereof, or by any suitable hinging material or design consistent with the other teachings herein.
  • the vertex hinge points 240, the facing pair hinge points 235, the supplemental hinge points 710, the inner core hinge points 740, and/or the vertex hinge links 910 may be simple hinges or assemblies of one or more hinges, hinging mechanisms, jointed assemblies, or other combinations thereof which connect two or more adjacent inner core sections 115 and/or outer facing sections 120 such that the centers of the hinge points or assemblies retain their arrangement as described above.
  • a panel In use, a panel may be transported to and/or from its use destination with the collapsible portion fully compressed and the longitudinal support structures separate from the collapsible portion. In this way, when transporting more than one panel at a time, multiple collapsible portions may be stacked upon or against each other, and the longitudinal support structures may be bundled together in an efficient manner, as well.
  • a collapsible portion of a panel may be fully extended then held rigid with the longitudinal support structures.
  • the volume between the inner core sections may be left empty.
  • some or all of the volume between the inner core sections may be filled with material found at the destination location or with material transported with the panel for that purpose.
  • the volume between the inner core sections may be filled with sand before completing the panel with the addition of the longitudinal support structures.
  • an insulating material such as for example a foaming insulating material, may be inserted into the volume between the inner core sections.
  • a panel may be constructed and used in conjunction with other panels and/or other construction materials to build a structure.
  • Panels may be connected to each other and/or other construction materials using adhesives, tape, physical joining methods, or any combination thereof.
  • interlocking clips can be included as part of (or add-on components to) the longitudinal support structures.
  • panels of straight and curving sections can be combined to form walls and roofs.
  • Temporary or portable shelters, shade structures, walkways, bridges, or the like may be constructed which are light, easily portable, and reusable.

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Panels For Use In Building Construction (AREA)
  • Toys (AREA)
PCT/US2016/014772 2015-01-26 2016-01-25 Expandable panel WO2016123038A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP16743918.1A EP3250773A4 (en) 2015-01-26 2016-01-25 Expandable panel
JP2017558354A JP2018503762A (ja) 2015-01-26 2016-01-25 伸縮式パネル
CA2974436A CA2974436A1 (en) 2015-01-26 2016-01-25 Expandable panel
AU2016211704A AU2016211704A1 (en) 2015-01-26 2016-01-25 Expandable panel

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US201562107955P 2015-01-26 2015-01-26
US62/107,955 2015-01-26
US201562187193P 2015-06-30 2015-06-30
US62/187,193 2015-06-30

Publications (1)

Publication Number Publication Date
WO2016123038A1 true WO2016123038A1 (en) 2016-08-04

Family

ID=56544206

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2016/014772 WO2016123038A1 (en) 2015-01-26 2016-01-25 Expandable panel

Country Status (6)

Country Link
US (1) US20170233997A1 (ja)
EP (1) EP3250773A4 (ja)
JP (1) JP2018503762A (ja)
AU (1) AU2016211704A1 (ja)
CA (1) CA2974436A1 (ja)
WO (1) WO2016123038A1 (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107956403A (zh) * 2017-11-14 2018-04-24 惠州永笙精密模具制品有限公司 一种新型家居柔性光伏采集窗

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10273935B2 (en) * 2016-01-15 2019-04-30 General Electric Company Rotor blades having structural skin insert and methods of making same
US10246932B2 (en) * 2016-04-18 2019-04-02 James G. Arendts Deployable sandwich-like shell structural system
US11408216B2 (en) 2018-03-20 2022-08-09 Divergent Technologies, Inc. Systems and methods for co-printed or concurrently assembled hinge structures
US11590727B2 (en) * 2018-05-21 2023-02-28 Divergent Technologies, Inc. Custom additively manufactured core structures
CN115188263B (zh) * 2022-06-09 2023-10-31 深圳市华星光电半导体显示技术有限公司 多折折叠组件和多折显示装置

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2101836A (en) * 1936-10-21 1937-12-14 Elb Products Inc Thermal insulating building unit
US2786004A (en) * 1953-08-07 1957-03-19 Leobarb Corp Thermal insulation
US5974763A (en) * 1998-01-23 1999-11-02 Hunter Douglas Inc. Cell-inside-a-cell honeycomb material
US20010005964A1 (en) * 1995-11-22 2001-07-05 Colson Wendell B. Cladding system and panel for use in such system
US20020020142A1 (en) * 2000-04-24 2002-02-21 Swiszcz Paul G. Compressible structural panel
US20020084042A1 (en) * 1999-03-16 2002-07-04 Kimmet Stephen G. Security system for a cubicle
US20140054108A1 (en) * 2010-12-08 2014-02-27 Wolf Bavaria Gmbh Sheet-Like Finishing Element

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5620035A (en) * 1987-03-25 1997-04-15 Judkins; Ren Material utilizing flexible strands
US20130133301A1 (en) * 2011-11-28 2013-05-30 General Filters, Inc. Modular air filter
FR3029559B1 (fr) * 2014-12-08 2017-01-13 Flexoma Structure alveolaire retractable et son procede de fabrication

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2101836A (en) * 1936-10-21 1937-12-14 Elb Products Inc Thermal insulating building unit
US2786004A (en) * 1953-08-07 1957-03-19 Leobarb Corp Thermal insulation
US20010005964A1 (en) * 1995-11-22 2001-07-05 Colson Wendell B. Cladding system and panel for use in such system
US5974763A (en) * 1998-01-23 1999-11-02 Hunter Douglas Inc. Cell-inside-a-cell honeycomb material
US20020084042A1 (en) * 1999-03-16 2002-07-04 Kimmet Stephen G. Security system for a cubicle
US20020020142A1 (en) * 2000-04-24 2002-02-21 Swiszcz Paul G. Compressible structural panel
US20140054108A1 (en) * 2010-12-08 2014-02-27 Wolf Bavaria Gmbh Sheet-Like Finishing Element

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3250773A4 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107956403A (zh) * 2017-11-14 2018-04-24 惠州永笙精密模具制品有限公司 一种新型家居柔性光伏采集窗

Also Published As

Publication number Publication date
CA2974436A1 (en) 2016-08-04
US20170233997A1 (en) 2017-08-17
JP2018503762A (ja) 2018-02-08
AU2016211704A1 (en) 2017-08-10
EP3250773A1 (en) 2017-12-06
EP3250773A4 (en) 2018-10-24

Similar Documents

Publication Publication Date Title
US20170233997A1 (en) Expandable Panel
CN114018095B (zh) 可部署的折纸启发的屏障
JP3802569B2 (ja) 三次元等方トラス
US3783573A (en) Expandable truss structure
US9376796B2 (en) Rapidly deployable structures based upon negative poisson's ratio (NPR) auxetic components
US7541085B2 (en) Flexible construction element with large bonding surface area and method of manufacture
US8800718B2 (en) Ultra lightweight segmented ladder/bridge system
US20090056237A1 (en) Shelter and associated method of assembly
US20040105960A1 (en) Structural sandwich members
US7197856B2 (en) Modular truss assembly
US8844674B2 (en) Assault ladder
EA028978B1 (ru) Модульный структурный элемент копира для образования изогнутых изделий
CN110892124A (zh) 纤维增强的细长压型物体
JP2013541429A (ja) 高強度低密度多目的パネル
US7509779B2 (en) Lightweight building blocks
EP1379379A1 (en) Improved structural sandwich members
WO2014170650A2 (en) Folded shell structures
US20040000620A1 (en) Foldable support structure with hinged sawtooth wall members
US4150516A (en) Framework and sheet material building structure
WO2007040508A2 (en) Shelter and associated method of assembly
Liew et al. Recent development of deployable tension-strut structures
JP2020165150A (ja) 骨組構造体及びそれを用いたビニルハウス
JP7334947B2 (ja) 折り畳み式テント及び構造材
US11680398B2 (en) Strata space frame
EP3144437A1 (en) Module assembly for a building

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 16743918

Country of ref document: EP

Kind code of ref document: A1

ENP Entry into the national phase

Ref document number: 2974436

Country of ref document: CA

ENP Entry into the national phase

Ref document number: 2017558354

Country of ref document: JP

Kind code of ref document: A

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2016211704

Country of ref document: AU

Date of ref document: 20160125

Kind code of ref document: A

REEP Request for entry into the european phase

Ref document number: 2016743918

Country of ref document: EP