1. Field of Invention
The present invention relates to building panels particularly suitable for use as exterior siding on building wall surfaces.
2. Description of the Related Art
In constructing exterior walls of a building, it is known to fasten building panels to a building frame using fasteners or adhesives. Daily and yearly climatic changes require that the building panels have means for expansion and contraction. It is known to use various filler materials such as grout, silicone and recessed filler strips, e.g., metal strips of matching color to resiliently fill the gap between adjacent building panels. Filler materials have the disadvantage of requiring additional labor during application and eventual replacement as the material weathers due to exposure to the elements.
It is also known to use shiplap boards which use shiplap joints to clad the side of a building. Shiplap joints are typically formed by cutting matching rabbets into opposite faces of adjoining boards. A rabbet is cut along an edge of one board on a frontface surface and the adjacent board is cut with a rabbet on the backface. The depth of the rabbet cuts are made so the adjacent panels can be positioned next to each other and the overlap and underlap edges of the adjacent boards mate together. This produces a shiplap joint that prevents gaps from forming between the boards as they expand and contract. As illustrated in
An improved shiplap building panel having four corners and four edges, a first corner with a backunderlap (230), a first edge (DA) with a backlap (240), a second corner (B) with a backcenterlap (210) and a frontcenterlap (310), a second edge (AB) with a backlap (250), a third corner (C) with a frontunderlap (330), a third edge (BC) with a frontlap (340), a fourth corner (D) with a backcenterlap (220) and a frontcenterlap (320), a fourth edge (CD) with a frontlap (350), a front face (201), and a back face (301) such that when the improved shiplap building panels are assembled with the same orientation the panels overlap and there no visible gaps between panels and panels are free to expand and contract with temperature changes without forming any gaps among panels.
The following terms provide descriptions of planes and surfaces with dimensions that if exceeded would result in two adjacent panels attempting to occupy the same space. The dimensions could be smaller to allow for manufacturing tolerances.
The term “frontface” (102, 201) is used to distinguish a first face of a building panel from the second face of a building panel. The frontface is that face of the building panel which is exposed to view. It is opposite to the backface of a building panel.
The term “backface” (103, 301) is used to distinguish a second face of a building panel from a first side of the building panel. The backface is the face of the building panel which is fastened to a wall of a building. It is opposite to the frontface of a building panel.
The term “plane of the frontface” (202) herein refers to the flat surface of the frontface (201) and on which a straight line joining any two points on it would wholly lie.
The term “plane of the backcenterlap” (203) herein refers to a flat surface that is located between the plane of the frontface and the plane of the backface and on which a straight line joining any two points on it would wholly lie. It is located closer to the frontface (201) than the backface (301).
The term “plane of the centerline” (204) herein refers to a flat surface that is located centrally between the plane of the frontface (202) and the plane of the backface (206) and on which a straight line joining any two points on it would wholly lie. It is also located centrally to the plane of the front centerlap (203) and the plane of the back centerlap (205).
The term “plane of the frontcenterlap” (205) herein refers to a flat surface that is located between the plane of the frontface and the plane of the backface and on which a straight line joining any two points on it would wholly lie. It is located closer to the backface (301) than the frontface (201).
The term “plane of the backface” (206) herein refers to the flat surface of the backface (301) and on which a straight line joining any two points on it would wholly lie.
The term “overlap” herein refers to a projection from the frontface of a shiplap building panel that remains after a rabbet is cut from the backface. The overlap of the present invention is illustrated in
The term “underlap” herein refers to a projection from the backface of a shiplap building panel that remains after a rabbet is cut from the frontface. The underlap of the present invention is illustrated in
The term “backcenterlap” (210, 220) herein refers to a projection from an edge of the building panel that is shared by the overlap (310-350) and underlap (210-250) but does not extend from either the frontface (201) or the backface (301). It has a first surface at the plane of the front centerlap (203), half of the backcenterlap merges with the backlap (250, 240) and the other half has a second surface at the plane of the backcenterlap (205) and forms a portion of the surface of the “frontcenterlap” (310, 320). A first backcenterlap (310) is located in the figures at corner B and a second backcenterlap (320) is located in the figures at corner D.
The term “backlap” (240, 250) herein refers to portion of the underlap (210-250) that extends from the plane of the backface (206) to the plane of the centerline (204).
The term “backunderlap” (230) herein refers to portion of the underlap (210-250) that extends from the plane of the backface (206) to the plane of the back centerlap (205). The backunderlap is located in the figures at corner A.
The term “frontlap” (340, 350) herein refers to portion of the overlap (310-350) that extends from the plane of the frontface (202) to the plane of the centerline (204).
The term “frontoverlap” (330) herein refers to portion of the underlap (310-350) that extends from the plane of the backface (206) to the plane of the front centerlap (203). The frontoverlap is located in the figures at corner C.
The term “frontcenterlap” (310, 320) herein refers to a projection from an edge of the building panel that is shared by the underlap (210-250) and overlap (310-350) but does not extend from either the backface (301) or the frontface (201). It has a first surface at the plane of the back centerlap (205), half of the frontcenterlap merges with the frontlap (350, 340), and the other half has a second surface at the plane of the frontcenterlap (203) and forms a portion of the surface of the “backcenterlap” (210, 220). A first frontcenterlap (210) is located in the figures at corner B, and a second frontcenterlap (220) is located in the figures at corner D.
The term “improved shiplap joint” herein refers to matching shiplap joints as described by the present invention.
The term “improved shiplap building panel” herein refers to building panels with the improved shiplap joints as described by the present invention.
For purposes of this invention, edges of the improved shiplap panel may be designated by the corners at the end of the edge. As shown in
The subject invention is a building panel with an improved shiplap joint that eliminates the coverage gaps at the corner intersection of building panels. The building panel includes a first face known as a frontface (201) which is exposed to view after installation on the building, which includes an overlap (210-350) portion adapted to overlay the underlap (210-250) of a second face known as backface (301) of one or more improved shiplap building panels laid up in the next higher course of a building wall surface. Prior art shiplap joints use an overlay (110) and underlay (105) that typically mate along the plane of a centerline (101) of the panel. The improved shiplap joint uses backcenterlaps (210, 220) and frontcenterlaps (310, 320) formed along a third plane, or thickness, of material at a center plane of building panels which straddle the plane of the centerline (204). Each pair of backcenterlaps (210, 220) and frontcenterlaps (310, 320) are located at diagonally opposite corners of the improved shiplap building panel, while each front/back pair (210, 310) and (220, 320) are located in the same corner, but rotated 90 degrees relative to each other.
The overlap (310-350) and underlap (210-250) must be thinner at the corners to accommodate for mating with the center plane thickness of the backcenterlaps (210, 220) and frontcenterlaps (310, 320). The backunderlap (230) is a thinner section of the underlap with a thickness defined by the plane of the backface (206) and the plane of the frontcenterlap (205). The backunderlap is located at the corner shared by the backlaps (240, 250).
Description of Overlaps of Panels BL and BR
When installed, the side connecting Corners A and B, or Side AB, of Panel BL meets Side CD of Panel BR in such a manner that frontlap (350) of Panel BR mates with backlap (250) of panel BL at the plane of the centerline (204). At the meeting of Corner B of panel BL and Corner C of panel BR the upper left half of frontoverlap (330) of panel BR mates with backcenterlap (210) of panel BL at the plane of the backcenterlap (203). At the meeting of Corner A of panel BL and Corner D of panel BR the frontcenterlap (320) of panel BR mates with the lower right half of backunderlap (230) of panel BL at the plane of the frontcenterlap (205).
Description of Overlaps of Panels BL and TL
When installed, the side connecting Corners D and A, or Side DA, of Panel BL meets Side BC of Panel TL in such a manner that frontlap (340) of Panel TL mates with backlap (240) of panel BL at the plane of the centerline (204). At the meeting of Corner D of panel BL and Corner C of panel TL the lower right half of frontoverlap (330) of panel TL mates with backcenterlap (220) of panel BL at the plane of the backcenterlap (203). At the meeting of Corner A of panel BL and Corner B of panel TL the frontcenterlap (310) of panel TL mates with the upper left half of backunderlap (230) of panel BL at the plane of the frontcenterlap (205).
Description of Overlaps of Panels TL and TR
When installed, the side connecting Corners A and B, or Side AB, of Panel TL meets Side CD of Panel TR in such a manner that frontlap (350) of Panel BR mates with backlap (250) of panel TL at the plane of the centerline (204). At the meeting of Corner B of panel TL and Corner C of panel TR the upper left half of frontoverlap (330) of panel TR mates with backcenterlap (210) of panel TL at the plane of the backcenterlap (203). At the meeting of Corner A of panel TL and Corner D of panel TR the frontcenterlap (320) of panel TR mates with the lower right half of backunderlap (230) of panel TL at the plane of the frontcenterlap (205).
Description of Overlaps of Panels TR and BR
When installed, the side connecting Corners D and A, or Side DA, of Panel BR meets Side BC of Panel TR in such a manner that frontlap (340) of Panel TR mates with backlap (240) of panel BR at the plane of the centerline (204). At the meeting of Corner D of panel BR and Corner C of panel TR the lower right half of frontoverlap (330) of panel TR mates with backcenterlap (220) of panel BR at the plane of the backcenterlap (203). At the meeting of Corner A of panel BR and Corner B of panel TR the frontcenterlap (310) of panel TR mates with the upper left half of backunderlap (230) of panel BR at the plane of the frontcenterlap (205).
Description of Intersection of the Four Panels where they Meet
The bottommost layer is backunderlap (230) of panel BL. The lower right half of backunderlap (230) of panel BL is mated with frontcenterlap (320) of panel BR at the plane of the frontcenterlap (205). The upper left half of backunderlap (230) of panel BL is mated with frontcenterlap (310) of panel TL at the plane of the frontcenterlap (205). The backcenterlap (210) of panel TL and backcenterlap (220) of panel BR then mate with the topmost layer frontoverlap (330) of panel TR, mating with the top left and bottom right halves respectively at the plane of the backcenterlap (202). It is this overlapping system of three layers (bottom (230), middle (310 and 320), and top (330) that meet at two planes (lower (205) and upper (203)) that allow panels to expand and contract without creating visible gaps in the assembly.
The improved shiplap building panel of the present invention is not limited by the material of construction. It is found that by utilizing a material that is easy to cut with high speed router bits and a material with consistent color throughout its thickness, the geometry outlined above can be quickly and easily integrated into exterior cladding façade panels for complete homogenous material coverage. Solid surface materials are found preferable. Corian® solid surface materials from E.I. du Pont de Nemours and Company, Wilmington, Del. are examples.
Optionally, all edges may be beveled to facilitate drainage of rainwater, dew, or the like.
Optionally, the improved shiplap building panel may be designed such that all cuts may be made with a single tool, such as a router bit or a shaper bit. It is found most preferable to use a cutter with a 15 degree angle with a radius on the end. The process for using the cutter uses two steps, one to cut a first face, then the panel is flipped and a second face is cut.
The improved shiplap building panel is installed according to typical shingle siding technique wherein a first course of improved shiplap building panels are fastened along the bottom of the building with the underlap (210-250) at the top. Successive courses of shingles are fastened above the previous course.
Number | Date | Country | |
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61515029 | Aug 2011 | US |