NZ592598B - Structural Improvements Relating To Building Panels - Google Patents
Structural Improvements Relating To Building Panels Download PDFInfo
- Publication number
- NZ592598B NZ592598B NZ592598A NZ59259812A NZ592598B NZ 592598 B NZ592598 B NZ 592598B NZ 592598 A NZ592598 A NZ 592598A NZ 59259812 A NZ59259812 A NZ 59259812A NZ 592598 B NZ592598 B NZ 592598B
- Authority
- NZ
- New Zealand
- Prior art keywords
- panel
- web
- egg
- webs
- closed cell
- Prior art date
Links
- 210000003491 Skin Anatomy 0.000 claims abstract description 85
- 239000011120 plywood Substances 0.000 claims abstract description 45
- 239000006260 foam Substances 0.000 claims abstract description 40
- 230000036961 partial Effects 0.000 claims abstract description 10
- 239000000853 adhesive Substances 0.000 claims description 10
- 230000001070 adhesive Effects 0.000 claims description 9
- 239000000203 mixture Substances 0.000 claims description 6
- 239000011180 sandwich-structured composite Substances 0.000 claims description 5
- 239000007767 bonding agent Substances 0.000 claims 1
- 230000035882 stress Effects 0.000 description 36
- 239000003292 glue Substances 0.000 description 19
- 210000001503 Joints Anatomy 0.000 description 14
- 238000005452 bending Methods 0.000 description 12
- 238000010276 construction Methods 0.000 description 12
- 239000000463 material Substances 0.000 description 12
- 238000005096 rolling process Methods 0.000 description 10
- 238000004026 adhesive bonding Methods 0.000 description 8
- 210000000614 Ribs Anatomy 0.000 description 6
- 210000002435 Tendons Anatomy 0.000 description 6
- 239000002131 composite material Substances 0.000 description 6
- 210000003746 Feathers Anatomy 0.000 description 5
- 230000000875 corresponding Effects 0.000 description 5
- 239000000835 fiber Substances 0.000 description 5
- 230000002787 reinforcement Effects 0.000 description 5
- 238000005728 strengthening Methods 0.000 description 5
- 238000007906 compression Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000009413 insulation Methods 0.000 description 4
- 230000002829 reduced Effects 0.000 description 4
- 238000004458 analytical method Methods 0.000 description 3
- 230000003247 decreasing Effects 0.000 description 3
- 238000010030 laminating Methods 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 210000001145 Finger Joint Anatomy 0.000 description 2
- 235000013601 eggs Nutrition 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 150000002500 ions Chemical class 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 238000003475 lamination Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 241000894007 species Species 0.000 description 2
- -1 timber Substances 0.000 description 2
- 239000002023 wood Substances 0.000 description 2
- 239000004698 Polyethylene (PE) Substances 0.000 description 1
- 239000004793 Polystyrene Substances 0.000 description 1
- 229940035295 Ting Drugs 0.000 description 1
- 229920002522 Wood fibre Polymers 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000000670 limiting Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000011505 plaster Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 229920002223 polystyrene Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- 239000004800 polyvinyl chloride Substances 0.000 description 1
- 230000000452 restraining Effects 0.000 description 1
- 238000004805 robotic Methods 0.000 description 1
- 231100000817 safety factor Toxicity 0.000 description 1
- 238000003892 spreading Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
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Abstract
Patent 592598 Disclosed is a structural building panel allowing lighter and stronger building panels. The panel is a stressed-skinned panel, serving as whole or part floor or roof or ceiling or wall panels of room spaces, in single or multi-storey buildings, and comprises a pair of skins, where each skin is a plurality of plywood sheets, and a core formed from an egg-crate structure of interlocking longitudinal and transverse web strips at an angle that is substantially 90° and an surrounding edge frame, where each web has notches at one half the depth of the web at their points of intersection, Partial or full infills of structured open or closed cell foam of a density of 16kg/m³ or more and a compressive strength greater than 85KPa is fitted within cells formed by the interlocking webs of the egg-crate structure. re each skin is a plurality of plywood sheets, and a core formed from an egg-crate structure of interlocking longitudinal and transverse web strips at an angle that is substantially 90° and an surrounding edge frame, where each web has notches at one half the depth of the web at their points of intersection, Partial or full infills of structured open or closed cell foam of a density of 16kg/m³ or more and a compressive strength greater than 85KPa is fitted within cells formed by the interlocking webs of the egg-crate structure.
Description
Recevied at IPONZ 23 August 2012
Post-dated under Section12(4)
23 August 2012
PATENT SPECIFICATION
APPLICATION NUMBER 592598
LODGED
COMPLETE SPECIFICATION URAL
ENTITLED IMPROVEMENTS RELATING TO
BUILDING PANELS
APPLICANT KEITH ERIC HAY
ACTUAL INVENTOR KEITH ERIC HAY
Received 3 Aug 2012
The objective of the invention is to produce a range of stable, flat,
structural building panels by using stressed skinned panels in
combination with open or closed cell structured foam infills, where
the risk of buckling of the stressed skinned panels’ skins and core
webs is decreased, correspondingly increasing the panels tolerance
to shear and other load forces.
The ion is for cost-effective componentry, primarily though not
solely for use as whole or part floors or roof and ceiling panels of
room spaces, as non-load or load-bearing walls, shear walls and
el panels or as one or two-way spanning panels, each type of
use having increased structural performance by post-tensioning
individual or component combinations in both single and multi-storey
timber buildings.
The panels are lightweight and economic in use, of mainly
commonly available sustainable als, and low in energy use in
their simplicity of manufacture using standard sized materials with
minimum waste for m efficiency.
The panels can be constructed in a range of modular sizes allowing a
wide range of layout urations.
These structural panels are ideally suited to where there is a
propensity to standardised componentry such as in modular design
of pre-fabricated single or storey timber buildings.
Received 3 Aug 2012
The panels’ components can be varied at specific points by
thickening, increasing depths, ing density, tions or the
use of different material reinforcements in order to take care of
variable or concentrated loads at those points. rly where
higher stiffness to g is required, it is achievable by the use of
a variety of structured open or closed cell foam core cell infills and/or
skin stiffening by increasing skin thickness or by the use of differing
laminations such as metal sheet to plywood or cross- laminating.
The structural panel can act as a panel system to resist shear forces
in the plane of the panel as in a braced wall and as shear walls of
vertical elements of a horizontal force resisting system.
With the modular layouts within the panel cores and their overall
dimensions, consistency of material choices and methods of
assembly, future cost effectiveness and efficiencies could be
achieved in volume tion by the use of robotics.
The invention comprises a pair of skins, an egg-crate core,edge
members and s of structured open or closed cell foams in the
cells formed by the egg-crate core. The skins are continuous and
formed by a plurality of sheets bonded edge to edge. The core is a
plurality of strips in at least two directions, usually at 90° to each
other, cross-halved at their intersections to form an egg- crate
Received 3 Aug 2012
structure. Edge members form a perimeter to core and skin edges.
The structured open or closed cell foam infills are l or full
infills to the core cells.
Edges of core strips are adhesive bonded to each skin and to the
inner face of edge members. Edge s are adhesive bonded
to the skins and the structured open or closed cell foam infills may be
unbonded or partially or fully bonded on contact faces to the core
cells, skins and/or edge members.
If the structured open or closed cell foam is a l or full cell infill,
not fixed to any contact face but friction fitted, it will partially restrain
buckling of the core strip, increasing the stressed skinned panels
resistance to shearforces. If the infill is a partial or full cell infill
fixed to one skin only, it will reduce buckling of that skin and partially
restrain ng of the core strips increasing panels resistance to
shearforces and bending stress. If the infill is a full cell infill fixed to
both skins, the panels capacity for resistance to shear and bending
stress is increased as the s and the skins bonded to them
become sandwich-structured composites within each of the core cells.
If the full cell infill is bonded on all six faces to the skins and the core
strips then the panel becomes a stressed skinned sandwich
structured composite.
Recevied at IPONZ 23 August 2012
The panels skins and the core web s can be comprised of
plywood, veneer board, oriented strand board, hardboard, particle
board, high or medium density fibre board, reinforced
cementitious materials, carbon fibre, timber, metal sheets, plaster
board laminates, glass, rced thermoplastics and thermoset
polymers. However as with the core webs, plywood sheets remain
the most efficient and cost-effective material for the skins at this time.
The core cell infills are of open or closed cell structured foams such
as polyvinyl chloride, polyurethane, polyethylene, polystyrene or
syntactic foams of a density of 16kg/m3 or more and a compressive
strength greater than 85 KPA.
The panels uction is advantageous in that it allows large
lightweight panel sizes to be assembled, the limitations being the
press size and/or the method of transportation, and in being able to
construct structural members of a building by a consistency of
method.
It can be shown that core members are analysed as being the web of
a simple beam, the flanges of which are the width of the skins to a
point halfway n the core member and adjacent core members
on either side.
Thinness of core s is limited both by the tendency to buckle
due to the diagonal component of the shear force of the web and by
the shear forces perpendicular to the plane of the web caused by
stress in the structure which would cause the web to collapse
sideways or shear at the junction of the web and flanges.
The tendency to buckle can be avoided if the ratio of the thickness of
the web member to the diagonal ement of its height taken at
45° to the vertical is less than 50. It is therefore advantageous to be
able to adjust the thickness of the web independently of any other
element in the panel so that it is as close as possible to the ratio of
50 in order to achieve maximum y.
The shear forces dicular to the plane of the web have in other
examples been taken care of by making the web thick at the flange
junction by using solid rectangular timber webs. A thin web member
can be stiffened against collapse by bracing it ersely with
similar thin sections placed at right angles at frequent intervals by
employing the well- known principle of interlocking egg-crate
construction to brace the webs by a series of transverse webs placed
at the same intervals as the primary webs. This stiffens webs in both
directions before any adhesive set and permits the erse webs
to absorb all of the secondary stress due to shear perpendicular to
the primary webs and the primary shear stress. Hence such a
stressed skinned panel can be viewed as acting according to the
‘plate’ theory where forces on the panel are considered to be acting
in a multitude of directions.
Core members should be acting in at least two ions at a
substantial angle to each other, such as 90 degrees, especially when
the skins composing the flanges are plywood and are intrinsically
capable of acting equal, or near equal strength in the two major
directions of the panel plane. Therefore both sets of webs can be
considered as stress ing members and the core can be
analysed as a two-directional shear core. This is ed by the
spacing of one set of webs to similar intervals as the other set and by
ensuring that the two sets co-act at the ections. To co-act
equally can only be achieved by forming a slot in one set of exactly
half the web depth and a corresponding slot in the other set with both
slot widths corresponding to the width of the intersecting web.
Maximum continuity is achieved when the intersection is glued
together on assembly so that there is continuity of shear forces in
any one web member through the erse web and the vertical
component of the shear forces to shear the web member at the slot
is overcome by erring the vertical shear stress via the glue line
at the flange to the web of the transverse member.
Timber is known to have one of the highest strength to weight ratios,
is commonly available, has low initial cost and is easily worked. ln
laminated form such as plywood the strength-to—weight ratio is
increased, more stable and more dependable in moisture content,
dimensions and evenness of structural properties. Its advantage in
stressed skinned panels is that each part of the elements is used to
its m structural advantage with a minimum of urally
redundant material.
The limiting shear stress in d is usually taken to be that
determined by what is termed the ng shear’ which occurs when
one part of the shear force acts in the plane of one veneer in the
direction of its grain and the other opposing part of the shear force
acts in the next corresponding veneer, causing the fibres of the
intervening transverse veneer to separate from each other in a rolling
manner. The allowable shear stress in such circumstances is y
taken to be less than the allowable shear in solid timber sections of
the same timber species.
However, when the shear forces acting in the plane of a plywood
sheet can be said to be acting over the whole cross sectional area of
the plywood, and not on individual veneers, the d is said to be
acting in ‘panel’ shear for which the allowable stress is usually taken
as being twice that of the allowable shear stress in solid timber of the
same species and three times as great as the allowable rolling shear
stress in the same plywood. The advantage is to use plywood in
such a manner that it is subjected to panel shear and not limited by
rolling shear.
Previous attempts to use the panel shear characteristic of plywood
have been to use the plywood for the web members of beams by
attaching the plywood members to the flange members of the beams
by gluing the flange members to the sides of the plywood webs. This
method of attachment causes rolling shear in the plywood web over
the area of attachment, due to the horizontal component of the shear
force in the web. In the current design, e the lateral stability
of the web is assured by the ocking effect of the egg crate
construction, it is le to glue the d webs to the flanges, or
skins of panels, at their edges only, thus eliminating the possibility of
rolling shear occurring in the webs.
Where the skin of the panel is made from plywood, rolling shear will
occur in the plywood skin at the point of attachment to the webs, but
this will not limit the shear stresses allowable in the whole
construction as long as the flange width corresponding to each web
is more than three times the thickness of the web member. This is
because the allowable stress in the panel shear is three times
greater than the allowable stress in rolling shear for the same
plywood. Therefore web thicknesess for panels are to be
considerably less than the flange width appropriate to each web.
The th of the design depends on the use of an adhesive at the
junction of the web flange members which is as strong or stronger
than the on of the wood fibres to each other. A further aspect
of the design is that part of its particular th at the web flange
junction is that plywood is always made of an unequal number of
veneers. The two s on the outside are parallel in fibre, or
grain direction and the next inner veneer or veneers have a fibre
direction transverse to this. It follows that maximum adhesion of the
plywood sheet is obtained when the edge being glued is parallel to
the fibre direction or grain of the face veneers.
Therefore in the plywood webs the high bond strength of the web to
the flange ary is in part obtained by maintaining the face grain
of the plywood webs parallel to the length of the webs, and to the
plane of the flanges. This ensures that no matter how many veneers
are used to make up the plywood used in the webs, the greater
number are glued with the sides of the fibres in contact with the
flanges of the panel and that the shear stress is buted
symmetrically over the width of the web.
Therefore the design web thicknesses of 9mm and upwards, while
large enough to ensure good gluing area on the edges, are very thin
compared with the cell size. Similarly the access holes for bolting of
panels together, which have to be in the order of 100mm in diameter
to enable a bolt, hand or tool to be inserted, are small relative to the
cell size or the panel size and hence do not have a marked effect in
weakening the construction. thening is re-established once
connections are complete by gluing tapered caps into the edge
d access holes using caps of the same ess and material
as the panel skins. Given the area of cell size considered, extra
strengthening can be inserted by using smaller cell-sized egg-crate
into particular cells where local resistance to ng shear is
required, or sely thickening of the skins by cross lamination at
these points of additional stress. Similarly, where it is desired, web
spacing or thickness of webs and angles of web intersections can be
varied locally.
When comparing the use of d webs to those of sawn lumber
for the construction, a simplification of analysis is that the glued
contact area between the web and the skin is greater in the timber
web than in the ply web, and hence the amount of ‘pull’ the timber
web can exert on the inner skin veneer, causing it to roll on the other
veneer, is greater than in the case of the plywood web where the
contact area is very narrow. Therefore somewhat imately it
can be said that the greater strength of the plywood web, plus the
fact that it is narrow, compared to the flange widths, makes the
construction in plywood webs much stronger than the construction in
sawn lumber webs.
The question of how thin the webs can become is limited by the point
at which the stress causes them to buckle. The limit is derived from
the shear stress which acts both vertically and horizontally in the web
and are the same in each direction resulting in a diagonal stress in
the web plane at 45 degrees. If the rule is applied that a column or
thin plane will buckle if the ratio of the thickness to the length is
greater than 50, then for a 9mm thick web the limit is .
450mm, so the diagonal measurement of the web should not be
greater than 450mm. That gives a web height of 300mm before
buckling will occur under the diagonal compression induced by the
two sets of opposing shear forces in the web. If ever required to
exceed 300mm in depth the web can be thickened and a new limit
applies or we can introduce a ite al into the cells so
that each cell forms a sandwich, changing the construction into a
stressed skinned/sandwich panel combination.
A problem is to what effect do the cross-ribs have on the construction
and three points emerge.
3. Although not envisaged at this stage due to the difficulties of
glue application and lay-ups, gluing of the intersection of the
webs will greatly strengthen the construction. By doing this
panel shear will p in the cross ribs as well which could
be limited by rolling shear at the point of intersection and such
gluing will overcome the weakness in the ribs caused by the
slots.
b. The cross webs take care of secondary stresses, minimising
them, and allow the whole panel to be analysed as a ‘plate’
rather than in simple beam theory.
Received 3 Aug 2012
c. If the panel is analysed as a plate the stresses acting can be
drastically reduced. Thus in the floor and ceiling panel
analyses, if taken as a two-way slab, all stresses are halved.
When bending stresses are considered, if the plywood flange in
compression has a length (L) of , width 400mm, thickness (t)
of 9mm then L/t = 3600/9 = 400; the flange could buckle, but if the
flange is supported at each 400mm by the cross web of the core, the
unsupported flange length becomes 400mm and being continuous
this reduces to (400)(9)/10 = 360 and L/t s 360/9 = 40, a
factor which makes the flange safe against buckling.
When structured open or closed cell foams are layered, placed or
foamed into the cell spaces formed by the webs, the structural
analysis in conjunction with the plate theory regarding spans,
tions, shear loadings and panel thickness to span ratios
becomes a combination of stress-skinned panel and a ch
structured composite.
The structured open or closed cell foams are of a density of 16kg/m3
or more and a compressive strength greater than 85KPA.
The foams can be either partial or full cell infill and where they are
a l cell infill it is in the form of a thin layer or thickness, glue-
fixed to one skin only with an adhesive of high bond strength.
Any bending moment shear in this skin being in compression or
Received 3 Aug 2012
tension will be reduced by the increase in skin thickness and the web
buckling is reduced where the l composite es a degree of
lateral int to the webs.
Where the structured open or closed cell foams are a full cell infill
glue-fixed to both skins with an adhesive of high bond strength it
provides a high degree of lateral restraint to buckling of the webs and
the thickness of the web member to the diagonal measurement of its
height taken at 45° to vertical alters substantially the ratio of 50. This
also applies where the cell infill is glue-fixed to all six faces of the cell.
Full cell infills of structured open or closed cell foams overcome the
problem of web gluing at their intersections and provide high
strengthening by spreading shear into the cross ribs and decreasing
the effects of rolling shear . Where the structured open or closed cell
foams of full cell inserts are bonded to each of the panel skins, each
cell becomes a sandwich structured composite with a high shear
stiffness to weight ratio for the composite and the linear ch
theory becomes important to the design and analysis of each of
these cell sandwich panels in combination with the stress-skinned
panel as a whole. The composite has a high tensile strength to
weight ratio and the higher the stiffness of the panel skins there will
be a higher bending stiffness to weight ratio for the ite.
Higher stiffness in the skins can also be achieved by cross-
lamination or thickening or the tion of other materials.
Received 3 Aug 2012
The behaviour of a panel with a sandwich cross-section under load
differs from a panel with a constant elastic cross-section in that the
radius of curvature during bending is small compared to the
thickness of a sandwich composite and the strains in the component
als are small. Deformation can be separated into two parts
being bending deformation due to bending moments and shear
deformation due to transverse .
The ch panel theories assume that the reference stress state
is zero. In order to use this reference it es an absence of
temperature differentials to ally the skin sheets during the
pressing and curing of the panels, thereby ating induced
cturing bending stress so that the reference stress state
solutions when the problem is linear is provided by sandwich theory.
If manufacturing residual stress develops or is a design parameter
such as camber, then the initial stress state has to be incorporated
directly into the sandwich theory.
The introduction of structured open or closed cell foam infills to the
panel cells affects the cross-ribs and the panels as follows:-
a) Whether partial or full cell infill, they increase the strength of
the construction at the web intersections by their allowing
panel shear to develop in the cross ribs and rolling shear will
be limited at the point of intersection caused by weakness in
ed 3 Aug 2012
the ribs by the slots by the restraining action of the infills
against all sides of the cells.
b) The cross webs and the infills take care of secondary
stresses, minimizing them and allow the whole panel to be
analysed as a plate rather than in simple beam theory, with,
in the case of partial infill, a strengthening of either top or
bottom skins, or both, and similarly a strengthening of the
skin joints.
0) When the panel is without infill and is analysed as a plate,
the acting stresses can be drastically reduced thus halving all
es when taken as a two-way slab. The stresses are
further d with full cell infills which are analysed as
plates using the linear sandwich theory in conjunction with a
two way slab.
When bending stresses are considered, full cell infills will
se the panel’ 3 limit for both tension and ssion
bending stresses by forming a fully adhesive-bonded support
backing of the flange across the panel’s entire section increasing
the safety factor of the flange against buckling. Similarly when
partial cell infills are fully adhesive-bonded to either the panel’s
bottom or top or both flange skins, they will correspondingly, to
those respective positions, increase the limit of tension or
compression bending and decrease the ability of the flange
to buckle.
These panels are able to be post-tensioned in either direction
separately or in series using post-tensioned tendons. Plastic sleeves
can be positioned in pre-selected lines within the panel before
adhesive-bonding of the top skins, including stiffening of the anchor
points. Tendons, using either high e cable or rod, are threaded
through the sleeves and the panels are either factory or e post-
ned by tendon stretching and clamping once the design loading
is reached.
Post-tensioning produces compressive stress that es tensile
stress that the panel would othenNise experience when imposed
g loads are applied and allows the panel thickness to be
decreased or increases it’s ability to span longer distances.
Post-tensioning can also be applied outside of the panel by g
tendons against an underside skin face, strengthening the ribs along
the tendon lines and reinforced anchor points at the perimeter beams,
with the ability to adjust individual tendons and to de-stress them
during repair or required installation adjustments.
One preferred form of the invention will now be described with
reference to the accompanying drawings in which:
Received 3 Aug 2012
Fig.1 is a plan of a typical structural building panel of a width r
than 2400mm with the bottom skin partly removed and
showing d pad reinforcement laminated to the outer
face of the bottom skin at inset support points where a
cantilever of the panel may be required.
Fig.2 is a plan of an alternative structural layout for a typical panel of
width 2400mm or less, again with plywood pad reinforcement
laminated to the outer face of the bottom skin where a
cantilevered panel may be required.
Fig.3 is a sectional elevation of a typical panel on the line A-A as
shown in Fig.1 and Fig.2.
Fig.4 is an exploded view of components of a structural building
panel according to the invention shown in isometric projection.
Fig.5 is a part isometric view of a panel assembly according to the
Fig.6 is a detailed cross-section of the edge of the panel of Fig.5
with low density insulation.
Fig.7 is an alternative cross-section of the edge of the panel of Figs.
and 6 with part core infills of structured open or closed cell
foams.
Fig.8 is an alternative section of the edge of the panel of Figs.
, 6 and 7 with full core infills of structured open or closed cell
foams.
Received 3 Aug 2012
Fig.9 is an alternative section of the edge of the panel of Figs.
,6,7 and 8 with either full or part core infills of structured open
or closed cell foams.
Fig. 10 is a plan view of the intersection of unglued web joints and
unglued edge faces of part or full infills of structured open or
closed cell foams.
Fig. 11 is a plan view of the intersection of glued web joints and
unglued edge faces of part or full infills of structured open or
closed cell foams.
Fig.12 is a plan view of the intersection of glued web joints and glued
edge faces of part or full s of structured open or closed
cell foams.
Fig. 13 is a plan view of the intersection of unglued web joints and
glued edge faces of part or full infills of structured open or
closed cell foams.
Fig. 14 is an ed view of components shown in Fig.6.
Fig. 15 is an exploded view of components shown in Fig.7.
Fig. 16 is an exploded view of components shown in Fig.8.
Fig. 17 is an exploded view of components shown in Fig.7 with glued
edge faces of part infills of structured open or closed cell
foams.
Received 3 Aug 2012
Fig. 18 is an exploded view of components shown in Fig.9 with glued
edge faces of full infills of structured open or closed cell
foams.
Fig.19 is a detail of an assembled joint between panel edges.
Fig. 20 shows alternative construction of outer edge members.
Fig. 21 is a plan of assembled panels showing a typical location of
jointing means.
Fig.22 shows assembled components for connecting wall panels or
other constructions to the panels’ outer edge
Fig.23 shows led ents for ting wall panels or
other constructions to the panels’ outer edges at a panel to
panel butt joint
Figs. 24, 25, 26 and 27 show means ofjointing facing skin and web
materials.
Fig. 28 shows the location of material joints in relation to web g.
Fig.29 is an isometric view of a method of panel assembly
A reference key to the assembly componentry of the invention’s
accompanying drawings is:
1. Panel
2. Panel upper skin
3. Panel lower skin
4 . Upper longitudinal skin joint
Received 3 Aug 2012
SPF???“ Lower longitudinal skin joint
Upper and lower transverse skin joint
Intersecting core web members
Part core infills of structured open or closed cell foams.
9. Full core infills of structured open or closed cell foams.
. Edge s
11.lnset t point of plywood reinforcement pads
laminated to the outer face of the lower skin
12.Alternative internal panel t point of plywood
reinforcement pads laminated to the internal face of the
lower skin
13. Panel core transverse webs
14. Panel core longitudinal webs
. Inner edge member
16.0uter edge member
17.Web notches
18.Assembled web joints
19.Tapered circular access hole
.Tapered circular cap
21 .Glue joint
22. Rebate in outer edge member
23. Panel to panel tubularjoining member
24. Part or full core infills of low density insulation
Received 3 Aug 2012
. d contact face of web
26. Unglued contact face of structured open or closed cell
foams
27. Glued contact faces of webs
28.Transverse hole through tubularjointer
29.Jointing bolt
. Rebated slot in full infill composite at panel to panel bolting
point
31 .Wall panel edge member with rebate for glued plywood
tongue
32.Continuous plywood tongue
33. ed washer head wood screw
34.Wall edge member
.Jointing feather
36. Panel skin
37. Scarfed joint
38.Structural fingerjoint
Referring to the drawings a preferred form of panel is constructed as
follows:
In Fig 1 the panel 1 has a typical size of 3600 x 7200mm with core
web s at 400mm each way. The lower skin 3 has
longitudinal joints 5 and transverse joints 6 and the upper skin 2 has
Received 3 Aug 2012
corresponding joints 4. The core has intersecting web members 7
and in this described example they are 9mm plywood. The panel is
provided with edge members 10. Where floor panels are
evered, support points for the panel are provided by laminating
plywood pads to the outer face of the lower skin. Between the
intersecting web s part or full infill of low density insulation
or part infill of structured open or closed cell foams, or full infill of
structured open or closed cell foams, are on fitted with partial
infill 8 glue bonded to one skin and full infill 9 glue bonded to both
top and bottom skins. Inset support points may be additionally
reinforced with plywood pads laminated to the internal face of the
lower skin between the intersecting webs and edge members
surrounding these load points.
In Fig 2 is an alternative preferred form of the invention of a panel
with a typical panel size of 2400 x 7200mm using 2400 X 1200 mm
sheets to form the top skins 2 and ponding bottom skins 3 with
longitudinal joints 4 and no transverse joints. In all other respects the
descriptions for Fig 1 apply. Where floor panels are cantilevered,
support points for the panel are provided by laminating plywood
pads to the outer face of the lower skin and as shown in Fig.3
Received 3 Aug 2012
In Fig 4 the exploded isometric projection shows ents of a
panel, the upper skin being 2, transverse core webs 13,
longitudinal core webs 14, inner edge member 15, outer edge
member 16, the lower skin 3. Notches 17 are cut to half depth at the
same intervals in each set of web s and infill 8 or 9 or 24
between the intersecting webs.
In Fig 5 the components in Fig 4 are assembled to form the egg crate
core of web members with the range of infill 8, 9 or 24 friction fitted
between the core and edge members, with each set of web members
at right angles and the infill in ponding squares, although other
angles may be used.
In Fig 6 a detailed cross-section of the panel edge is shown with the
tapered insert access disc 20 removed from the upper skin 2, at
points of panel to panel joining and the inserted disc is placed in the
access hole 19 with its glue joint 21. The outer edge member 16 has
a rebated edge 22 for panel to panel joining into which is placed a
circular locating connector tube 23, and the infill 24 is part or full low
density insulation. All glue lines within the assembly are shown as
heavy lines referenced 21.
Received 3 Aug 2012
In Fig 7 it is a similar cross section to Fig 6 but with a part infill of
structured open or closed cell foam 8 friction fitted between the
intersecting webs and glue bonded 21 to the lower skin 3.
In Fig 8 it is a similar cross section to Fig 6 but with a full infill of a
structured open or closed cell foam 9 friction fitted between the
intersecting web and glue bonded 21 to both the upper skin 2 and the
lower skin 3.
In Fig 9 it is a similar cross section to Fig 6 but with the part infill 8
delineated by the dotted line or the full infill 9 of a structured open or
closed cell foam glue bonded 21 to not only the skins but on all four
edges to the faces referenced 27 of the intersecting webs 7 and the
face of the inner edge member 15.
In Fig 10 the contact faces of the intersecting webs are unglued 25
as are the edge faces 26 of all the core infill types in t with the
webs.
In Fig 11 the contact faces of the intersecting webs are glued 21
shown as heavy lines along the glue line, while the edge faces 26 of
all the core infill types in contact with the webs are not.
Received 3 Aug 2012
In Fig 12 both the contact faces of the intersecting webs are glued 21
and the edge faces of all the core infill types in t with the webs
are glued 27.
In Fig 13 the contact faces of the intersecting webs are unglued 25
while all the edge faces of all the core infill types in contact with the
webs are glued 27.
In Fig 14 ed components of the Fig 6 assembly are shown with
edges which are surfaces always glued 21 and surfaces 27 which
remain unglued but glued in the preferred form of the invention.
In Fig 15 are exploded components of Fig 7 assembly with glue line
21 to the surface of the face of the infill in contact with the skin.
In Fig 16 are ed components of Fig 8 assembly with glue lines
21 to both surfaces of the infill in contact with the upper and lower
skins.
In Fig 17 are exploded components of Fig 9 for part infill with glue
lines 27 to the surfaces of the infill in contact with the side faces of
the web in a preferred form of the invention.
ed at IPONZ 23 August 2012
In Fig 18 are exploded components of Fig 9 for full infill with glue
lines 27 to the surfaces of the infill in contact with the side faces of
the web in a preferred form of the invention.
In Fig 19 the joint between two assembled panels is shown in detail.
A circular hole 19 is cut into the skins for access to the jointing bolt
29 which passes h a transverse hole 28 in the tubularjointing
member, a formed rebated slot 30 in the infill 9 is formed at the
jointing access. Once jointing is ted the insert disc 20 is glued
into place.
In Fig 20 alternative outer edge s are shown.
In Fig 203 the outer edge member 16 is timber, finger-jointed timber,
laminated veneer lumber, oriented strand board, laminated strand
lumber, or parallel strand lumber and profiled for the tubular panel to
panel jointer.
Fig 20b. The edge member is of plywood Iaminations in a preferred
form of the invention and profiled for the tubular panel to panel jointer.
Fig 200 The outer edge member is not profiled as it is for an outer
panel face where there is no panel to panel jointing and is of the
same al options as in 20a.
Fig 20d The panel orientation is that of 200 and the member is of
laminated plywood in a preferred form of the invention.
Received 3 Aug 2012
In Fig 21 is a panel to panel plan showing a typical location ofjointing
tubes 23 of short s although full lengths can be inserted into
the profiled outer edge members 20a or 20b reference Fig.20 and the
positions of the bolting access holes 19.
In Fig 22 there is shown means of connecting wall panels or framed
walls to the panels by means of a continuous plywood tongue 32, the
length of the walls glue bonded into a rebate in the bottom and top
plates 31 of the walls and the tongue is then screw fixed into the
panels outer edge member 16.
In Fig 23 there is shown means of connecting internal wall panels or
frame walls at a panel to panel jointing by means of recessed case
hardened washer head wood screws 33 into the top or bottom wall
plates 34.
In Figs 24 to 27 there is shown means and methods ofjoining sheet
facing materials in the skins 2 and 3 of the panels and the webs of
the core.
In Figs 24 and 25 the skin 36 is ed with a v-shaped slot into
which a feather 35 of plywood or other suitable material is assembled
with a glue line 21 as shown. If the skin is of plywood of three
veneers the feather is of three veneers to obtain m contact
Received 3 Aug 2012
area between the parallel . In the preferred form of the
invention this ng is for the long edges of the plywood sheets
with the face s grain running parallel to the joint. The groove
in the skin edges and the slopes of the feather is a double taper of 1
in 8 with the feather slightly undersized to allow for the glue. Where
thicker skins are required a series of grooves and rs is possible.
In Fig 26 a scarfed joint 37 is used to join the ends of the plywood
skin sheets and webs 36, the scarfed joint being 1 in 10 for up to
12mm thick d and 1 in 8 for thicker sheets.
In Fig 27 an alternative jointing for the webs only is to use a structural
fingerjoint 38.
In Fig 28 there is shown the preferable position of the edge joints
carried between transverse webs to decrease the risk of joint
breaking over a web.
In Fig 29 a preferred method of assembly of the invention is where
the upper and lower skins 2 and 3, depending on the panels
configurations, are jointed, glued and pressed separately. The same
applies to the edge members 10 and the core webs, again
assembled and glued as a separate unit. Full infills have the option
of inclusion at this stage or installation as with part infills at the final
gluing and pressing together of all three components and the panel
constructed as bed will maintain a very flat surface when
erected in a horizontal or vertical plane even when fully loaded.
Received at IPONZ 13 September 2012
Claims (4)
- A structural building panel being a stressed-skinned panel, in combination with structured open or closed cell foams, of a density of 16kg/m3 or more and a compressive strength greater than 85KPA, serving as whole or part floor or roof or g or wall panels of room spaces, in single or multi-storey buildings, the stressed-skinned panel comprising a pair of skins, each skin is a plurality of plywood sheets, an egg-crate structure is formed by ocking web strips and an edge frame, a core between the skins is an egg-crate ure of longitudinal and transverse webs interlocking at an angle that is substantially 90°, with each web having notches at one half the depth of the web at their points of intersection, with partial or full infills of structured open or closed cell foam fitted within cells formed by the interlocking webs of the egg-crate structure.
- A ural building panel as claimed in Claim 1 in which the l or full infills of structured open or closed cell foams are friction-fitted within the cells formed by the interlocking webs of the egg-crate structure. Recevied at IPONZ 23 August 2012
- 3. A ural building panel as claimed in Claim 1 in which the partial or full infills of structured open or closed cell foams are friction- fitted within the cells formed by the interlocking webs of the egg-crate structure and adhesive bonded to either the upper or lower skin of the panel.
- 4. A structural building panel as claimed in claim 1 in which full s of structured open or closed cell foams are friction-fitted within the cells formed by the interlocking webs of the egg-crate structure and adhesive bonded to both the upper and lower skins of the panel forming a sandwich-structured composite within the cells formed by the interlocking webs of the egg-crate ure. A structural building panel as claimed in claim 1 in which full infills of structured open or closed cell foams are foamed into place with a bonding or adhesive agent or are fitted and ve-bonded to all the faces of the cells formed by the interlocking webs of the egg- crate structure and adhesive bonded to both the upper and lower skins of the panel and each of the filled cells becomes an individual sandwich structured composite panel within the stress-skinned panel. Recevied at IPONZ 23 August 2012 A structural building panel substantially as herein described with reference to and as shown in the anying drawings. Dated this 23rd ...... day of ...August....2012 Applicant: Keith Eric Hay fig.3 sechon A'-A 1of11
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NZ592598A NZ592598B (en) | 2012-08-23 | Structural Improvements Relating To Building Panels |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NZ592598A NZ592598B (en) | 2012-08-23 | Structural Improvements Relating To Building Panels |
Publications (2)
Publication Number | Publication Date |
---|---|
NZ592598A NZ592598A (en) | 2012-10-26 |
NZ592598B true NZ592598B (en) | 2013-01-29 |
Family
ID=
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