NZ221389A - Polystyrene foam panel: adhesively bonded coextensive frames on front and back surfaces: one frame in rebates on only one surface - Google Patents
Polystyrene foam panel: adhesively bonded coextensive frames on front and back surfaces: one frame in rebates on only one surfaceInfo
- Publication number
- NZ221389A NZ221389A NZ221389A NZ22138987A NZ221389A NZ 221389 A NZ221389 A NZ 221389A NZ 221389 A NZ221389 A NZ 221389A NZ 22138987 A NZ22138987 A NZ 22138987A NZ 221389 A NZ221389 A NZ 221389A
- Authority
- NZ
- New Zealand
- Prior art keywords
- laths
- core panel
- building element
- composite building
- frame
- Prior art date
Links
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/38—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure with attached ribs, flanges, or the like, e.g. framed panels
- E04C2/386—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure with attached ribs, flanges, or the like, e.g. framed panels with a frame of unreconstituted or laminated wood
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/38—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure with attached ribs, flanges, or the like, e.g. framed panels
- E04C2/382—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure with attached ribs, flanges, or the like, e.g. framed panels with a frame of concrete or other stone-like substance
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/38—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure with attached ribs, flanges, or the like, e.g. framed panels
- E04C2/384—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure with attached ribs, flanges, or the like, e.g. framed panels with a metal frame
Abstract
The composite building element comprises a core panel 1 of a rigid foamed material of an expanded synthetic resin and two stiff frames 3, 5 of essentially the same length and the same width as the length and width of the core panel 1. The stiff frames 3, 5 are bonded to the back and front surface 2, 12 of the core panel 1.
Description
22 1 3«9
ptiofrtV
Da1
MsV-
-£>$»•
v»%p r,»
St>8'
.«lea«on p\-ed".
,i£.
.^©r
1
;:Ucf^on
EVite' •
i^Sl:
SC]
NEW ZEALAND
PATENTS ACT, 1953
No.: Date:
COMPLETE SPECIFICATION
COMPOSITE BUILDING PANELS
■i/we. THE DOW CHEMICAL COMPANY 2030 Dow Center, Abbott Road, Midland, Michigan 48640, United States of America, a corporation organized and existing under the laws of the State of Delaware, United States of America,
hereby declare the invention for which-i / we pray that a patent may be granted to me/us, and the method by which it is to be performed, to be particularly described in and by the following statement: -
(foilowed bv Daqe la)
£213##
COMPOSITE BUILDING PANEL
The present invention relates to composite building elements and in particular to composite building panels which have various applications in the building industry, for •example for building walls, floors, ceilings and roofs.
One popular method of building a wall is to build a timber frame which is then filled with glass wool. Since these timber frames are not highly shear resistant, a plywood sheathing is usually nailed to the timber frame. However, the plywood sheathing is relatively expensive and it does not always provide the building element with sufficient shear resistance. Insufficient shear resistance is also experienced when a chip board is nailed to the timber frame instead of plywood. The use of a chip board is furthermore disadvantageous because of the excessive weight of the chip board which is required to obtain satisfactory strength.
In GB patent specification 1 587 012 it is suggested to close a wall space defined by the timber frames of a building with a foamed polyurethane or a foamed polystyrene. However, such timber frames of which the wall space is filled with foamed polyurethane or polystyrene sheets have several disadvantages when building the walls. First, the size of the frame and of the foam sheet or slab must be very well adjusted to each other in order to avoid gaps between the frame and the foam sheet or slab. Special seals have been suggested in GB patent specification 1 587 012 in order to fill such difficult to avoid gaps, but such seals increase the installation costs. Furthermore, the timber frame has much lower insulation properties than the foam loc
C-34,761
sheet or slab and therefore forms thermal bridges in the building panel.
In U.S.A. Patent Specification 4,193,244 a module block is disclosed which consists of two parallel fiber plates. To each fiber plate two parallel laths are fixed. For connecting the two fiber plates with each other, side plates, for example fiber plates or chip boards, are fixed to the laths perpendicularly to the first two fiber plates.Between the four plates, an insulation material such as rock-wool is placed. However, fiber-plates, ply-wood or chip boards of heavy weight are required for providing sufficient shear strength to the module block. Furthermore, the side plates produced of fiber plates,-chip board or ply-wood boards have insufficient insulation properties and therefore form thermal bridges in the module block.
Therefore, it is desirable to provide a composite building element which does not only have good insulation properties but also high strength, in particular high shear resistance. It is also desirable to provide a building element which can be prefabricated and easily installed and which preferably has a relatively low weight.
The present invention provides a composite building element which comprises
) a core panel of a rigid extruded polystyrene foam having a density of from 20 to 60 kg/m3, wherein at most one of the surfaces selected from the back surface and the front surface of the core panel is provided with a rabbet along the edges of the core panel and, if required, with one or more grooves and jtwo stiff frames of substantially the same length and the same width as the length and width of the core panel bonded to the back and front surfaces of the core panel by an adhesive, whereby one of the stiff frames is placed in the rabbets and the one or more grooves, when present, on the back or front surface of the core panel.
The composite building element of the present invention has a surprisingly high resistance to shearing forces.
221389
sheet or slab and therefore forms thermal bridges in the building panel.
In U.S.A. Patent Specification 4,193,244 a module-block is disclosed which consists of two parallel fiber plates. To each fiber plate two parallel laths are fixed. For connecting the two fiber plates with each other, side plates, for example fiber plates or chip boards, are fixed to the laths perpendicularly to the first two fiber plates.Between the four plates, an insulation material such as rock-wool is placed. However, fiber-plates, ply-wood or chip boards of heavy weight are required for providing sufficient shear strength to the module block. Furthermore, the side plates produced of fiber plates,• chip board or ply-wood boards have insufficient insulation properties and therefore form thermal bridges in the module block.
Therefore, it is desirable to provide a composite building element which does not only have good insulation properties but also high strength, in particular high shear resistance. It is also desirable to provide a building element which can be prefabricated and easily installed and which preferably has a relatively low weight.
The present invention provides a composite building element which comprises a core panel of a rigid extruded polystyrene foam having • a density of from 20 to 60 kg/m3, wherein at most one of \ the surfaces selected from the back surface and the front surface of the core panel is provided with a rabbet along the edges of the core panel and, if required, with one or more
J grooves and two stiff frames of substantially the same length and the same width as the length and width of the core panel bonded to the back and front surfaces of the core panel by an adhesive, whereby one of the stiff frames is placed in the rabbets and the one or more grooves, when present, on the back or front surface of the core panel.
The composite building element of the present invention has a surprisingly high resistance to shearing forces.
221389
o
Furthermore, the composite building element of the present invention does not provide thermal bridges.
Fig. 1 illustrates a back perspective view on a first embodiment on the composite building element of the present '5 invention.
Fig. 2.illustrates-a front perspective view on the first -embodiment on the composite building element.
Fig. 3 represents a schematic illustration of the cross-section of the composite building element along line A-A in 10 Figs. 1 and 2.
Fig. 4 to 7 are schematic illustrations of the cross-section of further embodiments of the composite building element of the invention.
The composite, building element of the present invention 15 will be further described with reference to the drawings.
With reference to Fig. 1, the composite building element comprises a core panel 1 of rigid foamed polystyrene. The core panel 1 is a rigid extruded polystyrene panel which has a density of from 20 kg/m3, preferably of from 30 kg/m3, to 20 - 60 kg/m3, preferably to 50 kg/m3. Most preferably, the core panel is moisture resistant. The thickness of the core panel 1 depends on the desired insulating properties and strength of the building element. Preferably, the thickness is from 30 ram to 200 mm, most preferably from 50 mm to 120 mm. The 30 • length and width of the panel is not critical. Usual lengths are from 2 to 6 m, preferably from 2 to 3 m. Usual widths are from 0.6 to 12 m, preferably from 1 to 5.
Wk¥s!Wi4-h-.-V ■
' . -O '• '"V.
221389
A stiff back frame 3 and a stiff front frame 5 are fixed to the back surface 2 and front surface of the core panel 1. The frames 3, 5 have substantially the same length and same width as the length and width of the core panel 1, however,
0 5 it is not necessary that the length and width of the frames
_
3, 5 are exactly the same as those of the core panel 1. The back frame 3 consists of a first set of at least two parallel laths 7a, 7b connected to a second set of at least two parallel laths 7c, 7d which are perpendicular to the laths 10 7a, 7b. As illustrated by Fig. 1, the back frame 3 can be subdivided by one or more additional laths 8 which are preferably parallel to the main laths 7c, 7d.
The laths 7a, 7b, 7c, 7d and 8 can be produced of any sufficiently strong and stiff material to resist forces 15 which are applied perpendicularly to the smallest cross-section of the back frame 3, i.e. to the cross-section ■ along line A-A and perpendicularly to the plane defined by the back frame 3. Usual materials are for example wood, metal, concrete or hard plastic materials. If the back
frame 3 is produced of wood, the main laths 7a, 7b, 7c, 7d have prefer ably a cross-section within the range of from 20 x 20 mm to 150 mm X
150 mm, most preferably of from 50 x 50 mm to 100 x 100 mm. The additional lath 8 can have the same cross-section. In ^ general, the cross-section of the additional lath 8 is
smaller, for example from 20 x 20 mm to 80 x 80 mm, prefer-'ably from 25 x 25 mm to 50 x 50 mm. Fig. 1 illustrates that the back frame 3 and the front frame 5 are not in contact • with each other. Therefore, the composite building element O of the present invention does not provide the undesired
thermal bridges through the thickness of the building element. The back frame 3 and front frame 5 can be fixed to the core panel 1 by applying an adhesive such as a polyurethafie. adhesive between the adjacent surfaces of the back frame 3. and the
22 13 8#
core panel 1 and between the adjacent surfaces of the front frame 5 and the core panel 1.
The main back laths 7a, 7b, 7c, 7d and optionally the additional back lath 8 can be fixed to each other by any suitable means to build the back frame 3 such as nailing or gluing.
If desired,, the corners of the back frame 3 can be. reinforced, for example by metal plates which are fixed to the corners of the back frame 3 and to the -core panel 1.
Fig. 2 illustrates the same embodiment of the composite building element of the present invention as Fig. 1, however, Fig. 2 represents a perspective front view on the building element. Fig. 2 illustrates a core panel 1 as described with reference to Fig. 1. A stiff front frame 5 is fixed to the front surface 12 of the core panel 1. The front frame 5 is built of a first set of at least two parallel laths 9a, 9b and a second set of at least two parallel laths 9c, 9d which are perpendicular to the first set of laths 9a, 9b. The frame consisting of the main laths 9a, 9b, 9c, 9d can be subdivided by one or more optional additional front laths 10. The front laths 9a, 9b, 9c, 9d and 10 can have the same dimension as the back laths 7a, 7b; 7c, 7d and 8 described with reference to Fig. 1.
Cut out along the edges of the front surface 12 of the core panel 1 are rabbets (see 14a and 14b in Fig. 3) which have essentially the same widths and depths as the widths and thickness of the main front laths 9a, 9b, 9c, 9d. The front surface 12 of the core panel 1 is further provided with a groove (see 16 in Fig. 3) extending parallel to the edges of the core panel 1 and which has essentially the same dimensions as the cross-section of the additional front lath 10. The front laths 9a, 9b, 9c, 9d and 10 are placed q-34,761
221339
in these rabbets and this groove and fixed to the core panel 1.
As an alternative or in addition to the rabbets and groove(s) in the front surface 12 of the core panel 1, the back surface 2 of the core panel 1 can be provided with rabbets and/or one or more grooves.
Fig. 1 and 2 illustrate composite building elements of rectangular shape. In some cases however, it may be desirable that the core panel does not have a rectangular back or front surface but that is has surfaces of a triangular or trapezoid shape. Such shapes are for example preferred when building the portion of a wall which will be in contact with a sloped roof. In such a case, the two stiff frames are adjusted to the shape of the core panel. In one embodiment of the frames, each frame consists of one set of at least two parallel laths, a lath which is perpendicular to this set of parallel laths and one lath which is neither parallel nor perpendicular to this set of parallel laths.
Fig. 3 illustrates a cross-section along the line A-A in Figs. 1 and 2. Fig. 3 illustrates how the main back laths 7c, 7d and the additional back lath 8 are arranged on the back surface 2 of the core panel 1. The front surface 12 of the core panel 1 is provided with rabbets 14a, 14b and with a groove 16. The main front laths 9c, 9d and the additional front lath 10 are placed in these rabbets 14a, 14b and the groove 16 respectively and fixed to the core panel 1.
Fig. 4 illustrates how the composite building panel described with reference to Fig. 3 can be combined with other materials to build a complete wall. An interior finishing layer 20, for example a wood sheet or a gypsum plaster
C-34,761
6
2213«S
board is attached to the main back laths 7c, 7d and to the additional lath 8 as well as to the main back laths 7a, 7b (not shown). Thereby a space 22 is built which allows any pipes and electric cables to be fit into the building element in a convenient way. The front surface 12 of the core panel 1 is covered with an external rendering 24.
Fig. 5 illustrates a cross-section through another embodiment of the composite building element of the present invention. The main front laths 9e, 9f, the main front laths 9a, 9b (not shown) and the additional front lath 11 are not flush with the front surface 12 of the core panel 1 but are protruding. An external finishing material 26 such as a wood cladding can be attached to the main front laths 9e, 9f, to the main front laths 9a, 9b (not shown) and to the additional front lath 11 whereby a second space 28 in addition to space 22 is provided.
In Fig. 6 a type of cross-section of the main back laths 7e, 7f and of the additional back lath 18 is illustrated which allows the attachment of a fire protection material 30, such as a gypsum layer, directly to the back surface 2 of the core panel 1.
Fig. 7 illustrates a cross-section through an embodiment of the composite building element similar to that illustrated by Fig. 5. However, the front surface 12 of the core panel 1 is not provided with grooves or rabbets.
The following exeanple illustrates the composite building element of the present invention and its shear resistance compared to known building elements used in the industry.
C-34,761
7
22 1
Example
A type of composite building element illustrated in Figs. 1 to 3 is tested. The core panel consists of rigid extruded polystyrene foam of a density of about 45 kg/m3. The length 5 of the panel is 240 cm, the width 120 cm and the thickness 80 mm. The stiff back frame is built of four main spruce laths of 75 mm x 55 mm cross-section and an additional -spruce lath of 40 mm x 55 mm cross-section. In the corners, the main timber frame built by the spruce laths of 75 mm x 10 55 mm cross-section is reinforced by diagonally divided square steel nail plates of 300 mm side length and a thickness of 2 mm. The steel plates are nailed irregularly and glued with a polyurethane adhesive to the back frame and to the core panel. The stiff front frame is built of 15 four main spruce laths and an additional spruce lath of 50 mm x 30 mm cross-section. The back and front timber frames are glued with a polyurethane adhesive to the back and front surfaces of the core panel.
Comparative Example A
A spruce frame of 240 cm length and the same width is produced of
- 5 parallel laths of 240 cm length placed at equal distance from each other, the middle lath has a cross-section of 45 x 97 mm and the other four laths have a
cross-section of 36 x 97 mm, and
- a pair of studs of 36 x 97 mm cross-section which are perpendicular to the set of 5 parallel laths. Each stud is fixed to each lath with two nails of 3.3 x 90 mm.
8
C-34,761
/
o
—N 15
; O
22 1 389
The shear resistance of this frame is provided by a sheet of 8 mm plywood nailed with nails (2.1 x 45 mm) on each lath and stud of the frame, every 15 cm on the studs and the two outside laths and every 30 cm on the three middle laths. A gypsum plaster board is nailed to the other side of the frame. The space between these two faces is filled with a glass fiber insulation of 100 mm thickness.
Comparative Example B
The same frame as described in Comparative Example A is produced. The shear resistance is provided on both sides by a sheet of 12 mm chipboard nailed with nails (2.8 x 55 mm) every 15 cm on the studs and the two outside laths and every 30 cm on the three middle laths of the frame. The space between the two chipboard sheets is filled with a glass fiber insulation of 100 mm thickness.
For testing the shear resistance of the building elements, two identical composite building panels of the Example are installed vertically side by side, fixed firmly to the floor and interconnected. One panel of each of Comparative Examples A and B is also installed vertically and fixed firmly to the floor. Across the surface of the panels variable horizontal shearing forces are applied near the upper edge of the panels. The following table illustrates
9
C-34,761
2213 8$
the weight of the building elements,
the horizontal shearing force (load) which needs to be applied until the building element breaks,
the horizontal shearing force (load) which is necessary to cause 5 mm deflection of the building element in the cases where a) no vertical load and b) additionally 2.5 kN vertical load is applied and the insulation properties"of the building elements.
C-34,761
o o
• o 0
Example 1
Comp. Example A Comp. Example B
Overall dimension (mm)
2400 X 2400 2400 x 2400
Weight (kg) 62
Horizontal load at rupture (kN) 39,6
Horizontal load for 5 mm deflection with 2.5 kN vertical load (kN) 5,05
Horizontal load for 5 mm deflection with no vertical load (kN) 4
Thermal conductivity (W/m2K) 0,28
71 11
3,92
2,51 0,34
2400 x 2400 137 28
0,32
o
©
12
Claims (6)
1. A composite building element comprising a) a core panel of a rigid extruded polystyrene foam having a density of from 20 to 60 kg/m3, wherein at most one of : the surfaces selected from the back surface and the front surface of the core panel is provided with a rabbet along the edges of the core panel and , if required, with one or more grooves and b) two Stiff frames of substantially the same length and the same width as the length and width of the core panel, bonded to the back and front surfaces of the core panel ^ by an adhesive, whereby one of the stiff frames is placed in the rabbets and the one or more grooves, when o present, on the back or front surface of the core panel.
2. The composite building element of claim 1 wherein each frame consists of a first set of at least two laths connected to a second set of at least two laths whereby the laths of the second set are parallel to each ^ other and are perpendicular to at least one lath of the first set.
3. The composite building element of claim 1 wherein each frame consists of a first set of at least two parallel laths connected to a second set of at least two parallel laths which second set of laths is {Appendicular to the first set of laths and the laths have a cross-section within the range of from 20 mm x 20 mm to 150 nun x 150 mm. 221389 - 13 -
4. The composite building element of claim 2 or claim 3 wherein the laths of the frames are made of wood, metal or concrete.
5. The composite building element of any one of claims 1 to 4 wherein the core panel is a rigid extruded polystyrene foam panel having a density of from 30 to 50 kg/m3. to 5 wherein eitherthe front surface orthe back surface of the core panel is provided with a rabbet along the edges of the core panel and, if required, with one or more grooves. 7. The composite building element of claim 1 substantially as hereinbefore described with reference to any one of Figures 1 to 7. 8. The composite building element of claim 1 substantially as hereinbefore described with reference to the Example.
6. The composite building element of any one of claims 1 OAT
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH3290/86A CH670671A5 (en) | 1986-08-15 | 1986-08-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NZ221389A true NZ221389A (en) | 1991-12-23 |
Family
ID=4252786
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NZ221389A NZ221389A (en) | 1986-08-15 | 1987-08-10 | Polystyrene foam panel: adhesively bonded coextensive frames on front and back surfaces: one frame in rebates on only one surface |
Country Status (8)
| Country | Link |
|---|---|
| EP (1) | EP0260435B1 (en) |
| AT (1) | ATE50612T1 (en) |
| AU (1) | AU596683B2 (en) |
| CH (1) | CH670671A5 (en) |
| DE (1) | DE3761775D1 (en) |
| ES (1) | ES2013279B3 (en) |
| NO (1) | NO171647C (en) |
| NZ (1) | NZ221389A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7713615B2 (en) | 2001-04-03 | 2010-05-11 | James Hardie International Finance B.V. | Reinforced fiber cement article and methods of making and installing the same |
| US7993570B2 (en) | 2002-10-07 | 2011-08-09 | James Hardie Technology Limited | Durable medium-density fibre cement composite |
| US7998571B2 (en) | 2004-07-09 | 2011-08-16 | James Hardie Technology Limited | Composite cement article incorporating a powder coating and methods of making same |
| US8281535B2 (en) | 2002-07-16 | 2012-10-09 | James Hardie Technology Limited | Packaging prefinished fiber cement articles |
| US8297018B2 (en) | 2002-07-16 | 2012-10-30 | James Hardie Technology Limited | Packaging prefinished fiber cement products |
| US8993462B2 (en) | 2006-04-12 | 2015-03-31 | James Hardie Technology Limited | Surface sealed reinforced building element |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| HRP20021035B1 (en) * | 2002-12-30 | 2011-02-28 | Jurić Rozarijo | Wall panels for fast construction of structures |
| GB201009727D0 (en) * | 2010-06-11 | 2010-07-21 | Module Home Future Bvba | Building system |
| DE102014112987A1 (en) * | 2014-09-09 | 2016-03-10 | Holz Element Produktion Gmbh & Co. Kg | module element |
| JP6386430B2 (en) * | 2015-09-14 | 2018-09-05 | 大建工業株式会社 | Panels and doors with decorative joints |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3305986A (en) * | 1962-08-07 | 1967-02-28 | Foam Products Corp | Insulated enclosures and panels therefor |
| SE405029B (en) * | 1977-04-19 | 1978-11-13 | Samuelsson Sture Lennart | MODULE BLOCKS AND MODULE SYSTEMS FOR HOUSE BUILDINGS AND WAYS OF MANUFACTURE OF MODULE BLOCKS |
| CA1124482A (en) * | 1978-06-28 | 1982-06-01 | Cano Thermo Systems Inc. | Panel structure and building structures made therefrom |
| DE3440297A1 (en) * | 1984-11-05 | 1986-05-22 | Greschbach, Manfred, 7637 Ettenheim | PANEL SHAPED WALL ELEMENT |
-
1986
- 1986-08-15 CH CH3290/86A patent/CH670671A5/de not_active IP Right Cessation
-
1987
- 1987-08-10 NZ NZ221389A patent/NZ221389A/en unknown
- 1987-08-10 AU AU76734/87A patent/AU596683B2/en not_active Ceased
- 1987-08-11 ES ES87111611T patent/ES2013279B3/en not_active Expired - Lifetime
- 1987-08-11 DE DE8787111611T patent/DE3761775D1/en not_active Expired - Fee Related
- 1987-08-11 AT AT87111611T patent/ATE50612T1/en not_active IP Right Cessation
- 1987-08-11 EP EP87111611A patent/EP0260435B1/en not_active Expired - Lifetime
- 1987-08-14 NO NO873431A patent/NO171647C/en not_active IP Right Cessation
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7713615B2 (en) | 2001-04-03 | 2010-05-11 | James Hardie International Finance B.V. | Reinforced fiber cement article and methods of making and installing the same |
| US8281535B2 (en) | 2002-07-16 | 2012-10-09 | James Hardie Technology Limited | Packaging prefinished fiber cement articles |
| US8297018B2 (en) | 2002-07-16 | 2012-10-30 | James Hardie Technology Limited | Packaging prefinished fiber cement products |
| US7993570B2 (en) | 2002-10-07 | 2011-08-09 | James Hardie Technology Limited | Durable medium-density fibre cement composite |
| US7998571B2 (en) | 2004-07-09 | 2011-08-16 | James Hardie Technology Limited | Composite cement article incorporating a powder coating and methods of making same |
| US8993462B2 (en) | 2006-04-12 | 2015-03-31 | James Hardie Technology Limited | Surface sealed reinforced building element |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0260435A1 (en) | 1988-03-23 |
| NO171647B (en) | 1993-01-04 |
| NO171647C (en) | 1993-04-14 |
| ES2013279B3 (en) | 1990-05-01 |
| AU7673487A (en) | 1988-02-18 |
| AU596683B2 (en) | 1990-05-10 |
| NO873431L (en) | 1988-02-16 |
| CH670671A5 (en) | 1989-06-30 |
| NO873431D0 (en) | 1987-08-14 |
| ATE50612T1 (en) | 1990-03-15 |
| DE3761775D1 (en) | 1990-04-05 |
| EP0260435B1 (en) | 1990-02-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6205729B1 (en) | Asymmetric structural insulated panel | |
| US10024057B2 (en) | Construction panel system and methods of assembly thereof | |
| US5899037A (en) | Composite wall structure | |
| US6209284B1 (en) | Asymmetric structural insulated panels for use in 2X stick construction | |
| US4329827A (en) | Roofing elements | |
| US4603531A (en) | Structural panels | |
| CA2692723C (en) | Structural insulated roof panels with a rigid foam core | |
| US4304080A (en) | Construction beam | |
| JPH08506150A (en) | Architectural panel and building using the panel | |
| WO2013070348A1 (en) | Structural interlocking wood panel | |
| EP0536161A1 (en) | Floor construction. | |
| WO1994013897A1 (en) | Foam sandwich enclosure with interlocking integral frame | |
| EP0260435B1 (en) | Composite building panels | |
| US5617700A (en) | Prefabricated building panel | |
| US6330775B1 (en) | Prefabricated building wall structure | |
| GB2082645A (en) | Composite long span in building panel | |
| US20040226255A1 (en) | Composite beam | |
| FI98398C (en) | Wall element | |
| KR101375028B1 (en) | the insulation complex panel with structural wood and the construct method of wall therewith | |
| EP0675990B1 (en) | Building unit, preferably for roofing structures, and a method of manufacturing it | |
| JPH11131683A (en) | Composite panel | |
| US4490955A (en) | Residential wall construction | |
| JP2000170305A (en) | Sound insulation floor panel and sound insulation floor panel mounting structure | |
| JP2561588B2 (en) | Construction method of partition in building | |
| JPH09132946A (en) | Earthquake-proof wall structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ERR | Error or correction |
Free format text: THE OWNER HAS BEEN CORRECTED TO 101320, THE DOW CHEMICAL COMPANY, 2030 DOW CENTER, MIDLAND, MICHIGAN 48674, US Effective date: 20140311 Free format text: THE AGENT HAS BEEN CORRECTED TO 101320, THE DOW CHEMICAL COMPANY, 2030 DOW CENTER, MIDLAND, MICHIGAN 48674, US; THE CONTACT HAS BEEN CORRECTED TO 101320, THE DOW CHEMICAL COMPANY, 2030 DOW CENTER, MIDLAND, MICHIGAN 48674, US Effective date: 20140311 |