EP0260435A1 - Panneau de construction composite - Google Patents

Panneau de construction composite Download PDF

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Publication number
EP0260435A1
EP0260435A1 EP87111611A EP87111611A EP0260435A1 EP 0260435 A1 EP0260435 A1 EP 0260435A1 EP 87111611 A EP87111611 A EP 87111611A EP 87111611 A EP87111611 A EP 87111611A EP 0260435 A1 EP0260435 A1 EP 0260435A1
Authority
EP
European Patent Office
Prior art keywords
laths
core panel
composite building
building element
frame
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
EP87111611A
Other languages
German (de)
English (en)
Other versions
EP0260435B1 (fr
Inventor
Jean-Philippe Jacques Deblander
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dow Chemical Co
Original Assignee
Dow Chemical Co
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 Dow Chemical Co filed Critical Dow Chemical Co
Priority to AT87111611T priority Critical patent/ATE50612T1/de
Publication of EP0260435A1 publication Critical patent/EP0260435A1/fr
Application granted granted Critical
Publication of EP0260435B1 publication Critical patent/EP0260435B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building 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
    • E04C2/38Building 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
    • E04C2/386Building 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
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building 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
    • E04C2/38Building 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
    • E04C2/382Building 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
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building 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
    • E04C2/38Building 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
    • E04C2/384Building 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

Definitions

  • 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.
  • 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.
  • such timber frames of which the wall space is filled with foamed polyurethane or polystyrene sheets have several disadvantages when building the walls.
  • 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.
  • the timber frame has much lower insulation properties than the foam sheet or slab and therefore forms thermal bridges in the building panel.
  • a module block 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.
  • 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
  • the composite building element of the present invention has a surprisingly high resistance to shearing forces. Furthermore, the composite building element of the present invention does not provide thermal bridges.
  • the composite building element comprises a core panel 1 of a rigid foamed material of an expanded synthetic resin, such rigid foamed polyurethane or rigid foamed polystyrene.
  • the core panel 1 is a rigid extruded polystyrene panel which has a density of from 20 kg/m 3 , preferably of from 30 kg/m 3 , to 60 kg/m 3 , preferably to 50 kg/m 3 .
  • 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 mm to 200 mm, most preferably from 50 mm to 120 mm.
  • the 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.
  • 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 essentially the same length and same width as the length and width of the core panel 1, however, 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 and a second set of at least two parallel laths 7c, 7d which are perpendicular to the laths 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 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.
  • the main laths 7a, 7b, 7c, 7d have preferably a cross-section of from 20 x 20 mm to 150 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.
  • the cross-section of the additional lath 8 is smaller, for example from 20 x 20 mm to 80 x 80 mm, preferably 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 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 in any suitable means, preferably by applying an adhesive such as a polyurethane adhesive between the adjacent surfaces of the back frame 3 and the 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
  • 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 in these rabbets and this groove and fixed to the core panel 1.
  • the back surface 2 of the core'panel 1 can be provided with rabbets and/or one or more grooves.
  • 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.
  • a fire protection material 30 such as a gypsum layer
  • Fig. 7 illustrates a cross-section through an embodiment of the composite building element similar to that illustrated by Fig. 5.
  • the front surface 12 of the core panel 1 is not provided with grooves or rabbets.
  • the following example illustrates the composite building element of the present invention and its shear resistance compared to known building elements used in the industry.
  • the core panel consists of rigid extruded polystyrene foam of a density of about 45 kg/m 3.
  • the length 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 5S 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 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 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.
  • a spruce frame of 240 cm length and the same width is produced of
  • 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 1 4 ths.
  • 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.
  • 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.
EP87111611A 1986-08-15 1987-08-11 Panneau de construction composite Expired - Lifetime EP0260435B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT87111611T ATE50612T1 (de) 1986-08-15 1987-08-11 Bauverbundplatte.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH3290/86A CH670671A5 (fr) 1986-08-15 1986-08-15
CH3290/86 1986-08-15

Publications (2)

Publication Number Publication Date
EP0260435A1 true EP0260435A1 (fr) 1988-03-23
EP0260435B1 EP0260435B1 (fr) 1990-02-28

Family

ID=4252786

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87111611A Expired - Lifetime EP0260435B1 (fr) 1986-08-15 1987-08-11 Panneau de construction composite

Country Status (8)

Country Link
EP (1) EP0260435B1 (fr)
AT (1) ATE50612T1 (fr)
AU (1) AU596683B2 (fr)
CH (1) CH670671A5 (fr)
DE (1) DE3761775D1 (fr)
ES (1) ES2013279B3 (fr)
NO (1) NO171647C (fr)
NZ (1) NZ221389A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004059098A1 (fr) * 2002-12-30 2004-07-15 Rozarijo Juric Panneaux muraux a montage rapide
WO2011154539A1 (fr) * 2010-06-11 2011-12-15 Module Home Future Bvba Système de construction
JP2017057555A (ja) * 2015-09-14 2017-03-23 大建工業株式会社 化粧目地付きパネル及びドア

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002081842A1 (fr) 2001-04-03 2002-10-17 James Hardie Research Pty Limited Article en fibrociment renforce et procedes de production et d'installation
US8281535B2 (en) 2002-07-16 2012-10-09 James Hardie Technology Limited Packaging prefinished fiber cement articles
EP1534511B1 (fr) 2002-07-16 2012-05-30 James Hardie Technology Limited Conditionnement d'articles prefinis en fibrociment
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
WO2007115379A1 (fr) 2006-04-12 2007-10-18 James Hardie International Finance B.V. Element de construction renforce a surface etanche
DE102014112987A1 (de) * 2014-09-09 2016-03-10 Holz Element Produktion Gmbh & Co. Kg Modulelement

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2816935A1 (de) * 1977-04-19 1978-11-02 Sture Lennart Samuelsson Modulblock und -system fuer den hausbau

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3305986A (en) * 1962-08-07 1967-02-28 Foam Products Corp Insulated enclosures and panels therefor
CA1124482A (fr) * 1978-06-28 1982-06-01 Cano Thermo Systems Inc. Panneaux de construction, et batiments faits desdits panneaux
DE3440297A1 (de) * 1984-11-05 1986-05-22 Greschbach, Manfred, 7637 Ettenheim Plattenfoermiges wandelement

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2816935A1 (de) * 1977-04-19 1978-11-02 Sture Lennart Samuelsson Modulblock und -system fuer den hausbau

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004059098A1 (fr) * 2002-12-30 2004-07-15 Rozarijo Juric Panneaux muraux a montage rapide
HRP20021035B1 (en) * 2002-12-30 2011-02-28 Jurić Rozarijo Wall panels for fast construction of structures
WO2011154539A1 (fr) * 2010-06-11 2011-12-15 Module Home Future Bvba Système de construction
JP2017057555A (ja) * 2015-09-14 2017-03-23 大建工業株式会社 化粧目地付きパネル及びドア

Also Published As

Publication number Publication date
EP0260435B1 (fr) 1990-02-28
ES2013279B3 (es) 1990-05-01
DE3761775D1 (de) 1990-04-05
NO873431L (no) 1988-02-16
AU7673487A (en) 1988-02-18
NZ221389A (en) 1991-12-23
NO171647B (no) 1993-01-04
ATE50612T1 (de) 1990-03-15
CH670671A5 (fr) 1989-06-30
AU596683B2 (en) 1990-05-10
NO873431D0 (no) 1987-08-14
NO171647C (no) 1993-04-14

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