WO2002009930A2 - Procede de fabrication d'un panneau composite - Google Patents

Procede de fabrication d'un panneau composite Download PDF

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Publication number
WO2002009930A2
WO2002009930A2 PCT/IB2001/001308 IB0101308W WO0209930A2 WO 2002009930 A2 WO2002009930 A2 WO 2002009930A2 IB 0101308 W IB0101308 W IB 0101308W WO 0209930 A2 WO0209930 A2 WO 0209930A2
Authority
WO
WIPO (PCT)
Prior art keywords
panel
thermosetting resin
composition
edging
mould
Prior art date
Application number
PCT/IB2001/001308
Other languages
English (en)
Other versions
WO2002009930A3 (fr
Inventor
Michael Windsor Symons
Original Assignee
Balmoral Technologies (Proprietary) Limited
Windsor Technologies Limited
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 Balmoral Technologies (Proprietary) Limited, Windsor Technologies Limited filed Critical Balmoral Technologies (Proprietary) Limited
Priority to AU2001276577A priority Critical patent/AU2001276577A1/en
Publication of WO2002009930A2 publication Critical patent/WO2002009930A2/fr
Publication of WO2002009930A3 publication Critical patent/WO2002009930A3/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/12—Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
    • B29C44/1228—Joining preformed parts by the expanding material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/12—Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
    • B29C44/18—Filling preformed cavities
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/003—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised by the matrix material, e.g. material composition or physical properties
    • B29C70/0035—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised by the matrix material, e.g. material composition or physical properties comprising two or more matrix materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/026—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers and with one or more layers of pure plastics material, e.g. foam layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/086—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core

Definitions

  • THIS invention relates to a method of making a composite panel from two substantially similar panel skins, and to the composite panel so made.
  • a method of making a composite panel from two substantially similar panel skins and an edging, each panel skin being made in a mould including the steps of: (1) forming a first panel skin by:
  • thermosetting resin a thermosetting resin
  • a catalyst for the thermosetting resin and inorganic filler particles to a surface of a first mould
  • thermosetting resin (b) allowing the thermosetting resin to set to form an outer face of the first panel skin; -9-
  • step (1)(b) forming a layer of a fibrous reinforcing material wetted with a second composition comprising a thermosetting resin and a catalyst for the thermosetting resin on the product of step (1)(b);
  • thermosetting resin in the second composition (3) allowing the thermosetting resin in the second composition to set to form a combination of the first panel skin with the edging attached thereto, and optionally removing the combination from the first mould;
  • thermosetting resin (b) allowing the thermosetting resin to set to form an outer face of the second panel skin
  • step (c) forming a layer of a fibrous reinforcing material wetted with the second composition on the product of step (4)(b); either
  • thermosetting resin in the second composition before the thermosetting resin in the second composition has set, placing an edging all around the edge of the product of step (4)(c);
  • thermosetting resin (6) allowing the thermosetting resin to set to form a combination of the second panel skin with the edging attached thereto, and removing the combination from the mould;
  • thermosetting resin in the second composition has set, placing the combination of step (3) on the product of step (4)(c) with the edging in contact with the product of step (4)(c);
  • thermosetting resin (9) allowing the thermosetting resin to set to form an intermediate panel from the second panel skin and the combination, the intermediate panel including a cavity defined by the first and second panel skins separated by the edging;
  • step (10) filling the cavity with a polyurethane foam to form the composite panel.
  • the method of the invention preferably includes the additional steps of: between steps (1)(b) and (1 )(c) and/or between steps (4)(b) and (4)(c), applying a layer of a third connecting composition comprising a thermosetting resin and a catalyst for the thermosetting resin to the product of step (1)(b) or the product of step (4)(b);
  • steps (6) and (7) removing any excess material from the two combinations so that the two combinations are of substantially similar size and of the desired thickness;
  • the edging or edgings do not include one or more holes therethrough, between steps (7) and (11) or between steps (10) and (1 1) forming one or more holes in the edging or edgings to allow access to the cavity in the intermediate panel;
  • step (1 1) applying a decorative coating and/or a sealant coating to one or both outer faces of the first and second panel skins of the composite panel.
  • Figure 1 is a plan view of a combination of a first panel skin with an edging attached thereto for use in a first aspect of the method of the invention
  • Figure 2 is a sectioned side view of the combination of Figure 1 , together with an identical combination
  • Figure 3 is a sectioned side view of a composite panel of the invention formed from the combinations of Figure 2
  • Figure 4 is a sectioned side view of a combination of a first panel skin with an edging attached thereto for use in a second aspect of the method of the invention
  • Figure 5 is a sectioned side view of the combination of Figure 4, together with a second panel skin
  • Figure 6 is a sectioned side view of a composite panel of the invention formed from the combination and second panel skin of Figure 5.
  • the crux of the invention is a method of making a composite panel from two substantially similar panel skins and an edging or edgings, wherein each panel skin is made in a mould.
  • Each mould is preferably made of a silicon rubber. Further, each mould preferably replicates the surface of a natural wood or other natural material, so that the composite panel made using the mould, replicates the appearance of the natural wood or other natural material.
  • the first step of the method of the invention is to form a first panel skin in a first mould by applying a layer of a first composition to a surface of the mould.
  • the first composition comprises a thermosetting resin, a catalyst for the thermosetting resin, and inorganic filler particles.
  • thermosetting resin in the first composition is preferably chosen from the group consisting of isophthalic or orthophthalic unsaturated polyester resins and phenol formaldehyde resole resins.
  • thermosetting resins in the first, second and third compositions do not need to be the same thermosetting resin.
  • phenol formaldehyde resole resin is J2018L by Borden Chemical Company, typically catalysed at between 6% to 10% with an acid catalyst such Phencat 10.
  • thermosetting resin is an unsaturated polyester resin
  • an orthophthalic unsaturated polyester resin is used for composite panels intended for interior use
  • an isophthalic unsaturated polyester resin preferably a neopentol glycol modified resin
  • examples of these resins are those manufactured by Scott Bader including Crystic 272. These resins are preferably pre-accelerated with accelerators such as a cobalt octoate or a naphthenate catalysed with an organic peroxide, such as methyl ethyl ketone peroxide.
  • the inorganic filler particles may be any suitable inorganic filler particles such as for example barium sulphate, or a combination of barium sulphate with calcium carbonate, the particles preferably having a particle size of from 10 to 20 micron inclusive.
  • the first composition preferably includes from 50% to 150% inclusive by mass of the thermosetting resin of the inorganic filler particles.
  • the first composition may also include a pigment so that the outer face of the composite panel is coloured.
  • the first composition is preferably applied to the mould by means of spraying or by means of brushing.
  • a uniform thickness layer is applied, at a thickness of from 100 to 1000 micron inclusive.
  • thermosetting resin After the first composition has been applied to the surface of the mould, the thermosetting resin is allowed to set to form an outer face of the first panel skin.
  • the next optional step of the method of the invention is to apply a layer of a third connecting composition comprising a thermosetting resin and a catalyst therefor, to the product of step (1 )(b).
  • thermosetting resin in the third composition may be any of those named above.
  • the next step of the method of the invention is to form a layer of a fibrous reinforcing material, wetted with a second composition comprising a thermosetting resin and a catalyst therefor, onto the product of step (1)(b) or the product of the optional step above.
  • the fibrous reinforcing material is preferably fibreglass, either in the form of chopped strand mat at weights of 300 kg/m 2 to 450 kg/m 2 or chopped strand applied by means of a chopper gun with a concurrent catalysed resin spray.
  • thermosetting resin with which the fibrous reinforcing material is wetted may be any of those named above. Where a build is required over a steep mould surface or indentation, to prevent resin slump and to provide adequate reinforcement and prevention of air bubbles, the thermosetting resin may be thickened with a suitable thickener such as micronised silica, e.g Aerosil by Degussa, added to the resin in an amount of from 15 to 60 g/600 g of resin.
  • a suitable thickener such as micronised silica, e.g Aerosil by Degussa
  • the layer of fibrous reinforcing material wetted with the thermosetting resin and catalyst therefor preferably has a thickness of from 0,2 mm to 2,5 mm inclusive.
  • the next step of the method of the invention is carried out before the thermosetting resins in the second composition and third composition (where present) have set, and involves placing an edging all around the edge of the product of step (1 )(c). It is important that the edging is placed in position before the setting of the thermosetting resins, in order to ensure intimate contact between the edging and the product of step (1)(c), and to ensure uniform thickness of the product of step (1)(c) below the edging.
  • the edging is preferably formed from a plurality of lengths of wood or other suitable lignocellulosic material.
  • the edging may also be a suitably profiled sheet metal edging.
  • the edging preferably has a width or thickness of from 24 mm to 100 mm inclusive. Where two edgings are used, the edgings preferably each have a width or thickness of from 12 mm to 50 mm inclusive. In other words the spacing between the first and second panel skins is preferably from 24 mm to 100 mm inclusive.
  • the edging When lengths of wood or other lignocellulosic material are used to form the edging, once the composite panel is complete, the edging is able to accommodate hinges, handles and other hardware, so that the composite panel may be used for the construction of a door or the like.
  • a suitable material for the construction of the edging is pine or the like.
  • the next step of the method of the invention is to allow the thermosetting resin to set to form a combination of the first panel skin with the edging attached thereto.
  • the combination may optionally be removed from the first mould.
  • the next step of the method of the invention is to form a second panel skin in a second mould which is substantially similar to the first mould.
  • the first mould may be used as the second mould, or two substantially similar moulds may be used as the first and second moulds.
  • the second panel skin is made in the same manner and from the same compositions as the first panel skin, i.e steps (1)(a) to (c) are repeated as steps (4)(a) to (c).
  • thermosetting resins in the second composition and third composition (where present) have set, an edging is placed all around the edge of the product of step (4)(c). Again it is important that the edging is placed in position before the setting of the thermosetting resins, in order to ensure intimate contact between the edging and the product of step (4)(c), and to ensure uniform thickness of the product of step (4)(c) below the edging.
  • the edging may be as described above.
  • the next step is to allow the thermosetting resin to set to form a combination of the second panel skin with the edging attached thereto. At this stage the combination is removed from the mould.
  • the next optional step of the method of the invention is to remove any excess material from the two combinations so that the two combinations are of substantially similar size and of the desired thickness. This may be achieved for example by passing each combination through a sander, so that the edgings, in combination with the panel skins, are dimensioned to their exact required thickness.
  • the surfaces of the edgings which are not adhesively secured to one another in formation of the composite panel, may be laminated with a material that simulates the appearance of the outer faces of the composite panel.
  • the next step of the method of the invention is to apply an adhesive composition to the edgings of the two combinations to join the edgings of the two combinations to each other to form an intermediate panel, including a cavity defined by the adhesively joined edgings.
  • the adhesive composition may comprise polyvinyl acetate or an acrylic dispersion in water, optionally containing up to 20% by mass of a water dispersible MDI, which is a urethane prepolymer, i.e. Duthane 1042 by Industrial Urethanes of South Africa.
  • a water dispersible MDI which is a urethane prepolymer, i.e. Duthane 1042 by Industrial Urethanes of South Africa.
  • This step is preferably carried out in a press to ensure good adhesion of the two combinations to each other.
  • the combination of step (3) may be placed on the product of step (4)(c), with the edging in contact with the product of step (4)(c). Again it is important that the edging is placed in position before the setting of the thermosetting resin, in order to ensure intimate contact between the edging and the product of step (4)(c), and to ensure uniform thickness of the product of step (4)(c) below the edging.
  • the next step of the method of the invention is to allow the thermosetting resin to set to form an intermediate panel from the second panel skin and the combination, the intermediate panel including a cavity defined by the first and second panel skins and the edging.
  • the next step of the method of the invention is to remove the intermediate panel from the second mould (and from the first mould, if necessary).
  • the edging or edgings do not include one or more holes therethrough, formed during manufacture of the edgings for example, then, between steps (7) and (11), or between steps (10) and (11) there is included the step of forming one or more holes in the edgings to allow access to the cavity in the intermediate panel.
  • holes may be drilled in one end of the intermediate panel through the edging, through which the polyurethane foam may be introduced, and holes may be drilled in the other end of the intermediate panel, to allow for the egress of air from the cavity.
  • the next step of the method of the invention is to fill the cavity with a polyurethane foam to form the composite product.
  • the polyurethane foam may be injected into the cavity through the hole or holes to fill the cavity at a density of from 25 kg/m 3 to 100 kg/m 3 inclusive.
  • the polyurethane foam may be any suitable polyurethane foam, such as for example 100 parts by mass of a fire retardant polyol, Duthane 0514, to 120 parts by mass of Duthane 5005, both by Industrial Urethanes of South Africa, to give an in situ foam mass with a density of 40 kg/m 3 .
  • the polyurethane foam serves the function of stiffening the composite panel. It adheres firmly to the two panel skins, it provides thermal insulation and maintains the two panel skins in parallel.
  • the step of filling the cavity of the intermediate panel with polyurethane foam is preferably carried out with the intermediate panel in a press to restrain both panel skins of the intermediate panel.
  • the composite panel may be trimmed to the size required.
  • the method of the invention also includes the optional step of applying to the outer faces of the composite panel a decorative coating, such as for example a pigment in an oil, the coating being applied by means of a spray gun or the like.
  • a decorative coating such as for example a pigment in an oil
  • this is applied as a wash coat which is worked into the surface of the outer faces. This is then allowed to dry, after which the oil binds the pigment to the surface of the outer faces.
  • sealant coating such as for example an acrylic or a polyurethane.
  • the advantages of the method of the invention are that two substantially identical panel skins are used to form a composite panel which results in the fact that any stresses in one panel skin are perfectly balanced by those in the other panel skin, thus providing the composite panel with strength and dimensional stability.
  • FIG. 1 to 3 there is shown two combinations 10, 12 each consisting of a panel skin comprising an outer face 14 formed from a first composition as described above and a layer 16 of a fibrous reinforcing material adhered to the outer face 14 as described above, and an edging 18 formed from lengths of pine.
  • the edgings 18 are adhered to each other with a suitable adhesive composition, to form an intermediate panel containing a cavity defined by the edgings 18. This cavity is then filled with a polyurethane foam 20 to form the composite panel of the invention.
  • first and second panel skins 40, 42 each consisting of an outer face 44 formed from a first composition as described above, and a layer 46 of a fibrous reinforcing material adhered to the outer face 44 as described above.
  • An edging 48 formed from length of pine is located between the two panel skins 40, 42.
  • the panel skin 40 is first made by the method described above, whereafter the edging 48 is attached thereto. Thereafter the second panel skin 42 is made by the method described above and the combination of the first panel skin 40 and edging 48 is then adhered thereto as described above. There is thus formed an intermediate panel containing a cavity defined by the first and second panel skins 40, 42 and the edging 48. This cavity is then filled with a polyurethane foam 50 to form the composite panel of the invention.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Physics & Mathematics (AREA)
  • Mathematical Physics (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

L'invention concerne un procédé de fabrication d'un panneau composite à partir de deux revêtements sensiblement similaires (40, 42) et d'une bordure (48). Le premier revêtement (40) est fabriqué dans un moule à partir d'une première composition renfermant une résine thermodurcissable, un catalyseur destiné à ladite résine thermodurcissable et des particules de charge inorganiques. Une couche de matière de renforcement fibreuse mouillée à l'aide d'une seconde composition renfermant la résine thermodurcissable et le catalyseur destiné à ladite résine est appliquée sur le premier revêtement. Avant que la résine thermodurcissable de la seconde composition ne durcisse, le rebord (48) est placé tout autour du bord du premier revêtement (40). La résine thermodurcissable de la seconde composition se durcit alors et forme une combinaison du premier revêtement (40) et du rebord (48) fixé au revêtement. Le second revêtement (42) est alors formé de la même manière que le premier revêtement (40) et, avant que la résine thermodurcissable de la seconde composition ne durcisse, la combinaison du premier revêtement (40) et du rebord (48) est placée sur le second revêtement (42) avec le rebord (48) en contact avec le second revêtement (42). La résine thermodurcissable se durcit et forme un panneau intermédiaire à partir du second revêtement (42) et de la combinaison. Le panneau intermédiaire renferme une cavité définie par le premier et le second revêtement (40, 42) séparés par le rebord (48), cette cavité étant remplie à l'aide d'une mousse de polyuréthanne (50) afin de former le panneau composite.
PCT/IB2001/001308 2000-07-31 2001-07-23 Procede de fabrication d'un panneau composite WO2002009930A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2001276577A AU2001276577A1 (en) 2000-07-31 2001-07-23 Method of making a composite panel

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
ZA2000/3864 2000-07-31
ZA200003864 2000-07-31
ZA2001/3061 2001-04-12
ZA200103061 2001-04-12

Publications (2)

Publication Number Publication Date
WO2002009930A2 true WO2002009930A2 (fr) 2002-02-07
WO2002009930A3 WO2002009930A3 (fr) 2002-05-02

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Application Number Title Priority Date Filing Date
PCT/IB2001/001308 WO2002009930A2 (fr) 2000-07-31 2001-07-23 Procede de fabrication d'un panneau composite

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AU (1) AU2001276577A1 (fr)
WO (1) WO2002009930A2 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004062893A1 (fr) * 2002-12-13 2004-07-29 Saint-Gobain Vetrotex France S.A. Procede et dispositif de fabrication d'une plaque composite
ES2238105A1 (es) * 2002-02-21 2005-08-16 Hermanos Llorente, S.L. Procedimiento de fabricacion de paneles tipo sandwich.
WO2011051085A1 (fr) * 2009-10-28 2011-05-05 Kraussmaffei Technologies Gmbh Élément sandwich isolé et dispositif pour fabriquer cet élément

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB877615A (en) * 1958-10-02 1961-09-20 Percy Henry Alcock Improvements in or relating to the production of laminated structures
US3573144A (en) * 1969-08-11 1971-03-30 Ralph A Andersen Sandwich panel type structural elements and method of making same
DE19814039A1 (de) * 1998-03-30 1999-10-07 Koegel Fahrzeugwerke Ag Sandwichelemente aus Kunststoff-Deckschichten und einem Kern zur Herstellung mobiler, temperaturgeführter Container

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB877615A (en) * 1958-10-02 1961-09-20 Percy Henry Alcock Improvements in or relating to the production of laminated structures
US3573144A (en) * 1969-08-11 1971-03-30 Ralph A Andersen Sandwich panel type structural elements and method of making same
DE19814039A1 (de) * 1998-03-30 1999-10-07 Koegel Fahrzeugwerke Ag Sandwichelemente aus Kunststoff-Deckschichten und einem Kern zur Herstellung mobiler, temperaturgeführter Container

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2238105A1 (es) * 2002-02-21 2005-08-16 Hermanos Llorente, S.L. Procedimiento de fabricacion de paneles tipo sandwich.
WO2004062893A1 (fr) * 2002-12-13 2004-07-29 Saint-Gobain Vetrotex France S.A. Procede et dispositif de fabrication d'une plaque composite
US7674495B2 (en) 2002-12-13 2010-03-09 Ocv Intellectual Capital, Llc Method and device for making a composite plate
WO2011051085A1 (fr) * 2009-10-28 2011-05-05 Kraussmaffei Technologies Gmbh Élément sandwich isolé et dispositif pour fabriquer cet élément

Also Published As

Publication number Publication date
WO2002009930A3 (fr) 2002-05-02
AU2001276577A1 (en) 2002-02-13

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