DK142403B - Sandwich laminate with a core of blocks of foamed plastic. - Google Patents
Sandwich laminate with a core of blocks of foamed plastic. Download PDFInfo
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- DK142403B DK142403B DK304077AA DK304077A DK142403B DK 142403 B DK142403 B DK 142403B DK 304077A A DK304077A A DK 304077AA DK 304077 A DK304077 A DK 304077A DK 142403 B DK142403 B DK 142403B
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- Denmark
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- core material
- core
- sandwich
- adhesive
- Prior art date
Links
- 239000004033 plastic Substances 0.000 title description 20
- 229920003023 plastic Polymers 0.000 title description 20
- 239000011162 core material Substances 0.000 description 41
- 239000000853 adhesive Substances 0.000 description 19
- 230000001070 adhesive effect Effects 0.000 description 19
- 239000002344 surface layer Substances 0.000 description 16
- 238000010276 construction Methods 0.000 description 11
- 239000000463 material Substances 0.000 description 11
- 239000011449 brick Substances 0.000 description 10
- 239000006260 foam Substances 0.000 description 9
- 239000010410 layer Substances 0.000 description 7
- 239000000835 fiber Substances 0.000 description 6
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- 238000002347 injection Methods 0.000 description 4
- 239000007924 injection Substances 0.000 description 4
- 240000007182 Ochroma pyramidale Species 0.000 description 3
- 238000005187 foaming Methods 0.000 description 3
- 230000002787 reinforcement Effects 0.000 description 3
- 230000001413 cellular effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000123 paper Substances 0.000 description 2
- 239000002023 wood Substances 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 1
- 102000029797 Prion Human genes 0.000 description 1
- 108091000054 Prion Proteins 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
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- 238000005266 casting Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
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- 238000006073 displacement reaction Methods 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 239000011491 glass wool Substances 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000011824 nuclear material Substances 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 239000002985 plastic film Substances 0.000 description 1
- 239000002984 plastic foam Substances 0.000 description 1
- 239000011120 plywood Substances 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 238000003892 spreading Methods 0.000 description 1
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- 238000013022 venting Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/18—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by an internal layer formed of separate pieces of material which are juxtaposed side-by-side
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B27/065—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of foam
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B29/00—Layered products comprising a layer of paper or cardboard
- B32B29/002—Layered products comprising a layer of paper or cardboard as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B29/007—Layered products comprising a layer of paper or cardboard as the main or only constituent of a layer, which is next to another layer of the same or of a different material next to a foam layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/30—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer formed with recesses or projections, e.g. hollows, grooves, protuberances, ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B5/00—Hulls characterised by their construction of non-metallic material
- B63B5/24—Hulls characterised by their construction of non-metallic material made predominantly of plastics
-
- 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
- E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
- E04C2/10—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products
- E04C2/20—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products of plastics
- E04C2/205—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products of plastics of foamed plastics, or of plastics and foamed plastics, optionally reinforced
-
- 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
- E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
- E04C2/10—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products
- E04C2/24—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products laminated and composed of materials covered by two or more of groups E04C2/12, E04C2/16, E04C2/20
- E04C2/243—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products laminated and composed of materials covered by two or more of groups E04C2/12, E04C2/16, E04C2/20 one at least of the material being insulating
-
- 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
- E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
- E04C2/26—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups
- E04C2/284—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating
- E04C2/296—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating composed of insulating material and non-metallic or unspecified sheet-material
-
- 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
- E04C2/34—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 composed of two or more spaced sheet-like parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2250/00—Layers arrangement
- B32B2250/40—Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/08—Reinforcements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/554—Wear resistance
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Wood Science & Technology (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Laminated Bodies (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
(11) FREMLÆGGELSESSKRIFT 142403 DANMARK (51> ,nt C|3 B 32 B 3/18 UrtINIVIMnA B 29 D 9/00 §(21) Ansøgning nr. J040/77 (22) Indleveret den 6. jul. 1977 (24) Løbedag 6. Jul. 1977 (44) Ansøgningen fremlagt og fremlæggelsøsskriftet offentliggjort døn 27· Okt. 19^0(11) PUBLICATION MANUAL 142403 DENMARK (51>, nt C | 3 B 32 B 3/18 UrtINIVIMnA B 29 D 9/00 § (21) Application No J040 / 77 (22) Filed on 6 Jul 1977 (24) Race day Jul 6, 1977 (44) Application submitted and petition published on Dec. 27 · Oct. 19 ^ 0
DIREKTORATET FORDIRECTORATE OF
PATE N T- 0 G VA R E MÆ R K EVÆ S E N ET <3°) Prion,et be9»ret ,ra den (71) £0PENCRAFT λ/Sj "Christianehus”, Usserød Kongevej 161, 297Ο Hørsholm, DK.PATE N T- 0 G VA R E MARCH EVENTS <3 °) Prion, a right, be it (71) £ 0PENCRAFT λ / Sj "Christianehus", Usserød Kongevej 161, 297Ο Hørsholm, DK.
(72) Opfinder: Eric Tornow, Søparken 7» Nødebo, J480 Fredensborg, DK: Per Tornow, Vedbæk Strandvej 499, 2950 Klampenborg, DK.(72) Inventor: Eric Tornow, Søparken 7 »Nødebo, J480 Fredensborg, DK: Per Tornow, Vedbæk Strandvej 499, 2950 Klampenborg, DK.
(74) Fuldmægtig under sagens behandling:(74) Plenipotentiary in the proceedings:
Kontor for Industriel Eneret v. Svend Schønning.Office of Industrial Excellence v. Svend Schønning.
(54) Sandwichlaminat med en kerne af 1 blokke opdelt skumplastmateriale·(54) Sandwich laminate with a core of 1 blocks of foamed plastic material ·
Opfindelsen angår et sandwichlaminat med en kerne af i blokke opdelt skumplastmateriale indesluttet mellem overfladelag af hårdt, tryk-, træk- og slidstærkt materiale, idet der mellem overfladelag og skumplastkerne findes beskyttelseslag for skumplasten.BACKGROUND OF THE INVENTION 1. Field of the Invention This invention relates to a sandwich laminate having a core of foamed plastics material enclosed between surface layers of hard, pressure, tensile and abrasion-resistant material, protective foam layer layers being provided between the surface layers and the foam plastic core.
Sandwichkonstruktioner anvendes på en række konstruktionstekniske områder, f.eks. til fremstilling af skrog til mindre og større både, til skotter i sådanne, til fremstilling af beholdere, såvel lukkede som åbne, og i bilindustrien til fremstilling af lad og vognkasser, f.eks. til kølevogne, samt i det hele ta- 2 162403 get til alle sådanne formål, hvor materialets lethed, styrke, især den store bøjningsstyrke, og isolerende egenskaber er fordelagtige.Sandwich structures are used in a variety of structural engineering areas, e.g. for the manufacture of hulls for smaller and larger boats, for bulkheads in such, for the manufacture of containers, both closed and open, and in the automotive industry for the manufacture of barges and crates, e.g. for refrigerated vehicles, as well as for all such purposes where the lightness, strength, especially the high bending strength, and insulating properties are advantageous.
Der kendes således sandwichkonstruktioner, hvor kernematerialet består af balsaendetræ, dvs., at fiberretningen er i det væsentlige vinkelret på overfladelagene. Træet er udskåret i små flade klodser, der anbringes kant mod kant i konstruktionen, idet de midlertidigt kan være sammenholdt af pålimede tråde eller væv. Sammensætningen af kernen af sådanne små klodser muliggør fremstilling af mere eller mindre buede sandwichkonstruktioner .Thus, sandwich structures are known in which the core material consists of bale end wood, i.e., the fiber direction is substantially perpendicular to the surface layers. The wood is cut into small flat bricks that are placed edge to edge in the structure, being temporarily joined together by glued threads or tissues. The composition of the core of such small bricks allows the preparation of more or less curved sandwich structures.
Balsatræ er imidlertid forholdsvis kostbart, og tilgangen deraf begrænset, så der er behov for et billigere og mere lettilgængeligt kernemateriale. Som sådant har der været anvendt forskellige typer skumplast, hvor man efter opskumning af plasten i store blokke og efterfølgende hærdning skærer blokkene i skiver og eventuelt yderligere opdeler disse skiver i små klodser.However, balsa wood is relatively expensive, and its supply is limited, so that a cheaper and more easily accessible core material is needed. As such, different types of foam plastic have been used, where after foaming the plastic into large blocks and subsequent curing, the blocks are cut into slices and possibly further these slices are divided into small blocks.
Dette er imidlertid i flere henseender uhensigtsmæssigt.However, this is inappropriate in several respects.
Først og fremmest gælder dette trykstyrken, idet denne kan variere op til 50% hen over overfladen af en skive skåret af en større blok. Endvidere vil overfladen have talrige fordybninger fra gennemskårne celler, hvilket dels medfører en reduktion af trykstyrken, dels bevirker ekstra forbrug af bindemiddel ved materialets indbygning i sandwichkonstruktionen, idet alle disse fordybninger må fyldes med bindemiddel for at få en forsvarlig binding til overfladelagene.First of all, this applies to compressive strength as it can vary up to 50% over the surface of a disc cut by a larger block. Furthermore, the surface will have numerous recesses from cut cells, which will result in a reduction of the compressive strength and also cause additional consumption of binder when the material is incorporated into the sandwich structure, since all these recesses must be filled with binder in order to have a proper bond to the surface layers.
Fra svensk patentskrift nr 227.310 kendes anvendelsen af skumplast til flydelegemer til indbygning i både, og det angives, at man uden på celleplasten kan anbringe et lag af mod slag og mekanisk påvirkning modstandsdygtig plast; men at dette i nogle tilfælde kan medføre en kemisk reaktion, der ødelægger skumplasten. Ifølge patentet kan dette undgås ved, at et lag olieret papir anbringes mellem celleplasten og overfladelaget. Patentet giver således ingen anvisning på at anvende skumplast i et sandwichlaminat.Swedish Patent Specification No. 227,310 discloses the use of foam plastic for floating bodies for installation in boats, and it is stated that a layer of impact-resistant plastic and mechanical impact can be applied to the outside of the cellular plastic; but that in some cases this can cause a chemical reaction that destroys the foam. According to the patent, this can be avoided by placing a layer of oily paper between the cellular plastic and the surface layer. Thus, the patent does not give any instruction to use foam plastic in a sandwich laminate.
Opfindelsens formål er at afhjælpe ulemperne ved den hidtidige anvendelse af skumplast som kernemateriale i et sandwich-laminat, og dette opnås ved den i krav l's kendetegnende del angivne udformning af kernematerialet.The object of the invention is to overcome the disadvantages of the previous use of foam plastic as a core material in a sandwich laminate, and this is achieved by the design of the core material according to the characterizing part of claim 1.
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Det er yderst overraskende, at ingen tidligere har foreslået anvendelse af et sådant kernemateriale, i regelen kaldet integralskum, men at man i stedet har anvendt ved opskæring fremstillede klodser, der har de ovenfor omtalte ulemper.It is very surprising that no one has previously proposed the use of such a core material, usually called integral foam, but that bricks made of cutting have been used instead, which have the disadvantages mentioned above.
Integralskummet har således et opskummet indre omgivet af et hårdt og tæt overfladelag, og idet de små klodser, der indgår i kernematerialet,støbes og opskummes samtidig i et stort antal, men i hver sin form, kan man få klodser med et tæt og hårdt overfladelag på alle sider, dvs., at klodserne hver for sig udgør en art kassekonstruktion med god hjørne- og sidestivhed. Foruden at bidrage til, at sandwichkonstruktionen som helhed får større styrke, medfører de tætte og hårde overflader, at lokale trykpåvirkninger fordeles bedre over overfladen og ind i klodsen, så at konstruktionen ikke så let beskadiges» Endvidere medfører de tætte overflader et minimalt bindemiddelforbrug ved opbygningen af sandwichkonstruktionen. Endelig modvirker eller forhindrer de tætte overflader fugtansamling i klodserne, og selv om enkelte klodsers overflade skulle blive beskadiget, så fugt kan trænge ind, kan denne ikke brede sig til de ubeskadigede naboklodser.Thus, the integral foam has a foamed interior surrounded by a hard and dense surface layer, and the small bricks included in the core material are simultaneously molded and foamed in a large number, but in each shape, blocks with a dense and hard surface layer can be obtained. on all sides, ie the bricks individually constitute a type of box construction with good corner and side stiffness. In addition to contributing to the overall strength of the sandwich structure as a whole, the dense and hard surfaces result in a better distribution of local pressure over the surface and into the bricks so that the structure is not easily damaged »Furthermore, the dense surfaces result in minimal binder consumption during construction of the sandwich construction. Finally, the dense surfaces counteract or prevent moisture accumulation in the bricks, and although the surface of individual bricks should be damaged so that moisture can penetrate, it cannot spread to the undamaged neighboring bricks.
For at forenkle og lette fremstillingen har kernematerialeenhederne ifølge en hensigtsmæssig udførelsesform for opfindelsens genstand form som sekssidede parallelepipeder. De kan f.eks. have dimensionerne Jo x 3o x lo mm, hvor siderne er vinkelrette på hinanden.In order to simplify and facilitate the manufacture, the core material units according to a suitable embodiment of the object of the invention take the form of six-sided parallelepipeds. For example, they can have the dimensions Jo x 3o x lo mm, with the sides perpendicular to each other.
Ifølge en anden udførelsesform kan to modstående sider ifølge opfindelsen have form som parallellogrammer, hvorved det opnås, at den enkelte klods fungerer som en art skråstiver i sandwichkonstruktionen.According to another embodiment, two opposing sides of the invention can take the form of parallelograms, whereby it is obtained that the individual bricks act as a kind of oblique strut in the sandwich structure.
Det kan endvidere være hensigtsmæssigt, at kernemateriale-enhederne er armerede. Dette forøger i væsentlig grad styrken og stivheden, hvilket især har betydning ved sandwichkonstruktioner, hvor tykkelsen går op til 3o mm og derover, Sandwichkonstruktionens robusthed og styrke er nemlig ikke blot et spørgsmål om, at den kan modstå påvirkninger vinkelret på overfladen, men også om, at den kan modstå påvirkninger parallelt med overfladen, dvs., at kernematerialet er modstandsdygtigt mod sådanne påvirkninger.Furthermore, it may be convenient for the core material units to be reinforced. This significantly increases the strength and stiffness, which is especially important in sandwich designs where the thickness goes up to 3o mm and above, because the robustness and strength of the sandwich construction is not only a matter of being able to withstand the effects perpendicular to the surface, but also about that it can withstand stresses parallel to the surface, i.e., that the core material is resistant to such stresses.
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Armeringen kan eksempelvis udgøres af fibre, især glasfibre, der inkorporeres i plasten før opskumningen; men også andre former for armering, såsom papir, vævet stof eller plastfolie i ark eller strimmelform, kan indbygges, ved at den anbringes i formene, i hvilke opskumningen af plastmaterialet finder sted. Armeringen kan også fortsætte hen over skillevægge mellem formene og derved tjene til at sammenlåse et antal af enhederne til større flager.For example, the reinforcement may consist of fibers, especially glass fibers, which are incorporated into the plastic prior to foaming; but also other forms of reinforcement, such as paper, woven fabric or plastic sheet in sheet or strip form, can be incorporated by placing it in the molds in which the foaming of the plastic material takes place. The reinforcement can also continue across the partitions between the molds, thereby serving to interlock a number of the units into larger flakes.
Især med henblik på fremstillingen af større sandwichkonstruktioner vil det ofte være hensigtsmæssigt, at kernematerialeenhederne er således sammenlåst eller samlet til et pladelignende produkt på anden måde, f.eks. ved at være fastgjort til en plastfolie, et bærevæv eller bæretråde. En sådan fastgørelse kan let gennemføres i forbindelse med enhedernes fremstilling, og det vundne produkt er lethåndterligt og kan rulles sammen og transporteres til anvendelsesstedet, hvor man også kan indbygge det i så store plader eller flager, det er praktisk at gøre ad gangen. Sandwichkonstruktionerne opbygges nemlig oftest på stedet, idet man i en form først opbygger det ene overfladelag af plastmateriale forstærket med fibre eller væv, derefter klæber kernematerialelaget fast hertil I passende store stykker ad gangen og til sidst opbygger det andet overfladelag.In particular, for the purpose of making larger sandwich designs, it will often be appropriate that the core material units are thus interlocked or assembled into a plate-like product by other means, e.g. by being attached to a plastic wrap, carrier tissue or carrier wires. Such attachment can be easily carried out in connection with the manufacture of the units, and the product obtained is easily manageable and can be rolled up and transported to the place of application, where it can also be built into such large sheets or flakes as is convenient to do at a time. The sandwich structures are most often built on site, in which in one mold the first surface layer of plastic material is reinforced with fibers or tissue, then the core material layer adheres thereto in suitable large pieces at a time and finally the other surface layer builds up.
Det er af allerstørste betydning for sandwichkonstruktionens styrke, at der ikke ved fastklæbningen af kernematerialeenhederne, hvadenten dette sker ved anvendelse af et separat klæbemiddel eller simpelthen ved nedtrykning af enhederne i et overfladelag, før dette endnu er hærdet eller afbundet, indesluttes luft mellem enheder og overfladelag. Ved anvendelse af balsaklodser som kernemateriale er dette ikke så stort et problem, idet balsatræet i nogen grad er porøst, hvilket sammen med hårrørsvirkning i forhold til klæbemidlet bevirker, at luften forsvinder, og klæbemidlet trænger ind, så sådanne klodser næsten suger sig fast.It is of the utmost importance for the strength of the sandwich construction that, when adhering to the core material units, whether by using a separate adhesive or simply by depressing the units in a surface layer before it is even cured or unbound, air between units and surface layer is enclosed. . When using balsa blocks as a core material, this is not such a problem, as the balsa wood is somewhat porous, which, together with hair tube action relative to the adhesive, causes the air to dissipate and the adhesive penetrates so that such boulders almost suck.
Ved kernematerialeenheder som her omhandlet er der ikke de samme muligheder, og når det derfor drejer sig om at opnå størst mulig styrke, må der særlige foranstaltninger til for at undgå den omtalte indeslutning af luft. Ved en udførelsesform for opfindelsens genstand opnås dette ifølge opfindelsen ved, at der er udformet udluftningshuller tværs gennem laget af kernematerialeenheder.In the case of nuclear material units referred to here, the same options are not available and, therefore, when it comes to achieving the greatest possible strength, special measures must be taken to avoid the aforementioned containment of air. In one embodiment of the object of the invention, this is achieved according to the invention in that vent holes are formed across the layer of core material units.
5 1424035 142403
Man kan således ifølge opfindelsen udforme enhederne med et centralt gennemgående hul på tværs af enhedernes Største hegrænsningsflader.Thus, according to the invention, the units can be formed with a central through-hole across the largest edge boundary surfaces of the units.
Produktionsteknisk kan sådanne huller på kendt måde frembringes ved anvendelse af udtrækkelige kernestifter; men det gør støbeapparaturet temmelig kompliceret. Dette kan undgås, ved at man i stedet udformet hullerne ved kernematerialeenhedernes hjørner, idet enhederne ifølge opfindelsen er udført med af-fasede hjørner. Derved vil der dannes et gennemgående hul, hvor hjørnerne af fire i firkant liggende enheder støder sammen, hvadenten kun ét hjørne eller alle fire hjørner af enhederne er affasede. Om det gennemgående hul har cylindrisk eller kantet overflade, er uden betydning for funktionen som undslipningsvej for bag enhederne indespærret luft.Technically, such holes can be produced in known manner by the use of retractable core pins; but it makes the casting machine quite complicated. This can be avoided by forming the holes at the corners of the core material units instead, the units according to the invention being made with chamfered corners. This will create a through-hole, where the corners of four square units collide, whether only one corner or all four corners of the units are beveled. Whether the through-hole has a cylindrical or angular surface is irrelevant to the function of escape route for trapped air behind the units.
Udformningen af sådanne gennemgående huller gør det også muligt at fastgøre enhederne ved injektionsstøbning, idet man simpelthen injicerer klæbemiddel under tryk gennem nogle af hul- ' lerne. Det injicerede klæbemiddel jager da eventuelt indesluttet luft foran sig hen til andre huller eller spalter mellem enhederne, ud gennem hvilke luften kan undslippe. Også klæbemidlet vil kunne trænge ud de samme steder, så man får en kontrol på klæbningens udbredelse og kan afpasse injektionsstedernes antal og fordeling herefter.The design of such through holes also makes it possible to attach the units by injection molding, simply injecting adhesive under pressure through some of the holes. The injected adhesive then chases air trapped in front of it to other holes or gaps between the units through which the air can escape. Also, the adhesive will be able to penetrate the same places, so that the distribution of the adhesive is controlled and the number and distribution of the injection sites can be adjusted accordingly.
For at lette klæbemidlets udbredelse på tværs kan enhederne yderligere ifølge opfindelsen have rendeformede fordybninger enten i den ene eller i begge overflader med den største udstrækning. Man kan også ved at lægge to sådanne enheder sammen opnå en tykkere kerne med huller på langs og tværs gennem kernedelen, således at alle hulrum lettere udfyldes til opnåelse af stor styrke i konstruktionen. Eventuelt kan udfyldningen understøttes ved etablering af et vakuum.In order to facilitate the spreading of the adhesive transversely, the units may further have, according to the invention, gutter-shaped recesses either on one or both surfaces with the greatest extent. Also, by adding two such units together, a thicker core with holes longitudinally and transversely through the core portion can be obtained, so that all cavities are more easily filled to obtain great strength in the construction. Optionally, the filling may be supported by establishing a vacuum.
Hvis sandwichkonstruktionen skal være buet, som f.eks. i dele af et bådskrog, kan de enkelte kernematerialeenheders smalle sideflader ifølge opfindelsen være udformet som henholdsvis konvekse og konkave cylinderflader med samme krumningsradius. Derved opnås, at enhederne kan udlægges langs en buet flade, uden at der opstår kileformede spalter mellem naboenheder, idet en konveks sideflade passer ind og drejer i en konkav sideflade. Kernekonstruktionen kan således blive mere kompakt, og klæbemid-delforbruget mindre, fordi spalterne ikke udvides ved krumningen.If the sandwich structure is to be curved, such as. in parts of a boat hull, the narrow side faces of the individual core material units according to the invention may be formed as convex and concave cylinder faces, respectively, with the same radius of curvature. This results in the fact that the units can be laid along a curved surface without creating wedge-shaped gaps between neighboring units, with a convex side surface fitting and turning in a concave side surface. Thus, the core structure can become more compact and the adhesive consumption less because the gaps do not expand at the curvature.
6 1424036 142403
Hver enhed kan være udformet med to konvekse og to konkave sideflader, eller hveranden enhed kan have udelukkende konvekse sideflader og hveranden udelukkende konkave.Each unit may be formed with two convex and two concave side surfaces, or each other unit may have exclusively convex side surfaces and each other exclusively concave.
En udførelsesform for en sandwichkonstruktion ifølge opfindelsen illustreres af medfølgende tegning, hvor fig. 1 viser konstruktionen i tværsnit, fig. 2 nogle i konstruktionen indgående kernematerialeenheder fastgjort til et grovmasket væv, fig. 3 en kernematerialeenhed med to skrå sideflader, fig. 4 en kernematerialeenhed med to konvekse og to konkave sideflader, fig. 5 en speciel udformning af en kernematerialeenhed, og fig. 6 en buet sandwichkonstruktion.An embodiment of a sandwich construction according to the invention is illustrated by the accompanying drawing, in which fig. 1 shows the construction in cross section; FIG. 2 shows some core material assemblies included in the structure attached to a coarse mesh tissue; FIG. 3 shows a core material unit with two oblique side faces; FIG. 4 shows a core material unit with two convex and two concave side faces; FIG. 5 shows a special embodiment of a core material unit, and FIG. 6 a curved sandwich construction.
Som det fremgår af tegningen, består sandwichkonstruktionen af et kernemateriale sammensat af små, parallellepipediske enheder 5 og 6 af et opskummet plastmateriale, f.eks. polyurethan af den såkaldte integral-skin type, hvor den opskummede plast har en fasthæftende, hård og tæt overflade på alle sider. Fremstillingen af et plastskum af denne art hører til kendt teknik og skal derfor ikke beskrives her.As can be seen from the drawing, the sandwich construction consists of a core material composed of small, parallelepipedic units 5 and 6 of a foamed plastic material, e.g. polyurethane of the so-called integral-skin type, where the foamed plastic has an adhesive, hard and dense surface on all sides. The manufacture of a plastic foam of this kind is well known in the art and is therefore not to be described here.
Kernematerialeenhederne støder sammen kant mod kant i en pladelignende struktur og har på begge sider et overfladelag 7 og 8, der kan være ens eller forskelligt på de to sider.The core material units bump edge to edge in a sheet-like structure and have on both sides a surface layer 7 and 8 that may be the same or different on the two sides.
Overfladelagene kan være prefabrikerede plader af et hvilket snm helst egnet materiale, f.eks. metal, plast eller krydsfiner, der ved hjælp af et egnet bindemiddellag 9 er klæbet til kernematerialeenhederne.The surface layers may be prefabricated sheets of any suitable material, e.g. metal, plastic or plywood which is adhered to the core material units by means of a suitable binder layer 9.
Overfladelagene kan også være frembragt ved direkte sprøjtning af selvhærdende plastmateriale, der om ønsket kan være armeret med fibre lo, f.eks. glasuldsfibre, mod en formflade, og kernematerialeenhederne kan nedlægges i materialet, inden dette er afhærdet. Kernematerialeenhederne kan også være armerede, f.eks. fiberarmerede, som antydet i enheden 6.The surface layers may also be produced by direct spraying of self-curing plastics material which may, if desired, be reinforced with fibers 10, e.g. glass wool fibers, against a mold surface, and the core material units can be deposited in the material before cured. The core material units may also be reinforced, e.g. fiber reinforced, as indicated in the unit 6.
Sandwichkonstruktionens opbygning lettes i høj grad ved, at de små kernematerialeenheder 5 (eller 6) er fastgjort til et bæremateriale, f.eks. som vist i fig. 2 et grovmasket, vævet materiale 11. Derved kan et stort antal kernematerialeenheder bringes på plads på én gang, ligesom transport og opbevaring af enhederne lettes, idet vævet med de dertil fastgjorte enheder let kan rulles eller foldes sammen.The structure of the sandwich structure is greatly facilitated by the small core material units 5 (or 6) being attached to a carrier material, e.g. as shown in FIG. 2, a coarse mesh, woven material 11. In this way, a large number of core material units can be put in place at one time, and the transport and storage of the units is facilitated, since the tissue with the attached units can be easily rolled or folded.
7 1424037 142403
Fastgørelsen kan f.eks. ske ved klæbning af enhederne til vævet, og ved passende valg af klæbemidlet kan forbindelsen til vævet gøres midlertidig, dvs., at vævet er bestemt til afrivning, efter at kernematerialeenhedeme er permanent fastgjort til det ene af overfladelagene 7 og 8 i sandwichkonstruktionen, eller vævet kan indgå som et armeringselement i denne.The attachment can e.g. is made by adhering the units to the fabric, and by appropriate selection of the adhesive, the connection to the fabric can be made temporarily, i.e., the fabric is destined for tearing after the core material units are permanently attached to one of the surface layers 7 and 8 of the sandwich structure, or the fabric can be included as a reinforcing element in this.
Som vist i fig. 3 kan enhederne også udformes som parallel-lepipeder, der på den ene led ikke er retvinklede. Derved kan opnås en art skråstivereffekt i sandwichkonstruktionen, og at fugerne mellem de enkelte enheder ikke åbner sig så meget i krumme sandwichkonstruktioner, idet der i stedet sker en forskydning mellem naboenheder.As shown in FIG. 3, the units can also be designed as parallel lip pipes which are not at right angles on one link. Thereby, a kind of oblique stiffening effect can be obtained in the sandwich structure, and that the joints between the individual units do not open as much in curved sandwich structures, as a displacement between neighboring units takes place instead.
Som vist i fig. 4 kan en enhed også være udformet, så den ene af to modstående sideflader danner en konkav cylinderflade 12 og den anden en tilsvarende konveks cylinderflade 13, hvorved enhederne kan ligge tæt an mod hinanden også i buede konstruktioner. Det er styrkemæssigt fordelagtigt, idet sandwichkonstruktionen derved bliver mere kompakt, og samtidig spares der klæbemiddel, da spalterne mellem enhederne ikke åbner sig ved oplægning efter en buet flade.As shown in FIG. 4, a unit may also be formed so that one of two opposite side faces forms a concave cylinder surface 12 and the other a corresponding convex cylinder surface 13, whereby the units may be close to one another also in curved structures. This is advantageous in strength, as the sandwich structure thereby becomes more compact, and at the same time, adhesive is saved, as the gaps between the units do not open when laying on a curved surface.
En anden udformning af en enhed er vist i fig. 5. Her er hjørnerne 14 på enheden 5 affaset cylindrisk, således at, når fire enheder lægges sammen i firkant, dannes der et gennemgående hul.Another embodiment of a unit is shown in FIG. 5. Here, the corners 14 of the unit 5 are bevelled cylindrical so that when four units are folded in a square, a through hole is formed.
Fig. 5 illustrerer ligeledes, at der også kan være et centralt hul 15 tværs gennem enheden 5, og rendeformede fordybninger 16 fra hullet 15 ud til kanterne.FIG. 5 also illustrates that there may also be a central hole 15 transverse through the unit 5, and gutter-shaped recesses 16 from the hole 15 to the edges.
Sådanne enheder muliggør, at fastklæbning af enhederne kan ske ved injektion af klæbemidlet, f.eks. et klæbemiddel i form af eller baseret på en polyester eller en epoxyforbindelse. Klæbemidlet injiceres da gennem nogle af de tværsgående huller og driver luften på klæbestederne foran sig frem til og ud gennem andre huller, så der sikres intim forbindelse mellem kernematerialeenheder og overfladelag i sandwichkonstruktionen, hvorved der opnås optimal styrke af denne. Der kan også etableres et vakuum, der fremmer fjernelse af luftlommer bag kernematerialeenhederne under klæbemiddelinjiceringen.Such units allow the adhesion of the units to occur by injection of the adhesive, e.g. an adhesive in the form of or based on a polyester or epoxy compound. The adhesive is then injected through some of the transverse holes and drives the air at the adhesive points forward and out through other holes to ensure intimate connection between core material units and surface layers of the sandwich structure, thereby achieving optimum strength thereof. A vacuum may also be established to promote the removal of air pockets behind the core material units during adhesive injection.
8 1424038 142403
De tværgående rendeformede fordybninger 16 kan tjene til at lette klæbemiddelfordelingen, og til at understøtte sammenklæbningen, hvis der ønskes en tykkere kerne i sandwichkonstruktionen, ved at flere kernematerialeenheder placeres oven på hinanden.The transverse gutter-shaped recesses 16 can serve to facilitate the adhesive distribution and to support the adhesion, if a thicker core is desired in the sandwich structure, by placing several core material units on top of one another.
Når således to enheder lægges med fladerne med de rendeformede fordybninger 16 mod hinanden, fås en tykkere enhed med fordelingskanaler, der er parallelle med sandwichkonstruktionens længdeudstrækning og kan tjene til injicering af klæbemiddel.Thus, when two units are laid with the gutter-shaped recesses 16 facing each other, a thicker unit with distribution channels is obtained which is parallel to the length of the sandwich construction and can serve to inject adhesive.
Fig. 6 illustrerer opbygningen af en buet sandwichkonstruktion ved hjælp af kernematerialeenheder 5 (eller 6). Der er her anvendt enheder i form af rektangulære parallellepipeder med centralt udluftnings- eller injiceringshul 15, idet den buede udlægning skaber større luftmellemrum tinder og mellem enhederne, således at det er betydningsfuldt, at der er mulighed for udluftning, eventuelt understøttet med sugning (evakuering).FIG. 6 illustrates the structure of a curved sandwich structure by means of core material units 5 (or 6). Units are used here in the form of rectangular parallel pipes with central vent or injection hole 15, the curved layout creating larger air gap peaks and between the units, so that it is important that there is a possibility of venting, possibly supported by suction (evacuation). .
Priority Applications (15)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK304077AA DK142403B (en) | 1977-07-06 | 1977-07-06 | Sandwich laminate with a core of blocks of foamed plastic. |
GB7828293A GB2000725B (en) | 1977-07-06 | 1978-06-29 | Sandwich construction |
DE19782828734 DE2828734A1 (en) | 1977-07-06 | 1978-06-30 | LAYER STRUCTURE |
NZ187770A NZ187770A (en) | 1977-07-06 | 1978-07-03 | Laminate with core of integral skin foam blocks |
FI782158A FI782158A (en) | 1977-07-06 | 1978-07-04 | SANDWICH CONSTRUCTION |
NL7807253A NL7807253A (en) | 1977-07-06 | 1978-07-04 | SANDWICH CONSTRUCTION. |
FR7819861A FR2396647A1 (en) | 1977-07-06 | 1978-07-04 | LAMINATED PRODUCT |
CA000306788A CA1121258A (en) | 1977-07-06 | 1978-07-05 | Sandwich construction |
NO782348A NO782348L (en) | 1977-07-06 | 1978-07-05 | SANDWICH CONSTRUCTION. |
SE7807569A SE7807569L (en) | 1977-07-06 | 1978-07-05 | SANDWICK CONSTRUCTION |
CH735078A CH625465A5 (en) | 1977-07-06 | 1978-07-06 | |
JP8152878A JPS5433577A (en) | 1977-07-06 | 1978-07-06 | Sandwich structure |
IT25408/78A IT1097504B (en) | 1977-07-06 | 1978-07-06 | STRUCTURE IN SANDWICH |
AU37827/78A AU3782778A (en) | 1977-07-06 | 1978-07-06 | Laminated structure |
ES1978244599U ES244599Y (en) | 1977-07-06 | 1978-07-08 | WALLED STRUCTURE. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK304077 | 1977-07-06 | ||
DK304077AA DK142403B (en) | 1977-07-06 | 1977-07-06 | Sandwich laminate with a core of blocks of foamed plastic. |
Publications (3)
Publication Number | Publication Date |
---|---|
DK304077A DK304077A (en) | 1979-01-07 |
DK142403B true DK142403B (en) | 1980-10-27 |
DK142403C DK142403C (en) | 1981-03-30 |
Family
ID=8118410
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DK304077AA DK142403B (en) | 1977-07-06 | 1977-07-06 | Sandwich laminate with a core of blocks of foamed plastic. |
Country Status (15)
Country | Link |
---|---|
JP (1) | JPS5433577A (en) |
AU (1) | AU3782778A (en) |
CA (1) | CA1121258A (en) |
CH (1) | CH625465A5 (en) |
DE (1) | DE2828734A1 (en) |
DK (1) | DK142403B (en) |
ES (1) | ES244599Y (en) |
FI (1) | FI782158A (en) |
FR (1) | FR2396647A1 (en) |
GB (1) | GB2000725B (en) |
IT (1) | IT1097504B (en) |
NL (1) | NL7807253A (en) |
NO (1) | NO782348L (en) |
NZ (1) | NZ187770A (en) |
SE (1) | SE7807569L (en) |
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FR2509685A2 (en) * | 1976-08-17 | 1983-01-21 | Sodistra | Boat for navigating rivers - has hull bottom and side panels of cellular plastics material coated with stratified plastics |
EP0018328A3 (en) * | 1979-04-19 | 1980-11-26 | Procima S.A. | Prefabricated building element |
NO154220C (en) * | 1979-04-20 | 1986-08-20 | Sentralinst For Ind Forskning | WALL CONSTRUCTION AND PROCEDURE FOR ITS MANUFACTURING. |
FR2459956A1 (en) * | 1979-06-26 | 1981-01-16 | Cristiani Jacques | Ballistic screens partic. for bulletproof sheeting for car body mfr. - incorporates laminate of fibrous materials combined with metal sheet, light in wt. and thin |
JPS56133155A (en) * | 1979-11-28 | 1981-10-19 | Nat Res Dev | Thick board for reinforcing fitness |
GB2066731B (en) * | 1979-11-28 | 1983-12-07 | Nat Res Dev | Conformable reinforcement board |
SE435352B (en) * | 1983-05-04 | 1984-09-24 | Hydro Betong Ab | CONSTRUCTION BODY FOR A PREPARED CONSTRUCTION CONSISTING OF A NUMBER WITH OTHER COMBINED PLASTICS OF PLASTIC MATERIAL, OF EXV URETANCUM AND SET TO MAKE SAID BODY |
US4774118A (en) * | 1987-06-10 | 1988-09-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Cryogenic insulation system |
DE19624881A1 (en) * | 1995-06-29 | 1997-01-02 | Louise Dr Schlaaff | Wash-stand layered material |
DE10058982A1 (en) * | 2000-11-28 | 2002-05-29 | Basf Ag | Process for the production of composite elements |
DE10135213A1 (en) * | 2001-07-24 | 2003-02-06 | Basf Ag | composite elements |
GB2384461B (en) * | 2002-01-28 | 2005-03-16 | Intelligent Engineering | Improved structural sandwich plate members |
DE10213753A1 (en) * | 2002-03-26 | 2003-10-16 | Basf Ag | composite elements |
GB2387809A (en) * | 2002-04-23 | 2003-10-29 | Duncan Res And Dev Ltd | Multi-beam panel structures |
GB2389072B (en) * | 2002-05-29 | 2005-04-06 | Intelligent Engineering | Improved structural sandwich plate members |
DE10225338A1 (en) * | 2002-06-06 | 2003-12-18 | Basf Ag | Method for producing a compound element with two metal, plastic or wooden cover layers bracketing a plastic core layer involves introduction of the latter in liquid state in at least two steps |
EP1382764A1 (en) * | 2002-07-15 | 2004-01-21 | ASMUSSEN, Edgar | Load bearing, insulating airtight sandwich element for ceilings and roofs |
WO2005016642A1 (en) * | 2003-08-13 | 2005-02-24 | Bluescope Steel Limited | Foam core composite panel and method of manufacturing same |
ES2209669B1 (en) * | 2004-03-18 | 2005-10-01 | Jose Antonio Asumendi Garcia | CONSTRUCTION SYSTEM FROM PREFABRICATED PANELS AND PREFABRICATED PANEL USED. |
EP1736609B1 (en) * | 2004-03-18 | 2011-04-20 | ASUMENDI GARCIA, Jose Antonio | System for construction with pre-fabricated panels, and pre-fabricated panel |
WO2009105010A1 (en) * | 2008-02-22 | 2009-08-27 | Fagerdala Marine Systems Ab | A method for producing an improved hull |
DK2153982T3 (en) * | 2008-07-30 | 2011-09-05 | 3A Technology & Man Ag | Foamed plastic sheet |
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FR999527A (en) * | 1949-11-08 | 1952-02-01 | building element in the form of a panel, plank, and method for its manufacture | |
CH463063A (en) * | 1967-03-03 | 1968-09-30 | Pixner Siegfried Dr | Thermal insulation board for cold room insulation |
US3544417A (en) * | 1969-04-28 | 1970-12-01 | Unicor Inc | Cellular foam core assembly |
US3573144A (en) * | 1969-08-11 | 1971-03-30 | Ralph A Andersen | Sandwich panel type structural elements and method of making same |
DE1942795A1 (en) * | 1969-08-22 | 1971-03-04 | Dlw Ag | Continuous production of structural - building elements |
-
1977
- 1977-07-06 DK DK304077AA patent/DK142403B/en unknown
-
1978
- 1978-06-29 GB GB7828293A patent/GB2000725B/en not_active Expired
- 1978-06-30 DE DE19782828734 patent/DE2828734A1/en not_active Withdrawn
- 1978-07-03 NZ NZ187770A patent/NZ187770A/en unknown
- 1978-07-04 FI FI782158A patent/FI782158A/en not_active Application Discontinuation
- 1978-07-04 FR FR7819861A patent/FR2396647A1/en active Granted
- 1978-07-04 NL NL7807253A patent/NL7807253A/en not_active Application Discontinuation
- 1978-07-05 NO NO782348A patent/NO782348L/en unknown
- 1978-07-05 CA CA000306788A patent/CA1121258A/en not_active Expired
- 1978-07-05 SE SE7807569A patent/SE7807569L/en unknown
- 1978-07-06 CH CH735078A patent/CH625465A5/fr not_active IP Right Cessation
- 1978-07-06 AU AU37827/78A patent/AU3782778A/en active Pending
- 1978-07-06 JP JP8152878A patent/JPS5433577A/en active Pending
- 1978-07-06 IT IT25408/78A patent/IT1097504B/en active
- 1978-07-08 ES ES1978244599U patent/ES244599Y/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2828734A1 (en) | 1979-01-25 |
SE7807569L (en) | 1979-01-07 |
GB2000725B (en) | 1982-02-17 |
NL7807253A (en) | 1979-01-09 |
DK304077A (en) | 1979-01-07 |
IT7825408A0 (en) | 1978-07-06 |
DK142403C (en) | 1981-03-30 |
GB2000725A (en) | 1979-01-17 |
AU3782778A (en) | 1980-01-10 |
ES244599Y (en) | 1981-05-16 |
JPS5433577A (en) | 1979-03-12 |
CH625465A5 (en) | 1981-09-30 |
NO782348L (en) | 1979-01-09 |
FR2396647B1 (en) | 1983-05-20 |
NZ187770A (en) | 1981-11-19 |
ES244599U (en) | 1980-11-16 |
FI782158A (en) | 1979-01-07 |
CA1121258A (en) | 1982-04-06 |
IT1097504B (en) | 1985-08-31 |
FR2396647A1 (en) | 1979-02-02 |
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