CN107696645A - A kind of composite panel and casing - Google Patents
A kind of composite panel and casing Download PDFInfo
- Publication number
- CN107696645A CN107696645A CN201610642221.8A CN201610642221A CN107696645A CN 107696645 A CN107696645 A CN 107696645A CN 201610642221 A CN201610642221 A CN 201610642221A CN 107696645 A CN107696645 A CN 107696645A
- Authority
- CN
- China
- Prior art keywords
- composite
- composite panel
- fiber
- panel described
- fibre
- 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
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 208
- 239000000463 material Substances 0.000 claims abstract description 49
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 38
- 239000002184 metal Substances 0.000 claims abstract description 34
- 229910052751 metal Inorganic materials 0.000 claims abstract description 34
- 238000000034 method Methods 0.000 claims abstract description 24
- 230000008569 process Effects 0.000 claims abstract description 15
- 238000004519 manufacturing process Methods 0.000 claims abstract description 7
- 238000000576 coating method Methods 0.000 claims abstract description 5
- 238000001816 cooling Methods 0.000 claims abstract description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 5
- 239000011248 coating agent Substances 0.000 claims abstract description 3
- 239000000835 fiber Substances 0.000 claims description 40
- 230000002787 reinforcement Effects 0.000 claims description 31
- 239000004744 fabric Substances 0.000 claims description 19
- 229920005989 resin Polymers 0.000 claims description 16
- 239000011347 resin Substances 0.000 claims description 16
- 229910000831 Steel Inorganic materials 0.000 claims description 13
- 229920002635 polyurethane Polymers 0.000 claims description 13
- 239000004814 polyurethane Substances 0.000 claims description 13
- 239000010959 steel Substances 0.000 claims description 13
- 150000001875 compounds Chemical class 0.000 claims description 12
- 239000003822 epoxy resin Substances 0.000 claims description 12
- 229920000647 polyepoxide Polymers 0.000 claims description 12
- 239000003365 glass fiber Substances 0.000 claims description 11
- 125000001931 aliphatic group Chemical group 0.000 claims description 9
- 239000011159 matrix material Substances 0.000 claims description 9
- -1 polyethylene Polymers 0.000 claims description 8
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 claims description 7
- 125000003118 aryl group Chemical group 0.000 claims description 7
- 229920006387 Vinylite Polymers 0.000 claims description 6
- 239000010960 cold rolled steel Substances 0.000 claims description 6
- 238000009833 condensation Methods 0.000 claims description 6
- 230000005494 condensation Effects 0.000 claims description 6
- 238000000465 moulding Methods 0.000 claims description 5
- 229910000838 Al alloy Inorganic materials 0.000 claims description 4
- 230000007797 corrosion Effects 0.000 claims description 4
- 238000005260 corrosion Methods 0.000 claims description 4
- 229920003023 plastic Polymers 0.000 claims description 4
- 239000004033 plastic Substances 0.000 claims description 4
- 238000007711 solidification Methods 0.000 claims description 4
- 230000008023 solidification Effects 0.000 claims description 4
- 229920001169 thermoplastic Polymers 0.000 claims description 4
- 229920001187 thermosetting polymer Polymers 0.000 claims description 4
- 239000002023 wood Substances 0.000 claims description 4
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000000853 adhesive Substances 0.000 claims description 3
- 230000001070 adhesive effect Effects 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 238000005253 cladding Methods 0.000 claims description 3
- 235000013305 food Nutrition 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 210000003205 muscle Anatomy 0.000 claims description 3
- 229920005594 polymer fiber Polymers 0.000 claims description 3
- 230000035939 shock Effects 0.000 claims description 3
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 claims description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 2
- 239000004593 Epoxy Substances 0.000 claims description 2
- 229920000877 Melamine resin Polymers 0.000 claims description 2
- 229920000914 Metallic fiber Polymers 0.000 claims description 2
- 239000004677 Nylon Substances 0.000 claims description 2
- 239000004952 Polyamide Substances 0.000 claims description 2
- 239000004698 Polyethylene Substances 0.000 claims description 2
- 239000004372 Polyvinyl alcohol Substances 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 239000000805 composite resin Substances 0.000 claims description 2
- XLJMAIOERFSOGZ-UHFFFAOYSA-M cyanate Chemical compound [O-]C#N XLJMAIOERFSOGZ-UHFFFAOYSA-M 0.000 claims description 2
- 239000002657 fibrous material Substances 0.000 claims description 2
- JDSHMPZPIAZGSV-UHFFFAOYSA-N melamine Chemical compound NC1=NC(N)=NC(N)=N1 JDSHMPZPIAZGSV-UHFFFAOYSA-N 0.000 claims description 2
- 238000002156 mixing Methods 0.000 claims description 2
- 229920001778 nylon Polymers 0.000 claims description 2
- 239000003973 paint Substances 0.000 claims description 2
- 229920001568 phenolic resin Polymers 0.000 claims description 2
- 239000005011 phenolic resin Substances 0.000 claims description 2
- 229920002647 polyamide Polymers 0.000 claims description 2
- 229920001083 polybutene Polymers 0.000 claims description 2
- 229920000573 polyethylene Polymers 0.000 claims description 2
- 229920000139 polyethylene terephthalate Polymers 0.000 claims description 2
- 239000005020 polyethylene terephthalate Substances 0.000 claims description 2
- 229920006324 polyoxymethylene Polymers 0.000 claims description 2
- 229920002451 polyvinyl alcohol Polymers 0.000 claims description 2
- 229920000915 polyvinyl chloride Polymers 0.000 claims description 2
- 239000004800 polyvinyl chloride Substances 0.000 claims description 2
- 239000010453 quartz Substances 0.000 claims description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 2
- 239000010935 stainless steel Substances 0.000 claims description 2
- 229910001220 stainless steel Inorganic materials 0.000 claims description 2
- 229920006337 unsaturated polyester resin Polymers 0.000 claims description 2
- 229920001707 polybutylene terephthalate Polymers 0.000 claims 2
- 229920000642 polymer Polymers 0.000 claims 2
- FPYJFEHAWHCUMM-UHFFFAOYSA-N maleic anhydride Chemical compound O=C1OC(=O)C=C1 FPYJFEHAWHCUMM-UHFFFAOYSA-N 0.000 claims 1
- QQONPFPTGQHPMA-UHFFFAOYSA-N propylene Natural products CC=C QQONPFPTGQHPMA-UHFFFAOYSA-N 0.000 claims 1
- 125000004805 propylene group Chemical group [H]C([H])([H])C([H])([*:1])C([H])([H])[*:2] 0.000 claims 1
- 239000011435 rock Substances 0.000 claims 1
- 239000004416 thermosoftening plastic Substances 0.000 claims 1
- 239000007769 metal material Substances 0.000 abstract description 4
- 239000010410 layer Substances 0.000 description 22
- 239000011152 fibreglass Substances 0.000 description 10
- 229920000728 polyester Polymers 0.000 description 7
- 238000005246 galvanizing Methods 0.000 description 5
- 238000004080 punching Methods 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 101100334009 Caenorhabditis elegans rib-2 gene Proteins 0.000 description 3
- 150000002148 esters Chemical class 0.000 description 3
- 229920005749 polyurethane resin Polymers 0.000 description 3
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 238000005097 cold rolling Methods 0.000 description 2
- 229920001971 elastomer Polymers 0.000 description 2
- 230000002708 enhancing effect Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000007747 plating Methods 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 239000005060 rubber Substances 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229920002748 Basalt fiber Polymers 0.000 description 1
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- 239000004743 Polypropylene Substances 0.000 description 1
- 239000004433 Thermoplastic polyurethane Substances 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- QGZKDVFQNNGYKY-UHFFFAOYSA-N ammonia Natural products N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 1
- 150000008064 anhydrides Chemical class 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010924 continuous production Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 229920000620 organic polymer Polymers 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000009738 saturating Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- KUCOHFSKRZZVRO-UHFFFAOYSA-N terephthalaldehyde Chemical compound O=CC1=CC=C(C=O)C=C1 KUCOHFSKRZZVRO-UHFFFAOYSA-N 0.000 description 1
- 229920002803 thermoplastic polyurethane Polymers 0.000 description 1
- 239000004634 thermosetting polymer Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- 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
- B32B5/02—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 structural features of a fibrous or filamentary layer
-
- 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
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
-
- 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
- B32B1/00—Layered products having a non-planar shape
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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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- 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
- B32B27/08—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 synthetic resin
-
- 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
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
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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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/40—Layered products comprising a layer of synthetic resin comprising polyurethanes
-
- 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
- B32B3/02—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 features of form at particular places, e.g. in edge regions
- B32B3/06—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 features of form at particular places, e.g. in edge regions for securing layers together; for attaching the product to another member, e.g. to a support, or to another product, e.g. groove/tongue, interlocking
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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
- B32B3/02—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 features of form at particular places, e.g. in edge regions
- B32B3/08—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 features of form at particular places, e.g. in edge regions characterised by added members at particular 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
- 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
- B32B3/266—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 an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
-
- 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
- B32B3/28—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 comprising a deformed thin sheet, i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D15/00—Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, sections made of different materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D15/00—Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, sections made of different materials
- B65D15/24—Connections between walls
-
- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- 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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0276—Polyester fibres
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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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
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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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/554—Wear resistance
-
- 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
- B32B2307/70—Other properties
- B32B2307/712—Weather resistant
-
- 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
- B32B2307/70—Other properties
- B32B2307/714—Inert, i.e. inert to chemical degradation, corrosion
- B32B2307/7145—Rot proof, resistant to bacteria, mildew, mould, fungi
-
- 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
- B32B2419/00—Buildings or parts thereof
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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
- B32B2439/00—Containers; Receptacles
- B32B2439/02—Open containers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
The present invention discloses a kind of composite panel containing reinforcing rib structure and coating metal material and metal edge frame system and the casing being spliced by described composite panel and its application in container, water tank, cooling column body, one off houses etc.；Further, the invention further relates to a kind of pultrude process to manufacture the composite containing the skin-material different from inner layer composite material.
Description
Technical field
The present invention relates to a kind of containing reinforcing rib structure and the composite panel of metal edge frame system and matallic surface layer
With the casing being spliced by described composite panel and its in container, water tank, cooling column body, one off houses etc.
Using；Further, the invention further relates to a kind of pultrude process to manufacture containing the skin-material different from inner layer composite material
Composite.
Background technology
One casing can be prepared by various materials.Due to cost considerations, steel, aluminium alloy, plastic and glass
Sheet material made from fibre reinforced plastics and section bar are the main materials for manufacturing casing, but these materials have some to lack in itself
Point：Steel strength is high, modulus is big, is easy to weld, but density is too big, makes casing too heavy, while needs to make rust resistance and corrosion resistance
Surface treatment；Aluminium alloy equally exists oxidation and etching problem；Although plastics and in general fiberglass reinforced plastics density are small,
But the problem of intensity and toughness is small and weatherability is poor be present.
In order to solve the above problems, the invention provides a kind of composite panel, on the one hand, and its fiber content is high, because
This strength and stiffness is big；On the other hand, it can be as the pultrude process known to industrial quarters, prepreg molding or expressing technique
It is made, has along the pultrusion either arrangement of extrusion molding direction or shaft orientation reinforcing rib knot parallel to most of individual event fibers
Structure, there is the good rigidity of structure and can be with continuous production；Another further aspect, it can be compound laterally strong with increase on top layer
Degree, shock resistance, weather-proof, the not function such as contaminated food products, incrustation, anti-skidding, wear-resisting, corrosion-resistant material, to solve different casees
The individual demand of body application；Another aspect, described composite panel also have horizontal reinforcement and metal edge frame, had
The rigidity of structure is big, and weight is small, is easy to the characteristics of assembly.Thus, composite panel provided by the invention solves tradition well
The shortcomings that material, the casing of manufacture can be made to mitigate weight, reduce cost, improve performance, in some typical applications such as packaging
Case, water tank, one off houses, cooling column body etc. have very big economic value.Further, present invention also offers a kind of pultrusion work
Skill, this composite panel with functional surface material can be manufactured to on-line continuous, production can be substantially increased
Efficiency, reduce cost.
The content of the invention
In view of this, the first aspect of the present invention, it provides a kind of composite panel, it is characterized in that：1）It is described compound
Material contains by fibre reinforced materials as dispersed phase and matrix material as continuous phase；2）Matrix material accounts for all described compound
The volume ratio of material is less than 45% or weight ratio is less than 35%, it is preferred that matrix material accounts for the volume of all composites
Than less than 37% or weight ratio be less than 27%；3）The composite panel contains frame made of metal.
In the advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described multiple
Condensation material plate has corrugated cross sectional shape, it is preferred that cross sectional shape is sinusoidal waveform.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Composite panel has pultrude process or expressing technique to have axially the arrange and integrally formed composite of composite panel
Reinforcement.
Signified " axial direction " refers in the pultrude process either forming direction of expressing technique or parallel to exhausted in the present invention
The arragement direction of mostly unidirectional fiber, corresponding, " transverse direction " then refers to the direction vertical with " axial direction ".Institute of the present invention
" reinforcement " stated is to be projected on the part of composite panel, and it is combined as a whole with composite panel, it can by with it is compound
The same material of plate of material is made, and can also be made up of the material different from composite panel.
In the advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：The base
One or more kinds of combinations of the body material in thermoplastic polymer and thermosetting polymer.The thermoplastic polymer base
Body material is selected from polyvinyl chloride, polyethylene, polypropylene, nylon, polyethylene terephthalate, polyformaldehyde, poly- terephthaldehyde
Sour butanediol ester, polybutene, polyvinyl alcohol, thermoplastic polyurethane, polyamide；The thermoset polymer matrix material is selected from
Unsaturated polyester resin, vinylite, epoxy resin, melamine formal, phenolic resin, polyurethane, cyanate, Malaysia
Anhydride resin.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Fibre reinforced materials is selected from glass fibre, basalt fibre, boron fibre, quartz fibre, carbon fiber, polymer fiber, natural fibre
One or more kinds of combinations in dimension, metallic fiber.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The cross sectional shape of composite reinforcement is selected from：Complete or a part of circle, ellipse, annular, rectangle, side's annular,
Hexagon, six sides are annular, U-shaped, L-type, T types.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The distance between center line of composite reinforcement is 30 ~ 300mm, preferably 50 ~ 200mm, more preferably 50 ~
100mm。
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The bottom width of composite reinforcement is 2 ~ 50mm, preferably 2 ~ 20mm, more preferably 2 ~ 10mm.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The height of composite reinforcement is 2 ~ 300mm, preferably 5 ~ 100mm, more preferably 5 ~ 50mm.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Contain the composite reinforcement in composite board edge；
In another advantageous embodiment of the present invention, it has supplied a kind of composite panel, it is characterized in that：The reinforcement
Containing the structure being interlocked with the adjacent mutually isostructural composite board, the structure being interlocked includes but unlimited
In conventional structures of industrial quarters such as convex-concave groove, convex-concave platform fastenings.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Be combined in composite panel edge with reinforcement made of metal material, with reference to mode include but is not limited to it is tight with bolt
Gu, bonding etc. mode, preferably with using Self-locking bolt fasten, it is furthermore preferred that using bolt fasten combine bonding by the way of.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Composite is board-like also containing horizontal reinforcement, and the material that cross reinforcing is made be selected from metal or composite or
Their combination of person, it is preferred that cross reinforcing is made up of steel, it is furthermore preferred that cross reinforcing is the groove of galvanizing steel
Steel.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Horizontal reinforcement has the wave-like similar to the composite panel cross section.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：The transverse direction
Reinforcement is bolted with the shaft orientation reinforcing rib or the mode that coordinates jointly of bonding agent bonding or both is combined.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Composite board is combined into an entirety by fiber-reinforced resin prepreg tape and metal reinforcing or metal edge frame；It is preferred that
, the resin of the fiber-reinforced resin prepreg tape is selected from epoxy resin, aromatic urethane, aliphatic polyurethane；Fiber selects
The fabric being made into from glass fibre, carbon fiber or organic polymer fiber.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The thickness of composite panel is 1.2mm ~ 10mm, preferably 1.5 ~ 4mm, more preferably 1.7 ~ 3mm.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The width of composite panel is 50mm ~ 20000mm, preferably 100 ~ 10000mm, more preferably 200 ~ 8000mm.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described compound
The material different from inner layer composite material is contained on plate of material top layer, and provides one or more kinds of groups in following functions
Close：Increase transverse strength, shock resistance, weather-proof, not contaminated food products, incrustation, anti-skidding, wear-resisting, corrosion-resistant.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Composite panel is made up of pultrude process, prepreg molding or expressing technique.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The inner layer composite material of composite panel include but is not limited to aromatic urethane composite, epoxy resin-base composite material,
Unsaturated-resin based composites and vinylite composite；Skin-material includes but is not limited to aluminium alloy, steel, stainless
Steel, plastics, aliphatic polyurethane composite, food-grade unsaturated-resin matrix composite, vinylite base composite wood
Any one in material, paint coatings or combinations thereof.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The inner fiber material of composite panel is unidirectional continuous fiber, and surface fibre material is selected from fabric or fiber and fabric
Mixing.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：1）Institute
The skin-material for the composite stated contains the generally uniform sheet metal that distributed hole；2）The area in the hole accounts for sheet metal
Total face be more than 60%；Preferably, more than 80%；3）The thickness of the sheet metal is less than 3mm, it is preferred that less than 1.5mm, more
Preferably, less than 1mm.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
The shape in hole is one or more kinds of in circle, quadrangle, hexagon, pentagon, triangle on coating metal thin plate
Combination, it is preferred that the governor in the hole is less than 40mm.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described
Sheet metal is made up of cold-rolled steel sheet.
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：1）Institute
State metal sheet surface strengthens aliphatic polyurethane composite covered with one layer of fabric；Preferably, the fiber is to have
Machine polymer fiber；2）The fatty compound polyurethane material thickness is less than 1mm, it is preferred that less than 0.5mm.Preferably, it is described
Sheet metal, inner layer composite material plate and external fat adoption urethane composite layer by bath towel material mould pressing process integral into
Type；It is furthermore preferred that the sheet metal has the flange of non-perforate, to facilitate the connection between the composite panel.
Another aspect of the present invention, it provides a kind of pultrude process for preparing composite, it is characterized in that：The pultrusion
Technique comprises the steps of：1）Respectively with different resin impregnated inner fibers and surface fibre；2）Pultrusion die is by front and rear same
The pultrusion die 1 and pultrusion die 2 of axle arrangement are formed, will be solidified by pultrusion die 1 by the inner fiber that resin 1 is impregnated with or
It is partially cured；3）The surface fibre 2 being impregnated with by resin 2 cladding is had been cured or partially cured inner fiber；4）Will be solid
Change or the surface fibre on its surface of partially cured inner fiber and cladding is solidified into composite wood by pultrusion die 2 together
Material.Preferably, resin 1 is aromatic urethane, and resin 2 is aliphatic polyurethane.
In the advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that：It is described multiple
Condensation material plate is made up of foregoing pultrude process.
Another aspect of the present invention, it provides a kind of composite material casing, it is characterized in that：The composite material casing by
Foregoing composite panel is made up of the connection assembly between metal edge frame, it is preferable that the connected mode is selected from weldering
Connect, any one or combinations thereof in bolt connection, adhesive bonding.
In the advantageous embodiment of the present invention, it provides a kind of composite material casing, it is characterized in that：It is described
The column of composite material casing is made up of metal material；
In another advantageous embodiment of the present invention, it provides a kind of composite material casing, it is characterized in that：It is described multiple
The crossbeam of condensation material casing is made up of metal material；
In another advantageous embodiment of the present invention, it provides a kind of composite material casing, it is characterized in that：1）It is described
Composite Box body length is more than width and height；2）The composite material casing spliced by foregoing composite panel and
Into and composite panel shaft orientation reinforcing rib perpendicular to the length direction of described composite material casing, described cross reinforcing
Parallel to the length direction of described composite material casing.
Another aspect of the invention, it provides the application field of composite material casing, it is characterized in that：The composite
The application of casing including but not limited to aviation, sea-freight, railway, highway container, water tank, cooling column body, one off houses.
Brief description of the drawings
In order to further illustrate the composite panel and casing of the present invention, enter below in conjunction with the drawings and specific embodiments
Row describes in detail, wherein:
Fig. 1 is the top view and side view of the first preferred embodiment of the present invention;
Fig. 2 is the top view and side view of the second preferred embodiment of the present invention;
Fig. 3 is the top view and side view of the 3rd preferred embodiment of the present invention;
Fig. 4 is the top view and side view of the 4th preferred embodiment of the present invention;
Fig. 5 is the front view and profile of the 5th preferred embodiment of the present invention
Fig. 6 is the front view and profile of the 6th preferred embodiment of the present invention
Fig. 7 is front view, side view, top view and the profile of the 7th preferred embodiment of the present invention
Embodiment
Below with reference to multiple preferred embodiments of the composite panel and casing of the brief description of the drawings present invention.
（First preferred embodiment）:
Fig. 1 is the top view and side view of the first preferred embodiment of the present invention.Composite board 1 shown in figure is by poly- ammonia
Ester resin and alkali-free glass fibre yarn, alkali-free glass fibre tape edge felt, polyester anticorrosion cloth are made up of pultrude process, the tool of fiber
Body structure is followed successively by from the inner surface of plate to outer surface：（40g/m2）One layer of polyester anticorrosion cloth/（300g/m2）Alkali-free glass fibre
The direct yarn of tape edge felt one layer/4800tex alkali-free glass fibres/（300g/m2）One layer of alkali-free glass fibre tape edge felt/（40g/m2）
One layer of polyester anticorrosion cloth.Pultrude process uses two pultrusion dies of front and rear head and the tail series connection, is first soaked with aromatic polyurethane resins
Saturating alkali-free glass fibre yarn, it is impregnated with respectively up and down by first pultrusion die curing molding, then with aliphatic polyurethane resin
Two layers of alkali-free glass fibre tape edge felt and polyester anticorrosion cloth, and the tape edge felt that is saturated and anticorrosion cloth is coated on from first drawing
Solidify all composites as made from the direct yarn of alkali-free glass fibre and aromatic polyurethane resins pulled out in extruding mold
Plate upper and lower surface, then both finally pulled out second pultrusion mould simultaneously into curing molding in second pultrusion die
Tool, turns into composite board 1.The surfacing of the composite board 1 is that fabric enhancing aliphatic polyurethane is answered
Condensation material, have the advantages that weather-proof, wear-resisting, transverse strength is big, inner layer material is that unidirectional fibre enhancing aromatic urethane is compound
Material, there is the advantages of axial strength and modulus superelevation.The composite panel 1 is strengthened containing the shape axial direction different with height
Muscle 2,3,4, the wherein cross sectional shape of shaft orientation reinforcing rib 2 are diameter 10mm solid semicircle, and the section of shaft orientation reinforcing rib 3 is to contain right side
The solid L-shaped of boss, top width 20mm, high 40mm, the wide 5mm in bottom；The cross sectional shape of shaft orientation reinforcing rib 4 is to contain left groove
Solid L-shaped, top width 20mm, high 40mm, the wide 5mm in bottom；The boss on the right side of shaft orientation reinforcing rib 3 and the left side of shaft orientation reinforcing rib 4
Groove be just harmonious, close padlock when splicing two pieces of composite panels 1.Composite panel 1 shown in figure
Thickness be 2mm, width 300mm, length can be intercepted arbitrarily as needed, and the distance between shaft orientation reinforcing rib is 50mm；
In use, this composite panel 1 has very strong axial strength and rigidity, and densely arranged shaft orientation reinforcing rib 2
Composite panel 1 can be helped to resist external impact, and the reinforcement 3 and 4 of edge arrangement can both strengthen composite panel 1
Rigidity, the connection between polylith composite panel 1 can be provided again.Preferably, aliphatic can be laid on composite panel 1
The polyester anticorrosion cloth that polyurethane is impregnated with, the galvanizing punching cold-rolled steel sheet with the similar shape of composite 1 is then placed on polyester
In anticorrosion cloth, then lay a strata ester anticorrosion cloth again on punching cold-rolled steel sheet, finally pressed at an elevated temperature by rubber slab
The composite panel with metal surface is made in shaping, has it is furthermore preferred that the hole of the cold rolling punched-plate is the length of side less than 50mm
Hexagon, the distance on adjacent holes side is less than 10mm.
（Second preferred embodiment）:
Fig. 2 is the top view and side view of the second preferred embodiment of the present invention.It is preferable that second preferred embodiment employs first
Same pultrude process has manufactured composite panel 8 in embodiment.Composite panel 8 is waveform, inside and outside wave crest on
It is distributed with the reinforcement 2 with the second preferable case study on implementation identical axial direction, the spacing between shaft orientation reinforcing rib 2 is 100mm.It is compound
The height of the single ripple of plate of material 8 is 50mm, width 100mm；The thickness of composite panel 8 is 1.7mm, width 600mm.
There is the axial notch 19 of upward opening on the leftmost side ripple 9 of composite panel 8, have on the rightmost side ripple 10 of composite 8 downwards
Axial boss 18 can with leftmost side ripple 9 groove be fitted close.
（3rd preferred embodiment）:
Fig. 3 is the top view and side view of the 3rd preferred embodiment of the present invention.It is preferable that 3rd preferred embodiment employs first
Composite panel 1 in embodiment, and show and how to connect between the composite panel 1 in the first preferred embodiment.Spelling
Connect in technique, first epoxy resin fiberglass prepreg tape is laid in the groove in shaft orientation reinforcing rib 4, then in hot conditions
Under to shaft orientation reinforcing rib 3 and 4 apply clamping pressure make epoxy resin fiberglass prepreg tape solidification so that two panels composite
Plate 1 is combined into an entirety.
（4th preferred embodiment）:
Fig. 4 is the top view and side view of the 4th preferred embodiment of the present invention.It is preferable that 4th preferred embodiment employs second
Composite panel 8 in embodiment, and show and how to connect between the composite panel 8 in the second preferred embodiment.Connection
It is middle to lay epoxy resin fiberglass prepreg tape in the axial notch 19 on the leftmost side ripple 9 of composite panel 8, in high temperature bar
Pressure under being applied with part to the rightmost side ripple 10 of leftmost side ripple 9 on adjacent composite panel 8 makes the axle on the river ripple 10 of ripple 9
Closely fastened to boss 18 and axial notch 19, and high temperature make the solidification of epoxy resin fiberglass prepreg tape so as to by two pieces or
Person's polylith composite panel 8 is spliced into a piece of big plate.Preferably, fat can be laid on the big plate that composite panel 8 is spliced into
The polyester anticorrosion cloth that adoption urethane is impregnated with, then the galvanizing punching cold-rolled steel sheet with the similar shape of composite 8 is placed on poly-
In ester anticorrosion cloth, a strata ester anticorrosion cloth is then laid again on punching cold-rolled steel sheet, finally at an elevated temperature by rubber slab
Lower pressing formation be made with metal surface composite panel, it is furthermore preferred that the hole of the cold rolling punched-plate be the length of side have it is small
In 50mm hexagon, the distance on adjacent holes side is less than 10mm, it is furthermore preferred that the bore edges have a flange, and cold-reduced sheet
Edge has flange.
（5th preferred embodiment）:
Fig. 5 is the front view and profile of the 5th preferred embodiment of the present invention, and it is preferable that the 5th preferred embodiment employs first
Composite panel 1 in embodiment, and employ cross reinforcing 6 and pass through with the shaft orientation reinforcing rib 3,4 on composite panel 1
Adhesive is connected with lock 7 to be integrally formed.Cross reinforcing 6 is made up of Thermal zinc plating bath steel, sectional dimension 100mm*100mm*
The distance between 4mm, the center line of cross reinforcing 6 is 1200mm.Polylith composite panel 1 is connected into one by cross reinforcing 6
The big plate of block, while enhance the transverse strength and rigidity of composite panel 1.Widthwise edge is placed with the surrounding of composite panel 1
Frame 20 and axial frame 21.Horizontal frame 20 and axial frame 21 are 50mm*50mm*3mm galvanizing angle steel.In jigsaw
In technique, first epoxy resin fiberglass prepreg tape is laid on the frame that horizontal frame 20 and axial frame 21 be welded into, so
The big plate that composite panel 1 is spliced into afterwards is placed on epoxy resin fiberglass prepreg tape, to composite panel 1 and frame
20,21 apply pressure, while at high temperature solidify epoxy resin fiberglass prepreg tape, are made compound with metal edge frame
The big plate of material.
（6th preferred embodiment）:
Fig. 6 is the front view and profile of the 6th preferred embodiment of the present invention, and it is preferable that the 6th preferred embodiment employs second
Composite panel 8 in embodiment, having of laterally arranging and composite wood are distributed with the inner side and outer side of composite panel 8
The inside waveform reinforcement 15 and outer wave reinforcement 14 of the same waveform of flitch 8；Internal waveform reinforcement 15 and outer wave
Reinforcement 14 welds together respectively at inner transverse reinforcement 16 and outside cross reinforcing 13；Composite 8 is spliced
Big edges of boards edge be with inside casing and the He of outer layer transverse direction frame 22 that internal layer transverse direction frame 23 and internal layer axial direction frame 18 are welded
The housing that outer layer axial direction frame 17 is welded, and the both ends of inner transverse reinforcement 16 and outside cross reinforcing 13 are welded respectively
It is connected on inside casing and housing.In board-splicing process, epoxy resin fiberglass prepreg tape is laid in the interior appearance of composite panel 8
The position with cross reinforcing 14,15 and the combination of frame 17,18,22,23, internal outer rim and inside are needed on face and edge
Cross reinforcing 16 and outside cross reinforcing 13, which apply pressure heating simultaneously, makes the solidification of epoxy resin fiberglass prepreg tape, from
And it is made with the big plate of the composite of housing and cross reinforcing in metal.Internal waveform is strengthened in this preferably case study on implementation
Muscle 15 and outer wave reinforcement 14 and inner transverse reinforcement 16 and outside cross reinforcing 13 are that Thermal zinc plating bath steel is made,
Sectional dimension is 50mm*50mm*3mm；The size of inner transverse reinforcement 16 and outside cross reinforcing 13 is 50mm*
50mm*3mm；Internal waveform channel-section steel 15 and outer wave channel-section steel 14 and inner transverse reinforcement 16 and outside cross reinforcing 13
Between spacing be 1200mm;Internal layer transverse direction frame 23 and internal layer axial direction frame 18 and outer layer transverse direction frame 22 and outer layer axial direction
Frame 17 is galvanizing angle steel, and sectional dimension is 100mm*100mm*3mm.
（7th preferred embodiment）:
Fig. 7 is front view, side view and the sectional view of the 7th preferred embodiment of the present invention, how preferable using the 5th is illustrated
How the big plate of the composite with metal edge frame in case study on implementation and the 6th preferable case study on implementation is assembled into a casing.It is real
In the assembling process on border, it can both be spliced by way of welding metal frame and casing is made, bolt lock deposit can also be passed through
Casing is made in the mode for belonging to frame, it is preferred that bolt uses self-locking screw, it is further preferred that bolt coordinates adhesive to metal
Frame is attached.In a preferable case study on implementation, obtained casing uses obtained multiple in the 5th preferable case study on implementation
The big plate of condensation material is as bottom plate, using the obtained big plate of composite in the 6th preferable case study on implementation as side plate and top plate.
Although the board-like structure of composite and casing of the present invention are illustrated above in association with preferred embodiment,
It is those of ordinary skill in the art it should be appreciated that above-mentioned example is intended merely to explanation, and cannot function as to this
The limitation of invention.Therefore, modification can be carried out to the present invention in the spirit of claims.These modifications all will
Fall within the scope of required by claims of the present invention.
Claims (26)
1. a kind of composite panel, it is characterized in that：1) composite contains by fibre reinforced materials as dispersed phase and base
Body material is as continuous phase；2) described matrix material accounts for the volume ratio of all composites less than 45% or weight is than small
In 35%；3) composite panel contains metal edge frame.
2. the composite panel described in claim 1, it is characterized in that：The composite panel has corrugated cross sectional shape.
3. the composite panel described in claim 1, it is characterized in that：The composite panel has axially arrange and composite wood
The integrally formed composite reinforcement of flitch.
4. the composite panel described in claim 1-3, it is characterized in that：Described matrix material is selected from thermoplastic polymer and thermosetting
One or more kinds of combinations in property polymer.The polymer thermoplastic matrix material is selected from polyvinyl chloride, polyethylene, gathers
Propylene, nylon, polyethylene terephthalate, polyformaldehyde, polybutylene terephthalate (PBT), polybutene, polyvinyl alcohol, heat
Plastotype polyurethane, polyamide；The thermoset polymer matrix material is selected from unsaturated polyester resin, vinylite, epoxy
Resin, melamine formal, phenolic resin, polyurethane, cyanate, maleic anhydride resin.
5. the composite panel described in claim 1-4, it is characterized in that：The fibre reinforced materials is selected from glass fibre, the Black Warrior
It is one or more kinds of in rock fiber, boron fibre, quartz fibre, carbon fiber, polymer fiber, natural fiber, metallic fiber
Combination.
6. the composite panel described in claim 1-5, it is characterized in that：Between the center line of the composite reinforcement away from
From for 30-300mm.
7. the composite panel described in claim 1-6, it is characterized in that：The bottom width of the composite reinforcement be 2
In another advantageous embodiment of the present invention, it provides a kind of composite panel, it is characterized in that 2-50mm.
8. the composite panel described in claim 1-7, it is characterized in that：The height of the composite reinforcement is 2-300mm.
9. the composite panel described in claim 1-8, it is characterized in that：The composite is board-like also containing horizontal reinforcement
Muscle, and the material that cross reinforcing is made is selected from metal either composite or their combination.
10. the composite panel described in claim 9, it is characterized in that, the horizontal reinforcement has and the composite
The similar wave-like in plate cross section.
11. the composite panel described in claim 1-10, it is characterized in that：The composite board passes through fiber-reinforced resin
Prepreg tape is combined into an entirety with metal reinforcing or metal edge frame.
12. the composite panel described in claim 1-11, it is characterized in that：The thickness of the composite panel is 1.2mm-
10mm。
13. the composite panel described in claim 1-12, it is characterized in that：Contain compound with internal layer in the composite panel top layer
The different material of material, and one or more kinds of combinations in following functions are provided：Increase transverse strength, shock resistance, resistance to
Wait, not contaminated food products, incrustation, anti-skidding, wear-resisting, corrosion-resistant.
14. the composite panel described in claim 1-18, it is characterized in that：The composite panel is by pultrude process, prepreg
Molding or expressing technique are made.
15. the composite panel described in claim 13-14, it is characterized in that：The inner layer composite material bag of the composite panel
Aromatic urethane composite, epoxy resin-base composite material, unsaturated-resin based composites and vinylite is included to answer
Condensation material；Skin-material includes the unsaturated tree of aluminium alloy, steel, stainless steel, plastics, aliphatic polyurethane composite, food-grade
Any one in aliphatic radical composite material, vinylite based composites, paint coatings or combinations thereof.
16. the composite panel described in claim 13-15, it is characterized in that：The inner fiber material of the composite panel is
Unidirectional continuous fiber, surface fibre material are selected from the mixing of fabric or fiber and fabric.
17. the composite panel described in claim 13-16, it is characterized in that：1) skin-material of the composite described in contains
The generally uniform sheet metal that distributed hole；2) area in the hole accounts for total face of sheet metal more than 60%；3) metal
Gauge of sheet is less than 3mm.
18. the composite panel described in claim 13-17, it is characterized in that：The shape that the coating metal dominates hole is selected from
One or more kinds of combinations in circle, quadrangle, hexagon, pentagon, triangle.
19. the composite panel described in claim 13-18, it is characterized in that：The sheet metal is made up of cold-rolled steel sheet.
20. the composite panel described in claim 13-16, it is characterized in that：1) metal sheet surface is covered with one layer of fibre
Dimensional fabric strengthens aliphatic polyurethane composite；2) the fatty compound polyurethane material thickness is less than 1mm.
21. a kind of pultrude process for preparing composite, it is characterized in that：The pultrude process comprises the steps of：1) use respectively
Different resin impregnated inner fibers and surface fibre；2) pultrusion die is by the front and rear pultrusion die 1 and pultrusion mould coaxially arranged
Tool 2 is formed, and will be solidified by the inner fiber that resin 1 is impregnated with by pultrusion die 1 or partially cured；3) will be impregnated with by resin 2
The cladding of surface fibre 2 have been cured or partially cured inner fiber；4) by solidification or partially cured inner fiber
Composite is solidified into by pultrusion die 2 together with the surface fibre for being coated on its surface.
22. a kind of composite material casing, it is characterized in that：The composite material casing is as the composite described in claim 1-21
Plate assembly is made.
23. a kind of composite material casing, it is characterized in that：The side plate or top plate of the composite material casing are by claim 2-21
Described composite panel assembly is made.
24. the composite material casing described in claim 22-23, it is characterized in that：The composite material casing is by described compound
Any one or a variety of combinations of the metal edge frame of plate of material by the following method are attached：1) it is welded to each other；2) use
Bolt or self-locking screw connection；) spliced with bolt cooperation adhesive.
25. the composite material casing described in claim 22-24, it is characterized in that：1) the Composite Box body length is more than width
Degree and height；2) shaft orientation reinforcing rib of the composite panel is perpendicular to length direction, and described cross reinforcing is parallel to length
Spend direction.
26. the composite material casing described in claim 22-25, it is characterized in that：The application of the composite material casing includes：Boat
Sky, sea-freight, railway, highway container, water tank, cooling column body, one off houses.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610642221.8A CN107696645B (en) | 2016-08-08 | 2016-08-08 | Composite material plate and box body |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610642221.8A CN107696645B (en) | 2016-08-08 | 2016-08-08 | Composite material plate and box body |
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| CN107696645B CN107696645B (en) | 2022-07-26 |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108891098A (en) * | 2018-06-26 | 2018-11-27 | 苏州海马消防设备制造有限公司 | A kind of fire water box composite material and preparation method |
| CN110217463A (en) * | 2019-05-28 | 2019-09-10 | 武汉理工大学 | Composite material drawing and extruding section bar combined box and preparation method thereof |
| CN110744871A (en) * | 2019-11-12 | 2020-02-04 | 合肥山秀碳纤科技有限公司 | Firmly combined composite material plate |
| CN111216381A (en) * | 2020-01-19 | 2020-06-02 | 南京聚发新材料有限公司 | Fiber reinforced double-layer resin composite material, and extrusion molding device and process thereof |
| CN111805943A (en) * | 2020-07-16 | 2020-10-23 | 吉尔博建筑科技(上海)有限公司 | A new type of composite scaffolding rod and manufacturing process |
| CN113696577A (en) * | 2021-08-09 | 2021-11-26 | 安徽森泰木塑集团股份有限公司 | Continuous fiber reinforced plate, preparation method and mold |
| CN114770973A (en) * | 2022-03-15 | 2022-07-22 | 东华大学 | Bending and torsion-resistant composite molding method and production line for polygonal composite cylinder with long inner ribs |
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| CN108891098A (en) * | 2018-06-26 | 2018-11-27 | 苏州海马消防设备制造有限公司 | A kind of fire water box composite material and preparation method |
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| CN111216381A (en) * | 2020-01-19 | 2020-06-02 | 南京聚发新材料有限公司 | Fiber reinforced double-layer resin composite material, and extrusion molding device and process thereof |
| CN111805943A (en) * | 2020-07-16 | 2020-10-23 | 吉尔博建筑科技(上海)有限公司 | A new type of composite scaffolding rod and manufacturing process |
| CN113696577A (en) * | 2021-08-09 | 2021-11-26 | 安徽森泰木塑集团股份有限公司 | Continuous fiber reinforced plate, preparation method and mold |
| CN114770973A (en) * | 2022-03-15 | 2022-07-22 | 东华大学 | Bending and torsion-resistant composite molding method and production line for polygonal composite cylinder with long inner ribs |
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