WO2018209797A1 - 一种玻璃钢复合板 - Google Patents
一种玻璃钢复合板 Download PDFInfo
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- WO2018209797A1 WO2018209797A1 PCT/CN2017/093740 CN2017093740W WO2018209797A1 WO 2018209797 A1 WO2018209797 A1 WO 2018209797A1 CN 2017093740 W CN2017093740 W CN 2017093740W WO 2018209797 A1 WO2018209797 A1 WO 2018209797A1
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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
- 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
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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
- 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
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
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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
- B32B27/06—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
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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
- B32B27/12—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
- B32B27/42—Layered products comprising a layer of synthetic resin comprising condensation resins of aldehydes, e.g. with phenols, ureas or melamines
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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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
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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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/041—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
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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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/047—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material made of fibres or filaments
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L61/00—Compositions of condensation polymers of aldehydes or ketones; Compositions of derivatives of such polymers
- C08L61/04—Condensation polymers of aldehydes or ketones with phenols only
- C08L61/06—Condensation polymers of aldehydes or ketones with phenols only of aldehydes with phenols
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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
- 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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- 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
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
- B32B2307/3065—Flame resistant or retardant, fire resistant or retardant
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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
- B32B2307/536—Hardness
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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
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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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/554—Wear resistance
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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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/558—Impact strength, toughness
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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
- B32B2307/70—Other properties
- B32B2307/714—Inert, i.e. inert to chemical degradation, corrosion
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K3/00—Use of inorganic substances as compounding ingredients
- C08K3/16—Halogen-containing compounds
- C08K2003/166—Magnesium halide, e.g. magnesium chloride
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K3/00—Use of inorganic substances as compounding ingredients
- C08K3/18—Oxygen-containing compounds, e.g. metal carbonyls
- C08K3/24—Acids; Salts thereof
- C08K3/26—Carbonates; Bicarbonates
- C08K2003/265—Calcium, strontium or barium carbonate
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2201/00—Properties
- C08L2201/02—Flame or fire retardant/resistant
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2201/00—Properties
- C08L2201/08—Stabilised against heat, light or radiation or oxydation
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L2205/00—Polymer mixtures characterised by other features
- C08L2205/03—Polymer mixtures characterised by other features containing three or more polymers in a blend
Definitions
- the invention relates to the technical field of glass reinforced plastics, in particular to a glass steel composite board.
- the traditional composite board adopts metal materials. Because the offshore petroleum engineering platform, chemical enterprise, sewage treatment, and biogas tank have acidity and alkalinity, it is easy to corrode the composite board, and the glue is bonded between the flat plate and the legs, and the differentiation is long. Easy to stratify, short service life, and its corrosion resistance, wear resistance, high temperature resistance.
- a FRP composite panel comprising a FRP panel and a FRP bottom plate, wherein the lower end surface of the FRP panel is bonded to the fiberboard, the lower end of the fiberboard is provided with an aluminum-magnesium alloy sheet, and the fiberboard is A glass fiber reinforced mesh is disposed between the aluminum-magnesium alloy sheets, and a flame-retardant layer is disposed between the aluminum-magnesium alloy sheets and the glass reinforced plastic sheets.
- the flame retardant layer is made of an ammonium polyphosphate flame retardant layer.
- the fiberboard is a high density board.
- the FRP panel and the FRP bottom plate are completely identical, and the components thereof include 20-40 parts of phenolic resin, 10-20 parts of unsaturated polyester resin, 5-15 parts of ceramic powder, and 5-15 of silicon powder in parts by weight. Parts, polymer toughener 3-10 parts, expandable graphite 10-20 parts, light calcium carbonate 5-10 parts, cyclohexanone 5-15 parts, magnesium chloride 2-8 parts, cerium dioxide 2-8 parts.
- the preferred distribution ratio is: 30 parts of phenolic resin, 15 parts of unsaturated polyester resin, 10 parts of ceramic powder, 10 parts of silicon micropowder, 7 parts of polymer toughener, 15 parts of expandable graphite, and light calcium carbonate. 8 parts, 10 parts of cyclohexanone, 5 parts of magnesium chloride, and 5 parts of cerium oxide.
- the method for preparing the FRP panel comprises the following steps:
- the ceramic powder, silicon micropowder, expandable graphite, light calcium carbonate, magnesium chloride and cerium oxide are mixed and added to the pulverizer for pulverization.
- the pulverizer rotates at a speed of 500-1000 rpm, and the pulverization time is 10 min-20 min. Passing through a 100 mesh sieve to obtain a mixture A;
- step C the mixture obtained in step B is added to the preforming mold for preforming;
- the preform is placed in a molding heating mold, and continuously solidified by heating under the traction of the tractor to obtain a FRP panel.
- the invention has the advantages that the structural design of the invention is novel, the manufacturing cost is low, and the advantages of wear resistance, pressure resistance, high temperature resistance and high strength are obtained; the glass fiber reinforced plastic panel and the glass fiber reinforced plastic bottom plate used in the invention have the weight. Light weight, high strength, corrosion resistance, anti-aging, flame retardant, impact resistance, long service life.
- Figure 1 is a schematic view of the structure of the present invention.
- the present invention provides a technical solution: a FRP composite panel comprising a FRP panel 1 and a FRP bottom plate 2, the lower end surface of the FRP panel 1 is bonded to the fiberboard 3, and the lower end of the fiberboard 3 is provided with an aluminum-magnesium alloy sheet. 4, and a fiberglass reinforced mesh 5 is disposed between the fiberboard 3 and the aluminum-magnesium alloy plate 4, a flame-retardant layer 6 is disposed between the aluminum-magnesium alloy plate 4 and the FRP bottom plate 2; and the flame-retardant layer 6 is made of ammonium polyphosphate.
- Fiberboard 3 is made of high density board; glass steel panel 1 and glass steel floor 2 It is completely consistent, and its components include 20-40 parts of phenolic resin, 10-20 parts of unsaturated polyester resin, 5-15 parts of ceramic powder, 5-15 parts of silicon fine powder, and 3-10 parts of polymer toughener. 10-20 parts of expandable graphite, 5-10 parts of light calcium carbonate, 5-15 parts of cyclohexanone, 2-8 parts of magnesium chloride, and 2-8 parts of cerium oxide.
- Embodiment 1 is a diagrammatic representation of Embodiment 1:
- the FRP panel 1 and the FRP bottom plate 2 are completely identical, and the components thereof include 20 parts of phenolic resin, 10 parts of unsaturated polyester resin, 5 parts of ceramic powder, 5 parts of silicon micropowder, 3 parts of polymer toughener, and expandable by weight. 10 parts of graphite, 5 parts of light calcium carbonate, 5 parts of cyclohexanone, 2 parts of magnesium chloride, and 2 parts of cerium oxide.
- the method for preparing the FRP panel includes the following steps:
- the ceramic powder, silicon micropowder, expandable graphite, light calcium carbonate, magnesium chloride and cerium oxide are mixed and added to the pulverizer for pulverization.
- the pulverizer rotates at 500 rpm, the pulverization time is 10 min, and then passes through a 100 mesh sieve. , obtaining a mixture A;
- step C the mixture obtained in step B is added to the preforming mold for preforming;
- the preform is placed in a molding heating mold, and continuously solidified by heating under the traction of the tractor to obtain a FRP panel.
- Embodiment 2 is a diagrammatic representation of Embodiment 1:
- the FRP panel 1 and the FRP bottom plate 2 are completely identical, and the components thereof include 40 parts of phenolic resin, 20 parts of unsaturated polyester resin, 15 parts of ceramic powder, 15 parts of silicon micropowder, 10 parts of polymer toughener, and expandable by weight. 20 parts of graphite, 10 parts of light calcium carbonate, 15 parts of cyclohexanone, 8 parts of magnesium chloride, and 8 parts of cerium oxide.
- the method for preparing the FRP panel includes the following steps:
- A mixing ceramic powder, silicon micropowder, expandable graphite, light calcium carbonate, magnesium chloride, cerium oxide
- the pulverizer is added to the pulverizer, the pulverizer rotates at 1000 rpm, the pulverization time is 20 min, and then passes through a 100 mesh sieve to obtain a mixture A;
- step C the mixture obtained in step B is added to the preforming mold for preforming;
- the preform is placed in a molding heating mold, and continuously solidified by heating under the traction of the tractor to obtain a FRP panel.
- Embodiment 3 is a diagrammatic representation of Embodiment 3
- the FRP panel 1 and the FRP bottom plate 2 are completely identical, and the components thereof include 25 parts of phenolic resin, 12 parts of unsaturated polyester resin, 7 parts of ceramic powder, 7 parts of silicon powder, 4 parts of polymer toughener, and expandable by weight. 12 parts of graphite, 7 parts of light calcium carbonate, 7 parts of cyclohexanone, 3 parts of magnesium chloride, and 3 parts of cerium oxide.
- the method for preparing the FRP panel includes the following steps:
- the ceramic powder, silicon micropowder, expandable graphite, light calcium carbonate, magnesium chloride and cerium oxide are mixed and added to the pulverizer for pulverization.
- the pulverizer rotates at 550 rpm, the pulverization time is 12 min, and then passes through a 100 mesh sieve. , obtaining a mixture A;
- step C the mixture obtained in step B is added to the preforming mold for preforming;
- the preform is placed in a molding heating mold, and continuously solidified by heating under the traction of the tractor to obtain a FRP panel.
- Embodiment 4 is a diagrammatic representation of Embodiment 4:
- the FRP panel 1 and the FRP bottom plate 2 are completely identical, and the components thereof include phenolic trees in parts by weight. 35 parts of fat, 18 parts of unsaturated polyester resin, 13 parts of ceramic powder, 13 parts of silicon micropowder, 9 parts of polymer toughener, 18 parts of expandable graphite, 9 parts of light calcium carbonate, 14 parts of cyclohexanone, magnesium chloride 7 Parts, 7 parts of cerium oxide.
- the method for preparing the FRP panel includes the following steps:
- the ceramic powder, silicon micropowder, expandable graphite, light calcium carbonate, magnesium chloride and cerium oxide are mixed and added to the pulverizer for pulverization.
- the pulverizer rotates at 900 rpm, the pulverization time is 18 min, and then passes through a 100 mesh sieve. , obtaining a mixture A;
- step C the mixture obtained in step B is added to the preforming mold for preforming;
- the preform is placed in a molding heating mold, and continuously solidified by heating under the traction of the tractor to obtain a FRP panel.
- Embodiment 5 is a diagrammatic representation of Embodiment 5:
- the FRP panel 1 and the FRP bottom plate 2 are completely identical, and the components thereof include 32 parts of phenolic resin, 16 parts of unsaturated polyester resin, 12 parts of ceramic powder, 9 parts of silicon fine powder, 8 parts of polymer toughener, and expandable parts by weight. 16 parts of graphite, 7 parts of light calcium carbonate, 12 parts of cyclohexanone, 6 parts of magnesium chloride, and 6 parts of cerium oxide.
- the method for preparing the FRP panel includes the following steps:
- the ceramic powder, silicon micropowder, expandable graphite, light calcium carbonate, magnesium chloride and cerium oxide are mixed and added to the pulverizer for pulverization.
- the pulverizer rotates at 700 rpm, the pulverization time is 16 min, and then passes through a 100 mesh sieve. , obtaining a mixture A;
- step C the mixture obtained in step B is added to the preforming mold for preforming;
- the preform is placed in a molding heating mold, and continuously solidified by heating under the traction of the tractor to obtain a FRP panel.
- the FRP panel 1 and the FRP bottom plate 2 are completely identical, and the components thereof include 30 parts of phenolic resin, 15 parts of unsaturated polyester resin, 10 parts of ceramic powder, 10 parts of silicon micropowder, 7 parts of polymer toughener, and expandable parts by weight. 15 parts of graphite, 8 parts of light calcium carbonate, 10 parts of cyclohexanone, 5 parts of magnesium chloride, and 5 parts of cerium oxide.
- the method for preparing the FRP panel includes the following steps:
- the ceramic powder, silicon micropowder, expandable graphite, light calcium carbonate, magnesium chloride and cerium oxide are mixed and added to the pulverizer for pulverization.
- the pulverizer rotates at 750 rpm, the pulverization time is 15 min, and then passes through a 100 mesh sieve. , obtaining a mixture A;
- step C the mixture obtained in step B is added to the preforming mold for preforming;
- the preform is placed in a molding heating mold, and continuously solidified by heating under the traction of the tractor to obtain a FRP panel.
- the glass panel obtained by each embodiment of the present invention and the glass fiber reinforced plastic panel obtained by the conventional method were subjected to impact strength and bending strength tests, and the data were obtained as follows:
- Embodiment 2 292 548 Embodiment 3 288 552 Embodiment 4 287 542 Embodiment 5 287 550 Embodiment 6 297 559
- the invention has novel structural design, low manufacturing cost, and has the advantages of wear resistance, pressure resistance, high temperature resistance and high strength; the FRP panel and the FRP bottom plate used in the invention have the advantages of light weight, high strength, corrosion resistance, anti-aging, flame retardant, Anti-shock features and long service life.
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- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
一种玻璃钢复合板,包括玻璃钢面板(1)和玻璃钢底板(2),玻璃钢面板(1)下端面粘合纤维板(3),纤维板(3)下端设置铝镁合金板(4),且纤维板(3)与铝镁合金板(4)之间设置玻璃纤维加强网(5),铝镁合金板(4)与玻璃钢底板(2)之间设有阻燃层(6),该复合板结构设计新颖,制作成本低,具有耐磨、耐压、耐高温、强度高的优点。
Description
本发明涉及玻璃钢技术领域,具体为一种玻璃钢复合板。
传统的复合板采用金属材料,由于海洋石油工程平台、化工企业、污水处理、沼气池具有酸碱性,容易对复合板产生腐蚀性,且平板与支脚之间采用胶水粘合,日久分化,易分层,使用寿命短,而且其耐腐、耐磨、耐高温性能差。
发明内容
本发明的目的在于提供一种玻璃钢复合板,以解决上述背景技术中提出的问题。
为实现上述目的,本发明提供如下技术方案:一种玻璃钢复合板,包括玻璃钢面板和玻璃钢底板,所述玻璃钢面板下端面粘合纤维板,所述纤维板下端设置铝镁合金板,且所述纤维板与铝镁合金板之间设置玻璃纤维加强网,所述铝镁合金板与玻璃钢底板之间设有阻燃层。
优选的,所述阻燃层采用聚磷酸铵阻燃层。
优选的,所述纤维板采用高密度板。
优选的,所述玻璃钢面板和玻璃钢底板完全一致,其组分按重量份数包括酚醛树脂20-40份、不饱和聚酯树脂10-20份、陶瓷粉5-15份、硅微粉5-15份、高分子韧性剂3-10份、可膨胀石墨10-20份、轻质碳酸钙5-10份、环己酮5-15份、氯化镁2-8份、二氧化锑2-8份。
优选的,优选的成分配比为:酚醛树脂30份、不饱和聚酯树脂15份、陶瓷粉10份、硅微粉10份、高分子韧性剂7份、可膨胀石墨15份、轻质碳酸钙8份、环己酮10份、氯化镁5份、二氧化锑5份。
优选的,所述玻璃钢面板的制备方法包括以下步骤:
A、将陶瓷粉、硅微粉、可膨胀石墨、轻质碳酸钙、氯化镁、二氧化锑混合后加入粉碎机中粉碎,粉碎机转速为500-1000转/分,粉碎时间为10min-20min,之后过100目筛,得到混合物A;
B、在混合物中加入酚醛树脂、不饱和聚酯树脂、高分子韧性剂、环己酮,混合后加入混炼机中混炼,混炼温度为60℃-90℃,混炼时间为20min-40min,得到混合物B;
C、将步骤B得到的混合物加入预成型模中进行预成型;
D、将预成型物放入成型加热模具中,在牵引机的牵引下通过加热连续固化成型,得到玻璃钢面板。
与现有技术相比,本发明的有益效果是:本发明结构设计新颖,制作成本低,具有耐磨、耐压、耐高温、强度高的优点;本发明采用的玻璃钢面板和玻璃钢底板具有重量轻、强度高、耐腐蚀、抗老化、阻燃、抗冲击的特点,使用寿命长。
图1为本发明结构示意图。
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。
请参阅图1,本发明提供一种技术方案:一种玻璃钢复合板,包括玻璃钢面板1和玻璃钢底板2,所述玻璃钢面板1下端面粘合纤维板3,所述纤维板3下端设置铝镁合金板4,且所述纤维板3与铝镁合金板4之间设置玻璃纤维加强网5,所述铝镁合金板4与玻璃钢底板2之间设有阻燃层6;阻燃层6采用聚磷酸铵阻燃层;纤维板3采用高密度板;玻璃钢面板1和玻璃钢底板2
完全一致,其组分按重量份数包括酚醛树脂20-40份、不饱和聚酯树脂10-20份、陶瓷粉5-15份、硅微粉5-15份、高分子韧性剂3-10份、可膨胀石墨10-20份、轻质碳酸钙5-10份、环己酮5-15份、氯化镁2-8份、二氧化锑2-8份。
实施例一:
玻璃钢面板1和玻璃钢底板2完全一致,其组分按重量份数包括酚醛树脂20份、不饱和聚酯树脂10份、陶瓷粉5份、硅微粉5份、高分子韧性剂3份、可膨胀石墨10份、轻质碳酸钙5份、环己酮5份、氯化镁2份、二氧化锑2份。
本实施例中,玻璃钢面板的制备方法包括以下步骤:
A、将陶瓷粉、硅微粉、可膨胀石墨、轻质碳酸钙、氯化镁、二氧化锑混合后加入粉碎机中粉碎,粉碎机转速为500转/分,粉碎时间为10min,之后过100目筛,得到混合物A;
B、在混合物中加入酚醛树脂、不饱和聚酯树脂、高分子韧性剂、环己酮,混合后加入混炼机中混炼,混炼温度为60℃,混炼时间为20min,得到混合物B;
C、将步骤B得到的混合物加入预成型模中进行预成型;
D、将预成型物放入成型加热模具中,在牵引机的牵引下通过加热连续固化成型,得到玻璃钢面板。
实施例二:
玻璃钢面板1和玻璃钢底板2完全一致,其组分按重量份数包括酚醛树脂40份、不饱和聚酯树脂20份、陶瓷粉15份、硅微粉15份、高分子韧性剂10份、可膨胀石墨20份、轻质碳酸钙10份、环己酮15份、氯化镁8份、二氧化锑8份。
本实施例中,玻璃钢面板的制备方法包括以下步骤:
A、将陶瓷粉、硅微粉、可膨胀石墨、轻质碳酸钙、氯化镁、二氧化锑混
合后加入粉碎机中粉碎,粉碎机转速为1000转/分,粉碎时间为20min,之后过100目筛,得到混合物A;
B、在混合物中加入酚醛树脂、不饱和聚酯树脂、高分子韧性剂、环己酮,混合后加入混炼机中混炼,混炼温度为90℃,混炼时间为40min,得到混合物B;
C、将步骤B得到的混合物加入预成型模中进行预成型;
D、将预成型物放入成型加热模具中,在牵引机的牵引下通过加热连续固化成型,得到玻璃钢面板。
实施例三:
玻璃钢面板1和玻璃钢底板2完全一致,其组分按重量份数包括酚醛树脂25份、不饱和聚酯树脂12份、陶瓷粉7份、硅微粉7份、高分子韧性剂4份、可膨胀石墨12份、轻质碳酸钙7份、环己酮7份、氯化镁3份、二氧化锑3份。
本实施例中,玻璃钢面板的制备方法包括以下步骤:
A、将陶瓷粉、硅微粉、可膨胀石墨、轻质碳酸钙、氯化镁、二氧化锑混合后加入粉碎机中粉碎,粉碎机转速为550转/分,粉碎时间为12min,之后过100目筛,得到混合物A;
B、在混合物中加入酚醛树脂、不饱和聚酯树脂、高分子韧性剂、环己酮,混合后加入混炼机中混炼,混炼温度为70℃,混炼时间为25min,得到混合物B;
C、将步骤B得到的混合物加入预成型模中进行预成型;
D、将预成型物放入成型加热模具中,在牵引机的牵引下通过加热连续固化成型,得到玻璃钢面板。
实施例四:
玻璃钢面板1和玻璃钢底板2完全一致,其组分按重量份数包括酚醛树
脂35份、不饱和聚酯树脂18份、陶瓷粉13份、硅微粉13份、高分子韧性剂9份、可膨胀石墨18份、轻质碳酸钙9份、环己酮14份、氯化镁7份、二氧化锑7份。
本实施例中,玻璃钢面板的制备方法包括以下步骤:
A、将陶瓷粉、硅微粉、可膨胀石墨、轻质碳酸钙、氯化镁、二氧化锑混合后加入粉碎机中粉碎,粉碎机转速为900转/分,粉碎时间为18min,之后过100目筛,得到混合物A;
B、在混合物中加入酚醛树脂、不饱和聚酯树脂、高分子韧性剂、环己酮,混合后加入混炼机中混炼,混炼温度为80℃,混炼时间为35min,得到混合物B;
C、将步骤B得到的混合物加入预成型模中进行预成型;
D、将预成型物放入成型加热模具中,在牵引机的牵引下通过加热连续固化成型,得到玻璃钢面板。
实施例五:
玻璃钢面板1和玻璃钢底板2完全一致,其组分按重量份数包括酚醛树脂32份、不饱和聚酯树脂16份、陶瓷粉12份、硅微粉9份、高分子韧性剂8份、可膨胀石墨16份、轻质碳酸钙7份、环己酮12份、氯化镁6份、二氧化锑6份。
本实施例中,玻璃钢面板的制备方法包括以下步骤:
A、将陶瓷粉、硅微粉、可膨胀石墨、轻质碳酸钙、氯化镁、二氧化锑混合后加入粉碎机中粉碎,粉碎机转速为700转/分,粉碎时间为16min,之后过100目筛,得到混合物A;
B、在混合物中加入酚醛树脂、不饱和聚酯树脂、高分子韧性剂、环己酮,混合后加入混炼机中混炼,混炼温度为80℃,混炼时间为32min,得到混合物B;
C、将步骤B得到的混合物加入预成型模中进行预成型;
D、将预成型物放入成型加热模具中,在牵引机的牵引下通过加热连续固化成型,得到玻璃钢面板。
实施例六:
玻璃钢面板1和玻璃钢底板2完全一致,其组分按重量份数包括酚醛树脂30份、不饱和聚酯树脂15份、陶瓷粉10份、硅微粉10份、高分子韧性剂7份、可膨胀石墨15份、轻质碳酸钙8份、环己酮10份、氯化镁5份、二氧化锑5份。
本实施例中,玻璃钢面板的制备方法包括以下步骤:
A、将陶瓷粉、硅微粉、可膨胀石墨、轻质碳酸钙、氯化镁、二氧化锑混合后加入粉碎机中粉碎,粉碎机转速为750转/分,粉碎时间为15min,之后过100目筛,得到混合物A;
B、在混合物中加入酚醛树脂、不饱和聚酯树脂、高分子韧性剂、环己酮,混合后加入混炼机中混炼,混炼温度为75℃,混炼时间为30min,得到混合物B;
C、将步骤B得到的混合物加入预成型模中进行预成型;
D、将预成型物放入成型加热模具中,在牵引机的牵引下通过加热连续固化成型,得到玻璃钢面板。
实验例:
将本发明各实施例制得的玻璃面板与常规方法制得的玻璃钢面板进行冲击强度和弯曲强度试验,得到数据如下表:
冲击强度(KJ/m2) | 弯曲强度(Mpa) | |
常规方法 | 117 | 318 |
实施例一 | 290 | 545 |
实施例二 | 292 | 548 |
实施例三 | 288 | 552 |
实施例四 | 287 | 542 |
实施例五 | 287 | 550 |
实施例六 | 297 | 559 |
由以上表格数据可知,实施例六制得的玻璃钢面板达到最佳效果。
本发明结构设计新颖,制作成本低,具有耐磨、耐压、耐高温、强度高的优点;本发明采用的玻璃钢面板和玻璃钢底板具有重量轻、强度高、耐腐蚀、抗老化、阻燃、抗冲击的特点,使用寿命长。
尽管已经示出和描述了本发明的实施例,对于本领域的普通技术人员而言,可以理解在不脱离本发明的原理和精神的情况下可以对这些实施例进行多种变化、修改、替换和变型,本发明的范围由所附权利要求及其等同物限定。
Claims (6)
- 一种玻璃钢复合板,包括玻璃钢面板(1)和玻璃钢底板(2),其特征在于:所述玻璃钢面板(1)下端面粘合纤维板(3)所述纤维板(3)下端设置铝镁合金板(4),且所述纤维板(3)与铝镁合金板(4)之间设置玻璃纤维加强网(5),所述铝镁合金板(4)与玻璃钢底板(2)之间设有阻燃层(6)。
- 根据权利要求1所述的一种玻璃钢复合板,其特征在于:所述阻燃层(6)采用聚磷酸铵阻燃层。
- 根据权利要求1所述的一种玻璃钢复合板,其特征在于:所述纤维板(3)采用高密度板。
- 根据权利要求1所述的一种玻璃钢复合板,其特征在于:所述玻璃钢面板(1)和玻璃钢底板(2)完全一致,其组分按重量份数包括酚醛树脂20-40份、不饱和聚酯树脂10-20份、陶瓷粉5-15份、硅微粉5-15份、高分子韧性剂3-10份、可膨胀石墨10-20份、轻质碳酸钙5-10份、环己酮5-15份、氯化镁2-8份、二氧化锑2-8份。
- 根据权利要求4所述的一种玻璃钢复合板,其特征在于:优选的成分配比为:酚醛树脂30份、不饱和聚酯树脂15份、陶瓷粉10份、硅微粉10份、高分子韧性剂7份、可膨胀石墨15份、轻质碳酸钙8份、环己酮10份、氯化镁5份、二氧化锑5份。
- 根据权利要求1所述的一种玻璃钢复合板,其特征在于:所述玻璃钢面板的制备方法包括以下步骤:A、将陶瓷粉、硅微粉、可膨胀石墨、轻质碳酸钙、氯化镁、二氧化锑混合后加入粉碎机中粉碎,粉碎机转速为500-1000转/分,粉碎时间为10min-20min,之后过100目筛,得到混合物A;B、在混合物中加入酚醛树脂、不饱和聚酯树脂、高分子韧性剂、环己酮,混合后加入混炼机中混炼,混炼温度为60℃-90℃,混炼时间为20min-40min, 得到混合物B;C、将步骤B得到的混合物加入预成型模中进行预成型;D、将预成型物放入成型加热模具中,在牵引机的牵引下通过加热连续固化成型,得到玻璃钢面板。
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