WO2014109021A1 - 繊維強化複合材料、その製造方法、それを用いたエレベータ用構成部材及びエレベータかご - Google Patents
繊維強化複合材料、その製造方法、それを用いたエレベータ用構成部材及びエレベータかご Download PDFInfo
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- WO2014109021A1 WO2014109021A1 PCT/JP2013/050232 JP2013050232W WO2014109021A1 WO 2014109021 A1 WO2014109021 A1 WO 2014109021A1 JP 2013050232 W JP2013050232 W JP 2013050232W WO 2014109021 A1 WO2014109021 A1 WO 2014109021A1
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- flame retardant
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- 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
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
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- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
- B29C43/12—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
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- B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
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- C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
- C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
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Definitions
- the present invention relates to a fiber-reinforced composite material, a manufacturing method thereof, an elevator component using the same, and an elevator car.
- Fiber reinforced composite materials are characterized by light weight and high strength.
- fiber reinforced composite materials in which glass fibers and resins are combined are used in many industrial fields such as helmets, skis, rackets, bathtubs, building materials, industrial electronic equipment materials, small ships, and automobiles.
- the fiber reinforced composite material using carbon fiber has higher strength and is expected to be used as an alternative material for weight reduction of metals such as iron and aluminum.
- Flame retardance is required when expanding the field of application of fiber reinforced composite materials and using them as consumer electronics, railway vehicle components or building materials.
- As flame retardant standards the United States UL (Underwriters Laboratories) “UL94 standard” for electrical products in general, “The flammability standard for railway vehicle materials”, also called the Japanese Ministry of Transportation combustion test method for railway vehicles, and building materials
- UL94 standard for electrical products in general
- UL94 standard for electrical products in general
- the flammability standard for railway vehicle materials also called the Japanese Ministry of Transportation combustion test method for railway vehicles, and building materials
- flame retardant standards stipulated in the Japanese Building Standards Act.
- the flame retardant standard set forth in the Japanese Building Standards Law is a highly flame retardant standard even in the world.
- the elevator car components are required to use flame retardant materials specified in the Japanese Building Standards Law.
- the car room and car frame are made of steel or aluminum alloy.
- such cars are heavy and require a large driving force. Cost. Therefore, lightweight elevator cars have been proposed that employ a sandwich panel structure with a fiber reinforced composite material as a skin material and a foam as a core material, or a hollow cross-section panel structure with a fiber reinforced composite material as a skin material and stringers. (For example, refer to Patent Document 1).
- Fiber reinforced composite materials used for consumer-related electrical products, railway vehicles, aircraft, building-related products including elevator cars, and the like are required to have high flame resistance in addition to being lightweight and high in strength.
- a fiber-reinforced composite material having high flame retardancy has not been obtained.
- a fiber reinforced composite material that meets the flame retardant standards as stipulated in the Japanese Building Standards Law has not been obtained.
- the present invention has been made to solve the above-described problems, and an object of the present invention is to provide a fiber-reinforced composite material having high flame retardancy, light weight and high strength, and a method for producing the same. .
- the present invention is a method for producing a fiber-reinforced composite material comprising impregnating a fiber structure with resin using a differential pressure between vacuum pressure and atmospheric pressure, and then curing the resin, comprising aluminum hydroxide and water
- a mixture of a powdered flame retardant containing at least one selected from magnesium oxide and having an average particle size in the range of 0.1 to 20 ⁇ m and a bromine-containing resin is used to form individual openings surrounded by fibers.
- the surface of the fiber structure is powdered It is a manufacturing method of the fiber reinforced composite material characterized by unevenly distributing a flame retardant.
- a fiber-reinforced composite material having high flame retardancy, light weight and high strength can be easily produced.
- Embodiment 1 FIG.
- a manufacturing apparatus for manufacturing a fiber reinforced composite material in which a powdered flame retardant is unevenly distributed on the surface of a fiber structure and a fiber reinforced composite material in which a powdered flame retardant is unevenly distributed on the surface of the fiber structure A method will be described.
- FIG. 1 is a cross-sectional view of a manufacturing apparatus for manufacturing the fiber-reinforced composite material according to the first embodiment.
- a manufacturing apparatus for manufacturing a fiber reinforced composite material includes a molding die 11 in which a fiber structure 10 such as a woven fabric, a nonwoven fabric, and a non-woven fabric molding is disposed, and a first resin diffusion sheet 12a.
- a sealing material 15 that shuts off the space from the outside, a vacuum pump 16 that evacuates the sealing film 14, and a resin tank 17 that supplies bromine-containing resin into the sealing film 14.
- the manufacturing apparatus is provided with a resin inlet 18 for injecting a bromine-containing resin supplied from the resin tank 17 into the sealing film 14. Further, the manufacturing apparatus is provided with an exhaust port 19 for exhausting the air in the sealing film 14. The exhaust port 19 also serves as an exhaust port for discharging excess bromine-containing resin in the sealing film 14. Note that the first resin diffusion sheet 12a and the first release sheet 13a installed on the mold 11 can be omitted. At this time, in order to prevent fixation of the bromine-containing resin, it is preferable to perform a mold release treatment on the mold 11.
- a fiber base material is prepared (step S1). Subsequently, the fiber base material is cut into a predetermined shape (step S2). Next, the first resin diffusion sheet 12a and the first release sheet 13a are sequentially stacked on the mold 11 (step S3). This step can be omitted. Subsequently, the cut fiber substrate is placed on the first mold release sheet 13a (the mold 11 that has been mold-released when the first resin diffusion sheet 12a and the first mold release sheet 13a are omitted). To form a fiber structure 10 (step S4). Next, the sealing material 15 is arrange
- step S6 the resin injection port 18 and the exhaust port 19 are installed (step S6).
- step S7 the surface of the fiber structure 10 is covered with the second release sheet 13b (step S7).
- step S8 the surface of the second release sheet 13b is covered with the second resin diffusion sheet 12b (step S8).
- the sealing film 14 is covered so as to cover the fiber structure 10, and the space in the sealing film 14 is blocked from the outside by the sealing material 15 (step S9).
- preparation for molding is completed (step S10).
- the vacuum pump 16 is driven to exhaust the air in the sealing film 14 (step S11).
- step S12 the bromine-containing resin and the powdered flame retardant are mixed, and the powdered flame retardant is dispersed in the bromine-containing resin.
- step S13 a mixture of the powdered flame retardant filled with the resin tank 17 and the bromine-containing resin is injected into the space in the sealing film 14 from the resin injection port 18 and impregnated into the fiber structure 10 (step S13).
- step S13 the mixture of the powdered flame retardant and the bromine-containing resin is filtered at the opening of the fiber base material, and the powdered flame retardant is unevenly distributed on the surface layer of the fiber structure 10.
- step S14 the bromine-containing resin injected into the sealing film 14 is cured
- a curing method room temperature curing or heat curing can be performed by selecting a type of bromine-containing resin and a catalyst.
- the bromine-containing resin is cured to such an extent that the mold 11 can be removed
- the second release sheet 13b is peeled off together with the second resin diffusion sheet 12b, and the fiber structure 10 is impregnated with the bromine-containing resin.
- the fiber reinforced composite material is removed from the mold 11 as a molded body (step S15).
- the removed molded body is subjected to a post-curing process using a drying furnace (step S16).
- a molded body made of the fiber reinforced composite material is completed (step S17).
- a fiber-reinforced composite material in which the powdered flame retardant 21 is unevenly distributed on the surface layer of the fiber structure 10 can be obtained as shown in FIG.
- step S13 the mixture of the powdered flame retardant 21 and the bromine-containing resin 22 injected from the resin tank spreads in the surface direction of the fiber structure 10 by the resin diffusion sheet as shown in FIG.
- the powdered flame retardant 21 is filtered through the opening of the fiber base material, so that it is difficult to impregnate the fiber structure 10 and is unevenly distributed on the surface layer of the fiber structure 10. To do.
- the position which shifted the opening part which exists in each layer (fiber base material) of the fiber structure 10 shifts
- the number of openings that penetrate the front and back is reduced.
- a part of the mixture of the powdered flame retardant 21 and the bromine-containing resin 22 passes through the openings of the fiber base and the layers of the fiber structure 10 during impregnation, and impregnates the entire fiber structure 10.
- the powdered flame retardant 21 exists only in the surface layer, the powdered flame retardant 21 exists only in the vicinity of the surface layer and in the opening in the vicinity of the surface layer.
- the concentration of the powdered flame retardant 21 in the vicinity of the surface layer and the opening in the vicinity of the surface layer is particularly high and the concentration of the powdered flame retardant 21 in the fiber structure 10 is low, the surface of the fiber structure 10 is directed from the surface to the inside.
- the case where the powdered flame retardant 21 is distributed in a gradient is included.
- the fiber reinforced composite material thus obtained shows extremely high flame retardancy because the powdered flame retardant 21 is densely present on the surface layer and the powdered flame retardant 21 also exhibits an effect of shielding heat.
- the state of uneven distribution of the powdered flame retardant 21 can be confirmed by microscopic observation of a cross section of the fiber reinforced composite material.
- Each layer (fiber substrate) of the fiber structure 10 has a mode of the size of individual openings surrounded by fibers in the range of 0.03 to 3 mm 2 and an opening ratio per 10 cm 2 area of 0. Must be in the range of 1-10%. If the mode value of the size of the opening is less than 0.03 mm 2 , the bromine-containing resin 22 is not sufficiently impregnated into the fiber structure 10. On the other hand, when the mode value of the size of the opening exceeds 3 mm 2 , the powdered flame retardant 21 cannot be unevenly distributed on the surface layer of the fiber structure 10. Further, when the opening ratio is less than 0.1%, the bromine-containing resin 22 is not sufficiently impregnated into the fiber structure 10.
- the fiber base material preferably has a mode of opening size in a range of 0.2 to 0.6 mm 2 and an opening ratio per 10 cm 2 area of 0.8 to 6.3%. is there.
- an opening part refers to the clearance gap part of the mesh
- the aperture ratio is a numerical value representing the ratio of the area occupied by the opening to the total area of one layer (one sheet) of the fiber base material.
- the gap between the warp yarns and weft yarns (glass fibers, etc.) knitted in the direction orthogonal to the fiber direction used to fix the fibers is opened.
- the measurement of the area of the opening and the calculation of the opening ratio are preferably carried out by measuring the area of the opening in the fiber substrate having a total area of 100 cm 2 per sheet.
- the mode value is a value that appears most frequently in the data group or probability distribution.
- organic fiber such as inorganic fibers, such as a carbon fiber, glass fiber, an alumina fiber, or an aramid fiber
- carbon fiber is preferable from the viewpoint of obtaining a lightweight and high-strength fiber-reinforced composite material.
- the fiber base material it is possible to use various crosses such as plain weave, twill weave, satin weave, or a unidirectional cross in which fibers arranged in one direction are bundled with other fibers into a sheet shape.
- the fiber volume content (Vf) indicating the ratio of the volume occupied by the fiber structure 10 in the total volume of the fiber-reinforced composite material is 25 to 85% by volume from the viewpoint of strength and flame retardancy. It is preferably 40 to 75% by volume.
- the proportion of the volume occupied by the fiber structure 10 is less than 25% by volume, the reinforcing effect by the fibers may not be sufficient, and the flame retardancy may not be sufficient.
- the volume ratio occupied by the fiber structure 10 exceeds 85% by volume, the effect of the bromine-containing resin 22 binding the fibers decreases, resulting in a decrease in strength and difficulty in molding.
- the powdery flame retardant 21 contains at least one selected from aluminum hydroxide and magnesium hydroxide and has an average particle size in the range of 0.1 to 20 ⁇ m.
- the average particle size of the powdered flame retardant 21 is less than 0.1 ⁇ m, the powdered flame retardant 21 cannot be unevenly distributed on the surface layer of the fiber structure 10 and sufficient flame retardancy cannot be obtained.
- the average particle diameter of the powdered flame retardant 21 exceeds 20 ⁇ m, the powdered flame retardant 21 causes clogging in the first release sheet 13a and the second release sheet 13b, which makes it difficult to mold.
- the average particle size of the powdered flame retardant 21 is preferably 0.5 to 10 ⁇ m.
- At least one selected from aluminum hydroxide and magnesium hydroxide as the powder flame retardant 21 is preferably added in an amount of 5 to 200 parts by weight with respect to 100 parts by weight of the bromine-containing resin 22. It is more preferable to add part.
- the powdery flame retardant 21 may further include at least one selected from antimony trioxide and zinc borate in addition to aluminum hydroxide and magnesium hydroxide. Further, at least one selected from antimony trioxide and zinc borate can be added in the range of 0 to 20 parts by weight with respect to 100 parts by weight of the bromine-containing resin 22.
- an additive type or reactive type flame retardant such as a phosphate ester type flame retardant or a phosphorus-nitrogen compound type may be used in combination.
- an average particle diameter represents the value of a particle diameter when the sum total of the volume ratio below a certain particle diameter will be 50% with respect to the total value of the volume ratio of the particle
- the bromine-containing resin 22 may be a thermosetting resin containing bromine.
- the brominated unsaturated polyester resin one obtained by introducing bromine in the production stage or one obtained by mixing brominated monomers can be used.
- the following four methods can be used as a method for introducing bromine in the production stage.
- the first method uses dibromoneopentyl glycol as the polyhydric alcohol component.
- the second method is a method using tetrabromophthalic acid and its anhydride as a saturated dibasic acid or its anhydride.
- an unsaturated polyester is produced using tetrahydrophthalic acid and its anhydride, endmethylenetetrahydrophthalic acid and its anhydride, etc. as a saturated dibasic acid or its anhydride, and then this saturated dibasic acid or its anhydride.
- bromine is added to the double bond of the basic acid component.
- the fourth method uses an unsaturated polyester using a dicyclopentadiene-maleic acid adduct having both the function of a saturated dibasic acid component and the function of an ⁇ , ⁇ -unsaturated dibasic acid component as a part of the raw material. Is then added to the residual double bond of dicyclopentadiene.
- the brominated epoxy acrylate resin can also be obtained by introducing bromine in the production stage or by mixing brominated monomers.
- Examples of the method of introducing bromine in the production stage include a method of using a bromine-containing epoxy type epoxy resin as the epoxy compound.
- Brominated epoxy acrylate resins include tetrabromobisphenol A-type epoxy (meth) acrylate, tetrabromobisphenol F-type epoxy (meth) acrylate, tetrabromobisphenol S-type epoxy (meth) acrylate, etc. from the viewpoint of excellent flexibility. preferable.
- the bromine content in the brominated unsaturated polyester resin or brominated epoxy acrylate resin is preferably 5 to 60% by weight, and more preferably 10 to 40% by weight. If the bromine content is less than 5% by weight, sufficient flame retardancy may not be obtained. On the other hand, if the bromine content exceeds 60% by weight, the toxicity during combustion may increase, and those having a bromine content exceeding 60% by weight are difficult to obtain.
- the thickness of the fiber reinforced composite material is selected based on strength design and economical reasons, but a thickness of about 100 ⁇ m to 3 cm is preferable, and a thickness of 0.5 mm to 1 cm is more preferable.
- a thickness of the fiber reinforced composite material is less than 100 ⁇ m, it may be difficult to obtain sufficient strength.
- the thickness of the fiber reinforced composite material exceeds 3 cm, the weight increases and the lightness required for the fiber reinforced composite material is impaired.
- the fiber which comprises the fiber structure 10 is carbon fiber, since carbon fiber is expensive, the fiber reinforced composite material which has thickness exceeding 3 cm is not preferable economically.
- a fiber-reinforced composite material having high flame retardancy can be manufactured by a simple process using an atmospheric pressure vacuum injection method using a relatively inexpensive material. Further, by simplifying the manufacturing equipment and the manufacturing process, the production cost can be reduced, the production time can be shortened, and the fiber-reinforced composite material can be mass-produced.
- Embodiment 2 instead of laminating the fiber base material cut into a predetermined shape in the first embodiment to form the fiber structure 10, the fiber structure 10 is prepared by winding continuous fibers around a mold. By impregnating a mixture of the powdered flame retardant 21 and the bromine-containing resin 22 from the surface direction of the fiber structure 10, a fiber-reinforced composite material in which the powdered flame retardant 21 is unevenly distributed on the surface layer of the fiber structure is manufactured.
- continuous fibers examples include inorganic fibers such as carbon fibers, glass fibers, and alumina fibers, or organic fibers such as aramid fibers. Among these, carbon fiber is preferable from the viewpoint of obtaining a lightweight and high-strength fiber-reinforced composite material.
- the fiber diameter of the continuous fiber is not particularly limited, but is preferably 1 ⁇ m to 20 ⁇ m.
- the same materials as those in the first embodiment can be used.
- the fiber volume content and thickness of the fiber reinforced composite material are the same as those in the first embodiment.
- Embodiment 3 a fiber-reinforced composite material panel (hereinafter referred to as a sandwich panel) in which a powdered flame retardant 21 is unevenly distributed on the surface of a structure formed by sandwiching both side surfaces of a core material made of foam with a fiber structure 10.
- a sandwich panel in which a powdered flame retardant 21 is unevenly distributed on the surface of a structure formed by sandwiching both side surfaces of a core material made of foam with a fiber structure 10.
- FIG. 5 is a sectional view of a manufacturing apparatus for manufacturing the sandwich panel according to the third embodiment.
- a manufacturing apparatus for manufacturing a sandwich panel has a mold 11 in which a fiber structure 10 and a foam 31 are sequentially laminated, a first resin diffusion sheet 12a, and resin permeability.
- the first release sheet 13a, the second release sheet 13b having resin permeability, the second resin diffusion sheet 12b, the sealing film 14, and the space in the sealing film 14 are blocked from the outside.
- a sealing material 15, a vacuum pump 16 that evacuates the inside of the sealing film 14, and a resin tank 17 that supplies a bromine-containing resin into the sealing film 14 are provided.
- the manufacturing apparatus is provided with a resin inlet 18 for introducing bromine-containing resin supplied from the resin tank 17 into the sealing film 14. Further, the manufacturing apparatus is provided with an exhaust port 19 for exhausting the inside of the sealing film 14. The exhaust port 19 also serves as an exhaust port for discharging excess bromine-containing resin in the sealing film 14. Note that the first resin diffusion sheet 12a and the first release sheet 13a installed on the mold 11 can be omitted. At this time, in order to prevent the bromine-containing resin from sticking, it is preferable to perform a mold release treatment on the mold 11.
- the fiber base material and the foam 31 are prepared (step S21). Subsequently, the fiber base material and the foam 31 are cut into a predetermined shape (step S22). Next, the first resin diffusion sheet 12a and the first release sheet 13a are sequentially laminated on the mold 11 (step S23). This step can be omitted. Subsequently, the cut fiber substrate is placed on the first mold release sheet 13a (the mold 11 that has been mold-released when the first resin diffusion sheet 12a and the first mold release sheet 13a are omitted).
- the fiber structure 10 is laminated to form a fiber structure 10, the foam 31 cut on the fiber structure 10 is disposed, and the fiber base material cut on the foam 31 is further laminated to form the fiber structure. 10 and the both surfaces of the foam 31 are sandwiched between the fiber structures 10 (step S24).
- the fiber structure 10 may be laminated only on one side of the foam 31.
- the sealing material 15 is arrange
- the resin injection port 18 and the exhaust port 19 are installed (step S26).
- the surface of the structure formed by sandwiching both surfaces of the foam 31 with the fiber structure 10 is covered with the second release sheet 13b (step S27).
- step S28 the surface of the second release sheet 13b is covered with the second resin diffusion sheet 12b (step S28).
- the sealing film 14 is covered so as to cover the structure formed by sandwiching the both surfaces of the foam 31 with the fiber structure 10, and the space in the sealing film 14 is shut off from the outside by the sealing material 15 (step). S29).
- the preparation for molding is completed (step S30).
- the vacuum pump 16 is driven to exhaust the air in the sealing film 14 (step S31).
- step S31 the powdered flame retardant 21 and the bromine-containing resin 22 are mixed, and the powdered flame retardant 21 is dispersed in the bromine-containing resin 22 (step S32).
- a mixture of the powdered flame retardant 21 and the bromine-containing resin 22 filled in the resin tank 17 is injected into the space in the sealing film 14 from the resin injection port 18 and impregnated in the fiber structure 10 (step S33). ).
- the mixture of the powdered flame retardant 21 and the bromine-containing resin 22 is filtered at the opening of the fiber base material, and the powdered flame retardant 21 is unevenly distributed on the surface layer of the fiber structure 10.
- the bromine-containing resin 22 injected into the sealing film 14 is cured (step S34).
- a curing method room temperature curing or heat curing is possible by selecting the type of bromine-containing resin 22 and a catalyst.
- step S35 the removed molded body is subjected to a post-curing process using a drying furnace. In this way, a molded body made of a sandwich panel is completed (step S37).
- the same structure as in the first and second embodiments can be used.
- the powder-form flame retardant 21 and the bromine containing resin 22 the thing similar to Embodiment 1 can be used.
- the foam 31 examples include rigid foams (foam materials) such as polyvinyl chloride resin, polyurethane resin, polystyrene resin, polyethylene resin, polypropylene resin, acrylic resin, phenol resin, polymethacrylimide resin, epoxy resin, and ethylene propylene rubber. Formed from.
- foam materials such as polyvinyl chloride resin, polyurethane resin, polystyrene resin, polyethylene resin, polypropylene resin, acrylic resin, phenol resin, polymethacrylimide resin, epoxy resin, and ethylene propylene rubber. Formed from.
- foam 31 an inorganic foam such as an aluminum foam or a syntactic foam can be used.
- the flame retardant foam obtained by mixing the above-described resin material with a flame retardant and foamed, and the phenol resin foam are preferable as the foam 31 because of excellent flame retardancy. Since the flame retardance is further improved by using a flame retardant foam as the foam 31, the obtained sandwich panel is suitable as a component for an elevator
- a foam 31 having a density in the range of 0.01 to 0.2 g / cm 3 it is preferable to use a foam 31 having a density in the range of 0.01 to 0.2 g / cm 3 .
- the density of the foam 31 is smaller than 0.01 g / cm 3 , the sandwich panel is likely to buckle.
- the density of the foam 31 is greater than 0.2 g / cm 3 , weight reduction of the sandwich panel may be hindered.
- the fiber volume content and thickness of the fiber reinforced composite material are the same as those in the first embodiment.
- a sandwich panel having high flame retardancy suitable for an elevator component is manufactured by a simple process using an atmospheric pressure vacuum injection method using a relatively inexpensive material. be able to.
- by simplifying the manufacturing equipment and the manufacturing process it is possible to reduce the production cost, shorten the production time, and mass-produce sandwich panels.
- Embodiment 4 FIG.
- carbon fiber is used as the fiber in Embodiment 1 or 2, and carbon fiber is impregnated from the surface direction of the carbon fiber structure by impregnating a mixture of powdered flame retardant 21 and bromine-containing resin 21.
- a carbon fiber reinforced composite material CFRP: Carbon Fiber Reinforced Plastics
- CFRP Carbon Fiber Reinforced Plastics
- the carbon fiber base material it is possible to use various carbon fiber cloths such as plain weave, twill weave, and satin weave, and unidirectional cloth in which carbon fibers arranged in one direction are bundled with other fibers to form a sheet.
- the fiber diameter of the continuous carbon fiber is not particularly limited, but is preferably 1 ⁇ m to 20 ⁇ m.
- the same materials as those in the first embodiment can be used.
- FIG. 7 shows an example of the result of the exothermic test for the carbon fiber reinforced composite material according to the fourth embodiment.
- FIG. 7A shows the heat generation rate
- FIG. 7B shows the total heat generation amount.
- 7 (a) and 7 (b) shows the result of the carbon fiber reinforced composite material obtained by impregnating a carbon fiber structure with a bromine-free resin
- (b) shows bromine.
- the result of the carbon fiber reinforced composite material obtained by impregnating the carbon-containing structure with the containing resin is shown.
- the result of the carbon fiber reinforced composite material (Embodiment 4) obtained by impregnating the carbon fiber structure with the resin mixture added with antimony trioxide was shown.
- the carbon fiber reinforced composite material according to Embodiment 4 can improve the flame retardancy as compared with the conventional material, and reaches the flame retardant material standard defined in the Japanese Building Standard Law. That is, in the carbon fiber reinforced composite material according to Embodiment 4, the carbon fiber that is a highly flame-retardant fiber becomes a heat-resistant heat blocking layer, the combustion of the resin is suppressed, and the flame-retardant effect is exhibited.
- the presence of at least one selected from aluminum hydroxide and magnesium hydroxide reduces the amount of resin and suppresses the amount of combustion, and also due to the endothermic action during thermal decomposition. An increase in temperature is also suppressed, and a fire extinguishing action by generated steam can be obtained.
- the endothermic action during pyrolysis of at least one selected from aluminum hydroxide and magnesium hydroxide can provide a synergistic effect that maintains the flame retardant effect of bromine for a long time. it can.
- at least one kind of inorganic substance selected from aluminum hydroxide and magnesium hydroxide remains in the gaps between the carbon fibers, so that the heat shielding effect can be further enhanced and high flame retardancy can be obtained. it can.
- continuous carbon fiber is used, the shape is maintained after combustion, and high strength can be achieved by fiber reinforcement.
- the fiber volume content and thickness of the carbon fiber reinforced composite material are the same as those in the first embodiment.
- the fourth embodiment it is possible to obtain a carbon fiber reinforced composite material having high flame retardancy and light weight and high strength at a low cost by a simple process.
- the carbon fiber reinforced composite material according to Embodiment 4 can be suitably used for a component for an elevator because it reaches the flame retardant material standard defined in the Japanese Building Standard Law.
- Embodiment 5 a carbon fiber reinforced composite material panel (hereinafter referred to as a sandwich panel) in which a powdered flame retardant is unevenly distributed on the surface of a structure formed by sandwiching both surfaces of a core material made of a foam between carbon fiber structures. Manufacturing.
- a sandwich panel can be manufactured by the method of sticking the carbon fiber reinforced composite material produced in the fourth embodiment to the core material with an adhesive, or by the integral molding of the third embodiment.
- FIG. 8 is a sectional view showing a sandwich panel according to the fifth embodiment.
- both side surfaces of the core material made of the foam 31 are joined to the carbon fiber reinforced composite material 52 by an adhesive 51.
- an adhesive 51 an epoxy adhesive, an acrylic adhesive, a silicone adhesive, a flame retardant adhesive, or the like can be used.
- the adhesive layer can be integrated with the carbon fiber reinforced composite material 52.
- the carbon fiber reinforced composite material 52 may be bonded only to one side of the foam 31.
- the same materials as those in the first embodiment can be used.
- the same one as in the third embodiment can be used.
- a carbon fiber base material and continuous carbon fiber the thing similar to Embodiment 4 can be used.
- the fiber volume content and thickness of the fiber reinforced composite material are the same as those in the first embodiment.
- the flame retardancy of the carbon fiber reinforced composite material of the fourth embodiment is improved in flame retardancy compared to the conventional material by the synergistic effect of the constituent materials. This is equivalent to the flame retardant material standards stipulated in the Japanese Building Standards Law.
- a sandwich panel having high flame retardancy and light weight and high rigidity and strength comparable to metal can be obtained at a low cost by a simple process.
- the sandwich panel according to the fifth embodiment has high rigidity and strength comparable to metal and meets the flame retardant material standards stipulated in the Japanese Building Standard Law, it is an elevator component, particularly an elevator car. Can be suitably used.
- Embodiment 6 an elevator car (a car room and a car frame) to which the carbon fiber reinforced composite material produced in the fourth embodiment is applied will be described.
- an elevator car in which the above-described carbon fiber reinforced composite material is applied to an elevator car room or a car frame structural member (a car structural member) will be described.
- the elevator car includes a car room 61 that accommodates people and things, a car door 62 and a car frame 63 for people to enter and exit.
- the car frame 63 is provided to reinforce the car room 61 as shown in FIG.
- the carbon fiber reinforced composite material can be used for the entire car frame 63 or a part of the diagonal storage 63a (support portion).
- the carbon fiber reinforced composite material can also be used for an elevator panel 61a applied as a floor plate, a ceiling plate, a side plate and a back plate of the cab 61.
- a carbon fiber reinforced composite material can also be used as a part of the constituent material of the panel for elevators.
- a carbon fiber reinforced composite material can be used as the reinforcing member 65 fixed to the back surface of the metal front plate 64.
- the specific strength expressed by strength per weight is about 5 for carbon fiber reinforced composite material, about 0.5 for iron and about 0.8 for aluminum.
- the weight can be reduced to, for example, 1/6 to 1/10 of the weight of a conventional elevator panel.
- Embodiment 7 An elevator car in which the sandwich panel produced in the third and fifth embodiments is applied to an elevator car room or a car frame component (a car member) will be described.
- the sandwich panel can be used for an elevator panel 61 a applied as a floor plate, a ceiling plate, a side plate, and a back plate of the cab 61.
- a sandwich panel may be applied to at least one of the floor panel, ceiling panel, side panel, and back panel.
- the elevator panel to which the above-mentioned sandwich panel is applied can reliably maintain sufficient strength and small flexibility comparable to conventional elevator panels made of metal plates against impact force.
- the weight can be reduced to, for example, 1/3 to 1/5 (about 7 kg for a CFRP sandwich panel) of the weight of a conventional elevator panel (about 36 kg for iron and about 20 kg for aluminum mixing). .
- the case where the sandwich panel is applied to an elevator car member has been described as an example.
- the use of the sandwich panel according to the third and fifth embodiments is limited to this. is not.
- elevator car members are illustrated as application examples.
- the fiber-reinforced composite material and the sandwich panel according to the present invention may be used in any field such as electrical products, building products, and mechanical products. It can also be applied to.
- the sandwich panel applied to the elevator panel is described as an example of the sandwich panel.
- the sandwich panel is not limited to an elevator panel, and can be applied to, for example, a satellite structure.
- the fiber reinforced composite material and the sandwich panel according to the present invention target the highest level of flame retardancy with respect to the flame retardance standard, but flame retardancy defined in UL94 applied to general electric products.
- flame retardancy defined in UL94 applied to general electric products.
- the standard V0 since it has high flame retardance that can easily clear the V0 level, it is extremely useful for applications that require high flame retardancy.
- the fiber-reinforced composite material of the present invention will be specifically described with reference to examples.
- the present invention is not limited to these examples.
- the fiber reinforced composite materials of Examples 1 to 5 and Comparative Examples 1 to 6 were prepared using the following materials and the manufacturing apparatus shown in FIG.
- the average particle diameter of each powdery flame retardant is a manufacturer catalog value.
- Resin 1 Brominated epoxy acrylate resin (Neopol (registered trademark) 8197 manufactured by Nippon Iupika Co., Ltd., bromine content: 25 to 27% by weight)
- Resin 2 Brominated unsaturated polyester resin (Nippon Iupika Co., Ltd.
- Resin 3 Epoxy acrylate resin (Lipoxy (registered trademark) R806 manufactured by Showa Denko KK)
- Powdered flame retardant 1 Aluminum hydroxide (HP-360 manufactured by Showa Denko KK, average particle size 2.7 ⁇ m)
- Powdered flame retardant 2 antimony trioxide (Daiichi Kogyo Seiyaku Co., Ltd.
- Powdered flame retardant 3 Aluminum hydroxide (HP-360 (pulverized product) manufactured by Showa Denko KK, average particle size 0.05 ⁇ m) Powdered flame retardant 4: Aluminum hydroxide (B52 manufactured by Nippon Light Metal Co., Ltd., average particle size 55 ⁇ m)
- Curing agent 1 Organic peroxide (328E manufactured by Kayaku Akzo Corporation)
- Curing agent 2 Methyl ethyl ketone peroxide / dimethyl phthalate solution (Permec (registered trademark) N, NOF Corporation, concentration 55% by weight)
- Curing accelerator Cobalt octenoate solution (Cobalt O, Showa Denko Co., Ltd., 8% by weight of metal)
- Fiber base material 1 Carbon fiber plain woven cloth (Toray Industries, Inc.
- Fiber base material 2 Carbon fiber plain weave cloth (Toray Industries, Inc. (trademark) cloth T300-3000, mode value 0.2 to 0.25 mm 2 , aperture ratio 6.2%)
- Fiber base material 3 Carbon fiber plain weave cloth (woven with Toray Co., Ltd.
- Fiber base material 4 Carbon fiber plain weave cloth (woven with Toray Industries, Inc., Torayca (registered trademark) T700S, mode value 0.03 to 0.05 mm 2 , aperture ratio 6.5%)
- Fiber base material 5 Carbon fiber plain weave cloth (obtained plain using TORAYCA (registered trademark) T700S manufactured by Toray Industries Inc., mode 0.10 to 0.15 mm 2 , opening ratio 9.5%)
- Fiber base material 6 Carbon fiber plain weave cloth (obtained plain using TORAYCA (registered trademark) T700S manufactured by Toray Industries, Inc., mode value 0.01 to 0.03 mm 2 , opening ratio 0.05%)
- Fiber base material 7 Carbon fiber plain weave cloth (obtained plain using TORAYCA (registered trademark) T700S manufactured by Toray Industries, Inc., mode 3.1 to 3.5 mm 2 , opening ratio 13%)
- Example 1 A fiber structure in which eight fiber substrates 1 (ply) were laminated was placed on a mold, and a release sheet and a resin diffusion sheet were sequentially placed thereon. These were covered with a sealing film, and the gap between the sealing film and the mold was closed with a sealing material to completely seal it, and the sealed space was decompressed with a vacuum pump. Thereafter, 25 parts by weight of the powdered flame retardant 1, 6 parts by weight of the powdered flame retardant 2, 1 part by weight of the curing agent 1 and a curing accelerator with respect to 100 parts by weight of the resin 1 in the decompressed sealed space. was added from the resin injection port to impregnate the fiber structure.
- the sealing film was removed, and the fiber-reinforced composite material was taken out.
- the fiber-reinforced composite material of Example 1 was obtained by standing at 80 ° C. for 2 hours, at 100 ° C. for 2 hours, and at 120 ° C. for 2 hours.
- Example 2 A fiber structure in which twelve (ply) fiber substrates 1 were laminated was placed on a mold, and a release sheet and a resin diffusion sheet were sequentially placed thereon. These were covered with a sealing film, and the gap between the sealing film and the mold was closed with a sealing material to completely seal it, and the sealed space was decompressed with a vacuum pump. Thereafter, 25 parts by weight of the powdered flame retardant 1, 6 parts by weight of the powdered flame retardant 2, 1 part by weight of the curing agent 1 and a curing accelerator with respect to 100 parts by weight of the resin 1 in the decompressed sealed space. was added from the resin injection port to impregnate the fiber structure.
- the sealing film was removed, and the fiber-reinforced composite material was taken out.
- the fiber-reinforced composite material of Example 2 was obtained by standing at 80 ° C. for 2 hours, at 100 ° C. for 2 hours, and at 120 ° C. for 2 hours.
- Example 3 A fiber-reinforced composite material of Example 3 was obtained in the same manner as in Example 1 except that the fiber substrate 3 was used instead of the fiber substrate 1.
- Example 4 A fiber-reinforced composite material of Example 4 was obtained in the same manner as in Example 1 except that the fiber substrate 4 was used instead of the fiber substrate 1.
- Example 5 A fiber-reinforced composite material of Example 5 was obtained in the same manner as in Example 1 except that the fiber base material 5 was used instead of the fiber base material 1.
- Example 2 except that the fiber base material 2 was used instead of the fiber base material 1, the resin 3 was used instead of the resin 1, and the powdered flame retardant 1 and the powdered flame retardant 2 were not added. A fiber-reinforced composite material of Comparative Example 1 was obtained.
- Comparative Example 2 The fiber-reinforced composite material of Comparative Example 2 was obtained in the same manner as in Example 2 except that the fiber base material 2 was used instead of the fiber base material 1 and the powdered flame retardant 1 and the powdered flame retardant 2 were not added. Obtained.
- Comparative Example 3 A fiber-reinforced composite material of Comparative Example 3 was obtained in the same manner as in Example 1 except that the fiber substrate 6 was used instead of the fiber substrate 1.
- Comparative Example 4 A fiber-reinforced composite material of Comparative Example 4 was obtained in the same manner as in Example 1 except that the fiber substrate 7 was used instead of the fiber substrate 1.
- Comparative Example 5 A fiber-reinforced composite material of Comparative Example 5 was obtained in the same manner as in Example 1 except that powdered flame retardant 3 was used instead of powdered flame retardant 1.
- the fiber reinforced composite materials of Examples 1 to 5 are remarkably superior in flame retardancy as compared with Comparative Examples 1 and 2 in which no powdered flame retardant was added. It can also be seen that the fiber-reinforced composite materials of Examples 1 to 5 reach the flame retardant material standards stipulated in the Japanese Building Standard Law. On the other hand, the fiber reinforced composite materials of Comparative Examples 3 and 4 using fibers whose opening size mode or opening ratio is outside the range of the present invention, and powder whose average particle size is outside the range of the present invention It can be seen that the fiber reinforced composite material of Comparative Example 5 using a flame retardant has insufficient flame retardancy.
- the sandwich panels of Examples 6 to 9 and Comparative Examples 7 to 10 were made of the above-mentioned materials, phenol resin foam as core material 1 (Neoma (registered trademark) foam manufactured by Asahi Kasei, thickness 25 mm, density 0.040 g / cm 3 ). It was produced using a phenol resin foam (Neoma (registered trademark) foam manufactured by Asahi Kasei, density 0.027 g / cm 3 ) as the core material 2 and the production apparatus shown in FIG.
- phenol resin foam as core material 1
- phenol resin foam Neoma (registered trademark) foam manufactured by Asahi Kasei, density 0.027 g / cm 3
- Example 6 Prepare two fiber structures (thickness 0.8 to 1 mm) in which four fiber base materials 1 (ply) are laminated, and sandwich the both sides of the core material 1 with these fiber structures on the mold.
- the release sheet and the resin diffusion sheet were sequentially arranged thereon. These were covered with a sealing film, and the gap between the sealing film and the mold was closed with a sealing material to completely seal it, and the sealed space was decompressed with a vacuum pump. Thereafter, 25 parts by weight of the powdered flame retardant 1, 6 parts by weight of the powdered flame retardant 2, 1 part by weight of the curing agent 1 and a curing accelerator with respect to 100 parts by weight of the resin 1 in the decompressed sealed space.
- Example 7 Example 6 except that a resin composition obtained by adding 80 parts by weight of powdered flame retardant 1, 6 parts by weight of powdered flame retardant 2 and 1 part by weight of curing agent 2 to 100 parts by weight of resin 2 was used. In the same manner, the sandwich panel was taken out. In order to fully cure, it was left to stand at 40 ° C. for 16 hours to obtain a sandwich panel of Example 7.
- Example 8 Resin composition in which 6 parts by weight of powdered flame retardant 1, 2 parts by weight of powdered flame retardant 2, 1 part by weight of curing agent 1 and 0.2 part by weight of curing accelerator are added to 100 parts by weight of resin 1
- a sandwich panel of Example 8 was obtained in the same manner as Example 6 except that the product was used.
- Example 9 A sandwich panel of Example 9 was obtained in the same manner as in Example 6 except that the fiber base material 2 was used instead of the fiber base material 1 and the core material 2 was used instead of the core material 1.
- Comparative Example 7 A sandwich panel of Comparative Example 7 was obtained in the same manner as in Example 6 except that the fiber base material 2 was used instead of the fiber base material 1 and the powdered flame retardant 1 and the powdered flame retardant 2 were not added. .
- Comparative Example 8 A sandwich is obtained in the same manner as in Example 6 except that a fiber base material 2 is used instead of the fiber base material 1 and a resin composition in which 1 part by weight of the curing agent 2 is added to 100 parts by weight of the resin 2 is used. The panel was taken out. In order to cure completely, it was allowed to stand at 40 ° C. for 16 hours to obtain a sandwich panel of Comparative Example 8.
- Example 9 Example 6 except that a resin composition in which 35 parts by weight of powdered flame retardant 1, 1 part by weight of curing agent 1 and 0.2 part by weight of a curing accelerator was added to 100 parts by weight of resin 3 was used. In the same manner, a sandwich panel of Comparative Example 9 was obtained.
- the sandwich panels of Examples 6 to 9 are remarkably superior in flame retardancy when compared with Comparative Examples 7 and 8 in which no powdered flame retardant was added. It can also be seen that the sandwich panels of Examples 6 to 9 reach the flame retardant material standards stipulated in the Japanese Building Standard Law. As can be seen from the comparison between Example 6 and Example 8, even in Example 8 where the amount of powdered flame retardant added is small, the total calorific value and the maximum heat generation rate are kept low, which is due to the uneven distribution of the powdered flame retardant. The effect was remarkable. On the other hand, it can be seen that the flame retardant properties of the sandwich panel of Comparative Example 9 in which no bromine-containing resin was used and the sandwich panel of Comparative Example 10 in which aluminum hydroxide was not used were insufficient.
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Abstract
Description
本発明は、上記のような課題を解決するためになされたものであり、高い難燃性を有し、軽量で且つ高強度な繊維強化複合材料及びその製造方法を提供することを目的とする。
この実施の形態では、繊維構造体の表面に粉末状難燃剤が偏在した繊維強化複合材料を製造するための製造装置及び繊維構造体の表面に粉末状難燃剤が偏在した繊維強化複合材料の製造方法について説明する。
まず、繊維基材を用意する(ステップS1)。
続いて、その繊維基材を所定の形状に裁断する(ステップS2)。
次に、成形型11の上に、第1樹脂拡散用シート12a及び第1離型用シート13aを順次積層する(ステップS3)。なお、この工程は省略することもできる。
続いて、裁断された繊維基材を、第1離型用シート13a(第1樹脂拡散用シート12a及び第1離型用シート13aを省略した場合、離型処理された成形型11)の上に積層して繊維構造体10とする(ステップS4)。
次に、繊維構造体10の周囲にシール材15を配置する(ステップS5)。
続いて、樹脂注入口18及び排気口19を設置する(ステップS6)。
次に、繊維構造体10の表面を第2離型用シート13bで覆う(ステップS7)。
続いて、第2離型用シート13bの表面を第2樹脂拡散用シート12bで覆う(ステップS8)。
次に、繊維構造体10を覆うように密閉用フィルム14を被せ、シール材15にて密閉用フィルム14内の空間を外部と遮断する(ステップS9)。この段階で、図1に示すように、成型準備が完了する(ステップS10)。
続いて、真空ポンプ16を駆動させて、密閉用フィルム14内の空気を排気する(ステップS11)。
次に、臭素含有樹脂及び粉末状難燃剤を混合し、臭素含有樹脂中に粉末状難燃剤を分散させる(ステップS12)。
次に、樹脂タンク17に充填された粉末状難燃剤及び臭素含有樹脂の混合物を、樹脂注入口18から密閉用フィルム14内の空間に注入し、繊維構造体10に含浸させる(ステップS13)。このとき、粉末状難燃剤及び臭素含有樹脂の混合物が繊維基材の開口部でろ過され、粉末状難燃剤は繊維構造体10の表層に偏在するようになる。
続いて、密閉用フィルム14内に注入された臭素含有樹脂を硬化させる(ステップS14)。ここで、硬化の方法としては、臭素含有樹脂の種類及び触媒を選択することによって、室温硬化又は加熱硬化が可能である。
次に、成形型11を取り外すことができる程度に臭素含有樹脂が硬化したら、第2樹脂拡散用シート12bとともに第2離型用シート13bを剥がし、繊維構造体10に臭素含有樹脂を含浸させた繊維強化複合材料を成形体として成形型11から取り外す(ステップS15)。
続いて、必要に応じて、取り外された成形体に、乾燥炉による後硬化処理を実施する(ステップS16)。
こうして、繊維強化複合材料からなる成形体が完成する(ステップS17)。
開口部の面積の測定及び開口率の算出は、1枚あたり100cm2の総面積を有する繊維基材における開口部の面積を計測することにより実施することが好ましい。ここで、最頻値とは、データ群又は確率分布で最も頻繁に出現する値である。
繊維基材としては、平織り、綾織り、朱子織り等の各種クロス、又は一方向に並べた繊維を別の繊維で束ねてシート状にした一方向クロスを用いることができる。
また、粉末状難燃剤21は、水酸化アルミニウム及び水酸化マグネシウムの他に、三酸化アンチモン及びホウ酸亜鉛から選択される少なくとも1種を更に含んでもよい。また、三酸化アンチモン及びホウ酸亜鉛から選択される少なくとも1種は、100重量部の臭素含有樹脂22に対して、0~20重量部の範囲で添加することができる。
また、難燃性をより向上させるため、りん酸エステル系難燃剤、りん-窒素化合物系等の添加型又は反応型難燃剤を併用してもよい。
なお、本発明において、平均粒径とは、測定される粒子の体積割合の合計値に対して、ある粒子径以下の体積割合の合計が50%となるときの粒子径の値を表す。
臭素化不飽和ポリエステル樹脂は、製造段階において臭素を導入したもの、又は臭素化したモノマーを混合したものを用いることができる。なお、製造段階において臭素を導入する方法として、例えば以下に挙げる4つの方法を用いることができる。
まず、第1の方法は、多価アルコール成分として、ジブロモネオペンチルグリコールを用いる方法である。
また、第2の方法は、飽和二塩基酸又はその無水物としてテトラブロムフタル酸及びその無水物を用いる方法である。
また、第3の方法は、飽和二塩基酸又はその無水物として、テトラヒドロフタル酸及びその無水物、エンドメチレンテトラヒドロフタル酸及びその無水物等を用いて不飽和ポリエステルを製造した後、この飽和二塩基酸成分の二重結合に臭素を付加する方法である。
更に、第4の方法は、飽和二塩基酸成分の機能とα,β-不飽和二塩基酸成分の機能とを併せ持つジシクロペンタジエン-マレイン酸付加物を原料の一部として用いて不飽和ポリエステルを製造した後、ジシクロペンタジエンの残存二重結合に臭素を付加する方法である。
臭素化エポキシアクリレート樹脂としては、可撓性に優れる観点から、テトラブロムビスフェノールA型エポキシ(メタ)アクリレート、テトラブロムビスフェノールF型エポキシ(メタ)アクリレート、テトラブロムビスフェノールS型エポキシ(メタ)アクリレート等が好ましい。
この実施の形態では、実施の形態1において、所定の形状に裁断した繊維基材を積層して繊維構造体10とする代わりに、連続繊維を型に巻き付けて繊維構造体10を準備し、この繊維構造体10の面方向から、粉末状難燃剤21及び臭素含有樹脂22の混合物を含浸することによって、繊維構造体の表層に粉末状難燃剤21を偏在させた繊維強化複合材料を製造する。
この実施の形態では、発泡体からなるコア材の両側表面を繊維構造体10で挟み込んでなる構造体の表面に粉末状難燃剤21が偏在した繊維強化複合材料パネル(以下、サンドイッチパネルと呼ぶ)を製造するための製造装置及びサンドイッチパネルの製造方法について説明する。
まず、繊維基材及び発泡体31を用意する(ステップS21)。
続いて、繊維基材及び発泡体31を所定の形状に裁断する(ステップS22)。
次に、成形型11の上に、第1樹脂拡散用シート12a及び第1離型用シート13aを順次積層する(ステップS23)。なお、この工程は省略することもできる。
続いて、裁断された繊維基材を、第1離型用シート13a(第1樹脂拡散用シート12a及び第1離型用シート13aを省略した場合、離型処理された成形型11)の上に積層して繊維構造体10とし、その繊維構造体10の上に裁断された発泡体31を配置し、更に、その発泡体31の上に裁断された繊維基材を積層して繊維構造体10とし、発泡体31の両側表面を繊維構造体10で挟み込んだ状態にする(ステップS24)。なお、繊維構造体10は発泡体31の片面のみに積層されてもよい。
次に、発泡体31の両側表面を繊維構造体10で挟み込んでなる構造体の周囲にシール材15を配置する(ステップS25)。
続いて、樹脂注入口18及び排気口19を設置する(ステップS26)。
次に、発泡体31の両側表面を繊維構造体10で挟み込んでなる構造体の表面を第2離型用シート13bで覆う(ステップS27)。
続いて、第2離型用シート13bの表面を第2樹脂拡散用シート12bで覆う(ステップS28)。
次に、発泡体31の両側表面を繊維構造体10で挟み込んでなる構造体を覆うように密閉用フィルム14を被せ、シール材15にて密閉用フィルム14内の空間を外部と遮断する(ステップS29)。この段階で、図5に示すように、成型準備が完了する(ステップS30)。
続いて、真空ポンプ16を駆動させて、密閉用フィルム14内の空気を排気する(ステップS31)。
次に、粉末状難燃剤21及び臭素含有樹脂22を混合し、臭素含有樹脂22中に粉末状難燃剤21を分散させる(ステップS32)。
次に、樹脂タンク17に充填された粉末状難燃剤21及び臭素含有樹脂22の混合物を、樹脂注入口18から密閉用フィルム14内の空間に注入し、繊維構造体10に含浸させる(ステップS33)。このとき、粉末状難燃剤21及び臭素含有樹脂22の混合物が繊維基材の開口部でろ過され、粉末状難燃剤21は繊維構造体10の表層に偏在するようになる。
続いて、密閉用フィルム14内に注入された臭素含有樹脂22を硬化させる(ステップS34)。ここで、硬化の方法としては、臭素含有樹脂22の種類及び触媒を選択することによって、室温硬化又は加熱硬化が可能である。
次に、成形型11を取り外すことができる程度に臭素含有樹脂22が硬化したら、第2樹脂拡散用シート12bとともに第2離型用シート13bを剥がし、臭素含有樹脂22が含浸され且つ表層に粉末状難燃剤21が偏在する繊維構造体10で発泡体31の両側表面を挟み込んでなるサンドイッチパネルを成形体として成形型11から取り外す(ステップS35)。
続いて、必要に応じて、取り外された成形体に、乾燥炉による後硬化処理を実施する(ステップS36)。
こうして、サンドイッチパネルからなる成形体が完成する(ステップS37)。
この実施の形態では、実施の形態1又は2において、繊維として炭素繊維を用い、炭素繊維構造体の面方向から、粉末状難燃剤21及び臭素含有樹脂21の混合物を含浸することによって、炭素繊維構造体の表層に粉末状難燃剤21を偏在させた炭素繊維強化複合材料(CFRP:Carbon Fiber Reinforced Plastics)を製造する。
これに対して、(ハ)では、発熱速度が上昇開始する時間、つまり着火時間が抑えられており、上記「(1)加熱開始後5分間の総発熱量が、8MJ/m2以下であること。(2)加熱開始後5分間、最高発熱速度が、10秒以上継続して200kW/m2を超えないこと。」が達成されている。
また、連続炭素繊維を用いた場合、燃焼後に形状が保持されるとともに、繊維強化により高強度を達成することができる。
この実施の形態では、発泡体からなるコア材の両側表面を炭素繊維構造体で挟み込んでなる構造体の表面に粉末状難燃剤が偏在した炭素繊維強化複合材料パネル(以下、サンドイッチパネルと呼ぶ)を製造する。このようなサンドイッチパネルは、実施の形態4で作製した炭素繊維強化複合材料を接着剤でコア材に貼り付ける方法、又は実施の形態3の一体成形によって製造することができる。
この実施の形態では、実施の形態4で作製した炭素繊維強化複合材料を適用したエレベータのかご(かご室及びかご枠)について説明する。
図9~12を参照しながら、上述した炭素繊維強化複合材料を、エレベータのかご室又はかご枠の構成部材(かご用構成部材)に適用したエレベータのかごについて説明する。
図9に示すように、エレベータのかごは、人や物等を収容するかご室61、人等が出入りするためのかごドア62及びかご枠63を備えている。かご枠63は、図10に示すように、かご室61を補強するために設けられている。炭素繊維強化複合材料は、特に、かご枠63の全体、又は斜め控え63a(支え部)等の一部に使用することができる。
実施の形態3及び5で作製したサンドイッチパネルを、エレベータのかご室又はかご枠の構成部材(かご用部材)に適用したエレベータのかごについて説明する。サンドイッチパネルは、例えば図11に示すように、かご室61の床板、天井板、側板及び背板として適用されるエレベータ用パネル61aに使用することができる。なお、床板、天井板、側板及び背板のうち、少なくとも1つにサンドイッチパネルが適用されてもよい。
樹脂1:臭素化エポキシアクリレート樹脂(日本ユピカ株式会社製ネオポール(登録商標)8197、臭素含有量25~27重量%)
樹脂2:臭素化不飽和ポリエステル樹脂(日本ユピカ株式会社製FLH-350R、臭素含有量11重量%)
樹脂3:エポキシアクリレート樹脂(昭和電工株式会社製リポキシ(登録商標)R806)
粉末状難燃剤1:水酸化アルミニウム(昭和電工株式会社製HP-360、平均粒径2.7μm)
粉末状難燃剤2:三酸化アンチモン(第一工業製薬株式会社製AN-800(T)、平均粒径1.25μm)
粉末状難燃剤3:水酸化アルミニウム(昭和電工株式会社製HP-360(粉砕加工品)、平均粒径0.05μm)
粉末状難燃剤4:水酸化アルミニウム(日本軽金属株式会社製B52、平均粒径55μm)
硬化剤1:有機過酸化物(化薬アクゾ株式会社製328E)
硬化剤2:メチルエチルケトンパーオキサイド・フタル酸ジメチル溶液(日油株式会社製パーメック(登録商標)N、濃度55重量%)
硬化促進剤:オクテン酸コバルト溶液(昭和電工株式会社製コバルトO、金属8重量%)
繊維基材1:炭素繊維平織りクロス(東レ株式会社製トレカ(登録商標)クロスT700S-12000、最頻値0.5~0.6mm2、開口率1.0%)
繊維基材2:炭素繊維平織りクロス(東レ株式会社製トレカ(登録商標)クロスT300-3000、最頻値0.2~0.25mm2、開口率6.2%)
繊維基材3:炭素繊維平織りクロス(東レ株式会社製トレカ(登録商標)T700Sを使用して平織りしたもの、最頻値2.5~3.0mm2、開口率0.1%)
繊維基材4:炭素繊維平織りクロス(東レ株式会社製トレカ(登録商標)T700Sを使用して平織りしたもの、最頻値0.03~0.05mm2、開口率6.5%)
繊維基材5:炭素繊維平織りクロス(東レ株式会社製トレカ(登録商標)T700Sを使用して平織りしたもの、最頻値0.10~0.15mm2、開口率9.5%)
繊維基材6:炭素繊維平織りクロス(東レ株式会社製トレカ(登録商標)T700Sを使用して平織りしたもの、最頻値0.01~0.03mm2、開口率0.05%)
繊維基材7:炭素繊維平織りクロス(東レ株式会社製トレカ(登録商標)T700Sを使用して平織りしたもの、最頻値3.1~3.5mm2、開口率13%)
繊維基材1を8枚(ply)積層した繊維構造体を成形型上に配置し、その上に離型用シート及び樹脂拡散用シートを順次に配置した。これらを密閉用フィルムで覆い、密閉用フィルムと成形型と間の隙間をシール材で塞ぎ完全に密閉し、密閉された空間内を真空ポンプで減圧した。その後、減圧された密閉空間内に、100重量部の樹脂1に対し、粉末状難燃剤1を25重量部、粉末状難燃剤2を6重量部、硬化剤1を1重量部及び硬化促進剤を0.2重量部添加した樹脂組成物を樹脂注入口から注入し、繊維構造体に含浸させた。室温で2時間経過後、樹脂が硬化していることを確認した後、密閉用フィルムを除去し、繊維強化複合材料を取り出した。完全硬化させるため、80℃で2時間、100℃で2時間及び120℃で2時間静置し、実施例1の繊維強化複合材料を得た。
繊維基材1を12枚(ply)積層した繊維構造体を成形型上に配置し、その上に離型用シート及び樹脂拡散用シートを順次に配置した。これらを密閉用フィルムで覆い、密閉用フィルムと成形型と間の隙間をシール材で塞ぎ完全に密閉し、密閉された空間内を真空ポンプで減圧した。その後、減圧された密閉空間内に、100重量部の樹脂1に対し、粉末状難燃剤1を25重量部、粉末状難燃剤2を6重量部、硬化剤1を1重量部及び硬化促進剤を0.2重量部添加した樹脂組成物を樹脂注入口から注入し、繊維構造体に含浸させた。室温で2時間経過後、樹脂が硬化していることを確認した後、密閉用フィルムを除去し、繊維強化複合材料を取り出した。完全硬化させるため、80℃で2時間、100℃で2時間及び120℃で2時間静置し、実施例2の繊維強化複合材料を得た。
繊維基材1の代わりに繊維基材3を用いたこと以外は実施例1と同様にして、実施例3の繊維強化複合材料を得た。
繊維基材1の代わりに繊維基材4を用いたこと以外は実施例1と同様にして、実施例4の繊維強化複合材料を得た。
繊維基材1の代わりに繊維基材5を用いたこと以外は実施例1と同様にして、実施例5の繊維強化複合材料を得た。
繊維基材1の代わりに繊維基材2を用い、樹脂1の代わりに樹脂3を用い且つ粉末状難燃剤1及び粉末状難燃剤2を添加しなかったこと以外は実施例2と同様にして、比較例1の繊維強化複合材料を得た。
繊維基材1の代わりに繊維基材2を用い且つ粉末状難燃剤1及び粉末状難燃剤2を添加しなかったこと以外は実施例2と同様にして、比較例2の繊維強化複合材料を得た。
繊維基材1の代わりに繊維基材6を用いたこと以外は実施例1と同様にして、比較例3の繊維強化複合材料を得た。
繊維基材1の代わりに繊維基材7を用いたこと以外は実施例1と同様にして、比較例4の繊維強化複合材料を得た。
粉末状難燃剤1の代わりに粉末状難燃剤3を用いたこと以外は実施例1と同様にして、比較例5の繊維強化複合材料を得た。
粉末状難燃剤1の代わりに粉末状難燃剤4を用いて実施例1と同様にして繊維強化複合材料を作製しようとしたところ、樹脂の含浸が不十分で成形することができなかった。
日本の建築基準法に準拠した難燃性試験では、コーンカロリーメータを使用した発熱性試験を実施した。発熱性試験では、日本の建築基準法施行令第108条の2に規定された発熱性試験に準拠して、試験体1片の長さが100mmの試験体を、輻射強度50kW/m2、試験時間5分間の諸条件で試験し、最大発熱速度及び総発熱量を計測した。
発熱性試験の合否の判定基準は、以下の通りである。
最大発熱速度:10秒以上継続して200kW/m2を超えないこと
総発熱量:8MJ/m2以下であること
その他:防火上有害な裏面まで貫通する亀裂及び穴がないこと
難燃性の評価結果を表1及び2に示す。
繊維基材1を4枚(ply)積層した繊維構造体(厚さ0.8~1mm)を2個用意し、これらの繊維構造体でコア材1の両側表面を挟み込んだものを成形型上に配置し、その上に離型用シート及び樹脂拡散用シートを順次に配置した。これらを密閉用フィルムで覆い、密閉用フィルムと成形型と間の隙間をシール材で塞ぎ完全に密閉し、密閉された空間内を真空ポンプで減圧した。その後、減圧された密閉空間内に、100重量部の樹脂1に対し、粉末状難燃剤1を25重量部、粉末状難燃剤2を6重量部、硬化剤1を1重量部及び硬化促進剤を0.2重量部添加した樹脂組成物を樹脂注入口から注入し、繊維構造体に含浸させた。室温で2時間経過後、樹脂が硬化していることを確認した後、密閉用フィルムを除去し、サンドイッチパネルを取り出した。完全硬化させるため、80℃で2時間、100℃で2時間及び120℃で2時間静置し、実施例6のサンドイッチパネルを得た。
100重量部の樹脂2に対し、粉末状難燃剤1を80重量部、粉末状難燃剤2を6重量部及び硬化剤2を1重量部添加した樹脂組成物を用いたこと以外は実施例6と同様にして、サンドイッチパネルを取り出した。完全硬化させるため、40℃で16時間静置し、実施例7のサンドイッチパネルを得た。
100重量部の樹脂1に対し、粉末状難燃剤1を6重量部、粉末状難燃剤2を2重量部、硬化剤1を1重量部及び硬化促進剤を0.2重量部添加した樹脂組成物を用いたこと以外は実施例6と同様にして、実施例8のサンドイッチパネルを得た。
繊維基材1の代わりに繊維基材2を用い且つコア材1の代わりにコア材2を用いたこと以外は実施例6と同様にして、実施例9のサンドイッチパネルを得た。
繊維基材1の代わりに繊維基材2を用い且つ粉末状難燃剤1及び粉末状難燃剤2を添加しなかったこと以外は実施例6と同様にして、比較例7のサンドイッチパネルを得た。
繊維基材1の代わりに繊維基材2を用い且つ100重量部の樹脂2に対し、硬化剤2を1重量部添加した樹脂組成物を用いたこと以外は実施例6と同様にして、サンドイッチパネルを取り出した。完全硬化させるため、40℃で16時間静置し、比較例8のサンドイッチパネルを得た。
100重量部の樹脂3に対し、粉末状難燃剤1を35重量部、硬化剤1を1重量部及び硬化促進剤を0.2重量部添加した樹脂組成物を用いたこと以外は実施例6と同様にして、比較例9のサンドイッチパネルを得た。
繊維基材2を4枚(ply)積層した繊維構造体(厚さ0.8~1mm)を2個用意し、これらの繊維構造体でコア材1の両側表面を挟み込んだものに、100重量部の樹脂1に対し、粉末状難燃剤2を6重量部、硬化剤1を1重量部及び硬化促進剤を0.2重量部添加した樹脂組成物をハンドレイアップ法で含浸させた。樹脂を完全硬化させるため、80℃で2時間、100℃で2時間及び120℃で2時間静置し、比較例10のサンドイッチパネルを得た。
Claims (9)
- 真空圧と大気圧との差圧を利用して繊維構造体に樹脂を含浸した後、樹脂を硬化させることを含む繊維強化複合材料の製造方法であって、
水酸化アルミニウム及び水酸化マグネシウムから選択される少なくとも1種を含み且つ平均粒径が0.1~20μmの範囲にある粉末状難燃剤と、臭素含有樹脂との混合物を、繊維に囲まれた個々の開口部の大きさの最頻値が0.03~3mm2の範囲にあり且つ開口率が0.1~10%の範囲にある繊維構造体の面方向から含浸することにより、繊維構造体の表層に粉末状難燃剤を偏在させることを特徴とする繊維強化複合材料の製造方法。 - 真空圧と大気圧との差圧を利用して繊維構造体に樹脂を含浸した後、樹脂を硬化させることを含む繊維強化複合材料の製造方法であって、
水酸化アルミニウム及び水酸化マグネシウムから選択される少なくとも1種を含み且つ平均粒径が0.1~20μmの範囲にある粉末状難燃剤と、臭素含有樹脂との混合物を、連続繊維を成形型に巻き付けて得られる繊維構造体の面方向から含浸することにより、繊維構造体の表層に粉末状難燃剤を偏在させることを特徴とする繊維強化複合材料の製造方法。 - 離型処理された成形型上に繊維構造体を積層するステップと、積層された繊維構造体上に離型用シート及び樹脂拡散用シートを順次積層するステップと、繊維構造体、樹脂拡散用シート及び離型用シートからなる積層体を密閉用フィルムで覆って外気と遮断するステップと、密閉用フィルム内の空気を真空吸引するステップと、粉末状難燃剤と臭素含有樹脂との混合物を、離型用シート及び樹脂拡散用シートを通じて密閉用フィルム内に注入し、繊維構造体に含浸させるステップと、臭素含有樹脂を硬化させるステップと、樹脂拡散用シートとともに、離型用シートを剥離するステップとを含むことを特徴とする請求項1に記載の繊維強化複合材料の製造方法。
- 離型処理された成形型上に発泡体からなるコア材の両側表面を繊維構造体で挟み込んでなる構造体を設置するステップと、設置された構造体上に離型用シート及び樹脂拡散用シートを順次積層するステップと、構造体、樹脂拡散用シート及び離型用シートからなる積層体を密閉用フィルムで覆って外気と遮断するステップと、密閉用フィルム内の空気を真空吸引するステップと、粉末状難燃剤と臭素含有樹脂との混合物を、離型用シート及び樹脂拡散用シートを通じて密閉用フィルム内に注入し、繊維構造体に含浸させるステップと、臭素含有樹脂を硬化させるステップと、樹脂拡散用シートとともに、離型用シートを剥離するステップとを含むことを特徴とする請求項1に記載の繊維強化複合材料の製造方法。
- 請求項1~4の何れか一項に記載の方法により製造した繊維強化複合材料であって、前記繊維構造体が、炭素繊維を含むことを特徴とする繊維強化複合材料。
- 前記臭素含有樹脂が、臭素化不飽和ポリエステル樹脂及び臭素化エポキシアクリレート樹脂から選択される少なくとも1種を含むことを特徴とする請求項5に記載の繊維強化複合材料。
- 前記粉末状難燃剤が、三酸化アンチモン及びホウ酸亜鉛から選択される少なくとも1種を更に含むことを特徴とする請求項5に記載の繊維強化複合材料。
- 請求項5に記載の繊維強化複合材料を用いたことを特徴とするエレベータ用構成部材。
- 請求項5に記載の繊維強化複合材料を用いたことを特徴とするエレベータかご。
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2016221734A (ja) * | 2015-05-28 | 2016-12-28 | 三菱航空機株式会社 | VaRTM工法におけるシール構造 |
WO2017050578A1 (de) * | 2015-09-24 | 2017-03-30 | Thyssenkrupp Elevator Ag | Flächiges fahrkorbelement für eine aufzugsanlage |
KR20180035320A (ko) * | 2016-09-29 | 2018-04-06 | (주)엘지하우시스 | 열가소성 복합재, 열가소성 복합재의 제조방법 및 패널 |
JP2018134863A (ja) * | 2017-01-30 | 2018-08-30 | ゼネラル・エレクトリック・カンパニイ | 複合構造体を注入するためのシステム、方法、および装置 |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2536255B (en) * | 2015-03-10 | 2017-11-01 | Gurit (Uk) Ltd | Moulding material for composite panels |
US10029887B2 (en) * | 2016-03-29 | 2018-07-24 | Otis Elevator Company | Electroless metal coating of load bearing member for elevator system |
DE102016106402A1 (de) | 2016-04-07 | 2017-10-12 | Saertex Multicom Gmbh | Verfahren zum Verstärken von Bauteilen mit Verstärkungsfasern |
CN107364035A (zh) * | 2016-05-12 | 2017-11-21 | 三菱电机株式会社 | 层间增强纤维预成型体及制造方法、电梯用结构部件及制造方法、纤维增强塑料及制造方法 |
US11274017B2 (en) * | 2017-08-25 | 2022-03-15 | Otis Elevator Company | Belt with self-extinguishing layer and method of making |
CN110386535A (zh) * | 2018-04-12 | 2019-10-29 | 三菱电机株式会社 | 难燃性结构部件和使用了该难燃性结构部件的电梯轿厢 |
BE1028055B1 (nl) * | 2020-02-13 | 2021-09-13 | Basaltex Nv | Werkwijze voor het produceren van een brand- en warmtewerend voorgeïmpregneerd vezelmateriaal |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5995113A (ja) * | 1982-11-22 | 1984-06-01 | Mitsubishi Electric Corp | 繊維強化プラスチツクパイプ成形方法 |
JPS61275347A (ja) * | 1984-12-21 | 1986-12-05 | Kanegafuchi Chem Ind Co Ltd | 電気用積層板用不飽和ポリエステル樹脂組成物 |
JPS63122507A (ja) * | 1986-11-13 | 1988-05-26 | Matsushita Electric Works Ltd | 積層板の連続製造法 |
JPH11107107A (ja) * | 1997-08-04 | 1999-04-20 | Toray Ind Inc | 炭素繊維織物と繊維強化プラスチックおよび繊維強化プラスチックの成形方法 |
JP2000238140A (ja) * | 1999-02-17 | 2000-09-05 | Toray Ind Inc | Frp筒状体およびその製造方法 |
JP2001062932A (ja) * | 1999-08-25 | 2001-03-13 | Toray Ind Inc | 繊維強化樹脂構造体およびその製造方法 |
JP2011116504A (ja) * | 2009-12-03 | 2011-06-16 | Mitsubishi Electric Corp | エレベータ用かご及びその製造方法 |
JP2011230408A (ja) * | 2010-04-28 | 2011-11-17 | Mitsubishi Electric Corp | 炭素繊維強化複合材料、その製造方法及びそれを用いたエレベータかご |
JP2012051130A (ja) * | 2010-08-31 | 2012-03-15 | Mitsubishi Electric Corp | 繊維強化複合材料の製造方法及びエレベータかごの製造方法 |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
LU66454A1 (ja) * | 1972-11-10 | 1974-06-05 | ||
US3891605A (en) * | 1974-04-04 | 1975-06-24 | Dow Chemical Co | Brominated pentaerythritolic polyesters and process therefor |
GB1572940A (en) * | 1977-07-09 | 1980-08-06 | Freeman Chemical Corp | Unsaturated polyester resin |
JPS6449638A (en) * | 1987-08-20 | 1989-02-27 | Hitachi Chemical Co Ltd | Fire retardant electrical laminated-sheet |
US4902215A (en) * | 1988-06-08 | 1990-02-20 | Seemann Iii William H | Plastic transfer molding techniques for the production of fiber reinforced plastic structures |
JP2993791B2 (ja) * | 1991-12-09 | 1999-12-27 | 三菱電機株式会社 | 低熱膨張複合材料およびその製造方法 |
IE921328A1 (en) * | 1992-04-23 | 1993-11-03 | Defped Ltd | Particulate magnesium hydroxide |
US5665301A (en) * | 1995-07-11 | 1997-09-09 | Arctek Inc. | Apparatus and method for forming fiber reinforced composite articles |
EP0754728A1 (de) * | 1995-07-14 | 1997-01-22 | Hoechst Aktiengesellschaft | Flammwidrige Epoxidharz-Formmassen |
JP2856317B2 (ja) * | 1996-03-04 | 1999-02-10 | 東レ株式会社 | エレベータ用かご |
US5760161A (en) * | 1997-02-10 | 1998-06-02 | Albemarle Corporation | Process for making unsaturated, thermosetting, brominated phthalic anhydride/polyol polyester resins |
ATE283163T1 (de) * | 1997-05-15 | 2004-12-15 | Toray Industries | Gewebe-prepreg und nassverfahren zur herstellung desselben |
JP3356010B2 (ja) * | 1997-07-28 | 2002-12-09 | 松下電工株式会社 | 金属箔張り積層板の製造方法 |
US6495621B1 (en) * | 1997-11-12 | 2002-12-17 | Mitsubishi Engineering-Plastics Corporation | Molding material for OA machine parts with improved vibration damping properties |
DE60217405T2 (de) * | 2001-06-28 | 2007-11-29 | Toray Industries, Inc. | Epoxidharzzusammensetzung mit hervorragender witterungsbeständigkeit und faserverstärkte verbundwerkstoffe |
US6858314B2 (en) * | 2002-10-22 | 2005-02-22 | Ashland, Inc. | Brominated polyester resins, resin compositions containing brominated polyester resins, and laminate compositions |
US7591973B2 (en) * | 2002-11-28 | 2009-09-22 | Mitsubishi Rayon Co., Ltd. | Method for producing a fiber-reinforced composite material plate |
DE102004018336A1 (de) * | 2004-04-15 | 2005-11-10 | Albemarle Corporation | Flammhemmender Füllstoff für Kunststoffe |
DE102004039664B4 (de) * | 2004-08-16 | 2007-08-02 | Albemarle Corp. | Flammschutzzusammensetzung mit monomodaler Korngrößenverteilung auf Basis von Metallhydroxid und Ton, deren Herstellungsverfahren und Verwendung sowie flammgeschütztes Polymer |
DE102005016195A1 (de) * | 2005-04-08 | 2006-10-12 | Clariant Produkte (Deutschland) Gmbh | Stabilisiertes Flammschutzmittel |
GB2449146B (en) * | 2008-01-22 | 2009-04-22 | Gurit | Fibre-reinforced composite material and manufacture thereof |
JP4775520B2 (ja) * | 2009-08-17 | 2011-09-21 | Dic株式会社 | 繊維強化複合材料用樹脂組成物、その硬化物、繊維強化複合材料、繊維強化樹脂成形品、及びその製造方法 |
CN102574986B (zh) * | 2009-09-18 | 2014-02-26 | Dic株式会社 | 纤维增强复合材料用树脂组合物、其固化物、纤维增强复合材料、纤维增强树脂成形品、及其制造方法 |
JP5574949B2 (ja) * | 2010-12-27 | 2014-08-20 | 三菱電機株式会社 | エレベータかご用パネルおよびそれを用いたエレベータかご |
JP2012214651A (ja) * | 2011-04-01 | 2012-11-08 | Mitsubishi Electric Corp | 難燃性繊維強化複合材料、サンドイッチパネル、それらの製造方法及びエレベータかご |
JP2012214287A (ja) * | 2011-04-01 | 2012-11-08 | Mitsubishi Electric Corp | 繊維強化複合材料成形体およびその製造方法ならびにそれを用いたエレベータかご |
CN102558852A (zh) * | 2011-12-16 | 2012-07-11 | 深圳市富恒塑胶新材料有限公司 | 一种低成本阻燃玻纤增强pa6工程塑料及其制备方法 |
-
2013
- 2013-01-09 US US14/654,922 patent/US20150336335A1/en not_active Abandoned
- 2013-01-09 WO PCT/JP2013/050232 patent/WO2014109021A1/ja active Application Filing
- 2013-01-09 CN CN201380069549.XA patent/CN104903067A/zh active Pending
- 2013-01-09 JP JP2014556256A patent/JPWO2014109021A1/ja active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5995113A (ja) * | 1982-11-22 | 1984-06-01 | Mitsubishi Electric Corp | 繊維強化プラスチツクパイプ成形方法 |
JPS61275347A (ja) * | 1984-12-21 | 1986-12-05 | Kanegafuchi Chem Ind Co Ltd | 電気用積層板用不飽和ポリエステル樹脂組成物 |
JPS63122507A (ja) * | 1986-11-13 | 1988-05-26 | Matsushita Electric Works Ltd | 積層板の連続製造法 |
JPH11107107A (ja) * | 1997-08-04 | 1999-04-20 | Toray Ind Inc | 炭素繊維織物と繊維強化プラスチックおよび繊維強化プラスチックの成形方法 |
JP2000238140A (ja) * | 1999-02-17 | 2000-09-05 | Toray Ind Inc | Frp筒状体およびその製造方法 |
JP2001062932A (ja) * | 1999-08-25 | 2001-03-13 | Toray Ind Inc | 繊維強化樹脂構造体およびその製造方法 |
JP2011116504A (ja) * | 2009-12-03 | 2011-06-16 | Mitsubishi Electric Corp | エレベータ用かご及びその製造方法 |
JP2011230408A (ja) * | 2010-04-28 | 2011-11-17 | Mitsubishi Electric Corp | 炭素繊維強化複合材料、その製造方法及びそれを用いたエレベータかご |
JP2012051130A (ja) * | 2010-08-31 | 2012-03-15 | Mitsubishi Electric Corp | 繊維強化複合材料の製造方法及びエレベータかごの製造方法 |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2016221734A (ja) * | 2015-05-28 | 2016-12-28 | 三菱航空機株式会社 | VaRTM工法におけるシール構造 |
WO2017050578A1 (de) * | 2015-09-24 | 2017-03-30 | Thyssenkrupp Elevator Ag | Flächiges fahrkorbelement für eine aufzugsanlage |
CN108137287A (zh) * | 2015-09-24 | 2018-06-08 | 蒂森克虏伯电梯股份公司 | 用于电梯设备的平面轿厢部件 |
KR20180035320A (ko) * | 2016-09-29 | 2018-04-06 | (주)엘지하우시스 | 열가소성 복합재, 열가소성 복합재의 제조방법 및 패널 |
KR101942258B1 (ko) * | 2016-09-29 | 2019-01-25 | (주)엘지하우시스 | 열가소성 복합재, 열가소성 복합재의 제조방법 및 패널 |
US10808088B2 (en) | 2016-09-29 | 2020-10-20 | Lg Hausys, Ltd. | Thermoplastic composite, method for preparing thermoplastic composite, and panel |
JP2018134863A (ja) * | 2017-01-30 | 2018-08-30 | ゼネラル・エレクトリック・カンパニイ | 複合構造体を注入するためのシステム、方法、および装置 |
Also Published As
Publication number | Publication date |
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JPWO2014109021A1 (ja) | 2017-01-19 |
CN104903067A (zh) | 2015-09-09 |
US20150336335A1 (en) | 2015-11-26 |
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