HK1047071B - Fiber reinforced epoxy resin product and method for the manufacture thereof - Google Patents
Fiber reinforced epoxy resin product and method for the manufacture thereof Download PDFInfo
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- HK1047071B HK1047071B HK02108774.3A HK02108774A HK1047071B HK 1047071 B HK1047071 B HK 1047071B HK 02108774 A HK02108774 A HK 02108774A HK 1047071 B HK1047071 B HK 1047071B
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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
- B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
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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
- B29C70/467—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 during mould closing
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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
- B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
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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
- B32B27/38—Layered products comprising a layer of synthetic resin comprising epoxy resins
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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
- B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- 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
- B32B2363/00—Epoxy resins
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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
- B32B2605/00—Vehicles
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Medicinal Chemistry (AREA)
- Materials Engineering (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
- Bridges Or Land Bridges (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
A fiber reinforced epoxy resin product and a method for manufacturing the epoxy resin product is provided. The fiber reinforced epoxy resin product comprises a hardened epoxy resin mixture which includes epoxy resin, silica and a fibrous material, wherein the fibrous material is a material selected from the group consisting of glass fiber, carbon fiber, aramid fiber and Kevlar fiber or a mixture of these fibers, and at least one layer of glass fiber roving cloth is arranged parallel to each other in the hardened epoxy resin mixture. The method for manufacturing a fiber reinforced epoxy resin product comprises the steps of providing a mold for the product, applying a release agent to inner surfaces of the mold, providing at least one layer of glass fiber roving cloth in the mold, casting an unhardened epoxy resin mixture in the mold, pressing the epoxy resin mixture in the mold, hardening the epoxy resin mixture in the mold under a temperature between about 20 DEG C and about 80 DEG C for more than 30 minutes, releasing the hardened epoxy resin mixture from the mold, and curing the hardened epoxy resin mixture under a temperature between about 20 DEG C and 35 DEG C for about 24 hours to form the product.
Description
Technical Field
The present invention relates to a fiber-reinforced epoxy resin product and a method for manufacturing the same, and more particularly, to a fiber-reinforced epoxy resin product comprising a hardened epoxy resin mixture containing an epoxy resin, silica and reinforcing materials such as glass fiber, carbon fiber, aramid fiber and kevlar fiber, and at least one layer of glass fiber roving cloth, and a method for manufacturing the same.
Background
Generally, various methods such as a steel plate bonding method, a prestressing method, and a cross-sectional growing method can be used for reinforcing and repairing a concrete member.
The bending strength of the bridge deck or the shearing strength of the bridge piers is enhanced by adopting a steel plate bonding method. When the magnitude of the prestress is less than the desired value, a prestressing method is used in the concrete casting. When the number of the reinforcing rods and the size of the cross section of the concrete member are insufficient, a cross section reinforcing method is adopted.
Recently, the steel plate adhesion method is the most widely used one among the above-mentioned methods. In this method, the steel plate is bonded to the concrete surface by a cement material such as epoxy resin, and the transfer of shear stress between the concrete surface and the steel plate and the sufficient adhesive strength can be ensured.
However, in this method, continuous maintenance is required to maintain the adhesive strength between the concrete surface and the steel plate. Also, when the concrete member is exposed to seawater, it is difficult to sufficiently reinforce or repair because of corrosion of the steel plate or problems associated with durability of the cement material. Also, the member load increases as the number of steel sheets increases, wherein the steel has a relatively high specific gravity. Further, the steel plate is generally bonded on the bottom surface of the member. Therefore, a large number of man-hours and workers are required, thereby increasing costs.
By using Fiber Reinforced Plastic (FRP) plates instead of steel plates, problems caused by corrosion are avoided. However, FRP plates have so low a strength that it only functions as a covering for concrete surfaces.
In order to solve these problems, several improved methods have been proposed, such as the method described in korean laid-open publication No.174,161, entitled "epoxy resin sheet for reinforcing concrete member and method for manufacturing the same", filed by the present applicant, or japanese laid-open publication No.4-67946, entitled "thermosetting resin composite sheet". The resin board proposed in these methods includes a metal wire as a reinforcing material. However, the metal wires are corroded after a period of use, the adhesive strength between the resin material and the metal wires is reduced, and cracks or delamination in the resin sheet are also propagated. In addition, the weather resistance and chemical resistance of the metal wire are insufficient, and in most cases, physical properties such as tensile strength or compressive strength are deteriorated due to the decrease in adhesive strength.
Summary of The Invention
It is therefore an object of the present invention to provide a fiber reinforced epoxy resin product having improved physical and chemical properties and better weatherability and chemical resistance by mixing the epoxy resin with short fibers and casting the mixture into a mold in which at least one layer of glass fiber roving fabric is arranged. It is a further object of the present invention to provide a method for manufacturing such a fiber-reinforced epoxy resin product.
The fiber reinforced epoxy resin panels of the present invention may be used in a variety of fields, such as, 1) reinforcing and repairing various concrete members, 2) protecting the surface of concrete members in the presence of seawater, sewage, freeze-thaw damage or other chemical action, 3) reinforcing of tunnel linings, 4) corner casting panels for container terminals, 5) vehicle slides, and the like.
According to a preferred embodiment of the present invention, there is provided a method of manufacturing a fiber-reinforced epoxy resin product, comprising the steps of: providing a mold for the product; applying a release agent to the inner surface of the mold; placing at least one layer of glass fiber roving fabric in a mold; casting an uncured epoxy resin mixture into a mold; compressing the epoxy resin mixture in a mold; curing the epoxy resin mixture in the mold at between about 20 ℃ and about 80 ℃ for more than 30 minutes; demolding the hardened epoxy resin mixture from the mold; the hardened epoxy resin mixture is then cured at between about 20 c and 35 c for about 24 hours to form a product.
According to another preferred embodiment of the present invention, there is provided a fiber reinforced epoxy resin product comprising a hardened epoxy resin mixture comprising epoxy resin, silica and a fiber material, wherein the fiber material is a material selected from the group consisting of glass fiber, carbon fiber, aramid fiber and kevlar fiber or a mixture thereof, and at least one layer of glass fiber roving cloth placed in the hardened epoxy resin mixture in a position parallel to each other.
Brief description of the invention
The above and other objects and features of the present invention will become more apparent from the following description of the preferred embodiments taken in conjunction with the accompanying drawings, in which:
FIGS. 1A-1F illustrate an exemplary method of making a fiber reinforced epoxy resin product of the present invention;
FIG. 2 shows a cross-sectional view of a fiber reinforced epoxy board made according to the method of the present invention;
FIG. 3 depicts a cross-sectional view of a fiber reinforced epoxy board of the present invention bonded to a concrete member surface for reinforcement;
FIG. 4A shows a plan view of one application of the fiber-reinforced epoxy resin product of the present invention, namely, a corner casting panel;
FIG. 4B is a side view of the corner casting plate of FIG. 4A;
FIG. 4C shows an installation view of the panel of the present invention;
FIGS. 5A-5C show a vehicle slider made in accordance with the method of the present invention;
FIG. 6 is a bottom view of the installed vehicle slide;
fig. 7 depicts a cross-sectional view taken along line I-I of fig. 6.
Description of the specific embodiments
Fig. 1A-1F illustrate an exemplary method of making a fiber reinforced epoxy product according to the present invention.
Step (a): providing a rectangular mold (10) of a predetermined size and removing dirt or other unwanted matter therefrom. The mold (10) can be of various sizes and shapes depending on the end product application. Preferably, the mold (10) is composed of a durable metal and is reusable after cleaning of the inner surface.
Step (b): a conventional type release agent is coated on the inner surface of the mold (10) in a uniform thickness, and the release agent (20) easily separates the final product from the mold.
Step (c): a first layer of a fibrous web (30A) having a predetermined mesh size is placed in a mold (10) over a release agent (20). Prior to this, the first layer of web (30A) is cut to the appropriate size for the mold and may be impregnated with epoxy resin for strength. Preferably, the epoxy resin used for impregnation has the following physical properties: a viscosity of 380mPas (380csp), a gel time of about 15 minutes, a compressive strength of 1000kg/cm or more2Bending strength of 500kg/cm or more2Shear strength of 800kg/cm or more2Adhesive strength of 130kg/cm or more2A tensile strain at break rate of 0.02 or more and an expansion coefficient of 1.0X 10-5-2.0×10-5cm/cm/deg.C, and heat distortion temperature of 50-70 deg.C.
Step (d): the epoxy resin is mixed with the reinforcing fibre material in a ratio of 9: 1 and the mixture is cast onto a first layer of a fibre web (30A) impregnated with epoxy resin (first casting step). The mixture includes an epoxy resin, a small amount of cement, silica and a cut reinforcing fiber material. The reinforcing fiber material is selected from glass fibers, carbon fibers, aramid fibers and Kevlar fibers or mixtures thereof.
Preferably, the epoxy resin in this step has the following properties: specific gravity of 1.15-1.20, hardness of M70-M80, viscosity of 19,000-24,000cps, absorptivity of less than or equal to 0.14%, shrinkage of less than or equal to 1.1%, and epoxy equivalent of 180-230. Preferred properties of the silica are as follows: purity greater than or equal to 95%, specific gravity of 2.25-2.65, Mohs hardness of 6.5-7.0 and pH value of 7-9.
A step (e): after the first casting step, a second web (30B) having the same size and shape as the first web (30A) is placed in a mold, and an epoxy resin mixture is cast thereon (second casting step). When the second casting step is complete, the third web (30C) is positioned in the mold in a direction parallel to the first and second webs (30A, 30B). The number of fiber web layers can vary depending on the use of the final epoxy product. When used to reinforce and repair concrete members, the final epoxy product preferably has multiple layers, and, for example, the number of layers and fibers may be determined based on the desired strength increase from structural analysis.
After the first and second casting steps are completed, vibration is applied to the mold (10) by a vibrator so that the fiber network is moved into the epoxy resin mixture as shown in fig. 1E.
After the vibration step was completed, the epoxy resin mixture was hardened at 60 ℃ for 30 minutes and then compressed with a 1000kg load. Next, the epoxy resin mixture was hardened at 80 ℃ for 3 hours.
Step (f): the hardened epoxy resin mixture is demolded from the mold (10) and cured at between 25 ℃ and 30 ℃ for a predetermined time to form a fiber reinforced epoxy resin product (1). The mould (10) can be reused after removing dirt thereon.
Fig. 2 shows a cross-sectional view of a fibre-reinforced epoxy board manufactured according to the method of the invention.
Fig. 3 is a cross-sectional view of a fiber reinforced epoxy board bonded to a surface of a concrete member for reinforcement.
First, the surface of the concrete member (80) is pretreated. The surface area to be reinforced and repaired is determined and the compressive strength of the concrete element is measured. The size of the reinforcing plate is determined according to the required strength. Damaged parts of the concrete element are removed and the surface is pretreated. If necessary, the corroded steel reinforcing strip is repaired.
Next, the fiber reinforced epoxy resin plate (1) is fixed to the surface of the concrete member (80) by anchor bolts or chemical anchor bolts (84). The epoxy board (1) is spaced from the surface to be anchored by a gap of about 2 to about 6 mm. An adhesive epoxy is injected into the gap between the plate and the surface. It is preferred that the gap between the plate and the surface is as small as possible. The head of the anchor bolt (84) is removed or covered with an anchor bolt cover to prevent corrosion. Preferably the distance between the anchor bolts (84) to the edge of the panel is not more than 100mm and the length of the anchor bolts is at least 2-3 times the depth of the damaged part. About 9 anchor bolts are installed per square meter and typically the spacing between two anchor bolts is 30 cm.
Subsequently, an adhesive epoxy (90) is injected into the voids. Before injection, the periphery of the plate (1) is sealed with a sealant, preferably of the same type as the adhesive epoxy. Preferably, the bonding epoxy (90) has the same properties as the epoxy resin constituting the epoxy resin mixture but its viscosity is lower. The performance and operating conditions of the adhesive epoxy (90) are preferably checked using a model test. The adhesive epoxy resin (90) is injected under a certain pressure, such as 0.5-2.5kg/cm2Is injected into the void. The injection process is initially at a lower pressure and then slowly pressurized to avoid the formation of air bubbles. This step is carried out at 5-30 ℃.
After this injection step is completed, the adhesive epoxy is cured for 3 days, and the epoxy board is covered with a vinyl sheet or other material or the like to prevent rain or dirt. The head of the anchor bolt is removed for aesthetic purposes.
Fig. 4A shows a plan view of a corner casting panel as one application of the fiber reinforced epoxy resin product of the present invention. Fig. 4B shows a side view thereof, and fig. 4C shows the assembly of the panels.
The corner casting sheet (100) is an article of manufacture for protecting the container joint surfaces (110) from damage by container box corner components. The panels (100) are positioned to support the corners of the container.
These angle cast panels are made by the same steps as described above except that more layers of fiber web are included and the composition of some of the components are varied to increase strength. The plates can be made in various sizes, such as: {420 mm. times.1350 mm. times.20 mm }, {420 mm. times.600 mm. times.20 mm }, or {1000 mm. times.1350 mm. times.20 mm }.
Fig. 5A-5C illustrate a vehicle slider made according to the method of the present invention.
These vehicle sliders (200, 200A, 200B) are manufactured in various sizes by the same method as described above. The vehicle slider (200, 200A, 200B) is provided with a through hole (212) for fixing the bolt (210). Preferably, the fixing bolt (210) is more than 2 times greater than the height of the vehicle slider (200, 200A, 200B). The number of through holes (212) may vary depending on the length of the slider.
FIG. 6 is a bottom view of the assembled vehicle slide. Fig. 7 shows a cross-sectional view taken along the line I-I in fig. 6.
These vehicle sliders are manufactured in the same manner as described above, except that the epoxy resin mixture preferably has the following composition: 10-30 wt% of epoxy resin, 20-39 wt% of silica, 30-68 wt% of pebbles and 0.01-0.1 wt% of reinforcing substance, and more preferably 13.64 wt% of epoxy resin, 39.59 wt% of silica, 46.70 wt% of pebbles and 0.07 wt% of reinforcing fiber material.
Preferably, the web has the following properties: weight 550-610g/m2A density of 6.3 or more and a tensile strength of 1500kg/mm or more2And a flexural strength of 1295kg/mm or more2。
Furthermore, the epoxy resin mixture may contain inorganic materials having fire-resistant and self-extinguishing properties, such as aluminum hydroxide, antimony oxide, hydrogen bromide. In order to maintain the strength of the member, it is preferable that the epoxy resin mixture contains not more than 5% by weight of the inorganic material relative to the total weight of the epoxy resin mixture.
As shown in the drawing, the vehicle sliders (200, 200C) are arranged at predetermined intervals. The interval depends on the width of the vehicle, and vehicle sliders (200B) having inclined surfaces are arranged at both ends of a vehicle slider line.
After cleaning the position surface (300) of the slide block to be fixed, the vehicle is screwed (210)The slider (200) is fixed in this position. Next, the periphery of each slider is sealed with a sealant to form a resin gate and an air outlet. An adhesive epoxy (220) is injected into the interface between the surface and the slider to prevent water penetration and to ensure that the slider is firmly secured to the surface. Preferably, the thickness of the bonding epoxy layer is about 2mm to 6 mm. The injection step starts at a lower injection pressure and then gradually and slowly increases to a higher pressure in order to prevent the generation of air bubbles. Preferably, the injection pressure is 0.5-2.5kg/cm2. The bonding epoxy performs the same as the bonding epoxy described above, except that the bonding epoxy has a lower viscosity and a setting time of about 3 hours.
After the injection step is completed, the adhesive epoxy is cured for more than 3 hours. An epoxy based paint may be applied to the surface of the vehicle slider. The above steps can also be used in the manufacture of angle cast panels.
Examples
An embodiment of manufacturing the concrete reinforcing plate and the vehicle slider is described below.
Example 1
A mold having a size of 1000mm × 1000mm × 11mm is prepared, a release agent is applied to the inner surface of the mold, and at least three layers of the fiber web are placed in the mold. Subsequently, an epoxy resin mixture comprising 30.1% epoxy resin, 0.5% cement by weight, 69.3% silica by weight and 0.1% short fibers by weight was cast into a mold and then the mold was vibrated. After curing at 60 ℃ for 30 minutes, the epoxy resin mixture was compressed with a 1000kg load. The epoxy resin mixture was further hardened at 80 ℃ for 3 hours and demolded from the mold. The hardened epoxy resin mixture was cured at 25-30 ℃ and humidity of 40-50% for 3 days. The properties of the final epoxy board were tested and the following results were obtained:
TABLE 1
| Mechanical properties | Test results | Remarks for note | ||
| Compressive Strength (kg/cm)2) | 800 | Strain at break rate 0.017 | ||
| Direct tensile Strength (kg/cm)2) | 340 | Strain at break rate 0.017 | ||
| Flexural Strength (kg/cm)2) | 400 | |||
| Modulus of elasticity | Compression (kg/cm)2) | 74.000 | ||
| Stretching (kg/cm)2) | 34.000 | |||
| Poisson ratio | Compression | 0.34 | ||
| Stretching | 0.22 | |||
| Strain rate at break | Compression | 0.020 | 0.017-0.037 | |
| Stretching | 0.010 | 0.010-0.014 | ||
| Coefficient of thermal expansion | 6.5×10-6 | |||
| Weather resistance | Curing in water | Is not substantially affected | 3 months old | |
| Is placed in the air | Is not substantially affected | 3 months old | ||
| Chemical resistance | Strong acid and alkali resistance | |||
As shown in table 1, the fiber reinforced epoxy resin plate has higher compressive strength and tensile strength than concrete, and also has considerably higher flexural strength.
From the samples cured in water and the samples placed in low-temperature air, the properties of the epoxy resin product of the present invention are not affected by weather conditions such as humidity, time of placing in water, and the epoxy resin product also has strong acid and alkali resistance. Thus, the epoxy resin products have proven to be suitable for use in places with severe conditions such as sea water, sewage, vehicle exhaust, and the like.
Example 2
A mold having a size of 800mm by 1500mm by 11mm was manufactured, a release agent was applied to the inner surface of the mold, and at least three layers of the fiber web were placed in the mold. Subsequently, an epoxy resin mixture comprising 23.9% epoxy resin, 1.5% cement by weight, 74.5% silica by weight and 0.1% short fibers by weight was cast into a mold and then the mold was vibrated. After curing at 60 ℃ for 30 minutes, the epoxy resin mixture was compressed with a 1000kg load. The epoxy resin mixture was further hardened at 80 ℃ for 3 hours and demolded from the mold. The hardened epoxy resin mixture was cured at 25-30 ℃ and humidity of 40-50% for 3 days. The results obtained from testing the properties of the final epoxy boards are essentially the same as in table 1.
Example 3
A mold having a size of 170mm by 150mm by 1000mm is manufactured, a release agent such as 700-NC or PS-100 is coated on the inner surface of the mold, and a plurality of layers of the web are placed in the mold. Subsequently, an epoxy resin mixture comprising epoxy resin, silica, reinforcing fibers, pebbles and an inorganic material is cast into a mold and air bubbles are removed from the mold, the residual amount of air bubbles being less than 4%. The epoxy resin mixture was subjected to a pressure of 800-1000kg and cured for 1-3 hours, and then released from the mold. The hardened epoxy resin mixture is cured at 25-30 ℃ and a humidity of 40-50% for 24 hours. The results obtained from testing the performance of the final epoxy vehicle slider were as follows:
TABLE 2
| Performance of | Test results | Concrete and its production method | |
| Compressive Strength (kg/cm)2) | 1128 | 300 | |
| Direct tensile Strength (kg/cm)2) | 360 | 340 | |
| Flexural Strength (kg/cm)2) | 450 | 400 | |
| Weather resistance | Curing in water | Is not substantially affected | Have an influence on |
| Is placed in the air | Is not substantially affected | Have an influence on | |
| Chemical resistance | Strong acid and alkali resistance | Is poor | |
As shown in fig. 2, the fiber reinforced epoxy vehicle slider has higher compressive and tensile strengths than concrete and also has a considerably higher flexural strength. Moreover, the durability is better than that of concrete. From the samples cured in water and the samples exposed to low temperature air, the epoxy resin products of the present invention are substantially unaffected by climatic conditions such as temperature and humidity, and the time of exposure to water. The epoxy resin product also has strong acid and alkali resistance. Thus, the epoxy resin products have proven suitable for use in harsh conditions such as sea water, sewage and vehicle exhaust.
The invention has been shown and described with reference to the preferred embodiments. It will be apparent to those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention as defined in the following claims.
Claims (17)
1. A method of manufacturing a fiber reinforced epoxy resin product comprising the steps of:
(a) providing a mold for the product;
(b) applying a release agent to the inner surface of the mold;
(c) providing a layer of glass fiber roving fabric in a mold;
(d) casting an uncured epoxy resin mixture onto the glass fiber roving fabric in the mold;
(e) vibrating the mold to remove air bubbles from the uncured epoxy resin mixture;
(f) hardening the epoxy resin mixture in the mold at 20-80 ℃ for more than 30 minutes;
(g) demolding the hardened epoxy resin mixture from the mold; and
(h) the cured epoxy resin mixture was cured between 20 ℃ and 35 ℃ for 24 hours.
2. The method of claim 1, wherein the epoxy resin mixture comprises epoxy resin, silica, and a reinforcing fiber material selected from the group consisting of glass fiber, carbon fiber, aramid fiber, kevlar fiber, and mixtures thereof.
3. The method of claim 2, wherein the epoxy resin mixture further comprises cement.
4. The method of claim 2, wherein the epoxy resin mixture further comprises an inorganic material having fire resistant and self-extinguishing properties.
5. The method of claim 4, wherein the inorganic material is selected from the group consisting of aluminum hydroxide, antimony oxide, and hydrogen bromide.
6. The method of claim 1, further comprising the step of impregnating at least one layer of glass fiber roving fabric with an epoxy resin.
7. The method of claim 1, wherein the fiber reinforced epoxy product is a fiber reinforced epoxy board and steps (c) and (d) are repeated to provide at least two layers of glass fiber roving fabric.
8. The method of claim 7, wherein the epoxy resin mixture comprises epoxy resin, silica, and a reinforcing fiber material selected from the group consisting of glass fiber, carbon fiber, aramid fiber, Kevlar fiber, and mixtures thereof.
9. The method of claim 7, further comprising the step of impregnating said at least two layers of glass fiber roving fabric with an epoxy resin.
10. The method of claim 1, wherein steps (c) and (d) are repeated to provide at least two layers of glass fiber roving fabric, the hardening step is performed at between 60 ℃ and 80 ℃ for 1 to 3 hours, and the curing step is performed at between 20 ℃ and 35 ℃ and at a humidity between 30% and 60% for 24 hours.
11. The method of claim 10, wherein the number of air bubbles in the uncured epoxy resin mixture is maintained below 4%.
12. The method of claim 10, wherein the epoxy resin mixture comprises epoxy resin, silica, pebbles, and a reinforcing fiber material selected from the group consisting of glass fibers, carbon fibers, aramid fibers, kevlar fibers, and mixtures thereof.
13. The method of claim 12, wherein the epoxy resin further comprises an inorganic material having fire resistant and self-extinguishing properties.
14. A fiber reinforced epoxy resin product produced according to the process of claim 1, comprising:
a hardened epoxy resin mixture comprising an epoxy resin, silica and a fibrous material selected from the group consisting of glass fibers, carbon fibers, aramid fibers, kevlar fibers, and mixtures thereof; and
at least one layer of glass fiber roving fabric, which are placed parallel to each other in the hardened epoxy resin mixture.
15. The fiber reinforced epoxy resin product of claim 14, which is a panel comprising at least three layers of glass fiber roving fabric placed parallel to each other in the hardened epoxy resin mixture.
16. A vehicle slider member comprising a body made using the fiber reinforced epoxy product of claim 14, said body comprising a hardened epoxy resin mixture and a glass fiber roving fabric, said hardened epoxy resin mixture comprising epoxy resin, silica, and a fiber material selected from the group consisting of glass fiber, carbon fiber, aramid fiber, kevlar fiber, and mixtures thereof.
17. The vehicle slider component of claim 16, further comprising an adhesive epoxy layer to secure the component in a desired position.
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR1019990015219A KR100310016B1 (en) | 1999-04-28 | 1999-04-28 | Fiber-Reinforced Epoxy Panel And Process For Preparing Thereof |
| KR1999/15219 | 1999-04-28 | ||
| KR1019990038063A KR100314750B1 (en) | 1999-09-08 | 1999-09-08 | Fiber-Reinforced Epoxy Vehicle Block And Process For Preparing Thereof |
| KR1999/38063 | 1999-09-08 | ||
| PCT/KR2000/000403 WO2000066338A1 (en) | 1999-04-28 | 2000-04-28 | Fiber reinforced epoxy resin product and method for the manufacture thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| HK1047071A1 HK1047071A1 (en) | 2003-02-07 |
| HK1047071B true HK1047071B (en) | 2007-01-12 |
Family
ID=26635022
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| HK02108774.3A HK1047071B (en) | 1999-04-28 | 2000-04-28 | Fiber reinforced epoxy resin product and method for the manufacture thereof |
Country Status (5)
| Country | Link |
|---|---|
| JP (1) | JP2002542965A (en) |
| CN (1) | CN1264665C (en) |
| AU (1) | AU4435600A (en) |
| HK (1) | HK1047071B (en) |
| WO (1) | WO2000066338A1 (en) |
Families Citing this family (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2372706B (en) * | 2001-03-02 | 2005-08-17 | Steven Streatfield Gill | Frame |
| DE10318836A1 (en) * | 2003-04-25 | 2004-11-11 | Voith Paper Patent Gmbh | Process for coating a cylindrical body |
| CN100435210C (en) * | 2003-12-08 | 2008-11-19 | 朱富良 | Arch bar of stringed instrument made from carbon fiber and preparation technique |
| ITTO20040178A1 (en) * | 2004-03-17 | 2004-06-17 | Fiat Auto Spa | SELF-ADHESIVE STRUCTURAL STRENGTHENING ELEMENT FOR VEHICLE BODIES AND PROCEDURE FOR ITS APPLICATION |
| ITMI20060447A1 (en) * | 2006-03-14 | 2007-09-15 | Paper Technologies S R L | METHOD TO PRODUCE ONE OR MORE PRODUCTS PRODUCED MADE WITH A CALLED METHOD AND SYSTEM FOR ITS REALIZATION |
| CN100384933C (en) * | 2006-04-27 | 2008-04-30 | 上海交通大学 | Preparation method of seawater-resistant glass fiber reinforced epoxy resin nanocomposite |
| CN102147034B (en) * | 2010-02-09 | 2013-01-09 | 李爱军 | Manufacture method of cable holder stand column |
| CN101955666B (en) * | 2010-09-30 | 2012-04-18 | 长安大学 | Preparation method of glass fiber reinforced thermosetting resin-based composite material |
| CN102278400A (en) * | 2011-06-03 | 2011-12-14 | 贺智挺 | Glass fibre spring and manufacture method thereof |
| CN102879119A (en) * | 2011-07-13 | 2013-01-16 | 河海大学 | Composite material temperature sensor and manufacturing method of composite material temperature sensor |
| CN102490369B (en) * | 2011-12-02 | 2014-12-03 | 曹如锋 | Processing process of large-diameter anti-static fiber glass epoxy plastic pipeline |
| CN102528988A (en) * | 2011-12-20 | 2012-07-04 | 四川兴达明科机电工程有限公司 | Process for manufacturing bearing pad on surface of sensor |
| CN103224019B (en) * | 2013-04-24 | 2015-05-27 | 哈尔滨飞机工业集团有限责任公司 | Manufacture method of helicopter cabin cover windshield positioning pad |
| CN104552974A (en) * | 2013-10-09 | 2015-04-29 | 中航贵州飞机有限责任公司 | Preparation method of carbon fiber and fiberglass-combined reinforced composite |
| CN104175652A (en) * | 2014-08-26 | 2014-12-03 | 常州慧运复合材料有限公司 | Carbon fiber and glass fiber mixed type plane grating rib |
| CN104403306A (en) * | 2014-11-03 | 2015-03-11 | 安徽蓝翔电器成套设备有限公司 | Fiber adhesive-tape film composition, preparation method for fiber adhesive-tape film and fiber adhesive tape |
| CN104356416B (en) * | 2014-11-14 | 2017-09-15 | 西安超码复合材料有限公司 | A kind of preparation method of special type protection material |
| CN106808711A (en) * | 2015-12-01 | 2017-06-09 | 宁波华翔汽车纤维研发有限公司 | A kind of rapid shaping wet method mould pressing process of carbon fiber auto parts and components |
| CN106128746B (en) * | 2016-08-19 | 2018-11-27 | 浙江艾默可科技有限公司 | A kind of curing method reducing amorphous iron core internal stress |
| CN106189097A (en) * | 2016-08-19 | 2016-12-07 | 常州市宏发纵横新材料科技股份有限公司 | A kind of fan blade glass fiber reinforced materials and preparation method thereof |
| CN108530838B (en) * | 2018-04-20 | 2021-02-23 | 江苏澳盛复合材料科技有限公司 | Carbon fiber and glass fiber reinforced epoxy resin composite material and preparation method thereof |
| CN108973164B (en) * | 2018-08-21 | 2023-11-17 | 杭州友凯船艇有限公司 | Compression molding die with overflow hole, fitting and preparation scheme thereof |
| CN111873490B (en) * | 2020-08-12 | 2025-01-14 | 西安永兴科技发展有限公司 | Pre-embedded strips, equipment and process for epoxy resin-based fiber-reinforced high modulus wind turbine blades |
| CN112063115A (en) * | 2020-09-18 | 2020-12-11 | 海南大学 | Preparation method of natural coconut fiber reinforced epoxy resin composite fabric |
| CN112440369B (en) * | 2020-10-30 | 2022-04-22 | 颐华建筑材料有限公司 | Concrete test block apparatus for producing |
| CN113402743B (en) * | 2021-07-15 | 2022-09-16 | 北京化工大学 | A kind of preparation method of epoxy resin potting compound |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3922413A (en) * | 1974-06-03 | 1975-11-25 | Richard G Reineman | Lightweight, high strength, reinforced concrete constructions |
| JPS5621816A (en) * | 1979-07-31 | 1981-02-28 | Nissan Motor Co Ltd | Manufacture of elastic model |
| JPS56159121A (en) * | 1980-05-14 | 1981-12-08 | Mitsubishi Gas Chem Co Inc | Manufacture of multi-ply sheet |
| JPS57203511A (en) * | 1981-06-10 | 1982-12-13 | Sumitomo Electric Ind Ltd | Epoxy resin cast molding |
| JPS58205730A (en) * | 1982-05-25 | 1983-11-30 | Mitsubishi Heavy Ind Ltd | Forming method of composite product |
| JPH0925393A (en) * | 1995-05-09 | 1997-01-28 | Toray Ind Inc | Epoxy resin composition for fiber reinforced composite material, prepreg and fiber reinforced composite material |
-
2000
- 2000-04-28 HK HK02108774.3A patent/HK1047071B/en not_active IP Right Cessation
- 2000-04-28 AU AU44356/00A patent/AU4435600A/en not_active Abandoned
- 2000-04-28 CN CNB00808176XA patent/CN1264665C/en not_active Expired - Fee Related
- 2000-04-28 JP JP2000615205A patent/JP2002542965A/en active Pending
- 2000-04-28 WO PCT/KR2000/000403 patent/WO2000066338A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| JP2002542965A (en) | 2002-12-17 |
| WO2000066338A1 (en) | 2000-11-09 |
| HK1047071A1 (en) | 2003-02-07 |
| CN1353637A (en) | 2002-06-12 |
| AU4435600A (en) | 2000-11-17 |
| CN1264665C (en) | 2006-07-19 |
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| Date | Code | Title | Description |
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| PC | Patent ceased (i.e. patent has lapsed due to the failure to pay the renewal fee) |
Effective date: 20100428 |