CN108314880A - A kind of cellular epoxy resin composite material production method and using body structure made of the material - Google Patents
A kind of cellular epoxy resin composite material production method and using body structure made of the material Download PDFInfo
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- CN108314880A CN108314880A CN201810234505.2A CN201810234505A CN108314880A CN 108314880 A CN108314880 A CN 108314880A CN 201810234505 A CN201810234505 A CN 201810234505A CN 108314880 A CN108314880 A CN 108314880A
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- epoxy resin
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- honeycomb
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- 239000003822 epoxy resin Substances 0.000 title claims abstract description 47
- 229920000647 polyepoxide Polymers 0.000 title claims abstract description 47
- 239000002131 composite material Substances 0.000 title claims abstract description 30
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 10
- 239000000463 material Substances 0.000 title abstract description 8
- 230000001413 cellular effect Effects 0.000 title abstract 4
- 239000003365 glass fiber Substances 0.000 claims abstract description 47
- 239000004744 fabric Substances 0.000 claims abstract description 30
- 239000007791 liquid phase Substances 0.000 claims abstract description 15
- 239000007790 solid phase Substances 0.000 claims abstract description 12
- 238000007499 fusion processing Methods 0.000 claims abstract description 4
- 239000003973 paint Substances 0.000 claims description 15
- 229920005989 resin Polymers 0.000 claims description 12
- 239000011347 resin Substances 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 5
- 239000003795 chemical substances by application Substances 0.000 claims description 4
- 238000004513 sizing Methods 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 238000002360 preparation method Methods 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims 1
- 239000011152 fibreglass Substances 0.000 abstract description 4
- 229910000831 Steel Inorganic materials 0.000 abstract description 3
- 239000007769 metal material Substances 0.000 abstract description 3
- 239000010959 steel Substances 0.000 abstract description 3
- 239000011521 glass Substances 0.000 abstract 3
- 230000035939 shock Effects 0.000 abstract 1
- 241001391944 Commicarpus scandens Species 0.000 description 5
- 238000009413 insulation Methods 0.000 description 3
- 101100495270 Caenorhabditis elegans cdc-26 gene Proteins 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000000779 smoke Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000000805 composite resin Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
Classifications
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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
- C08J9/00—Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof
- C08J9/0085—Use of fibrous compounding ingredients
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- 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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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/32—Vehicles adapted to transport, to carry or to comprise special loads or objects comprising living accommodation for people, e.g. caravans, camping, or like vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D25/00—Superstructure or monocoque structure sub-units; Parts or details thereof not otherwise provided for
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B3/00—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties
- H01B3/18—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances
- H01B3/30—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes
- H01B3/40—Insulators or insulating bodies characterised by the insulating materials; Selection of materials for their insulating or dielectric properties mainly consisting of organic substances plastics; resins; waxes epoxy resins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
- B29L2031/608—Honeycomb structures
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- B32B2255/00—Coating on the layer surface
- B32B2255/10—Coating on the layer surface on synthetic resin layer or on natural or synthetic rubber layer
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- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
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- B32B2260/046—Synthetic resin
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- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
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- C—CHEMISTRY; METALLURGY
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- C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
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Abstract
Description
技术领域technical field
本发明涉及一种房车的车身制造技术,具体地说是一种蜂窝状环氧树脂复合材料制作方法及采用该材料制成的车身结构。The invention relates to a car body manufacturing technology, in particular to a manufacturing method of a honeycomb epoxy resin composite material and a body structure made of the material.
背景技术Background technique
现有的房车车身普遍采用三明治板制成(0.5-1mm玻璃钢+泡沫+多层板),采用现有的这种材料和结构制成的壳体虽然具有一定的坚固性,但是抗冲击能力差,当出现事故时壳体容易折断破碎,因此,其安全性是难以得到保障的,特别是对于房车来说,由于户外生活行驶在乡间道路、海滩戈壁、冰雪道路,经常会经历台风、严寒、酷暑等,不但其安全性更为重要,而且还需要具有良好的阻燃性以及保温隔热性,后来现有技术中虽然出现了一些复合材料制成的壳体,但是其性能指标依然很低,很难达到高安全性、高阻燃性以及高保温隔热性、甚至是轻质量等综合性能。Existing car bodies are generally made of sandwich panels (0.5-1mm FRP + foam + multi-layer panels). Although the shells made of such materials and structures have certain firmness, they have poor impact resistance , when an accident occurs, the shell is easy to break and break, so its safety is difficult to be guaranteed, especially for RVs, because outdoor life is driven on country roads, beaches, Gobi, and ice and snow roads, often experiencing typhoons, severe cold, In severe heat, etc., not only its safety is more important, but also it needs to have good flame retardancy and thermal insulation. Later, although some shells made of composite materials appeared in the prior art, their performance indicators are still very low. , it is difficult to achieve comprehensive properties such as high safety, high flame retardancy, high thermal insulation, and even light weight.
发明内容Contents of the invention
本发明要解决的技术问题是提供一种蜂窝状环氧树脂复合材料的制作方法及采用该材料制成的车身结构。The technical problem to be solved by the present invention is to provide a manufacturing method of honeycomb epoxy resin composite material and a vehicle body structure made of the material.
为了解决上述技术问题,本发明的蜂窝状环氧树脂复合材料的制作方法,包括以下步骤:In order to solve the above-mentioned technical problems, the preparation method of honeycomb epoxy resin composite material of the present invention, comprises the following steps:
A、将玻璃纤维加工成蜂窝状的玻璃纤维织物;A. Process glass fiber into honeycomb glass fiber fabric;
B、将步骤A中的玻璃纤维织物浸于液相的环氧树脂中,当液相的环氧树脂与固相的玻璃纤维织物接触时,液相的环氧树脂沿着固相的玻璃纤维表面不断扩张并相互融合;B, the glass fiber fabric in step A is immersed in the epoxy resin of liquid phase, when the epoxy resin of liquid phase contacts with the glass fiber fabric of solid phase, the epoxy resin of liquid phase is along the glass fiber of solid phase Surfaces expand and merge with each other;
C、用外力将融合过程中固相的玻璃纤维中所多余的环氧树脂挤出,形成一个蜂窝状腔体,此时环氧树脂迅速固化,成为蜂窝状的环氧树脂复合材料。C. Use external force to extrude the excess epoxy resin in the solid-phase glass fiber during the fusion process to form a honeycomb cavity. At this time, the epoxy resin solidifies rapidly and becomes a honeycomb epoxy resin composite material.
所述步骤A中,玻璃纤维织物的厚度为3—5mm。In the step A, the thickness of the glass fiber fabric is 3-5 mm.
所述步骤B中,玻璃纤维织物浸于液相的环氧树脂中时,添加浸润剂。In the step B, when the glass fiber fabric is immersed in the epoxy resin in liquid phase, a sizing agent is added.
一种采用上述蜂窝状复合材料制成的车身结构,包括有作为支撑框架的龙骨以及龙骨外依次设置的至少两层玻璃纤维布层,玻璃纤维布层外的环氧树脂复合材料层,环氧树脂复合材料层外的玻璃纤维面毡,玻璃纤维面毡外的树脂胶衣层以及树脂胶衣层外涂覆的至少一层的刷漆层。A vehicle body structure made of the above-mentioned honeycomb composite material, including a keel as a supporting frame and at least two layers of glass fiber cloth layers arranged in sequence outside the keel, an epoxy resin composite material layer outside the glass fiber cloth layer, epoxy A glass fiber facing mat outside the resin composite material layer, a resin gel coat layer outside the glass fiber facing mat, and at least one paint layer coated outside the resin gel coat layer.
所述玻璃纤维布层设置为三层。The glass fiber cloth layers are arranged in three layers.
所述刷漆层包括树脂胶衣层外涂覆的抗紫外线漆以及抗紫外线漆外涂覆的双组份汽车表面漆。The paint layer includes an anti-ultraviolet paint coated on the resin gel coat layer and a two-component automobile surface paint coated on the outer layer of the anti-ultraviolet paint.
所述龙骨由两层玻璃纤维布层以及玻璃纤维面毡和玻璃纤维面毡外的树脂胶衣层构成。The keel is composed of two layers of glass fiber cloth layers, a glass fiber mat and a resin gel coat layer outside the glass fiber mat.
本发明的优点在于:The advantages of the present invention are:
由于采用特殊制造工艺制成的蜂窝状环氧树脂复合材料,不但使其抗拉强度远远高于钢丝,比重远远轻于金属材料,而且达到了良好的抗冲击性能以及较强回弹性,其应用于壳体遇到意外状况即便是整车翻滚也不易折断,再者其配方搭配化学稳定性好、耐候性好、不吸水,使其遇火不燃烧、不冒烟,保温隔热性好,特别适用于房车制造,将其龙骨组成一体化全承载车身,遇到外力冲击或挤压时,回弹力高,变形小,不易破碎,产生的有效空间能够更有效的保护生命安全,意义重大。Because the honeycomb epoxy resin composite material made by special manufacturing process not only makes its tensile strength much higher than that of steel wire, and its specific gravity is much lighter than that of metal materials, but also achieves good impact resistance and strong resilience. It is not easy to break even if the whole vehicle rolls over when it is applied to the shell. In addition, its formula has good chemical stability, good weather resistance, and no water absorption, so that it does not burn or emit smoke when it encounters fire. Well, it is especially suitable for the manufacture of RVs. The keel is formed into an integrated full-load body. When encountering external impact or extrusion, it has high resilience, small deformation, and is not easy to break. The effective space generated can more effectively protect life safety. major.
附图说明Description of drawings
图1为本发明蜂窝状环氧树脂复合材料制成的车身结构各层之间的剖面示意图。Fig. 1 is a schematic cross-sectional view between layers of a vehicle body structure made of a honeycomb epoxy resin composite material according to the present invention.
具体实施方式Detailed ways
下面结合附图和具体实施方式对本发明的蜂窝状环氧树脂复合材料制作方法及采用该材料制成的车身结构进一步详细说明。The manufacturing method of the honeycomb epoxy resin composite material of the present invention and the vehicle body structure made of the material will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
实施例一:Embodiment one:
本发明的蜂窝状环氧树脂复合材料制作方法,包括以下步骤:The preparation method of honeycomb epoxy resin composite material of the present invention comprises the following steps:
A、将高强度玻璃纤维加工成蜂窝状的高强度玻璃纤维织物,高强度玻璃纤维织物的厚度为3—5mm;A. Process high-strength glass fibers into honeycomb-shaped high-strength glass fiber fabrics, and the thickness of the high-strength glass fiber fabrics is 3-5mm;
B、将步骤A中的高强度玻璃纤维织物浸于液相的环氧树脂中,当液相的环氧树脂与固相的玻璃纤维织物接触时,在高强度玻璃纤维织物浸于液相的环氧树脂的过程中添加浸润剂,在浸润剂的作用下,液相的环氧树脂沿着固相的玻璃纤维表面不断扩张并相互融合;B, the high-strength fiberglass fabric in step A is immersed in the epoxy resin of liquid phase, when the epoxy resin of liquid phase contacts with the glass fiber fabric of solid phase, when high-strength fiberglass fabric is immersed in the epoxy resin of liquid phase A sizing agent is added during the epoxy resin process. Under the action of the sizing agent, the liquid-phase epoxy resin continues to expand along the solid-phase glass fiber surface and fuse with each other;
C、用外力将融合过程中固相的高强度玻璃纤维中所多余的环氧树脂挤出,形成一个蜂窝状腔体,此时环氧树脂迅速固化,成为蜂窝状的环氧树脂复合材料,经验证,此材料更轻、抗冲击、强回弹性、不易折断、遇火不燃烧、不冒烟,保温隔热性好。C. Use external force to extrude the excess epoxy resin in the high-strength glass fiber in the solid phase during the fusion process to form a honeycomb cavity. At this time, the epoxy resin solidifies rapidly and becomes a honeycomb epoxy resin composite material. It has been verified that this material is lighter, impact-resistant, strong resilience, not easy to break, does not burn in case of fire, does not emit smoke, and has good thermal insulation.
经过实践证明,采用本发明制成的蜂窝状环氧树脂复合材料,抗拉强度远远高于钢丝,比重大大轻于金属材料,抗疲劳强度高、绝缘强度高、介电常数低、尺寸稳定性好,在最大应力条件下伸张率仅为1%-2%,耐高温,抗拉强度保留率50%,化学稳定性好、耐候性好,不吸水、不燃烧、保温性好。It has been proved by practice that the honeycomb epoxy resin composite material made by the present invention has much higher tensile strength than steel wire, much lighter specific gravity than metal materials, high fatigue resistance, high dielectric strength, low dielectric constant and stable size. Good resistance, the elongation rate is only 1%-2% under the maximum stress condition, high temperature resistance, 50% tensile strength retention rate, good chemical stability, good weather resistance, no water absorption, no combustion, and good heat preservation.
实施例二:Embodiment two:
一种采用实施例一所述蜂窝状复合材料制成的车身结构,包括有作为支撑框架的龙骨1以及龙骨1外依次设置的2-8层(根据强度)高强度玻璃纤维布层2,高强度玻璃纤维布层2外的环氧树脂复合材料层3,环氧树脂复合材料层3外的玻璃纤维面毡4,玻璃纤维面毡4外的树脂胶衣层5以及树脂胶衣层外涂覆的至少一层的刷漆层6。A vehicle body structure made of the honeycomb composite material described in Embodiment 1, including a keel 1 as a supporting frame and 2-8 layers (according to strength) of high-strength glass fiber cloth layers 2 arranged in sequence outside the keel 1. Epoxy resin composite material layer 3 outside the strength glass fiber cloth layer 2, glass fiber mat 4 outside the epoxy resin composite layer 3, resin gel coat layer 5 outside the glass fiber mat 4, and resin gel coat outer coating Overlaid at least one layer of paint layer 6.
进一步地,所说的高强度玻璃纤维布层3优选地设置为三层,所说的刷漆层6包括树脂胶衣层外涂覆的抗紫外线漆以及抗紫外线漆外涂覆的双组份汽车表面漆,所说的龙骨1由两层玻璃纤维布层以及玻璃纤维面毡和玻璃纤维面毡外的树脂胶衣层构成,进一步提高了其优良的特性。Further, said high-strength fiberglass cloth layer 3 is preferably set to three layers, and said paint layer 6 includes the anti-ultraviolet paint coated on the outside of the resin gel coat layer and the two-component coating on the outside of the anti-ultraviolet paint. Automotive surface paint, said keel 1 is made of two layers of glass fiber cloth layers, glass fiber facing mat and resin gel coat layer outside the glass fiber facing felt, which further improves its excellent characteristics.
经过试验验证,采用本发明制成的蜂窝状环氧树脂复合材料与龙骨组成一体化全承载车身,遇到外力冲击或挤压时,回弹力高,变形小,不易破碎,产生的有效空间能够更有效的保护生命安全。It has been verified by experiments that the honeycomb epoxy resin composite material made by the present invention and the keel form an integrated full load-carrying vehicle body. When encountering external impact or extrusion, it has high resilience, small deformation, and is not easy to break, and the effective space produced can be More effective protection of life safety.
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