Patent Application
20090233044
The present application claims priority to Chinese Patent Application No. 200810007781.1, filed Mar. 12, 2008, the entirety of which is hereby incorporated by reference.
The present disclosure relates to a carbon fiber composite material, a product comprising the same, and a method for preparing the same.
Carbon fiber is a common industry material. Carbon fiber has the advantages of light weight, high strength, high modulus, high temperature resistance (up to 2000° C.), high corrosion resistance, anti-fatigue and so on. As the carbon fiber composite material has excellent physical and chemical properties, it is widely used in the fields of aerospace industries, aviation industries, transportation and sports equipments, civil constructions, firefighting equipments, and so on. Furthermore, electromagnetic shielding, anti static and other properties of carbon fiber extend its application in the field of electronic appliances. However, at present, the application in the field of electronic appliances is limited in the housing of portable computers. Processing technologies are still under investigation.
Carbon fiber composite material is typically a combination of carbon fibers and a matrix (e.g. resin, metal, ceramic and so on). Generally, carbon fiber clothes and a resin (e.g. epoxy resin, phenol formaldehyde resin and so on) are hot-pressing molded to provide a carbon fiber composite material. The method of manufacturing the product made of carbon fiber composite material usually comprises the steps of: soaking the multiple layers of carbon fiber clothes in the resin, stacking the carbon fiber clothes in a hot press mould, flatting the carbon fiber clothes, and hot-press molding the multiple layers of carbon fiber clothes to form a half-finished product. Then the half-finished product is further treated to provide a smooth surface. In general, certain gaps and pores form when the fibers are knitted into a carbon fiber cloth. When the multiple layers of carbon fiber clothes are stacked together, the overlap of the pores from different layers may produce concave holes on the surface, which may cause uneven distribution of the resin. Therefore, to obtain a uniform and firm coating layer on the surface of the half-finished product, it is necessary to treat the surface of the product before spraying the coating material. The treating step is usually to fill the concave holes on the surface of the half-finished product with suitable materials. For example, liquid resin can be applied on the surface of the half-finished product by brushing or spraying. Then the resin is solidified by heating. After treatment, the surface of the half-finished product should be polished with a water proof abrasive paper. The treatment and polishing should be performed several times according to the smooth degree of the half-finished product. As a result, in the known method of manufacturing the product made of carbon fiber composite material, treatment and polishing on the surface of half-finished product are necessary steps.
In one aspect, a carbon fiber composite material comprises a plurality of carbon fiber layers, each layer having a first set of carbon fibers aligned substantially parallel to the long axis of the fibers; and a resin covering at least a portion of the carbon fiber layers. The carbon fiber layers are stacked and laminated together; and at least two layers are disposed so that the first set fibers in the two layers have a relative angle of about 5-90° with each other.
In another aspect, a product comprises a carbon fiber composite material. The carbon fiber composite material comprises a plurality of carbon fiber layers, each layer having a first set of carbon fibers aligned substantially parallel to the long axis of the fibers; and a resin covering at least a portion of the carbon fiber layers. The carbon fiber layers are stacked and laminated together; and at least two layers are disposed so that the first set fibers in the two layers are in a relative angle of about 5-90° with each other.
In yet another aspect, a method for preparing a product comprises applying a resin onto at least a portion of a plurality of carbon fiber layers; and stacking the carbon fiber layers with each other. Each layer has a first set of carbon fibers aligned substantially parallel to the long axis of the fibers; and at least two layers are disposed so that the first set fibers in the two layers are in a relative angle of about 5-90° with each other. The method further comprises laminating the carbon fiber layers to form a product.
The present disclosure provides a carbon fiber composite material comprising a carbon fiber and a resin.
Any suitable carbon fiber can be used in the present disclosure. Examples are unidirectional carbon fiber cloth, cross-knitted carbon fiber cloth, and other carbon fiber clothes with various knitting patterns.
The resin can be any suitable resin. The examples include phenol formaldehyde resin, epoxy resin and the like. The preferred example is epoxy resin, such as bisphenol-F epoxy resin.
In one embodiment, the carbon fiber composite material comprises a plurality of carbon fiber layers and a resin. Each layer has a plurality of carbon fibers aligned substantially parallel to the long axis of the fiber. There are gaps between the fibers. The carbon fiber layers are covered with the resin. The covered carbon fiber layers are stacked and laminated together. The fibers of at least two layers are in a staggered pattern. Therefore, at least some gaps in different layers are not overlapped. The resin may be distributed evenly to provide a smooth surface of the product.
Preferably, the fibers of at least two layers have a relative angle of about 5-90° with each other. More preferably, the angle is about 45°.
Preferably, the fibers of the adjacent layers have a relative angle of about 5-90° with each other. Preferably, the angles of the fibers between any adjacent layers are substantially the same.
In another embodiment, the carbon fiber composite material comprises a plurality of carbon fiber layers and a resin. Each layer has a first set of carbon fibers aligned substantially parallel to the long axis of the first set fibers, and a second set of carbon fibers aligned substantially parallel to the long axis of the second set fibers. The fibers of the first set and the second set are perpendicular to each other. The fibers of the first set and the second set cross each other. The first set of gaps between the first set of fibers and the second set of gaps between the second set of fibers also cross each other, forming pores. The resin is disposed between the carbon fiber layers. The carbon fiber layers and the resin are laminated together. The long axis of the first set fibers is assigned as the direction of the layer. The directions of at least two layers have a relative angle of about 5-45° with each other. Therefore, at least some pores from different layers are not overlapped. The concave holes on the surface may be prevented. The resin may be distributed evenly to provide a smooth surface of the product. The product can be coated without further treatment or polishing.
Preferably, the angle is about 45°.
Preferably, the directions of the adjacent layers have a relative angle of about 5-45° with each other.
Preferably, the angles of the directions between any adjacent layers are substantially the same.
In lamination process (eg. hot-pressing), the carbon fiber layer and resin will expand because of the heat. The different expansive degrees would cause distortion of the material. When the fiber layers are in a staggered pattern, preferably, with a similar angles of the directions between adjacent layers, at least part of the internal stresses may counteract each other. Thus the distortion of the product may be reduced. The staggered angle can be selected according to the specific condition, such as about 5°-90°. Preferably, the staggered angle is about 45°, so that the better isotropy will be achieved.
The present disclosure also provides a product comprising a carbon fiber composite material of the present disclosure.
The product of the present disclosure can further comprise a coating. The coating can be any suitable coating material known in the art. Preferably, the coating materials are transparent, providing a visual effect of brightness for the product. The coating can enhance the mechanical strength of the surface of the product. The coating may include a bottom layer and a top layer. The bottom layer can fill the concave holes produced in hot-pressing. The bottom layer can also increase the adhesion of the top layer to the product. The material of the top layer can be the same as the bottom layer. Also a different material can be used in the top layer. The coating can be a material with high rigidity, so that the product can have a relatively hard surface. For example, the bottom layer can be epoxy resin paint, polyurethane paint, phenol formaldehyde resin paint, or the like. The top layer can be polyurethane paint, acrylic paint, or the like.
The product comprising carbon fiber composite material can be plates, housings for electronic devices, parts of devices or other products. The product can be prepared in a certain way according to the size and the structure. For example, a product with a small size and complex structure can be prepared by precision injection molding. An example is a housing for mobile phones. The housing includes the main portion and snap joints. The housing can be assembled with the main body of the mobile phone by the snap joints. The housing can further comprise a sticky interior surface. The shape of the interior surface matches the shape of the main body of the mobile phone, so that the adhesive area may be enlarged, and the main body may be held firmly in the housing.
The present disclosure provides a method for preparing a product comprising a carbon fiber composite material. The method comprises: applying a resin onto a plurality of carbon fiber layers; stacking the pretreated carbon fiber layers with each other; and laminating the carbon fiber layers and the resin to form a product. The carbon fiber layers are arranged as disclosed in the present disclosure.
Any suitable carbon fiber can be used in the present disclosure. Examples are unidirectional carbon fiber cloth, cross-knitted carbon fiber cloth, and other carbon fiber clothes with various knitting patterns.
The resin can be any suitable resin. The examples include phenol formaldehyde resin, epoxy resin and the like. The preferred example is epoxy resin.
In one embodiment, a unidirectional carbon fiber cloth is used. Each layer has a plurality of carbon fibers aligned substantially parallel to the long axis of the fiber. The fibers of at least two layers are in a staggered pattern. Preferably, the fibers of at least two layers have a relative angle of about 5-90° with each other. More preferably, the angle is about 45°. Preferably, the fibers of the adjacent layers are in different directions. Preferably, the angles of the fibers between any adjacent layers are substantially the same.
In another embodiment, a cross-knitted carbon fiber cloth is used. Each layer has a first set of carbon fibers aligned substantially parallel to the long axis of the first set fibers, and a second set of carbon fibers aligned substantially parallel to the long axis of the second set fibers. The fibers of the first set and the second set are perpendicular to each other. The fibers of the first set and the second set cross each other. The long axis of the first set fibers is assigned as the direction of the layer. The directions of at least two layers have a relative angle of about 5-45° with each other. Preferably, the angle is about 45°. Preferably, the directions of the adjacent layers have a relative angle of about 5-45° with each other. Preferably, the angles of the directions between any adjacent layers are substantially the same.
The method for applying the resin to the carbon fiber can be any suitable methods. The examples include soaking, brushing, and spraying. Preferably, the carbon fiber cloth is soaked in the resin.
The laminating can be performed in any suitable machine. For example, a hot-pressing mould is used.
The method can further comprise a step of flatting the carbon fiber cloth.
The method can further comprising a step of coating. The coating material can be any suitable coating material known in the art. Preferably, the coating materials are transparent, providing a visual effect of brightness for the product. The coating can enhance the mechanical strength of the surface of the product. The coating may include coating a bottom layer and coating a top layer. The bottom layer can fill the concave holes produced in hot-pressing. The bottom layer can also increase the adhesion of the top layer to the product. The material of the top layer can be the same as the bottom layer. A different material can be used in the top layer. The coating can be a material with high rigidity, so that the product can have a relatively hard surface. For example, the bottom layer can be epoxy resin paint, polyurethane paint, phenol formaldehyde resin paint, or the like. The top layer can be polyurethane paint, acrylic paint, or the like.
Referring to
In
Referring to
The example illustrates a process to prepare a housing for mobile phones.
The housing of the mobile phones is shown in
Carbon fiber clothes were soaked in the resin to provide a presoaked carbon fiber clothes. The presoaked carbon fiber clothes were cut into a predetermined shape and size. Then the fiber clothes were placed and flatted in a hot-pressing mould. The fibers of each layer were in a staggered pattern. The hot-pressing mould was closed and a certain temperature and pressure were applied. For example, the temperature and pressure can be controlled at about 100° C. and 3 MPa. The fiber clothes were solidified and cooled. The half-finished housing was tailored according to the predetermined shape and size. Then a paint was sprayed on the exterior surface of the half-finished housing. The paint was heated to form a bottom layer. The bottom layer was polished. Then another paint was sprayed on the bottom layer to form a top layer. The top layer was solidified by UV irradiation in an UV curing machine for 2-4 seconds.
The part 13 in
Many modifications and other embodiments of the present disclosure will come to mind to one skilled in the art to which the present disclosure pertains having the benefit of the teachings presented in the foregoing description. It will be apparent to those skilled in the art that variations and modifications of the present disclosure can be made without departing from the scope or spirit of the present disclosure. Therefore, it is to be understood that the invention is not to be limited to the specific embodiments disclosed and that modifications and other embodiments are intended to be included within the scope of the appended claims. Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation.
| Number | Date | Country | Kind |
|---|---|---|---|
| 200810007781.1 | Mar 2008 | CN | national |
