Described below is a fibrous planar structure in which fibers are embedded in a matrix.
Compared with metallic constructional materials, fiber-reinforced plastics materials are characterized by a significantly lower specific weight and higher specific properties.
Fiber-reinforced plastics materials are known for example from DE 20 2004 008 122. They are also referred to as “organo sheets” or “hybrid yarn fabrics” and are employed in aircraft construction, shipbuilding or vehicle manufacturing as well as in the energy industry, generally in lightweight design applications.
A fiber-reinforced plastics (FRP) material is a multiphase or hybrid material composed of at least two main components, a bedding matrix and reinforcing fibers. A resin is used as the bedding matrix, while a glass, carbon and/or aramid fiber for example is used as the fiber. FRP components find application in known static constructions and increasingly also in parts or components subject to dynamic loads, for example in turbine components for power generation including wind turbines, parts for (rail) vehicles, components for electrotechnical devices (transformers, generators, motors) or in photovoltaics.
During production, a fiber is impregnated with or infiltrated by the resin. The fibers generally carry at least a partial coating, such as a so-called size or sizing on the surface for example, which on the one hand ensures a smooth fiber surface for weaving and on the other hand establishes a compatibility with the matrix. The size for example may be wet-chemically applied silane, ester, acrylate or epoxy resin compounds, and others.
There is always the requirement to optimize the rigidity, solidity, tensile strength, (impact) resistance, the improvement in the wetting characteristics of the fiber, as well as the fatigue strength and compactness of the FRP.
It is therefore desirable to provide an FRP which has improved mechanical properties compared with the prior art.
It is common general knowledge of the inventors that the adhesion between the fiber and the bedding matrix is essential for the mechanical properties of the FRP.
Described below is a fiber-reinforced plastics material formed of fibers and a bedding matrix, wherein the surface of the fiber is activated chemically and/or physically, such that upon contact with the bedding matrix the fiber reacts with the latter and thereby establishes chemical and/or physical bonds with the matrix material. Also described is a method for producing a fiber-reinforced plastics material, wherein the surface of the fiber is physically and/or chemically activated immediately before the fiber is embedded in the matrix.
These and other aspects and advantages will become more apparent and more readily appreciated from the following description of the exemplary embodiments, taken in conjunction with the accompanying drawing which is a graph of a reference glass fiber with epoxy resin in comparison with the flame-silanized and a plasma-activated surface of the glass fiber.
Reference will now be made in detail to the preferred embodiments, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to like elements throughout.
Covalent single or multiple bonds are referred to as chemical bonding. Polar or ionogenically structured bonds and hydrogen bonds designate physical, dative covalent bonds.
All types of fibers, in particular high-performance fibers, can be used as the fiber, selected for example from the following group of fibers: carbon fibers, glass fiber, aramid fiber, polymer fibers such as polyethylene fiber, polypropylene fiber, polystyrene fiber, polyethylene terephtalate fiber, ceramic fiber such as silicon carbide fiber, aluminum oxide fibers, or other reinforcing fibers. The fibers can be present in the form of a weave, an interlaced yarn, a multilayer lattice, a mesh, a fiber web, etc.
All types of plastic matrices can be used as the bedding matrix, for example thermoplastics, resins, such as epoxy resins, unsaturated polyester (UP) resins, vinyl ester (VE) resins, duromers, thermosetting resins and/or synthetic resins. The resins can contain all types of fillers. According to an embodiment variant, nanoscale particles are incorporated into the bedding matrix, which is to say for example the resin.
According to an embodiment variant, the fibers are coated such that for example a size is applied to the fiber in a wet-chemical process and sheathes the fiber.
The size is composed for example of silane or epoxy resin materials. Further examples are acrylate ester compounds and polyurethane as well as the entire gamut of polymer resin systems which can be applied to the fibers as a solution or in a dispersion.
“Chemical activation” denotes for example the contacting of the coated or uncoated reinforcing fiber with acids, oxidizing acids, bases, reducing bases, flame silanization, or similar.
“Physical activation” refers for example to activation through introduction into a plasma, for example exposure to a low-pressure or atmospheric-pressure plasma. Furthermore, corona systems are also suitable for physical surface activation.
As a result of the chemical and/or physical activation of the surface of the fiber, which is also coated for example, the fiber is placed into a reactive state, in other words brought to an energetic peak, such that it exhaustively reacts with everything that it comes into contact with and consequently drops into an energy trough. Accordingly, the contacting with the bedding matrix may follow immediately after the activation such that the reaction takes place with the matrix and not with the surrounding gases or moisture.
The fiber-reinforced plastics material may be produced in such a way that the surface of the fiber is physically and/or chemically activated immediately before the fiber is embedded in the matrix.
Through the physical activation by plasma it is also possible to deposit a thin organic or inorganic film from the plasma, which film then forms the reactive fiber surface, this also being referred to as a plasma coating.
Significant improvements in organo-sheet materials are achieved, in particular with regard to
It will be shown hereinbelow with reference to a figure how the strength of the FRP was successfully increased through the activation of the fiber surface and subsequent improved adhesion between fiber and bedding matrix:
The reference had a strength of 12.42 MPa. A pretreatment technique known as the pyrosil process, entailing the deposition of a silicate layer improving the hydrophilic properties, therefore also referred to as flame silanization, enabled this strength value to be increased by 25%, and by 33% through 100 seconds in the plasma, and by 50% through 30 seconds in the plasma.
As described herein, increases in strength can be achieved by improving the adhesion between the fiber and the bedding matrix in FRPs.
The fibrous planar structure in which fibers are embedded in a matrix have an increase in mechanical resistance that is achieved through improvement of the adhesion between the fiber and the matrix. Improved fiber/matrix adhesion is demonstrated for example by interlaminar shear strength testing, also called splitting tensile strength or transverse fiber bundle test (TFBT).
A description has been provided with particular reference to preferred embodiments thereof and examples, but it will be understood that variations and modifications can be effected within the spirit and scope of the claims which may include the phrase “at least one of A, B and C” as an alternative expression that means one or more of A, B and C may be used, contrary to the holding in Superguide v. DIRECTV, 358 F3d 870, 69 USPQ2d 1865 (Fed. Cir. 2004).
Number | Date | Country | Kind |
---|---|---|---|
10 2011 003 312.2 | Jan 2011 | DE | national |
This application is the U.S. national stage of International Application No. PCT/EP2012/050567, filed Jan. 16, 2012 and claims the benefit thereof. The International Application claims the benefit of German Application No. 10 2011 003 312.2 filed on Jan. 28, 2011, both applications are incorporated by reference herein in their entirety.
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/EP12/50567 | 1/16/2012 | WO | 00 | 7/26/2013 |