Abstract
The invention relates to a fiber reinforced structural component, which may be used in a surfboard for stand-up paddling, wave riding, wind surfing and the like, comprising a body made of plastic, wherein the body is delimited by a surface, to which a laminate layer made of a fiber mat and a matrix is undetachably connected. The surface has at least one circumferential groove-shaped recess, by means of which a predetermined partial area of the surface is delimited.
Claims
1-22. (canceled)
23. A fiber-reinforced structural component, comprising: a body made of plastic; a laminate layer; and a circumferential groove-shaped recess; wherein the body is delimited by a surface, to which the laminate layer made of at least one fiber mat and a matrix is undetachably connected; wherein the surface has at least one circumferential groove-shaped recess at least in one subregion; and wherein a predetermined partial area of the surface is delimited by the at least one circumferential groove-shaped recess.
24. The fiber-reinforced structural component according to claim 23, wherein the first partial area having the first circumferential groove-shaped recess is adjoined by a second partial area having a second circumferential groove-shaped recess.
25. The fiber-reinforced structural component according to claim 24, wherein a predetermined subsection of the first circumferential groove-shaped recess of the first partial area forms a predetermined subsection of the second circumferential groove-shaped recess of the second partial area adjoining the first partial area.
26. The fiber-reinforced structural component according to claim 23, wherein the subregion of the surface comprises a plurality of partial areas delimited by circumferential groove-shaped recesses which adjoin one another and in which respectively predetermined subsections of the circumferential groove-shaped recess of a partial area are formed by predetermined subsections of the circumferential groove-shaped recess of a neighboring partial area.
27. The fiber-reinforced structural component according to claim 23, wherein the circumferential groove-shaped recess is formed by a sequence of distance sections, curve sections or a mixture thereof.
28. The fiber-reinforced structural component according to claim 23, wherein the circumferential groove-shaped recess has a contour of a hexagon which has at least four first sides of substantially the same length each opposite one another in pairs and two mutually opposite second sides of substantially the same length.
29. The fiber-reinforced structural component according to claim 23, wherein the circumferential groove-shaped recess is configured as a regular hexagon.
30. The fiber-reinforced structural component according to claim 24, wherein each partial area has an area content, wherein the area contents are at least partially of different size.
31. The fiber-reinforced structural component according to claim 23, wherein the circumferential groove-shaped recess penetrates into the body measured from the surface of the adjacent partial area with a depth, wherein the depth is approximately 0.5 mm to approximately 15 mm.
32. The fiber-reinforced structural component according to claim 31, wherein the depth of the circumferential groove-shaped recess is constant.
33. The fiber-reinforced structural component according to claim 31, wherein the depth of the circumferential groove-shaped recess varies.
34. The fiber-reinforced structural component according to claim 31, wherein the depth of the circumferential groove-shaped recess of two adjacent partial areas is different.
35. The fiber-reinforced structural component according to claim 23, wherein the fiber mat lies fully against the circumferential groove-shaped recess, and wherein the foamed plastic has passed at least partially through the fiber mat.
36. The fiber-reinforced structural component according to claim 23, wherein the body comprises a core and an intermediate layer having a predefinable thickness extending between the core and the surface, and wherein the intermediate layer is filled with the matrix.
37. The fiber-reinforced structural component according to claim 23, wherein a second laminate layer comprising a fiber mat and a matrix is laminated onto an upper side of the laminate layer extending on the surface of the body, wherein an underside of the second laminate layer extends along the upper side of the laminate layer.
38. The fiber-reinforced structural component according to claim 23, wherein a second laminate layer comprising a fiber mat and a matrix is laminated onto an upper side of the laminate layer extending on the surface of the body, wherein an underside of the second laminate layer extends exclusively along the upper side of the laminate layer of the partial areas so that the upper side of the second laminate layer is flat.
39. A method for producing a structural component with a reinforcement made of a fiber-plastic composite comprising a body made of plastic, wherein the body is delimited by a surface to which a laminate layer comprising a fiber mat and a matrix is undetachably connected, the method comprising: applying the fiber mat to the body delimited by the surface; and forming at least one circumferential groove-shaped recess at least in a subregion of the surface, wherein a predetermined partial area of the surface is delimited by the circumferential groove-shaped recess.
40. The method according to claim 39, further comprising heating a punch to a predetermined temperature, wherein the punch has at least one elevation corresponding to the circumferential groove-shaped recess.
41. The method according to claim 40, wherein the punch has all the elevations corresponding to the circumferential groove-shaped recesses.
42. The method according to one of claim 40, wherein the predetermined temperature of the punch is between approximately 90 C. and approximately 220 C.
43. The method according to claim 40, wherein the punch is pressed with a predetermined pressure during a predetermined time period via the fiber mat onto the surface of the body.
44. A surfboard for stand-up paddling, wave riding or wind surfing, comprising: a body having an underside configured to float on water and an upper side opposite the underside having a surface that at least in a subregion has at least one circumferential groove-shaped recess that delimits a predetermined partial area of the surface.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0055] FIG. 1 shows a plan view of a section of a device having hexagonal circumferential groove-shaped recesses in a subregion with a laminate layer;
[0056] FIG. 2 shows an enlarged section from the subregion of the device shown in FIG. 1 in plan view;
[0057] FIG. 3 shows a first alternative embodiment of the circumferential groove-shaped recesses in plan view;
[0058] FIG. 4 shows a second alternative embodiment of the circumferential groove-shaped recesses in pan view;
[0059] FIG. 5 shows a surfboard with circumferential groove-shaped recesses arranged in a honeycomb shape in plan view;
[0060] FIG. 6 shows a cross-section through a section of the device known from FIG. 1;
[0061] FIG. 7 shows a cross-section through a section of the device known in FIG. 1 with a second laminate layer in a first embodiment;
[0062] FIG. 8 shows a cross-section through a section of the device known in FIG. 1 with a second laminate layer in a second embodiment; and
[0063] FIG. 9 shows a process sequence to produce the device.
DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS
[0064] At this point it should be assumed that the same parts in the individual figures have the same reference numbers.
[0065] FIG. 1 shows a plan view of a section of a proposed device 10. The device 10 consists of a board-like body 12 which is made of expanded polystyrene. The body 10 can however also have any other three-dimensional geometrical shape. The body 10 itself can also be produced in sandwich design from several layers of plastics. In this case, the plastics can be homogeneous, inhomogeneous and/or heterogeneous. Chambers which are filled with gas, preferably air, can also be provided in the body. The body 10 is delimited by a surface 14 to which a first laminate layer 16 comprising a fiber mat, specifically nonwoven consisting of glass fibers and a matrix, namely epoxy resin, is undetachably connected. The surface 14 has a subregion 18 in which a plurality of circumferential groove-shaped recesses 20 are formed, covering the subregion 18 of the surface 14 in a network-like manner. The circumferential groove-shaped recesses 20 delimit partial areas 22 with a predetermined area content.
[0066] FIG. 2 shows an enlarged section of the subregion 18 of the surface 14 of the device 10 coated with the laminate layer 16. A first groove-shaped recess 20 is formed circumferentially and delimits a first predetermined partial area 22 of the surface 14. The first circumferential groove-shaped recess 20 forms a regular hexagon 30. In this case, all sections 32 from which the hexagon 30 is formed are the same length. Accordingly the angles a enclosed between the adjacent sections 32 are substantially the same, i.e. 60. The first partial area 22 with the first circumferential groove-shaped recess 20 is adjoined by a second partial area 22 with a second circumferential groove-shaped recess 20. This second circumferential groove-shaped recess 20 is also configured as a hexagon 34. However the hexagon 34 differs from the regular hexagon 30. The hexagon 34 has four sides 36 which are mutually opposite in pairs and which have substantially the same length as the sides of the regular hexagon 30. Two mutually opposite sides 38 of the second circumferential groove-shaped recess 20 extending in the direction of the longitudinal axis I-I are longer than the other sides 36. Accordingly, the first partial area 22 delimited by the first circumferential groove-shaped recess 20 configured as a regular hexagon 30 is smaller than the second partial area 22 delimited by the second circumferential groove-shaped recess 20 configured as hexagon 34.
[0067] FIG. 3 shows a first alternative embodiment of the circumferential groove-shaped recesses 200, 210 which in plan view form a circular shape, wherein each circle 200, 210 has the same diameter. Five circles 200, 210 are shown, of which four 200 are arranged spaced apart from one another adjacently and below one another. Connecting lines g which connect the centre points of the adjacent circles 200 are either parallel to one another or perpendicular to one another. Each of the four circles 200 is spaced apart from the adjacent circle with the same spacing. The fifth circle 210 is arranged centrally between the four circles 200 and extends into each of the four circles 200. This arrangement results in nine partial areas 220, 222, 224 with substantially three different area contents. Each of the four circles 200 includes a first partial area 220. Furthermore there are four second partial areas 224 which are delimited by the fifth circle 210 from a total area of each of the four circles 200. The fifth circle includes a third partial area 222.
[0068] FIG. 4 shows a second alternative embodiment of the circumferential groove-shaped recesses 300, 300, 310, 310 in plan view. Nine circumferential groove-shaped recesses 300, 300 are circles having the same diameter. These circles 300, 300 are shown in a 33 arrangement, i.e. in the present exemplary embodiment, three lines arranged under one another each with three adjacently arranged circles 300, 300. The centre points of the adjacent circles 300, 300 have a distance from one another which is greater than the diameter of a circle 300, 300. Each connecting line g through the centre points of adjacent circles 300, 300 extends in the present exemplary embodiment either along the longitudinal axis I-I or at right angles to this, i.e. along the transverse axis II-II. Each tile-shaped partial area 320, 320 is delimited by the circumferential groove-shaped recess 310, 310 which is obtained from an alternating arrangement of distance sections 302 and curve sections 304. In this case, the straight distance sections 302 of the circumferential groove-shaped recess 310 of a partial area 320 form a subsection of the circumferential groove-shaped recess 310 of the adjacent partial area 320. Each of the curve sections 304 which delimit the tile-shaped partial area 320, also forms a subsection of the circular circumferential groove-shaped recess 300, 300 of the circular partial areas 322 adjoining the tile-shaped partial area 320.
[0069] FIG. 5 shows the device 10 in the form of a surfboard which has circumferential groove-shaped recesses 20 extending over the entire surface 14, each of which has the form of a rectangular hexagon 30, a so-called honeycomb having substantially the same area content 22. In this case, two mutually opposite distance sections 32 extend substantially parallel to a longitudinal axis I-I along which the surfboard 10 extends. Each distance section 32 forms a subsection of the circumferential groove-shaped recess 20 of adjacent partial areas 22.
[0070] FIG. 6 shows a cross-section through a section of the device 10 known from FIG. 1 along a line of intersection A-A which can be seen in FIG. 1. The cross-section extends along a vertical axis III-Ill perpendicular to the longitudinal axis I-I and the transverse axis II-II. The surface 14 delimiting the body 12 has partial areas 22 which are delimited by circumferential groove-shaped recesses 20. The laminate layer 16 which is undetachably connected to the surface 14, extends along the surface 14. In the exemplary embodiment shown here, a depth t, t which extends from the partial area 22 as far as a deepest point of the circumferential groove-shaped recess 20, varies. The different depths t, t can be clearly seen in this exemplary embodiment. The depths can be approximately 0.5 mm to approximately 15 mm. In the present exemplary embodiment the greater depth t is 5 mm and the smaller depth t is 3 mm. Not shown in this exemplary embodiment is a penetration of the foamed polystyrene from which the body 10 is made through the nonwoven made of glassfibers. From the laminate layer 16 the matrix 26 extends into the body 12 and forms an intermediate layer 40 between the surface 14 and a core 42 of the body 12. This intermediate layer 40 prevents an interface stress between the laminate layer 16 and the surface 14. On the contrary, a force acting on the laminate layer 16 is at least partially absorbed due to the intermediate layer 40 in which a fraction of the matrix 26 from the surface 14 as far as the core 42 is reduced to a predetermined extent and merely the remaining force is introduced into the core.
[0071] FIG. 7 shows a cross-section through a section of the device 10 known from FIG. 1 along the transverse axis II-II which can be seen in FIG. 1. Here also the cross-section extends along the vertical axis III-Ill. A second laminate layer 44 which is connected undetachably to the first laminate layer 16, extends on an upper side 41 of the first laminate layer 16. Thus, the second laminate layer 44 extends along the circumferential groove-shaped recesses 20 and maps the surface 14 with the circumferential groove-shaped recesses 20 on its upper side 46.
[0072] FIG. 8 shows a cross-section through a section of the device 10 known from FIG. 1 along the transverse axis II-II which can be seen in FIG. 1. Here also the cross-section extends along the vertical axis III-Ill. In contrast to the embodiment of FIG. 7, the circumferential groove-shaped recesses 20 mapped on the upper side 41 of the first laminate layer 16 are filled with a filled matrix 28. A filled matrix 28 is achieved by adding filler in the form of glass fiber scraps to the matrix in the present exemplary embodiment. A filled matrix 28 can also cure free from stresses in greater layer thicknesses and can be elastic as a result of the fillers. The recesses 20 mapped on the upper side 41 of the first laminate layer 16 are filled with so much matrix 28 that the recesses 20 are bridged and a second laminate layer 44 is undetachably connected to the first laminate layer 16 in the region of the partial areas 22 and to the filled matrix 28 in the region of the recesses 20. The second laminate layer 44 forms a substantially flat upper side 46.
[0073] The surface can be enlarged by the circumferential groove-shaped recesses so that the laminate layer can rest on an enlarged area compared with a surface without recesses. More adhesion forces can act through the surface enlarged by the groove-shaped recess, which thus lead to an improved connection of the laminate layer to the foamed plastic of the body. Furthermore, the matrix can be adjusted by suitable measures in such a manner that it penetrates into the body, forms an intermediate layer there which improves the connection of the laminate layer to the body. The circumferential groove-shaped recesses delimit partial areas of the surface with an arbitrary contour. Due to the circumferential groove-shaped recesses, not only the surface can be increased to increase the connecting forces of the laminate layer to the body but also the bending stiffnesses around the longitudinal axis extending in the longitudinal direction of the device, the transverse axis and the vertical axis. Furthermore the bending stiffnesses about the longitudinal axis, the transverse axis and/or the vertical axis can be specifically adapted to the actually occurring loads by constant or varied depth of the circumferential groove-shaped recess and by the area content of the partial areas inscribed by the circumferential groove-shaped recess. Additional laminate layers can be applied to the first laminate layer to increase the bending stiffness.
[0074] FIG. 9 shows a process diagram for manufacturing a structural component with a reinforcement of a fiber-plastic composite, in particular a surfboard for stand-up paddling, wave riding, wind surfing and the like. Process step S1 comprises providing a substantially board-like body of foamed plastic which is delimited by a surface and completely encased with a fiber mat, in the present exemplary embodiment by a nonwoven of glassfibers. In a following process step S2 the circumferential groove-shaped recesses are applied in a subregion of the surface, wherein predetermined partial areas of the surface are delimited by the circumferential groove-shaped recesses. For this purpose there is a stamper which in the present exemplary embodiment has a size to execute all the circumferential groove-shaped recesses in one process step. Elevations are formed on the stamper, which correspond to the circumferential groove-shaped recesses to be applied. The stamper will be placed on the fiber mat at the predetermined point so that the elevations point towards the fiber mat. In a following process step S3 the stamper will be pressed by pneumatic cylinders with a predetermined force onto the fiber mat-body composite and the stamper will be heated to about 150 C. heating cartridges arranged in the stamper. By a lower temperature of the stamper, the penetration depth of the stamper into the body of the fiber mat-body composite can be reduced. Due to the temperature the plastic of the body melts and penetrates at least partially through the fiber mat. After application of the recesses, the stamper will be removed from the fiber mat-body composite. In a further process step S4 the fiber mat will be impregnated with matrix, covered with a tear-off fabric, placed in a vacuum bag and a predetermined negative pressure will be produced to make the matrix penetrate into the fiber mat. In this case, the matrix can penetrate through the fiber mat into the body and thus form an intermediate layer adjoining the surface of the body in which the volume fraction of the matrix decreases with increasing distance from the surface as far as a specific concentration. After reaching this concentration, the matrix usually does not penetrate more deeply into the body. After removing the structural component and removing the tear-off fabric, this process step is ended. In order to reinforce the structural component, in a further process step S5 one or more laminate layers can be applied to the first laminate layer. In this case, the recesses can be mapped in the following laminate layers or bridged. Also the at least one additional laminate layer can be applied to only a subregion onto one of the laminate layers in order to increase, for example, the impact resistance or the maximum permissible pressure loading in subregions. The optional nature of process step S5 is indicated by a dashed arrow.
