EP3216944B1 - Assembly for reinforcing support structures - Google Patents

Assembly for reinforcing support structures Download PDF

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Publication number
EP3216944B1
EP3216944B1 EP17163975.0A EP17163975A EP3216944B1 EP 3216944 B1 EP3216944 B1 EP 3216944B1 EP 17163975 A EP17163975 A EP 17163975A EP 3216944 B1 EP3216944 B1 EP 3216944B1
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EP
European Patent Office
Prior art keywords
bore
fiber bundle
groove
supporting structure
support structure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP17163975.0A
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German (de)
French (fr)
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EP3216944A1 (en
Inventor
Thierry Berset
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Sika Technology AG
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Sika Technology AG
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Publication of EP3216944A1 publication Critical patent/EP3216944A1/en
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    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04GSCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G23/00Working measures on existing buildings
    • E04G23/02Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
    • E04G23/0218Increasing or restoring the load-bearing capacity of building construction elements
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/07Reinforcing elements of material other than metal, e.g. of glass, of plastics, or not exclusively made of metal
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04GSCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G23/00Working measures on existing buildings
    • E04G23/02Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
    • E04G23/0218Increasing or restoring the load-bearing capacity of building construction elements
    • E04G2023/0251Increasing or restoring the load-bearing capacity of building construction elements by using fiber reinforced plastic elements
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04GSCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G23/00Working measures on existing buildings
    • E04G23/02Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
    • E04G23/0218Increasing or restoring the load-bearing capacity of building construction elements
    • E04G2023/0251Increasing or restoring the load-bearing capacity of building construction elements by using fiber reinforced plastic elements
    • E04G2023/0262Devices specifically adapted for anchoring the fiber reinforced plastic elements, e.g. to avoid peeling off

Definitions

  • the invention relates to the field of reinforcement of supporting structures, preferably by applying surface reinforcement, in particular the introduction of forces into the surface reinforcement.
  • a widely used method consists in inserting fiber bundles into a hole in the support structure and anchoring them there and spreading out or fanning out an end of the fiber bundle protruding beyond the surface and gluing it onto the surface.
  • a surface reinforcement can then be glued to the reinforced structure surface.
  • the surface reinforcement can first be glued to the structure surface so that when an anchor made from a fiber bundle is attached afterwards, the protruding end of this is glued to the surface of the surface reinforcement.
  • the potential fracture surface near the surface is only broken through by each anchor at one point (on the shaft).
  • the resistance of this potential fracture surface is only increased to a limited extent.
  • the power transmission from the fibers of the fiber bundle spread out on the surface to the fibers of the fabric is not optimal.
  • the very thin fiber composite material formed by the fibers of the fiber bundle on the surface can only be significantly loaded in the tensile direction. When subjected to pressure, the fiber composite material kinks; when subjected to shear and bending, only very small forces can be transmitted. Therefore, only the fibers lying approximately in the tensile direction of the surface reinforcement are fully effective. These make up only a small part of the fiber bundle cross-section and only cover a small part of the width of the surface reinforcement.
  • Another disadvantage of the known method is that the end of the fiber bundle protruding over the surface is spread out on the surface itself and is thus caused by protrusions, protruding deformations on the surface, which on the one hand can disturb the appearance of a building, but on the other hand also technical Can have disadvantages. For example, elevations in an otherwise flat surface can lead to water, in particular rainwater, or snow, but also dirt, accumulating on these elevations and impairing the long-term effect.
  • the object of the present invention is therefore to provide an arrangement according to which an improvement in the introduction of force into a surface reinforcement is to be achieved.
  • the essence of the invention is accordingly an arrangement comprising a support structure with a surface consisting of several surfaces, with a bore running from one surface into an inner area of the support structure, and this bore is filled with an adhesive and with a section of a fiber bundle protruding beyond this bore is, wherein the support structure is provided on the one surface from which the bore extends into an inner region of the support structure with at least one groove which extends from the bore in at least one direction on the surface and the protruding part of the Fiber bundle is at least partially located in the at least one groove and is fixed therein with the adhesive.
  • the supporting structure is typically a building or a component part of a building, for example a plate, a ceiling, a wall, a column, a rib, a beam or the like.
  • the supporting structure typically consists of concrete, in particular reinforced concrete, but can also consist of bricks or other bricks, wood, steel or other materials and any combination of these materials.
  • the structures are civil engineering structures such as houses, bridges, tunnels, dams, sports facilities, etc.
  • the fiber bundle is a loose arrangement of essentially unidirectional individual fibers or filaments, in particular made of carbon, glass, basalt, aramid, steel or other inorganic or organic materials.
  • the fibers are preferably carbon fibers.
  • the strength of the fiber bundle depends on the area of application and the forces that are to be transmitted through the fiber bundle. If the fiber bundle consists of carbon fibers, it comprises in particular 1000 to 50,000 individual fibers, each of which has a diameter in the range from 5 to 10 ⁇ m. A typical fiber bundle preferably has a cross-sectional area of 20 to 70 mm 2 , in particular 25 to 40 mm 2 .
  • a bore is made at the desired location, which hole serves to receive a section of the fiber bundle.
  • the bore can be created by any means, such means being very well known to the person skilled in the art.
  • the dimensions of the bore result from the strength and the length of the fiber bundle and these in turn from the requirements which are placed on the arrangement according to the invention.
  • a suitable bore typically has a diameter of 1 to 5 cm, in particular 1.5 to 3 cm, and a depth of 5 to 30 cm, in particular 7 to 20 cm.
  • one or more grooves are made.
  • the grooves can also be created by any means, for example with an angle grinder.
  • the groove or grooves are dimensioned in such a way that they can accommodate the fiber bundle in their entirety, which can be divided into individual fiber strands in the event that several grooves are present.
  • the number and arrangement of the grooves is dependent on the area of application of the arrangement according to the invention.
  • the fiber bundle is inserted into the bore and groove and glued therein.
  • an adhesive is first introduced into the bore and into the at least one groove.
  • the fiber bundle which is preferably impregnated with a resin beforehand, is then introduced into the bore in such a way that a section of the fiber bundle protrudes beyond the bore.
  • the section of the fiber bundle protruding beyond the bore usually also protrudes beyond the surface of the supporting structure.
  • the section of the fiber bundle which, however, is located in a groove in the assembled arrangement then does not protrude more beyond the surface of the supporting structure, whereby a uniform and smooth surface can be guaranteed.
  • This protruding section of the fiber bundle is at least partially inserted into the groove provided with adhesive or evenly divided into a number of fiber strands corresponding to the number of grooves and inserted into the grooves. Most preferably, the entire fiber bundle or all fiber strands are inserted into one or more grooves, so that the fiber bundle does not protrude at any point beyond the surface of the support structure.
  • the fiber bundle can be pressed into it. Adhesive that oozes out of the borehole or from the groove is then removed or evenly distributed in the area of the surface affected by the arrangement. If there are still cavities in the bore or in the at least one groove after the fiber bundle has been inserted, these can be filled with adhesive.
  • the fiber bundle is introduced into the bore in particular with a needle-like object.
  • a clamp, a cable tie or the like, on which the needle-like object can be hooked can be attached to the fiber bundle.
  • Impregnating the fiber bundle with a resin before inserting it into the bore and groove has the advantage that the entire fiber bundle can be wetted with resin, even in the inner area.
  • the resin for impregnating the fiber bundle has, in particular, the same chemical basis as the adhesive for fastening the fiber bundle in the bore and groove.
  • both the resin and the adhesive are epoxy resin compositions. It is possible for the adhesive and the resin to have the same composition, the viscosity of the resin typically being set somewhat lower than that of the adhesive, which in turn serves to improve the wetting of the fibers.
  • a two-component epoxy resin composition is preferably used both for the adhesive for fastening the fiber bundle in the bore and groove and for the resin for any impregnation of the fiber bundle.
  • Suitable epoxy resin compositions are, for example, commercially available under the trade name Sikadur® from Sika Buch AG.
  • the bonding points on the supporting structure are preferably clean, dry, and free of dust and grease.
  • suitable cleaning measures or pretreatments can be applied.
  • the arrangement according to the invention can be attached to a support structure for different purposes.
  • the arrangement itself serves as a reinforcement for the supporting structure and / or it serves as an anchor or anchoring for a surface reinforcement attached to the supporting structure.
  • the arrangement itself can serve to reinforce a supporting structure.
  • the arrangement according to the invention can have a plurality of grooves, as described above.
  • the arrangement has a second bore which runs into the inner region of the support structure, the second bore being on a different surface of the surface.
  • the at least one groove runs from the entry point of the one, i.e. the first, bore along the surface the support structure to the entry point of the second bore, the two bores are therefore connected to one another in the surface area of the support structure via the at least one groove. Since the two bores are not located on the same area of the surface of the support structure, i.e.
  • the at least one groove also runs over these edges.
  • the two bores are located on mutually opposite surfaces of the support structure, and the two bores are connected to one another in the extension of their respective drilling axes.
  • the two holes can be created by drilling through the wall in one place.
  • a groove is then made in particular in such a way that it connects the entry point and the exit point of the bore in the wall with one another across the end face.
  • the exit point of one hole in the wall represents the entry point of the second hole.
  • a surface reinforcement can be attached to the surface of the supporting structure.
  • the surface reinforcement is preferably attached in such a way that it extends in at least one groove on the surface of the supporting structure Section of the fiber bundle and the hole or the entry point of the hole in the surface covers as a whole and is glued to the surface of the support structure over this entire area.
  • Particularly suitable surface reinforcement are lamellae or fabric which run along the surface of a supporting structure and are glued to it, in particular over the entire area.
  • Particularly suitable slats are unidirectional fiber-reinforced plastic flat strip slats.
  • the fiber reinforcement is usually done with carbon fibers, but like with the fiber bundle, it can also be done with glass, basalt or aramid.
  • an epoxy resin matrix is used as the plastic matrix.
  • a plastic matrix can likewise suitably be based on polyurethane, vinyl ester, polyacrylate or other compositions which have structural properties.
  • Suitable fiber-reinforced plastic flat strip lamellae are commercially available, for example, under the trade name Sika® CarboDur® from Sika für AG.
  • a carbon fiber fabric in particular a unidirectional one, is preferably suitable as the fabric, it also being possible for this to consist of glass, basalt or aramid fibers.
  • the fabric is typically not already applied to the surface in a hardened plastic matrix, but provided with a hardenable composition before or after it is attached to the surface.
  • the curable composition is in particular an epoxy resin composition, in which case polyurethane or polyacrylate could also be used here.
  • a carbon fiber fabric such as is commercially available from Sikatician AG, for example under the name SikaWrap®, is particularly suitable as the fabric.
  • Both as a plastic matrix for the fiber-reinforced plastic flat strip lamellae and for gluing these or the fabric to the supporting structure are preferably two-component Epoxy resin compositions used, such as are commercially available, for example, under the trade name Sikadur® from Sika Nurse AG.
  • the fiber bundle runs in the at least one groove over edges which connect different areas of the surface of the support structure to one another.
  • This edge preferably has a rounding in the interior of the groove.
  • the radius of the rounding is in particular about 0.5 to 10 cm, in particular 1 to 5 cm.
  • the rounding of the edge protects the fiber bundle that is inserted in the bore and groove, which means that there are fewer fiber breaks and improved power transmission is possible.
  • all edges of the support structure over which a groove with a fiber bundle is to run are rounded within the groove.
  • the transition from the bore into the groove also has a rounding as described above.
  • the arrangement according to the invention is typically used in the reinforcement of existing supporting structures, for example in renovation, repair or in the case of earthquake reinforcement subsequently attached to supporting structures. If the supporting structure is a reinforced concrete structure, the reinforcement takes place, for example, where the steel reinforcement is inadequate or where it has been damaged by an unforeseen event.
  • Figure 1A shows a section through a support structure 1 with a surface consisting of several surfaces 2a, 2b, 2c, with a bore 3 extending from surface 2a into an inner region of the support structure.
  • This bore is filled with an adhesive 12 and with a portion of a fiber bundle 4 protruding beyond this bore Face extends in one direction on the surface.
  • the part of the fiber bundle 4 protruding beyond the bore is located in the groove 5 and is fastened therein with adhesive 12.
  • Figure 1B shows a top view of the in Figure 1A The arrangement shown, not according to the invention, wherein a single groove 5 extends from the bore 3 in one direction on the surface. Furthermore, the entire protruding part of the fiber bundle is located in the groove and is fastened therein with adhesive 12.
  • Figure 1C also shows a plan view of the in Figure 1A arrangement shown, wherein in this embodiment several grooves 5 extend from the bore 3 in different directions on the surface.
  • the protruding part of the fiber bundle 4 is divided into fiber strands, these fiber strands preferably having approximately the same thickness, and the fiber strands are located in the grooves and are fixed therein with adhesive 12.
  • FIGS Figures 2A and 2B shows essentially an analogous embodiment not according to the invention as shown in FIGS Figures 1A and 1C is shown, wherein the plurality of grooves 5, starting from the bore 3, extend radially on the surface of the support structure 1.
  • the section of the fiber bundle which is located in the bore is in particular one of the two loose ends of the fiber bundle.
  • the other loose end of the fiber bundle represents that part of the fiber bundle which protrudes beyond the bore or which is located in the groove or the grooves and is attached there.
  • Figure 2C shows an embodiment not according to the invention, in which a central section of the fiber bundle is located in the bore.
  • the support structure 1 shown here has a surface consisting of several surfaces 2a, 2b, 2c, etc. and a first bore 3a, which extends from the surface 2a into the inner region of the support structure.
  • the second bore 3b runs from the surface 2b into the inner region of the supporting structure.
  • the surface 2b faces away from the surface 2a and the two bores 3a and 3b are arranged in such a way that they are connected to one another in the extension of their respective drilling axes.
  • the two bores can be created in that the support structure is pierced from a surface and the second bore thus represents the exit point of the first bore.
  • the holes 3a and 3b are with an adhesive 12 and filled with a section of a fiber bundle 4. In particular, this
  • Embodiment a fiber bundle is arranged in the bore in such a way that its central section is located in the bore and that its loose ends each protrude beyond the surface of the support structure.
  • a plurality of grooves 5 each extend from the bores 3a and 3b in different directions on the surface, for example in the manner as shown in FIG Figure 2B is shown.
  • the protruding parts of the fiber bundle 4 are divided into fiber strands and the fiber strands are located in the grooves and are fixed therein with adhesive.
  • FIG. 3A Cross-section
  • FIG. 3B top view shows an embodiment of the arrangement which is not according to the invention.
  • a surface 2a of the surface of a support structure 1 has several bores 3, which run into the inner area of the support structure 1, and a single groove 5 for each bore, which extends along the surface (see also FIG Figure 1B ).
  • the bores 3 and the grooves 5 are offset from one another, but in their entirety are attached linearly to the surface.
  • a lamella 6 is attached as surface reinforcement over the grooves 5 with the sections of the fiber bundles 4, this lamella being glued to the surface of the supporting structure at least in this area. In particular, such a lamella is glued over the entire surface to the surface of the support structure.
  • FIG. 11 shows a plan view of an arrangement not according to the invention, which is essentially that of FIG Figure 1C corresponds, with a fabric 7 being attached as surface reinforcement over the grooves 5, which extend from the bore 3 and are provided with fiber strands of the fiber bundle 4 and with adhesive.
  • a fabric is also preferably glued over the entire area to the surface of the support structure. The gluing of the fiber bundle glued into the grooves leads to an improved transmission of force between the supporting structure and the fabric, that is to say the surface reinforcement.
  • FIGS Figures 1C and 3C shown An embodiment of the arrangement not according to the invention as shown in FIGS Figures 1C and 3C shown is still in the Figure 3D shown.
  • the bore 3, which runs into the inner area of the supporting structure is located at a joint between two flat elements of a supporting structure, for example at a joint between two walls or between wall and base plate.
  • a surface reinforcement in the form of a fabric 7 is attached over the anchor area.
  • FIG Figure 3E Another embodiment not according to the invention is shown in FIG Figure 3E shown.
  • the support structure 1 shown here has a surface consisting of several surfaces 2a, 2b, 2c and a first bore 3a, which extends from the surface 2a into the inner region of the support structure.
  • the second bore 3b runs from the surface 2b into the inner region of the supporting structure.
  • the surface 2b faces away from the surface 2a and the two bores 3a and 3b are arranged in such a way that they are connected to one another in the extension of their respective drilling axes.
  • the two bores can be created in that the support structure is pierced from a surface and the second bore thus represents the exit point of the first bore.
  • the bores 3a and 3b are filled with an adhesive (not shown) and with a section of a fiber bundle 4.
  • a fiber bundle is arranged in the bore in such a way that its central section is located in the bore and that its loose ends each protrude beyond the surface of the support structure.
  • a plurality of grooves 5 each extend from the bores 3a and 3b in different directions on the surface.
  • the protruding parts of the fiber bundle 4 are divided into fiber strands and the fiber strands are located in the grooves and are fixed therein with adhesive.
  • a fabric 7 is attached over the described arrangements, which runs over the end face of the support structure and is glued to the support structure in the area of the grooves running from the entry point of the bore 3a to that of the bore 3b.
  • FIG. 3F Cross-section
  • 3G top view
  • a T-shaped support structure with a surface comprising a plurality of surfaces 2a, 2b, etc. at the joint between its two flat elements has two bores 3a and 3b which connect the surfaces 2a and 2b to one another.
  • the fiber bundle 4 is arranged in the bore in such a way that its central section is located in the bore and that its loose ends each protrude beyond the surface of the support structure.
  • Several grooves 5 each run in different directions on the surface from the bores.
  • the protruding parts of the fiber bundle 4 are divided into fiber strands and the fiber strands are located in the grooves and are fixed therein with adhesive.
  • the supporting structure 1 is a concrete slab 10 which has several reinforcing ribs 11, that is to say T-shaped sections.
  • the reinforcement ribs 11 had holes 3 in the area of their abutment points with the concrete slab 10, these being laid out in such a way that two holes in each case are connected to one another in the extension of their drilling axes. Starting from the entry point of the respective borehole 3, several grooves run along the surface of the concrete slab.
  • boreholes and grooves are filled with a fiber bundle or with fiber strands of the fiber bundle and adhesive.
  • a surface reinforcement in the form of a fabric 7 is attached over the surfaces of the concrete slab, which are located between the reinforcement ribs 11. In particular, this fabric is glued over the entire surface to the underlying surface.
  • FIGS Figures 4A (Cross-section) and 4B (top view) shows a further embodiment not according to the invention, in which arrangements, such as are for example in FIGS Figures 2A and 2B are shown, are attached to a support structure 1 at regular intervals.
  • the arrangements can be attached to one area of the surface of the support structure or to several areas.
  • a fabric 7 is also glued at least to the arrangements, but in particular over the entire area, to the surface of the support structure.
  • the fabric can run continuously over corners and edges in the surface of the support structure.
  • Figure 5A shows a section through an embodiment not according to the invention of an arrangement with a support structure 1 with a surface consisting of several surfaces 2a, 2b, 2c, etc. and a first bore 3a, which runs from the surface 2a into the inner area of the support structure.
  • the second bore 3b runs from the surface 2b into the inner region of the supporting structure.
  • the surface 2b faces away from the surface 2a.
  • a groove 5 runs from one bore 3a along the surface of the support structure to the point of entry of the other bore into the support structure. The groove, which thus connects the two entry holes of the bores with one another, runs in particular on the shortest path between the two bores.
  • the groove takes a different course between the bores, for example in order to ensure the most uniform possible force distribution.
  • a fiber bundle 4 runs in the groove 5, which ends with its loose ends in the two bores 3a and 3b. Both the bores and the groove contain adhesive 12 for fastening the fiber bundle.
  • FIG Figure 5A A similar embodiment not according to the invention as in FIG Figure 5A is also in Figure 5B shown, the fiber bundle here wrapping around a reinforcing rib 11 of a supporting structure 1.
  • Figure 6A shows a section through an embodiment according to the invention, which is a modification of the embodiment not according to the invention Figure 5A is equivalent to.
  • the embodiment in Figure 6A two bores 3a, 3b in different, mutually facing away surfaces 2a, 2b of the surface of the support structure, the two bores 3a and 3b being arranged so that they are connected to one another in the extension of their respective drilling axes.
  • the entry holes of the two Bores 3a and 3b are as in Figure 5A connected to one another via a groove 5.
  • Both the bores 3a, 3b and the groove 5 contain an adhesive 12 and a fiber bundle 4.
  • the fiber bundle is in particular arranged in such a way that its two ends overlap. This overlap can be in the bore or at any point in the groove.
  • the length of the overlapping area of the fiber bundle is in particular selected in such a way that the transmission of force as seamless as possible is guaranteed and is approximately 5 to 50 cm.
  • the two bores 3a and 3b are arranged so that they are connected to each other in the extension of their respective drilling axes, and the fiber bundle can be arranged so that its two ends at least overlap.
  • the fiber bundle forms a closed loop, as a result of which the transmission of the thrust force takes place between the two ends of the fiber bundle, i.e. within the same material, which is critical for contact.
  • the preferred embodiments allow a higher efficiency of the reinforcement and a significantly better utilization of the fiber bundle.
  • Figures 6B and 6C show modifications of the embodiment according to the invention as shown in FIG Figure 6A is described. Arrangements according to the invention are shown here, such as can be used, for example, to reinforce a rectangular column as part of a support structure.
  • Figure 6C shows that it is also possible for the fiber bundle 4 to be guided several times through a bore, but to run in two different grooves from the entry point of the first bore to that of the second bore. on the other hand can make the embodiment Figure 6C can also be created by the part of the fiber bundle protruding beyond the bore is divided into two fiber strands, which then run in different grooves.
  • Figure 6D shows a modification of the embodiment shown in FIG Figure 5B is shown, the fiber bundle 4 completely wrapping around the reinforcing rib 11 here.
  • FIG. 11 shows a side view of a support structure which the in FIGS Figures 6A, 6B and 6C includes variants of the arrangement according to the invention shown. Depending on the requirements, the different variants can be combined with one another or several identical arrangements can be attached to a supporting structure.
  • Figure 6G shows support structure 1 comprising a base plate 10 and a wall created thereon, the wall being provided in its lower area with several arrangements according to the invention, which consist of those from Figure 6A correspond.
  • a fabric for additional reinforcement of the supporting structure can be attached via these arrangements (not shown here).
  • Figure 6F shows a cylindrical column which comprises several arrangements not according to the invention.
  • Figure 7A shows a detailed view of a section of a support structure 1 with a surface consisting of several surfaces 2a, 2b, 2c, with a bore 3 extending from one surface 2a into an inner region of the support structure.
  • the support structure 1 is provided with a groove 5 on the surface 2a, from which the bore extends into an inner region of the support structure, which, starting from the bore, extends in one direction on the surface.
  • the groove 5 runs over an edge 8, which connects the two surfaces 2a and 2c, or 2c and 2b of the surface of the supporting structure with one another, and this one edge 8 has a rounding 9 inside the groove 5.
  • Figure 7B shows a section through a region of a support structure 1, which has two bores 3a, 3c in different, mutually facing away surfaces 2a, 2c of the surface of the support structure, the two Bores 3a and 3c are arranged so that they are connected to one another in the extension of their respective drilling axes.
  • the entry holes of the two bores 3 a and 3 b are connected to one another via a groove 5.
  • the edges 8 each have a rounding 9.
  • the respective transitions from the bore into the groove can have a rounding according to the preceding description.
  • Concrete cubes with an edge length of 20 cm were produced as test specimens, with concrete from the same batch being used for all cubes.
  • the concrete cubes were stored for 28 days at 23 ° C and 50% relative humidity.
  • the concrete cubes were sanded down on one side to remove cement slurry.
  • a hole with a diameter of 20 mm and a depth of 100 mm was made in the center of the treated area.
  • Two concrete cubes were left without drilling. Starting from the borehole, eight grooves were made evenly around the borehole with an angle grinder on the concrete cubes. The grooves were 5 mm wide and 5 mm deep and extended over a length of 8 cm. The angle between the grooves was 45 ° in each case.
  • Sikadur®-330 commercially available from Sika Nurse AG, with an average layer thickness of approx. 1 mm was applied to the machined surface of the concrete cubes without drilling. With the concrete cubes The bore was filled with Sikadur®-330 from the bottom up and the grooves. Care was taken to ensure that no air was trapped in the borehole.
  • a fiber bundle with a length of 20 cm and a fiber cross-sectional area of about 25 mm 2 was completely impregnated with Sikadur® 300 from Sika für AG using a brush.
  • a cable tie was then attached to a loose end of the impregnated fiber bundle, tightened and cut to length. With the help of a knitting needle, which was hooked into the cable tie, the fiber bundle was inserted into the hole as far as it would go.
  • the protruding end of the fiber bundle was divided into fiber strands, whereby the number of fiber strands had to correspond to that of the previously made grooves, and placed in the grooves. In the case of the concrete cubes without grooves, the protruding end of the fiber bundle was evenly fanned out and spread over the machined surface of the concrete cube.
  • the Sikadur®-330 fiber bundle was then evenly distributed over the grooves on the processed surface of the concrete cube, so that the entire processed surface was covered with sufficient adhesive.
  • a fabric made of SikaWrap® 300 C NW (width 20 cm, length 180 cm) provided was laminated with Sikadur®-300 in the area of the last 20 cm of its loose ends using a paint roller.
  • a laminated loose end was placed on the machined surface of the concrete cube and pressed there with a paint roller.
  • Sikadur®-330 was applied over the attached tissue using a notched trowel.
  • the fabric was put in a loop and the other loose and laminated end was placed on the same spot on the concrete cube so that the two ends of the fabric lay on top of each other. Again the fabric was pressed on with the paint roller.
  • Excess adhesive was removed from the test specimen with a spatula the width of the concrete cube.
  • test specimens produced in this way were left at 23 ° C. and 50% relative humidity for 7 days so that the adhesive could cure.
  • Test specimens with fiber bundles made of glass fibers with a fiber cross-sectional area of about 25 mm 2 were also produced in the same way.
  • the tensile shear strength of different test specimens was measured according to ISO 527-4 / EN 2561 with a measuring speed of 2 mm / min at 23 ° C. and a relative humidity of 50%.
  • the tensile shear strength of the bond was tested by placing the loop formed by the SikaWrap-300C NW fabric around a steel tube connected to the movable frame of the testing machine.
  • the concrete cube was connected to the fixed frame of the testing machine via a steel crossbeam and threaded rods.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Mechanical Engineering (AREA)
  • Reinforcement Elements For Buildings (AREA)
  • Working Measures On Existing Buildindgs (AREA)
  • Bridges Or Land Bridges (AREA)
  • Foundations (AREA)

Description

Technisches GebietTechnical area

Die Erfindung betrifft das Gebiet der Verstärkung von Tragstrukturen, vorzugsweise durch Anbringen von Oberflächenbewehrung, insbesondere der Krafteinleitung in die Oberflächenbewehrung.The invention relates to the field of reinforcement of supporting structures, preferably by applying surface reinforcement, in particular the introduction of forces into the surface reinforcement.

Stand der TechnikState of the art

Verfahren, um den Tragwiderstand bestehender Tragstrukturen, typischerweise Stahlbetonbauteile, zu vergrössern, werden bereits seit vielen Jahren verwendet. Oftmals geschieht dies mittels oberflächlich angebrachter zusätzlicher Bewehrung. Weitgehend durchgesetzt haben sich dabei überwiegend oberflächlich aufgeklebte Bewehrungen aus Faserverbundwerkstoffen. Die Wirksamkeit dieser Oberflächenbewehrung wird im Normalfall durch die maximal vom Beton auf die Bewehrung übertragbare Kraft begrenzt.Methods to increase the load-bearing resistance of existing load-bearing structures, typically reinforced concrete components, have been used for many years. Often this is done by means of additional reinforcement attached to the surface. Reinforcements made of fiber composite materials that are glued to the surface have largely prevailed. The effectiveness of this surface reinforcement is normally limited by the maximum force that can be transferred from the concrete to the reinforcement.

Verschiedenste Methoden zur Verbesserung der Kraftübertragung von der Tragstruktur auf die Oberflächenbewehrung sind bekannt. Ein weit verbreitetes Verfahren besteht darin, Faserbündel in eine Bohrung in der Tragstruktur einzuführen und dort zu verankern und ein über die Oberfläche überstehendes Ende des Faserbündels auszubreiten bzw. auszufächern und auf der Oberfläche aufzukleben. Anschliessend kann dann eine Oberflächenbewehrung auf die verstärkte Tragwerksoberfläche aufgeklebt werden. Alternativ kann zuerst auch die Oberflächenbewehrung auf die Tragwerksoberfläche aufgeklebt werden, sodass bei einem danach angebrachten Anker aus einem Faserbündel, das überstehende Ende dieses auf die Oberfläche der Oberflächenbewehrung aufgeklebt wird. Bei Oberflächenbewehrungen mit mehreren Lagen wird zur besseren Kraftübertragung vielfach empfohlen, die Anker zwischen den Gewebelagen auszubreiten.Various methods for improving the power transmission from the supporting structure to the surface reinforcement are known. A widely used method consists in inserting fiber bundles into a hole in the support structure and anchoring them there and spreading out or fanning out an end of the fiber bundle protruding beyond the surface and gluing it onto the surface. A surface reinforcement can then be glued to the reinforced structure surface. Alternatively, the surface reinforcement can first be glued to the structure surface so that when an anchor made from a fiber bundle is attached afterwards, the protruding end of this is glued to the surface of the surface reinforcement. In the case of surface reinforcement with several layers, it is often recommended to spread the anchors between the fabric layers for better power transmission.

Die Wirksamkeit dieser Massnahme ist experimentell nachgewiesen bleibt jedoch aus verschiedenen Gründen beschränkt.The effectiveness of this measure has been proven experimentally, but remains limited for various reasons.

Einerseits wird die oberflächennahe potenzielle Bruchfläche von jedem Anker nur an einer Stelle (beim Schaft) durchbrochen. Der Widerstand dieser potenziellen Bruchfläche wird damit nur in beschränktem Mass vergrössert. Andererseits ist die Kraftübertragung von den auf der Oberfläche ausgebreiteten Fasern des Faserbündels auf die Fasern des Gewebes nicht optimal. Der sehr dünne, von den Fasern des Faserbündels auf der Oberfläche gebildete Faserverbundwerkstoff kann nur in Zugrichtung wesentlich belastet werden. Bei Belastung auf Druck knickt der Faserverbundwerkstoff, bei Belastung auf Schub und Biegung können nur sehr geringe Kräfte übertragen werden. Es sind daher nur die annähernd in Zugrichtung der Oberflächenbewehrung liegenden Fasern voll wirksam. Diese machen nur einen kleinen Teil des Fasebündelquerschnitts aus und decken nur einen kleinen Teil der Breite der Oberflächenbewehrung ab.On the one hand, the potential fracture surface near the surface is only broken through by each anchor at one point (on the shaft). The resistance of this potential fracture surface is only increased to a limited extent. On the other hand, the power transmission from the fibers of the fiber bundle spread out on the surface to the fibers of the fabric is not optimal. The very thin fiber composite material formed by the fibers of the fiber bundle on the surface can only be significantly loaded in the tensile direction. When subjected to pressure, the fiber composite material kinks; when subjected to shear and bending, only very small forces can be transmitted. Therefore, only the fibers lying approximately in the tensile direction of the surface reinforcement are fully effective. These make up only a small part of the fiber bundle cross-section and only cover a small part of the width of the surface reinforcement.

Ein weiterer Nachteil des bekannten Verfahrens liegt darin, dass das über die Oberfläche überstehende Ende des Faserbündels auf der Oberfläche selbst ausgebreitet ist und somit durch Vorsprünge, überstehende Verformungen an der Oberfläche verursacht werden, welche einerseits die Optik eines Bauwerks stören können, andererseits aber auch technische Nachteile mit sich bringen können. Beispielsweise können Erhebungen in einer sonst ebenen Oberfläche dazu führen, dass Wasser, insbesondere Regenwasser, oder Schnee, aber auch Schmutz sich an diesen Erhebungen ansammeln und die langfristige Wirkung beeinträchtigen.Another disadvantage of the known method is that the end of the fiber bundle protruding over the surface is spread out on the surface itself and is thus caused by protrusions, protruding deformations on the surface, which on the one hand can disturb the appearance of a building, but on the other hand also technical Can have disadvantages. For example, elevations in an otherwise flat surface can lead to water, in particular rainwater, or snow, but also dirt, accumulating on these elevations and impairing the long-term effect.

US 6 324 805 B1 offenbart eine Anordnung mit den Merkmalen des einleitenden Teils des Anspruchs 1. US 6,324,805 B1 discloses an arrangement having the features of the introductory part of claim 1.

Darstellung der ErfindungPresentation of the invention

Die Aufgabe der vorliegenden Erfindung ist es daher eine Anordnung bereitzustellen, wonach eine Verbesserung der Krafteinleitung in eine Oberflächenbewehrung erreicht werden soll.The object of the present invention is therefore to provide an arrangement according to which an improvement in the introduction of force into a surface reinforcement is to be achieved.

Weiterhin ist es die Aufgabe der vorliegenden Erfindung die Kraftübertragung von Faserbündeln, welche an einem Tragwerk angebracht sind, insbesondere in einen Oberflächen- oder in einen oberflächennahen Bereich zu verbessern.Furthermore, it is the object of the present invention to improve the power transmission of fiber bundles which are attached to a supporting structure, in particular in a surface area or in an area close to the surface.

Überraschenderweise wurde gefunden, dass mittels einer Anordnung nach Anspruch 1 diese Aufgabe gelöst werden kann.It has surprisingly been found that this object can be achieved by means of an arrangement according to claim 1.

Kern der Erfindung ist demnach eine Anordnung umfassend eine Tragstruktur mit einer Oberfläche bestehend aus mehreren Flächen, wobei von einer Fläche aus eine Bohrung in einen inneren Bereich der Tragstruktur verläuft, und diese Bohrung mit einem Klebstoff und mit einem Abschnitt eines über diese Bohrung hinausragenden Faserbündels gefüllt ist, wobei die Tragstruktur an der einen Fläche, von welcher aus die Bohrung in einen inneren Bereich der Tragstruktur verläuft, mit mindestens einer Nut versehen ist, welche sich ausgehend von der Bohrung in mindestens eine Richtung auf der Oberfläche erstreckt und sich der hinausragende Teil des Faserbündels zumindest teilweise in der mindestens einen Nut befindet und darin mit dem Klebstoff befestigt ist.The essence of the invention is accordingly an arrangement comprising a support structure with a surface consisting of several surfaces, with a bore running from one surface into an inner area of the support structure, and this bore is filled with an adhesive and with a section of a fiber bundle protruding beyond this bore is, wherein the support structure is provided on the one surface from which the bore extends into an inner region of the support structure with at least one groove which extends from the bore in at least one direction on the surface and the protruding part of the Fiber bundle is at least partially located in the at least one groove and is fixed therein with the adhesive.

Als Tragstruktur wird hier ein Element oder ein Teil eines Elements bezeichnet, welches Kräften ausgesetzt ist. Typischerweise ist die Tragstruktur ein Bauwerk oder ein Bestandteil eines Bauwerks, beispielsweise eine Platte, eine Decke, eine Wand, eine Säule, eine Rippe, ein Balken oder dergleichen. Die Tragstruktur besteht dabei typischerweise aus Beton, insbesondere aus Stahlbeton, kann aber auch aus Ziegel- oder anderen Mauersteinen, aus Holz, aus Stahl oder aus anderen Materialien sowie aus beliebigen Kombinationen dieser Materialien bestehen. Typischerweise handelt es sich bei den Bauwerken um Bauwerke des Hoch- und Tiefbaus, wie Häuser, Brücken, Tunnels, Staudämmen, Sportanlagen, etc.An element or part of an element that is exposed to forces is referred to here as a support structure. The supporting structure is typically a building or a component part of a building, for example a plate, a ceiling, a wall, a column, a rib, a beam or the like. The supporting structure typically consists of concrete, in particular reinforced concrete, but can also consist of bricks or other bricks, wood, steel or other materials and any combination of these materials. Typically, the structures are civil engineering structures such as houses, bridges, tunnels, dams, sports facilities, etc.

Beim Faserbündel handelt es sich um eine lose Anordnung von im Wesentlichen gleichgerichteten Einzelfasern bzw. Filamenten, insbesondere aus Kohle (Carbon), Glas, Basalt, Aramid, Stahl oder anderen anorganischen oder organischen Materialien. Bevorzugt handelt es sich bei den Fasern um Kohlefasern.The fiber bundle is a loose arrangement of essentially unidirectional individual fibers or filaments, in particular made of carbon, glass, basalt, aramid, steel or other inorganic or organic materials. The fibers are preferably carbon fibers.

Der Stärke des Faserbündels ist abhängig vom Einsatzbereich und von den Kräften, welche durch das Faserbündel übertragen werden sollen. Besteht das Faserbündel aus Kohlefasern, umfasst dieses insbesondere 1000 bis 50'000 Einzelfasern, welche jeweils selbst einen Durchmesser im Bereich von 5 bis 10 µm aufweisen. Ein typisches Faserbündel weist vorzugsweise eine Querschnittsfläche von 20 bis 70 mm2, insbesondere von 25 bis 40 mm2, auf.The strength of the fiber bundle depends on the area of application and the forces that are to be transmitted through the fiber bundle. If the fiber bundle consists of carbon fibers, it comprises in particular 1000 to 50,000 individual fibers, each of which has a diameter in the range from 5 to 10 µm. A typical fiber bundle preferably has a cross-sectional area of 20 to 70 mm 2 , in particular 25 to 40 mm 2 .

Das Anbringen des Faserbündels an der Tragstruktur erfolgt typischerweise dadurch, dass in einem ersten Schritt an der gewünschten Stelle eine Bohrung angebracht wird, welche der Aufnahme eines Abschnitts des Faserbündels dient. Die Bohrung kann dabei mit beliebigen Mitteln erstellt werden, wobei solche Mittel dem Fachmann bestens bekannt sind. Die Dimensionen der Bohrung ergeben sich aus der Stärke und der Länge des Faserbündels und diese wiederum von den Anforderungen, welche an die erfindungsgemässe Anordnung gestellt werden. Typischerweise weist eine geeignete Bohrung einen Durchmesser von 1 bis 5 cm, insbesondere von 1.5 bis 3 cm auf und eine Tiefe von 5 bis 30 cm, insbesondere von 7 bis 20 cm.
In einem weiteren Schritt wird ausgehend von der Bohrung bzw. von der Eintrittsstelle der Bohrung in die Oberfläche der Tragstruktur eine oder mehrere Nuten angebracht. Auch die Nuten können mit beliebigen Mitteln erstellt werden, beispielsweise mit einem Winkelschleifer.
Die Nut oder die Nuten sind dabei so dimensioniert, dass sie in ihrer Gesamtheit das Faserbündel, welches im Fall, dass mehrere Nuten vorhanden sind, in einzelne Faserstränge aufgeteilt sein kann, aufnehmen können.
Die Anzahl und Anordnung der Nuten ist dabei abhängig vom Einsatzbereich der erfindungsgemässen Anordnung.
The attachment of the fiber bundle to the support structure typically takes place in that, in a first step, a bore is made at the desired location, which hole serves to receive a section of the fiber bundle. The bore can be created by any means, such means being very well known to the person skilled in the art. The dimensions of the bore result from the strength and the length of the fiber bundle and these in turn from the requirements which are placed on the arrangement according to the invention. A suitable bore typically has a diameter of 1 to 5 cm, in particular 1.5 to 3 cm, and a depth of 5 to 30 cm, in particular 7 to 20 cm.
In a further step, starting from the bore or from the entry point of the bore into the surface of the support structure, one or more grooves are made. The grooves can also be created by any means, for example with an angle grinder.
The groove or grooves are dimensioned in such a way that they can accommodate the fiber bundle in their entirety, which can be divided into individual fiber strands in the event that several grooves are present.
The number and arrangement of the grooves is dependent on the area of application of the arrangement according to the invention.

Nach Anbringen der Bohrung und der mindestens einen Nut wird das Faserbündel in Bohrung und Nut eingelegt und darin verklebt. Hierzu wird zuerst ein Klebstoff in die Bohrung und in die mindestens eine Nut eingebracht. Danach wird das Faserbündel, welches vorab vorzugsweise mit einem Harz getränkt ist, so in die Bohrung eingebracht, dass ein Abschnitt des Faserbündels über die Bohrung hinausragt. Im Verlauf des Anbringens der erfindungsgemässen Anordnung an einem Tragwerk ragt der über die Bohrung hinausragende Abschnitt des Faserbündels in der Regel auch über die Oberfläche der Tragstruktur hinaus. Der Abschnitt des Faserbündels, welcher sich jedoch bei der montierten Anordnung in einer Nut befindet, ragt dann nicht mehr über die Oberfläche der Tragstruktur hinaus, wodurch eine einheitliche und glatte Oberfläche gewährleistet werden kann.After the bore and the at least one groove have been made, the fiber bundle is inserted into the bore and groove and glued therein. For this purpose, an adhesive is first introduced into the bore and into the at least one groove. The fiber bundle, which is preferably impregnated with a resin beforehand, is then introduced into the bore in such a way that a section of the fiber bundle protrudes beyond the bore. In the course of the attachment of the arrangement according to the invention to a supporting structure, the section of the fiber bundle protruding beyond the bore usually also protrudes beyond the surface of the supporting structure. The section of the fiber bundle which, however, is located in a groove in the assembled arrangement, then does not protrude more beyond the surface of the supporting structure, whereby a uniform and smooth surface can be guaranteed.

Dieser hinausragende Abschnitt des Faserbündels wird zumindest teilweise in die mit Klebstoff versehene Nut eingelegt bzw. gleichmässig in eine der Anzahl der Nuten entsprechenden Anzahl Faserstränge aufgeteilt und in die Nuten eingelegt. Meist bevorzugt werden das gesamte Faserbündel bzw. alle Faserstränge in eine oder mehrere Nuten eingelegt, so dass das Faserbündel an keiner Stelle über die Oberfläche der Tragstruktur hinausragt. Nach dem Einlegen des Faserbündels in die mindestens eine Nut, kann das Faserbündel darin angedrückt werden. Aus dem Bohrloch oder aus der Nut hervorquellender Klebstoff wird danach entfernt oder gleichmässig im Bereich der von der Anordnung betroffenen Oberfläche verteilt. Befinden sich nach dem Einlegen des Faserbündels noch Hohlräume in der Bohrung oder in der mindestens einen Nut, können diese mit Klebstoff ausgefüllt werden.
Das Einführen des Faserbündels in die Bohrung erfolgt insbesondere mit einem nadelartigen Gegenstand. Am Faserbündel kann zur besseren Führung mit dem nadelartigen Gegenstand eine Klammer, ein Kabelbinder oder dergleichen angebracht sein, an welchem der nadelartige Gegenstand eingehakt werden kann.
Das Tränken des Faserbündels mit einem Harz vor dem Einlegen in Bohrung und Nut hat den Vorteil, dass die Benetzung des gesamten Faserbündels mit Harz, auch im inneren Bereich, erreicht werden kann. Zur Gewährleistung einer optimalen Haftung zwischen Faserbündel und Tragstruktur weist das Harz zum Tränken des Faserbündels insbesondere die gleiche chemische Basis auf wie der Klebstoff zum Befestigen des Faserbündels in Bohrung und Nut. Insbesondere handelt es sich sowohl beim Harz als auch beim Klebstoff um Epoxidharzzusammensetzungen. Es ist möglich, dass es sich beim Klebstoff und beim Harz um dieselbe Zusammensetzung handelt, wobei beim Harz die Viskosität typischerweise etwas niedriger eingestellt ist als beim Klebstoff, was wiederum der besseren Benetzung der Fasern dient.
This protruding section of the fiber bundle is at least partially inserted into the groove provided with adhesive or evenly divided into a number of fiber strands corresponding to the number of grooves and inserted into the grooves. Most preferably, the entire fiber bundle or all fiber strands are inserted into one or more grooves, so that the fiber bundle does not protrude at any point beyond the surface of the support structure. After the fiber bundle has been inserted into the at least one groove, the fiber bundle can be pressed into it. Adhesive that oozes out of the borehole or from the groove is then removed or evenly distributed in the area of the surface affected by the arrangement. If there are still cavities in the bore or in the at least one groove after the fiber bundle has been inserted, these can be filled with adhesive.
The fiber bundle is introduced into the bore in particular with a needle-like object. For better guidance with the needle-like object, a clamp, a cable tie or the like, on which the needle-like object can be hooked, can be attached to the fiber bundle.
Impregnating the fiber bundle with a resin before inserting it into the bore and groove has the advantage that the entire fiber bundle can be wetted with resin, even in the inner area. To ensure optimal adhesion between the fiber bundle and the support structure, the resin for impregnating the fiber bundle has, in particular, the same chemical basis as the adhesive for fastening the fiber bundle in the bore and groove. In particular, both the resin and the adhesive are epoxy resin compositions. It is possible for the adhesive and the resin to have the same composition, the viscosity of the resin typically being set somewhat lower than that of the adhesive, which in turn serves to improve the wetting of the fibers.

Sowohl beim Klebstoff zum Befestigen des Faserbündels in Bohrung und Nut als auch beim Harz zum allfälligen Tränken des Faserbündels wird bevorzugt eine zweikomponentige Epoxidharzzusammensetzung verwendet. Geeignete Epoxidharzzusammensetzungen sind beispielsweise unter den Handelsnamen Sikadur® kommerziell erhältlich sind von Sika Schweiz AG.A two-component epoxy resin composition is preferably used both for the adhesive for fastening the fiber bundle in the bore and groove and for the resin for any impregnation of the fiber bundle. Suitable epoxy resin compositions are, for example, commercially available under the trade name Sikadur® from Sika Schweiz AG.

Die Verklebungsstellen an der Tragstruktur sind vorzugsweise sauber, trocken, staub- und fettfrei. Abhängig von den Materialien, aus welchen die Tragstruktur besteht, können geeignete Reinigungsmassnahmen oder Vorbehandlungen angewendet werden.The bonding points on the supporting structure are preferably clean, dry, and free of dust and grease. Depending on the materials from which the supporting structure is made, suitable cleaning measures or pretreatments can be applied.

Die erfindungsgemässe Anordnung kann für unterschiedliche Zwecke an einer Tragstruktur angebracht werden. Insbesondere dient dabei die Anordnung selbst als Verstärkung für die Tragstruktur und/oder sie dient als Anker bzw. als Verankerung für eine an der Tragstruktur angebrachten Oberflächenbewehrung.The arrangement according to the invention can be attached to a support structure for different purposes. In particular, the arrangement itself serves as a reinforcement for the supporting structure and / or it serves as an anchor or anchoring for a surface reinforcement attached to the supporting structure.

In einer weiteren Ausführungsform kann die Anordnung selbst zur Verstärkung einer Tragstruktur dienen. In diesem Fall werden insbesondere mehrere der beschriebenen Anordnungen in regelmässigen Abständen an einer Tragstruktur angebracht. Auch in diesem Fall kann die erfindungsgemässe Anordnung wie vorhergehend beschrieben mehrere Nuten aufweisen. Erfindungsgemäß weist die Anordnung eine zweite Bohrung auf, welche in den inneren Bereich der Tragstruktur verläuft, wobei sich die zweite Bohrung auf einer anderen Fläche der Oberfläche befindet, Die mindestens eine Nut verläuft dabei vom Eintrittsort der einen, also er ersten, Bohrung entlang der Oberfläche der Tragstruktur hin zum Eintrittsort der zweiten Bohrung, die beiden Bohrungen sind also im Oberflächenbereich der Tragstruktur über die mindestens eine Nut miteinander verbunden. Da sich die beiden Bohrungen nicht auf derselben Fläche der Oberfläche der Tragstruktur befinden, d.h. es liegt bzw. liegen also eine oder mehrere Kanten zwischen den Flächen, verläuft die mindestens eine Nut auch über diese Kanten. Erfindungsgemäß befinden sich die beiden Bohrungen an sich gegenseitig abgewandten Flächen der Tragstruktur, und die zwei Bohrungen sind in der Verlängerung ihrer jeweiligen Bohrachsen miteinander verbunden.In a further embodiment, the arrangement itself can serve to reinforce a supporting structure. In this case, in particular, several of the arrangements described are attached to a support structure at regular intervals. In this case as well, the arrangement according to the invention can have a plurality of grooves, as described above. According to the invention, the arrangement has a second bore which runs into the inner region of the support structure, the second bore being on a different surface of the surface. The at least one groove runs from the entry point of the one, i.e. the first, bore along the surface the support structure to the entry point of the second bore, the two bores are therefore connected to one another in the surface area of the support structure via the at least one groove. Since the two bores are not located on the same area of the surface of the support structure, i.e. there is or are one or more edges between the surfaces, the at least one groove also runs over these edges. According to the invention, the two bores are located on mutually opposite surfaces of the support structure, and the two bores are connected to one another in the extension of their respective drilling axes.

Beispielsweise ist dies der Fall, wenn die erfindungsgemässe Anordnung im Bereich der Stirnseite einer mindestens einseitig freistehenden Wand angebracht werden soll. In diesem Fall können die zwei Bohrungen dadurch erstellt werden, dass die Wand an einer Stelle durchbohrt wird. Eine Nut wird dann insbesondere so angebracht, dass sie den Eintrittsort und den Austrittsort der Bohrung in der Wand miteinander über die Stirnseite hinweg verbindet. Der Austrittsort der einen Bohrung in der Wand stellt dabei den Eintrittsort der zweiten Bohrung dar.This is the case, for example, when the arrangement according to the invention is to be attached in the area of the end face of a wall that is free on at least one side. In this case, the two holes can be created by drilling through the wall in one place. A groove is then made in particular in such a way that it connects the entry point and the exit point of the bore in the wall with one another across the end face. The exit point of one hole in the wall represents the entry point of the second hole.

Auch bei einem derartigen Einsatz der erfindungsgemässen Anordnung kann eine Oberflächenbewehrung an der Oberfläche der Tragstruktur angebracht werden.Even with such a use of the arrangement according to the invention, a surface reinforcement can be attached to the surface of the supporting structure.

Unabhängig von der Beschaffenheit der erfindungsgemässen Anordnung, wird die Oberflächenbewehrung vorzugsweise so angebracht, dass sie den sich an der Oberfläche der Tragstruktur in mindestens einer Nut verlaufenden Abschnitt des Faserbündels und die Bohrung bzw. den Eintrittsort der Bohrung in die Oberfläche gesamthaft abdeckt und über diesen gesamten Bereich mit der Oberfläche der Tragstruktur verklebt ist.Regardless of the nature of the arrangement according to the invention, the surface reinforcement is preferably attached in such a way that it extends in at least one groove on the surface of the supporting structure Section of the fiber bundle and the hole or the entry point of the hole in the surface covers as a whole and is glued to the surface of the support structure over this entire area.

Als Oberflächenbewehrung kommen insbesondere Lamellen oder Gewebe in Frage, welche entlang der Oberfläche einer Tragstruktur verlaufen und mit dieser, insbesondere vollflächig, verklebt sind. Als Lamellen eignen sich insbesondere unidirektional faserverstärkte Kunststoff-Flachbandlamellen. Die Faserverstärkung erfolgt üblicherweise durch Kohlefasern, kann jedoch wie beim Faserbündel auch, durch Glas, Basalt oder Aramid erfolgen. Als Kunststoffmatrix dient insbesondere eine Epoxidharzmatrix. Ebenfalls geeignet kann eine Kunststoffmatrix auf Polyurethan, Vinylester, Polyacrylat oder anderen Zusammensetzungen basieren, welche strukturelle Eigenschaften aufweisen. Geeignete faserverstärkte Kunststoff-Flachbandlamellen sind beispielsweise unter dem Handelsnamen Sika® CarboDur® kommerziell erhältlich sind von Sika Schweiz AG.
Als Gewebe eignet sich vorzugsweise ein, insbesondere unidirektionales, Kohlefasergewebe, wobei auch dieses aus Glas-, Basalt- oder Aramidfasern bestehen kann. Im Gegensatz zu den faserverstärkten Kunststoff-Flachbandlamellen, wird das Gewebe typischerweise nicht bereits in einer ausgehärteten Kunststoffmatrix auf die Oberfläche aufgetragen, sondern vor oder nach dem Anbringen an der Oberfläche mit einer härtbaren Zusammensetzung versehen. Bei der härtbaren Zusammensetzung handelt es sich insbesondere um eine Epoxidharzzusammensetzung, wobei auch hier Polyurethan oder Polyacrylat verwendet werden könnte.
Als Gewebe eignet sich insbesondere ein Kohlefasergewebe, wie es beispielsweise unter der Bezeichnung SikaWrap® kommerziell erhältlich ist von Sika Schweiz AG.
Particularly suitable surface reinforcement are lamellae or fabric which run along the surface of a supporting structure and are glued to it, in particular over the entire area. Particularly suitable slats are unidirectional fiber-reinforced plastic flat strip slats. The fiber reinforcement is usually done with carbon fibers, but like with the fiber bundle, it can also be done with glass, basalt or aramid. In particular, an epoxy resin matrix is used as the plastic matrix. A plastic matrix can likewise suitably be based on polyurethane, vinyl ester, polyacrylate or other compositions which have structural properties. Suitable fiber-reinforced plastic flat strip lamellae are commercially available, for example, under the trade name Sika® CarboDur® from Sika Schweiz AG.
A carbon fiber fabric, in particular a unidirectional one, is preferably suitable as the fabric, it also being possible for this to consist of glass, basalt or aramid fibers. In contrast to the fiber-reinforced plastic flat strip lamellas, the fabric is typically not already applied to the surface in a hardened plastic matrix, but provided with a hardenable composition before or after it is attached to the surface. The curable composition is in particular an epoxy resin composition, in which case polyurethane or polyacrylate could also be used here.
A carbon fiber fabric such as is commercially available from Sika Schweiz AG, for example under the name SikaWrap®, is particularly suitable as the fabric.

Sowohl als Kunststoffmatrix für die faserverstärkten Kunststoff-Flachbandlamellen als auch zur Verklebung dieser oder des Gewebes mit der Tragstruktur werden vorzugsweise zweikomponentige Epoxidharzzusammensetzungen verwendet, wie sie beispielsweise unter den Handelsnamen Sikadur® kommerziell erhältlich sind von Sika Schweiz AG.Both as a plastic matrix for the fiber-reinforced plastic flat strip lamellae and for gluing these or the fabric to the supporting structure are preferably two-component Epoxy resin compositions used, such as are commercially available, for example, under the trade name Sikadur® from Sika Schweiz AG.

Wie bereits vorhergehend beschrieben verläuft das Faserbündel in der mindestens einen Nut über Kanten, welche unterschiedliche Flächen der Oberfläche der Tragstruktur miteinander verbinden. Diese Kante weist im Inneren der Nut vorzugsweise eine Abrundung auf. Der Radius der Abrundung beträgt insbesondere etwa 0.5 bis 10 cm, insbesondere 1 bis 5 cm.
Durch die Abrundung der Kante wird das Faserbündel, welches in Bohrung und Nut eingelegt ist, geschont, wodurch es zu weniger Faserbrüchen kommt und eine verbesserte Kraftübertragung möglich ist. Meist bevorzugt sind unabhängig von der jeweiligen Ausführungsform der vorliegenden Erfindung alle Kanten der Tragstruktur, über welche eine Nut mit Faserbündel verlaufen soll, innerhalb der Nut abgerundet.
Weiterhin ist es auch möglich, dass auch der Übergang von der Bohrung in die Nut eine Abrundung gemäss vorhergehender Beschreibung aufweist.
As already described above, the fiber bundle runs in the at least one groove over edges which connect different areas of the surface of the support structure to one another. This edge preferably has a rounding in the interior of the groove. The radius of the rounding is in particular about 0.5 to 10 cm, in particular 1 to 5 cm.
The rounding of the edge protects the fiber bundle that is inserted in the bore and groove, which means that there are fewer fiber breaks and improved power transmission is possible. Most preferably, regardless of the particular embodiment of the present invention, all edges of the support structure over which a groove with a fiber bundle is to run are rounded within the groove.
Furthermore, it is also possible that the transition from the bore into the groove also has a rounding as described above.

Die erfindungsgemässe Anordnung wird typischerweise in der Verstärkung von bestehenden Tragstrukturen eingesetzt, beispielweise bei Renovation, Instandstellung oder bei der nachträglich an Tragstrukturen angebrachten Erdbebenverstärkung. Handelt es sich bei der Tragstruktur um Stahlbetonbauwerk erfolgt die Verstärkung beispielsweise dort, wo die Stahlarmierung unzureichend ist oder wo sie durch ein unvorhergesehenes Ereignis Schaden genommen hat.The arrangement according to the invention is typically used in the reinforcement of existing supporting structures, for example in renovation, repair or in the case of earthquake reinforcement subsequently attached to supporting structures. If the supporting structure is a reinforced concrete structure, the reinforcement takes place, for example, where the steel reinforcement is inadequate or where it has been damaged by an unforeseen event.

Kurze Beschreibung der ZeichnungenBrief description of the drawings

Anhand der Zeichnungen werden sowohl erfindungsgemäße als auch nicht erfindungsgemäße Ausführungsbeispiele näher erläutert. Gleiche Elemente sind in den verschiedenen Figuren mit den gleichen Bezugszeichen versehen. Selbstverständlich ist die Erfindung nicht auf gezeigte und beschriebene erfindungsgemässe Ausführungsbeispiele beschränkt, sondern nur durch die angehängten Ansprüche.With the aid of the drawings, both inventive and non-inventive embodiments are explained in more detail. The same elements are provided with the same reference symbols in the various figures. It goes without saying that the invention is not restricted to the exemplary embodiments according to the invention that are shown and described, but rather only by the appended claims.

Es zeigen:

  • Figuren 1A bis 2C (nicht erfindungsgemäß): Tragstrukturen mit Bohrungen und Nuten und darin eingeklebten Faserbündeln bzw. Fasersträngen;
  • Figuren 3A bis 4B (nicht erfindungsgemäß): Tragstrukturen mit Bohrungen und Nuten und darin eingeklebten Faserbündeln bzw. Fasersträngen sowie Oberflächenbewehrung;
  • Figuren 5A, 5B und 6F (nicht erfindungsgemäß) und
  • Figuren 6A, 6B, 6C, 6D, 6E und 6G (erfindungsgemäß): Ausführungsformen von Tragstrukturen mit Bohrungen und Nuten und darin eingeklebten Faserbündeln bzw. Fasersträngen;
  • Figuren 7A und 7B (erfindungsgemäß, das Faserbündel und der Kleber in der Nut und den Bohrungen ist jedoch nicht dargestellt): Detailansichten von Tragstrukturen mit abgerundeten Kanten innerhalb der Nut.
Show it:
  • Figures 1A to 2C (not according to the invention): support structures with bores and grooves and fiber bundles or fiber strands glued into them;
  • Figures 3A to 4B (not according to the invention): support structures with bores and grooves and fiber bundles or fiber strands glued into them, as well as surface reinforcement;
  • Figures 5A, 5B and 6F (not according to the invention) and
  • Figures 6A, 6B, 6C, 6D, 6E and 6G (according to the invention): Embodiments of support structures with bores and grooves and fiber bundles or fiber strands glued into them;
  • Figures 7A and 7B (according to the invention, but the fiber bundle and the adhesive in the groove and the bores are not shown): Detailed views of support structures with rounded edges within the groove.

In den Figuren sind nur die für das unmittelbare Verständnis der Erfindung wesentlichen Elemente gezeigt.In the figures, only the elements essential for a direct understanding of the invention are shown.

Figur 1A zeigt einen Schnitt durch eine Tragstruktur 1 mit einer Oberfläche bestehend aus mehreren Flächen 2a, 2b, 2c, wobei von der Fläche 2a aus, eine Bohrung 3 in einen inneren Bereich der Tragstruktur verläuft. Diese Bohrung ist gefüllt mit einem Klebstoff 12 und mit einem Abschnitt eines über diese Bohrung hinausragenden Faserbündels 4. Die Tragstruktur 1, ist an der Fläche 2a mit einer Nut 5 versehen, welche sich ausgehend von der Bohrung 3 bzw. vom Eintrittsort der Bohrung in die Fläche in eine Richtung auf der Oberfläche erstreckt. Der über die Bohrung hinausragende Teil des Faserbündels 4 befindet sich in der Nut 5 und ist darin mit Klebstoff 12 befestigt. Figure 1A shows a section through a support structure 1 with a surface consisting of several surfaces 2a, 2b, 2c, with a bore 3 extending from surface 2a into an inner region of the support structure. This bore is filled with an adhesive 12 and with a portion of a fiber bundle 4 protruding beyond this bore Face extends in one direction on the surface. The part of the fiber bundle 4 protruding beyond the bore is located in the groove 5 and is fastened therein with adhesive 12.

Figur 1B zeigt eine Draufsicht auf die in Figur 1A gezeigte, nicht erfindungsgemäße Anordnung, wobei eine einzige Nut 5 von der Bohrung 3 in eine Richtung auf der Oberfläche verläuft. Weiterhin befindet sich der gesamte hinausragende Teil des Faserbündes in der Nut und ist darin mit Klebstoff 12 befestigt. Figure 1B shows a top view of the in Figure 1A The arrangement shown, not according to the invention, wherein a single groove 5 extends from the bore 3 in one direction on the surface. Furthermore, the entire protruding part of the fiber bundle is located in the groove and is fastened therein with adhesive 12.

Figur 1C zeigt ebenfalls eine Draufsicht auf die in Figur 1A gezeigte Anordnung, wobei in dieser Ausführungsform mehrere Nuten 5 von der Bohrung 3 in verschiedene Richtungen auf der Oberfläche verlaufen. Der hinausragende Teil des Faserbündels 4 ist nach Fasersträngen aufgeteilt, wobei diese Faserstränge bevorzugt etwa die gleiche Stärke haben, und die Faserstränge befinden sich in den Nuten und sind darin mit Klebstoff 12 befestigt. Figure 1C also shows a plan view of the in Figure 1A arrangement shown, wherein in this embodiment several grooves 5 extend from the bore 3 in different directions on the surface. The protruding part of the fiber bundle 4 is divided into fiber strands, these fiber strands preferably having approximately the same thickness, and the fiber strands are located in the grooves and are fixed therein with adhesive 12.

Figur 2A und 2B zeigt im Wesentlichen eine analoge nicht erfindungsgemäße Ausführungsform, wie sie in den Figuren 1A und 1C gezeigt ist, wobei die mehreren Nuten 5 ausgehend von der Bohrung 3 radial an der Oberfläche der Tragstruktur 1 verlaufen. Figures 2A and 2B shows essentially an analogous embodiment not according to the invention as shown in FIGS Figures 1A and 1C is shown, wherein the plurality of grooves 5, starting from the bore 3, extend radially on the surface of the support structure 1.

Unabhängig von den oben beschriebenen nicht erfindungsgemäßen Ausführungsformen, stellt der Abschnitt des Faserbündels, welcher sich in der Bohrung befindet, insbesondere eines der beiden losen Enden des Faserbündels dar. Das andere lose Ende des Faserbündels stellt jenen Teil des Faserbündels dar, welcher über die Bohrung hinausragt bzw. welcher in der Nut oder den Nuten befindet und dort befestigt ist.Regardless of the above-described non-inventive embodiments, the section of the fiber bundle which is located in the bore is in particular one of the two loose ends of the fiber bundle. The other loose end of the fiber bundle represents that part of the fiber bundle which protrudes beyond the bore or which is located in the groove or the grooves and is attached there.

In einer anderen, weniger bevorzugten nicht erfindungsgemäßen Ausführungsform ist es auch möglich, ein Faserbündel insbesondere im Bereich seiner Mitte bzw. seines geometrischen Schwerpunkts umzufalten und so die beiden losen Enden des Faserbündels übereinander zu legen. Danach wird dann das Faserbündel, bevorzugt mit dem gefalteten Ende in die Bohrung eingeführt und die beiden losen Enden werden in die Nut eingelegt bzw. auf mehrere Nuten aufgeteilt. In beiden Fällen ist jeweils der Abschnitt des Faserbündels, welcher sich in der Bohrung befindet, insbesondere in etwa gleich lang wie jener, welcher über die Bohrung hinausragt.In another, less preferred embodiment not according to the invention, it is also possible to fold over a fiber bundle in particular in the area of its center or its geometric center of gravity and thus to place the two loose ends of the fiber bundle on top of one another. Then the fiber bundle is then inserted into the bore, preferably with the folded end, and the two loose ends are inserted into the groove or divided into several grooves. In both cases, the section of the fiber bundle which is located in the bore is in particular approximately the same length as that which protrudes beyond the bore.

Figur 2C zeigt eine nicht erfindungsgemäße Ausführungsform, bei welcher sich ein Mittelabschnitt des Faserbündels in der Bohrung befindet. Die hier gezeigte Tragstruktur 1 weist eine Oberfläche bestehend aus mehreren Flächen 2a, 2b, 2c, etc. auf und eine erste Bohrung 3a, welche von der Fläche 2a aus in den inneren Bereich der Tragstruktur verläuft. Die zweite Bohrung 3b verläuft von der Fläche 2b aus in den inneren Bereich der Tragstruktur. Die Fläche 2b ist der Fläche 2a abgewandt und die zwei Bohrungen 3a und 3b sind so angeordnet, dass sie in der Verlängerung ihrer jeweiligen Bohrachsen miteinander verbunden sind. Selbstverständlich können die zwei Bohrungen im gezeigten Fall dadurch erstellt werden, dass die Tragstruktur von einer Fläche aus durchbohrt wird und die zweite Bohrung somit die Austrittsstelle der ersten Bohrung darstellt. Die Bohrungen 3a und 3b sind mit einem Klebstoff 12 und mit einem Abschnitt eines Faserbündels 4 gefüllt. Insbesondere wird bei dieser Figure 2C shows an embodiment not according to the invention, in which a central section of the fiber bundle is located in the bore. The support structure 1 shown here has a surface consisting of several surfaces 2a, 2b, 2c, etc. and a first bore 3a, which extends from the surface 2a into the inner region of the support structure. The second bore 3b runs from the surface 2b into the inner region of the supporting structure. The surface 2b faces away from the surface 2a and the two bores 3a and 3b are arranged in such a way that they are connected to one another in the extension of their respective drilling axes. Of course, in the case shown, the two bores can be created in that the support structure is pierced from a surface and the second bore thus represents the exit point of the first bore. The holes 3a and 3b are with an adhesive 12 and filled with a section of a fiber bundle 4. In particular, this

Ausführungsform ein Faserbündel so in der Bohrung angeordnet, dass sich sein Mittelabschnitt in der Bohrung befindet und dass seine losen Enden jeweils über die Oberfläche der Tragstruktur überstehen. Von den Bohrungen 3a und 3b aus verlaufen jeweils mehrere Nuten 5 in verschiedene Richtungen auf der Oberfläche, beispielsweise in der Art, wie es in Figur 2B dargestellt ist. Die hinausragenden Teile des Faserbündels 4 sind nach Fasersträngen aufgeteilt und die Faserstränge befinden sich in den Nuten und sind darin mit Klebstoff befestigt.Embodiment a fiber bundle is arranged in the bore in such a way that its central section is located in the bore and that its loose ends each protrude beyond the surface of the support structure. A plurality of grooves 5 each extend from the bores 3a and 3b in different directions on the surface, for example in the manner as shown in FIG Figure 2B is shown. The protruding parts of the fiber bundle 4 are divided into fiber strands and the fiber strands are located in the grooves and are fixed therein with adhesive.

In den Figuren 3A (Querschnitt) und 3B (Draufsicht) ist eine nicht erfindungsgemäße Ausführungsform der Anordnung gezeigt. Dabei weist eine Fläche 2a der Oberfläche einer Tragstruktur 1 mehrere Bohrungen 3 auf, welche in den inneren Bereich der Tragstruktur 1 verlaufen, und jeweils pro Bohrung eine einzige Nut 5, welche sich entlang der Oberfläche erstreckt (vgl. auch Figur 1B). Die Bohrungen 3 und die Nuten 5 sind dabei versetzt zueinander, in ihrer Gesamtheit jedoch linear an der Oberfläche angebracht. Über den Nuten 5 mit den Abschnitten der Faserbündel 4 ist eine Lamelle 6 als Oberflächenbewehrung angebracht, wobei diese Lamelle zumindest in diesem Bereich mit der Oberfläche der Tragstruktur verklebt ist. Insbesondere ist eine derartige Lamelle vollflächig mit der Oberfläche der Tragstruktur verklebt. Anordnungen, wie sie in den Figuren 3A und 3B gezeigt sind, kommen insbesondere im Bereich der Endabschnitte, bspw. in den letzten 0.5 bis 1 Metern, der Lamellen vor und dienen der verbesserten Kraftübertragung zwischen Tragstruktur und Lamelle, also Oberflächenbewehrung.In the Figures 3A (Cross-section) and FIG. 3B (top view) shows an embodiment of the arrangement which is not according to the invention. A surface 2a of the surface of a support structure 1 has several bores 3, which run into the inner area of the support structure 1, and a single groove 5 for each bore, which extends along the surface (see also FIG Figure 1B ). The bores 3 and the grooves 5 are offset from one another, but in their entirety are attached linearly to the surface. A lamella 6 is attached as surface reinforcement over the grooves 5 with the sections of the fiber bundles 4, this lamella being glued to the surface of the supporting structure at least in this area. In particular, such a lamella is glued over the entire surface to the surface of the support structure. Arrangements like those in the Figures 3A and 3B shown, occur in particular in the area of the end sections, for example in the last 0.5 to 1 meters, of the lamellas and serve to improve the transmission of force between the supporting structure and the lamella, i.e. surface reinforcement.

Figur 3C zeigt eine Draufsicht auf eine nicht erfindungsgemäße Anordnung, welche im Wesentlichen jener aus Figur 1C entspricht, wobei über den Nuten 5, welche von der Bohrung 3 ausgehen und mit Fasersträngen des Faserbündels 4 und mit Klebstoff versehen sind, ein Gewebe 7 als Oberflächenbewehrung angebracht ist. Auch ein solches Gewebe ist vorzugsweise vollflächig mit der Oberfläche der Tragstruktur verklebt. Die Verklebung des über den Bereich des in die Nuten verklebten Faserbündels führt zu einer verbesserten Kraftübertragung zwischen Tragstruktur und Gewebe, also Oberflächenbewehrung. Figure 3C FIG. 11 shows a plan view of an arrangement not according to the invention, which is essentially that of FIG Figure 1C corresponds, with a fabric 7 being attached as surface reinforcement over the grooves 5, which extend from the bore 3 and are provided with fiber strands of the fiber bundle 4 and with adhesive. Such a fabric is also preferably glued over the entire area to the surface of the support structure. The gluing of the fiber bundle glued into the grooves leads to an improved transmission of force between the supporting structure and the fabric, that is to say the surface reinforcement.

Eine nicht erfindungsgemäße Ausführungsform der Anordnung, wie sie in den Figuren 1C und 3C gezeigt ist, ist weiterhin in der Figur 3D dargestellt. In diesem Fall befindet sich die Bohrung 3, welche in den inneren Bereich der Tragstruktur verläuft, an einer Stossstelle zwischen zwei flächigen Elementen einer Tragstruktur, bspw. an einer Stossstelle zwischen zwei Wänden oder zwischen Wand und Bodenplatte. Auch in diesem Fall ist über dem Ankerbereich eine Oberflächenbewehrung in Form eines Gewebes 7 angebracht.An embodiment of the arrangement not according to the invention as shown in FIGS Figures 1C and 3C shown is still in the Figure 3D shown. In this case, the bore 3, which runs into the inner area of the supporting structure, is located at a joint between two flat elements of a supporting structure, for example at a joint between two walls or between wall and base plate. In this case too, a surface reinforcement in the form of a fabric 7 is attached over the anchor area.

Eine weitere nicht erfindungsgemäße Ausführungsform ist in Figur 3E gezeigt. Die hier gezeigte Tragstruktur 1 weist eine Oberfläche bestehend aus mehreren Flächen 2a, 2b, 2c auf und eine erste Bohrung 3a, welche von der Fläche 2a aus in den inneren Bereich der Tragstruktur verläuft. Die zweite Bohrung 3b verläuft von der Fläche 2b aus in den inneren Bereich der Tragstruktur. Die Fläche 2b ist der Fläche 2a abgewandt und die zwei Bohrungen 3a und 3b sind so angeordnet, dass sie in der Verlängerung ihrer jeweiligen Bohrachsen miteinander verbunden sind. Selbstverständlich können die zwei Bohrungen im gezeigten Fall dadurch erstellt werden, dass die Tragstruktur von einer Fläche aus durchbohrt wird und die zweite Bohrung somit die Austrittsstelle der ersten Bohrung darstellt. Die Bohrungen 3a und 3b sind mit einem Klebstoff (nicht dargestellt) und mit einem Abschnitt eines Faserbündels 4 gefüllt. Insbesondere wird bei dieser Ausführungsform ein Faserbündel so in der Bohrung angeordnet, dass sich sein Mittelabschnitt in der Bohrung befindet und dass seine losen Enden jeweils über die Oberfläche der Tragstruktur überstehen. Von den Bohrungen 3a und 3b aus verlaufen jeweils mehrere Nuten 5 in verschiedene Richtungen auf der Oberfläche. Die hinausragenden Teile des Faserbündels 4 sind nach Fasersträngen aufgeteilt und die Faserstränge befinden sich in den Nuten und sind darin mit Klebstoff befestigt. Über den beschriebenen Anordnungen ist ein Gewebe 7 angebracht, welches über die Stirnseite der Tragstruktur verläuft und im Bereich der Nuten verlaufend von der Eintrittsstelle der Bohrung 3a hin zu jener von Bohrung 3b mit der Tragstruktur verklebt ist.Another embodiment not according to the invention is shown in FIG Figure 3E shown. The support structure 1 shown here has a surface consisting of several surfaces 2a, 2b, 2c and a first bore 3a, which extends from the surface 2a into the inner region of the support structure. The second bore 3b runs from the surface 2b into the inner region of the supporting structure. The surface 2b faces away from the surface 2a and the two bores 3a and 3b are arranged in such a way that they are connected to one another in the extension of their respective drilling axes. Of course, in the case shown, the two bores can be created in that the support structure is pierced from a surface and the second bore thus represents the exit point of the first bore. The bores 3a and 3b are filled with an adhesive (not shown) and with a section of a fiber bundle 4. In particular, in this embodiment a fiber bundle is arranged in the bore in such a way that its central section is located in the bore and that its loose ends each protrude beyond the surface of the support structure. A plurality of grooves 5 each extend from the bores 3a and 3b in different directions on the surface. The protruding parts of the fiber bundle 4 are divided into fiber strands and the fiber strands are located in the grooves and are fixed therein with adhesive. A fabric 7 is attached over the described arrangements, which runs over the end face of the support structure and is glued to the support structure in the area of the grooves running from the entry point of the bore 3a to that of the bore 3b.

Eine nicht erfindungsgemäße Ausführungsform, bei welcher ebenfalls zwei Bohrungen vorhanden sind, welche in der Verlängerung ihrer Bohrachsen miteinander verbunden sind ist in den Figuren 3F (Querschnitt) und 3G (Draufsicht) dargestellt. Hierbei weist eine T-förmige Tragstruktur mit einer Oberfläche umfassend mehrere Flächen 2a, 2b, etc. an der Stossstelle zwischen ihren zwei flächigen Elementen zwei Bohrungen 3a und 3b auf, welche die Flächen 2a und 2b miteinander verbinden. Das Faserbündel 4 ist so in der Bohrung angeordnet, dass sich sein Mittelabschnitt in der Bohrung befindet und dass seine losen Enden jeweils über die Oberfläche der Tragstruktur überstehen. Von den Bohrungen aus verlaufen jeweils mehrere Nuten 5 in verschiedene Richtungen auf der Oberfläche. Die hinausragenden Teile des Faserbündels 4 sind nach Fasersträngen aufgeteilt und die Faserstränge befinden sich in den Nuten und sind darin mit Klebstoff befestigt. In den Figuren 3H und 3I ist eine mögliche Anwendung der in den Figuren 3F und 3G gezeigten nicht erfindungsgemäßen Anordnung. Bei der Tragstruktur 1 handelt es sich hierbei um eine Betonplatte 10, welche mehrere Verstärkungsrippen 11, also T-förmige Abschnitte aufweist. Die Verstärkungsrippen 11 wiesen im Bereich ihrer Stossstellen mit der Betonplatte 10 Bohrungen 3 auf, wobei diese so angelegt sind, dass jeweils zwei Bohrungen in der Verlängerung ihrer Bohrachsen miteinander verbunden sind. Ausgehend von der Eintrittsstelle des jeweiligen Bohrlochs 3 verlaufen mehrere Nuten entlang der Oberfläche der Betonplatte. Analog zu den oben beschriebenen nicht erfindungsgemäßen Ausführungsformen sind Bohrlöcher und Nuten mit einem Faserbünden bzw. mit Fasersträngen des Faserbündels und Klebstoff gefüllt. Über den Oberflächen der Betonplatte, welche sich zwischen den Verstärkungsrippen 11 befinden, ist eine Oberflächenarmierung in Form eines Gewebes 7 angebracht. Dieses Gewebe ist insbesondere vollflächig mit der darunterliegenden Oberfläche verklebt.An embodiment not according to the invention, in which two bores are also present, which are connected to one another in the extension of their drilling axes, is in the Figures 3F (Cross-section) and 3G (top view). Here, a T-shaped support structure with a surface comprising a plurality of surfaces 2a, 2b, etc. at the joint between its two flat elements has two bores 3a and 3b which connect the surfaces 2a and 2b to one another. The fiber bundle 4 is arranged in the bore in such a way that its central section is located in the bore and that its loose ends each protrude beyond the surface of the support structure. Several grooves 5 each run in different directions on the surface from the bores. The protruding parts of the fiber bundle 4 are divided into fiber strands and the fiber strands are located in the grooves and are fixed therein with adhesive. In the Figures 3H and 3I is one possible application of the Figures 3F and 3G shown arrangement not according to the invention. The supporting structure 1 is a concrete slab 10 which has several reinforcing ribs 11, that is to say T-shaped sections. The reinforcement ribs 11 had holes 3 in the area of their abutment points with the concrete slab 10, these being laid out in such a way that two holes in each case are connected to one another in the extension of their drilling axes. Starting from the entry point of the respective borehole 3, several grooves run along the surface of the concrete slab. Analogously to the above-described embodiments not according to the invention, boreholes and grooves are filled with a fiber bundle or with fiber strands of the fiber bundle and adhesive. A surface reinforcement in the form of a fabric 7 is attached over the surfaces of the concrete slab, which are located between the reinforcement ribs 11. In particular, this fabric is glued over the entire surface to the underlying surface.

In den Figuren 4A (Querschnitt) und 4B (Draufsicht) ist eine weitere nicht erfindungsgemäße Ausführungsform gezeigt, bei welcher Anordnungen, wie sie beispielsweise in den Figuren 2A und 2B gezeigt sind, in regelmässigen Abständen an einer Tragstruktur 1 angebracht sind. Die Anordnungen können dabei auf einer Fläche der Oberfläche der Tragstruktur angebracht sein oder auf mehreren Flächen. Über den Anordnungen ist weiterhin ein Gewebe 7 zumindest mit den Anordnungen, insbesondere jedoch vollflächig, mit der Oberfläche der Tragstruktur verklebt. Das Gewebe kann dabei durchgehend über Ecken und Kanten in der Oberfläche der Tragstruktur verlaufen.In the Figures 4A (Cross-section) and 4B (top view) shows a further embodiment not according to the invention, in which arrangements, such as are for example in FIGS Figures 2A and 2B are shown, are attached to a support structure 1 at regular intervals. The arrangements can be attached to one area of the surface of the support structure or to several areas. Above the arrangements, a fabric 7 is also glued at least to the arrangements, but in particular over the entire area, to the surface of the support structure. The fabric can run continuously over corners and edges in the surface of the support structure.

Figur 5A zeigt einen Schnitt durch eine nicht erfindungsgemäße Ausführungsform einer Anordnung mit einer Tragstruktur 1 mit einer Oberfläche bestehend aus mehreren Flächen 2a, 2b, 2c, etc. und einer ersten Bohrung 3a, welche von der Fläche 2a aus in den inneren Bereich der Tragstruktur verläuft. Die zweite Bohrung 3b verläuft von der Fläche 2b aus in den inneren Bereich der Tragstruktur. Die Fläche 2b ist der Fläche 2a abgewandt. Von der einen Bohrung 3a verläuft eine Nut 5 entlang der Oberfläche der Tragstruktur hin zum Eintrittsort der anderen Bohrung in die Tragstruktur. Die Nut, welche also die beiden Eintrittslöcher der Bohrungen miteinander verbindet, verläuft insbesondere auf dem kürzesten Weg zwischen den beiden Bohrungen. Je nach Anforderungen an die Verstärkung der Tragstruktur ist jedoch auch denkbar, dass die Nut einen anderen Verlauf zwischen den Bohrungen einnimmt, bspw. um eine möglichst gleichmässige Kraftverteilung zu gewährleisten. In der Nut 5 verläuft ein Faserbündel 4, welches mit seinen losen Enden in den beiden Bohrungen 3a und 3b mündet. Sowohl in den Bohrungen als auch in der Nut befindet sich Klebstoff 12 zur Befestigung des Faserbündels. Eine ähnliche nicht erfindungsgemäße Ausführungsform wie in Figur 5A ist auch in Figur 5B dargestellt, wobei hier das Faserbündel eine Verstärkungsrippe 11 eines Tragwerks 1 umschnürt. Figure 5A shows a section through an embodiment not according to the invention of an arrangement with a support structure 1 with a surface consisting of several surfaces 2a, 2b, 2c, etc. and a first bore 3a, which runs from the surface 2a into the inner area of the support structure. The second bore 3b runs from the surface 2b into the inner region of the supporting structure. The surface 2b faces away from the surface 2a. A groove 5 runs from one bore 3a along the surface of the support structure to the point of entry of the other bore into the support structure. The groove, which thus connects the two entry holes of the bores with one another, runs in particular on the shortest path between the two bores. Depending on the requirements for the reinforcement of the support structure, however, it is also conceivable that the groove takes a different course between the bores, for example in order to ensure the most uniform possible force distribution. A fiber bundle 4 runs in the groove 5, which ends with its loose ends in the two bores 3a and 3b. Both the bores and the groove contain adhesive 12 for fastening the fiber bundle. A similar embodiment not according to the invention as in FIG Figure 5A is also in Figure 5B shown, the fiber bundle here wrapping around a reinforcing rib 11 of a supporting structure 1.

Figur 6A zeigt einen Schnitt durch eine erfindungsgemäße Ausführungsform, welche eine Abwandlung der nicht erfindungsgemäßen Ausführungsform aus Figur 5A entspricht. Im Gegensatz zu dieser, weist die Ausführungsform in Figur 6A zwei Bohrungen 3a, 3b in unterschiedlichen, sich gegenseitig abgewandten Flächen 2a, 2b der Oberfläche der Tragstruktur auf, wobei die zwei Bohrungen 3a und 3b so angeordnet sind, dass sie in der Verlängerung ihrer jeweiligen Bohrachsen miteinander verbunden sind. Die Eintrittslöcher der beiden Bohrungen 3a und 3b sind wie in Figur 5A über eine Nut 5 miteinander verbunden. Sowohl die Bohrungen 3a, 3b als auch die Nut 5 enthalten einen Klebstoff 12 und ein Faserbündel 4. Das Faserbündel ist dabei insbesondere so angeordnet, dass seine beiden Enden sich überlappen. Diese Überlappung kann in der Bohrung oder an einer beliebigen Stelle der Nut liegen. Die Länge des überlappenden Bereichs des Faserbündels ist dabei insbesondere so gewählt, dass eine möglichst lückenlose Kraftübertragung gewährleistet ist und beträgt etwa 5 bis 50 cm. Je nach Anforderung an die Tragstruktur ist es auch möglich, das Faserbündel mehrfach um die Tragstruktur umzuwickeln. In Bezug auf die Ausführungsformen der Erfindung, wie sie in den Figuren 6A bis 6D gezeigt sind, sind die zwei Bohrungen 3a und 3b so angeordnet sind, dass sie in der Verlängerung ihrer jeweiligen Bohrachsen miteinander verbunden, und das Faserbündel kann so angeordnet sein, dass sich seine beiden Enden mindestens überlappen. Dadurch bildet das Faserbündel eine geschlossene Schlaufe, wodurch die Übertragung der Schubkraft zwischen den beiden Enden des Faserbündes, also kontaktkritisch innerhalb des gleichen Materials, stattfindet. Gegenüber Ausführungsformen, bei welchen die Enden des Faserbündes in separaten Bohrungen eingesetzt werden und die Übertragung der Schubkraft somit zwischen der Tragstruktur und dem Faserbündel, also verbundkritisch, erfolgt, erlauben die bevorzugten Ausführungsformen eine höhere Effizienz der Verstärkung und eine deutlich bessere Ausnützung des Faserbündels. Figure 6A shows a section through an embodiment according to the invention, which is a modification of the embodiment not according to the invention Figure 5A is equivalent to. In contrast to this, the embodiment in Figure 6A two bores 3a, 3b in different, mutually facing away surfaces 2a, 2b of the surface of the support structure, the two bores 3a and 3b being arranged so that they are connected to one another in the extension of their respective drilling axes. The entry holes of the two Bores 3a and 3b are as in Figure 5A connected to one another via a groove 5. Both the bores 3a, 3b and the groove 5 contain an adhesive 12 and a fiber bundle 4. The fiber bundle is in particular arranged in such a way that its two ends overlap. This overlap can be in the bore or at any point in the groove. The length of the overlapping area of the fiber bundle is in particular selected in such a way that the transmission of force as seamless as possible is guaranteed and is approximately 5 to 50 cm. Depending on the requirements placed on the support structure, it is also possible to wrap the fiber bundle several times around the support structure. With respect to the embodiments of the invention as set forth in FIGS Figures 6A to 6D are shown, the two bores 3a and 3b are arranged so that they are connected to each other in the extension of their respective drilling axes, and the fiber bundle can be arranged so that its two ends at least overlap. As a result, the fiber bundle forms a closed loop, as a result of which the transmission of the thrust force takes place between the two ends of the fiber bundle, i.e. within the same material, which is critical for contact. Compared to embodiments in which the ends of the fiber bundle are inserted in separate bores and the shear force is thus transmitted between the support structure and the fiber bundle, i.e. in a critical manner, the preferred embodiments allow a higher efficiency of the reinforcement and a significantly better utilization of the fiber bundle.

Die Figuren 6B und 6C zeigen Abwandlungen der erfindungsgemäßen Ausführungsform, wie sie in Figur 6A beschrieben ist. Gezeigt sind hier erfindungsgemässe Anordnungen, wie sie beispielsweise zur Verstärkung einer rechteckigen Säule als Bestandteil einer Tragstruktur eingesetzt werden können. Figur 6C zeigt dabei, dass es auch möglich ist, dass das Faserbündel 4 mehrmals durch eine Bohrung geführt wird, jedoch in zwei unterschiedlichen Nuten vom Eintrittsort der ersten Bohrung zu jenem der zweiten Bohrung zu verlaufen. Andererseits kann die Ausführungsform aus Figur 6C auch dadurch erstellt werden, indem der über die Bohrung hinausragende Teil des Faserbündels in zwei Faserstränge aufgeteilt wird, welche dann in unterschiedlichen Nuten verlaufen.the Figures 6B and 6C show modifications of the embodiment according to the invention as shown in FIG Figure 6A is described. Arrangements according to the invention are shown here, such as can be used, for example, to reinforce a rectangular column as part of a support structure. Figure 6C shows that it is also possible for the fiber bundle 4 to be guided several times through a bore, but to run in two different grooves from the entry point of the first bore to that of the second bore. on the other hand can make the embodiment Figure 6C can also be created by the part of the fiber bundle protruding beyond the bore is divided into two fiber strands, which then run in different grooves.

Figur 6D zeigt eine Abwandlung der Ausführungsform, wie sie in Figur 5B dargestellt ist, wobei hier das Faserbündel 4 die Verstärkungsrippe 11 vollständig umschnürt. Figure 6D shows a modification of the embodiment shown in FIG Figure 5B is shown, the fiber bundle 4 completely wrapping around the reinforcing rib 11 here.

Figur 6E zeigt eine Seitenansicht einer Tragstruktur, welche die in den Figuren 6A, 6B und 6C dargestellten Varianten der erfindungsgemässen Anordnung umfasst. Je nach Anforderungen können die verschiedenen Varianten miteinander kombiniert werden oder es werden durchgehend mehrere identische Anordnungen an eine Tragstruktur angebracht. Figure 6E FIG. 11 shows a side view of a support structure which the in FIGS Figures 6A, 6B and 6C includes variants of the arrangement according to the invention shown. Depending on the requirements, the different variants can be combined with one another or several identical arrangements can be attached to a supporting structure.

Figur 6G zeigt Tragstruktur 1 umfassend eine Bodenplatte 10 und eine darauf erstellte Wand, wobei die Wand in ihrem unteren Bereich mit mehreren erfindungsgemässen Anordnungen versehen ist, welche jenen aus Figur 6A entsprechen. Optional kann über diese Anordnungen noch ein Gewebe zur zusätzlichen Verstärkung der Tragstruktur angebracht werden (hier nicht dargestellt). Figure 6G shows support structure 1 comprising a base plate 10 and a wall created thereon, the wall being provided in its lower area with several arrangements according to the invention, which consist of those from Figure 6A correspond. Optionally, a fabric for additional reinforcement of the supporting structure can be attached via these arrangements (not shown here).

Figur 6F zeigt eine zylinderförmige Säule, welche mehrere nicht erfindungsgemässe Anordnungen umfasst. Figure 6F shows a cylindrical column which comprises several arrangements not according to the invention.

Figur 7A zeigt eine detaillierte Ansicht eines Ausschnitts einer Tragstruktur 1 mit einer Oberfläche bestehend aus mehreren Flächen 2a, 2b, 2c, wobei von einer Fläche 2a aus eine Bohrung 3 in einen inneren Bereich der Tragstruktur verläuft. Die Tragstruktur 1 ist an der Fläche 2a, von welcher aus die Bohrung in einen inneren Bereich der Tragstruktur verläuft, mit einer Nut 5 versehen ist, welche sich ausgehend von der Bohrung in eine Richtung auf der Oberfläche erstreckt. Figure 7A shows a detailed view of a section of a support structure 1 with a surface consisting of several surfaces 2a, 2b, 2c, with a bore 3 extending from one surface 2a into an inner region of the support structure. The support structure 1 is provided with a groove 5 on the surface 2a, from which the bore extends into an inner region of the support structure, which, starting from the bore, extends in one direction on the surface.

Die Nut 5 verläuft dabei über jeweils eine Kante 8, welche die zwei Flächen 2a und 2c, bzw. 2c und 2b der Oberfläche des Tragwerks miteinander verbindet, und diese eine Kante 8 weist im Inneren der Nut 5 eine Abrundung 9 auf. Figur 7B zeigt einen Schnitt durch einen Bereich einer Tragstruktur 1, welche zwei Bohrungen 3a, 3c in unterschiedlichen, sich gegenseitig abgewandten Flächen 2a, 2c der Oberfläche der Tragstruktur aufweist, wobei die zwei Bohrungen 3a und 3c so angeordnet sind, dass sie in der Verlängerung ihrer jeweiligen Bohrachsen miteinander verbunden sind. Die Eintrittslöcher der beiden Bohrungen 3a und 3b sind über eine Nut 5 miteinander verbunden. Innerhalb der Nut 5 weisen die Kanten 8 jeweils eine Abrundung 9 auf. Auch hier können die jeweiligen Übergänge von der Bohrung in die Nut eine Abrundung gemäss vorhergehender Beschreibung aufweisen.The groove 5 runs over an edge 8, which connects the two surfaces 2a and 2c, or 2c and 2b of the surface of the supporting structure with one another, and this one edge 8 has a rounding 9 inside the groove 5. Figure 7B shows a section through a region of a support structure 1, which has two bores 3a, 3c in different, mutually facing away surfaces 2a, 2c of the surface of the support structure, the two Bores 3a and 3c are arranged so that they are connected to one another in the extension of their respective drilling axes. The entry holes of the two bores 3 a and 3 b are connected to one another via a groove 5. Within the groove 5, the edges 8 each have a rounding 9. Here, too, the respective transitions from the bore into the groove can have a rounding according to the preceding description.

BeispieleExamples

Im Folgenden sind nicht erfindungsgemäße Ausführungsbeispiele aufgeführt.Embodiments not according to the invention are listed below.

PrüfkörperTest specimen

Als Prüfkörper wurden Betonwürfel mit einer Kantenlänge von 20 cm hergestellt, wobei für alle Würfel Beton aus der gleichen Charge verwendet wurde. Die Betonwürfel wurden währen 28 Tagen bei 23°C und 50 %relativer Luftfeuchtigkeit gelagert. Die Betonwürfel wurden an einer Seite abgeschliffen, um sie von Zementschlamm zu befreien. In der Mitte der behandelten Fläche wurde eine Bohrung mit einem Durchmesser von 20 mm und einer Tiefe von 100 mm angebracht. Zwei Betonwürfel wurden ohne Bohrung belassen. Ausgehend von der Bohrung wurden bei den Betonwürfeln jeweils gleichmässig um die Bohrung herum acht Nuten mit einem Winkelschleifer angebracht. Die Nuten waren 5 mm breit und 5 mm tief und erstreckten sich über eine Länge von 8 cm. Der Winkel zwischen den Nuten betrug jeweils 45°. Bei vier Betonwürfeln wurden jeweils nur fünf Nuten halbkreisförmig angebracht. Die Kanten beim Übergang von der Bohrung in die Nuten wurde leicht abgerundet. Bei zwei Würfeln wurden keine Nuten angebracht. Anschliessend wurden die Betonwürfel wiederholt an der bearbeiteten Oberfläche und im Inneren der Bohrung mit Druckluft und einer Bürste gereinigt und so weitgehend von Staub befreit.Concrete cubes with an edge length of 20 cm were produced as test specimens, with concrete from the same batch being used for all cubes. The concrete cubes were stored for 28 days at 23 ° C and 50% relative humidity. The concrete cubes were sanded down on one side to remove cement slurry. A hole with a diameter of 20 mm and a depth of 100 mm was made in the center of the treated area. Two concrete cubes were left without drilling. Starting from the borehole, eight grooves were made evenly around the borehole with an angle grinder on the concrete cubes. The grooves were 5 mm wide and 5 mm deep and extended over a length of 8 cm. The angle between the grooves was 45 ° in each case. In the case of four concrete cubes, only five grooves were made in a semicircle. The edges at the transition from the hole to the grooves were slightly rounded. No grooves were made for two cubes. The concrete cubes were then repeatedly cleaned on the machined surface and inside the bore with compressed air and a brush, and thus largely freed of dust.

Auf die bearbeitete Oberfläche der Betonwürfel ohne Bohrung wurde mittels Zahntraufel Sikadur®-330, kommerziell erhältlich von Sika Schweiz AG, mit einer mittleren Schichtstärke von ca. 1mm appliziert. Bei den Betonwürfeln mit Bohrung wurde die Bohrung von unten nach oben sowie die Nuten mit Sikadur®-330 befüllt. Dabei wurde darauf geachtet, dass keine Luft in der Bohrung eingeschlossen blieb.Sikadur®-330, commercially available from Sika Schweiz AG, with an average layer thickness of approx. 1 mm was applied to the machined surface of the concrete cubes without drilling. With the concrete cubes The bore was filled with Sikadur®-330 from the bottom up and the grooves. Care was taken to ensure that no air was trapped in the borehole.

Ein Faserbündel einer Länge von 20 cm und einer Faserquerschnittsfläche von etwa 25 mm2 wurde mit Hilfe eines Pinsels mit Sikadur® 300 von Sika Schweiz AG vollständig imprägniert. Anschliessend wurde an einem losen Ende des imprägnierten Faserbündels ein Kabelbinder angebracht und fest angezogen und abgelängt. Mit Hilfe einer Stricknadel, welche am Kabelbinder eingehakt wurde, wurde das Faserbündel bis zum Anschlag in die Bohrung eingeführt. Das überstehende Ende des Faserbündels wurde in Faserstränge aufgeteilt, wobei die Anzahl der Faserstränge jener der vorher angebrachten Nuten entsprechen musste, und in die Nuten eingelegt. Bei den Betonwürfeln ohne Nuten wurde das überstehende Ende des Faserbündels gleichmässig aufgefächert und an der bearbeiteten Oberfläche des Betonwürfels ausgebreitet.A fiber bundle with a length of 20 cm and a fiber cross-sectional area of about 25 mm 2 was completely impregnated with Sikadur® 300 from Sika Schweiz AG using a brush. A cable tie was then attached to a loose end of the impregnated fiber bundle, tightened and cut to length. With the help of a knitting needle, which was hooked into the cable tie, the fiber bundle was inserted into the hole as far as it would go. The protruding end of the fiber bundle was divided into fiber strands, whereby the number of fiber strands had to correspond to that of the previously made grooves, and placed in the grooves. In the case of the concrete cubes without grooves, the protruding end of the fiber bundle was evenly fanned out and spread over the machined surface of the concrete cube.

An der bearbeiteten Oberfläche des Betonwürfels wurde nun über den Nuten mit dem Faserbündel Sikadur®-330 gleichmässig verteilt, sodass die gesamte bearbeitete Oberfläche mit ausreichend Klebstoff bedeckt war.The Sikadur®-330 fiber bundle was then evenly distributed over the grooves on the processed surface of the concrete cube, so that the entire processed surface was covered with sufficient adhesive.

Ein bereitgestelltes Gewebe aus SikaWrap® 300 C NW (Breite 20 cm, Länge 180 cm) wurde im Bereich der letzten 20 cm seiner losen Enden mittels Farbroller mit Sikadur®-300 laminiert. Ein laminiertes loses Ende wurde auf die bearbeitete Fläche des Betonwürfels gelegt und dort mit einem Farbroller angedrückt. Über dem angebrachten Gewebe wurde mittels Zahntraufel Sikadur®-330 appliziert. Das Gewebe wurde in einer Schleife umgelegt und das andere lose und laminierte Ende wurde auf der gleichen Stelle des Betonwürfels gelegt, so, dass die beiden Enden des Gewebes übereinander zu liegen kamen. Wiederum wurde das Gewebe mit dem Farbroller angedrückt. Mit einem Spachtel der Breite des Betonwürfels wurde überschüssiger Klebstoff vom Prüfkörper entfernt.A fabric made of SikaWrap® 300 C NW (width 20 cm, length 180 cm) provided was laminated with Sikadur®-300 in the area of the last 20 cm of its loose ends using a paint roller. A laminated loose end was placed on the machined surface of the concrete cube and pressed there with a paint roller. Sikadur®-330 was applied over the attached tissue using a notched trowel. The fabric was put in a loop and the other loose and laminated end was placed on the same spot on the concrete cube so that the two ends of the fabric lay on top of each other. Again the fabric was pressed on with the paint roller. Excess adhesive was removed from the test specimen with a spatula the width of the concrete cube.

Die so hergestellten Prüfkörper wurden während 7 Tagen bei 23°C und 50% relativer Luftfeuchtigkeit belassen, damit der Klebstoff aushärten konnte.The test specimens produced in this way were left at 23 ° C. and 50% relative humidity for 7 days so that the adhesive could cure.

Auf die gleiche Weise wurden auch Prüfkörper mit Faserbündel aus Glasfasern mit einer Faserquerschnittsfläche von etwa 25 mm2 hergestellt.Test specimens with fiber bundles made of glass fibers with a fiber cross-sectional area of about 25 mm 2 were also produced in the same way.

Es wurden jeweils von jedem Typ zwei identische Prüfkörper hergestellt. Die Resultate der Messungen stellen den Mittelwert der Messungen an den zwei identischen Prüfkörpern dar.Two identical test specimens of each type were produced. The results of the measurements represent the mean value of the measurements on the two identical test specimens.

MessmethodeMeasurement method

Es wurde die Zugscherfestigkeit unterschiedlicher Prüfkörper gemessen nach ISO 527-4 / EN 2561 mit einer Messgeschwindigkeit von 2 mm/min bei 23°C und einer relativen Luftfeuchtigkeit von 50%.The tensile shear strength of different test specimens was measured according to ISO 527-4 / EN 2561 with a measuring speed of 2 mm / min at 23 ° C. and a relative humidity of 50%.

Die Zugscherfestigkeit der Verklebung wurde dadurch geprüft, dass die durch das Gewebe SikaWrap-300C NW gebildete Schlaufe um ein mit dem beweglichen Rahmen der Prüfmaschine verbundenes Stahlrohr gelegt wurde. Der Betonwürfel wurde über eine aufgelegte Stahltraverse und Gewindestangen mit dem festen Rahmen der Prüfmaschine verbunden.The tensile shear strength of the bond was tested by placing the loop formed by the SikaWrap-300C NW fabric around a steel tube connected to the movable frame of the testing machine. The concrete cube was connected to the fixed frame of the testing machine via a steel crossbeam and threaded rods.

ResultateResults

Bohrungdrilling Nuten (Anzahl)Grooves (number) Material FaserbündelMaterial fiber bundle Maximale Last (kN)Maximum load (kN) Mittelwert (kN)Mean value (kN) Neinno KeineNo -- 36.136.1 37.137.1 40.340.3 34.934.9 JaYes KeineNo KohlefaserCarbon fiber 47.647.6 44.644.6 39.039.0 47.247.2 JaYes KeineNo Glasfaserglass fiber 54.954.9 52.652.6 50.650.6 52.252.2 JaYes 88th KohlefaserCarbon fiber 61.961.9 64.364.3 66.866.8 64.364.3 JaYes 88th Glasfaserglass fiber 70.970.9 63.863.8 56.856.8 63.763.7

BezugszeichenlisteList of reference symbols

11
TragstrukturSupport structure
22
Flächen (2a, 2b, 2c)Surfaces (2a, 2b, 2c)
33rd
Bohrung (3a, 3b, 3c)Bore (3a, 3b, 3c)
44th
Faserbündel bzw. FasersträngeFiber bundles or fiber strands
55
NutGroove
66th
LamelleLamella
77th
Gewebetissue
88th
KanteEdge
99
AbrundungRounding off
1010
BetonplatteConcrete slab
1111
VerstärkungsrippeReinforcement rib
1212th
Klebstoffadhesive

Claims (5)

  1. Arrangement comprising a supporting structure (1) with a surface consisting of a plurality of faces (2a, 2b, 2c), wherein a bore (3) runs from one of the faces into an inner region of the supporting structure (1), and said bore (3) is filled with an adhesive (12) and with a portion of a fibre bundle (4) protruding beyond said bore (3), wherein the supporting structure (1) on the one face (2a) from which the bore (3) runs into the inner region of the supporting structure (1) is provided with at least one groove (5) which, proceeding from the bore (3), extends in at least one direction on the surface, and the protruding part of the fibre bundle (4) is at least partially situated in the at least one groove (5) and is fastened in the latter with an adhesive (12), wherein a second bore (3b) runs from another face (2b, 2c) of the surface of the supporting structure (1) into the inner region of the supporting structure (1), and the at least one groove (5) runs from the point of entry of the one bore (3a) along the surface of the supporting structure (1) to the point of entry of the second bore (3b), wherein the protruding portion of the fibre bundle (4) runs at least partially in the at least one groove (5) and opens into the second bore (3b) and is fastened in the latter with an adhesive (12),
    characterized in that
    the other face is a face that faces away from the one face, in that the two bores (3b) in the extension of the respective bore axes thereof are connected to one another, and in that the groove (5) runs across at least one edge (8) which connects the two faces of the surface of the supporting structure (1) to one another.
  2. Arrangement according to one of the preceding claims, wherein this at least one edge (8) has a rounded portion (9) in the interior of the groove (5).
  3. Arrangement according to one of the preceding claims, wherein the surface of the supporting structure (1) is at least partially connected to at least one surface reinforcement, in particular to a lamella (6) and/or to at least one woven fabric (7), wherein the surface reinforcement, at least in the region of the fibre bundle (4) which has been fastened in the groove (5) by means of an adhesive (12), is adhesively bonded to the surface of the supporting structure (1).
  4. Arrangement according to one of the preceding claims, wherein the fibre bundle (4) is disposed such that the two ends thereof at least overlap, the fibre bundle (4) forming a closed loop.
  5. Arrangement according to Claim 4, wherein a length of the overlapping region of the fibre bundle (4) is 5 to 50 cm.
EP17163975.0A 2013-06-06 2014-06-06 Assembly for reinforcing support structures Active EP3216944B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP13170879 2013-06-06
PCT/EP2014/061915 WO2014195504A1 (en) 2013-06-06 2014-06-06 Arrangement and method for reinforcing supporting structures
EP14728978.9A EP3004490B1 (en) 2013-06-06 2014-06-06 Assembly and method for reinforcing support structures

Related Parent Applications (2)

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EP14728978.9A Division EP3004490B1 (en) 2013-06-06 2014-06-06 Assembly and method for reinforcing support structures
EP14728978.9A Division-Into EP3004490B1 (en) 2013-06-06 2014-06-06 Assembly and method for reinforcing support structures

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EP3216944A1 EP3216944A1 (en) 2017-09-13
EP3216944B1 true EP3216944B1 (en) 2021-09-29

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EP17163975.0A Active EP3216944B1 (en) 2013-06-06 2014-06-06 Assembly for reinforcing support structures

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JP (1) JP6437534B2 (en)
CN (2) CN107663953B (en)
AU (2) AU2014276778B2 (en)
BR (1) BR112015030524A2 (en)
CA (1) CA2914506C (en)
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Also Published As

Publication number Publication date
AU2017276343B2 (en) 2019-08-15
US20160138285A1 (en) 2016-05-19
CN107663953A (en) 2018-02-06
WO2014195504A1 (en) 2014-12-11
EP3216944A1 (en) 2017-09-13
CN105431601B (en) 2017-09-29
AU2014276778B2 (en) 2017-10-12
US9574359B2 (en) 2017-02-21
ES2900021T3 (en) 2022-03-15
EP3004490A1 (en) 2016-04-13
JP2016524669A (en) 2016-08-18
CA2914506C (en) 2022-09-06
JP6437534B2 (en) 2018-12-12
ES2646943T3 (en) 2017-12-18
CN107663953B (en) 2020-03-10
AU2017276343A1 (en) 2018-01-18
AU2014276778A1 (en) 2016-01-21
CA2914506A1 (en) 2014-12-11
BR112015030524A2 (en) 2017-07-25
EP3004490B1 (en) 2017-08-09
CN105431601A (en) 2016-03-23

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