EP2140077A1 - Reinforcing device for prefabricated parts - Google Patents

Reinforcing device for prefabricated parts

Info

Publication number
EP2140077A1
EP2140077A1 EP08700878A EP08700878A EP2140077A1 EP 2140077 A1 EP2140077 A1 EP 2140077A1 EP 08700878 A EP08700878 A EP 08700878A EP 08700878 A EP08700878 A EP 08700878A EP 2140077 A1 EP2140077 A1 EP 2140077A1
Authority
EP
European Patent Office
Prior art keywords
elements
connecting device
tension
tensile
reinforcing
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.)
Granted
Application number
EP08700878A
Other languages
German (de)
French (fr)
Other versions
EP2140077B1 (en
Inventor
Gerhard Maier
Erich Kastner
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
KAPPEMA FERTIGTEILINDUSTRIE GmbH
Original Assignee
Kastner Erich
Maier Gerhard
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Kastner Erich, Maier Gerhard filed Critical Kastner Erich
Publication of EP2140077A1 publication Critical patent/EP2140077A1/en
Application granted granted Critical
Publication of EP2140077B1 publication Critical patent/EP2140077B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/01Reinforcing elements of metal, e.g. with non-structural coatings
    • E04C5/06Reinforcing elements of metal, e.g. with non-structural coatings of high bending resistance, i.e. of essentially three-dimensional extent, e.g. lattice girders
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B28WORKING CEMENT, CLAY, OR STONE
    • B28BSHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
    • B28B23/00Arrangements specially adapted for the production of shaped articles with elements wholly or partly embedded in the moulding material; Production of reinforced objects
    • B28B23/0062Arrangements specially adapted for the production of shaped articles with elements wholly or partly embedded in the moulding material; Production of reinforced objects forcing the elements into the cast material, e.g. hooks into cast concrete
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B28WORKING CEMENT, CLAY, OR STONE
    • B28BSHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
    • B28B23/00Arrangements specially adapted for the production of shaped articles with elements wholly or partly embedded in the moulding material; Production of reinforced objects
    • B28B23/02Arrangements specially adapted for the production of shaped articles with elements wholly or partly embedded in the moulding material; Production of reinforced objects wherein the elements are reinforcing members
    • B28B23/028Arrangements specially adapted for the production of shaped articles with elements wholly or partly embedded in the moulding material; Production of reinforced objects wherein the elements are reinforcing members for double - wall articles
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B2/00Walls, e.g. partitions, for buildings; Wall construction with regard to insulation; Connections specially adapted to walls
    • E04B2/84Walls made by casting, pouring, or tamping in situ
    • E04B2/86Walls made by casting, pouring, or tamping in situ made in permanent forms
    • E04B2/8611Walls made by casting, pouring, or tamping in situ made in permanent forms with spacers being embedded in at least one form leaf
    • E04B2/8617Walls made by casting, pouring, or tamping in situ made in permanent forms with spacers being embedded in at least one form leaf with spacers being embedded in both form leaves
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/04Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of concrete or other stone-like material; of asbestos cement; of cement and other mineral fibres
    • E04C2/044Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of concrete or other stone-like material; of asbestos cement; of cement and other mineral fibres of concrete
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/04Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of concrete or other stone-like material; of asbestos cement; of cement and other mineral fibres
    • E04C2/06Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of concrete or other stone-like material; of asbestos cement; of cement and other mineral fibres reinforced
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • 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

Definitions

  • the present invention relates to a reinforcement device for prefabricated parts, which consists of a plurality of elements arranged substantially parallel to each other, which are made of hardenable casting compound and which are interconnected by at least one connecting device.
  • Reinforcement devices are known in high numbers and many embodiments.
  • the contact with the outer surfaces of the precast element to be cast should be minimal, and due to the 540 "twisting and bending, a better bond with the cast concrete should be produced, which should provide the highest possible additional strength and elasticity with least use of steel Advantages are given in the description there.
  • the invention is based on the object to provide a reinforcing device, which does not have the disadvantages of the prior art, and which, when used in the manufacture of finished parts and the latest regulations in terms of static, thermal insulation, corrosion resistance and the like but still a small mass points, low manufacturing costs and allows a simple and therefore cost-effective processing.
  • a reinforcement device for prefabricated parts which consists of a plurality of elements arranged substantially parallel to each other, which are made of hardenable casting compound and which are interconnected by at least one connecting device when the connecting device is formed two-dimensionally multi-dimensional and with the elements of hardenable casting material forms tension-resistant and shear-resistant composite.
  • a reinforcement device for prefabricated parts which consists of a plurality of substantially parallel elements arranged, which are made of curable casting compound and which are interconnected by at least one connecting device, when the connecting device of a composite of at least two tensile, pressure and There are shear elements, which can be arranged between the mutually parallel elements and anchored in the curable casting material.
  • connection device consists of a composite of at least two tensile and / or pressure elements, wherein the longitudinal axis of at least one tensile, compressive and shear element is substantially perpendicular to the plane of the parallel arranged elements ,
  • a reinforcing device is advantageous when the composite of the at least two tensile, compressive and shear elements is produced by a composite component, which is located between the ends of the tensile and compressive elements, and opposite spatially reset these ends, these ends are anchored in the curable casting.
  • the composite component is formed by a planar element having a wave-shaped cross section, or if it is formed by a planar element with a meandering cross section.
  • the composite component is formed by a flat element with a structured surface, or if the composite component is formed by a wire-like element.
  • Reinforcement devices are advantageously used when the connecting device are arranged in multiple execution between the mutually parallel elements and anchored in the curable casting composition.
  • connection devices For particularly favorable processing of connection devices, it is recommended that it can be magazineed in multiple designs.
  • a connecting device is configured particularly favorably when the composite component extends in a plane that runs perpendicularly between the elements arranged parallel to one another, and when the outer edges of the composite component facing the elements arranged parallel to one another can be anchored in their hardenable casting compound are.
  • the composite component extends in a plane which extends perpendicularly between the mutually parallel elements, wherein the mutually parallel elements facing outer edges of the composite component in the curable casting compound are anchored form-fitting manner.
  • a connecting device is also particularly advantageous if the tension and / or pressure elements can be arranged between the elements arranged parallel to one another and configured such that they can be anchored in a form-fitting manner in their hardenable casting compound.
  • tension and / or pressure elements are designed in several parts.
  • the tensile and / or pressure elements may advantageously consist of different materials.
  • the tensile and / or pressure elements may consist of fiber composite materials, or they may consist of metallic materials.
  • a connecting device can also be designed advantageously if the composite component is designed in several parts, wherein the composite component may consist of different materials. These materials may be fiber composite materials and / or metallic materials.
  • a connecting device can be configured if it consists of a combination of three tensile and / or pressure elements, wherein the longitudinal axis of a tensile and / or pressure element is substantially perpendicular to the plane of the mutually parallel elements, and the longitudinal axes of two other tensile and / or pressure elements at a small angle to the longitudinal axis of the vertical tension and / or pressure element.
  • An advantageous connecting device also results when it consists of a composite of several tensile and / or pressure elements, wherein the longitudinal axes of the tensile and / or pressure elements at a small angle to Senkrech- th run on the plane of the mutually parallel elements , Furthermore, it can be very advantageous if the connecting device consists of corrosion-resistant material or is corrosion-resistant surface-finished.
  • FIG. 1 shows a prefabricated part with a usable connection device
  • Figure 2 shows a prefabricated part with inserted connecting device in partial section
  • FIG. 3 shows a side view of the connecting device used in FIG. 2;
  • Figure 4 is a detail view of a unilaterally inserted connection device;
  • FIG. 5 shows a connecting device with a wave-shaped cross section
  • Figure 6 shows a variant of a connecting device with different tensile and / or pressure elements
  • FIG. 7 shows a further variant of a connecting device
  • FIG. 8 shows an additional variant of a connecting device
  • FIG. 9 shows a tension and / or pressure element
  • Figure 10 different multi-part tensile and / or pressure elements
  • Figure 11 different multi-part tensile and / or pressure elements made of different materials; 11 shows a further variant of a connecting device in two views;
  • FIG. 12 shows a detail of a cast-in connection device
  • Figure 14 shows a variant with inclined tensile and / or pressure elements;
  • Figure 15 shows a meander-shaped connecting device and
  • Figure 16 shows another variant with comb-like serrated outer edge.
  • FIG. 1 shows a prefabricated part 1 in the form of a double-walled wall.
  • a double-walled wall here consists for example of two mutually parallel elements 2 and 3, which are also referred to as inner 2 and outer shell 3.
  • inner 2 and outer shells 3 respectively mild steel or Baustahlgewebe 4, 5 is cast, each already in the production of the individual shells, as described in an earlier, but not yet published application of the applicant in detail.
  • the reference numeral 6 denotes a connecting device, which is shown above the prefabricated part 1.
  • the connecting device 6 has a plurality of tensile and / or pressure elements 7, which are interconnected by a composite component 8.
  • the composite component 8 is located between the free ends of the tension and / or pressure elements 7 and is spatially set back relative to these.
  • the connecting device 6 is in the case of an already completed wall - which was formed by the prefabricated part 1 - between the inner shell 2 and the outer shell 3, that is different from the illustration in Figure 1.
  • Figure 1 is to be illustrated in which Alignment, the connecting device 6 between the inner shell 2 and the outer shell 3 to be positioned.
  • An arrow 9 makes this clear.
  • the connecting device 6 positioned in its position between the inner shell 2 and the outer shell 3 and the bivalve wall is positioned vertically in the manufacture of the prefabricated part 1, it is filled with hardenable casting compound, here with concrete G.
  • the connecting device 6 then serves to stiffen the prefabricated building part 1, in that it has a multidimensional surface and forms a tension-proof and shear-resistant composite with the elements 2 and 3 of hardenable casting compound.
  • connecting device 6 shows a prefabricated part 1 with inserted connecting device 6 is illustrated in partial section, and in Figure 3, a connecting device 6, as used in the embodiment in Figure 2, shown in cross section.
  • the composite component 8 with its regions extending on the outer edges 10, is anchored in the mutually parallel inner and outer shells 2 and 3.
  • This anchoring takes place by insertion into the not yet cured casting compound G in the production of the individual inner and outer shells 2 and 3.
  • the tensile and / or pressure elements 7 dive far into the casting mass G.
  • the connecting device 6 has a multidimensional surface and, together with the inner and outer shells 2 and 3 of curable casting material G, forms a tension-proof and shear-resistant composite.
  • the tension and / or pressure elements 7 do not extend to the outer surfaces of the inner and outer shells 2 and 3.
  • a sufficient distance between the outer surfaces of the inner and outer shells 2 and 3 and the ends of the tensile, pressure elements 7 gives good corrosion protection and good thermal insulation, since cold bridges are avoided. If this requirement is not met, the tensile and / or pressure elements can also penetrate to the outer surfaces of the inner and outer shell 2 and 3.
  • the connecting device 6 with the tensile and pressure-resistant elements 7 made of corrosion-resistant material or corrosion resistant surface-finished.
  • the regions of the outer edges 10 of the composite component 8 are anchored in the manufacture of the elements that make up the inner and outer shells 2 and 3, in this.
  • Each of the elements 2 or 3 is poured in a mold.
  • the already finished element 2 is inserted with the connecting devices 6 and the tensile and / or pressure elements 7 ahead in the not yet cured casting G of the second element 3, until the still free outer edge 11 of the composite component 8 also in this element 3 abuts the Baustahlgewebe 5 and rests there.
  • the casting compound G of the second element 3 hardens and a reinforced double-shell prefabricated part 1 is produced.
  • This double-shell prefabricated part 1 is taken out of the mold, placed vertically and is in the position as shown in Figure 2.
  • the connecting device 6 in each case with the areas of the outer edges 10 and 11 of their composite component 8 in the hardened casting composition G of the inner and outer shells 2 and 3 is anchored, wherein the connecting device 6 has a multi-dimensional surface, forms a tensile and shear bond with the elements 2 and 3 of hardenable casting compound and makes a significant contribution to stability of prefabricated part 1 contributes.
  • FIG. 5 shows a connection device 6 in a perspective view.
  • This connecting device 6 corresponds to the previously described connecting devices 6 from FIGS. 1 to 4; it is shown in cross-section in FIG.
  • the waveform of the cross section of their composite component 8 is particularly well suited to ensure the prefabricated part 1 sufficient stability with low weight, ease of use and low cost.
  • the material suitable for this embodiment any material with sufficient strength, standard corrugated metal appears particularly advantageous.
  • the design of the tension and / or pressure elements 7 is rod-cylindrical in this embodiment. They are attached to the composite component 8 in any suitable manner
  • FIG. 6 illustrates a variant of a connecting device 12, in which the wave-shaped composite component 13 is made of stronger material, for example fiber-composite material.
  • this fiber composite material can be arbitrarily shaped tensile and / or pressure elements insert.
  • several examples are shown here simultaneously on a composite component 13.
  • the reference numeral 14 is a train and / or
  • the reference numeral 15 stands for a club-shaped tension and / or pressure element.
  • 16 designates a short-wave bent tensile and / or pressure element and 17 represents a rod-shaped, cylindrical tensile and / or pressure element, as in FIG. 5.
  • Reference numeral 18 denotes a tensile and / or pressure element bent in the long-wave 19 stands for a serrated pulling and / or pressure element.
  • the respective cross sections are adapted to the shape.
  • a connecting device 20 in a further variant of a connecting device 20 according to FIG. 7, it is shown that still other embodiments for tension and / or pressure elements are conceivable.
  • the anchoring in the casting material G is further improved.
  • rod-shaped cylindrical tensile and / or pressure elements are referred to with different diameters.
  • the reference numerals 25 and 26 are helical tensile and / or pressure elements with different cross-sections, also jagged tensile and / or pressure elements with 27 and meandering tensile and / or pressure elements 28 are designated.
  • FIG. 8 shows a further variant of a connecting device 29, which essentially corresponds to the connecting device 20 according to FIG.
  • the composite component 30 has no breakthroughs with respect to the connecting device 20, the tensile and / or pressure elements correspond largely as possible and are therefore provided with the same reference numerals.
  • Figure 9 shows a tension and / or pressure element 31, which is rod-shaped cylindrical, and at its front ends each carrying a tuft of wires 32, which may be welded, for example.
  • FIG. 10 shows that a tensile and / or pressure element 33 can also be joined together from a plurality of individual parts.
  • a hollow cylindrical central portion 33a in each of which a respective one End piece 33b and 33c can be introduced by means of an unspecified approach.
  • These three individual parts combine to form a complete tensile and / or pressure element 33, wherein the end pieces 33b and 33c can be beveled at their respective free end faces.
  • Such variations are particularly useful when the middle parts and the end pieces are made of different materials, or if they have different surface finish.
  • the end pieces may, for example, be roughened or otherwise structured in order to be better anchored in the casting compound G.
  • FIG. 11 A very similar variant is shown in Figure 11:
  • there is a hollow cylindrical central portion 34a in each of which an end piece 34b and 34c can be introduced from both ends by means of an unspecified approach.
  • These three individual parts combine to form a complete tensile and / or pressure element 34, wherein the end pieces 34b and 34c can be beveled at their respective free end faces.
  • end piece 34e and 34f can be attached.
  • Such variations are particularly useful when the middle parts and the end pieces are made of different materials, or if they have different surface finish.
  • the end pieces can be sanded, for example, in order to be better anchored in the casting material G.
  • FIG. 12 once again shows a detail of an inner shell 2 in which a tensile and / or pressure element 35 is anchored in the casting compound G.
  • the front of the train and / or Pressure element 35 has a teardrop-shaped end portion 36 which is positively fixed in the casting mass G.
  • the unspecified outer edge of a composite component which is likewise not designated in more detail, is likewise anchored in the casting compound in a manner already described and largely corresponds to the above-described exemplary embodiments.
  • FIG. 13 very schematically shows an advantageous further development of a connecting device according to the invention:
  • a number of tension and / or pressure elements 37, 38, 39 are connected to one another by a composite component 40.
  • the composite component is realized here as an arrangement of parallel wires 40.
  • additional wireforms 41 may be provided. This embodiment illustrates the possibility of winding a plurality of connecting devices on a roll and thus make it magazinierbar.
  • the tension and / or pressure elements 42, 43, 44 can also assume small angles relative to one another, and that they can be connected to one another by a metal strip 45.
  • the weight is extremely reduced, which ensures lowest material consumption and lowest cost with sufficient strength.
  • the surface of the tensile and / or pressure elements can be structured in any desired manner.
  • a connecting device 46 can be realized, in which the composite component 47 has a meandering cross section.
  • the tension and / or pressure elements 48, 49 and 50 are inserted into the meander suitable and can be configured arbitrarily.
  • FIG. 1 Another embodiment is shown in FIG.
  • a formwork plate 51 which is a part of a casting mold, as already described above, is a structural steel tissue 52 placed.
  • This Baustahlgewebe 52 stabilizes the inner or outer shell, which is to be poured.
  • a connecting device 53 is provided with rectangular cutouts 54 into which the rods 57 of the structural steel fabric 52 project. Cutouts may also be formed as comb-like cutouts 55 and form the edge of the connecting device 53.
  • the comb-like cutouts 55 engage in the reinforcement formed by the reinforcing steel mesh of the second inner shell or outer shell to be cast later.
  • a composite of pressure and / or tension elements is provided in this embodiment by a continuous, flat structure 58, which is stabilized by a band as a composite component 59.
  • end piece 34 multi-part tension and / or pressure element

Abstract

The invention relates to a reinforcing device (6) for prefabricated parts (1), which comprise a plurality of elements (2, 3) that are arranged substantially parallel to each other, produced of a casting compound (G) that can be hardened, and are connected to each other by at least one connecting device (6). The connecting device (6) is implemented by tensile, pressure, and shearing elements (7) that are connected to each other by means of a composite component (8), wherein the ends of the tensile and pressure elements (8) and also the edges of the composite components (8) are anchored in the casting compound (G) of the elements (2, 3) that are arranged substantially parallel to each other.

Description

Beschreibungdescription
Bewehrungsvorrichtung für Fertigbau-TeileReinforcement device for prefabricated parts
Die vorliegende Erfindung bezieht sich auf eine Bewehrungsvorrichtung für Fertigbau-Teile, welche aus mehreren weitgehend parallel zueinander angeordneten Elementen besteht, die aus aushärtbarer Gießmasse hergestellt und die durch wenigstens eine Verbindungsvorrichtung miteinander verbunden sind.The present invention relates to a reinforcement device for prefabricated parts, which consists of a plurality of elements arranged substantially parallel to each other, which are made of hardenable casting compound and which are interconnected by at least one connecting device.
Bewehrungsvorrichtungen sind in hoher Zahl und vielen Ausführungsformen bekannt.Reinforcement devices are known in high numbers and many embodiments.
Aus der DE 2 139 197 Al ist es bekannt bei Bauten mit verlo- rener Schalung zwei gegossene oder gespritzte Schalungswände als verlorene Schalung vorzusehen und ein Baustahlgewebe in die gegossenen Schalungswände so einzusetzen, dass die Knotenpunkte in den noch flüssigen Kunststoff der Schalungswände eingedrückt werden, so dass die Knotenpunkte der Bewehrungs- stäbe des Baustahlgewebes nach dem Aushärten von dem Kunststoff vollkommen umschlossen sind. Baustahlgewebe ist in seiner Handhabung schwierig und muss im Einzelfall nach den Erfordernissen individuell angepasst werden, was eine rationelle Produktion von Fertigteilen erschwert und verteuert.It is known from DE 2 139 197 Al in buildings with lost formwork to provide two cast or sprayed formwork walls as permanent formwork and to use a structural steel mesh in the cast shuttering walls in such a way that the nodal points are pressed into the still liquid plastic of the formwork walls that the nodal points of the reinforcing bars of Baustahlgewebes are completely enclosed by the plastic after curing. Structural steel mesh is difficult to handle and must be adapted to the individual requirements of the individual case, which complicates a rational production of finished parts and expensive.
Eine weitere Lösung für das Herstellen von Fertigteilen im Baugewerbe wird in der DE 2 305 651 Al gezeigt und beschrieben. Auch dort werden die Nachteile von Moniereisen- Einlagerungen und von Baustahlgewebe ausführlich erörtert, wobei in dieser Druckschrift insbesondere die umständliche, teure und zeitraubende Vorbereitung und Verarbeitung aufgeführt werden. Demgegenüber soll mit der dort beschriebenen Erfindung die Herstellung von gießfertigem Stahlbeton dadurch erleichtert werden, dass Verfestigungselemente, z.B. Stahl- Stäbchen dem Gießbeton in kleinen und/oder größeren Ausführungen beim Gießen beigemischt werden. Die Stahlstäbchen sollen besonders geformt sein. Als beispielhafte Verformungen ist dort angegeben, dass sie derart oberflächenverformt sein sollen, dass sie fortlaufend in axialer Richtung ihren Querschnitt in zügigem Übergang fortlaufend von flach zu Vierkant zu rund und wieder zu vierkant zu flach jeweils um die Achse verdrehen - vorzugsweise um 180° - und so wiederholend verformt werden, wobei der Materialquerschnitt in etwa immer in gleicher Querschnittsgröße bleibt. Diese fortlaufend verformten Stäbchen werden in ihrer Längsachse so verbogen, dass jedes Stäbchen eine flache, spiralige Form einnimmt, wobei die Verdrehung dieser Spirale vorzugsweise ca. 1 1/2 Umdrehungen beträgt, also um ca. 540° gedreht ist. Verständlich wird die Formgebung der beschriebenen Stäbchen durch die dort beigefügten Zeichnungen. Als Vorteile werden dort eine verringerte Sinkgeschwindigkeit im Gießbeton aufgrund der besonderen Formgebung angeführt. Außerdem soll der Kontakt zu den Außenflächen des zu gießenden Fertigteils minimal sein, sowie aufgrund der 540"-Verdrehung und der Verbiegung ein besserer Verbund mit dem Gießbeton hergestellt werden, was bei geringstem Einsatz von Stahl die höchstmögliche Zusatzfestig- keit und Elastizität erbringen soll. Weitere Vorteile sind in der dortigen Beschreibung angegeben.Another solution for the manufacture of precast elements in the construction industry is shown and described in DE 2 305 651 A1. There, too, the disadvantages of Moniereisen- deposits and Baustahlgewebe are discussed in detail, in particular, the cumbersome, expensive and time-consuming preparation and processing are listed in this document. In contrast, the production of cast-ready reinforced concrete should be facilitated by the invention described therein that hardening elements, such as steel rods are added to the cast concrete in small and / or larger versions during casting. The steel rods should be specially shaped. As exemplary deformations is there specified that they should be so surface deformed that they continuously in the axial direction of their cross section in a smooth transition continuously from flat to square to round and again to square too flat respectively about the axis twist - preferably 180 ° - and so repeatedly deformed be, with the material cross section remains approximately always in the same cross-sectional size. These continuously deformed rods are bent in their longitudinal axis so that each rod occupies a flat, spiral shape, wherein the rotation of this spiral is preferably about 1 1/2 revolutions, that is rotated by about 540 °. Understandably, the shape of the rods described by the drawings attached there. As advantages, a reduced rate of sinking in cast concrete due to the special shape are cited there. In addition, the contact with the outer surfaces of the precast element to be cast should be minimal, and due to the 540 "twisting and bending, a better bond with the cast concrete should be produced, which should provide the highest possible additional strength and elasticity with least use of steel Advantages are given in the description there.
Aus dieser Druckschrift ist allerdings nicht ersichtlich, wie die statische Stabilität der zu gießenden Fertigteile gezielt bestimmt werden könnte. Ferner ist nicht zu entnehmen, dass ein definierter Verbund von Außenschalen und Gießbeton zustande kommen könnte. Zusammengefasst ist der Druckschrift nicht zu entnehmen, wie Bewehrungselemente ausgestaltet sein könnten, welche in mehrschaligen Fertigteilen einsetzbar sind und deren Festigkeit definiert bestimmbar ist.From this document, however, it is not apparent how the static stability of the finished parts to be cast could be determined specifically. Furthermore, it can not be deduced that a defined combination of outer shells and cast concrete could come about. In summary, the document does not show how reinforcing elements could be designed, which can be used in multi-shell prefabricated parts and their strength can be determined defined.
Demgegenüber liegt der Erfindung die Aufgabe zu Grunde, eine Bewehrungsvorrichtung zu schaffen, welche die Nachteile des Stands der Technik nicht aufweist, und die beim Einsatz in der Fertigteile-Herstellung auch den neuesten Vorschriften hinsichtlich Statik, Wärmedämmung, Korrosionsfestigkeit und dgl. Rechnung trägt, die aber dennoch eine geringe Masse auf- weist, geringe Kosten bei der Herstellung verursacht und eine einfache und damit kostengünstige Verarbeitung erlaubt.In contrast, the invention is based on the object to provide a reinforcing device, which does not have the disadvantages of the prior art, and which, when used in the manufacture of finished parts and the latest regulations in terms of static, thermal insulation, corrosion resistance and the like but still a small mass points, low manufacturing costs and allows a simple and therefore cost-effective processing.
Diese Aufgabe wird durch eine Vorrichtung mit den Merkmalen des Anspruchs 1 gelöst. Vorteilhafte Weiterbildungen sind den abhängigen Ansprüchen zu entnehmen.This object is achieved by a device having the features of claim 1. Advantageous developments can be found in the dependent claims.
Sehr vorteilhaft ist eine Bewehrungsvorrichtung für Fertigbau-Teile, welche aus mehreren weitgehend parallel zueinander angeordneten Elementen besteht, die aus aushärtbarer Gießmasse hergestellt und die durch wenigstens eine Verbindungsvorrichtung miteinander verbunden sind, wenn die Verbindungsvorrichtung flächig mehrdimensional ausgebildet ist und mit den Elementen aus aushärtbarer Gießmasse einen zug- druck- und scherfesten Verbund bildet.Very advantageous is a reinforcement device for prefabricated parts, which consists of a plurality of elements arranged substantially parallel to each other, which are made of hardenable casting compound and which are interconnected by at least one connecting device when the connecting device is formed two-dimensionally multi-dimensional and with the elements of hardenable casting material forms tension-resistant and shear-resistant composite.
Besonders vorteilhaft ist eine Bewehrungsvorrichtung für Fertigbau-Teile, welche aus mehreren weitgehend parallel zueinander angeordneten Elementen besteht, die aus aushärtbarer Gießmasse hergestellt und die durch wenigstens eine Verbindungsvorrichtung miteinander verbunden sind, wenn die Verbindungsvorrichtung aus einem Verbund von wenigstens zwei Zug-, Druck- und Scherelementen besteht, die zwischen den parallel zueinander angeordneten Elemente anordbar und die in deren aushärtbarer Gießmasse verankerbar sind.Particularly advantageous is a reinforcement device for prefabricated parts, which consists of a plurality of substantially parallel elements arranged, which are made of curable casting compound and which are interconnected by at least one connecting device, when the connecting device of a composite of at least two tensile, pressure and There are shear elements, which can be arranged between the mutually parallel elements and anchored in the curable casting material.
Vorteilhaft ist eine Bewehrungsvorrichtung auch dann, wenn die Verbindungsvorrichtung aus einem Verbund von wenigstens zwei Zug- und/oder Druckelementen besteht, wobei die Längs- achse von wenigstens einem Zug-, Druck- und Scherelement im Wesentlichen senkrecht zur Ebene der parallel zueinander angeordneten Elemente verläuft.A reinforcement device is also advantageous if the connection device consists of a composite of at least two tensile and / or pressure elements, wherein the longitudinal axis of at least one tensile, compressive and shear element is substantially perpendicular to the plane of the parallel arranged elements ,
Außerdem ist ein Bewehrungsvorrichtung vorteilhaft, wenn der Verbund der wenigstens zwei Zug-, Druck und Scherelemente durch ein Verbund-Bauteil erzeugt wird, welches sich zwischen den Enden der Zug- und Druckelemente befindet, und gegenüber diesen Enden räumlich zurückgesetzt ist, wobei diese Enden in der aushärtbaren Gießmasse verankerbar sind.In addition, a reinforcing device is advantageous when the composite of the at least two tensile, compressive and shear elements is produced by a composite component, which is located between the ends of the tensile and compressive elements, and opposite spatially reset these ends, these ends are anchored in the curable casting.
Sehr vorteilhaft ist es, wenn das Verbund-Bauteil durch ein flächiges Element mit wellenförmigem Querschnitt gebildet wird, oder wenn es durch ein flächiges Element mit mäander- förmigem Querschnitt gebildet wird.It is very advantageous if the composite component is formed by a planar element having a wave-shaped cross section, or if it is formed by a planar element with a meandering cross section.
Außerdem kann es vorteilhaft sein, wenn das Verbund-Bauteil durch ein flächiges Element mit strukturierter Oberfläche gebildet wird, oder wenn das Verbund-Bauteil durch ein drahtartiges Element gebildet wird.Moreover, it can be advantageous if the composite component is formed by a flat element with a structured surface, or if the composite component is formed by a wire-like element.
Bewehrungsvorrichtungen sind dann mit Vorteil einsetzbar, wenn die Verbindungsvorrichtung in mehrfacher Ausführung zwischen den parallel zueinander angeordneten Elemente angeordnet und in deren aushärtbarer Gießmasse verankert sind.Reinforcement devices are advantageously used when the connecting device are arranged in multiple execution between the mutually parallel elements and anchored in the curable casting composition.
Zur besonders günstigen Verarbeitung von Verbindungsvorrich- tungen empfiehlt es sich, dass sie in mehrfacher Ausführung magazinierbar ist.For particularly favorable processing of connection devices, it is recommended that it can be magazineed in multiple designs.
Eine Verbindungsvorrichtung ist dann besonders günstig ausgestaltet, wenn sich das Verbund-Bauteil in einer Ebene er- streckt, die senkrecht zwischen den parallel zueinander angeordneten Elemente verläuft, und wenn die den parallel zueinander angeordneten Elementen zugewandten Außenkanten des Verbund-Bauteils in deren aushärtbarer Gießmasse verankerbar sind.A connecting device is configured particularly favorably when the composite component extends in a plane that runs perpendicularly between the elements arranged parallel to one another, and when the outer edges of the composite component facing the elements arranged parallel to one another can be anchored in their hardenable casting compound are.
Darüber hinaus ist es vorteilhaft, wenn sich das Verbund- Bauteil in einer Ebene erstreckt, die senkrecht zwischen den parallel zueinander angeordneten Elemente verläuft, wobei die den parallel zueinander angeordneten Elementen zugewandten Außenkanten des Verbund-Bauteils in deren aushärtbarer Gießmasse formschlüssig verankerbar sind. Besonders vorteilhaft ist eine Verbindungsvorrichtung auch dann, wenn die Zug- und/oder Druckelemente zwischen den parallel zueinander angeordneten Elemente anordbar und so ausgebildet sind, dass sie in deren aushärtbarer Gießmasse formschlüssig verankerbar sind.Moreover, it is advantageous if the composite component extends in a plane which extends perpendicularly between the mutually parallel elements, wherein the mutually parallel elements facing outer edges of the composite component in the curable casting compound are anchored form-fitting manner. A connecting device is also particularly advantageous if the tension and / or pressure elements can be arranged between the elements arranged parallel to one another and configured such that they can be anchored in a form-fitting manner in their hardenable casting compound.
Ebenso kann es von Vorteil sein, wenn die Zug- und/oder Druckelemente mehrteilig ausgeführt sind.It may also be advantageous if the tension and / or pressure elements are designed in several parts.
Die Zug- und/oder Druckelemente können in vorteilhafter Weise aus unterschiedlichen Werkstoffen bestehen. Beispielsweise können die Zug- und/oder Druckelemente aus Faserverbund- Werkstoffen bestehen, oder sie können aus metallischen Werkstoffen bestehen.The tensile and / or pressure elements may advantageously consist of different materials. For example, the tensile and / or pressure elements may consist of fiber composite materials, or they may consist of metallic materials.
Eine Verbindungsvorrichtung kann auch vorteilhaft gestaltet sein, wenn das Verbund-Bauteil mehrteilig ausgeführt ist, wobei das Verbund-Bauteil aus unterschiedlichen Werkstoffen bestehen kann. Diese Werkstoffe können Faserverbund-Werkstoffe und/oder metallische Werkstoffen sein.A connecting device can also be designed advantageously if the composite component is designed in several parts, wherein the composite component may consist of different materials. These materials may be fiber composite materials and / or metallic materials.
Sehr vorteilhaft kann eine Verbindungsvorrichtung ausgestaltet sein, wenn sie aus einem Verbund von drei Zug- und/oder Druckelementen besteht, wobei die Längsachse von einem Zug- und/oder Druckelement im Wesentlichen senkrecht zur Ebene der parallel zueinander angeordneten Elemente verläuft, und die Längsachsen der beiden anderen Zug- und/oder Druckelemente unter einem kleinen Winkel zur Längsachse des senkrechten Zug- und/oder Druckelements verlaufen.Very advantageously, a connecting device can be configured if it consists of a combination of three tensile and / or pressure elements, wherein the longitudinal axis of a tensile and / or pressure element is substantially perpendicular to the plane of the mutually parallel elements, and the longitudinal axes of two other tensile and / or pressure elements at a small angle to the longitudinal axis of the vertical tension and / or pressure element.
Eine vorteilhafte Verbindungsvorrichtung ergibt sich auch dann, wenn sie aus einem Verbund von mehreren Zug- und/oder Druckelementen besteht, wobei die Längsachsen der Zug- und/oder Druckelemente in einem kleinen Winkel zur Senkrech- ten auf die Ebene der parallel zueinander angeordneten Elemente verlaufen. Ferner kann es sehr vorteilhaft sein, wenn die Verbindungsvorrichtung aus korrosionsfestem Werkstoff besteht oder korrosionsfest oberflächenveredelt ist.An advantageous connecting device also results when it consists of a composite of several tensile and / or pressure elements, wherein the longitudinal axes of the tensile and / or pressure elements at a small angle to Senkrech- th run on the plane of the mutually parallel elements , Furthermore, it can be very advantageous if the connecting device consists of corrosion-resistant material or is corrosion-resistant surface-finished.
Mit Hilfe von Ausführungsbeispielen wird die Erfindung nachstehend anhand von Zeichnungen noch näher erläutert.With the aid of exemplary embodiments, the invention will be explained in more detail below with reference to drawings.
Es zeigtIt shows
Figur 1 ein Fertigbau-Teil mit einsatzfähiger Verbin- dungsVorrichtung;FIG. 1 shows a prefabricated part with a usable connection device;
Figur 2 ein Fertigbau-Teil mit eingesetzter Verbindungsvorrichtung im Teilschnitt;Figure 2 shows a prefabricated part with inserted connecting device in partial section;
Figur 3 eine Seitenansicht der in Figur 2 eingesetzten Verbindungsvorrichtung; Figur 4 eine Detailansicht einer einseitig eingesetzten VerbindungsVorrichtung;FIG. 3 shows a side view of the connecting device used in FIG. 2; Figure 4 is a detail view of a unilaterally inserted connection device;
Figur 5 eine Verbindungsvorrichtung mit wellenförmigem Querschnitt; Figur 6 eine Variante einer Verbindungsvorrichtung mit unterschiedlichen Zug- und/oder Druckelementen;FIG. 5 shows a connecting device with a wave-shaped cross section; Figure 6 shows a variant of a connecting device with different tensile and / or pressure elements;
Figur 7 eine weitere Variante einer Verbindungsvorrichtung;FIG. 7 shows a further variant of a connecting device;
Figur 8 eine zusätzliche Variante einer Verbindungsvorrichtung; Figur 9 ein Zug- und/oder Druckelement;FIG. 8 shows an additional variant of a connecting device; FIG. 9 shows a tension and / or pressure element;
Figur 10 verschiedene mehrteilige Zug- und/oder Druckelemente;Figure 10 different multi-part tensile and / or pressure elements;
Figur 11 verschiedene mehrteilige Zug- und/oder Druckelemente aus verschiedenen Werkstoffen; Figur 11 eine weitere Variante einer Verbindungsvorrichtung in zwei Ansichten;Figure 11 different multi-part tensile and / or pressure elements made of different materials; 11 shows a further variant of a connecting device in two views;
Figur 12 eine Einzelheit einer eingegossenen Verbindungsvorrichtung; Figur 13 Zug- und/oder Druckelemente in magazinierbarer Mehrfach-Anordnung;FIG. 12 shows a detail of a cast-in connection device; Figure 13 tensile and / or pressure elements in magazinierbarer multiple arrangement;
Figur 14 eine Variante mit schräg gestellten Zug- und/oder Druckelementen; Figur 15 eine mäanderförmige Verbindungsvorrichtung und Figur 16 eine weitere Variante mit kammartig gezacktem Außenrand.Figure 14 shows a variant with inclined tensile and / or pressure elements; Figure 15 shows a meander-shaped connecting device and Figure 16 shows another variant with comb-like serrated outer edge.
In Figur 1 ist ein Fertigbau-Teil 1 in Form einer doppelscha- ligen Wand dargestellt. Eine doppelschalige Wand besteht hier beispielsweise aus zwei parallel zueinander angeordneten Elementen 2 und 3, die auch als Innen- 2 und Außenschale 3 bezeichnet werden. In die beiden Innen- 2 und Außenschalen 3 ist jeweils Baustahl bzw. Baustahlgewebe 4, 5 eingegossen, und zwar jeweils bereits bei der Herstellung der einzelnen Schalen, wie dies in einer früheren, jedoch noch nicht veröffentlichten Anmeldung der Anmelder im Detail beschrieben ist. Mit dem Bezugszeichen 6 ist eine Verbindungsvorrichtung be- zeichnet, die oberhalb des Fertigbau-Teils 1 dargestellt ist. Die Verbindungsvorrichtung 6 weist mehrere Zug- und/oder Druckelemente 7 auf, welche durch ein Verbund-Bauteil 8 miteinander verbunden sind. Das Verbund-Bauteil 8 befindet sich zwischen den freien Enden der Zug- und/oder Druckelemente 7 und ist gegenüber diesen räumlich zurückgesetzt. Die Verbindungsvorrichtung 6 befindet sich im Falle einer bereits fertig gestellten Wand - die durch das Fertigbau-Teil 1 gebildet wurde - zwischen der Innenschale 2 und der Außenschale 3, also abweichend von der Darstellung in Figur 1. In Figur 1 soll veranschaulicht werden, in welcher Ausrichtung die Verbindungsvorrichtung 6 zwischen der Innenschale 2 und der Außenschale 3 positioniert werden soll. Ein Pfeil 9 macht dies deutlich. Nachdem die Verbindungsvorrichtung 6 bei der Herstellung des Fertigbau-Teils 1 in seiner Lage zwischen der Innenschale 2 und der Außenschale 3 positioniert und die zweischalige Wand senkrecht aufgestellt ist, wird diese mit aushärtbarer Gießmasse, hier mit Beton G, ausgegossen. Die Verbindungsvorrichtung 6 dient dann zur Versteifung des Fertigbau-Teils 1, indem sie flächig mehrdimensional ausgebildet ist und mit den Elementen 2 und 3 aus aushärtbarer Gießmasse einen zug- druck- und scherfesten Verbund bildet. In Figur 2 ist ein Fertigbau-Teil 1 mit eingesetzter Verbindungsvorrichtung 6 im Teilschnitt veranschaulicht, und in Figur 3 ist eine Verbindungsvorrichtung 6, wie sie bei dem Ausführungsbeispiel in Figur 2 eingesetzt ist, im Querschnitt dargestellt. Wie in Figur 2 veranschaulicht, ist das Verbund- Bauteil 8 mit seinen an den Außenkanten 10 verlaufenden Bereichen in den parallel zueinander stehenden Innen- und Außenschalen 2 und 3 verankert. Diese Verankerung erfolgt durch Einsetzen in die noch nicht ausgehärtete Gießmasse G bei der Herstellung der einzelnen Innen- und Außenschalen 2 und 3. Dabei tauchen die Zug- und/oder Druckelemente 7 weit in die Gießmasse G ein. Vorteilhafter Weise ist die Verbindungsvorrichtung 6 flächig mehrdimensional ausgebildet und bildet mit den Innen- und Außenschalen 2 und 3 aus aushärtbarer Gießmas- se G einen zug- druck- und scherfesten Verbund. Von Vorteil ist es, wenn die Zug- und/oder Druckelemente 7 nicht bis zu den Außenflächen der Innen- und Außenschalen 2 und 3 reichen. Ein hinreichender Abstand zwischen den Außenflächen der Innen- und Außenschalen 2 und 3 und den Enden der Zug-, Druck- elemente 7 ergibt einen guten Korrosionsschutz und eine gute Wärmedämmung, da Kältebrücken vermieden werden. Wenn diese Maßgabe nicht erfüllt sein muss, können die Zug- und/oder Druckelemente auch bis zu den Außenflächen der Innen- und Außenschale 2 und 3 durchdringen. Vorteilhafter Weise kann die Verbindungsvorrichtung 6 mit den zug- und druckfesten Elemente 7 aus korrosionsbeständigem Werkstoff bestehen oder korrosionsfest oberflächenveredelt sein. Die Bereiche der Außenkanten 10 des Verbund-Bauteils 8 werden bei der Herstellung der Elemente, aus denen die Innen- und die Außenschalen 2 und 3 bestehen, in diesen verankert. Jedes der Elemente 2 oder 3 wird in einer Form gegossen.FIG. 1 shows a prefabricated part 1 in the form of a double-walled wall. A double-walled wall here consists for example of two mutually parallel elements 2 and 3, which are also referred to as inner 2 and outer shell 3. In the two inner 2 and outer shells 3 respectively mild steel or Baustahlgewebe 4, 5 is cast, each already in the production of the individual shells, as described in an earlier, but not yet published application of the applicant in detail. The reference numeral 6 denotes a connecting device, which is shown above the prefabricated part 1. The connecting device 6 has a plurality of tensile and / or pressure elements 7, which are interconnected by a composite component 8. The composite component 8 is located between the free ends of the tension and / or pressure elements 7 and is spatially set back relative to these. The connecting device 6 is in the case of an already completed wall - which was formed by the prefabricated part 1 - between the inner shell 2 and the outer shell 3, that is different from the illustration in Figure 1. In Figure 1 is to be illustrated in which Alignment, the connecting device 6 between the inner shell 2 and the outer shell 3 to be positioned. An arrow 9 makes this clear. After the connecting device 6 positioned in its position between the inner shell 2 and the outer shell 3 and the bivalve wall is positioned vertically in the manufacture of the prefabricated part 1, it is filled with hardenable casting compound, here with concrete G. The connecting device 6 then serves to stiffen the prefabricated building part 1, in that it has a multidimensional surface and forms a tension-proof and shear-resistant composite with the elements 2 and 3 of hardenable casting compound. 2 shows a prefabricated part 1 with inserted connecting device 6 is illustrated in partial section, and in Figure 3, a connecting device 6, as used in the embodiment in Figure 2, shown in cross section. As illustrated in FIG. 2, the composite component 8, with its regions extending on the outer edges 10, is anchored in the mutually parallel inner and outer shells 2 and 3. This anchoring takes place by insertion into the not yet cured casting compound G in the production of the individual inner and outer shells 2 and 3. In this case, the tensile and / or pressure elements 7 dive far into the casting mass G. Advantageously, the connecting device 6 has a multidimensional surface and, together with the inner and outer shells 2 and 3 of curable casting material G, forms a tension-proof and shear-resistant composite. It is advantageous if the tension and / or pressure elements 7 do not extend to the outer surfaces of the inner and outer shells 2 and 3. A sufficient distance between the outer surfaces of the inner and outer shells 2 and 3 and the ends of the tensile, pressure elements 7 gives good corrosion protection and good thermal insulation, since cold bridges are avoided. If this requirement is not met, the tensile and / or pressure elements can also penetrate to the outer surfaces of the inner and outer shell 2 and 3. Advantageously, the connecting device 6 with the tensile and pressure-resistant elements 7 made of corrosion-resistant material or corrosion resistant surface-finished. The regions of the outer edges 10 of the composite component 8 are anchored in the manufacture of the elements that make up the inner and outer shells 2 and 3, in this. Each of the elements 2 or 3 is poured in a mold.
Dieses Verfahren ist allgemein bekannt und soll hier ohne Anspruch auf Vollständigkeit anhand von Figur 4 nur kurz aufge- führt werden, um anschließend das Einsetzen der erfindungsgemäßen Verbindungsvorrichtungen 6 erläutern zu können. In eine waagerecht liegende Form, welche eine im allgemeinen glatte Schalungsfläche aufweist, wird Beton oder eine andere aushärtbare Gießmasse G bis zu einer vorbestimmbaren Höhe eingefüllt. Die so entstehende Platte aus Beton oder einer anderen aushärtbaren Gießmasse wird mit einer Bewehrung aus Baustahl bzw. Baustahlgewebe 4 versehen und diese durch weiteres Be- füllen der Form mit Beton oder einer anderen aushärtbaren Gießmasse G eingegossen. In diese waagerecht liegende, noch nicht ausgehärtete Platte aus gegossenem Beton oder einer anderen aushärtbaren Gießmasse G werden die erfindungsgemäßen Verbindungsvorrichtungen 6 eingesetzt. Dies geschieht derart, dass wenigstens eine Verbindungsvorrichtung 6 mit den Zug- und/oder Druckelementen 7 voran in die noch nicht ausgehärtete Gießmasse G eingedrückt wird. Die Zug- und/oder Druckelemente 7 gleiten dabei an dem als Bewehrung eingegossenen Bau- stahlgewebe 4 vorbei und die Außenkante 10 des Verbund- Bauteils 8 der Verbindungsvorrichtung 6 taucht in die Gießmasse G soweit ein, bis sie in Kontakt mit dem Baustahlgewebe 4 bekommt und dort aufliegt. Anschließend härtet die Gießmasse G aus . Nach dem Aushärten wird das Element 2 aus der Form entnommen, diese gesäubert und eine neue Schicht Gießmasse wird zur Herstellung eines weiteren Elements 3 (nicht dargestellt) in die Form eingefüllt, mit Baustahlgewebe 5 verstärkt und dieses vollständig eingegossen. Bevor diese neue Platte zu einem festen Element aushärtet, wird das bereits fertige Element 2 mit den darin befindlichen Verbindungsvorrichtungen 6 und den Zug- und/oder Druckelementen 7 voran in die noch nicht ausgehärtete Gießmasse G des zweiten Elements 3 eingesetzt, bis die noch freie Außenkante 11 des Verbund- Bauteils 8 auch bei diesem Element 3 auf das Baustahlgewebe 5 stößt und dort anliegt. In dieser Position härtet die Gießmasse G des zweiten Elements 3 aus und ein bewehrtes doppel- schaliges Fertigbau-Teil 1 ist hergestellt. Dieses doppel- schalige Fertigbau-Teil 1 wird aus der Gussform genommen, senkrecht aufgestellt und befindet sich in der Position, wie in Figur 2 gezeigt ist. Aus dieser Darstellung ist ersichtlich, dass die Verbindungsvorrichtung 6 jeweils mit den Bereichen der Außenkanten 10 und 11 ihres Verbund-Bauteils 8 in der ausgehärteten Gießmasse G der Innen- und Außenschalen 2 und 3 verankert ist, wobei die Verbindungsvorrichtung 6 flächig mehrdimensional ausgebildet ist, mit den Elementen 2 und 3 aus aushärtbarer Gießmasse einen zug- druck- und scherfes- ten Verbund bildet und einen wesentlichen Beitrag zur Stabilität des Fertigbau-Teils 1 beiträgt.This method is generally known and is intended to be given only briefly here without any claim to completeness with reference to FIG. 4 in order subsequently to be able to explain the insertion of the connecting devices 6 according to the invention. In a horizontal shape, which is a generally smooth Formwork surface, concrete or other curable casting material G is filled to a predetermined height. The resulting plate made of concrete or other hardenable casting material is provided with a reinforcement of structural steel or Baustahlgewebe 4 and this poured by further filling the mold with concrete or other curable casting material G. In this horizontally located, not yet cured slab of cast concrete or other hardenable casting material G, the connecting devices 6 according to the invention are used. This is done in such a way that at least one connecting device 6 with the tensile and / or pressure elements 7 is pressed ahead in the not yet cured casting G. The tensile and / or pressure elements 7 slide past the structural steel 4 cast in as reinforcement and the outer edge 10 of the composite component 8 of the connecting device 6 dives into the casting compound G until it gets into contact with the reinforcing steel mesh 4 and lying there. Subsequently, the casting compound G hardens. After curing, the element 2 is removed from the mold, this cleaned and a new layer of casting material is poured into the mold for producing a further element 3 (not shown), reinforced with 5 Baustahlgewebe and this completely poured. Before this new plate hardens to a solid element, the already finished element 2 is inserted with the connecting devices 6 and the tensile and / or pressure elements 7 ahead in the not yet cured casting G of the second element 3, until the still free outer edge 11 of the composite component 8 also in this element 3 abuts the Baustahlgewebe 5 and rests there. In this position, the casting compound G of the second element 3 hardens and a reinforced double-shell prefabricated part 1 is produced. This double-shell prefabricated part 1 is taken out of the mold, placed vertically and is in the position as shown in Figure 2. From this representation it can be seen that the connecting device 6 in each case with the areas of the outer edges 10 and 11 of their composite component 8 in the hardened casting composition G of the inner and outer shells 2 and 3 is anchored, wherein the connecting device 6 has a multi-dimensional surface, forms a tensile and shear bond with the elements 2 and 3 of hardenable casting compound and makes a significant contribution to stability of prefabricated part 1 contributes.
In Figur 5 ist eine Verbindungsvorrichtung 6 in perspektivischer Darstellung gezeigt. Diese Verbindungsvorrichtung 6 entspricht den bisher beschriebenen Verbindungsvorrichtungen 6 aus den Figuren 1 bis 4, sie ist in Figur 3 im Querschnitt gezeigt. Die Wellenform des Querschnitt ihres Verbund- Bauteils 8 ist besonders gut geeignet, um dem Fertigbau-Teil 1 hinreichend Stabilität bei geringem Gewicht, einfachster Handhabung und niedrigen Kosten zu gewährleisten. Als Werkstoff ist für dieses Ausführungsbeispiel jedes Material mit ausreichender Festigkeit geeignet, standardmäßiges Wellblech erscheint besonders vorteilhaft. Die Ausführung der Zug- und/oder Druckelemente 7 ist bei diesem Ausführungsbeispiel stabförmig-zylindrisch. Sie sind in beliebiger geeigneter Weise an dem Verbund-Bauteil 8 befestigtFIG. 5 shows a connection device 6 in a perspective view. This connecting device 6 corresponds to the previously described connecting devices 6 from FIGS. 1 to 4; it is shown in cross-section in FIG. The waveform of the cross section of their composite component 8 is particularly well suited to ensure the prefabricated part 1 sufficient stability with low weight, ease of use and low cost. The material suitable for this embodiment, any material with sufficient strength, standard corrugated metal appears particularly advantageous. The design of the tension and / or pressure elements 7 is rod-cylindrical in this embodiment. They are attached to the composite component 8 in any suitable manner
In Figur 6 ist eine Variante einer Verbindungsvorrichtung 12 dargestellt, bei der das wellenförmige Verbund-Bauteil 13 aus stärkerem Material, beispielsweise Faser-Verbund-Werkstoff hergestellt ist. In diesen Faser-Verbund-Werkstoff lassen sich beliebig geformte Zug- und/oder Druckelemente einfügen. Zur Verdeutlichung der verschiedenen Möglichkeiten sind hier an einem Verbund-Bauteil 13 gleichzeitig mehrere Beispiele gezeigt. Mit dem Bezugszeichen 14 ist ein Zug- und/oderFIG. 6 illustrates a variant of a connecting device 12, in which the wave-shaped composite component 13 is made of stronger material, for example fiber-composite material. In this fiber composite material can be arbitrarily shaped tensile and / or pressure elements insert. To illustrate the various options, several examples are shown here simultaneously on a composite component 13. By the reference numeral 14 is a train and / or
Druckelement mit geradem prismatischen Querschnitt bezeichnet. Das Bezugszeichen 15 steht für ein keulenförmiges Zug- und/oder Druckelement. Mit 16 ist kurzwellig gebogenes Zug- und/oder Druckelement bezeichnet und die 17 steht für ein- stabförmig-zylindrisches Zug- und/oder Druckelement, wie in Figur 5. Mit dem Bezugszeichen 18 ist ein langwellig gebogenes Zug- und/oder Druckelement bezeichnet und 19 steht für ein zackenförmiges Zug- und/oder Druckelement. Die jeweiligen Querschnitte sind der Form angepasst.Printing element with straight prismatic cross section called. The reference numeral 15 stands for a club-shaped tension and / or pressure element. 16 designates a short-wave bent tensile and / or pressure element and 17 represents a rod-shaped, cylindrical tensile and / or pressure element, as in FIG. 5. Reference numeral 18 denotes a tensile and / or pressure element bent in the long-wave 19 stands for a serrated pulling and / or pressure element. The respective cross sections are adapted to the shape.
In einer weiteren Variante einer Verbindungsvorrichtung 20 gemäß Figur 7 ist gezeigt, dass noch andere Ausführungsformen für Zug- und/oder Druckelemente vorstellbar sind. Mit Durchbrüchen 21 in der Oberfläche eines Verbund-Bauteils 22 wird die Verankerung in der Gießmasse G noch verbessert. Mit den Bezugszeichen 23 und 24 werden stabförmig-zylindrische Zug- und/oder Druckelemente mit unterschiedlichen Durchmessern bezeichnet. Die Bezugszeichen 25 und 26 stehen für wendeiförmige Zug- und/oder Druckelemente mit verschiedenen Querschnitten, ferner sind zackenförmige Zug- und/oder Druckelemente mit 27 und mäanderförmige Zug- und/oder Druckelemente mit 28 bezeichnet.In a further variant of a connecting device 20 according to FIG. 7, it is shown that still other embodiments for tension and / or pressure elements are conceivable. With openings 21 in the surface of a composite component 22, the anchoring in the casting material G is further improved. By the reference numerals 23 and 24 rod-shaped cylindrical tensile and / or pressure elements are referred to with different diameters. The reference numerals 25 and 26 are helical tensile and / or pressure elements with different cross-sections, also jagged tensile and / or pressure elements with 27 and meandering tensile and / or pressure elements 28 are designated.
In Figur 8 ist eine weitere Variante einer Verbindungsvorrichtung 29 dargestellt, welche im Wesentlichen der Verbindungsvorrichtung 20 gemäß Figur 7 entspricht. Das Verbund- Bauteil 30 weist gegenüber der Verbindungsvorrichtung 20 keine Durchbrüche auf, die Zug- und/oder Druckelemente entsprechen sich weitestgehend und sind deshalb mit den gleichen Bezugszeichen versehen.FIG. 8 shows a further variant of a connecting device 29, which essentially corresponds to the connecting device 20 according to FIG. The composite component 30 has no breakthroughs with respect to the connecting device 20, the tensile and / or pressure elements correspond largely as possible and are therefore provided with the same reference numerals.
Figur 9 zeigt ein Zug- und/oder Druckelement 31, welches stabförmig-zylindrisch geformt ist, und an seinen stirnseitigen Enden jeweils ein Büschel aus Drähten 32 trägt, die beispielsweise angeschweißt sein können.Figure 9 shows a tension and / or pressure element 31, which is rod-shaped cylindrical, and at its front ends each carrying a tuft of wires 32, which may be welded, for example.
Auf die unterschiedlichsten Möglichkeiten, die Zug- und/oder Druckelemente auszugestalten wird in den Figuren 10 bis 12 Bezug genommen.In the various ways to design the tensile and / or pressure elements is taken in Figures 10 to 12 reference.
In Figur 10 ist gezeigt, das ein Zug- und/oder Druckelement 33 auch aus mehreren Einzelteilen zusammen gefügt sein kann. Bei .einer dieser Ausführungsformen gibt es ein hohles zylindrisches Mittelteil 33a, in das von beiden Enden jeweils ein Endstück 33b und 33c mit Hilfe eines nicht näher bezeichneten Ansatzes eingeführt werden kann. Diese drei Einzelteile verbinden sich zu einem vollständigen Zug- und/oder Druckelement 33, dabei können die Endstücke 33b und 33c an ihren jeweili- gen freien Stirnseiten abgeschrägt sein. Darüber hinaus besteht die Möglichkeit, ein Zug- und/oder Druckelement aus einem zylindrischen Mittelteil 33d herzustellen, an dessen Stirnseiten jeweils ein passendes Endstück 33e und 33f ansetzbar ist. Sinnvoll sind derartige Variationen vor allem dann, wenn die Mittelteile und die Endstücke aus unterschiedlichen Materialien hergestellt sind, oder wenn sie unterschiedliche Oberflächenbeschaffenheit aufweisen. Die Endstücke können beispielsweise aufgeraut oder anderweitig strukturiert sein, um besser in der Gießmasse G verankert werden zu können.FIG. 10 shows that a tensile and / or pressure element 33 can also be joined together from a plurality of individual parts. In one of these embodiments, there is a hollow cylindrical central portion 33a, in each of which a respective one End piece 33b and 33c can be introduced by means of an unspecified approach. These three individual parts combine to form a complete tensile and / or pressure element 33, wherein the end pieces 33b and 33c can be beveled at their respective free end faces. In addition, it is possible to produce a tensile and / or pressure element from a cylindrical central part 33d, on whose end faces in each case a matching end piece 33e and 33f can be attached. Such variations are particularly useful when the middle parts and the end pieces are made of different materials, or if they have different surface finish. The end pieces may, for example, be roughened or otherwise structured in order to be better anchored in the casting compound G.
Eine sehr ähnliche Variante ist in Figur 11 dargestellt: Bei dieser Ausführungsformen gibt es ein hohles zylindrisches Mittelteil 34a, in das von beiden Enden jeweils ein Endstück 34b und 34c mit Hilfe eines nicht näher bezeichneten Ansatzes eingeführt werden kann. Diese drei Einzelteile verbinden sich zu einem vollständigen Zug- und/oder Druckelement 34, dabei können die Endstücke 34b und 34c an ihren jeweiligen freien Stirnseiten abgeschrägt sein. Darüber hinaus besteht die Mög- lichkeit, ein Zug- und/oder Druckelement aus einem zylindrischen Mittelteil 34d herzustellen, an dessen Stirnseiten je-A very similar variant is shown in Figure 11: In these embodiments, there is a hollow cylindrical central portion 34a, in each of which an end piece 34b and 34c can be introduced from both ends by means of an unspecified approach. These three individual parts combine to form a complete tensile and / or pressure element 34, wherein the end pieces 34b and 34c can be beveled at their respective free end faces. In addition, it is possible to produce a tension and / or pressure element from a cylindrical middle part 34d, on whose end faces each
* weils ein passendes Endstück 34e und 34f ansetzbar ist. Sinnvoll sind derartige Variationen vor allem dann, wenn die Mittelteile und die Endstücke aus unterschiedlichen Materialien hergestellt sind, oder wenn sie unterschiedliche Oberflächenbeschaffenheit aufweisen. Die Endstücke können beispielsweise besandet sein, um besser in der Gießmasse G verankert werden zu können. * because a matching end piece 34e and 34f can be attached. Such variations are particularly useful when the middle parts and the end pieces are made of different materials, or if they have different surface finish. The end pieces can be sanded, for example, in order to be better anchored in the casting material G.
In Figur 12 ist nochmals ein Detail einer Innenschale 2 dargestellt, bei der ein Zug- und/oder Druckelement 35 in der Gießmasse G verankert ist. Die Stirnseite des Zug- und/oder Druckelements 35 weist einen tropfenförmigen Endbereich 36 auf, der formschlüssig- in der Gießmasse G fixiert ist. Die nicht näher bezeichnete Außenkante eines ebenfalls nicht näher bezeichneten Verbund-Bauteils ist ebenfalls auf eine be- reits beschriebene Weise in der Gießmasse verankert und entspricht weitgehend den vorbeschriebenen Ausführungsbeispielen.FIG. 12 once again shows a detail of an inner shell 2 in which a tensile and / or pressure element 35 is anchored in the casting compound G. The front of the train and / or Pressure element 35 has a teardrop-shaped end portion 36 which is positively fixed in the casting mass G. The unspecified outer edge of a composite component, which is likewise not designated in more detail, is likewise anchored in the casting compound in a manner already described and largely corresponds to the above-described exemplary embodiments.
In Figur 13 ist sehr schematisch eine vorteilhafte Weiterbil- düng einer Verbindungsvorrichtung na'ch der Erfindung gezeigt: Eine Anzahl von Zug- und/oder Druckelementen 37, 38, 39 sind durch ein Verbund-Bauteil 40 miteinander verbunden. Das Verbund-Bauteil ist hier als eine Anordnung aus parallel verlaufenden Drähten 40 realisiert. Zur Verbesserung der Fixierung in der Gießmasse G können zusätzliche Drahtgebilde 41 vorgesehen sein. Dieses Ausführungsbeispiel verdeutlicht die Möglichkeit, mehrere Verbindungsvorrichtungen auf eine Rolle aufzuwickeln und somit magazinierbar zu machen.FIG. 13 very schematically shows an advantageous further development of a connecting device according to the invention: A number of tension and / or pressure elements 37, 38, 39 are connected to one another by a composite component 40. The composite component is realized here as an arrangement of parallel wires 40. To improve the fixation in the casting compound G additional wireforms 41 may be provided. This embodiment illustrates the possibility of winding a plurality of connecting devices on a roll and thus make it magazinierbar.
In Figur 14 wird dargestellt, dass die Zug- und/oder Druckelemente 42, 43, 44 zueinander auch kleine Winkel einnehmen können, und dass sie durch einen Blechstreifen 45 miteinander verbunden sein können. Bei dieser Ausführungsform ist das Gewicht extrem reduziert, was geringsten Materialverbrauch und auch geringste Kosten bei ausreichender Festigkeit gewährleistet. Auch hier kann die Oberfläche der Zug- und/oder Druckelemente in beliebiger Weise strukturiert sein.In FIG. 14 it is shown that the tension and / or pressure elements 42, 43, 44 can also assume small angles relative to one another, and that they can be connected to one another by a metal strip 45. In this embodiment, the weight is extremely reduced, which ensures lowest material consumption and lowest cost with sufficient strength. Again, the surface of the tensile and / or pressure elements can be structured in any desired manner.
Schließlich ist eine Verbindungsvorrichtung 46 realisierbar, bei der das Verbund-Bauteil 47 einen mäanderförmigen Querschnitt aufweist. Die Zug- und/oder Druckelemente 48, 49 und 50 sind in die Mäander passend eingefügt und können beliebig ausgestaltet sein.Finally, a connecting device 46 can be realized, in which the composite component 47 has a meandering cross section. The tension and / or pressure elements 48, 49 and 50 are inserted into the meander suitable and can be configured arbitrarily.
Ein weiteres Ausführungsbeispiel ist in Figur 16 dargestellt. Auf einer Schalungsplatte 51, welche ein Teil einer Gießform ist, wie sie bereits vorbeschrieben wurde, ist ein Baustahl- gewebe 52 platziert. Dieses Baustahlgewebe 52 stabilisiert die Innen- oder Außenschale, welche gegossen werden soll. Eine Verbindungsvorrichtung 53 ist mit rechteckigen Ausschnitten 54 versehen, in welche die Stäbe 57 des Baustahlgewebes 52 hineinragen. Ausschnitte können auch als kammartige Ausschnitte 55 ausgebildet sein und den Rand der Verbindungsvorrichtung 53 bilden. Die kammartigen Ausschnitte 55 greifen im weiteren Herstellungsverfahren der Innen -oder Außenschale in die vom Baustahlgewebe gebildete Bewehrung der zweiten, spä- ter zu gießende Innen- oder Außenschale ein. Ein Verbund von Druck- und/oder Zugelementen wird in diesem Ausführungsbeispiel durch ein zusammenhängendes, flächiges Gebilde 58 geschaffen, welches durch ein Band als Verbund-Bauteil 59 stabilisiert ist.Another embodiment is shown in FIG. On a formwork plate 51, which is a part of a casting mold, as already described above, is a structural steel tissue 52 placed. This Baustahlgewebe 52 stabilizes the inner or outer shell, which is to be poured. A connecting device 53 is provided with rectangular cutouts 54 into which the rods 57 of the structural steel fabric 52 project. Cutouts may also be formed as comb-like cutouts 55 and form the edge of the connecting device 53. In the further manufacturing process of the inner or outer shell, the comb-like cutouts 55 engage in the reinforcement formed by the reinforcing steel mesh of the second inner shell or outer shell to be cast later. A composite of pressure and / or tension elements is provided in this embodiment by a continuous, flat structure 58, which is stabilized by a band as a composite component 59.
Die vorstehenden Ausführungsbeispiele machen deutlich, dass eine erfindungsgemäße Verbindungsvorrichtung in vielfältiger Form ausgestaltet werden kann ohne den erfinderischen Gedanken zu verlassen. So sollen die beschrieben Ausführungsformen die Erfindung auch keinesfalls einschränken, sondern vielmehr zeigen, dass die Erfindung auf die unterschiedlichte Art und Weise ausgestaltet werden kann. The above embodiments make it clear that a connecting device according to the invention can be configured in many forms without departing from the inventive idea. Thus, the described embodiments are not intended to limit the invention in any way, but rather show that the invention can be embodied in a different manner.
BezugszeichenlisteLIST OF REFERENCE NUMBERS
1 Fertigbau-Teil1 prefabricated part
2 Innenschale 3 Außenschale2 inner shell 3 outer shell
4 Baustahlgewebe4 structural steel mesh
5 Baustahlgewebe5 structural steel mesh
6 Verbindungsvorrichtung6 connection device
7 Zug- und/oder Druckelement 8 Verbund-Bauteil7 tensile and / or pressure element 8 composite component
9 Richtungspfeil9 directional arrow
10 Bereich Außenkante des Verbund-Bauteils10 Area outer edge of the composite component
11 Bereich Außenkante des Verbund-Bauteils11 Area outer edge of the composite component
12 Verbindungsvorrichtung 13 Verbund-Bauteil12 connecting device 13 composite component
14 Zug- und/oder Druckelement14 tensile and / or pressure element
15 Zug- und/oder Druckelement15 tensile and / or pressure element
16 Zug- und/oder Druckelement16 tensile and / or pressure element
17 Zug- und/oder Druckelement 18 Zug- und/oder Druckelement17 tensile and / or pressure element 18 tensile and / or pressure element
19 Zug- und/oder Druckelement19 tensile and / or pressure element
20 Verbindungsvorrichtung20 connection device
21 Durchbruch21 breakthrough
22 Verbund-Bauteil 23 Zug- und/oder Druckelement22 Composite component 23 Tensile and / or pressure element
24 Zug- und/oder Druckelement24 tensile and / or pressure element
25 Zug- und/oder Druckelement25 tensile and / or pressure element
26 Zug- und/oder Druckelement26 tensile and / or pressure element
27 Zug- und/oder Druckelement 28 Zug- und/oder Druckelement27 tensile and / or pressure element 28 tensile and / or pressure element
29 Verbindungsvorrichtung29 connecting device
30 Verbund-Bauteil30 composite component
31 Zug- und/oder Druckelement31 tensile and / or pressure element
32 Drähte 33 mehrteiliges Zug- und/oder Druckelement32 wires 33 multi-part tensile and / or pressure element
33a Mittelteil33a middle part
33b Endstück 33c Endstück33b tail 33c tail
33d Mittelteil33d middle part
33e Endstück33e tail
33f Endstück 34 mehrteiliges Zug- und/oder Druckelement33f end piece 34 multi-part tension and / or pressure element
34a Mittelteil34a middle part
34b Endstück34b tail
34c Endstück34c tail
34d Mittelteil 34e Endstück34d middle part 34e tail
34f Endstück34f tail
35 Zug- und/oder Druckelement35 tensile and / or pressure element
36 tropfenförmigen Endbereich36 drop-shaped end
37 Zug- und/oder Druckelement 38 Zug- und/oder Druckelement37 tensile and / or pressure element 38 tensile and / or pressure element
39 Zug- und/oder Druckelement39 tensile and / or pressure element
40 Verbindungsdraht40 connecting wire
41 Verankerungsdraht41 anchoring wire
42 Zug- und/oder Druckelement 43 Zug- und/oder Druckelement42 tensile and / or pressure element 43 tensile and / or pressure element
44 Zug- und/oder Druckelement44 tensile and / or pressure element
45 Verbund-Bauteil45 composite component
46 Verbindungsvorrichtung46 connection device
47 Verbund-Bauteil 48 Zug- und/oder Druckelement47 Composite component 48 Tensile and / or pressure element
49 Zug- und/oder Druckelement49 tensile and / or pressure element
50 Zug- und/oder Druckelement50 tensile and / or pressure element
51 Schalungsplatte51 formwork panel
52 Baustahlgewebe 53 Verbindungsvorrichtung52 structural steel mesh 53 connecting device
54 rechteckige Ausschnitte54 rectangular cutouts
55 kammartige Ausschnitte55 comb-like cutouts
56 Rand der Verbindungsvorrichtung56 edge of the connecting device
57 Stäbe 58 Zug- und/oder Druckelement57 bars 58 tensile and / or pressure element
59 Verbund-Bauteil 59 Composite component

Claims

Patentansprüche claims
1. Bewehrungsvorrichtung für Fertigbau-Teile, welche aus mehreren weitgehend parallel zueinander angeordneten Elementen besteht, die aus aushärtbarer Gießmasse hergestellt und die durch wenigstens eine Verbindungsvorrichtung miteinander verbunden sind, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (6, 12, 20, 29, 46, 53) flächig mehrdimensional ausgebildet ist und mit den Elementen (2, 3) aus aushärtbarer Gießmasse einen zug- druck- und scherfesten Ver- bund bildet.1. Reinforcement device for prefabricated parts, which consists of a plurality of substantially mutually parallel elements, which are made of hardenable casting compound and which are interconnected by at least one connecting device, characterized in that the connecting device (6, 12, 20, 29, 46, 53) has a multi-dimensional surface and forms a tension-proof and shear-resistant composite with the elements (2, 3) of hardenable casting compound.
2. Bewehrungsvorrichtung für Fertigbau-Teile nach Anspruch 1, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (6, 12, 20, 29, 46, 53) aus einem Verbund von wenigstens zwei Zug- Druck- und Scherelementen (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, • 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) besteht, die zwischen den parallel zueinander angeordneten Elemente (2, 3) anordbar und die in deren aushärtbarer Gießmasse (G) verankerbar sind.2. Reinforcement device for prefabricated parts according to claim 1, characterized in that the connecting device (6, 12, 20, 29, 46, 53) of a composite of at least two train pressure and shear elements (7, 14, 15, 16 , 17, 18, 19, 23, 24, 25, 26, 27, • 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58), which can be arranged between the elements (2, 3) arranged parallel to one another and which can be anchored in their hardenable casting compound (G).
3. Bewehrungsvorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (6, 12, 20, 29, 46, 53) aus einem Verbund von wenigstens zwei Zug-, Druck- und Scherelementen (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 43, 48, 49, 50, 58) besteht, wobei die Längsachse von wenigstens einem Zug- und Druckelement (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 43, 48, 49, 50, 58) im Wesentlichen senkrecht zur Ebene der parallel zueinander an- geordneten Elemente (2, 3) verläuft.3. Reinforcing device according to claim 1, characterized in that the connecting device (6, 12, 20, 29, 46, 53) consists of a composite of at least two tensile, compressive and shear elements (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 43, 48, 49, 50, 58), the longitudinal axis of at least one traction and pressure element (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 43, 48, 49, 50) , 58) extends substantially perpendicular to the plane of the mutually parallel elements (2, 3).
4. Bewehrungsvorrichtung nach Anspruch 2 oder 3, dadurch gekennzeichnet, dass der Verbund der wenigstens zwei Zug- , Druck- und Scherelemente (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44,4. Reinforcement device according to claim 2 or 3, characterized in that the composite of at least two tensile, compressive and shear elements (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44,
48, 49, 50, 58) durch ein Verbund-Bauteil (8, 13, 22, 30, 40, 41, 45, 47, 59) erzeugt wird, welches sich zwischen den Enden (33b, 33c, 33e, 33f; 34b, 34c, 34e, 34f) der Zug- und/oder Druckelemente (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) befindet, und gegenüber diesen Enden (33b, 33c, 33e, 33f; 34b, 34c, 34e, 34f) räumlich zurückgesetzt ist, wobei diese Enden (33b, 33c, 33e, 33f; 34b, 34c, 34e, 34f) in der aushärtbaren Gießmasse (G) verankerbar sind.48, 49, 50, 58) is produced by a composite component (8, 13, 22, 30, 40, 41, 45, 47, 59) extending between the ends (33b, 33c, 33e, 33f; 34b, 34c, 34e, 34f) of the tension and / or pressure elements (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28 , 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) and opposite these ends (33b, 33c, 33e, 33f; 34b, 34c, 34e, 34f) is spatially reset, said ends (33b, 33c, 33e, 33f, 34b, 34c, 34e, 34f) being anchored in the hardenable casting compound (G).
5. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (8, 13, 22, 30) durch ein flächiges Element mit wellenförmigem Querschnitt gebildet wird.5. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (8, 13, 22, 30) is formed by a flat element with corrugated cross-section.
6. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung durch ein flächiges Element mit mäander- förmigem Querschnitt (47) gebildet wird.6. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device is formed by a flat element with a meandering cross-section (47).
7. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (22) durch ein flächiges Element mit- strukturierter Oberfläche (21) gebildet wird.7. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (22) is formed by a flat element with a structured surface (21).
8. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (40, 45) durch ein drahtartiges Element gebildet wird.8. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (40, 45) is formed by a wire-like element.
9. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung () in mehrfacher Ausführung zwischen den parallel zueinander angeordneten Elemente (2, 3) anordbar und in deren aushärtbarer Gießmasse (G) verankerbar sind.9. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (12) can be arranged in multiple configurations between the mutually parallel elements (2, 3) and can be anchored in their hardenable casting compound (G).
10. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Ver- bindungsvorrichtung () in mehrfacher Ausführung magazinierbar ist .10. Reinforcing device according to at least one of the preceding claims, characterized in that the binding device () is magazines in multiple execution.
11. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass sich die Verbindungsvorrichtung (8, 13, 22, 30, 45, 47, 59) in einer Ebene erstreckt, die senkrecht zwischen den parallel zueinander angeordneten Elemente (2, 3) verläuft.11. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (8, 13, 22, 30, 45, 47, 59) extends in a plane perpendicular between the elements (2, 3) runs.
12. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass sich die Verbindungsvorrichtung (8, 13, 22, 30, 47, 59) in einer Ebene erstreckt, die senkrecht zwischen den parallel zueinander angeordneten Elemente (2, 3) verläuft, wobei die den parallel zueinander angeordneten Elementen (2, 3) zugewandten Außenkanten (10, 11, 56) des Verbund-Bauteils (8, 13, 22, 30, 47, 59) in deren aushärtbarer Gießmasse (G) verankerbar sind.12. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (8, 13, 22, 30, 47, 59) extends in a plane which extends perpendicularly between the mutually parallel elements (2, 3), wherein the mutually parallel elements (2, 3) facing outer edges (10, 11, 56) of the composite component (8, 13, 22, 30, 47, 59) in the curable casting compound (G) are anchored.
13. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass sich die13. Reinforcing device according to at least one of the preceding claims, characterized in that the
Verbindungsvorrichtung (8, 13, 22, 30, 47, 59) in einer Ebene erstreckt, die senkrecht zwischen den parallel zueinander angeordneten Elemente (2, 3) verläuft, wobei die den parallel zueinander angeordneten Elementen (2, 3) zugewandten Außen- kanten (10, 11, 56) des Verbund-Bauteils (8, 13, 22, 30, 47, 59) in deren aushärtbarer Gießmasse (G) formschlüssig verankerbar sind.Connecting device (8, 13, 22, 30, 47, 59) extends in a plane which extends perpendicularly between the mutually parallel elements (2, 3), wherein the mutually parallel elements (2, 3) facing outer edges (10, 11, 56) of the composite component (8, 13, 22, 30, 47, 59) in the curable casting compound (G) are positively anchored.
14. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass die Zug- und Druckelemente (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) zwischen den parallel zueinander angeordneten Elementen (2, 3) anordbar und so ausgebildet sind, dass sie in deren aushärtbarer Gießmasse (G) formschlüssig verankerbar sind. 14. Reinforcement device according to at least one of the preceding claims, characterized in that the tension and compression elements (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) are arranged between the mutually parallel elements (2, 3) and are formed so that in their curable casting material ( G) are positively anchored.
15. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Zug- und Druckelemente (33, 34) mehrteilig ausgeführt sind.15. Reinforcing device according to at least one of the preceding claims, characterized in that the tension and compression elements (33, 34) are designed in several parts.
16. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Zug- und Druckelemente (33, 34) aus unterschiedlichen Werkstoffen bestehen.16. Reinforcement device according to at least one of the preceding claims, characterized in that the tension and compression elements (33, 34) consist of different materials.
17. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Zug- und Druckelemente (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) aus Faserverbund-Werkstoffen bestehen.17. Reinforcing device according to at least one of the preceding claims, characterized in that the tension and compression elements (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) consist of fiber composite materials.
18. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Zug- und Druckelemente (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) aus metallischen Werkstoffen bestehen.18. Reinforcing device according to at least one of the preceding claims, characterized in that the tension and compression elements (7, 14, 15, 16, 17, 18, 19, 23, 24, 25, 26, 27, 28, 31, 33, 34, 35, 37, 38, 39, 42, 43, 44, 48, 49, 50, 58) consist of metallic materials.
19. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (40, 41) mehrteilig ausgeführt ist.19. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (40, 41) is designed in several parts.
20. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (40, 41) aus unterschiedlichen Werkstoffen besteht.20. Reinforcement device according to at least one of the preceding claims, characterized in that the connecting device (40, 41) consists of different materials.
21. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (8, 13, 22, 30, 40, 41, 45, 47, 59) aus Faserverbund-Werkstoffen besteht .21. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (8, 13, 22, 30, 40, 41, 45, 47, 59) consists of fiber composite materials.
22. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, d a du r c h g e ke n n z e i c h n e t , dass die Ver- bindungsvorrichtung (8, 13, 22, 30, 40, 41, 45, 47, 59) aus metallischen Werkstoffen besteht.22. Reinforcing device according to at least one of the preceding claims, since it indicates that the bonding device (8, 13, 22, 30, 40, 41, 45, 47, 59) consists of metallic materials.
23. Bewehrungsvorrichtung nach wenigstens einem der vorste- henden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (6, 12, 20, 29, 46, 53) aus einem Verbund von drei Zug- und Druckelementen (42, 43, 44) besteht, wobei die Längsachse von einem Zug- und Druckelement (43) im Wesentlichen senkrecht zur Ebene der parallel zueinander ange- ordneten Elemente (2, 3) verläuft, und die Längsachsen der beiden anderen Zug- und Druckelemente (42, 44) unter einem kleinen Winkel zur Längsachse des senkrechten Zug- und Druckelements (43) verlaufen.23. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (6, 12, 20, 29, 46, 53) consists of a composite of three tension and compression elements (42, 43, 44), wherein the longitudinal axis of a tension and compression element (43) is substantially perpendicular to the plane of the parallel arranged elements (2, 3), and the longitudinal axes of the other two tension and compression elements (42, 44) at a small angle to Longitudinal axis of the vertical tension and compression element (43) extend.
24. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (6, 12, 20, 29, 46, 53) aus einem Verbund von mehreren Zug- und Druckelementen (42, 44) besteht, wobei die Längsachsen der Zug- und Druckelemente (42, 44) in einem kleinen Winkel zur Senkrechten auf die Ebene der parallel zueinander angeordneten Elemente (2, 3) verlaufen.24. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (6, 12, 20, 29, 46, 53) consists of a composite of several tensile and compressive elements (42, 44), wherein the longitudinal axes of the train - And pressure elements (42, 44) at a small angle to the perpendicular to the plane of the mutually parallel elements (2, 3) extend.
25. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Ver- bindungsvorrichtung (6, 12, 20, 29, 46, 53) aus einem Verbund von Zug- und Druckelementen (58) besteht, wobei zwischen oder in den Zug- und Druckelementen (58) Freiraum (54, 55) gebildet wird, welcher von Stäben (57) durchdringbar ist, die Teil von Bewehrungselementen (52) der Innen- oder Außenschalen (2, 3) sind.25. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (6, 12, 20, 29, 46, 53) consists of a composite of tensile and compressive elements (58), wherein between or in the train and pressure elements (58) free space (54, 55) is formed, which is penetrable by rods (57), which are part of reinforcing elements (52) of the inner or outer shells (2, 3).
26. Bewehrungsvorrichtung nach Anspruch 24 , dadurch gekennzeichnet, dass die Freiräume (54) durch rechteckige Ausschnitte (54) in den Zug- und Druckelementen (58) gebildet werden. 26. Reinforcing device according to claim 24, characterized in that the free spaces (54) by rectangular cutouts (54) in the tension and compression elements (58) are formed.
27. Bewehrungsvorrichtung nach Anspruch 24, dadurch gekennzeichnet, dass die Freiräume (55) mittels einer kammartig gezackten Außenkante (56) der Zug- und Druckelemente (58) gebildet werden.27. Reinforcing device according to claim 24, characterized in that the free spaces (55) by means of a comb-like serrated outer edge (56) of the tension and compression elements (58) are formed.
28. Bewehrungsvorrichtung nach wenigstens einem der vorstehenden Ansprüche, dadurch gekennzeichnet, dass die Verbindungsvorrichtung (8, 13, 22, 30, 40, 41, 45, 47, 59) aus korrosionfestem Werkstoff besteht oder korrosionsfest ober- flächenveredelt ist. 28. Reinforcing device according to at least one of the preceding claims, characterized in that the connecting device (8, 13, 22, 30, 40, 41, 45, 47, 59) consists of corrosion-resistant material or is corrosion resistant surface-finished.
EP08700878.5A 2007-03-26 2008-01-22 Prefabricated part Active EP2140077B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007014366A DE102007014366A1 (en) 2007-03-26 2007-03-26 Reinforcement device for prefabricated parts
PCT/DE2008/000104 WO2008116434A1 (en) 2007-03-26 2008-01-22 Reinforcing device for prefabricated parts

Publications (2)

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EP2140077A1 true EP2140077A1 (en) 2010-01-06
EP2140077B1 EP2140077B1 (en) 2019-10-23

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EP08700878.5A Active EP2140077B1 (en) 2007-03-26 2008-01-22 Prefabricated part

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EP (1) EP2140077B1 (en)
DE (2) DE102007014366A1 (en)
ES (1) ES2766254T3 (en)
HU (1) HUE047008T2 (en)
WO (1) WO2008116434A1 (en)

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Also Published As

Publication number Publication date
ES2766254T3 (en) 2020-06-12
WO2008116434A1 (en) 2008-10-02
DE112008001463A5 (en) 2010-03-04
HUE047008T2 (en) 2020-04-28
EP2140077B1 (en) 2019-10-23
DE102007014366A1 (en) 2008-10-02

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