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EP1007809B1 - Reinforcement device for supporting structures - Google Patents

Reinforcement device for supporting structures Download PDF

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Publication number
EP1007809B1
EP1007809B1 EP98937382A EP98937382A EP1007809B1 EP 1007809 B1 EP1007809 B1 EP 1007809B1 EP 98937382 A EP98937382 A EP 98937382A EP 98937382 A EP98937382 A EP 98937382A EP 1007809 B1 EP1007809 B1 EP 1007809B1
Authority
EP
European Patent Office
Prior art keywords
cfk
panel
end element
reinforcing device
strips
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.)
Expired - Lifetime
Application number
EP98937382A
Other languages
German (de)
French (fr)
Other versions
EP1007809A1 (en
Inventor
Gregor Schwegler
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.)
Sika Schweiz AG
Original Assignee
StressHead AG
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Filing date
Publication date
Application filed by StressHead AG filed Critical StressHead AG
Publication of EP1007809A1 publication Critical patent/EP1007809A1/en
Application granted granted Critical
Publication of EP1007809B1 publication Critical patent/EP1007809B1/en
Anticipated expiration legal-status Critical
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Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/08Members specially adapted to be used in prestressed constructions
    • E04C5/12Anchoring devices
    • E04C5/127The tensile members being made of fiber reinforced plastics
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/20Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of concrete or other stone-like material, e.g. with reinforcements or tensioning members
    • E04C3/26Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of concrete or other stone-like material, e.g. with reinforcements or tensioning members prestressed
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C5/00Reinforcing elements, e.g. for concrete; Auxiliary elements therefor
    • E04C5/07Reinforcing elements of material other than metal, e.g. of glass, of plastics, or not exclusively made of metal
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04GSCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G23/00Working measures on existing buildings
    • E04G23/02Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
    • E04G23/0218Increasing or restoring the load-bearing capacity of building construction elements
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04GSCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G23/00Working measures on existing buildings
    • E04G23/02Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
    • E04G23/0218Increasing or restoring the load-bearing capacity of building construction elements
    • E04G2023/0251Increasing or restoring the load-bearing capacity of building construction elements by using fiber reinforced plastic elements
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04GSCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G23/00Working measures on existing buildings
    • E04G23/02Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
    • E04G23/0218Increasing or restoring the load-bearing capacity of building construction elements
    • E04G2023/0251Increasing or restoring the load-bearing capacity of building construction elements by using fiber reinforced plastic elements
    • E04G2023/0255Increasing or restoring the load-bearing capacity of building construction elements by using fiber reinforced plastic elements whereby the fiber reinforced plastic elements are stressed
    • E04G2023/0259Devices specifically adapted to stress the fiber reinforced plastic elements
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04GSCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
    • E04G23/00Working measures on existing buildings
    • E04G23/02Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
    • E04G23/0218Increasing or restoring the load-bearing capacity of building construction elements
    • E04G2023/0251Increasing or restoring the load-bearing capacity of building construction elements by using fiber reinforced plastic elements
    • E04G2023/0262Devices specifically adapted for anchoring the fiber reinforced plastic elements, e.g. to avoid peeling off
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10Methods of surface bonding and/or assembly therefor
    • Y10T156/1052Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1059Splitting sheet lamina in plane intermediate of faces

Definitions

  • the present invention relates to a Reinforcement device according to the preamble of claim 1 and a method for reinforcing beams after the Preamble of claim 11.
  • Support structures can consist of conventionally constructed walls Be brick or for example reinforced concrete walls or - beams, wood, plastic or steel beams.
  • the reinforcement of such has long been known Support structures with retrofitted steel plates.
  • the steel plates i.e. band-shaped steel sheets resp. Steel slats are placed on one or two sides of the Glued supporting structure, preferably on the train loaded sides of the supporting structure.
  • the advantage of this The process was that it was relatively quick can be carried out, but high demands the glue, i.e. the preparation of the parts and the Implementation of the gluing must be under precisely defined Ratios take place to get the desired effect to reach. Problems with this method occur in particular in the corrosion area, i.e. if supporting structures in Outdoor should be strengthened in such a way, for example Bridge girders.
  • clamping means in the form of strips made of metal or fiber-reinforced plastic to be used over end anchorages.
  • clamping device there is no flat connection of the clamping device with the supporting structure, but it is only in the two anchor points of the Clamping means a connection with the supporting structure intended.
  • Such clamping devices are conventional already included in the planning of the supporting structure, because a subsequent equipment practically not or only with very high effort can be realized because for the Corresponding channels created in the supporting structure Need to become.
  • the object of the present invention was now a CFRP reinforcement lamella, where the Force is transmitted from the carrier into the ends in such a way that detachment is practically avoided and which one also suitable for preloading.
  • the ends of the CFRP slats can be split preferably either in superimposed flags or juxtaposed flags take place, respectively. in a Combination of these two variants.
  • the ends of the CFRP slats can be split advantageously at the construction site itself in each required lengths and dimensions. So that is this system is very universal for amplifying suitable for practically any support components and can be used with or can also be used without pretension.
  • FIG. 1 now shows the cross section through a reinforcing beam 1.
  • the ends of the used for this CFRP slats 2 are, according to the invention, in end elements, here anchor heads 3 and 4 used.
  • the anchor heads 3,4 can be milled or tapered recesses of the Carrier 1 can be used, as in this figure shown.
  • the CFRP lamella 2 is by means of a Adhesive layer 5 with the carrier 1 over the entire surface or partially connected, as well as the anchor heads 3, 4 glued.
  • This Cross-clamping device 6 can, for example, through the Carrier 1 and the anchor heads 3, 4 passed through Threaded rods or dowels are made.
  • FIG. 2 now shows the cross section through one of the Anchor heads 3.
  • the holding slots 9 are here arranged widened upwards and downwards and have transverse bores 10. These holes 10 result in additional anchoring points for the adhesive, with which the flags 2 'of the CFRP lamella 2 with the Holding slots 9 are connected.
  • the great However, the advantage lies in splitting the end of the Lamella 2 in the flags 2 '. This split takes place preferably in the grain of the slats, and it will thus advantageously an enlargement of the adhesive surface achieved without the strength properties of the CFRP lamella 2 are affected.
  • transverse reinforcement 11 To in the exit area of the CFRP lamella 2 from the anchor head 3 bend or open the anchor head Lateral forces resulting from the wedge or arcuate Arrange the arrangement of the holding slots 9, is to be avoided preferably to install a transverse reinforcement 11, which in Figure 2 is only indicated schematically.
  • this transverse reinforcement 11 by means of appropriate Bores in the anchor head 3 and passed through nuts tensioned threaded rods.
  • FIG. 3 shows one end of the CFRP lamella 2 with the split into three flags 2 ' Slat end.
  • the CFRP slat can be used with conventional After cutting to length to the desired length desired number, flags of approximately the same thickness 2 ' be split up, for example by means of a plane or knife.
  • the advantage here is that in terms of quality the splitting relatively low requirements be divided into the essentials corresponding number of flags 2 'to achieve the Area enlargement for the connection with the anchor head 3rd
  • FIG. 5 now shows the cross section through a Anchor head 12 and the corresponding arrangement of the Holding slots 9.
  • the bottom slot 9 ' is parallel to the outer wall 12 'of the support lying on the support 1 Anchor head 12 formed, the remaining slots 9 are fan-shaped towards the outside at an acute angle arranged pointing.
  • this arrangement brings about the enlargement of the bonding surface of the CFRP lamella 2 the same advantages as already described, and on the other hand, enables the flat application of the Anchor heads 12, 13 without additional recesses on the carrier 1.
  • Cross reinforcement means 11 are also in these anchor heads 12, 13 shown to avoid bending or tearing open the anchor heads 12, 13 in the area of the exit of the CFRP lamella 2nd
  • the anchor heads 3.4, respectively. 12, 13 is suitable metal, which has a high strength, easy workability and good Has force introduction properties, and on the other hand also plastic, especially if the Corrosion requirements must be high.
  • a screw 16 for mutual Pressing the plates 15 respectively. the flags 2 'used become.
  • Figure 8 is the supervision of another Embodiment of the end of the CFRP lamella 2 shown.
  • the flags 2 ' are not formed one above the other, but are formed side by side.
  • the splitting is preferably along the grain made of CFRP lamella 2.
  • the reinforcement devices according to the invention are suitable are particularly interested in the renovation of existing concrete support structures, such as blankets or Bridge girders.
  • existing concrete support structures such as blankets or Bridge girders.
  • CFRP slats such as masonry and Wooden structures.
  • the easy preload enable the higher utilization of the strength properties of the CFRP slats than with the previously known methods.
  • preload causes that on the pull side existing support element is pre-pressed what is particularly advantageous for bridge girders, for example.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Mechanical Engineering (AREA)
  • Reinforcement Elements For Buildings (AREA)
  • Working Measures On Existing Buildindgs (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Bridges Or Land Bridges (AREA)
  • Tents Or Canopies (AREA)
  • Sewage (AREA)
  • Measurement And Recording Of Electrical Phenomena And Electrical Characteristics Of The Living Body (AREA)
  • Electric Cable Installation (AREA)

Abstract

The ends of carbon plates reinforcing supporting elements, such as concrete beams, are divided into at least two splines having approximately the same thickness and are glued in the appropriate retaining slots of a terminal element. The splines form an angle in relation to each other. This assembly is then glued to the traction side of the supporting element, whereby the carbon plates are directly prestressed by the terminal elements in relation to the supporting element. The terminal element can be inserted into an appropriate groove in the supporting element or glued directly on the surface of the supporting element and/or doweled, optionally by using a transverse tensioning device.

Description

Die vorliegende Erfindung betrifft ein Verstärkungsvorrichtung nach dem Oberbegriff von Anspruch 1 sowie ein Verfahren zur Verstärkung von Trägern nach dem Oberbegriff von Anspruch 11.The present invention relates to a Reinforcement device according to the preamble of claim 1 and a method for reinforcing beams after the Preamble of claim 11.

Bei der Sanierung von Tragstrukturen an bestehenden Bauten stellt sich oft das Problem, dass die Tragstruktur für neue Lastfälle, welche die ehemalige Dimensionierung übersteigen, angepasst werden soll. Um nicht die Tragstruktur in derartigen Fällen ganz zu ersetzen, sind Methoden und Vorrichtungen zur Verstärkung solcher bestehender Tragstrukturen gefunden worden. Solche Tragstrukturen können herkömmlich aufgebaute Wände aus Backstein sein oder beispielsweise Stahlbetonwände oder - träger, Holz- Kunststoff- oder Stahlträger sein.When renovating supporting structures on existing buildings The problem often arises that the supporting structure for new ones Load cases that the former dimensioning exceed, should be adjusted. Not that Support structure must be replaced in such cases Methods and devices for reinforcing such existing support structures have been found. Such Support structures can consist of conventionally constructed walls Be brick or for example reinforced concrete walls or - beams, wood, plastic or steel beams.

Seit längerem bekannt ist die Verstärkung solcher Tragstrukturen mit nachträglich aufgebrachten Stahlplatten. Die Stahlplatten, d.h. bandförmige Stahlbleche resp. Stahllamellen, werden dabei auf eine oder zwei Seiten der Tragkonstruktion aufgeklebt, vorzugsweise auf die auf Zug belasteten Seiten der Tragkonstruktion. Der Vorteil dieses Verfahrens bestand darin, dass es verhältnismässig rasch durchgeführt werden kann, allerdings hohe Anforderungen an die Klebung stellt, d.h. die Vorbereitung der Teile und die Durchführung der Klebung muss unter genau definierten Verhältnissen stattfinden, um die gewünschte Wirkung zu erreichen. Probleme bei dieser Methode treten insbesondere im Korrosionsbereich auf, d.h. wenn Tragkonstruktionen im Freien derart verstärkt werden sollen, wie beispielsweise Brückenträger. Aufgrund des verhältnismässig hohen Gewichtes und der Herstellung solcher Stahllamellen ist die maximale einsetzbare Länge beschränkt. Ebenfalls kann aus Platzgründen der Einsatz in geschlossenen Räumen problematisch sein, wenn die starren Stahllamellen nicht in den entsprechenden Raum transportiert werden können. Zudem sind die Stahllamellen bei Applikationen "über Kopf" bis zum Aushärten des Klebstoffes gegen die zu verstärkende Tragstruktur anzupressen, was ebenfalls einen hohen Aufwand bedeutet.The reinforcement of such has long been known Support structures with retrofitted steel plates. The steel plates, i.e. band-shaped steel sheets resp. Steel slats are placed on one or two sides of the Glued supporting structure, preferably on the train loaded sides of the supporting structure. The advantage of this The process was that it was relatively quick can be carried out, but high demands the glue, i.e. the preparation of the parts and the Implementation of the gluing must be under precisely defined Ratios take place to get the desired effect to reach. Problems with this method occur in particular in the corrosion area, i.e. if supporting structures in Outdoor should be strengthened in such a way, for example Bridge girders. Because of the relatively high Weight and the manufacture of such steel slats is the maximum usable length limited. Can also from For reasons of space, use in closed rooms be problematic if the rigid steel fins are not in the corresponding space can be transported. In addition are the steel slats in applications "overhead" to for curing the adhesive against the one to be reinforced Pressing the supporting structure, which is also a high cost means.

Es ist aus der FR 2 590 608 bekannt, Spannmittel in Form von Bändern aus Metall oder Faserverstärktem Kunststoff über Endverankerungen einzusetzen. Bei dieser Ausführungsform erfolgt jedoch keine flächige Verbindung der Spannmittel mit der Tragkonstruktion, sondern es sind lediglich in den beiden Endverankerungspunkten der Spannmittel eine Verbindung mit der Tragkonstruktion vorgesehen. Derartige Spannmittel werden herkömmlicherweise bereits bei der Planung der Tragkonstruktion einbezogen, da eine nachträgliche Ausrüstung praktisch nicht oder nur mit sehr hohem Aufwand realisiert werden kann, da für die Spannmittel entsprechende Kanäle im Tragwerk erstellt werden müssen.It is known from FR 2 590 608, clamping means in the form of strips made of metal or fiber-reinforced plastic to be used over end anchorages. At this Embodiment, however, there is no flat connection of the clamping device with the supporting structure, but it is only in the two anchor points of the Clamping means a connection with the supporting structure intended. Such clamping devices are conventional already included in the planning of the supporting structure, because a subsequent equipment practically not or only with very high effort can be realized because for the Corresponding channels created in the supporting structure Need to become.

Neuerdings werden nun auch Kohlenstofflamellen (CFK-Lamellen) auf die Zugseiten der Tragkonstruktion aufgeklebt und damit die Tragfähigkeit solcher Konstruktionen durch Erhöhung des Tragwiderstandes und der Duktilität nachträglich verbessert. Vorteilhaft dabei sind die einfache und kostengünstige Applikation solcher Lamellen, welche eine höhere Festigkeit als die Stahllamellen bei weitaus geringerem Gewicht aufweisen und einfacher zu lagern sind. Ebenfalls ist die Korrosionsbeständigkeit besser, weshalb solche Verstärkungen auch für die Verstärkung von Tragkonstruktionen im Freien geeignet sind. Dabei hat sich nun aber besonders die Endverankerung der Lamellen als problematisch erwiesen. Gerade in diesem Bereich ist die Gefahr der Ablösung der Lamellen besonders gross und es besteht das Problem der Krafteinleitung vom Lamellenende in den Träger.Recently, carbon fins (CFRP fins) glued to the train sides of the supporting structure and thus the load-bearing capacity of such constructions Increasing the load resistance and ductility subsequently improved. They are advantageous here simple and inexpensive application of such slats, which has a higher strength than the steel fins have much less weight and easier to are stored. The corrosion resistance is also better, which is why such reinforcements also for the Reinforcement of supporting structures are suitable outdoors. However, the final anchorage of the Slats proved problematic. Especially in this Area, the danger of the slats becoming detached is special large and there is the problem of force transmission from Slat end in the carrier.

Eine diesbezügliche Lösung ist aus der WO96/21785 bekannt, bei welcher eine in einem flachen Winkel verlaufende Bohrung resp. keilförmige Ausnehmung im Träger angebracht wird, in welche die Enden der CFK-Lamellen eingebracht werden und ggf. mittels Bügel, Schlaufen, Platten etc. gegen den Träger angepresst werden. Dies führt nun bereits zu einer Verbesserung des Ablöseverhaltens und besseren Krafteinleitung vom Träger in die Lamelle. Allerdings werden derartige CFK-Lamellen ohne Vorspannung, d.h. schlaff, auf den Träger aufgeklebt. Damit wird jedoch ein grosser Teil des Verstärkungspotentials dieser Lamellen nicht genutzt, da diese erst nach Ueberschreiten der Grundlast, d.h. unter Beanspruchung durch die eigentliche Nutzlast, zu tragen beginnen.A solution in this regard is known from WO96 / 21785, where one is at a flat angle Hole respectively Wedge-shaped recess in the carrier into which the ends of the CFRP slats are inserted and if necessary by means of brackets, loops, plates etc. be pressed against the carrier. This already leads to improve the peeling behavior and better Force transmission from the carrier into the lamella. Indeed CFRP slats of this type are used without pre-tensioning, i.e. limp, glued to the carrier. However, this becomes a large part of the reinforcement potential of these slats not used, since this only after the Base load, i.e. under stress from the actual Payload, start carrying.

Um die Lamellen besser auszunützen, ist nun der Gedanke aufgetaucht, diese vorgespannt auf den Träger aufzukleben. Eine bekannte Lösung sieht diesbezüglich vor, dass an den Enden der CFK-Lamellen beidseitig kurze Stahlplatten aufgeleimt werden, die Stahlplatten dann voneinander weg verspannt und damit die CFK-Lamelle vorgespannt werden und diese vorgespannte Anordnung mit dem zu verstärkenden Träger verleimt wird. Nach der Trocknung der Verleimung werden die Lamellen an den Enden mittels Platten, Schlaufen etc. gegen den Träger gepresst und anschliessend die Enden mit den Stahlplatten abgetrennt. Dieses Verfahren ist nun aber sehr aufwendig und kann auch nicht bei allen Anwendungsfällen eingesetzt werden. Die obig beschriebene Verankerungsart der Lamellenenden eignet sich nun aber nicht für die Vorspannung auf Baustellen.The thought is now to make better use of the slats surfaced, glue them pretensioned on the carrier. A known solution provides in this regard that the The ends of the CFRP slats have short steel plates on both sides be glued on, the steel plates then away from each other braced and thus the CFRP lamella are prestressed and this biased arrangement with the one to be reinforced Carrier is glued. After the glue has dried the slats at the ends by means of plates, loops etc. pressed against the carrier and then the ends separated with the steel plates. This procedure is now but very complex and can’t work with everyone Use cases are used. The one described above Anchoring of the slat ends is now suitable not for pre-tensioning on construction sites.

Die Aufgabe der vorliegenden Erfindung lag nun darin, eine CFK-Verstärkungslamelle zu finden, bei welcher die Krafteinleitung vom Träger in die Enden derart erfolgt, dass eine Ablösung praktisch vermieden wird und welche sich auch für die Vorspannung eignet.The object of the present invention was now a CFRP reinforcement lamella, where the Force is transmitted from the carrier into the ends in such a way that detachment is practically avoided and which one also suitable for preloading.

Diese Aufgabe wird erfindungsgemäss durch eine CFK-Lamelle mit den Merkmalen von Anspruch 1 resp. durch das Verfahren nach Anspruch 11 gelöst. Bevorzugte Ausführungsformen der Erfindung ergeben sich aus den abhängigen Ansprüchen 2 bis 10 resp. 12 bis 14.According to the invention, this object is achieved by a CFRP lamella with the features of claim 1 respectively. through the process solved according to claim 11. Preferred embodiments of the Invention result from the dependent claims 2 to 10 resp. 12 to 14.

Durch das Aufspalten der Enden einer CFK-Lamelle in wenigstens zwei, vorzugsweise drei oder mehr Endfahnen wird die Oberfläche zur Verbindung mit einem Abschlusselement wesentlich vergrössert. Damit erfolgt nun eine gute Krafteinleitung in die Enden der CFK-Lamelle, welche über ein solches Abschlusselement auch einfach vorgespannt werden können. Das in Blockform ausgebildete Abschlusselement kann nun entweder in eine Vertiefung im Träger eingesetzt werden oder in der bevorzugten Ausführungsform mit keilförmiger Aufspaltung mit flachem oder rauhem Boden auch einfach auf den Träger flächig aufgeklebt und/oder verdübelt resp. verschraubt werden. Gerade diese Ausführungsform eignet sich vorzüglich für die Vorspannung, welche vorzugsweise direkt über den Trägerteil erfolgt. Beispielsweise kann dies durch Verspannung gegenüber einem in den Träger eingesetzten Beschlagsteil erfolgen.By splitting the ends of a CFRP lamella in at least two, preferably three or more end flags the surface for connection to a termination element significantly enlarged. So now there is a good one Force transmission into the ends of the CFRP lamella, which over such a termination element is also simply biased can be. The one trained in block form Closing element can now either be in a recess in the Carrier used or in the preferred Embodiment with wedge-shaped splitting with flat or rough floor also simply flat on the carrier glued and / or pegged or be screwed. This embodiment is particularly suitable for Preload, which is preferably directly over the support part he follows. For example, this can be caused by tension compared to a fitting part inserted into the carrier respectively.

Die Aufspaltung der Enden der CFK-Lamellen kann vorzugsweise entweder in übereinanderliegende Fahnen oder nebeneinanderliegende Fahnen erfolgen, resp. in einer Kombination aus diesen beiden Varianten.The ends of the CFRP slats can be split preferably either in superimposed flags or juxtaposed flags take place, respectively. in a Combination of these two variants.

Das Aufspalten der Enden der CFK-Lamellen kann vorteilhafterweise auf der Baustelle selbst in den jeweils erforderlichen Längen und Dimensionen erfolgen. Damit ist dieses System sehr universell für die Verstärkung von praktisch beliebigen Trägerbauteilen geeignet und kann mit oder auch ohne Vorspannung eingesetzt werden.The ends of the CFRP slats can be split advantageously at the construction site itself in each required lengths and dimensions. So that is this system is very universal for amplifying suitable for practically any support components and can be used with or can also be used without pretension.

Ein Ausführungsbeispiel der Erfindung wird nachstehend anhand von Figuren der beiliegenden Zeichnung noch näher erläutert. Es zeigen

  • Fig. 1 den Querschnitt durch einen Träger mit auf der Unterseite angebrachter erfindungsgemässer CFK-Lamelle;
  • Fig. 2 den Querschnitt durch den Kopfteil der CFK-Lamelle nach Figur 1;
  • Fig. 3 den Querschnitt durch das Ende einer CFK-Lamelle nach Figur 1 und 2;
  • Fig. 4 den Querschnitt durch einen Träger mit auf der Unterseite angebrachter weiterer erfindungsgemässer CFK-Lamelle;
  • Fig. 5 den Querschnitt durch den Kopfteil der CFK-Lamelle nach Figur 4;
  • Fig. 6 den schematischen Querschnitt durch einen erfindungsgemässen alternativen Kopfteil einer CFK-Lamelle;
  • Fig. 7 einen schematischen Querschnitt durch einen weiteren erfindungsgemässen alternativen Kopteil einer CFK-Lamelle;
  • Fig. 8 die Aufsicht auf eine weitere alternative Ausführungsform des Kopfteils einer CFK-Lamelle.
  • An embodiment of the invention is explained below with reference to figures of the accompanying drawings. Show it
  • Figure 1 shows the cross section through a carrier with CFRP lamella according to the invention attached to the underside.
  • 2 shows the cross section through the head part of the CFRP lamella according to FIG. 1;
  • 3 shows the cross section through the end of a CFRP lamella according to FIGS. 1 and 2;
  • 4 shows the cross section through a carrier with a further CFRP lamella according to the invention attached to the underside;
  • 5 shows the cross section through the head part of the CFRP lamella according to FIG. 4;
  • 6 shows the schematic cross section through an alternative head part of a CFRP lamella according to the invention;
  • 7 shows a schematic cross section through a further alternative head part of a CFRP lamella according to the invention;
  • Fig. 8 is a plan view of a further alternative embodiment of the head part of a CFRP lamella.
  • Figur 1 zeigt nun den Querschnitt durch einen zu verstärkenden Träger 1. Die Enden der hierfür eingesetzten CFK-Lamelle 2 sind erfindungsgemäss in Abschlusselemente, hier Ankerköpfen 3 und 4, eingesetzt. Die Ankerköpfe 3,4 können in gefrästen oder gespitzten Ausnehmungen des Trägers 1 eingesetzt werden, wie in dieser Figur dargestellt. Die CFK-Lamelle 2 wird mittels einer Kleberschicht 5 mit dem Träger 1 ganzflächig oder partiell verbunden, ebenso werden auch die Ankerköpfe 3,4 damit verklebt. Zusätzlich können die Ankerköpfe 3,4 durch eine Querspannvorrichtung 6, hier nur rein schematisch dargestellt, mit dem Träger verbunden sein, was zu einer besseren Krafteinleitung über die Ankerköpfe 3,4 von der CFK-Lamelle 2 in den Träger 1 führt. Dies Querspannvorrichtung 6 kann beispielsweise über durch den Träger 1 und die Ankerköpfe 3,4 hindurchgeführte Gewindestangen oder Dübel erfolgen.Figure 1 now shows the cross section through a reinforcing beam 1. The ends of the used for this CFRP slats 2 are, according to the invention, in end elements, here anchor heads 3 and 4 used. The anchor heads 3,4 can be milled or tapered recesses of the Carrier 1 can be used, as in this figure shown. The CFRP lamella 2 is by means of a Adhesive layer 5 with the carrier 1 over the entire surface or partially connected, as well as the anchor heads 3, 4 glued. In addition, the anchor heads 3.4 by a Cross clamping device 6, here only purely schematically shown to be connected to the carrier, resulting in a better force transmission via the anchor heads 3.4 from the CFRP lamella 2 leads into the carrier 1. This Cross-clamping device 6 can, for example, through the Carrier 1 and the anchor heads 3, 4 passed through Threaded rods or dowels are made.

    Die aus der CFK-Lamelle 2 und den Ankerköpfen 3,4 gebildete Verstärkungsvorrichtung kann nun auch einfach vorgespannt werden, wie auf der rechten Seite der Figur 1 schematisch dargestellt ist. Hierfür kann beispielsweise auf der Trägerunterseite 1 ein Winkelbeschlag 7 befestigt werden, an welchen eine Spannstange 8, welche an ihrem eine Ende mit dem Ankerkopf 4 verbunden ist, angreift. Es ist vorteihaft, dass für eine Vorspannung beide Ankerköpfe 3,4 mit einer solchen Spannvorrichtung ausgerüstet werden müssen. Die Spannvorrichtung wird vor dem Aufkleben angebracht und kann nach dem Aushärten der Klebeverbindung zwischen der CFK-Lamelle 2 resp. den Ankerköpfen 3,4 und dem Träger 1 wieder entfernt werden.The formed from the CFRP lamella 2 and the anchor heads 3.4 Reinforcement device can now also be simply biased are, as on the right side of Figure 1 schematically is shown. For example, on the An underside fitting 7 can be attached to the underside of the support 1 to which a tie rod 8, which at one end is connected to the anchor head 4, attacks. It is advantageous that both anchor heads 3.4 be equipped with such a clamping device have to. The clamping device is before sticking attached and can after curing the adhesive bond between the CFRP lamella 2 and the anchor heads 3,4 and the carrier 1 can be removed again.

    Figur 2 zeigt nun den Querschnitt durch einen der Ankerköpfe 3. Im quaderförmigen Ankerkopf 3 sind hier vorzugsweise drei Führungs- resp. Halteschlitze 9 übereinanderliegend angeordnet, welche das in drei Fahnen 2' aufgeteilte Ende der CFK-Lamelle 2, wie in Figur 3 dargestellt, aufnehmen kann. Die Halteschlitze 9 sind hier nach oben und unten keilförmig abgespreizt angeordnet und weisen querverlaufende Bohrungen 10 auf. Diese Bohrungen 10 ergeben zusätzliche Verankerungspunkte für die Klebemasse, mit welcher die Fahnen 2' der CFK-Lamelle 2 mit den Halteschlitzen 9 verbunden werden. Damit wird die Einleitung von Zugkräften vom Träger 1 über den Ankerkopf 3 in die CFK-Lamelle 2 zusätzlich verbessert. Der grosse Vorteil liegt allerdings in der Aufspaltung des Endes der Lamelle 2 in die Fahnen 2'. Diese Aufspaltung erfolgt vorzugsweise in Faserrichtung der Lamellen, und es wird damit vorteilhafterweise eine Vergrösserung der Klebefläche erreicht, ohne dass die Festigkeitseigenschaften der CFK-Lamelle 2 beeinträchtigt werden.Figure 2 now shows the cross section through one of the Anchor heads 3. In the cuboid anchor head 3 are here preferably three leadership resp. Holding slots 9 arranged one above the other in three flags 2 'split end of the CFRP lamella 2, as in FIG. 3 shown, can record. The holding slots 9 are here arranged widened upwards and downwards and have transverse bores 10. These holes 10 result in additional anchoring points for the adhesive, with which the flags 2 'of the CFRP lamella 2 with the Holding slots 9 are connected. With that the Introduction of tensile forces from the beam 1 via the anchor head 3 improved in the CFRP lamella 2. The great However, the advantage lies in splitting the end of the Lamella 2 in the flags 2 '. This split takes place preferably in the grain of the slats, and it will thus advantageously an enlargement of the adhesive surface achieved without the strength properties of the CFRP lamella 2 are affected.

    Im vorliegenden Beispiel mit drei Fahnen 2' wird die Klebefläche gegenüber einer herkömmlichen Lamelle, welche an ihrem Ende lediglich auf den Träger aufgeklebt ist, versechsfacht, gegenüber der bekannten Lösung mit keilförmiger Ausnehmung im Träger und Haftbrücken immer noch verdreifacht!In the present example with three flags 2 ' Adhesive surface compared to a conventional lamella, which is only glued to the carrier at the end, sixfold compared to the known solution wedge-shaped recess in the carrier and adhesive bridges always tripled!

    Um im Austrittsbereich der CFK-Lamelle 2 aus dem Ankerkopf 3 ein aufbiegen oder aufreissen der Ankerkopfes durch Querkräfte, welche aus der keil- oder bogenförmigen Anordnung der Halteschlitze 9 herrühren, zu vermeiden, ist vorzugsweise eine Querverstärkung 11 anzubringen, welche in Figur 2 nur schematisch angedeutet ist. Beispielsweise kann diese Querverstärkung 11 mittels durch entsprechende Bohrungen im Ankerkopf 3 hindurchgeführte und über Muttern verspannte Gewindestangen erfolgen. Somit werden allfällige Schubspannungsspitzen im Austrittsbereich des Ankerkopfes 3 überdrückt und grössere Schubspannungen in dieser Zone zulässig.To in the exit area of the CFRP lamella 2 from the anchor head 3 bend or open the anchor head Lateral forces resulting from the wedge or arcuate Arrange the arrangement of the holding slots 9, is to be avoided preferably to install a transverse reinforcement 11, which in Figure 2 is only indicated schematically. For example this transverse reinforcement 11 by means of appropriate Bores in the anchor head 3 and passed through nuts tensioned threaded rods. Thus, any Shear stress peaks in the exit area of the anchor head 3 depressed and greater shear stresses in this zone allowed.

    Weiter ist im Ankerkopf 3 beispielsweise eine Gewindebohrung 12 angebracht, in welche eine Vorspannvorrichtung eingeschraubt werden kann, wie dies schematisch in Figur 1 dargestellt ist.Next is in the anchor head 3, for example Threaded bore 12 attached, in which a Tensioner can be screwed in like this is shown schematically in Figure 1.

    Figur 3 zeigt, wie bereits erwähnt, ein Ende der CFK-Lamelle 2 mit dem in drei Fahnen 2' aufgespaltenen Lamellenende. Die CFK-Lamelle kann mit herkömmlichen Mitteln nach dem Ablängen auf die gewünschte Länge in die gewünschte Anzahl, in etwa gleich dicker Fahnen 2' aufgespalten werden, beispielsweise mittels eines Hobels oder Messers. Vorteilhaft dabei ist, dass an die Qualität der Aufspaltung verhältnismässig geringe Anforderungen gestellt werden, wesentlich ist die Aufteilung in die entsprechende Anzahl Fahnen 2' zur Erzielung der Flächenvergrösserung für die Verbindung mit dem Ankerkopf 3.As already mentioned, FIG. 3 shows one end of the CFRP lamella 2 with the split into three flags 2 ' Slat end. The CFRP slat can be used with conventional After cutting to length to the desired length desired number, flags of approximately the same thickness 2 ' be split up, for example by means of a plane or knife. The advantage here is that in terms of quality the splitting relatively low requirements be divided into the essentials corresponding number of flags 2 'to achieve the Area enlargement for the connection with the anchor head 3rd

    In Figur 4 ist nun der Querschnitt durch einen Träger 1 mit an der Unterseite (Zugseite) angebrachtem, erfindungsgemässen Verstärkungsvorrichtung, bestehend aus einer CFK-Lamelle 2 mit an den Enden angebrachten Ankerköpfen 12 und 13. Die Ankerköpfe 12, 13 sind nun derart ausgebildet, dass die CFK-Lamelle 2 praktisch auf der Höhe der Kleberschicht 5 aus den Ankerköpfen 12, 13 austritt, und diese damit nicht versenkt in der Unterseite des Trägers 1 angeordnet sein müssen, sondern ebenfalls flächig auf diese Unterseite beispielsweise angeklebt werden können. Selbstverständlich können auch hier die in Figur 1 angedeuteten Querspannvorrichtungen 6 angebracht werden, um einen höheren Anpressdruck und damit eine höhere Zugfestigkeit der Verbindung zwischen den Ankerköpfen 12, 13 und der Trägerunterseite zu bewirken. Ebenfalls lassen sich diese Ankerköpfe 12, 13, wie die bereits vorgängig beschriebenen Ausführungsform, einfach vorspannen.In Figure 4, the cross section through a carrier 1 is now with attached to the underside (train side) Reinforcement device according to the invention, consisting of a CFRP lamella 2 with attached at the ends Anchor heads 12 and 13. The anchor heads 12, 13 are now formed such that the CFRP lamella 2 practically the height of the adhesive layer 5 from the anchor heads 12, 13 emerges, and thus not sunk in the bottom of the carrier 1 must be arranged, but also glued flat on this underside, for example can be. Of course, the in Figure 1 indicated cross-tensioning devices 6 attached to a higher contact pressure and thus a higher Tensile strength of the connection between the anchor heads 12, 13 and the underside of the carrier. Also leave these anchor heads 12, 13, like the one previously mentioned described embodiment, simply pretension.

    Figur 5 zeigt nun noch den Querschnitt durch einen Ankerkopf 12 und der entsprechenden Anordnung der Halteschlitze 9. Der unterste Schlitz 9' ist dabei parallel zur auf den Träger 1 aufliegenden Aussenwand 12' des Ankerkopfes 12 ausgebildet, die übrigen Schlitze 9 sind unter einem spitzen Winkel dazu fächerförmig gegen Aussen weisend angeordnet. Diese Anordnung bringt einerseits durch die Vergrösserung der Verklebungsoberfläche der CFK-Lamelle 2 dieselben Vorteile wie bereits beschrieben, und ermöglicht andererseits das flächige Aufbringen auch der Ankerköpfe 12, 13 ohne zusätzliche Ausnehmungen am Träger 1. Auch bei diesen Ankerköpfen 12, 13 sind Querverstärkungsmittel 11, wie in Figur 2 schematisch dargestellt, zur Vermeidung des Aufbiegens oder Aufreissens der Ankerköpfe 12, 13 im Bereich des Austritts der CFK-Lamelle 2.Figure 5 now shows the cross section through a Anchor head 12 and the corresponding arrangement of the Holding slots 9. The bottom slot 9 'is parallel to the outer wall 12 'of the support lying on the support 1 Anchor head 12 formed, the remaining slots 9 are fan-shaped towards the outside at an acute angle arranged pointing. On the one hand, this arrangement brings about the enlargement of the bonding surface of the CFRP lamella 2 the same advantages as already described, and on the other hand, enables the flat application of the Anchor heads 12, 13 without additional recesses on the carrier 1. Also in these anchor heads 12, 13 are Cross reinforcement means 11, as schematically in Figure 2 shown to avoid bending or tearing open the anchor heads 12, 13 in the area of the exit of the CFRP lamella 2nd

    Als Material für die Ankerköpfe 3,4 resp. 12, 13 eignet sich einerseits Metall, welches eine hohe Festigkeit, einfache Bearbeitbarkeit und gute Krafteinleitungseigenschaften aufweist, und andererseits auch Kunststoff, insbesondere wenn die Korrosionsanforderungen hoch sein müssen. As a material for the anchor heads 3.4, respectively. 12, 13 is suitable metal, which has a high strength, easy workability and good Has force introduction properties, and on the other hand also plastic, especially if the Corrosion requirements must be high.

    In Figur 6 ist nun die schematische Ansicht einer weiteren Ausführungsform der erfindungsgemässen Verstärkungsvorrichtung dargestellt. Das Ende der CFK-Lamelle 2 ist hier in zwei übereinanderliegende Fahnen 2' aufgespalten, welche an die Aussenseite eines keilförmig ausgestalteten Ankerkopfes 14 zu liegen kommen. Sie können dort wiederum mit der Oberfläche des Ankerkopfes 14 durch eine Verklebung verbunden werden.In Figure 6 is now the schematic view of another Embodiment of the invention Reinforcement device shown. The end of the CFRP slat 2 is here in two superimposed flags 2 ' split which is wedge-shaped on the outside designed anchor head 14 come to rest. You can there again with the surface of the anchor head 14 an adhesive bond.

    In einer weiteren erfindungsgemässen Ausführungsform werden die aufgespaltenen Fahnen 2' des Endes der CFK-Lamelle 2 in einem aus parallel übereinander angeordneten Platten 15 gebildeten Ankerkopf gehalten, wie in Figur 7 im Längsschnitt dargestellt. Hier kann vorteilhafterweise zusätzlich eine Verschraubung 16 zum gegenseitigen Anpressen der Platten 15 resp. der Fahnen 2' eingesetzt werden.In a further embodiment according to the invention the split flags 2 'of the end of the CFRP lamella 2 in one of plates 15 arranged one above the other in parallel formed anchor head held, as in Figure 7 in Longitudinal section shown. Here can be advantageous additionally a screw 16 for mutual Pressing the plates 15 respectively. the flags 2 'used become.

    In Figur 8 ist weiter die Aufsicht auf eine weitere Ausführungsform des Endes der CFK-Lamelle 2 dargestellt. Hier sind die Fahnen 2' nun nicht übereinander ausgebildet, sondern sind seitlich nebeneinander ausgebildet. Auch hier wird die Aufspaltung vorzugsweise entlang der Faserrichtung der CFK-Lamelle 2 vorgenommen.In Figure 8 is the supervision of another Embodiment of the end of the CFRP lamella 2 shown. Here the flags 2 'are not formed one above the other, but are formed side by side. Here too the splitting is preferably along the grain made of CFRP lamella 2.

    Die erfindungsgemässen Verstärkungsvorrichtungen eignen sich insbesondere für die Sanierung von bestehenden Beton-Trägerstrukturen, wie beispielsweise Decken oder Brückenträger. Allerdings können sie auch für alle bekannten Anwendungen von herkömmlichen CFK-Lamellen eingesetzt werden, wie beispielsweise Mauerwerke und Holztragwerke. Die einfache Vorspannbarkeit ermöglichen die höhere Ausnützung der Festigkeitseigenschaften der CFK-Lamellen als bei den bislang bekannten Verfahren. Zudem bewirkt die Vorspannung, dass auf der Zugseite eines bestehenden Tragelementes eine Vorpressung erfolgt, was gerade beispielsweise bei Brückenträgern vorteilhaft ist.The reinforcement devices according to the invention are suitable are particularly interested in the renovation of existing concrete support structures, such as blankets or Bridge girders. However, they can be for everyone known applications of conventional CFRP slats are used, such as masonry and Wooden structures. The easy preload enable the higher utilization of the strength properties of the CFRP slats than with the previously known methods. In addition the preload causes that on the pull side existing support element is pre-pressed what is particularly advantageous for bridge girders, for example.

    Claims (14)

    1. Reinforcing device for supporting structures (1) with CFK panel (2) characterized in that at least one end of CFK panel (2) is split into at least two strips (2') and terminates in an end element (3, 4; 12, 13).
    2. Reinforcing device according to Claim 1 characterized in that each of the two ends of CFK panel (2) terminates in an end element (3, 4; 12, 13).
    3. Reinforcing device according to Claim 1 or 2 characterized in that the strips (2') are inserted at least partially into retaining slots (9; 9') of end element (3, 4; 12, 13) that are preferably located wedgewise relative to one another.
    4. Reinforcing device according to one of Claims 1 to 3 characterized in that the panel ends (2') are split into superimposed strips of approximately equal thickness.
    5. Reinforcing device according to one of Claims 1 to 4 characterized in that retaining slots (9) of end element (3, 4; 12, 13) have a rough or corrugated surface.
    6. Reinforcing device according to one of Claims 1 to 5 characterized in that bores (10) located transversely to the surface of the panel are located in end element (3) in the vicinity of retaining slots (9).
    7. Reinforcing device according to one of Claims 1 to 6 characterized in that the end element (3, 4; 12, 13) is a parallelepiped made of metal or plastic.
    8. Reinforcing device according to one of Claims 1 to 7 characterized in that the end element (3, 4; 12, 13) in the vicinity of the outlet of the CFK panel (2) has reinforcing devices (11), preferably threaded bolts, located transversely to the outlet direction.
    9. Reinforcing device according to one of Claims 1 to 8 characterized in that the end element (3, 4; 12, 13) has a force-introduction point, preferably a threaded bore (12) opposite the outlet of the CFK panel.
    10. Reinforcing device according to one of Claims 1 to 9 characterized in that the retaining slots (9) are located wedgewise in end element (3, 4; 12, 13) in such fashion that the lowest retaining slot (9') is parallel to the outlet direction of panel (2) and the other retaining slots (9) are each located fanwise with an increasing angle from the outlet opening.
    11. Method for reinforcing supporting elements (1) with reinforcing devices according to one of Claims 1 to 10 characterized in that the CFK panels (2) cut to the appropriate length are separated or split at at least one end into at least two strips (2') of approximately the same thickness or width and are brought into a connection with an end element (3, 4; 12, 13) and this arrangement is glued to the tension side of the supporting element (1) to be reinforced.
    12. Method according to Claim 11 characterized in that the strips (2') of CFK panel (2) are introduced into separate retaining slots (9, 9') of an end element (3, 4; 12, 13) preferably arranged fanwise with respect to one another and glued there or soaked with an adhesive.
    13. Method according to Claim 11 or 12 characterized in that the ends of the CFK strips (2) are each separated or split into three strips (2') and the arrangement, before gluing with supporting element (1), is pretensioned relative to the latter by clamping means (7, 8) and then glued in the pretensioned state to supporting element (1).
    14. Method according to one of Claims 11 to 13 characterized in that the CFK panel (2) is split in the fiber direction.
    EP98937382A 1997-08-26 1998-08-18 Reinforcement device for supporting structures Expired - Lifetime EP1007809B1 (en)

    Applications Claiming Priority (3)

    Application Number Priority Date Filing Date Title
    CH198797 1997-08-26
    CH198797 1997-08-26
    PCT/CH1998/000346 WO1999010613A1 (en) 1997-08-26 1998-08-18 Reinforcement device for supporting structures

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    EP1007809A1 EP1007809A1 (en) 2000-06-14
    EP1007809B1 true EP1007809B1 (en) 2001-10-10

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    EP (1) EP1007809B1 (en)
    JP (1) JP4202596B2 (en)
    CN (1) CN1131365C (en)
    AT (1) ATE206794T1 (en)
    AU (1) AU740242B2 (en)
    BR (1) BR9812141A (en)
    CA (1) CA2301755C (en)
    DE (1) DE59801706D1 (en)
    ES (1) ES2165693T3 (en)
    NO (1) NO313806B1 (en)
    NZ (1) NZ503251A (en)
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    Cited By (1)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE102012201518A1 (en) * 2012-02-02 2013-08-08 Sgl Carbon Se Reinforcement system for buildings

    Families Citing this family (53)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE19742210A1 (en) * 1997-09-24 1999-03-25 Goehler Bernhard Dipl Ing Concrete-strengthening and repairing system
    CH693616A5 (en) * 1999-09-15 2003-11-14 Empa An anchoring system for receiving the tensile forces from carbon fiber reinforced drawstrings (CFRP tapes).
    US6668457B1 (en) * 1999-12-10 2003-12-30 L&L Products, Inc. Heat-activated structural foam reinforced hydroform
    MXPA02007795A (en) * 2000-02-11 2005-06-06 L & L Products Inc Structural reinforcement system for automotive vehicles.
    JP2002030727A (en) * 2000-07-18 2002-01-31 Asante Inc How to reinforce the joints of wooden structures
    US6634698B2 (en) * 2000-08-14 2003-10-21 L&L Products, Inc. Vibrational reduction system for automotive vehicles
    JP2002097746A (en) * 2000-09-21 2002-04-05 Dps Bridge Works Co Ltd FRP reinforcement with fixing device
    GB0106911D0 (en) * 2001-03-20 2001-05-09 L & L Products Structural foam
    GB2375328A (en) * 2001-05-08 2002-11-13 L & L Products Reinforcing element for hollow structural member
    US6793274B2 (en) * 2001-11-14 2004-09-21 L&L Products, Inc. Automotive rail/frame energy management system
    EP1331327A1 (en) * 2002-01-29 2003-07-30 Sika Schweiz AG Reinforcing device
    US7318873B2 (en) 2002-03-29 2008-01-15 Zephyros, Inc. Structurally reinforced members
    US7169344B2 (en) * 2002-04-26 2007-01-30 L&L Products, Inc. Method of reinforcing at least a portion of a structure
    US7077460B2 (en) 2002-04-30 2006-07-18 L&L Products, Inc. Reinforcement system utilizing a hollow carrier
    GB0211775D0 (en) * 2002-05-23 2002-07-03 L & L Products Inc Multi segment parts
    US20040018353A1 (en) * 2002-07-25 2004-01-29 L&L Products, Inc. Composite metal foam damping/reinforcement structure
    US20040034982A1 (en) * 2002-07-30 2004-02-26 L&L Products, Inc. System and method for sealing, baffling or reinforcing
    US7105112B2 (en) * 2002-11-05 2006-09-12 L&L Products, Inc. Lightweight member for reinforcing, sealing or baffling
    US7313865B2 (en) * 2003-01-28 2008-01-01 Zephyros, Inc. Process of forming a baffling, sealing or reinforcement member with thermoset carrier member
    US7111899B2 (en) * 2003-04-23 2006-09-26 L & L Products, Inc. Structural reinforcement member and method of use therefor
    GB2401349A (en) * 2003-05-08 2004-11-10 L & L Products Reinforcement for a vehicle panel
    US7249415B2 (en) * 2003-06-26 2007-07-31 Zephyros, Inc. Method of forming members for sealing or baffling
    US7784186B2 (en) * 2003-06-26 2010-08-31 Zephyros, Inc. Method of forming a fastenable member for sealing, baffling or reinforcing
    US20050016807A1 (en) * 2003-07-21 2005-01-27 L&L Products, Inc. Crash box
    EP1507052A1 (en) 2003-08-13 2005-02-16 Sika Technology AG Force transfer element
    EP1507050A1 (en) 2003-08-13 2005-02-16 Sika Technology AG Force transfer element
    US7469459B2 (en) * 2003-09-18 2008-12-30 Zephyros, Inc. System and method employing a porous container for sealing, baffling or reinforcing
    US20050166532A1 (en) * 2004-01-07 2005-08-04 L&L Products, Inc. Structurally reinforced panels
    US20050172486A1 (en) * 2004-02-05 2005-08-11 L&L Products, Inc. Member for sealing, baffling or reinforcing and method of forming same
    GB2415658A (en) * 2004-06-21 2006-01-04 L & L Products Inc An overmoulding process
    US20060021697A1 (en) * 2004-07-30 2006-02-02 L&L Products, Inc. Member for reinforcing, sealing or baffling and reinforcement system formed therewith
    US7374219B2 (en) * 2004-09-22 2008-05-20 Zephyros, Inc. Structural reinforcement member and method of use therefor
    US20060090343A1 (en) * 2004-10-28 2006-05-04 L&L Products, Inc. Member for reinforcing, sealing or baffling and reinforcement system formed therewith
    US7503620B2 (en) * 2005-05-12 2009-03-17 Zephyros, Inc. Structural reinforcement member and method of use therefor
    US7926179B2 (en) 2005-08-04 2011-04-19 Zephyros, Inc. Reinforcements, baffles and seals with malleable carriers
    US20070089829A1 (en) * 2005-10-25 2007-04-26 L&L Products, Inc. Strength pearls
    GB0600901D0 (en) * 2006-01-17 2006-02-22 L & L Products Inc Improvements in or relating to reinforcement of hollow profiles
    CA2649585C (en) * 2006-04-27 2015-07-14 Jeffrey Allan Packer Cast structural connectors
    US7934347B2 (en) * 2006-07-28 2011-05-03 Paul Brienen Coupling beam and method of use in building construction
    US8022960B2 (en) 2007-02-22 2011-09-20 Qualcomm Incorporated Dynamic configurable texture cache for multi-texturing
    US10858850B2 (en) * 2007-09-18 2020-12-08 Fortress Stabilization Systems Wall reinforcement system and method
    KR101085407B1 (en) * 2008-12-10 2011-11-22 한국건설기술연구원 FRP plate tensioning device installed in the form of spreading and its construction method
    IT1399040B1 (en) * 2010-01-27 2013-04-05 Fidia Srl PROCEDURE FOR THE REINFORCEMENT OF STRUCTURAL ELEMENTS
    US9194140B2 (en) * 2010-11-04 2015-11-24 Garland Industries, Inc. Method and apparatus for repairing concrete
    DE102012216818A1 (en) * 2012-09-19 2014-04-10 Bilfinger SE component
    EP3216944B1 (en) * 2013-06-06 2021-09-29 Sika Technology Ag Assembly for reinforcing support structures
    US9790697B2 (en) 2014-12-31 2017-10-17 Fortress Stabilization Systems Structure reinforcement system and method
    US9290956B1 (en) * 2014-12-31 2016-03-22 Fortress Stabilization Systems Structure reinforcement system and method
    US9290957B1 (en) * 2014-12-31 2016-03-22 Fortress Stabilization Systems Structure reinforcement system and method
    ITVI20150072A1 (en) 2015-03-16 2016-09-16 Carbonveneta Tecnologia Nei Compositi S R L PROCEDURE FOR MAKING A CONNECTOR OF THE SO-CALLED "BOW" TYPE
    CN111608418B (en) * 2020-05-26 2021-08-03 华中科技大学 A kind of FRP bar with embedded anchoring device and application method thereof
    USD979385S1 (en) * 2020-10-20 2023-02-28 Garland Industries, Inc. Concrete connector
    US12221797B2 (en) * 2022-02-09 2025-02-11 Duktil Frp Llc Fiber-reinforced polymer anchoring system

    Family Cites Families (9)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    FR2517017B1 (en) * 1981-11-20 1986-09-19 Caoutchouc Manuf Plastique
    US4966802A (en) * 1985-05-10 1990-10-30 The Boeing Company Composites made of fiber reinforced resin elements joined by adhesive
    FR2582077B2 (en) * 1985-05-14 1987-12-24 Caoutchouc Manuf Plastique IMPROVEMENT TO A DILATABLE PIPE DEVICE
    FR2590608B1 (en) 1985-11-26 1989-05-05 Freyssinet Int Stup IMPROVEMENTS IN PRE-STRESS DEVICES OR THE LIKE COMPRISING TIE RODS.
    DE3640549A1 (en) * 1986-11-27 1988-06-01 Strabag Bau Ag End anchoring for a tensioning member
    US5313749A (en) * 1992-04-28 1994-05-24 Conner Mitchel A Reinforced steel beam and girder
    US5471812A (en) * 1993-07-13 1995-12-05 Muller; Jean Method for fabricating pretensioned concrete structures
    ES2122696T3 (en) * 1995-01-09 1998-12-16 Empa FASTENING OF REINFORCEMENT SHEETS.
    FR2732984B1 (en) * 1995-04-13 1997-07-04 Europ Propulsion PROCESS FOR MANUFACTURING COMPLEX ONE-PIECE STRUCTURAL PARTS IN COMPOSITE MATERIAL

    Cited By (1)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE102012201518A1 (en) * 2012-02-02 2013-08-08 Sgl Carbon Se Reinforcement system for buildings

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    AU8621098A (en) 1999-03-16
    JP4202596B2 (en) 2008-12-24
    AU740242B2 (en) 2001-11-01
    NO313806B1 (en) 2002-12-02
    ATE206794T1 (en) 2001-10-15
    NZ503251A (en) 2001-07-27
    CA2301755A1 (en) 1999-03-04
    BR9812141A (en) 2000-07-18
    US6851232B1 (en) 2005-02-08
    NO20000887L (en) 2000-02-25
    CA2301755C (en) 2007-11-13
    PT1007809E (en) 2002-04-29
    JP2001514349A (en) 2001-09-11
    WO1999010613A1 (en) 1999-03-04
    CN1131365C (en) 2003-12-17
    NO20000887D0 (en) 2000-02-23
    CN1268205A (en) 2000-09-27
    EP1007809A1 (en) 2000-06-14
    ES2165693T3 (en) 2002-03-16
    DE59801706D1 (en) 2001-11-15

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