DE19607061C1 - Adhesive bonding of fibre compound board materials - Google Patents
Adhesive bonding of fibre compound board materialsInfo
- Publication number
- DE19607061C1 DE19607061C1 DE19607061A DE19607061A DE19607061C1 DE 19607061 C1 DE19607061 C1 DE 19607061C1 DE 19607061 A DE19607061 A DE 19607061A DE 19607061 A DE19607061 A DE 19607061A DE 19607061 C1 DE19607061 C1 DE 19607061C1
- Authority
- DE
- Germany
- Prior art keywords
- parts
- tongues
- adhesive
- wetted
- flat
- 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 - Fee Related
Links
- 239000000835 fiber Substances 0.000 title claims abstract description 12
- 238000004026 adhesive bonding Methods 0.000 title claims abstract description 9
- 239000000463 material Substances 0.000 title abstract 2
- 150000001875 compounds Chemical class 0.000 title 1
- 210000002105 tongue Anatomy 0.000 claims abstract description 41
- 239000000853 adhesive Substances 0.000 claims abstract description 21
- 230000001070 adhesive effect Effects 0.000 claims abstract description 21
- 239000002131 composite material Substances 0.000 claims abstract description 12
- 238000000034 method Methods 0.000 claims abstract description 12
- 238000006073 displacement reaction Methods 0.000 claims abstract 2
- 239000012790 adhesive layer Substances 0.000 claims description 3
- 239000003292 glue Substances 0.000 claims description 3
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 239000006260 foam Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
- F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/139—Interpenetrating fingered joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/22—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being in the form of recurring patterns
- B29C66/225—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being in the form of recurring patterns being castellated, e.g. in the form of a square wave or of a rectangular wave
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/723—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/725—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs
- B29C66/7252—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs hollow-walled
- B29C66/72525—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs hollow-walled comprising honeycomb cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/727—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being porous, e.g. foam
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/022—Mechanical pre-treatments, e.g. reshaping
- B29C66/0222—Mechanical pre-treatments, e.g. reshaping without removal of material, e.g. cleaning by air blowing or using brushes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/022—Mechanical pre-treatments, e.g. reshaping
- B29C66/0224—Mechanical pre-treatments, e.g. reshaping with removal of material
- B29C66/02241—Cutting, e.g. by using waterjets, or sawing
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
- Connection Of Plates (AREA)
- Joining Of Building Structures In Genera (AREA)
- Laminated Bodies (AREA)
Abstract
Description
Die vorliegende Erfindung betrifft ein Verfahren zur Durchführung einer geklebten Verbindung ebener oder flächiger Teile, insbesondere Platten oder Sandwich- Strukturen, z. B. aus Faserverbundwerkstoffen.The present invention relates to a method for Implementation of a glued connection level or flat parts, especially plates or sandwich Structures, e.g. B. from fiber composite materials.
Ebene oder gekrümmte flächige Platten oder Sandwich- Strukturen aus Faserverbundwerkstoffen müssen häufig durch flächige Klebungen fest und dauerhaft miteinander verbunden werden. Insbesondere in der Verkehrstechnik, beispielsweise im Waggon- und Fahrzeugbau, werden immer mehr Bauteile aus Faserverbundwerkstoffen eingesetzt, die miteinander verklebt werden, wobei diese Klebeverbindungen sowohl den wechselnden Witterungseinflüssen als auch starken mechanischen Belastungen durch Schwingungen und Rüttelbewegungen ausgesetzt sind. Besondere Anforderungen werden dabei an die miteinander durch Klebung verbundenen Bereiche der Einzelteile gestellt.Flat or curved flat sheets or sandwich Structures made of fiber composite materials often have to go through two-dimensional bonds firmly and permanently bonded together will. Especially in traffic engineering, for example in wagon and vehicle construction, more and more components are being made Fiber composite materials used together are glued, these adhesive connections both the changing weather conditions as well as strong ones mechanical loads caused by vibrations and Vibrations are exposed. Special requirements are connected to each other by gluing Areas of the individual parts.
Aufgabe der vorliegenden Erfindung ist es, ein Verfahren zu schaffen, mit dem eine definierte Verklebung ebener oder gekrümmter Teile, z. B. aus Faserverbundwerkstoffen, miteinander erzielt wird, wobei diese Klebefügung trotz mechanischer und witterungsbedingter Einflüsse eine hohe Lebensdauer aufweist und leicht und einfach zu bewerkstelligen ist.The object of the present invention is to provide a method create with which a defined bonding level or curved parts, e.g. B. from fiber composite materials, is achieved with each other, this adhesive joining despite mechanical and weather-related influences a high Has lifespan and is light and easy to use is accomplished.
Die Lösung dieser Aufgabe erfolgt mit den in den Ansprüchen 1 bis 3 angegebenen Schritten.This problem is solved with the in the claims 1 to 3 specified steps.
Mit dem erfindungsgemäßen Verfahren wird es ermöglicht, auf einfache, schnelle und kostengünstige Weise größere Strukturflächen wie gekrümmte oder flache Platten oder auch Sandwich-Strukturen definiert miteinander zu verkleben, wobei die beiden jeweils mit Zungen versehenen zusammen zufügenden Teile unter einem Winkel ineinandergeschoben werden, z. B. ähnlich zweier gefalteter Hände, und die beiden Teile (oder eines der Teile) erst nach dem vollständigen Ineinanderschieben in die endgültige Lage verschwenkt werden, in der die beiden Teile im wesentlichen in einer Ebene zu liegen kommen, so daß die mit Klebstoff benetzten Flächen einander berühren.With the method according to the invention it is possible to simple, fast and inexpensive way to make bigger ones Structural surfaces such as curved or flat plates or also Sandwich structures defined to stick together, with the two tongues together parts to be pushed together at an angle be, e.g. B. similar to two folded hands, and the both parts (or one of the parts) only after the completely sliding into the final position be pivoted in which the two parts essentially come to lie in one plane, so that with glue wetted surfaces touch each other.
Im folgenden wird die Erfindung anhand der Zeichnung näher erläutert, in der vorteilhafte Ausführungsbeispiele zur Durchführung des erfindungsgemäßen Verfahrens dargestellt sind. In the following the invention with reference to the drawing explained in the advantageous embodiments Implementation of the method according to the invention shown are.
Es zeigenShow it
Fig. 1 Draufsichten auf die Endbereiche mit den aus gebildeten Zungen zweier miteinander zu verklebender Teile; FIG. 1 shows plan views of the end portions of the two tongues formed from each other to be bonded parts;
Fig. 2 eine Seitenansicht der Zungen der beiden Teile; Fig. 2 is a side view of the tongues of the two parts;
Fig. 3a die beiden miteinander zu verklebenden Teile zu Beginn ihrer Zusammenfügung; FIG. 3a shows the two parts to be bonded together at the beginning of their assembly;
Fig. 3b dieselbe Ansicht wie in Fig. 3a zusammen mit der Benetzung der Kontaktflächen; FIG. 3b shows the same view as in Figure 3a together with the wetting of the contact surfaces.
Fig. 4 ein anderes Ausführungsbeispiel zweier miteinander zu verbindenden Teile; FIG. 4 shows another embodiment of two parts to be connected;
Fig. 5 eine Seitenansicht der Zungen der beiden Teile und Fig. 5 is a side view of the tongues of the two parts and
Fig. 6 und 7 Ausführungsbeispiele von miteinander zu ver bindenden Sandwich-Strukturen. FIGS. 6 and 7 embodiments of binding to each other ver sandwich structures.
In den Figuren, in denen gleiche Teile mit gleichen Bezugszeichen versehen sind, ist mit 1 ein erstes flächiges Teil aus einem Faserverbundwerkstoff bezeichnet, das mit einem zweiten flächigen Teil 2, ebenfalls aus Faser verbundwerkstoff, mit einer definierten Haltekraft zu ver kleben ist. Erfindungsgemäß sind nun die Endbereiche der beiden Teile 1 und 2 jeweils mit Zungen 6, 7 versehen, deren mit dem anderen Teil nach der Zusammenfügung in Kontakt gelangende Seiten, sowie die Flächen 3, 4, auf denen nach dem Zusammenfügen die Zungen 6, 7 zur Ruhe kommen, mit einem Klebstoff 3, 4 benetzt sind.In the figures, in which the same parts are provided with the same reference numerals, 1 denotes a first flat part made of a fiber composite material, which is to be glued to a second flat part 2 , also made of fiber composite material, with a defined holding force. According to the invention, the end regions of the two parts 1 and 2 are each provided with tongues 6 , 7 , the sides of which come into contact with the other part after the assembly, and the surfaces 3 , 4 on which, after the assembly, the tongues 6 , 7 for Calm down, are wetted with an adhesive 3 , 4 .
Damit die beiden Teile 1, 2 im wesentlichen nach der Ver klebung in der gleichen Ebene angeordnet sind, werden vorteilhafterweise die Zungen, wie in Fig. 2 dargestellt, jeweils mit einem Doppelknick versehen, so daß die Zungen 6, 7 einen Versatz zueinander aufweisen, wenn sie nach der Überlappung miteinander verklebt sind.So that the two parts 1 , 2 are arranged essentially after the bonding in the same plane, the tongues, as shown in FIG. 2, are advantageously each provided with a double bend, so that the tongues 6 , 7 are offset from one another, if they are glued together after the overlap.
Fig. 3a und 3b zeigen nun das erfindungsgemäße Verfahren, mit dem es ermöglicht wird, auch große Strukturflächen definiert miteinander zu verkleben. Die mit den Klebstoffen benetzten Zungen 6, 7 und damit auch die beiden miteinander zu verbindenden Teile 1, 2 werden hierbei unter einem Winkel α ineinander geschoben und erst nach Erreichen der Endstellung derart verschwenkt, daß die Zungen des einen Teils auf der zugehörigen Kontaktfläche des anderen Teils zu liegen kommen. Bei einer nun einsetzenden Querbelastung der nicht mit Klebestoff versehenen freien Oberflächen der Zungen 6, 7 und damit der zusammengefügten Teile 1, 2 kann ein beliebiger Anpreßdruck während des Aushärtungsprozesses aufgebracht werden. Aufgrund der Tatsache, daß die Zungen 6, 7 nicht in der gleichen Ebene auf die entsprechenden Kontaktflächen des anderen Teils geschoben werden, erhält man eine gleichmäßige nicht beeinträchtigte Dicke der Klebeschicht. FIGS. 3a and 3b show now the inventive method, with which it is possible, even large surfaces defined structure to stick together. The tongues 6 , 7 wetted with the adhesives and thus also the two parts 1 , 2 to be joined together are pushed into one another at an angle α and only pivoted after reaching the end position in such a way that the tongues of one part on the associated contact surface of the other Partly come to rest. If the free surfaces of the tongues 6 , 7, which are not provided with adhesive, and thus the joined parts 1 , 2 are now subjected to a transverse load, any contact pressure can be applied during the curing process. Due to the fact that the tongues 6 , 7 are not pushed onto the corresponding contact surfaces of the other part in the same plane, a uniform, unimpaired thickness of the adhesive layer is obtained.
Die in Fig. 2 dargestellte Versatzmöglichkeit der Zungen 6, 7 ist insbesondere dann erforderlich, wenn flächige Teile, insbesondere Platten, mit nicht unerheblicher Dicke miteinander verklebt werden sollen. Die in Fig. 2 dargestellte Ausgestaltung mit dem Doppelknick ist besonders dann von Vorteil, wenn die Drehung der beiden Teile zueinander aus Montagegründen keine Nachteile mit sich bringt. Ist hingegen die Drehung der beiden Teile von Nachteil, so kann die in Fig. 4 dargestellte Ausgestaltung der Zungen 6 und 7 mit einer kammartigen Struktur erfolgen; hierbei sind dann Schlitze 8, 9 in den Endbereichen der beiden Teile vorgesehen; Fig. 5 zeigt, daß auch hier ein Versatz 12, 12′ zwischen den einzelnen Zungen durch einen Doppelknick entsteht, so daß die beiden miteinander zu verbindenden Teile im wesentlichen in der gleichen Ebene angeordnet bleiben, während die Zungen jeweils eines Endbereiches eines der Teile abwechselnd nach oben bzw. nach unten abgeknickt sind, so daß der in Fig. 5 dargestellte Versatz 12, 12′ entsteht.The possibility of offset of the tongues 6 , 7 shown in FIG. 2 is particularly necessary when flat parts, in particular plates, of considerable thickness are to be glued together. The embodiment shown in FIG. 2 with the double bend is particularly advantageous if the rotation of the two parts relative to one another does not have any disadvantages for reasons of assembly. If, on the other hand, the rotation of the two parts is disadvantageous, the configuration of the tongues 6 and 7 shown in FIG. 4 can take place with a comb-like structure; slots 8 , 9 are then provided in the end regions of the two parts; Fig. 5 shows that here too, an offset 12 , 12 'between the individual tongues is created by a double bend, so that the two parts to be connected to one another remain essentially in the same plane, while the tongues of one end region of one of the parts alternately are bent upwards or downwards, so that the offset 12 , 12 'shown in Fig. 5 is formed.
Fig. 6 und 7 zeigen nun das Verkleben zweier Sandwich- Strukturen mit erheblicher Dicke, so daß Stirnseiten entstehen, die sich senkrecht zu den ausgebildeten Zungen 6, 7 erstrecken. Derartige Sandwich-Strukturen weisen üblicherweise einen Schaum- oder Honigwabenkern 18 auf, der allseitig oder auf Oberseite und Unterseite von Deckhäuten 14 bedeckt ist. Gemäß dem in Fig. 6 dargestellten Ausführungsbeispiel werden zwischen zwei benachbarten Zungen 6 der ersten Sandwich-Struktur 1 beim Ausschneiden der Zungen verbliebene Stege 13 der Deckhaut derart abgeklappt, daß sie die entsprechenden Bereiche des Schaum- oder Honigwabenkerns 18 bedecken, wobei sie mit diesem Kern verklebt werden. Zum Verkleben der Teile 1 und 2 werden diese Deckhautstege zusätzlich zu den Zungen 6, 7 bzw. deren Seitenwänden mit einer Klebstoffschicht 17 benetzt, die für eine weitere Verbindung zwischen den beiden Teilen 1 und 2 sorgt. Eine derartige Verklebung der beiden Teile 1 und 2 miteinander führt zu einem besonders guten Formschluß der beiden Teilen wobei durch die große Klebefläche weiche und zähe Kleber verwendet werden können. Damit kann auch das Auseinanderreißen durch Sprödbruch der Klebestelle bei einer eventuellen Crashbelastung vermindert werden. FIGS. 6 and 7 now the bonding two sandwich show structures with considerable thickness so that end faces are formed which extend perpendicular to the formed tongues 6, 7. Such sandwich structures usually have a foam or honeycomb core 18 , which is covered on all sides or on the top and bottom of cover skins 14 . According to the exemplary embodiment shown in FIG. 6, webs 13 of the cover skin remaining when two tongues 6 of the first sandwich structure 1 are cut out are folded down in such a way that they cover the corresponding areas of the foam or honeycomb core 18 , with this core be glued. To glue parts 1 and 2 , these cover skin webs are additionally wetted with tongues 6 , 7 or their side walls with an adhesive layer 17 , which ensures a further connection between the two parts 1 and 2 . Such an adhesive bonding of the two parts 1 and 2 to one another leads to a particularly good interlocking of the two parts, whereby soft and tough adhesive can be used due to the large adhesive surface. This can also reduce tearing apart due to brittle fracture of the adhesive point in the event of a possible crash load.
Mit 16 und 7′ sind in Fig. 7 die mit Klebstoff benetzten Kontaktflächen des Strukturteils 2 bezeichnet, auf denen nach der Vereinigung die zugehörigen Flächen des Teils 1 zu liegen kommen.With 16 and 7 'in Fig. 7, the contact surfaces of the structural part 2 wetted with adhesive are referred to, on which the associated surfaces of part 1 come to lie after the union.
Das erfindungsgemäße Verfahren eignet sich vorzüglich zur Verbindung ebener oder flächiger Teile, insbesondere Platten oder Sandwich-Strukturen aus Faserverbundwerkstoff, wie sie in zunehmendem Maße in der Verkehrstechnik eingesetzt werden.The method according to the invention is particularly suitable for Connection of flat or flat parts, in particular Panels or sandwich structures made of fiber composite material, as they are increasingly used in traffic engineering be used.
Claims (4)
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19607061A DE19607061C1 (en) | 1996-02-24 | 1996-02-24 | Adhesive bonding of fibre compound board materials |
| GB9921500A GB2340066B (en) | 1996-02-24 | 1997-02-06 | Method of achieving a glued connection of planar or sheet parts |
| GB9921499A GB2340065B (en) | 1996-02-24 | 1997-02-06 | Method of achieving a glued connection of planar or sheet parts |
| GB9702399A GB2310396B (en) | 1996-02-24 | 1997-02-06 | Method of achieving a glued connection of planar or sheet parts |
| IT97MI000343A IT1290350B1 (en) | 1996-02-24 | 1997-02-18 | PROCEDURE FOR THE IMPLEMENTATION OF A JOINT GLUED BETWEEN FLAT OR SURFACE DEVELOPMENT ELEMENTS |
| FR9702000A FR2745295B1 (en) | 1996-02-24 | 1997-02-20 | PROCESS FOR THE PRODUCTION OF A GLUE ASSEMBLY BETWEEN PLANAR OR FLAT PARTS |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19607061A DE19607061C1 (en) | 1996-02-24 | 1996-02-24 | Adhesive bonding of fibre compound board materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE19607061C1 true DE19607061C1 (en) | 1997-05-15 |
Family
ID=7786393
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19607061A Expired - Fee Related DE19607061C1 (en) | 1996-02-24 | 1996-02-24 | Adhesive bonding of fibre compound board materials |
Country Status (4)
| Country | Link |
|---|---|
| DE (1) | DE19607061C1 (en) |
| FR (1) | FR2745295B1 (en) |
| GB (1) | GB2310396B (en) |
| IT (1) | IT1290350B1 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001059311A1 (en) * | 2000-02-09 | 2001-08-16 | Claus Reissig | Method for joining multi-layered sheets |
| EP1182243A1 (en) * | 2000-08-23 | 2002-02-27 | Honda Giken Kogyo Kabushiki Kaisha | Method for bonding non-magnetic members |
| DE102004056071B4 (en) * | 2004-11-15 | 2009-12-10 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | composite structure |
| EP2474409A1 (en) * | 2011-01-07 | 2012-07-11 | F&G Engineering GmbH | Connection between a basis component and a fibre reinforced multilayered composite component |
| EP1752667A3 (en) * | 2005-08-08 | 2013-12-18 | Behr GmbH & Co. KG | Process and tool to form structural components, particularly plastic structural components |
| US20140352876A1 (en) * | 2010-11-19 | 2014-12-04 | The Boeing Company | Method for making and joining composite sandwich shell edge joint |
| US9574592B2 (en) | 2010-11-19 | 2017-02-21 | The Boeing Company | Composite sandwich shell edge joint |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB9917446D0 (en) * | 1999-07-23 | 1999-09-29 | Flude Rodger E | Edge joint |
| EP3356611A4 (en) * | 2015-10-02 | 2019-06-26 | Modvion AB | COMPOSITE SECTION OF FIBERS AND ASSEMBLY |
| CN109109328B (en) * | 2018-10-23 | 2020-09-25 | 哈尔滨工程大学 | Adhesive connection structure of composite sandwich panel with no protrusion on surface and preparation method thereof |
| CN111911505A (en) * | 2020-08-11 | 2020-11-10 | 周玉珍 | Oblique angle butt joint traceless connecting device for wood blocks |
| CN113638949B (en) * | 2021-07-30 | 2025-07-04 | 江苏立导科技有限公司 | Laminating device |
| CN114483742B (en) * | 2022-04-15 | 2022-07-12 | 北京玻钢院复合材料有限公司 | Bonding and curing device for test piece reinforcing sheet made of composite material and using method |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0664326A2 (en) * | 1993-12-18 | 1995-07-26 | Leander Dr. Bathon | System for assembling wooden materials and materials of any kind using adhesives |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE459557A (en) * | 1941-06-18 | 1900-01-01 | ||
| GB620248A (en) * | 1947-01-11 | 1949-03-22 | Hills & Sons Ltd F | Improvements in or relating to glued joints for timber |
| US3895148A (en) * | 1973-10-12 | 1975-07-15 | Chang Ching Yu | Panel edge configuration |
| FR2557932B1 (en) * | 1984-01-10 | 1987-04-30 | Carrez Pierre | METHOD FOR JOINING TWO SANDWICH PANELS WITH A HONEYCOMB CORE AND COMPOSITE PANEL OBTAINED BY THIS PROCESS |
| SE8505003L (en) * | 1985-10-23 | 1987-04-24 | Folksam Auto Ab | Overlapping glued joint |
| DE3737210A1 (en) * | 1987-11-03 | 1989-05-24 | Opel Adam Ag | Method of connecting body parts of a vehicle body |
| GB8817632D0 (en) * | 1988-07-23 | 1988-09-01 | Hunting Eng Ltd | Quick release joint |
-
1996
- 1996-02-24 DE DE19607061A patent/DE19607061C1/en not_active Expired - Fee Related
-
1997
- 1997-02-06 GB GB9702399A patent/GB2310396B/en not_active Expired - Fee Related
- 1997-02-18 IT IT97MI000343A patent/IT1290350B1/en active IP Right Grant
- 1997-02-20 FR FR9702000A patent/FR2745295B1/en not_active Expired - Fee Related
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0664326A2 (en) * | 1993-12-18 | 1995-07-26 | Leander Dr. Bathon | System for assembling wooden materials and materials of any kind using adhesives |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001059311A1 (en) * | 2000-02-09 | 2001-08-16 | Claus Reissig | Method for joining multi-layered sheets |
| EP1182243A1 (en) * | 2000-08-23 | 2002-02-27 | Honda Giken Kogyo Kabushiki Kaisha | Method for bonding non-magnetic members |
| US6986827B2 (en) | 2000-08-23 | 2006-01-17 | Honda Giken Kogyo Kabushiki Kaisha | Method for bonding non-magnetic members |
| DE102004056071B4 (en) * | 2004-11-15 | 2009-12-10 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | composite structure |
| EP1752667A3 (en) * | 2005-08-08 | 2013-12-18 | Behr GmbH & Co. KG | Process and tool to form structural components, particularly plastic structural components |
| US20140352876A1 (en) * | 2010-11-19 | 2014-12-04 | The Boeing Company | Method for making and joining composite sandwich shell edge joint |
| US9505204B2 (en) * | 2010-11-19 | 2016-11-29 | The Boeing Company | Method for making and joining composite sandwich shell edge joint |
| US9574592B2 (en) | 2010-11-19 | 2017-02-21 | The Boeing Company | Composite sandwich shell edge joint |
| EP2474409A1 (en) * | 2011-01-07 | 2012-07-11 | F&G Engineering GmbH | Connection between a basis component and a fibre reinforced multilayered composite component |
| EP2474409B1 (en) * | 2011-01-07 | 2014-03-26 | F&G Engineering GmbH | Connection between a basis component and a fibre reinforced multilayered composite component |
Also Published As
| Publication number | Publication date |
|---|---|
| ITMI970343A1 (en) | 1998-08-18 |
| FR2745295A1 (en) | 1997-08-29 |
| GB2310396B (en) | 2000-06-28 |
| GB9702399D0 (en) | 1997-03-26 |
| FR2745295B1 (en) | 1999-01-22 |
| IT1290350B1 (en) | 1998-10-22 |
| GB2310396A (en) | 1997-08-27 |
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Legal Events
| Date | Code | Title | Description |
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| 8100 | Publication of the examined application without publication of unexamined application | ||
| D1 | Grant (no unexamined application published) patent law 81 | ||
| 8364 | No opposition during term of opposition | ||
| 8320 | Willingness to grant licences declared (paragraph 23) | ||
| 8327 | Change in the person/name/address of the patent owner |
Owner name: EUROCOPTER DEUTSCHLAND GMBH, 86609 DONAUWOERTH, DE |
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| R119 | Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee |
Effective date: 20110901 |