DE102005006937A1 - Arrangement for temporary joining of two parts made of same or different material, comprising elastic central layer held by spike elements - Google Patents
Arrangement for temporary joining of two parts made of same or different material, comprising elastic central layer held by spike elements Download PDFInfo
- Publication number
- DE102005006937A1 DE102005006937A1 DE102005006937A DE102005006937A DE102005006937A1 DE 102005006937 A1 DE102005006937 A1 DE 102005006937A1 DE 102005006937 A DE102005006937 A DE 102005006937A DE 102005006937 A DE102005006937 A DE 102005006937A DE 102005006937 A1 DE102005006937 A1 DE 102005006937A1
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- Prior art keywords
- components
- layer
- connection according
- joining connection
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Classifications
-
- 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
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
-
- 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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/76—Making non-permanent or releasable 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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/78—Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus
- B29C65/7855—Provisory fixing
-
- 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
- B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
- B29C66/3034—Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes
- B29C66/30341—Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes non-integral with the parts to be joined, e.g. making use of extra elements
-
- 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
-
- 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
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/08—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of welds or the like
-
- 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
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap 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
- B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
- B29C66/3032—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined
- B29C66/30321—Particular design of joint configurations the joint involving an anchoring effect making use of protrusions or cavities belonging to at least one of the parts to be joined making use of protrusions belonging to at least one of the parts to be joined
-
- 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
- B29C66/71—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 composition of the plastics material of the parts to be joined
- B29C66/712—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 composition of the plastics material of the parts to be joined the composition of one of the parts to be joined being different from the composition of the other part
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)
Abstract
Description
Die Erfindung betrifft eine Fügeverbindung zum Fixieren und/oder Verbinden von Bauteilen. Derartige Fügeverbindung finden beispielsweise beim Zusammenbau von Fahrzeugkarosserien Anwendung, insbesondere dann, wenn Bauteile aus Stahl- und/oder Leichtmetallblech und/oder anderen Materialien vor einer endgültigen und dauerhaften Befestigung zueinander fixiert und in dieser Fixierung gehalten werden müssen.The The invention relates to a joint connection to Fixing and / or connecting components. Such joint connection are used, for example, in the assembly of vehicle bodies, especially if components made of steel and / or light metal sheet and / or other materials prior to final and permanent attachment fixed to each other and must be kept in this fixation.
Während in
der Kraftfahrzeugtechnik bei der Stahlblechbauweise überwiegend
Punktschweißverfahren
und vereinzelt auch Lötverfahren
zum Verbinden der einzelnen Bauteile aus Blech Verwendung finden,
dominieren im Flugzeugbau Nietverbindungen zwischen den Bauteilen.
In anderen Bereichen der Technik und in den letzten Jahren verstärkt auch im
Flugzeug- und Fahrzeugbau, werden zunehmend auch Klebeverfahren
eingesetzt, vor allem bei Bauteilen aus Nichteisenmetallen und Kunststoffen
oder Verbundwerkstoffen. Außerdem
finden verstärkt Werkstoffkombinationen
Verwendung, bei denen traditionell eingesetzte Werkstoffe wie Stahl
gezielt durch andere Werkstoffe ersetzt werden. Dadurch müssen Bauteile
unterschiedlicher Werkstoffe miteinander verbunden werden. Aus der
Fügeverbindungen
werden außerdem
häufig mehrstufig
ausgeführt,
da die Bauteile in vielen Anwendungsfällen in festen Arbeitsfolgen
zusammengesetzt werden müssen
und erst in späteren
Arbeitsfolgen fest miteinander verbunden werden können. Dazu
ist es bekannt, die Bauteile mittels Haltevorrichtungen, wie beispielsweise
in der
Eine
weitere Möglichkeit
zur Fixierung und Verbindung von Bauteilen, insbesondere von Profilbauteilen
ist beispielsweise in den Patentschriften
Weitere Möglichkeiten bieten das Falzen oder Klemmen der Ränder oder angebrachter Laschen der zu verbindenden Bauteile, um sie vor einer endgültigen Verbindung zueinander zu fixieren. Bei sichtbaren Verbindungsstellen sind der Anwendung derartiger Verbindungstechniken jedoch Grenzen gesetzt.Further options offer folding or clamping of the edges or attached tabs the components to be connected to them before a final connection to fix each other. For visible joints are the However, application of such connection techniques limits.
Aufgabe der Erfindung ist es, eine Fügetechnik für innovative Konstruktions- und Fertigungstechniken mit unterschiedlichsten Anwendungen zur Verfügung zu stellen, die flexible Möglichkeiten des Zusammenbaus von Bauteilen aus gleichen und unterschiedlichen Werkstoffen zu flächenförmigen oder räumlichen Gebilden ermöglicht.task The invention is a joining technique for innovative Design and manufacturing techniques with a wide variety of applications to disposal to provide the flexible options the assembly of components from the same and different Materials to surface or spatial Made possible.
Die Lösung der Aufgabe gelingt mit einer Fügeverbindung gemäß Anspruch 1 und gemäß Anspruch 9. Weitere vorteilhafte Ausgestaltungen sind in den abhängigen Ansprüchen ausgeführt.The solution the task succeeds with a joint connection according to claim 1 and according to claim 9. Further advantageous embodiments are set forth in the dependent claims.
Eine erste erfindungsgemäße Fügeverbindung zum Fixieren und/oder Verbinden von Bauteilen, bei welcher die Bauteile mittels zwischen den Bauteilen befindlichen Zusatzelementen miteinander verbunden sind, umfasst ein erstes Zusatzelement, welches aus einer Schicht aus einer deformierbaren, hochviskosen Masse besteht, und aus einem oder mehreren an zumindest einem der Bauteile befindlichen zweiten Zusatzelementen, welche Eindringkörper sind und in der Schicht verankert sind.A first joint connection according to the invention for fixing and / or connecting components, in which the components connected by means of additional components located between the components , comprises a first additional element, which consists of a layer consists of a deformable, highly viscous mass, and of one or more located on at least one of the components second Additional elements which are indenters and in the layer are anchored.
Unter deformierbaren, hochviskosen Massen werden im Sinne dieser Erfindung Stoffe verstanden, die zäh- bis weichplastische Eigenschaften aufweisen, insbesondere Stoffe, welche eine Viskosität von mehr als 1000 mPa bei 20° C aufweisen. Die deformierbare, hochviskose Masse ist vorzugsweise nicht aushärtend, sondern dauerplastisch, damit die Fügeverbindung ohne Werkzeuge demontierbar bleibt., wobei diese Stoffe vorzugsweise beständig gegen Kälte bis –40 °C und Wärme bis 80 °C, kuzfristig auch gegen höhere Temperaturen, sind.Under deformable, highly viscous masses are within the meaning of this invention Substances understood to be tough have soft plastic properties, in particular substances, which has a viscosity of more than 1000 mPa at 20 ° C exhibit. The deformable, highly viscous mass is preferably not curing, but permanently plastic, so that the joint connection without tools remains removable., These substances preferably resistant to Cold to -40 ° C and heat up 80 ° C, in the short term also against higher ones Temperatures are.
In einer vorteilhaften Ausführung der ersten erfindungsgemäßen Fügeverbindung weist jedes der Bauteile zumindest einen, vorzugsweise mehrere Eindringkörper auf, diese sind in der zwischen den Bauteilen befindlichen Schicht vorzugsweise formschlüssig verankert und ermöglichen so zumindest eine Fixierung der Bauteile zueinander.In an advantageous embodiment of the first According to the invention, each of the components has at least one, preferably a plurality of indenters, these are preferably positively anchored in the layer located between the components and thus enable at least one fixation of the components to one another.
In einer alternativen vorteilhaften Ausführung der ersten erfindungsgemäßen Fügeverbindung ist die Schicht mit einem Bauteil haftend verbunden und das oder die mit diesem Bauteil fixierten und/oder verbundenen weiteren Bauteile weisen jeweils einen oder mehrere Eindringkörper auf, die in der Schicht vorzugsweise formschlüssig verankert sind. Weitere Varianten, bei denen beispielsweise eine Fügeverbindung zwischen mehreren Bauteilen mit einer haftenden Schicht und nur einem oder mehreren Bauteilen mit Eindringkörper bzw. Eindringkörpern besteht, sind ebenso eingeschlossen.In an alternative advantageous embodiment of the first joint connection according to the invention the layer is adhesively bonded to a component and the or the fixed with this component and / or other connected components each have one or more indenters, preferably in the layer form-fitting are anchored. Other variants in which, for example, a Retaining compound between several components with an adhesive layer and only one or more components with indenters or indenters consists, are also included.
Die auf dem Bauteil haftende Schicht ist vorzugsweise aufgeklebt, insbesondere ist die Schicht als einseitig selbstklebende Schicht ausgeführt, welche mit dem Bauteil klebend verbunden wurde oder mittels Oberflächenhaftung mit dem Bauteil verbunden und dadurch auf dem Bauteil fixiert ist.The adhered to the component layer is preferably adhered, in particular the layer is designed as a one-sided self-adhesive layer, which was adhesively bonded to the component or by surface adhesion connected to the component and thereby fixed on the component.
Die Eindringkörper sind vorzugsweise mittels einer Trägerplatte oder eines Trägerbandes auf dem Bauteil befestigt oder unmittelbar aus dem Bauteil herausgeformt.The indenter are preferably by means of a carrier plate or a carrier tape mounted on the component or molded directly out of the component.
Eine weitere erfindungsgemäße Fügeverbindung zum Fixieren und/oder Verbinden von Bauteilen, bei welcher die Bauteile mittels zwischen den Bauteilen befindlichen Zusatzelementen miteinander verbunden sind umfasst ein auf jedem Bauteil befindliches erstes Zusatzelement, welches jeweils eine Schicht aus einer deformierbaren, hochviskosen Masse ist und haftend auf jedem Bauteil aufgebracht ist, und jeweils zumindest ein zwischen den Schichten befindliches zweites Zusatzelement, welches eine Trägerplatte oder ein Trägerband mit beidseitig angeordneten Eindringkörpern ist, wobei die Eindringkörper in den Schichten verankert sind.A further joining compound according to the invention for fixing and / or connecting components, in which the components connected by means of additional components located between the components comprise a first additional element located on each component, which in each case a layer of a deformable, highly viscous mass is and is adhered to each component, and in each case at least a second additional element located between the layers, which is a support plate or a carrier tape with indenters arranged on both sides, wherein the indenters in anchored to the layers.
Die auf den Bauteilen haftenden Schichten der weiteren erfindungsgemäßen Fügeverbindung sind vorzugsweise aufgeklebt, insbesondere sind die Schichten als einseitig selbstklebende Schichten ausgeführt, welche mit den Bauteilen klebend verbunden wurden oder mittels Oberflächenhaftung mit den Bauteilen verbunden und dadurch auf den Bauteilen fixiert sind.The On the components adhering layers of the further joint connection according to the invention are preferably glued, in particular, the layers are as one-sided self-adhesive layers executed, which were adhesively bonded to the components or by surface adhesion connected to the components and thereby fixed on the components are.
In vorteilhaften Ausführungen der beiden erfindungsgemäßen Fügeverbindungen sind die Schichten als elastische Schichten oder als viskoelastische Schichten ausgeführt und bestehen vorzugsweise aus einer Butylverbindung, insbesondere aus einer volumenbeständigen, selbstklebenden Butylkautschukmasse.In advantageous embodiments the two joining compounds according to the invention are the layers as elastic layers or as viscoelastic Layers executed and preferably consist of a butyl compound, in particular of a volume-resistant, self-adhesive butyl rubber compound.
Die Eindringkörper sind vorzugsweise dornenförmig ausgeführt, insbesondere, wenn die Schicht elastisch ist oder sie sind haken- oder ankerförmig ausgeführt, insbesondere dann, wenn die Schicht viskoelastisch ist.The indenter are preferably thorn-shaped executed especially if the layer is elastic or they are hooked or anchor-shaped executed especially when the layer is viscoelastic.
Mit der erfindungsgemäßen Fügeverbindung kann der Abstand und die Lage der gefügten Bauteile zueinander so lange fixiert werden, bis die konstruktiv vorgesehene Verbindungsart erzeugt wird. Die Kräfte zum Fügen bzw. Verbinden der Bauteile werden vorzugsweise über die Bauteile selbst ausgeübt. Die Eindringkörper gehen mit der deformierbaren, hochviskosen Schicht keine feste, unlösbare Verbindung im Sinne einer chemischen Bindung ein, die Haltekräfte beruhen überwiegend auf physikalisch wirkenden Kräften wie der Oberflächenenergie und der Verkrallung bzw. des Formschlusses der Eindringkörper in der Schicht. Die Verbindung zwischen den Eindringkörpern und der Schicht kann durch die Wahl des Schichtmaterials zwischen elastisch und viskoelastisch auf die folgenden Beanspruchungen im Fertigungsablauf flexibel reagieren. Ist die Schicht elastisch gewählt, wird die einmal erzeugte Verbindung stabil gehalten. Die Schicht kann aber auch viskoelastisch ausgeführt sein und bei steigender Beanspruchung plastisch deformierbar sein. Damit können unerwünschte Verspannungen in fest gefügten Strukturen und Maßtoleranzen zwischen den Bauteilen ausgeglichen werden.With the joining compound according to the invention can the distance and the location of the joined Components are fixed to each other so long until the constructively provided Connection type is generated. The forces for joining or connecting the components are preferably over the components themselves exercised. The indenters go with the deformable, highly viscous layer no solid, unsolvable Connection in the sense of a chemical bond, the holding forces are based predominantly on physically acting forces like the surface energy and the claw or the positive connection of the indenter in the layer. The connection between the indenters and The layer can be elastic by choosing the layer material between and viscoelastic to the following stresses in the production process react flexibly. Is the layer selected elastically, is the connection once created kept stable. The layer can but also viscoelastic be and be plastically deformable with increasing stress. With that you can undesirable Tension in tight structures and dimensional tolerances be balanced between the components.
Die erfindungsgemäße Fügeverbindung bietet die Möglichkeit, Bauteile aus gleichen und unterschiedlichen Werkstoffen, insbesondere aus Stahlwerkstoffen, Leichtmetallstoffen und/oder Kunststoffen flexibel zueinander zu fixieren und zu verbinden.The inventive joint connection offers the possibility, Components made of the same and different materials, in particular made of steel materials, light metal materials and / or plastics flexible to fix each other and connect.
Die Erfindung wird im Weiteren an Hand von Ausführungsbeispielen näher erläutert.The The invention will be explained in more detail with reference to exemplary embodiments.
Die
Die
in
Bei
der in
- 11
- erstes Bauteilfirst component
- 22
- zweites Bauteilsecond component
- 33
- drittes Bauteilthird component
- 44
- verformbare, hochviskose Schichtdeformable, high viscosity layer
- 55
- verformbare hochviskose Schichtdeformable high viscosity layer
- 66
- Eindringkörperindenter
- 77
- Trägerplattesupport plate
- 88th
- Trägerband mit Eindringkörperncarrier tape with indenters
Claims (18)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102005006937A DE102005006937A1 (en) | 2005-02-16 | 2005-02-16 | Arrangement for temporary joining of two parts made of same or different material, comprising elastic central layer held by spike elements |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102005006937A DE102005006937A1 (en) | 2005-02-16 | 2005-02-16 | Arrangement for temporary joining of two parts made of same or different material, comprising elastic central layer held by spike elements |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE102005006937A1 true DE102005006937A1 (en) | 2006-08-24 |
Family
ID=36776096
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE102005006937A Withdrawn DE102005006937A1 (en) | 2005-02-16 | 2005-02-16 | Arrangement for temporary joining of two parts made of same or different material, comprising elastic central layer held by spike elements |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE102005006937A1 (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2450239A1 (en) * | 2010-11-04 | 2012-05-09 | Inalfa Roof Systems Group B.V. | Method for connecting two objects and panel using said method |
| EP2778440A1 (en) * | 2013-03-14 | 2014-09-17 | Stone Age Equipment Inc. | Releasable connection system |
| DE102015100263B3 (en) * | 2015-01-09 | 2016-03-31 | Audi Ag | Structural component for a body of a passenger car |
| DE102015207604A1 (en) * | 2015-04-24 | 2016-10-27 | Volkswagen Aktiengesellschaft | Method for connecting two components |
| EP2684789A3 (en) * | 2012-07-11 | 2017-07-05 | Stone Age Equipment Inc. | Releasable Connection System |
| DE102016206296A1 (en) * | 2016-04-14 | 2017-10-19 | Airbus Operations Gmbh | Connection system, connection arrangement and method |
| EP3584294A1 (en) * | 2018-06-19 | 2019-12-25 | 3M Innovative Properties Company | Frictional connection of components and process for making a frictional connection |
| EP3584296A1 (en) * | 2018-06-19 | 2019-12-25 | 3M Innovative Properties Company | Connecting element for the friction-increasing connection of components, process for making a connecting element and use of a connecting element |
| CN110978536A (en) * | 2019-10-29 | 2020-04-10 | 莆田市子都贸易有限公司 | Plastic part heat pressure maintaining equipment |
| EP4197753A1 (en) * | 2021-12-15 | 2023-06-21 | BAE SYSTEMS plc | Hybrid joint |
| WO2023111521A1 (en) * | 2021-12-15 | 2023-06-22 | Bae Systems Plc | Hybrid joint |
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Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2450239A1 (en) * | 2010-11-04 | 2012-05-09 | Inalfa Roof Systems Group B.V. | Method for connecting two objects and panel using said method |
| CN102536980A (en) * | 2010-11-04 | 2012-07-04 | 银娜珐天窗系统集团股份有限公司 | Method for connecting two objects and panel using said method |
| US8864219B2 (en) | 2010-11-04 | 2014-10-21 | Inalfa Roof Systems Group B.V. | Method for connecting two objects and panel using said method |
| CN102536980B (en) * | 2010-11-04 | 2016-02-17 | 英纳法天窗系统集团有限公司 | For connecting the method for two articles and using the lath of described method |
| EP2684789A3 (en) * | 2012-07-11 | 2017-07-05 | Stone Age Equipment Inc. | Releasable Connection System |
| EP2778440A1 (en) * | 2013-03-14 | 2014-09-17 | Stone Age Equipment Inc. | Releasable connection system |
| DE102015100263B3 (en) * | 2015-01-09 | 2016-03-31 | Audi Ag | Structural component for a body of a passenger car |
| US9669880B2 (en) | 2015-01-09 | 2017-06-06 | Audi Ag | Structural component for a body of a passenger car |
| DE102015207604A1 (en) * | 2015-04-24 | 2016-10-27 | Volkswagen Aktiengesellschaft | Method for connecting two components |
| US10343344B2 (en) | 2016-04-14 | 2019-07-09 | Airbus Operations Gmbh | Connection system, connection arrangement and method |
| DE102016206296A1 (en) * | 2016-04-14 | 2017-10-19 | Airbus Operations Gmbh | Connection system, connection arrangement and method |
| DE102016206296B4 (en) * | 2016-04-14 | 2024-05-02 | Airbus Operations Gmbh | Connection system, connection arrangement and method |
| EP3584294A1 (en) * | 2018-06-19 | 2019-12-25 | 3M Innovative Properties Company | Frictional connection of components and process for making a frictional connection |
| EP3584296A1 (en) * | 2018-06-19 | 2019-12-25 | 3M Innovative Properties Company | Connecting element for the friction-increasing connection of components, process for making a connecting element and use of a connecting element |
| WO2019244048A1 (en) * | 2018-06-19 | 2019-12-26 | 3M Innovative Properties Company | Frictional connection of components and process for making a frictional connection |
| US11820925B2 (en) | 2018-06-19 | 2023-11-21 | 3M Innovative Properties Company | Frictional connection of components and process for making a frictional connection |
| CN110978536A (en) * | 2019-10-29 | 2020-04-10 | 莆田市子都贸易有限公司 | Plastic part heat pressure maintaining equipment |
| CN110978536B (en) * | 2019-10-29 | 2021-12-17 | 泰兴市康威塑业有限公司 | Plastic part heat pressure maintaining equipment |
| EP4197753A1 (en) * | 2021-12-15 | 2023-06-21 | BAE SYSTEMS plc | Hybrid joint |
| WO2023111521A1 (en) * | 2021-12-15 | 2023-06-22 | Bae Systems Plc | Hybrid joint |
| JP2024546922A (en) * | 2021-12-15 | 2024-12-26 | ビ-エイイ- システムズ パブリック リミテッド カンパニ- | Hybrid Joints |
| JP7676670B2 (en) | 2021-12-15 | 2025-05-14 | ビ-エイイ- システムズ パブリック リミテッド カンパニ- | Hybrid Joints |
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| Date | Code | Title | Description |
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| OM8 | Search report available as to paragraph 43 lit. 1 sentence 1 patent law | ||
| R005 | Application deemed withdrawn due to failure to request examination |
Effective date: 20120217 |