The invention concerns a building element consisting of several individual layers and designed as a honeycomb construction with partial hollow bodies protruding over the basic construction, whereby surfaces of adjoining individual layers together form a wall of a small wall thickness.
Such elements are known from DE 100 22 742 A1. In order to bring the different layers together to form a building element, they must be connected. The starting point of any layer having a hollow body is a thin film or membrane, from which such a wall is then created. After any layer is deformed, the surfaces of the hollow body arrangements and their edges result. At the point when two layers are put together, the edge of the hollow body arrangement shows a stable behaviour. On the other hand it has proven problematic that the surfaces of the hollow body arrangement can turn out to be unstable; they are more or less borne by the edges.
The present invention therefore sets itself the task of creating a particularly homogeneous building element consisting of several individual layers and designed as a honeycomb construction.
This task is performed through surfaces of the individual layers having a pre-stressing for improving the connection with adjoining surfaces.
The goal of such a honeycomb arrangement is to create a static/dynamic honeycomb construction, in which materials such as plastics, metals or fibrous composites are interconnected in as stable and lastingly a manner as possible. Here, a number—geared to claim and purpose—of individual surfaces of the individual layers are specifically placed under pre-stressing in order to obtain a connection of the otherwise unstable surfaces.
One embodiment of the invention intends for the pre-stressing to be applied through the way in which surfaces of the individual layers are designed. In other words, according to this first alternative, the pre-stressing is created to a certain extent from the design of the surfaces, whether through their geometry, or through a design different from a smooth-walled profile.
According to a proposal for the geometry of the surfaces, the consideration is to apply the pre-stressing in the form of a convex deformation pointing inwards or outwards. In the surfaces of the hollow body arrangements, the necessary energy connection zones are formed within a welded connection for the purpose of stabilisation and pre-stressing. These energy connection zones are recesses or bulges of the hollow body surfaces as appropriate, which transport the energy flow of the customised welding method accurately into the zones of fusion. Apart from the pre-stressing for stabilising the surfaces for a welding connection, the deformations also assume the task of carrying energy thanks to targeted welded connection zones with the purpose of making precise sub-sections of the surfaces connectable. This solution is particularly helpful for purposes where large welding gaps have to be bridged.
Alternatively or as an addition to this deformation of the surfaces, it is possible for surfaces of the individual layers to be designed as profiled. Built-in components or raisings with a pimple or fine stick structure are what are in mind here. Here, the surfaces also receive the pre-stressing via the convex deformations if necessary. The carrying of energy and the welding connection zone however are executed via the pimple or fine stick structure until joining finally takes place. These built-in components or raisings can be designed to be chaotic or orderly. A preferred application is in the case of small surfaces and the bridging of small joining gaps.
A particularly suitable profiling can be recognised in the case of surfaces having a lamella-like structure. With this design, an average joining gap is bridged and a targeted carrying of energy effected to the lamellas via the energy edge. The surface structures given here form a targeted welding connection zone. The number, shaping and arrangement of such lamellas are dependent on the surfaces (their size in particular) as well as on the joining gap, on the zones to be joined and on the energy flow of the welding method employed. The lamellas perform the task of targeted energy carrying right up to the fusion of the tops of the surfaces, where they act as a compensation for the joining gap. They are preferably used when bridging medium-sized joining gaps.
In addition to the proposal of generating the pre-stress from the surface of the individual layer, it is intended for the pre-stress to be applied through a connecting medium introduced between adjoining surfaces of the individual layers. If the pre-stressing of the surfaces is effected by means of an appropriate connecting medium, the unstable surfaces become stressed and the energy flows via this medium. While the zones of fusion of the medium merge, the pre-stressed surfaces relax and connect up in the zones of fusion with the surfaces of the hollow body contour arrangements.
If different materials are interconnected, so-called bonding bridges or bonding supplements are required. Within the intended connections, these agents are prepared for the more difficult surface to handle, and a preparation on both sides may also be necessary. The bonding bridges of the individual layers may be pre-reactive and expand under warmth or the influence of moisture for example.
It is also conceivable for the bonding bridge to be profiled or contribute to the profiling of the existing surfaces, for example in the form of a pimple or fine stick structure on the layers. In this case the bonding bridge pre-stresses the surfaces in order to ensure stability within the pressure exerted for joining. In this context, the bonding bridge causes the individual layers stacked one into the other to join via the hollow bodies or partial hollow bodies.
In order to form a particularly close connection between individual layers of the same or different material, one measure intends for a flowing net construct to serve as an externally applied connecting medium. Such connecting media are understood as a thin net which leaves behind an orderly rough surface. In its raisings, this rough surface determines the zones of fusion of the honeycomb arrangements to be connected. Such a net can in turn be profiled. This net is designed depending on the requisite energy to be introduced, which is necessary for fusing on the connecting medium in the welding zones.
In order to achieve a sound distribution of the connecting medium between the surfaces or on them, it is intended for a connection support introduced as liquid to serve as a connecting medium. After the connection has been established, the connecting medium should reach the planned solidity. It is important that the medium is either volatile and that, within the connection, the surfaces of the hollow body arrangement lying one on top of the other are caused to relax, or that the walls merge into one another completely, which leads to higher mass portions however. It is to be understood by an ideal chemical connection here that the surfaces are lying pre-stressed one on top of the other. The pre-stressing points can be stick-shaped or pimple-like bulges or convex or lamella-like deformations lying one on top of the other. It goes without saying that sufficient space must be remaining in order to accurately displace the chemical connecting medium by way of the joining pressure and to at the same time develop the intended connecting gap and thus a connection.
Pre-stressing surface structures can also be attached for the purpose of stabilisation. To this effect, it is recommended for a chemically reactive connection support to serve as a connecting medium.
A favourable case is when the chemically reactive connecting medium has expanding characteristics.
According to a further embodiment of the invention, it is planned for the connection of adjoining individual layers to essentially take place via their edges, their coupling element, their pyramid point and/or the supporting edges created. The surfaces do not have to receive a connection here, but the connection can essentially be realised via the interlocking of the individual layers and the associated hollow bodies and partial hollow bodies. It is even conceivable here to not bother applying the pre-stress.
In order to improve the interconnection quality of the surfaces of the individual layers, it is also practicable for the individual layers to be manufactured from a liquid-absorbing material.
A further measure plans for individual layers to have air pockets or for individual layers to have a surface equipped with small bubble-like air pockets. This contributes to increasing the pre-stressing of the surfaces in such a way that they withstand the joining pressure, in order to be able to interconnect the hollow bodies or partial hollow bodies.
The building element according to the invention offers a great number of further possible uses, including when individual layers are designed to be electrically conductive, either in their complete profile or at least in the area of their surface.
In this way the cells can be used as air conditioning cells, shock absorbers, insulators, separators, as ion carriers through the support of compounds or for comparable processes for the use of energy storage. The key advantage of the building element according to the invention is the favourable relationship between maximum surface and minimum space thanks to the nesting. If a battery case is assumed, the subsequent layers of the construction in the space can be extended at will. The connection of greatest possible contact surfaces offered by the entire building element is crucial here.
According to a further embodiment of the invention, it is planned for individual layers to be made of doughy or liquid moulding material and/or for adjoining individual layers to merge into a so-called wet-on-wet connection or dry-wet connection.
The stability of the building elements according to the invention can be increased considerably through at least the upper-edge-side individual layer and/or the lower-edge-side individual layer having a reinforcement. This can be formed for example by way of a V-shaped strip, and it is also conceivable for this reinforcement to be used as a contact strip for electrical connections. The reinforcement is inserted in the form of spacer strips for example, in order to ensure a greater, sandwich-like surface loading by the bending forces over the edge-side inserts.
The proposal for adjoining individual layers to be designed to be linkable with one another is along the same lines. The individual layers partly interlock in this case, and an immobilisation in the form of undercuts is also possible. On the one hand, an insulator can be represented using a levelling compound. On the other hand, this can offer the exact opposite. It is thus conceivable for the compound to be used as an ion transporter in a battery at the same time.
According to a further advantageous embodiment of the invention, it is planned for adjoining individual layers to be designed as insulated from one another. Through the separation of individual layers, cell or layer gaps are separately and individually controllable here, in order to ensure the above mentioned uses e.g. in the form of air conditioning cells, shock absorbers, insulators or separators. The connection of greatest possible contact surfaces offered by the entire building element is crucial here. The individual layers can be merged into different requisite materials and they can be insulated from one another outstandingly in doing so. In the surfaces of the individual layers, conductive fibres or other composites can be introduced, which are needed in the modern development of nanocells. The supply of oxygen and special requisite cells and the isolation from oxygen at an immediately adjoining space within such a cell is possible by way of this cell separation.
As regards the proposal mentioned, it is appropriate for a sealing ring and/or a sealing lip to serve as insulation. The hollow bodies can be held and insulated from one another via such an all-round sealing ring or an accordingly designed sealing lip.
In addition, the invention concerns a procedure for the production of a building element built up of several individual layers and in the form of a honeycomb construction with partial hollow bodies protruding over the basic construction, where surfaces of adjoining individual layers form a common wall of a small wall thickness and where surfaces of the individual layers are joined, under pre-stressing, with surfaces of adjoining individual layers.
This pre-stressing can on the one hand be generated from individual surfaces of the layers, through a perhaps convex deformation pointing inwards or outwards being applied to these. A profiling is also a suitable measure, e.g. by way of lamella-like structures or suitable built-in components and raisings on the surfaces. As an alternative or addition to these procedure steps, an external connecting medium can be introduced between adjoining surfaces of the individual layers, by which both a net construct and a chemical connecting medium inserted as a liquid, with expanding characteristics if necessary, are understood.
In other words, surfaces of the individual layers are placed under pre-stress through their arrangement and/or design, or surfaces of the individual layers are placed under pre-stress through a connecting medium.
A further measure intends for the individual layers to be sealed in the joining process via the edge-side individual layer and the lower-edge-side individual layer and for the honeycomb construction to be placed under a vacuum until the joining process is complete.
A particularly useful variant of the invention intends for the appropriate surfaces of adjoining individual layers to be interconnected by means of ultrasonic welding. Such a procedure makes a particularly precise, lasting and effective connection possible for the individual layers, and the energy expenditure is comparatively low.
In the course of ultrasonic welding, it is to be noted that very thin film layers are welded with one another. A welding energy source that is set too high would inevitably lead to welding burns, and too low a welding energy source setting would lead too incomplete welds. Depending upon the connection zone, constantly changing welding resistances are to be reckoned with, due in particular to the manufacturing tolerance compensation at the honeycombs of the invention in the form of convex surfaces or other surface pre-stressing. In such a case, each welding resistance where different connecting tolerances may develop should be calculated before the welding is made.
For this purpose, it is suggested that the resistances of the surfaces to be welded be measured before welding. In the context of this so-called primary measurement welding, the energy welding source adjusts to the determined value after measurement, in order to avoid welding burns or faulty connections of the individual surfaces. Thanks to the primary measurement welding, it is also taken into consideration in particular that different materials of different densities can be interconnected. Bonding or connecting bridges must ultimately be created, in which both materials connect. If different masses have different coefficients of expansion in addition, the materials must be interconnected in such a way that one of these materials always adapts to the movement of the other one, without it becoming fatigued or destroyed. In order to now perform large-scale welding, the interconnections are either calculated or the manufacturing or expansion tolerances that arise are taken into account before the continuous manufacturing process and these tolerances are transferred to the manufacturing process.
According to a further proposal, it is planned for a sonotrode to be applied to the surfaces of the individual layers before ultrasonic welding takes place. This sonotrode acts on the surfaces to be welded with a prescribed force. That is to say, an appropriate tool is brought into high-frequency mechanical oscillation, which is then transferred to the surfaces to be welded. The sonotrode must act on the surfaces to be welded with a given force before this ultrasonic welding takes place. Since the surfaces may already be pre-stressed one beside the other, the surfaces are reinforced by pressing one down on the other, so that there is no hollowness between them at the time of welding pressing. Since all plastics ultimately have an elastic structure, the surfaces slacken a little after welding. In order to calculate this beforehand, a special convex sonotrode is used for each individual material. This convexity depends on the material, on the size of the surface to be processed, the material thickness and/or the material executions. Such sonotrodes can therefore be used for the surface welding of things such as paper, fibres, metals, non-ferrous metals or plastics.
Further details and advantages of the object of invention are given in the following description of the associated drawing, in which a preferential execution example with the necessary details and components are shown:
The honeycomb construction consists of a great number of individual layers with hollow bodies and partial hollow bodies. Both the edge-side individual layer 2 and the edge-side individual layer 4 with the honeycomb construction 3 joined in between consist of honeycomb part plates 17 of a small wall thickness.
The individual hollow bodies 7, 8, 9 according to
While the separation line shown in
An edge-side individual layer 2 and 4 is represented in
In
In the representation according to
In
A building element 1 is represented in
A five-layer building element 1 is shown in
Thanks to the separation of individual layers, the cells of the spaces between layers can be controlled separately and individually, for example in connection with the use of a battery case. Owing to the support of the masses 49 and 51, the cells can also be used as ion carriers or for comparable processes, which are needed for the use of energy storage. The connection of greatest possible contact surfaces offered by the entire building element is crucial here. The individual layers can be merged into different requisite materials here and can be insulated from one another outstandingly in this way.
Finally,
Number | Date | Country | Kind |
---|---|---|---|
10 2011 100 967.5 | May 2011 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/DE2012/000459 | 5/7/2012 | WO | 00 | 1/17/2014 |