Honeycomb structure element
09579866 ยท 2017-02-28
Assignee
Inventors
Cpc classification
Y10T428/24165
GENERAL 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
B32B3/28
PERFORMING OPERATIONS; TRANSPORTING
B32B2553/00
PERFORMING OPERATIONS; TRANSPORTING
B32B7/05
PERFORMING OPERATIONS; TRANSPORTING
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/24149
GENERAL 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
International classification
B32B3/12
PERFORMING OPERATIONS; TRANSPORTING
B32B3/28
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A honeycomb structure element including an at least partially closed honeycomb structure, which is formed by joining at least two structured layers having honeycomb cells that are open on one side. A method for manufacturing a honeycomb structure element including forming an at least partially closed honeycomb structure by joining at least two structured layers having honeycomb cells that are open on one side.
Claims
1. A honeycomb structure element comprising at least two layers, which are bonded together to form an at least partially closed honeycomb structure, wherein one of the two layers is a first structured layer with honeycomb cells open on one side, and the other of the two layers is a second structured layer with honeycomb cells open on one side, wherein the honeycomb cells are depressions with an essentially hexagonal footprint and exhibit wall surfaces which are trapezoidal, wherein the two structured layers are joined together in such a way that the openings of the honeycomb cells of the first structured layer point away from the second structured layer, and the openings of the honeycomb cells of the second structured layer point away from the first structured layer, and the two structured layers together form a honeycomb structure with closed honeycomb cells between the honeycomb cells of the first structured layer and the honeycomb cells of the second structured layer, wherein, when the layers are joined together, the footprint of each honeycomb cell of each structured layer is in contact with a surface of the opposing structured layer, wherein, when the layers are joined together, each closed honeycomb cell is formed between three wall surfaces of three separate honeycomb cells of the first structured layer and three separate wall surfaces of three separate honeycomb cells of the second structured layer, and the wall surface of each of the three honeycomb cells of the first structured layer forming the closed honeycomb cell has two adjacent wall surfaces in contact with adjacent wall surfaces of two of the honeycomb cells of the second structured layer, and the wall surface of each of the three honeycomb cells of the second structured layer forming the closed honeycomb cell has two adjacent wall surfaces in contact with adjacent wall surfaces of two of the honeycomb cells of the first structured layer, and wherein the closed honeycomb cells comprise a plurality of vacuum cells or wherein the closed honeycomb cells are filled with nitrogen, argon, krypton, SF6, or heat accumulating materials.
2. The honeycomb structure element according to claim 1, wherein the two structured layers are structured identically.
3. The honeycomb structure element according to claim 1, wherein the structured layers are comprised of deep-drawn films.
4. The honeycomb structure element according to claim 1, wherein one third of the honeycomb cells are closed honeycomb cells, except for the edge regions of the honeycomb structure element.
5. The honeycomb structure element according to claim 1, wherein the open honeycomb cells of at least one of the two structured layers are sealed by an outer flat layer.
6. The honeycomb structure element according to claim 5, wherein the open honeycomb cells of the two structured layers are each sealed by an outer flat layer.
7. The honeycomb structure element according to claim 5, wherein the one outer flat layer or outer flat layers are formed by a flat film.
8. The honeycomb structure element according to claim 1, wherein all honeycomb cells of the honeycomb structure element are closed, except for edge regions of the honeycomb structure element.
9. The honeycomb structure element according to claim 1, wherein, in addition to the first and second structured layer and/or the first and second structured layers sealed with outer flat layers, the honeycomb structure element comprises, bonded thereto, additional structured layers or structured layers sealed with outer flat layers.
10. The honeycomb structure element according to claim 1, wherein the honeycomb cells in the structured layers further comprise at least one counter-depression extending toward the opening of at least one honeycomb cell.
11. The honeycomb structure element according to claim 1, wherein the closed honeycomb cells comprise a plurality of vacuum cells.
12. The honeycomb structure element according to claim 1, wherein the closed honeycomb cells are filled with SF6.
13. The honeycomb structure element according to claim 1, wherein the closed honeycomb cells are filled with nitrogen.
14. The honeycomb structure element according to claim 1, wherein the closed honeycomb cells are filled with heat accumulating materials.
15. The honeycomb structure element according to claim 1, wherein the closed honeycomb cells are filled with krypton or argon.
16. A method for manufacturing a honeycomb structure element according to claim 1, wherein the honeycomb cells of the layers are deep drawn by means of a vacuum, and the layers are bonded with each other after being joined together.
17. The method according to claim 16, wherein the layers are joined and/or bonded together under a vacuum, in the air or in a gas atmosphere.
18. A honeycomb structure element comprising at least two layers, which are bonded together to form an at least partially closed honeycomb structure, wherein one of the two layers is a first structured layer with honeycomb cells open on one side, and the other of the two layers is a second structured layer with honeycomb cells open on one side, wherein the two structured layers are joined together in such a way that the openings of the honeycomb cells of the first structured layer point away from the second structured layer, and the openings of the honeycomb cells of the second structured layer point away from the first structured layer, and the two structured layers together form a honeycomb structure with closed honeycomb cells between the honeycomb cells of the first structured layer and the honeycomb cells of the second structured layer, and wherein the honeycomb cells in the structured layers further comprise at least one counter-depression extending toward the opening of at least one honeycomb cell.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention will be explained in more detail below based on exemplary embodiments, drawing reference to the attached drawings. It is shown:
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DESCRIPTION OF THE PREFERRED EMBODIMENTS
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(21) In
(22) The same also applies to the honeycomb cell arrangement depicted in
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(26) The corresponding adjustments to the manufacturing process can be easily resolved by the person skilled in the art, since only the tools, e.g., in a deep drawing process, must be tailored to the respective new honeycomb cell geometry. The same holds true for adjustments to the process while bonding the structured layers.
(27) A preferred honeycomb structure element according to the invention is fabricated in two steps:
(28) In a first step, each third honeycomb cell of a honeycomb structure to be constructed is deep drawn on a first surface 105 (and/or 206) of a film, thereby yielding a first film with honeycomb cells 104 (and/or 204) open on one side regularly distributed over the film.
(29) In a second step, two such films (101, 201) are joined together opposite each other and bonded (i.e., adhesively bonded or welded), thus forming closed honeycomb cells 500 of the secondary structure bordered by the wall surfaces 107 and 207 of the deep drawn honeycomb cells 104 and 204 of the primary structure.
(30) In further steps, several such dual layers can be placed one on top of the other and bonded together, so that some (or preferably) all of the honeycomb cells 104 and/or 204 open on one side are sealed by the overlying layer.
(31) Another preferred honeycomb structure element according to the invention is fabricated in three steps:
(32) In a first step, every third honeycomb cell of a honeycomb structure to be constructed is deep drawn on a first surface 105 (and/or 206) of a film, thereby yielding a first film with honeycomb cells 104 (and/or 204) open on one side regularly distributed over the film.
(33) In a second step, two such films (101, 201) are joined together opposite each other and bonded (i.e., adhesively bonded or welded), thus forming closed honeycomb cells 500 of the secondary structure bordered by the wall surfaces 107 and 207 of the deep drawn honeycomb cells 104 and 204 of the primary structure.
(34) In a third step, the resultant honeycomb structure is then covered on either side by a flat film 301 and 401 and bonded thereto (i.e., adhesively bonded or welded), thereby sealing the honeycomb cells 104 and 204 open on one side, and yielding a honeycomb structure element with exclusively closed honeycomb cells.
(35) In further steps, several such honeycomb structure elements can be placed one on top of the other and bonded together. Such multi-layer honeycomb structure elements, in particular those sealed by cover layers, are also referred to as panels.
(36) In the present invention, the mentioned exemplary embodiments can use various materials and different material thicknesses for the structured layers, as well as for the flat layers. For example, the structured layers can be manufactured out of a material permeable to thermal radiation (e.g., transparent PET, glass, etc.), and the flat layers can be manufactured out of a material impermeable to thermal radiation (e.g., aluminum, infrared filter, etc.).
(37) In particular the material used for the support structure of the structured layers most advantageously exhibits a slight thermal conductivity. By contrast, the material used for the flat layers most advantageously exhibits the lowest possible level of emission for thermal radiation, in particular in the case of a support structure transparent to thermal radiation. Materials with a low level of emission for thermal radiation, e.g., aluminum, often have a high thermal conductivity. This is why combining different materials for support and cover layers yields advantages in particular for applications involving insulation.
(38) In another advantageous exemplary embodiment of the invention, the two structured layers 101 and 201 are manufactured out of different materials. For example, the structured layer 101 consists of a thick, loadable material so as to support the structure, and the structured layer 201 consists of a thin material so as to close the secondary honeycomb cells.
(39) In another advantageous exemplary embodiment, the honeycomb cells of a honeycomb structure element according to the invention can be filled with air or different gases. Examples include gases like nitrogen or inert gases like argon or krypton, which are suitable for reducing the thermal conductivity, or gases like SF6, which is suitable for soundproofing. Such materials are suitable as building products and materials, among other things. It is here especially preferred that the honeycomb cells be filled with air.
(40) In another advantageous exemplary embodiment, the honeycomb cells of a honeycomb structure element according to the invention can be filled with different materials, for example heat accumulating materials, in particular materials known as latent heat accumulators. For example, these change consistency at a specific temperature, and can thereby keep the temperature constant for a long time. Among other things, such materials are suitable for packagings for drugs, which have to be transported at a constant temperature.
(41) In another advantageous exemplary embodiment, a honeycomb structure element with closed honeycomb cells encompasses a plurality of closed vacuum cells. The vacuum cells together form a closed vacuum cavity. Such honeycomb structure elements, in particular in the form of panels, are suitable as building products and materials, for example. While damage is done to the vacuum cavity during activities common in building construction, for example drilling, sawing or cutting, this only happens for a small number of the plurality of closed vacuum cells. As a consequence, a vacuum insulation established by the vacuum cavity as a whole is only slightly impaired. A honeycomb structure element with a plurality of closed vacuum cells makes it possible to take the panels fabricated out of the latter and mold them into individual shapes and/or also to correspondingly shape and process them at the building construction site, without significantly impairing the vacuum insulation in the process.
(42) Additional structural variations to the honeycomb structure elements described above can be realized. In particular combinations of the various exemplary embodiments or combinations of the used methods are conceivable for manufacturing a honeycomb structure element with an at least partially closed honeycomb structure.