Method of fastening an object to a construction element
10336029 ยท 2019-07-02
Assignee
Inventors
Cpc classification
B29C66/472
PERFORMING OPERATIONS; TRANSPORTING
B27D5/003
PERFORMING OPERATIONS; TRANSPORTING
B29C66/30223
PERFORMING OPERATIONS; TRANSPORTING
B29C66/1224
PERFORMING OPERATIONS; TRANSPORTING
B32B3/08
PERFORMING OPERATIONS; TRANSPORTING
B29C66/3452
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7392
PERFORMING OPERATIONS; TRANSPORTING
B29C66/21
PERFORMING OPERATIONS; TRANSPORTING
B29C66/61
PERFORMING OPERATIONS; TRANSPORTING
B29C63/0026
PERFORMING OPERATIONS; TRANSPORTING
B29K2077/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/303
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7212
PERFORMING OPERATIONS; TRANSPORTING
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/71
PERFORMING OPERATIONS; TRANSPORTING
B29C65/80
PERFORMING OPERATIONS; TRANSPORTING
B29K2069/00
PERFORMING OPERATIONS; TRANSPORTING
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/24008
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
B29C65/80
PERFORMING OPERATIONS; TRANSPORTING
B29C66/30221
PERFORMING OPERATIONS; TRANSPORTING
B29C66/303
PERFORMING OPERATIONS; TRANSPORTING
B29C66/5346
PERFORMING OPERATIONS; TRANSPORTING
B29C65/645
PERFORMING OPERATIONS; TRANSPORTING
B29K2311/14
PERFORMING OPERATIONS; TRANSPORTING
B29C66/534
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/8322
PERFORMING OPERATIONS; TRANSPORTING
B29C66/1222
PERFORMING OPERATIONS; TRANSPORTING
B29L2031/10
PERFORMING OPERATIONS; TRANSPORTING
B29K2055/02
PERFORMING OPERATIONS; TRANSPORTING
B29K2077/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2033/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2069/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/71
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7212
PERFORMING OPERATIONS; TRANSPORTING
B29K2055/02
PERFORMING OPERATIONS; TRANSPORTING
B29K2033/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2105/12
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B37/00
PERFORMING OPERATIONS; TRANSPORTING
B29C63/00
PERFORMING OPERATIONS; TRANSPORTING
B27D5/00
PERFORMING OPERATIONS; TRANSPORTING
B29C65/64
PERFORMING OPERATIONS; TRANSPORTING
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method of fastening an edge structure to a construction element includes providing the construction element, being a planar structure with two cover regions and a middle region between the cover regions; providing the edge structure being continuously extended, the edge structure having contact surfaces with a thermoplastic material shaped to lie against the cover regions in an outer surface of the construction element, and, opposite the contact surfaces, a coupling-in surface for coupling energy into the edge structure; coupling energy into the edge structure and pressing the contact surfaces against the cover regions until at least a portion of the thermoplastic material is liquefied and pressed into the cover regions; and repeating or continuing the steps of coupling and pressing until the edge structure is attached to the building element at a plurality of discrete locations or over an extended region along an edge of the construction element.
Claims
1. A method of fastening an object to a lightweight building element, the method comprising the steps of: providing the lightweight building element element, being a planar structure with a first cover layer, a second cover layer, and a middle layer between the first and second cover layers, wherein a material density in the first and second cover layers is larger than in the middle layer, the first and second cover layers defining a first and second cover layer plane; providing the object, the object comprising a first contact surface with a thermoplastic material, a second contact surface with thermoplastic material, and a coupling-in surface for coupling energy into the object; positioning the object relative to the lightweight building element to bring the first contact surface in contact with the first cover layer and the second contact surface with the second cover layer, coupling mechanical energy into the object and pressing the object against the lightweight building element to move the object substantially parallel to the first and second cover layer planes and to cause thermoplastic material of the object to become liquefied and to be pressed into the first and second cover layers, until the first contact surface lies against an inside of the first cover layer and the second contact surface lies against an inside of the second cover layer; and allowing the liquefied thermoplastic material to re-solidify, whereby the liquefied and re-solidified thermoplastic material pressed into the first and second cover layers anchors the object with respect to the lightweight building element.
2. The method according to claim 1, wherein the object is free of elements protruding vertically beyond the first and second cover layers.
3. The method according to claim 1, wherein the contact surfaces comprise energy directors.
4. The method according to claim 3, wherein the energy directors in the step of coupling and pressing lay against the inside of the first and second cover layers.
5. The method according to claim 3, wherein an inner height of the object being an extension of the object without the energy directors in a direction perpendicular to the first and second cover layer planes corresponds to a distance between the cover layers.
6. The method according to claim 1, wherein the object has a rear side forming the coupling-in surface and an upper and a lower side forming the first and second contact surfaces.
7. The method according to claim 3, wherein the object has a rear side forming the coupling-in surface and an upper and a lower side having the energy directors.
8. The method according to claim 7, wherein the energy directors are edges that have a triangular cross section.
9. The method according to claim 1, wherein the object is rectangular in cross section with the contact surfaces extending parallel to the cover layers.
10. The method according to claim 1, wherein the pressing force is applied until the coupling-in surface is flush with an narrow side surface of the lightweight building element, whereby the object when fastened is completely in a space between the cover layers.
11. The method according to claim 1, wherein the middle layer comprises a filling.
12. The method according to claim 11, wherein the filling forms a honeycomb structure.
13. The method according to claim 12, wherein the honeycomb structure is of card.
14. The method according to claim 11, wherein the filling is of a foam material.
15. The method according to claim 1, wherein the cover layers are at least one of particle boards, fiberboards, laminated boards, plastic composite boards.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Embodiments of the invention are described in detail below on the basis of drawings. The drawings are schematic and not to scale. In the drawings, the same designations refer to the same or analogous elements and:
(2)
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DETAILED DESCRIPTION OF THE INVENTION
(13) In the illustrative examples of
(14) The cut-to-size lightweight building board that can be seen in
(15) The thickness of the cover layers may be chosen according to the applications. If the cover layers are made of a derived timber material, the thickness may be, in particular, 10 mm or less, for example between 2 mm and 8 mm, since for such thicknesses there is specifically a need for the edge to be supported.
(16) Arranged between the cover layers is a filling 2. This consists of a material that is light in comparison with the cover layers, for example a honeycomb structure made of card or a similar material. Other fillings forming walls with cavities lying in between are also conceivable, for example regularly arranged strips (the lightweight component is then sometimes referred to as a multi-wall sheet) or tubular structures. Furthermore, the use of Styropor or similar foams as well as, for example, aluminum honeycombs is also conceivable. Quite generally, the invention is not dependent on the type of filling and works irrespective of the nature of the filling.
(17)
(18) An edge support 3 of the type depicted in
(19) The edge support 3 has a vertical extent that is a little less than the thickness of the lightweight building board. At the contact surface 3.1 with the cover layers 1.1, 1.2, it comprises energy directors, which are formed for example as projecting corners or ridges tapering to an edge. Furthermore, formed in the region between the cover layers 1.1, 1.2 is a projecting guiding portion 3.2, the vertical extent of which corresponds to the distance between the cover layers 1.1, 1.2. A rear surface 3.3 (with respect to the lightweight board in the configuration of
(20) The mechanical vibrations are, for example, ultrasonic oscillations. In general, oscillations in a frequency range between 2 kHz and 100 kHz, preferably between 10 kHz and 40 kHz, for example about 20 kHz, are used; other frequencies are not ruled out. The power of the device generating the oscillationsa commercially available ultrasonic device may be useddepends on the dimensionings; it may lie in the range between 100 W and 2 kW.
(21) The pressing force 7 (and possibly the supporting force 8) may optionally be exerted already before the mechanical oscillations begin, in order to press the edge support 3 a little into the material of the cover layers already in the region of the contact surface 3.1, which in the subsequent step makes it even easier for the edge support to be guided and can ensure optimum introduction of the mechanical oscillations into the edge support. It is particularly favorable if the supporting force 8 is exerted already before the edge support is placed on, in order to ensure that the cover layers are kept fixed in position during the entire process.
(22) As soon as the mechanical oscillations 9 are coupled in, mechanical energy is absorbed, in particular in the region of the contact surfaceson account of the energy directors and the friction with the material of the cover layersand as a result the liquefying of the thermoplastic material is initiated. The material begins to melt and is pressed into the cover layers 1.1, 1.2. At the same time, incipient melting of the thermoplastic material may also take place in the region of the horizontal supporting surfaces 3.4 of the guiding portion, on account of the friction with the cover layers.
(23) After the mechanical oscillations end, the liquefied material sets again, and a stable positively engaging connection with the material of the cover layers is obtained. This is represented in
(24) This anchoring process is carried out for a plurality of edge supports 3 along the narrow side, the edge supports preferably being arranged at regular intervals, which can be seen particularly well in
(25) In this case, each edge support may be anchored individually, or a number of edge supports may be inserted simultaneously with the aid of an extended sonotrode, covering a number of edge supports.
(26) This has the overall effect of producing an extended region of the narrow side, which is provided with edge supports in such a way that the edge 11 can be adhesively attached to the flat rear side 3.3, serving in the previous step as a coupling-in surface for the mechanical oscillations. This is illustrated in
(27) Before the adhesive attachment of the edge, a milling or grinding of the narrow sideincluding the edge supportmay possibly also take place, in order that the lightweight component has a smooth, regular surface in the region of the narrow side.
(28) If an edge support 3 of the type represented in
(29)
(30) As represented in
(31) If, as in
(32) The variant of the edge support depicted in
(33) The angled position of the edge support also makes it possible for the edge to be supported over a greater length.
(34) The variant according to
(35)
(36) In the embodiment according to
(37) Even if in the case of the edge support of this embodiment there is no guiding portion projecting beyond the contact surface 3.1, the actual edge support body (i.e. the edge support without the energy directors) can act in a guiding manner during introduction if the inner height h.sub.2 is chosen to correspond to the distance between the cover layers. This also applies if the edge support according to
(38) Also in the case of edge supports of this embodiment, a supporting force 8 is exerted on both cover layers. The supporting force 8 is especially important here, since the introduction of the edge support according to
(39) The embodiment according to
(40) It is a preferred principle of the invention that the sonotrode acts on the edge support from the narrow sidethat is to say not through the cover layers. In the embodiments described above, the pressing force 7 acts from the end side, that is to say horizontally. An embodiment in which the sonotrode likewise acts on the edge support from the narrow side, but in which the pressing force is applied vertically, is described below on the basis of
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(43) During the anchorage of the edge support 3, for example, upper and lower regions are anchored alternately along the narrow side. However, it is also possible, for example, first to anchor all the upper regions and then to anchor all the lower regions. Optionally, this may be accompanied by turning the lightweight component as a whole around. In the latter case, active application of the counter force may be made superfluous, in that during the anchoring there is always downward pressing and the supporting force can always be applied by the underlying surface against which the pressing force is directed.
(44) The attachment of the edge with the decoration takes place by analogy with the above embodiments; here, too, a milling or grinding of the narrow side may take place in advance. This embodiment is even particularly suitable for this, since, as illustrated, the edge support can be anchored such that it is set back with respect to the end side of the cover layers. If it is done in this way, it is necessary for the cover layers to be removed until they are flush with the edge support, in order for adhesive attachment of the edge to become possible.
(45) As a difference from the embodiments described above, however, in the case of the example according to
(46) Many other embodiments besides are conceivable, for example with network- or grid-like edge supports, differently formed sonotrodes, etc. It is also possible to construct the edge support from a number of materials and not just from one material, as in the examples illustrated above.
(47) Depicted in
(48) In an arrangement that is virtually identical to
(49) The method according to
(50)
(51) Alternatively, a middle layer material removal step may be carried out prior to the fastening, This alternative approach is also an option in case the middle layer 2 is of a material that is not substantially plastically or elastically deformable, such as of a metal foam (for example aluminium foam).
(52)
(53) To fasten an edge structure of the kind described for example referring to
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(55) The step of pressing and causing energy to impinge may be carried out until the ground of the shallow groove 3.21 abuts against the surface of the construction element, or may stop before this is the case. In the former case, the ground thereby serves as stop face, with no or comparably little energy being absorbed at the interface because no energy directing elements are present. In either case, a solid and dense connection along the upper and lower brinks 21.6, 21.7 results.
(56) In addition or as an alternative to the edge structure 3 comprising an indentation, the construction element 21 may be provided with an indentation 21.5, so that the edge structure is not in contact with the middle region 21.3 during an initial stage of the pressing and coupling energy into the edge structure.
(57) In the embodiment of
(58) In the previously illustrated embodiments, the sonotrode 5 that couples the energy in the form of mechanical vibration energy into the edge structure is assumed to be flat with a plane or roller-like outcoupling structure.
(59) The protrusions serve as an additional or alternative measure for ensuring that the edge structure 3 is pressed against the cover regions and not or only to a lesser extent against the coupling energy into the edge structure and pressing the contact surfaces against the cover regions middle region 2, especially if the edge structure 3 is sufficiently flexible.