The present invention refers to a panel structure and to a process for making it.
For some time panels have been present on the market having sheets of composite material that give high resistance to the overall structure.
Reinforcement sheets made from composite material, consisting of a resin-based matrix in which a fibrous phase is dispersed, is particularly advantageous due to the high ratio between mechanical strength and weight, and can thus have various applications in different technological fields, from the building trade to the transport sector, etc.
Such a panel structure can nevertheless suffer from various drawbacks due above all to not always being able to optimally resist delamination between core and outer reinforcement sheets, and to not always being able to withstand mechanical stresses above all in the direction perpendicular to the main plane on which it lies.
In order to at least partially overcome these drawbacks it has been proposed to fixedly join together the reinforcement sheets with a sewing operation carried out through the core of the structure, but such a method is extremely laborious and burdensome in terms of time and therefore is also expensive and not very productive.
The technical task proposed of the present invention is, therefore, that of making a process for making a panel structure and a process for making it that allow the aforementioned technical drawbacks of the prior art to be eliminated.
In this technical task a purpose of the invention is that of making a panel structure that has an optimal capability to resist delamination and/or mechanical stresses in the direction perpendicular to the plane on which it lies.
Another purpose of the invention is that of making a panel structure that is extremely simplified and light but at the same time mechanically strong.
Another purpose of the invention is that of making a simple, extremely versatile and highly productive process for making a reinforced panel structure.
The technical task, as well as these and other purposes, according to the present invention, are accomplished by making a panel structure, characterised in that through at least part or all of its thickness a plurality of channels extend in which there are structural stiffening elements comprising a resin-based material.
Further characteristics and advantages of the invention shall become clearer from the description of preferred but not exclusive embodiments of the panel structure according to the finding, illustrated for indicating and not limiting purposes
With reference to the quoted figures, a panel structure is shown wholly indicated with reference numeral 1.
The panel 1 has a plurality of channels 2 that extend through at least part or all of its thickness.
The channels 2 preferably flow on at least one of two opposite faces 3, 4 of the panel 1, in particular on at least one of the two opposite faces that define its thickness. In the channels 2 there are structural stiffening elements 5 comprising a resin-based material.
The channels 2 preferably extend perpendicular to such opposite faces 3, 4 of the panel 1, and can be uniformly distributed on a defined part of the panel 1 or even on the entire panel 1.
However, the channels 2 can also have a different inclination or a different combination of inclinations to allow the structural stiffening elements 5 to be arranged according to a lattice design.
Preferably, the resin-based material is also present on the outside of the channels 2, on at least one of the opposite faces 3, 4 of the panel 1 in which the channels 2 flow, where it forms at least one reinforcement layer 12.
The resin is spread without solution of continuity inside the channels 2, where it defines the structural stiffening elements, and outside of them, where it defines every reinforcement layer 12, and thereby it ensures substantial consolidation of the overall panel structure 1.
In order to allow them to be correctly impregnated and completely filled with resin, the channels 2, in the case in which they have a blind end (
The outlet holes 6 can extend on the extension of the channels 2, as shown, or else they can extend transversally to the channels and flow on a side face of the panel 1 other than the opposite faces 3, 4 that define its thickness. The resin can according to the application be of the thermoplastic and/or thermosetting type or any other type suitable for the purpose, for example resins known by the trade name “ISOPLAST” or “CYCLICS”.
The resin can also be reinforced with continuous fibres (
In the case of reinforcement with continuous fibres, it is possible to foresee at least one first plurality of continuous fibres 9 that extend with one portion thereof in the structural stiffening elements 5 and with the remaining portion in one or each reinforcement layer 12, and a second plurality of continuous fibres that extends inside one or each reinforcement layer 12 (
The second plurality of continuous fibres can also be ordered in one or more piled up and directly associated layers 13, 14 of parallel continuous fibres in which each layer of fibres has its own orientation of the fibres.
In each reinforcement layer 12 the first plurality of fibres 9, and in particular the portion of the first plurality of fibres 9 present in the reinforcement layer 12, is directly associated with the second plurality of fibres.
Such direct associated is in the form of simple contact (
In both cases the association between the first fibres 13 and the second fibres 13, 14 promotes the consolidation of the overall structure and in addition also the resistance to delamination between each reinforcement layer 12 and the panel 1.
As an example the panel 1 is a sheet of PVC, expanded polyurethane or expanded phenolic resin, the resin used is thermosetting epoxy, phenolic or polyurethane resin, and the fibre used is glass.
The panel 1 can take up a substantially flat configuration (as shown) or else it can have an alveolar configuration suitable for flexibly adapting to surfaces of various profile, even curvilinear.
The process for making the panel structure 1, in the case in which the resin is to be reinforced with the first and second plurality 9 and 13, 14 of continuous fibres, consists of forming the channels 2, positioning and associating the first and second plurality of fibres 9 and 13, 14, impregnating the channels 2 and the first and second plurality of fibres 9 and 13, 14 with resin to constitute the structural stiffening elements 5 and each reinforcement layer 12, and carrying out the polymerisation and/or setting of the resin so as to consolidate and/or stiffen the structure.
The impregnation with resin can advantageously be carried out in a continuous pultrusion process, or else with a closed mould vacuum infusion process.
The channels 2 are formed by suitable perforators, for example needles, to which the fibres of the first plurality of fibres 9 are hooked to be pulled into the channels just as they are being made.
As stated, the second plurality of fibres 13, 14 is in the form of one or more of piled up layers.
The positioning of the first plurality of fibres 9 can be before or after that of the second plurality of fibres 13, 14. In the first case the first plurality of fibres 9 is associated by simple contact with the inner layer 13 of the second plurality of fibres, in the second case the fibres of the first plurality of fibres 9 interweave with the fibres of the second plurality of fibres as the perforators pass through the thickness of the layer or layers 13, 14 formed by the second plurality of fibres.
In the case in which the resin is to be reinforced with discontinuous fibres, firstly the fibres are positioned and then impregnation takes place preferably with a closed mould vacuum infusion process or a pressure injection process. Also in the case in which the resin is not to be reinforced the impregnation is preferably carried out with a closed mould vacuum infusion process or a pressure injection process.
The panel structure and the process for making it thus conceived can undergo numerous modifications and variations, all of which are covered by the inventive concept; moreover, all of the details can be replaced with technically equivalent elements.
whatever according to the requirements and the state of the art.
This application claims priority to PCT application EP06/00594 and is a divisional application of U.S. application Ser. No. 11/814,702 incorporated herein by reference.
Number | Date | Country | |
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Parent | 11814702 | Jul 2007 | US |
Child | 12722890 | US |