• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    A polymeric sandwich structural core (1) comprising a resinous honeycomb structure (31) with a first and a second polymeric fabric sheet (8, 9) adhered at the location of an adhesive tape (17) . A cell (5) comprises a corrugated portion of a cell (12) on at least one of its faces (6), on which a resin is arranged and crosslinked. The invention also relates to a method for producing such a core of polymeric sandwich structural material.
    公开号:FR3016315A1
    申请号:FR1450309
    申请日:2014-01-15
    公开日:2015-07-17
    发明作者:Frederic Brun
    申请人:Chermant Alexis；Frederic Brun；
    IPC主号:
    专利说明:

    [0001] The present invention relates to processes for producing cores of polymeric sandwich structural material, to polymeric sandwich structural material cores obtained by such processes and to structural materials. BACKGROUND OF THE INVENTION with such a soul. The sandwich structural materials are generally composed of two external skins secured to the opposite faces of a core. Said core is made in such a way that it has a high structural resistance to compression and bending while maintaining a minimum weight. These structural materials have many applications for example in the field of aeronautics or the automobile. Among these materials, the best known are those having a honeycomb core. These souls consist of sheets shaped and then fixed together at specific points to form a network of cells of hexagonal profile, sometimes deformed, which extend perpendicularly audite external skins. BACKGROUND ART US 5,431,980 discloses webs of structural materials that can be used to create rigid, light, and curved walls. To do this, the document provides in particular a core of structural material which comprises cells in the form of honeycomb, which cells have sides with particular shapes, of the type with wavy shapes, semicircular designs etc. The cores are made from corrugated strips superimposed on each other, and punctually connected to each other by fixing areas. The wavy bands have a repeating pattern along their entire length, and the pattern includes a flat area alternating with a wavy area. The flat areas of each corrugated strip are alternately fixed either to a flat area of an upper corrugated strip or to a flat area of a lower corrugated strip. On the other hand, the web of material is deployable between a compact state and an expanded expanded state of superimposed corrugated webs in a direction perpendicular to the direction of said superimposed corrugated webs. Said core can be made in a wide variety of constituent materials including for example metals such as aluminum. Advantageously, such a core can be made of non-metallic materials such as polymeric materials. This increases in particular the fire resistance and reduce the release of toxic fumes. This also makes it possible to reduce the cost of the structure, simplify the production process and optimally control the mechanical characteristics obtained. OBJECT OF THE INVENTION The object of the invention is to provide a polymer sandwich structural material core having in particular improved mechanical characteristics, reduced density and / or reduced cost. To this end, the invention firstly relates to a process for producing a polymer sandwich structural material core comprising the steps of: providing at least a first sheet of polymeric fabric and a second sheet of polymeric fabric extending respectively substantially in extension directions, a sheet of the first and second sheets having at least one corrugated portion of sheet in a sheet thickness direction substantially perpendicular to the extension directions, a sheet of the first and the second sheet second sheet having at least one adhesive tape, superimposing the first and second sheets in the sheet thickness direction to obtain a sheet sandwich, pressing the sheet sandwich in the sheet thickness direction so that the sheets adhere to each other at the location of the adhesive strip, stretch the sheet sandwich in the direction of the strip A sheet-spreader for forming a honeycomb structure having at least one cell, said cell being provided with a corrugated portion of a cell on at least one side until a core of polymeric sandwich structural material is obtained. density within a predefined density range, reiterate the operations of: disposing a resin at least on the corrugated portion of cell of the honeycomb structure, and cross-linking the resin to obtain a resinous honeycomb structure. In preferred embodiments of the invention, one or more of the following steps may also be used: the step of providing at least a first sheet of polymeric fabric and a second sheet of polymeric fabric comprises: providing a strip of polymeric fabric extending substantially in directions of extension, deforming at least a portion of the strip of polymeric fabric in a sheet thickness direction substantially perpendicular to the directions of extending, so as to obtain a corrugated portion of the strip, disposing at least one adhesive strip on the strip of polymeric fabric, cutting the strip to form at least a first and a second sheet of polymeric fabric respectively extending substantially in the directions at least one of the first and second sheets having the corrugated portion of the strip, at least one sheet the second sheet comprising the adhesive tape; the first and second polymeric fabric sheets respectively comprise a first corrugated portion of a sheet and a second corrugated portion of a sheet, and the first and second sheets are superimposed to obtain a sandwich of sheets so as to arrange the first and the second second corrugated portions of sheet facing one another adhesive; The step of pressing the sheet sandwich comprises heating the sheet sandwich to activate the adhesive tape; the step of stretching the sheet sandwich to form a honeycomb structure comprises firing the honeycomb structure at a temperature above a glass transition temperature of the polymer fabric to obtain an adhesive self-supporting honeycomb structure; in order to dispose a resin at least over the corrugated cell portion of the honeycomb structure, the honeycomb structure is quenched in a resin bath. The invention also relates to a polymer sandwich structural material core extending substantially in core extension directions and being intended to be between a top surface and a bottom surface, opposite in a thickness direction. core, said core comprising a resinous honeycomb structure having at least one cell, said honeycomb structure having a sheet-like sandwich, stretched in a sheet-thickness direction, comprising at least a first sheet of polymeric fabric and a second sheet of polymeric fabric respectively extending substantially in directions of extension, substantially perpendicular to the sheet thickness direction, the first and second sheets adhering to each other at the location of at least one web adhesive, a resin being disposed, and crosslinked, at least on said cell of the honeycomb structure.
    [0002] A sheet of the first and second sheets of polymeric fabric has at least one corrugated portion of sheet, deformed in the sheet thickness direction, said at least one cell is provided with a corrugated portion of the cell on at least one face and the resin is disposed and crosslinked at least over the corrugated cell portion of the honeycomb structure. In preferred embodiments of the invention, one or more of the following may optionally be further employed: - a sheet of the first and second sheets of polymeric fabric has a web adhesive at a wavy portion of a sheet; the corrugated sheet portion and the corrugated cell portion have a plurality of overhang patterns, each pattern overlying the corrugated sheet portion extending substantially out of the extension plane formed by the sheet extension directions; the corrugated portion of a sheet has a general zigzag shape comprising at least two sheet bumps; said at least two bumps each have a peak apex.
    [0003] The invention finally relates to a sandwich structural material comprising a core as described above, and at least one outer skin attached to said core.
    [0004] BRIEF DESCRIPTION OF THE DRAWINGS In order to be executed, the invention is set forth in a sufficiently clear and complete manner in the following description which is, in addition, accompanied by drawings in which: FIG. 1 partially shows a core of structural material, seen in perspective and substantially from above, - Figure 2 shows a detail of a web of structural material according to the invention, front view and illustrating in particular a cell, - Figure 3 shows the tape supply steps, deformation of the tape and adhesive deposit of a method for producing a core 20 of polymeric sandwich structural material, - Figure 4 illustrates a detail of the deformation step of the strip of Figure 3, - Figure 5 shows a detail of the adhesive deposition step of FIG. 3; FIG. 6 shows the steps of cutting the web, superimposing the sheets, pressing the sheet sandwich, stretching the sheet sandwich, resin deposition and resin crosslinking of a method of making a core of polymeric sandwich structural material; FIG. 7 illustrates a honeycomb structure after the step of stretching the sheet sandwich of FIG. 6, and FIG. 8 illustrates a variant of the honeycomb structure after the step of stretching the sheet sandwich of FIG. 6.
    [0005] DETAILED DESCRIPTION In the following description, the terms "lower", "upper", "high", "low", etc. are used with reference to the drawings for greater ease of understanding. They should not be understood as limitations of the scope of the invention. Figure 1 illustrates a core 1 according to the invention. The core 1 extends substantially along core extension directions X ', Y' and is intended to be between an upper surface 1a and a lower surface 15b, opposite in a web thickness direction. Z ', to constitute a sandwich structural material 50. In the embodiment illustrated in Figures 1 and 2, the core 1 comprises eight sheets of polymer fabric 2 in the form of two single sheets surrounding three assemblies of two sheets each, eight leaves in total. A core of structural material according to the invention is however not limited to the presence of a particular amount of polymeric fabric sheets 2, and depending on the desired extension of the core 1 in the extension directions X 'and Y', the soul may comprise more or less sheets of polymer fabric 2 without departing from the scope of the invention. The sheets 2 are made of polymer fabric. In particular, the sheets 2 are made from 30 aramid fibers, for example meta-aramid or para-aramid. Such fibers may for example be woven or amalgamated in the form of pulp to form a lightweight and strong synthetic paper. Such a polymeric fabric has in particular "shape memory" characteristics which are exploited by the present invention as detailed below. In order to obtain a core of resistant polymer 1 structural sandwich material, the sheets 2 of polymer fabric are impregnated with a hardened resin 3 so as to obtain a composite material that is resistant in the three dimensions of space and that is therefore particularly light. Referring now more particularly to Figure 2 which illustrates a detail of a core 1 of polymer sandwich structural material 10 according to the invention, the core 1 comprises a honeycomb structure 4 having at least one cell 5. Advantageously, the structure 4 comprises a large number of cells 5 juxtaposed to each other along the directions of soul extension X ', Y' to form a periodic network of arbitrary dimensions. By "cell" is meant for example an elementary cell of said periodic network. By "honeycomb structure" is meant that the structure 4, although formed of originally planar sheets 2, is a three-dimensional structure, the sheets 2 being assembled and shaped to form a structure of arbitrary dimensions, mainly consisting of a void between the sheets 2, and having high mechanical strength characteristics. Each cell 5 comprises a plurality of faces 6, for example in the case of Figures 1 and 2, five faces 6. Advantageously, the cells 5 may form, once juxtaposed to each other, an array of cells 5a hexagonal, advantageously an array of regular hexagonal cells 5a. By "cell" is thus meant a three-dimensional structure of which a section has a closed shape on itself, in particular a hexagon, in the case of a honeycomb of a network type "honeycomb".
    [0006] The periodic network formed by the juxtaposition of the cells 3 can thus be a network of honeycomb type. In such a network with hexagonal cells 5a, the cells 5 can be juxtaposed so that each face 6 of a cell 5 constitutes a face 6 of two adjacent cells 5a. The honeycomb structure 4 thus forms a compact and resistant network, advantageously a "honeycomb" network. More specifically, as illustrated in FIGS. 1 and 2, the honeycomb structure 4 comprises a sheet sandwich 7 comprising at least a first sheet of polymer fabric 8 and a second sheet of polymer fabric 9. The first and second sheets of polymer fabric 15 extend respectively in directions of extension X, Y. They are shaped in a sheet thickness direction Z, substantially perpendicular to the extension directions X, Y, so that the sheet sandwich is stretched in the direction of sheet thickness. The directions of extension X, Y and thickness of sheet Z are usually not collinear respectively with the directions of extension of the core X ', Y' and core thickness Z 'but rotated by 90 ° , so that the X, Y extension directions are respectively collinear with a core extension direction X 'and the core thickness direction Z', while the sheet thickness direction Z is collinear with a direction of extension of the soul Y '. The first and second polymeric fabric sheets 8, 9 further adhere to each other at the location of at least one adhesive strip 17. In the example of Figure 2, the resin 3 is particularly arranged and cured at the location of the adhesive strip 17.
    [0007] As can be seen in FIGS. 1, 2 and 8, the core of sandwich structural material 1 is in particular such that the first and second sheets of polymer fabric 8, 9 comprise at least one corrugated portion of sheet 11, advantageously Deformed in the sheet thickness direction Z. As detailed below, the first and second polymeric fabric sheets 8, 9 are shaped in the sheet thickness direction Z, and the sheet sandwich 7 is set. shaped to form the honeycomb structure 4, said corrugated portions of sheet 11 then constitute corrugated portions of cell 12 disposed on at least one face 6 of a cell 5.
    [0008] Thus, the corrugated portion of sheet 11 and the corrugated portion of cell 12 may comprise a plurality of overlying patterns 14 so as to have a general zigzag shape, the overlying patterns 14 advantageously forming at least two bumps.
    [0009] The resin 3 is for example arranged and crosslinked on the corrugated portion of cell 12 of the honeycomb structure 4. In this way, the resin 3 forms a plurality of menisci 13 on the corrugated portion of cell 12 and more particularly, a meniscus 13 14. The menisci 13 make it possible to stiffen the overflow patterns 14 and thus to increase the tensile strength and compression of the core of the polymeric sandwich structural material 1, in particular according to the requirements of the invention. soul extension directions X 'and Y'. A method for making such a sandwich structural material core 1 and such a sandwich structural material 50 will now be described with particular reference to FIGS. 3 to 6. FIG. 3 in connection with FIGS. 4 and 5 illustrates the first steps of such a method while Figure 6, in conjunction with Figures 6A, 7 and 8, illustrates the further steps of the method. As shown in FIG. 3, the process for producing a polymer sandwich structural material core 1 according to the invention firstly comprises a first step 100 of supplying a strip of polymer fabric 15. More specifically, the polymeric web 15 may extend substantially in X, Y extension directions comprising a longitudinal extension direction X and a transverse extension direction Y. The polymeric web 15 may have a defined width, for example substantially also to the desired thickness E for the core 1, in the direction of transverse extension Y, for example between a few centimeters and a few meters. The polymeric fabric web 15 may furthermore have a significantly greater length in the direction of longitudinal extension X, for example from a few meters to several hundred meters. The strip of polymer fabric 15 may thus be wound around itself. of the transverse extension direction Y, so as to form a roll of polymeric fabric web unwound as the core of polymeric sandwich structural material 1 is made. Such a polymeric fabric strip 15 is constituted a polymer fabric for example aramid fibers as described above.
    [0010] In a second deformation step 200 of the strip, illustrated more particularly in FIG. 4, at least a portion of the strip of polymer fabric 15 is deformed in the sheet thickness direction Z, substantially perpendicular to the extension directions X Thus, a corrugated portion of strip 16 is obtained. As shown in FIG. 4, the strip of polymer fabric 15 can be compressed between two shaping rollers 18, 19 whose contact surfaces with the polymeric fabric web has a plurality of etched patterns 18a, 19a. The corrugated band portion 16 thus obtained has a plurality of overlying patterns 14, each overlying pattern 14 extending substantially out of the extension plane XY formed by the extension directions X, Y. Advantageously, the patterns in FIG. overhang 14 are one-dimensional patterns in the direction of transverse extension Y. The overflow patterns 14 are for example corrugated strips, aligned in the direction of transverse extension Y, and having corrugations or bumps in the direction of Longitudinal extension X. The overflow patterns 14 thus have a general zigzag shape in a section along an XZ plane perpendicular to the transverse extension direction Y. Alternatively, the overlying patterns 14 may be two-dimensional patterns extending according to the directions of longitudinal extension X and transverse Y. As can be seen in FIG. 4, all the contact surfaces of the form rollers 18, 19 with the polymer fabric strip 15 may be covered with etched patterns 18a, 19a, so that the strip of polymeric fabric 15, when pressed between the rollers 18 and 19, is corrugated throughout its longitudinal extension, In this embodiment, the corrugated portion of strip 16 thus constitutes the entire strip of polymer fabric 15. In this embodiment, it is possible to obtain a cellular structure 4 as shown in FIG. 8 , All of whose sheets 2 is wavy. Alternatively, the contact surfaces of the shaping rollers 18, 19 with the polymeric fabric web 15 may have smooth portions between etched patterns 18a, 19a, so that the polymeric fabric web 15 when pressed between the rollers 18 and 19 have residual smooth portions 27. In a third adhesive deposition step 300, illustrated more particularly in FIG. 5, at least one adhesive strip 17 is provided on the polymer fabric strip 15. The Adhesive tape 17 may, for example, extend substantially in the direction of transverse extension Y. Preferably, a plurality of adhesive strips 17 are arranged on the strip of polymer fabric 15, arranged for example periodically, in particular periodically according to the direction of longitudinal extension X. For this purpose, the strip of polymer fabric 15 can be pressed between two adhesive deposition rolls 20, 21. The contact surface one or both of the adhesive deposition rollers 20, 21 may in particular comprise one or more adhesive inlets 20a permitting an adhesive supply at the contact surfaces of the adhesive deposition rollers 20 With one embodiment of the invention, illustrated in particular in FIGS. 2 and 8, one or more adhesive strips 17 are arranged on one or more corrugated portions of strip 16.
    [0011] In another embodiment of the invention, illustrated for example in Figure 1, adhesive strips 17 may be disposed on residual smooth portions 27 of the polymeric fabric web 15.
    [0012] Advantageously, the adhesive strips 17 are disposed on the polymeric fabric strip 15 after the polymeric fabric web 15 has been deformed (step 200) to obtain the corrugated portion of the web 16. The shape memory of the polymeric fabric allows This is because the polymeric fabric web 15 is crushed between the substantially planar contacting surfaces of the two adhesive deposition rollers 20 and 21 without the corrugated portion of the web 16 being shaped at the deformation step 200 , do not disappear. Such an arrangement of the steps of the method of producing the core, the step of arranging the adhesive strip 300 being performed after the deformation step 200, also makes it possible to prevent an adhesive deposit on the setting rolls. 18, 19 which can occur when the deformation step 200 is performed after the disposition step 300. In a fourth tape cutting step 400, the polymeric web is cut to form a plurality of sheets. of polymeric fabric 2. A first sheet of polymeric fabric 8 and a second sheet of polymeric fabric 9 are formed in particular. More specifically, the strip of polymeric fabric 15 is cut out so that at least one sheet of the first and the last second sheet 8, 9 comprises the corrugated portion of strip 16 and so that at least one sheet of the first and second sheets 8, 9 comprises the adhesive strip 17. For this purpose, as ill In FIG. 6, the polymeric fabric web 15 may be cut in the direction of transverse extension Y to form substantially rectangular polymeric fabric sheets 2. In a fifth sheet-stacking step 500, also illustrated in FIG. 6, the polymeric fabric sheets 2 are superimposed on each other in the sheet thickness direction Z to obtain the sheet sandwich 7. Thus, in particular superimposing the first and second sheets 8, 9 to each other.
    [0013] More specifically, the first and second sheets 8, 9 may respectively comprise a plurality of adhesive strips 17 respectively extending in the direction of transverse extension Y. It is then possible to superimpose the first sheet of polymer fabric 8 on the second sheet of polymeric fabric 9 so as to alternate, in the direction of longitudinal extension X, the respective adhesive strips 17 of the first and second sheets 8, 9 as shown in the detail of Figure 6A. On the other hand, the first and second polymeric fabric sheets 8, 9 may respectively comprise a first corrugated portion of sheet 24 and a second corrugated portion of sheet 25. It is then advantageous to superimpose the first sheet of polymeric fabric 8 to the second polymeric fabric sheet 9 so as to have the first corrugated portion of sheet 24 facing the second corrugated portion of sheet 25. More specifically, the overlying patterns 14 of the first and second corrugated portions of sheet 24, 25 may be aligned.
    [0014] Alternatively, the steps of supplying (100), deformation (200), deposition of adhesive (300), cutting of the web (400) and superimposition (500) described above can be carried out in a different order. , omitting some of these steps and / or adding additional intermediate steps.
    [0015] Thus, by way of example, the deformation (200), adhesive deposition (300) and superposition (500) steps can be performed directly on pre-cut polymeric fabric sheets instead of a polymer web. . A sixth pressing step 600 of the sheet sandwich comprises pressing the sheet sandwich 7 in the sheet thickness direction Z. As shown schematically in Fig. 6, the flat sheet sandwich 7 may be provided for this purpose. in a press adapted to compress the sheet sandwich 7 in the sheet thickness direction Z. This sixth step of the method thus makes it possible to adhere the adjacent sheets 2 to each other at the location of the adhesive strips 17 so that that the sheet sandwich 7 forms a unique and solid structure. During this step 600, the sheet sandwich 7 can be further heated in particular to activate the adhesive strip 17. In an advantageous embodiment of step 600, the surfaces 28 of the press in contact with the sandwich Sheets 7 may have etched patterns 29 similar to the overlying patterns 14 of the sheets 2 of the sheet sandwich 7. In this way, the press step allows for optimum adhesion of the sheets 2 to each other. During a seventh step 700 of stretching of the sandwich, the sheet sandwich 7 obtained after the pressing step 600 is stretched in the direction of sheet thickness Z to form the cellular structure 4 illustrated in FIG. To this end, it is for example possible to fix two drawing supports 30, respectively on an upper end 7a and a lower end 7b of the sandwich of opposite sheets 7 in the sheet thickness direction Z. two drawing supports 30 are then moved and moved away from each other, in the sheet thickness direction Z, so as to space the upper ends 7a and 7b of the sandwich sandwich from each other sheets 7 to stretch said sandwich 7 and form a honeycomb structure 4. The honeycomb structure 4 thus obtained comprises a plurality of cells 5, each cell 5 having a plurality of faces 6. More precisely, as can be seen in FIG. 7, the plurality of faces 6 may comprise one or more double faces 22, each double face 22 being constituted by two sheets 2 bonded together by an adhesive tape 17, for example the first sheet of polymer fabric 8 and the second sheet The plurality of faces 6 also has one or more single faces 23, each single face 23 being constituted by a single sheet 2. According to the arrangement of the adhesive strips 17, different configurations can then be obtained for the honeycomb structure. 4. Thus, in the embodiment illustrated in FIG. 6, in which the adhesive strips 17 bonding adjacent sheets 2 are alternated in the direction of longitudinal extension X, as can be seen in particular in FIG. 6A, FIG. stretching step 700 makes it possible to obtain a cellular honeycomb structure 4, with cells 5a, formed by the network of cells 5, e form substantially hexagonal. Each cell 5 comprises in this embodiment five faces 6, including four single faces 23 connected together in pairs by a double face 22. The cells 5a of the network formed by the cells 5 35 and have a prism shape comprising a base located in a plane perpendicular XZ to the direction of transverse extension Y, and extending in said direction of transverse extension Y. The cells 5a of the network formed by the cells 5 have in particular a form of hexagonal prism in the example Figures 1 and 2. Depending on the stretching distance, said hexagonal prism may be smooth or may be stretched or compressed in the sheet thickness direction Z.
    [0016] The faces 6 of the cells 5 may not be strictly plane faces but have a generally curved shape, in particular as the shape presented by the single faces 23 of the cell 5 of FIG. 7. Furthermore, the cell 5 comprises a corrugated portion 15 of the corrugated portion of the sheet 11, after the stretching step 700. The corrugated portion of the cell 12 can be located at an adhesive strip 17 joining two sheets 2, that is to say say at the level of a double face 22, as illustrated in FIG. 2. Alternatively, the corrugated portion of the cell 12 can be located outside the adhesive strips 17, on a single face 23 of the cell 5. This seventh stage of the process 700, may further include a firing of the honeycomb structure 4 to obtain a self-supporting honeycomb structure 26. Such firing of the honeycomb structure 4 can for example be achieved by heating at a temperature rature higher than a glass transition temperature of the polymer fabric 30 so as to melt and re-solidify said polymer fabric, at least partially. Following such cooking, the honeycombed structure 4 then adopts the stretched form as a form at rest. Advantageously, the firing of the honeycomb structure 4 makes it possible to detach the cellular structure 4, made self-supporting, from the drawing supports 30 and thus to simplify the subsequent steps of the process by increasing the purity and the quality of the core 1 obtained in FIG. final.
    [0017] During an eighth resin deposition step 800, illustrated in FIG. 6, the resin 3 is placed at least on the corrugated cell portion 12 of the cellular structure 4. For this, the cellular structure 4 is quenched, for example, in a resin bath 3.
    [0018] Then, during a ninth 900 crosslinking step, the resin 3 is crosslinked to obtain a resinous honeycomb structure 31. The crosslinking of the resin 3 can for example be carried out by heating, and makes it possible to harden the resin 3 disposed on the honeycomb structure 4. A resinous cellular structure 31 is thus obtained, comprising the honeycomb structure 4 on which the resin 3 is arranged and crosslinked so as to obtain the desired mechanical characteristics for the core 1.
    [0019] The eighth and ninth process steps 800, 900 may advantageously be repeated until a polymeric sandwich structural material core 1 of density within a predefined density range is obtained.
    [0020] A method for producing a sandwich structural material 50 will advantageously comprise a tenth step 1000 of adding skins, comprising the addition of an upper surface 27 and / or a lower surface 28 on the core 1, of so in particular to close the openings 30 of the cells 5 of the honeycomb structure. The upper surface 27 and the lower surface 28 thus constitute skins external to the core 1 making it possible to protect the openings of the cells 5 and thus to constitute a sandwich-resistant structural material 50.
    权利要求:
    Claims (12)
    [0001]
    REVENDICATIONS1. A method of making a core of polymeric sandwich structural material, comprising the steps of: - providing (100, 200, 300, 400), at least a first sheet of polymeric fabric (8) and a second sheet of polymeric fabric (9 ) extending substantially respectively in extension directions (X, Y), a sheet of first and second sheets having at least one corrugated portion of sheet (11) in a sheet thickness direction (Z) substantially perpendicular to the extension directions, one sheet of the first and second sheets having at least one adhesive strip (17), - superimposing (500) the first and second sheets in the sheet thickness direction to obtain a sandwich of sheets (7), - pressing (600) the sheet sandwich in the sheet thickness direction so that the sheets adhere to each other at the location of the adhesive strip, - stretching (700) the sandwich of leaves in the sheet thickness direction to form a honeycomb structure (4) having at least one cell (5), said cell being provided with a corrugated cell portion (12) on at least one face (6), - until a polymeric sandwich structural material core (1) is obtained with a density within a predefined density range, repeat the operations of: disposing (800) a resin (3) at least over the corrugated cell portion of the honeycomb structure (4; 31), and. cross-linking (900) the resin to obtain a resinous honeycomb structure (31).
    [0002]
    The method of claim 1, wherein the step of providing at least a first sheet of woven polymer (8) and a second sheet of polymeric fabric (9) comprises: - providing (100) a strip of polymeric fabric (15) ) extending substantially in directions of extension (X, Y), deforming (200) at least a portion of the polymeric web in a sheet thickness direction (Z) substantially perpendicular to the extension directions , so as to obtain a corrugated portion of strip (16), - arranging (300) at least one adhesive strip (17) on the strip of polymer fabric, - cutting (400) the strip to form at least a first and a second sheet of polymeric fabric (8, 9) extending substantially respectively in the extension directions, at least one sheet of the first and second sheets having the corrugated portion of the strip, at least one sheet of the first and the second second sheet featuring the band e adhesive. 20
    [0003]
    The method of any of claims 1 and 2, wherein the first and second polymeric fabric sheets (8, 9) respectively comprise a first corrugated portion of a sheet (24) and a second corrugated portion of a sheet (25). ) and in which the first and second sheets (8, 9) are superimposed (500) to obtain a sheet sandwich (7) so as to have the first and second corrugated portions of the sheet facing each other. the other.
    [0004]
    The method of any one of claims 1 to 3, wherein the step of pressing (600) the sheet sandwich (7) comprises heating the sheet sandwich to activate the adhesive strip (17).
    [0005]
    The method of any one of claims 1 to 4, wherein the step of stretching (700) the sheet sandwich (7) to form a honeycomb structure (4) comprises baking the honeycomb structure to a temperature above a glass transition temperature of the polymer fabric to obtain a self-supporting honeycomb structure (26).
    [0006]
    6. Method according to any one of claims 1 to 5, wherein to arrange (800) a resin (3) at least on the corrugated portion of cell (12) of the honeycomb structure (4; 26; 31) is quenched the honeycomb structure in a resin bath.
    [0007]
    A polymeric sandwich structural material core (1) extending substantially in core extension directions (X ', Y') and being intended to be between an upper surface (1a) and a lower surface (1b). ), opposite in a core thickness direction (Z '), said core comprising a resin honeycomb structure (31) having at least one cell (5), said honeycomb structure comprising a sheet sandwich (7), stretched according to a sheet thickness direction (Z), comprising at least a first sheet of polymeric fabric (8) and a second sheet of polymeric fabric (9) respectively extending substantially in directions of extension (X, Y), substantially perpendicular to the sheet thickness direction (Z), the first and second sheets (8, 9) adhering to each other at the location of at least one adhesive strip (17), resin (3) being arranged, and crosslinked, at least on said cell (5) of the honeycomb structure (4), the core being characterized in that one sheet of the first and second polymeric fabric sheets has at least one corrugated portion of sheet (11), deformed in the sheet thickness direction ( Z), in that said at least one cell is provided with a corrugated cell portion (12) on at least one face (6), and that the resin (3) is disposed, and reticulated, at least on the corrugated cell portion of the honeycomb structure.
    [0008]
    The core of claim 7, wherein a sheet of the first and second polymeric fabric sheets (8,
    [0009]
    9) has an adhesive tape (17) at a wavy portion of a sheet (11). A core according to any one of claims 7 and 8, wherein the corrugated portion of the sheet (11) and the corrugated portion of the cell (12) comprise a plurality of overlying patterns (14), each pattern overflowing with the corrugated portion of sheet (11) extending substantially out of the extension plane (XY) formed by the extension directions (X, Y). 15
    [0010]
    10. A core according to any one of claims 7 to 9, wherein the corrugated portion of sheet (11) has a general zigzag shape comprising at least two bumps.
    [0011]
    11. The core of claim 10, wherein said at least two bumps each have a peak apex.
    [0012]
    A sandwich structural material (50) comprising a core (1) according to any one of claims 7 to 11, as well as at least one outer skin (1a, 1b) attached to said core.
    类似技术:
    公开号 | 公开日 | 专利标题
    EP3094486B1|2017-11-22|Process for the preparation of a core of a polymeric structural sandwich material, said core and said material
    EP2370253B1|2020-10-14|Waved wood assembly and method of making same
    EP2420379B1|2019-11-13|Structure, molded article, and method for manufacturing same
    EP2265435B1|2013-08-14|Cell-like structure manufacturing method and corresponding equipment
    EP2639047B1|2014-10-01|Method for producing a curved profile made of composite material from a rectilinear preform of fibre layers
    FR2918134A1|2009-01-02|STRUCTURAL ROD IN COMPOSITE MATERIAL AND METHOD FOR PRODUCING A ROD IN COMPOSITE MATERIAL
    FR2990896A1|2013-11-29|METHOD FOR MANUFACTURING A REINFORCED EQUIPMENT PIECE, IN PARTICULAR FOR A MOTOR VEHICLE
    CA2835518A1|2012-11-15|Composite panel and process for producing same
    EP2723558B1|2015-06-24|Core of sheet structural material and assembly process
    FR3065669B1|2019-07-19|METHOD FOR MAKING A SOUL OF STRUCTURAL MATERIAL SANDWICH AND AME
    FR3024863A1|2016-02-19|METHOD FOR MAKING A GARMENT COMPONENT COMPRISING AN ASPECT LAYER COMPRISING BANDS OF WOVEN MATERIAL
    EP3233444B1|2019-07-31|Method for manufacturing a composite component with impressions in relief and composite component derived from such a method
    WO2013092326A1|2013-06-27|Tyre and method of manufacturing a tyre triangulation belt
    EP2969544B1|2017-05-03|Structural material core based on profiled elements, structural material and manufacturing method
    FR2990430A1|2013-11-15|METHOD FOR FORMING A GLASS SHEET AND MIRROR COMPRISING SUCH A GLASS SHEET
    FR2892340A1|2007-04-27|IMPROVED SANDWICH LAMINATE STRUCTURE
    WO2004110728A1|2004-12-23|Thermoplastic foil reinforced by unidirectional reinforcing elements and a production method
    KR20040026068A|2004-03-27|Honeycomb core , mold for honeycomb core and manufacturing method of honeycomb core
    WO2016087721A1|2016-06-09|Method for manufacturing an antenna reflector shell, in particular of a space vehicle
    WO2014199080A2|2014-12-18|Process for obtaining a non-planar peelable shim and non-planar peelable shim thus obtained
    EP0315926B1|1992-12-23|Process for transforming copper patterns on a parabolic support made of a composite material
    FR2989619A1|2013-10-25|METHOD FOR MAKING A CURVED PROFILE OF COMPOSITE MATERIAL FROM A RECTILINE PREFORM OF FIBER PATCHES
    WO1999041075A1|1999-08-19|Method for making laminated articles and laminated sheets obtained by using said method
    FR2965747A1|2012-04-13|METHOD FOR MANUFACTURING A STIFFENER IN COMPOSITE MATERIAL
    EP2014458A1|2009-01-14|Manufacture method of a honeycomb type panel, installation for its implementation and the panel obtained
    同族专利:
    公开号 | 公开日
    FR3016315B1|2016-02-05|
    US20160332410A1|2016-11-17|
    EP3094486A1|2016-11-23|
    EP3094486B1|2017-11-22|
    WO2015107295A1|2015-07-23|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    GB2058661A|1979-07-19|1981-04-15|Secr Defence|Honeycomb Structure|
    US5431980A|1993-02-01|1995-07-11|Mccarthy; Daniel J.|Formable cellular material with synclastic behavior|
    US5958549A|1993-05-28|1999-09-28|Tenneco Packaging Inc.|Prestressed honeycomb method and apparatus therefor|
    WO1995022668A1|1994-02-16|1995-08-24|Eldim, Inc.|Honeycomb structure having stiffening ribs and method and apparatus for making same|WO2018197786A1|2017-04-26|2018-11-01|SAS Engineering Composite 3D|Method for creating a core of a structural sandwich material, and core|
    US8539737B2|2008-09-19|2013-09-24|Ford Global Technologies, Llc|Twelve-cornered strengthening member|
    US10393315B2|2016-04-26|2019-08-27|Ford Global Technologies, Llc|Cellular structures with twelve-cornered cells|
    US10704638B2|2016-04-26|2020-07-07|Ford Global Technologies, Llc|Cellular structures with twelve-cornered cells|
    US10473177B2|2016-08-23|2019-11-12|Ford Global Technologies, Llc|Cellular structures with sixteen-cornered cells|
    US10220881B2|2016-08-26|2019-03-05|Ford Global Technologies, Llc|Cellular structures with fourteen-cornered cells|
    US10279842B2|2016-08-30|2019-05-07|Ford Global Technologies, Llc|Twenty-eight-cornered strengthening member for vehicles|
    US10300947B2|2016-08-30|2019-05-28|Ford Global Technologies, Llc|Twenty-eight-cornered strengthening member for vehicles|
    US10429006B2|2016-10-12|2019-10-01|Ford Global Technologies, Llc|Cellular structures with twelve-cornered cells|
    CN106696361B|2016-12-15|2019-01-25|中航复合材料有限责任公司|A kind of large scale aramid fiber paper honeycomb sizing correction unwheeling|
    法律状态:
    2015-01-27| PLFP| Fee payment|Year of fee payment: 2 |
    2016-01-28| PLFP| Fee payment|Year of fee payment: 3 |
    2016-12-28| PLFP| Fee payment|Year of fee payment: 4 |
    2017-12-20| PLFP| Fee payment|Year of fee payment: 5 |
    2019-01-22| PLFP| Fee payment|Year of fee payment: 6 |
    2020-02-03| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1450309A|FR3016315B1|2014-01-15|2014-01-15|METHOD FOR PRODUCING A SOUTH OF STRUCTURAL MATERIAL FOR POLYMER SANDWICH, SOUL AND MATERIAL|FR1450309A| FR3016315B1|2014-01-15|2014-01-15|METHOD FOR PRODUCING A SOUTH OF STRUCTURAL MATERIAL FOR POLYMER SANDWICH, SOUL AND MATERIAL|
    US15/111,845| US20160332410A1|2014-01-15|2015-01-14|Production method for a core of polymer sandwich structural material, core and material|
    EP15704048.6A| EP3094486B1|2014-01-15|2015-01-14|Process for the preparation of a core of a polymeric structural sandwich material, said core and said material|
    PCT/FR2015/050083| WO2015107295A1|2014-01-15|2015-01-14|Method for producing a web made of polymer sandwich structural material, web and material|
    [返回顶部]