Printing method and device, composite material

Abstract

The present invention relates to a method of printing a composite material (1), for example polymeric, carbonaceous, siliconic or metallic comprising steps of: i) providing a plurality of bundles (2) of reinforcement fibres (4), wherein the reinforcement fibres (4) have a length in the range 3-50 mm and are in the number of about 1,000-100,000 in each bundle (2); ii) aligning the bundles (2) along a predetermined path (X, X′); iii) incorporating at least part of the bundles (2) into a matrix (6, 8), for example polymeric, carbonaceous, siliconic or metallic, preserving the alignment along said path (X, X′); iv) laying and solidifying at least one layer (8) of the matrix (6, 8) of step iii) to make the composite material (1).

Claims

1. Method of printing a composite material, for example polymeric, carbonaceous, siliconic or metallic, comprising steps of: i) providing a plurality of bundles of reinforcement fibres, wherein the reinforcement fibres have a length in the range 3-50 mm and are in the number of about 1,000-100,000 in each bundle; ii) aligning the bundles along a predetermined path; iii) incorporating at least part of the bundles into a matrix, for example polymeric, carbonaceous, siliconic or metallic, preserving the alignment along said path; iv) laying and solidifying at least one layer of the matrix of step iii) to make the composite material.

2. Method according to claim 1, wherein the bundles comprise said number of reinforcement fibres side by side and joined into a single body.

3. Method according to claim 1, wherein step ii) comprises an alignment of the bundles by means of a mechanical force, e.g. by means of vibrations, and/or by means of an electric field, a magnetic field or electromagnetic field, applied to the bundles.

4. Method according to claim 1, wherein step i) comprises sub-steps of: a) feeding filaments of continuous reinforcement fibres; b) separating, for example by means of cutting, the plurality of bundles of said filaments.

5. Method according to claim 1, wherein step iv) comprises a sub-step of laying at least one layer of the matrix with a thread-like conformation.

6. Method according to claim 1, wherein step iv) comprises a sub-step of laying at least one layer of the matrix in the form of a tape or mat containing a plurality of bundles rows which extend longitudinally and substantially parallel to each other inside said tape or mat.

7. Method according to claim 1, wherein step iv) comprises at least one step of superposing a plurality of layers of the step iii) product to obtain a three-dimensional composite material in which such layers differ from each other in the concentration of bundles in the matrix, in the number and/or length of the reinforcement fibres inside at least one pair of layers and/or in the orientation of the predetermined paths, and thus of the bundles in the composite material.

8. Method according to claim 1, in which step iii) and step iv) are separated by a sufficiently short time to prevent the fragmentation of the bundles into reinforcement fibres loose from the respective bundle, for example randomly dispersed in the matrix.

9. Method according to claim 1, comprising a localised compression step of the step iii) product, upstream of the solidifying sub-step.

10. Method according to claim 1, wherein the matrix of step iii) is liquid, (semi-) liquid or a powder.

11. Method according to claim 1, wherein the bundles are at least partially made from carbon fibre, glass fibre, basalt fibre, polymer fibres such as kevlar, other known fibres for making composites, or combinations thereof.

12. Printing equipment of a composite material, for example to implement a method according to claim 1, comprising: supply means of a plurality of bundles of reinforcement fibres, wherein the reinforcement fibres have a length in the range 3-50 mm and are in the number of about 1,000-100,000 in each bundle; alignment means of the bundles along a predetermined path; means of feeding a liquid, semi-liquid or powder matrix, for example polymeric, carbonaceous, silicone or metallic, ending along the predetermined path to incorporate at least part of the bundles in said matrix, and configured to preserve the alignment of the bundles along said path; means of laying at least one layer of the matrix incorporating at least part of the bundles to make the composite material.

13. Printing apparatus according to claim 12, wherein the supply means, alignment means, feed means and laying means are integrated in at least one laying head of said equipment.

14. Printing equipment according to claim 12, wherein the supply means comprise cutting means—such as a rotating knife—to separate reinforcement filaments, grouped together in a plurality of bundles, said supply means being positioned upstream or downstream of the ending area of the feed means along the predetermined path.

15. Printing equipment according to claim 12, wherein the laying means or said laying head are fitted in an articulated manner to the supply means, around at least one axis of rotation, in particular through at least one connection joint interposed between said means.

16. Composite material, for example obtained using the method according to claim 1, comprising a plurality of bundles of reinforcement fibres, wherein the reinforcement fibres are of a length in range 3-50 mm and there are in a number of about 1,000-100,000 in each bundle, wherein the bundles are aligned along a predetermined path and are at least partially incorporated in a matrix, said matrix being laid and solidified in one or more layers to make said material.

17. Material according to claim 16, wherein the matrix is polymer, carbonaceous, siliconic or metal.

18. Material according to claim 16, comprising superposed layers of matrix deposited and solidified to obtain a three-dimensional composite material, wherein said layers differ in the concentration of bundles in the matrix, in the number and/or in length of reinforcement fibres inside at least a pair of layers and/or in the orientation of the predetermined paths and thus in the orientation of the bundles.

Description

[0035] The present invention will now be described with the aid of the accompanying drawings, in which:

[0036] FIGS. 1, 2, 3, 4 show longitudinal sections of nozzles that can be used in the present laying process, according to various embodiments;

[0037] FIGS. 5 and 6, 7 and 8, 9 and 10, 11 and 12 show in pairs, respectively, a top view of examples of filament according to the present invention and a cross section through the same filaments, along planes A-A, B-B, C-C, D-D, respectively, where the fibre bundles in different concentration with respect to the matrix are visible;

[0038] FIGS. 13, 14, 15 show a top view of a further example of filament according to the present invention, a cross section through the same filament along plane E-E in FIG. 13, and a corresponding perspective view, respectively;

[0039] FIG. 16 shows a schematic of an equipment designed to implement the method object of the present invention, according to a variant;

[0040] FIGS. 17, 18, 19 show a schematic of possible orientations of a laying head 100 according to the present invention, rotated—according to the arrangement shown—leftwards, downwards and rightwards, respectively, by virtue of the connection joint denoted by reference numeral 21.

[0041] The above object is achieved by a printing method of an article or composite material 1 comprising the steps of:

i) providing a plurality of bundles 2 of reinforcement fibres 4, having a length approximately in the range 3-50 mm, where the reinforcement fibres 4 are in the range of about 1,000-100,000 for each bundle 2;
ii) aligning bundles 2 along a predetermined path X, X′, such as straight and/or curved;
iii) incorporating at least part of bundles 2 in a matrix (for example polymeric, carbon, silicone or metal), preserving the alignment thereof along such a path, for example by laying nozzle 62;
iv) laying and solidifying at least one layer of matrix 6 and 8 of step iii) to make the composite material 1.

[0042] Preferably, bundles 2 of step iii) are fully incorporated into matrix 6 and 8, such as shown in FIGS. 6, 8, 10, 12, 14.

[0043] Advantageously, step ii) takes place before step iii), whereby the bundle alignment is “dry”, before the matrix wets the bundles and the respective fibres. In this regard, see for example the embodiment in FIG. 1 or FIG. 4.

[0044] In the feeding line of the bundles, before reaching the laying means 62 (and specifically the nozzle), an equipment 50 is provided in which the bundle of fibres are oriented in mutual alignment. The role of such equipment 50 therefore is to create a continuous series of aligned bundles. Purely by way of example, a vibrating channel of such equipment 50, specifically having a shrinking width shape may be part of the alignment means 56 of bundles 2, being particularly usable to create a string of fibre bundles.

[0045] A bundle or packet of fibres having a certain length coming from the alignment means 56 reaches the laying means 62. Separately, within the feeding means 58, 60, the polymer matrix is heated and maintained at a specific melting temperature, in which it is in liquid or semi-liquid form, before feeding the laying means, preferably by extrusion from a piston 70. The viscosity of the resin must be defined so as to be compatible from the rheological standpoint and suitable for the selected extrusion system.

[0046] Alternatively, equipment 50 may comprise feeding means 58, 60, 61 of different types, to feed more than one matrix to the article or composite material (FIG. 4). A piston heating unit may be charged with the heated matrix, and extruded to feed—such as directly—the laying means, specifically to a printing head thereof, optionally with a resin other than the one that at least partly incorporates the fibre chops.

[0047] In a variant of the present invention, the matrix filament extruded from the second nozzle may be pre-charged with powders or single ground fibres, for example of carbon. The ground fibre and the matrix, for example in the form of powder, could be loaded into a mixer, the mixture may then be heated in a heating unit and then extruded, feeding directly the laying means. The percentage by weight of ground carbon fibre reinforcement should preferably be kept in the range of 1% to 20% by weight.

[0048] According to a further variant, matrix 6, 8 of step iii) is a flowing phase, such as liquid or (semi-) liquid. The melting, and thus heating, temperature of the matrix is between 60 and 200° C.

[0049] According to a second variant, the matrix 6, 8 is a cross-linkable/solidifiable matrix.

[0050] According to an advantageous embodiment, bundles 2 comprise between 1,000 and 100,000 reinforcement fibres 4 side by side (preferably in a substantially parallel manner) and joined (for example mutually glued or welded), preferably in one piece.

[0051] According to a further embodiment, the reinforcement fibres 4 (and therefore also the corresponding bundles) have a length about in the range 3-50 mm or in the range 6-30 mm.

[0052] According to different variants, step i) may comprise an alignment of bundles 2 through a mechanical force, e.g. through vibrations or manual, applied to the bundles, and/or may comprise an alignment of bundles 2 through an electric field, a magnetic field or an electromagnetic field, applied to bundles 2 themselves.

[0053] As regards step i), this step may comprise sub-steps of: a) feeding filaments of continuous fibres 10; b) separating, for example through cutting operations, the plurality of bundles 2 from a filament of continuous fibres 10.

[0054] The cutting step in order to produce bundles or chops 2 may take place starting from filaments of continuous fibres prior to the step of alignment and addition of the matrices (FIG. 1) or in the vicinity of the extrusion nozzle after the addition of the matrices to the fibre filaments (FIG. 2). Separating of sub-step b), bundles 2 are still joined in longitudinal direction and constitute reinforcement filaments 10 mutually joined. Only at sub-step b), for example comprising a cutting operation, filaments 10 are transformed into bundles or chops since these filaments are cut into shorter fragments which form the above bundles or packets 2.

[0055] As regards the technical means to apply the above method, reference shall be made to the following description. According to an advantageous variant, such as shown in FIG. 5 or 6, or in FIG. 8 or 10, step iv) comprises a sub-step of laying at least one layer of matrix 6, 8 with a thread-like conformation.

[0056] For example, the section of the product laid in step iv) may be substantially circular or polygonal.

[0057] According to a further advantageous variant, such as outlined in FIG. 12 or 15, step iv) comprises a sub-step of laying at least one layer of matrix 6, 8 in the form of tape or mat containing a plurality of bundles 14 that develop longitudinally, and for example substantially parallel to each other, within such a tape or mat.

[0058] The shape of the array layer will therefore depend on the technological contingencies and on the destination or use of the material.

[0059] The variants shown in FIGS. 5 to 15 show the shape of the filaments or tapes that can be created from the equipment necessary to carry out the blending of bundles-matrix. The shape and size of the filament/tape produced (continuous two-dimensional element) can range from size a little larger than that of the selected bundle with the addition of the matrix required by the selected process and application (minimum diameter of about 0.2 mm) to large enough as to incorporate multiple bundles side by side (for example 100-200 bundles; 10 cm2 section), and shapes that can in this case be different (cylindrical, parallelepiped laminar) and functional to the additive process to be carried out and shape of the article or composite material being manufactured.

[0060] In any case, the different shape of the matrix could be obtained through an appropriate selection of a laying/extrusion chain or nozzle usable in step iv).

[0061] For example, step iv) may comprise at least one step of mutually superposing a plurality of layers of the step iii) product to obtain a three-dimensional composite material 1 in which said layers preferably differ from each other in the concentration of bundles 2 in matrix 6, 8, in the number and/or length of the reinforcement fibres 4 inside the chop and/or in the orientation of the predetermined paths X, X′, and thus in relation to the orientation of bundles 4 in the composite material 1.

[0062] According to this embodiment, the printing method therefore is a real three-dimensional printing method, or additive manufacturing method, of the composite material enriched with the bundles that improve the mechanical and/or thermal strength features thereof, resulting in unusual and unexpected geometries and technical features in the light of the current technical landscape.

[0063] In other words, the mechanical features of the article or composite material can be designed in order to make it perform better at the zones or directions along which the greater stress is expected.

[0064] According to a technologically important variant, step iii) and step iv) are separated by a sufficiently short time to prevent the fragmentation of bundles 2 into reinforcement fibres 4 loose from the respective bundle 2, for example randomly dispersed in matrix 6, 8.

[0065] In other words, since some matrices in flowing form could exert deleterious effects on the integrity of the bundles (e.g. mainly due to phenomena linked to the scrolling of the matrix itself or by virtue of their solvency disruptive power), it is preferable that the time between step iii) and step iv) is commensurate with the nature of the matrix. It is also recommended that the degrees of relative motion between the bundles of fibres and matrix are reduced. Optionally, the present method may also comprise a step of localized compression of the product from step iii), upstream of the solidification sub-step, for example in order to impart a semi-temporary track to this product will be consolidated during the solidification step.

[0066] The above object is also achieved by a printing equipment 50 of a composite material 1, for example to implement a method according to any of the preceding claims.

[0067] Such equipment 50 comprises: [0068] supply means 52, 54 of a plurality of bundles 2 [0069] alignment means 56 of bundles 2 along a predetermined path X, X′; [0070] means of feeding 58, 60 at least a liquid, semi-liquid or powder matrix 6, 8, for example polymeric, carbonaceous, silicone or metallic, ending along the predetermined path X, X′ to incorporate at least part of bundles 2 in such a matrix 6, 8, and configured to preserve the alignment of bundles 4 along such a path X, X′; [0071] means of laying 62 at least one layer of matrix 6, 8 incorporating at least part of bundles 2 to make the composite material 1.

[0072] According to a preferred variant, the supply means 52, 54, the alignment means 56, the feeding means 58, 60 and the deposition means 62 are integrated in a laying head 100 of such equipment.

[0073] Preferably, the supply means 54 comprise cutting means 64—such as a rotating knife or a sharp element that is movable with respect to the filaments of continuous fibres 10—for separating the reinforcement filaments 10—grouped together—in a plurality of bundles 2, such supply means being arranged upstream (FIG. 1) or downstream (FIG. 2) of the ending zone 66 of the feeding means 58, 60 along the predetermined path.

[0074] Alternatively, the supply means 52 may comprise a container containing bundles 4 dispersed in a suitable means for their transport.

[0075] According to a further variant, the laying means 62 or said laying head 100 may be fitted in an articulated manner to the supply means 52, 54, around at least one axis of rotation R1, in particular through at least one connection joint 21 interposed between said means 52, 54, 62. Preferably, the laying head 100 could be articulated around a plurality of mutually incident axes of rotation, such as mutually orthogonal.

[0076] Finally, the above object is achieved by a composite material 1 as described hereinafter.

[0077] Preferably, such a composite material is achieved through the method according to any one of the preceding embodiments. It follows that, even where this is not expressly stated, this material may comprise any preferred or accessory feature deductible—from a structural or process point of view—from the description above.

[0078] Such a material 1 comprises a plurality of bundles of reinforcement fibres 4, wherein the reinforcement fibres 4 have a length in the range 3-50 mm and are in the number equal to or larger than about 1,000-100,000 in each bundle. Such bundles 2 are aligned along a predetermined path X, X′ and are at least partially embedded in a matrix 6, 8, such a matrix 6, 8 being laid and solidified in at least one layer to achieve such a material 1.

[0079] According to a further variant, such a material includes a plurality of superimposed matrix layers, laid and solidified to obtain a three-dimensional composite material 1 having desired thickness and/or morphology.

[0080] Innovatively, the invention described is able to overcome the above drawbacks of the prior art.

[0081] More precisely, the method, equipment and material object of the present invention combine desirable mechanical properties of the finished product with the ability to produce through additive technique.

[0082] In addition, the method and the equipment described advantageously allow obtaining product geometries that, with the same strength, were believed impossible according to the prior art.

[0083] Advantageously, the method and the equipment object of the present invention allow superior mechanical features compared to the articles that can be obtained traditionally in three-dimensional printing.

[0084] Advantageously, the method, the equipment and the material object of the present invention allow obtaining products with orders of magnitude higher than other thermo-melting plastics, and nevertheless suitable for a 3D printing process.

[0085] Advantageously, the method, equipment and material object of the present invention allow manufacturing materials in any shape, including the most complex shapes, with virtually absent waste of raw materials.

[0086] Advantageously, the method, equipment and material object of the present invention allow positioning the layers of matrix with very high accuracy and precision.

[0087] Advantageously, the object of the present invention allows obtaining articles, for example polymeric, with a high resistance.

[0088] A man skilled in the art may make several changes or replacements of elements with other functionally equivalent ones to the embodiments of the above method, equipment and composite material in order to meet specific needs.

[0089] Also such variants are included within the scope of protection as defined by the following claims.

[0090] Moreover, each variant described as belonging to a possible embodiment may be implemented independently of the other variants described.