专利摘要:
Machine for adapting a fiber structure to a mold for the manufacture of composite parts. It comprises a solid matrix (1), a deformable body (2) attached to the surface said matrix (1); a forming mold (3); and a fastening system (5) of the fiber structure (4). The matrix (1) is a solid element that has a functional face whose geometry depends on the piece to be manufactured. The deformable body (2) has an initial geometry dependent on the geometry that it is desired to confer to the fiber structure (4). The forming mold (3) has the geometry that it is desired to confer to the fiber structure (4) in the adaptation process on the forming mold (3), and the forming mold (3) is positioned such that The deformable body (2) is located between said forming mold (3) and the matrix (1). (Machine-translation by Google Translate, not legally binding)
公开号:ES2734598A1
申请号:ES201830979
申请日:2018-10-10
公开日:2019-12-10
发明作者:Rodriguez Alejandro Abou-Assali;Tanarro Enrique Chacon;Gijosa Juan Manuel Munoz;Orellana Rafael Escobar
申请人:Aeon T Composite Tech S L;Universidad Politecnica de Madrid;
IPC主号:
专利说明:

[0001] ADAPTATION MACHINE OF A FIBER STRUCTURE TO A MOLD
[0002]
[0003] Object of the invention
[0004] The present invention relates to a system for adapting a fiber structure (carbon, aramid or glass are the most used industrially) to a three-dimensional mold, obtaining a fiber preform for the manufacture of composite parts.
[0005]
[0006] Technical Sector
[0007] Manufacturing processes of composites, manufacturing engineering.
[0008]
[0009] Background of the invention and technical problem to be solved
[0010] The automated and high productivity production of composite parts is based on a flat fiber structure (for example, carbon fiber, aramid or glass are the most used) aligned according to the main directions of loading. Said fibers can be in the form of a fabric or arranged in a single direction (unidirectional). After stacking as many layers as necessary, the fibers are adapted to the shape of the piece to be manufactured, a process that is called preforming. The preform obtained is then subjected to a resin infiltration process, in case the fibers are not previously impregnated with resin, and then the piece is cured by applying pressure and temperature.
[0011]
[0012] Among the wide variety of existing preforming processes, the most common in the industry is compression preforming due to its high degree of automation and productivity, in which the fibers are tensioned and introduced between two preformed molds, male and female, among which they are compressed by a press.
[0013]
[0014] During compression preforming the fibers are prone to defects such as wrinkles, alignment according to unwanted directions, deformation of the strands of the fabric, formation of loops, all due to the tension in the fibers during the process, to friction with the mold and the degree of complexity of the piece to be manufactured. These defects are especially serious if the fibers are previously impregnated with resin, known as prepregs, in which case the phenomena of Adhesion between layers and between fibers and mold are very pronounced, preventing proper sliding between layers and enhancing the defects mentioned. A piece of composite that has these defects in the alignment of the fibers, is compromised its mechanical resistance in the areas where this phenomenon occurs, forcing designers to reinforce the piece with a greater amount of fibers, which increases the production cost of said piece.
[0015]
[0016] The defects in the direction of the fibers are highly dependent on the complexity of the piece to be manufactured, tending to be reduced the more simple and flat the piece. That is, these defects force designers to subdivide complex parts into other simpler units that can be manufactured. This increase in the number of pieces is accompanied by a considerable increase in the cost of production, since each of the sub-elements requires its respective manufacturing line. Therefore, it is of great industrial interest the development of fiber adaptation processes that allow avoiding the aforementioned defects with complex geometry parts. A solution to this problem is presented in the present invention.
[0017]
[0018] Description of the Invention
[0019] The present invention describes a machine for adapting a structure of fibers to a mold, a process also known in the industry as preforming, for the manufacture of pieces of composite material, which considerably reduces the friction that acts on the fibers during the process, allowing even the adaptation of pre-impregnated resin fibers to complex molds, for which the current compression preforming processes are not suitable due to the appearance of defects in the fiber direction.
[0020]
[0021] Unlike the current compression preforming processes, in which the fabric is forced to acquire the shape of the piece being compressed between two rigid molds, in the present invention the fabric (fiber structure) is introduced between a rigid mold of shaped and an easily deformable body that has an initial shape that is not detailed and that depends on the geometry of the piece to be manufactured. By means of the controlled deformation of said deformable body on the fiber structure and the mold, the fibers are progressively compressed against said mold, adapting to it with a very low tension level, thus avoiding a large number of defects in the alignment of the fibers that are produced because of these tensions. Controlled deformation of the deformable body is achieved through two methods: either by giving motion to a matrix, or by a deformable body elastic with inner cavities that are filled with a fluid, causing controlled volume increases. It is important to note that the combination of the two methods is contemplated.
[0022]
[0023] The machine comprises at least the following elements: a die, a deformable body, a forming mold and a fiber fastening system.
[0024]
[0025] The matrix is a solid element similar to a mold, and has a geometry that is not detailed, and that depends on the shape that is desired to give the fiber structure. Its function is to support the deformable body that is attached to said matrix on one of its faces.
[0026]
[0027] The forming mold, which has the shape to be conferred to the fiber structure, is positioned so that the deformable body is located between the matrix and said mold.
[0028]
[0029] The fiber structure is formed by at least one layer of fibers, which can be presented in any configuration, such as a unidirectional or tissue-shaped arrangement, and whose orientations are those required for the piece in question depending on its conditions of load. The fibers may be previously impregnated with resin, material known as "prepreg", or lacking it, referred to as "dry fibers".
[0030]
[0031] If the fiber adaptation process requires it, the layers can be joined together completely or in specific areas thereof, by applying adhesives or being sewn. The objective of this union is to transmit the tension generated by a clamping element of the clamping system to the layers that require it. In the case of fibers already impregnated with resin, it is possible to take advantage of the resin's own adhesion to join two consecutive layers, applying pressure in specific areas or simply by the effect of gravity. Thanks to the latter, it is possible to simplify the required machinery since the need to implement additional processes such as sewing or the addition of adhesives is eliminated. In addition, it is possible to suppress the costly resin injection systems associated with the use of dry preforms, which are also prone to failures in the piece such as resin deposits, bubbles, porosities or delaminations on the front of the resin.
[0032] The fiber structure adaptation machine object of the present invention allows to optimize the size of the fiber layers, some of them not being able to cover the total area of the fiber structure corresponding to the complete preform. In this way, the amount of fiber used is reduced, thus reducing the cost associated with each piece and allowing to reinforce certain areas of said piece with a greater number of layers arranged according to the necessary orientation. In this aspect, there are similarities with the invention WO 2015144411, which shows a fiber stacking process in which it is also not necessary for each layer to cover the total area of the preform, also reducing the amount of fibers needed to optimize the size and layer position. However, in said process the layers are stacked and attached to a substrate that is responsible for transmitting the tension to the fibers. Said substrate does not exist in the present invention, that is, the layers can be joined together or simply stacked without executing any bond between them.
[0033]
[0034] The fastening system, according to claim 1, has the function of fastening the fiber structure, allowing said fiber structure to be positioned in the preforming station and at the same time providing them with the necessary tension during the adaptation process, allowing each layer slide relatively to each other when they require it. The fastening system is formed by at least one fastening element comprising: a lower frame, separation sheets, an upper frame, a hook system between the lower frame, sheets and upper frame, and a closing system.
[0035]
[0036] The lower frame and the upper or closing frame are the structural elements of the fastening system between which it is attached to the fibers, and can be made of any material, sheet steel, aluminum, plastics, etc, and are the responsible for applying pressure on the structure of fibers that are placed between them as a "sandwich." It is contemplated that these elements have anchors or joining elements that are necessary for handling, transfer or storage that are not detailed.
[0037]
[0038] The separation sheets are the only elements that are in contact with the fiber structure and cover an area greater than or equal to the effective fastening area, that is, the area of the fiber structure that is covered by the fastening system of fibers at the initial moment of the adaptation process. According to claim 17, said sheets can be made of any flexible material, preferably plastics, and are coated with a medium. non-stick, such as Teflon or certain silicones, to allow the sliding of several layers of the fiber structure. Alternatively, they can be manufactured entirely with said non-stick material.
[0039]
[0040] To ensure a homogeneous distribution of the pressure on the fiber structure, according to claim 16, the placement of an elastic element, of the thickness that is necessary, such as flexible PVC foam, is contemplated on the surface of both frames, specifically on the face adjacent to the separation sheets, covering an area greater than or equal to the effective area of attachment. It is also contemplated that the various layers of the fiber structure may protrude from the fastener in areas that require it, for example, because the geometry of the forming mold to which it is desired to adapt the fiber structure requires a considerable amount of the fibers.
[0041]
[0042] The coupling system is necessary to avoid relative sliding between the lower, upper frames and the sheets according to their plane, and to allow the clamping effect, and it can be any geometric coupling system, such as pins or hinge mechanisms that link said elements. Also contemplated are mixed solutions formed by pins and hinge mechanisms, such as pins that link the lower frame and the sheets, and a hinge mechanism that joins the upper and lower frames. It is also possible to connect the upper frame and the sheets to the lower frame by means of hinge mechanisms.
[0043]
[0044] A concrete solution of the pin-based hitching system is that indicated in claim 20, which comprises a cylindrical pin integral to the lower frame and which crosses the sheets and the upper frame by means of custom holes, resulting in displacement according to the normal to the level of the elements as the only degree of relative freedom.
[0045]
[0046] The closure system applies a regulated force between the upper frame and the lower frame, with which the layers of the fiber structure are compressed, and prevents said elements from disengaging. Said closing system can be any mechanical, magnetic or electromechanical element such as for example calipers, magnets, pneumatic or hydraulic cylinders, servomotors or any other existing system, which allows to regulate the closing force and prevent the elements of the fastening system from being disassembled. accidentally.
[0047] An example of a closure system is the element that is fixed to the cylinder by means of a mechanical joint, and which has a spring, which is not detailed, in the part where it contacts the upper frame. This system is not detailed since it would not bring novelty or inventive activity given the wide variety of solutions available in the market.
[0048]
[0049] Another example of a closing system, in the event that the hitch system between the upper frame and lower frame is composed of hinges, is a rotary actuator integrated in said hinge that displaces said frames according to their degree of freedom of rotation as a "gripper".
[0050]
[0051] It should be noted that the fastening tools or anchors that each fastening element can possess in its corresponding lower frame and / or upper frame serve to store, transport, or manipulate, preferably by means of a robotic system, and with the help of a tool that does not It is detailed, all the fasteners at the same time, which together form the complete fiber restraint system.
[0052]
[0053] It is important to note that the fiber fastening system that is presented as part of this invention, is characterized by directly fastening the fibers that will be part of the preform, as opposed to the aforementioned invention WO 2015144411, in whose system it is fastened only a substrate on which the different layers of fibers are attached.
[0054]
[0055] Said fastening system is further characterized by fully or partially encompassing the contour of the fiber structure.
[0056]
[0057] It should be noted that the characteristics of the fastening system allow it to be stored together with the fiber structure at an intermediate stage of production if required.
[0058]
[0059] The operation of the present invention consists in adapting the fiber structure by progressive and controlled deformation of the deformable body against said fiber structure and the mold, forcing said fiber structure to take the form of said mold. Thanks to the progressive adaptation, it is possible to greatly reduce the tension between layers with respect to current compression preforming processes, allowing a relative sliding between them thanks to the fiber clamping system, since the blockage produced when the fibers enter in contact with the mold before reaching its correct position in it, thus eliminating the failures in the alignment of the fibers that this effect generated. The improvement is even more noticeable in the case of preimpregnated fibers, in which the aforementioned blocking effect is of such magnitude in current processes that it prevents even the formation of simple geometries.
[0060]
[0061] In the preferred embodiment of the invention, and according to claim 1, to achieve the progressive and controlled deformation of the deformable body, the matrix has the ability to move towards the mold, preferably by means of a press, compressing said deformable body against the fiber structure and forcing the latter to take the form of said mold.
[0062]
[0063] Said matrix can be formed by one or more elements that move according to a mechanism that can be formed by various elements such as joints, linear guides, springs, and which is actuated by at least one actuator, preferably a hydraulic cylinder. The objective of said mechanism is to provide a particular movement to each element of the matrix that exerts pressure on the deformable body, giving the system greater control over the deformable body path and, therefore, on the adaptation of the fiber structure. In an embodiment of the invention, the mechanism is operated only by a hydraulic cylinder and has joints and a spring that restrict the movement of the elements of the die. Such elements may also have independent movements and be displaced by hydraulic cylinders.
[0064]
[0065] It is important to note that a combination of the solutions is also contemplated, some of the elements of the matrix being able to have their independent action system, and the rest of the elements being united by means of a mechanism.
[0066]
[0067] In the preferred embodiment of the invention, the deformable body is a low strength material, such as wet clay, which is easily deformed by plastic deformation or creep processes, that is, once deformed and after the pressure ceases, the body deformable does not recover its initial form, as set out in claim 2. The sequence of plastic deformation of this type of materials and which is claimed in this embodiment of the invention is of vital importance when adapting the fibers without causing misalignments in them, allowing a greater degree of adaptation control.
[0068] This initial form, which is not detailed since it depends on the shape of the piece to be adapted, is of great importance for the process.
[0069]
[0070] In this case, the machine additionally requires a system for restoring the initial geometry of said deformable body, so that it is possible to repeat the process cyclically and be suitable for series production. Otherwise the invention would be of no interest for industrial production. Said restoration system comprises an additional mold that has the initial shape that it is desired to confer to the deformable body, and that is pushed and pressed against the matrix by means of a press, said deformable body remaining between these latter elements, being therefore obliged to fill the existing cavity between matrix and said additional restoration mold. So that the deformable body is attached to the matrix, and not to the additional restoration mold, once the conformation of said deformable body is finished, the use of different surface textures in the additional restoration mold and matrix is contemplated, so that the adhesion of the deformable body to said matrix is greater than the adhesion between said deformable body and said additional restoration mold, as described in claim 8. By means of the additional mold the deformable body is forced to acquire its initial shape so that can be reused to adapt a new fiber structure.
[0071]
[0072] Another strategy contemplated, and which is reflected in claim 9, is the introduction of an elastic film between the deformable body and said additional restoration mold. Said elastic film may be integral with said additional restoration mold or be introduced between it and said deformable body independently by means of a fastener.
[0073]
[0074] In a first embodiment of the invention, the film fixing system is integral with the additional restoration mold; in a second embodiment of the invention the film fixing system is integral with the matrix; and in a third embodiment of the invention the film fixing system is an independent system configured to move relatively with respect to the additional mold and with respect to the matrix.
[0075]
[0076] To control the volume of the deformable body during the restoration of its geometry and prevent the material from overflowing, an elastic joint capable of suffering large deformations is used; wherein said elastic seal is located on the contour of the restoration mold, so that when the die is pressed against said mold, the seal prevents the material from leaving the molding area, which would modify the volume of deformable material available for the following adaptation, preventing the correct automated operation of the invention. Said elastic joint may contain local or global reinforcements or have different sections.
[0077]
[0078] The elastic seal is deformable and can be located on the restoration mold, as described in claim 13, or be linked to the die as described in claim 14, in which case said elastic seal has a skirt towards the inside of the matrix that is in contact with the deformable material and that serves as an additional barrier to prevent the material from leaving the volume contained between the restoration mold and the matrix.
[0079]
[0080] To achieve the evacuation of the air that is enclosed between the matrix, the restoration mold and the deformable material, the film separating the deformable material from the restoration mold has small perforations through which air can flow but not the deformable material. In addition, the restoration mold has a porous surface or with holes connected to the outside, thus allowing the total evacuation of the air.
[0081]
[0082] In the main embodiment of the invention, the fiber fastening system must have, according to claim 2, an elastic film that separates the fiber structure from the deformable body during adaptation, to avoid contamination of said fiber structure. Said elastic film can be an external element to the fiber fastening system, which is simply placed between the deformable body and the fiber structure during adaptation; where said elastic film can be fixed to the die or to the forming mold.
[0083]
[0084] Said elastic film can also be attached to the fastening system by means of anchoring to the upper frame, the lower frame or to both elements by means of a fixing system such as tweezers. The film can also be placed between the mold and the fiber structure, in case of needing to separate the aforementioned elements, since the fiber structure, if found pre-impregnated, can have an excessive adhesion to the forming mold that would make removal difficult of said fiber structure once adapted.
[0085]
[0086] In another embodiment of the invention, it is contemplated that the deformable body according to claim 3 is a body that deforms elastically without reaching plasticity or creep, such as an elastomer, recovering its original shape upon cessation. the pressure exerted by the matrix, and inside which there is a hollow structure of cavities or ducts connected or not connected to each other, porosities or any combination of the above, filled with a gas or a liquid. Said fluid is enclosed as there is no escape route. Through the proper design of the internal structure and its external shape, it is possible to control the deformation paths that said deformable body will present when compressed due to the displacement of the matrix that is configured to move towards the mold.
[0087]
[0088] In another embodiment of the invention, according to claim 4, to achieve progressive and controlled deformation of the deformable body, said body is a material that elastically deforms without reaching plasticity or creep, such as an elastomer, and in which Inside there is a structure of cavities or ducts connected or not connected to each other, porosities or any combination of the above, filled with a gas or a liquid. Said fluid can enter or exit to the outside by at least one conduit connected to an external pumping system, which can be located inside the die or directed directly outside from the deformable body. By means of the injection of the fluid, the deformable body increases its volume following a concrete deformation path depending on its design, thereby achieving the progressive adaptation of the fiber structure to the forming mold.
[0089]
[0090] It is also contemplated that the matrix is formed by one or more elements that move according to a mechanism that can be formed by various elements such as joints, linear guides, springs, and that is actuated by at least one actuator, preferably a hydraulic cylinder . The objective of the actuator is to provide a particular movement to each element of the matrix, which exert pressure on the deformable body, giving the system greater control over the deformable body path and, therefore, on the adaptation of the fiber structure.
[0091]
[0092] In an embodiment of the invention, said actuator is operated only by a hydraulic cylinder, and has joints and a spring that restrict the movement of the elements that make up the die. Such elements may also have independent movements and be displaced by hydraulic cylinders.
[0093]
[0094] It is important to note that a combination of several described solutions is also contemplated, some of the elements of the matrix being able to have their independent actuation system, and the rest of the elements of the matrix being united by means of a certain mechanism.
[0095] The fiber structure is located between the deformable body and the mold, and is formed by at least one layer of fibers, where the fibers and the fiber layers can be joined together by adhesives or sewing processes, and which may contain inserts and core pieces such as polymer foam, cork, wood or metal.
[0096]
[0097] The pieces that make up the matrix can be coupled by some kind of intermediate mechanism such as joints, linear guides, springs, etc., or each have independent movement being actuated by their respective mechanical actuators, such as a hydraulic cylinder.
[0098]
[0099] In all embodiments of the invention, it is contemplated that the fiber fasteners are secured by a system comprising: a flexible arm, a rigid support and a displacement mechanism.
[0100]
[0101] The fiber holding element is attached to the flexible arm which is in turn anchored at its other end to a mobile element of the movement mechanism. Said arm is flexible enough to bend due to the tension of the fibers, so that the clamping element aligns with said tension, reducing the risk of tearing of the fibers at the end of the clamping element.
[0102]
[0103] To avoid deflection of the assembly formed by the fibers, the clamping element and the flexible arm, the rigid support is placed under said flexible arm, where said support is anchored to the same mobile element of the movement mechanism as said flexible arm, that is, one end of the flexible arm and the rigid support are integral.
[0104] The movement mechanism has the function of moving the set of fibers according to the direction required by the adaptation process, predominantly the vertical direction, that is, the direction of movement of the matrix; wherein said displacement mechanism can be operated by an independent automated element, or by a pusher coupled to the die, so that the movements of the die and the mobile element of the displacement mechanism are coupled.
[0105]
[0106] Brief description of the drawings
[0107] Figure 1 shows a plan view of a fiber structure with the fiber fastening system according to claim 1.
[0108]
[0109] Figure 2 shows a sectional view of the adaptation system at the initial moments of the adaptation phase according to claim 2.
[0110]
[0111] Figure 3 shows a sectional view of the adaptation system at an intermediate point of the adaptation phase according to claim 2.
[0112]
[0113] Figure 4 is similar to Figure 2, showing different characteristics in the deformable body according to claim 3.
[0114]
[0115] Figure 5 is similar to Figure 4, showing another deformation method of the deformable body according to claim 4.
[0116]
[0117] Figure 6 is similar to Figure 2, showing a matrix formed by different elements with independent movement.
[0118]
[0119] Figure 7 is similar to Figure 6, showing a system of cavities or pores in the deformable body.
[0120]
[0121] Figure 8 is similar to Figure 3, showing a matrix formed by different articulated elements actuated by a single actuator.
[0122]
[0123] Figure 9 is similar to Figure 8, showing different characteristics in the deformable body, according to claim 3.
[0124]
[0125] Figure 10 shows a sectional view of the adaptation machine at the final moment of adaptation according to the preferred embodiment of the invention.
[0126]
[0127] Figure 11 shows a diagram of the complete process of obtaining an adapted piece of fibers.
[0128]
[0129] A diagram of the restoration system integrated in the fiber adaptation machine according to claims 5 and 6 is shown in Figure 12.
[0130] A plan view of a fiber structure fastened by a fiber fastening system according to claim 1 is shown in Figure 13.
[0131]
[0132] Figure 14-14 shows a section 14-14 of an element of the fiber fastening system according to Figure 13.
[0133]
[0134] Figure 15-15 shows a section of an element of the fiber fastening system according to Figure 13.
[0135]
[0136] Figure 16 is similar to Figure 14, showing the independent sliding that has taken place in the fiber layers during adaptation.
[0137]
[0138] Figure 17 is similar to Figure 14, showing in this case the elastic film and a fixing system.
[0139]
[0140] Figure 18 shows a perspective view of a fastener that is part of the fiber restraint system.
[0141]
[0142] A diagram of the automated assembly of the fiber restraint system is shown in Figure 19.
[0143]
[0144] A section of the elements of the system for restoring the deformable body geometry according to claim 14 is shown in Figure 20.
[0145]
[0146] Figure 21 is similar to Figure 20, in this case showing a joint integral with the die, according to claim 15.
[0147]
[0148] Figure 22 is similar to Figure 20, in this case showing a section during compression of the deformable body on an additional mold.
[0149]
[0150] Figure 23 shows a sectional view of a fastening and guiding apparatus of elements of the fiber restraint system.
[0151]
[0152] Figures 24A and 24B show possible embodiments of the hitch system linked to the fiber restraint system.
[0153]
[0154] Detailed description of examples of embodiments of the invention.
[0155] Figure 1 shows a plan view of a fiber structure (4) according to claim 1 that will subsequently be shaped or adapted to the three-dimensional mold (3), and that is formed by a series of layers (13) of different geometry and oriented according to the loading paths of the corresponding composite part. The layers (13) can be partially or totally joined together by sewing or using adhesives. In case of using pre-impregnated resin fibers, or prepregs, it is possible to take advantage of the adhesion generated by the resin itself to join said layers.
[0156]
[0157] The objective of this union is to transmit the tension generated by the fiber clamping system (5) to the areas of the fiber structure (4) that require it, otherwise it may not make any connection between the layers (13 ). Said fastening system (5), shown in detail in Figures 13-19, at least partially covers the contour of the fiber structure (4), and allows the sliding of the fibers where required, for example. in areas where due to a more abrupt geometry, a greater amount of fibers is needed. The fastening system (5) of fibers has in each of its elements (42) anchor points that are not detailed, which allow, by means of a tooling prepared for this purpose, all those elements (42) are held at the same time , preferably by means of a robot, to be moved to the necessary positions, either in a vacuum, or with the fibers (4) attached.
[0158] For example, to be moved from the mounting area (19) of the fastening system (5), which is detailed in Figure 19, to the adaptation zone (20), specifically between the die (1) and the mold shaped (3).
[0159]
[0160] In addition, the concept of restraint system (5) presented, allows the intermediate storage of the same already mounted with the fibers (4), before being taken to the adaptation zone (20), allowing to absorb the productive inequalities of the manufacturing phases
[0161]
[0162] It is important to note that, the design of said fastening system (5) mounted with the fibers (4) allows, after being installed between the die (1) and the forming mold (3), that each element (42) has a independent movement during the adaptation of the fibers, thus being able to facilitate said adaptation in pieces of complex geometry. This independent guidance system is not detailed since it can be achieved through a variety of existing solutions in the market, such as robotic arms.
[0163] Figure 2 shows a sectional view of the adaptation machine according to the second claim, specifically in the initial moments of the fiber adaptation phase. The system consists of a matrix (1) that can have different shapes, on whose surface an easily deformable body (2) is attached, which has a certain initial geometry and depends on the shape of the piece to be manufactured. The mold (3) is positioned such that the deformable body is between said mold (3) and the matrix (1).
[0164]
[0165] After positioning the fiber structure (4) supported by the fiber clamping system (5) between the deformable body (2) and the mold (3), the matrix (1) is moved towards the mold with a certain speed , according to claim 2a, preferably with the help of a press, so that the deformable body is compressed against the mold (3), forcing the fiber structure (4) to gradually adopt the shape thereof, which allows the reduction of the tension between layers, avoiding the appearance of misalignment or wrinkles in the fibers (4) and making it possible to obtain preforms from preimpregnated resin fibers.
[0166]
[0167] During the adaptation of the fibers (4) that are initially arranged in a two-dimensional plane, the fiber (4) slides with respect to the fasteners (42) as they take a three-dimensional shape.
[0168] It is important to note that it is contemplated that the fasteners (42) have independent movement and according to the degrees of freedom that the adaptation of the fibers (4) requires. That is, said elements (42) could remain immobile throughout the process, move freely according to certain degrees of freedom, have forced movement according to said degrees of freedom, or a combination of the above.
[0169]
[0170] Figure 3 is similar to Figure 2, showing in this case the adaptation phase in a more advanced state, in which the fiber structure (4) has already partially taken the form of the mold (3). It should be noted that, in the example shown, the fiber clamping system (5) maintains the necessary tension but at the same time allows them to slide.
[0171]
[0172] Figure 4 is similar to Figure 2, showing the deformable body (2) different features, according to claim 3a, said body (2) being deformed elastically, without reaching plasticity or creep, and having cavities, ducts, porosities or any combination of the above (6), and which contains inside a gas or a enclosed liquid By an appropriate design of said cavities (6), the body is deformed according to the optimal sequence for the adaptation of the fiber structure (4). Note that the adaptation effect is the same as in the case of Figures 2 and 3, and that the difference is the deformation phenomena that take place.
[0173]
[0174] Figure 5 shows a sectional view of the adaptation machine according to claim 4a, wherein the deformable body (2) is made of an elastic material, which deforms without reaching plasticity or creep, and that has cavities, ducts, porosities or any combination of the above (6), and that contains inside a gas or a liquid connected to the outside through at least one duct (7).
[0175]
[0176] In this case, instead of moving the matrix (1) towards the mold (3) to achieve adaptation, a gas or a liquid is injected through at least one conduit (7) inside the deformable body (2) causing an increase in volume in it. By proper design of said cavities (6) the deformation sequence can be controlled to produce the desired adaptation.
[0177]
[0178] Figure 6 is similar to Figure 2, showing in this case, as contemplated in claim 25a, a matrix (1) divided into several elements (8) that are independently displaced by mechanical actuators, preferably hydraulic cylinders (9), describing what is stated in the 2nd claim. This achieves greater control of the deformation sequence, allowing more complex mold geometries to be adapted.
[0179]
[0180] Figure 7 is similar to Figure 6, showing in this case a deformable body (2) according to claim 3a, which deforms elastically, without reaching plasticity or creep, and which has cavities, ducts, porosities or any combination of the above (6), and that contains inside a gas or a liquid enclosed.
[0181]
[0182] Figure 8 is similar to Figure 3, showing in this case a matrix (1) divided into several elements (8) joined by any mechanism (10), set forth in the 26th claim, which is actuated by a mechanical actuator, preferably a hydraulic cylinder (9). This figure shows an example of a mechanism (10) containing joints (11) and a spring (12), through which it is possible that the whole system works with a single actuator (9).
[0183] Figure 9 is similar to Figure 8, showing in this case a deformable body (2) elastic or viscoelastic that has cavities, ducts, porosities or any combination of the above (6), according to the 3rd claim, and which contains in its inside a gas or a liquid enclosed. By an appropriate design of said cavities (6), the body is deformed according to the optimal sequence for the adaptation of the fiber structure (4).
[0184]
[0185] Figure 10 shows a sectional view of the machine object of the present invention, at the time of having completed the adaptation of the fibers, specifically after the moment indicated in Figure 3. In this case, the die (1) is raised returning to its initial position and releasing the preformed fibers (4). It should be noted, as mentioned in the claim, that the fastening system (5) of the fibers allows them to slide in the areas where it is necessary, being able to detach (14B) from said fastening system ( 5) at the appropriate time, where the tension of the fibers is no longer required, or on the contrary, remain subject to the system (14A) until the end of the adaptation process.
[0186]
[0187] In the case shown in the present figure 10, the deformable body (2) is a material that deforms plastically and does not recover its initial geometry when the pressure ceases, according to claim 2a. It is therefore necessary to reshape said deformable body (2) to confer its initial shape. That is why it is contemplated that the machine additionally comprises an additional restoration mold (24), as expressed in claim 5a.
[0188]
[0189] Figure 11 shows a diagram of the process of obtaining the fiber preform, in which the machine exposed in the present invention is integrated, which corresponds in this case to the zones (18) (19) and (20).
[0190]
[0191] The zone (17) corresponds to the obtaining of the fiber pieces (13), by means of already existing processes such as the cut by numerical control (15) or automated fiber deposition systems (16), or AFP.
[0192]
[0193] Next, the zone (18) corresponds to the preparation of the fiber layers (13) or layers, through an automated positioning system, such as the robot (21).
[0194] Within this space (18), the realization of joining processes between the layers that require it, such as sewing, the addition of an adhesive, or the application of pressure between two or more layers (13) is also contemplated. in the case of preimpregnated resin. Additionally, pieces of core material can be introduced for composites such as polymer foams, cork, wood or metal, and inserts of different materials. It is important to note that the aforementioned additional processes that may take place during step (18) can be performed in different positions within the production line, and are executed by automated tools such as robots (39).
[0195]
[0196] In the following area (19), the fiber structure (4) is fixed in the fiber fastening system (5), which is detailed in Figure 19, where the layers (13) are stacked and enclosed between the sheets (30) of the fastening system, and can be previously stacked, sewn, with core material or presented individually. It is important to note that in the case of being presented individually, that is, without additional sewing operations, insertion of the core or glue, the layers (13) can come directly from the area (17) for obtaining said layers.
[0197]
[0198] As for the subject, note that it covers at least partially the contour of said layers (13).
[0199]
[0200] In the area (20), corresponding to the adaptation, are the forming mold (3) and the matrix (1) together with the deformable body (2), where the fastening system (5) is positioned, once been mounted together with the fibers (4) in the area (19). The positioning of said fastening system (5) together with the fibers (4) is preferably carried out by means of a robot (22) which has a tool that holds each of the elements (42) of the fastening system.
[0201]
[0202] The additional mold (24) for restoring the initial shape of the deformable body (2) is not detailed in the present figure.
[0203]
[0204] Figure 12 shows a scheme of the restoration system that is part of the fiber adaptation machine object of the present invention, in which fiber adaptation and restoration are carried out in the same place (20), and by means of the same press (23), according to the 6th claim, wherein it is stated that the mold (3) and the additional mold (24) for restoration have a movement system (27) that Allows them to align alternately with the matrix (1). Note that when the additional restoration mold (24) is aligned with said matrix (1), in the press (23), the forming mold (3) moves to another position (26) in which a robot is expected collecting the adapted fibers (4), and positioning, on said forming mold (3), new fibers by means of the fastening system (5) proposed in the present invention.
[0205]
[0206] This figure shows the operation of the machine at the moment when the fiber structure (4) has already taken the required form and the additional restoration mold begins its displacement towards its position in alignment with the die (1) at the same time in which the forming mold (3) moves towards the area (26).
[0207]
[0208] Once said additional restoration mold (24) has been positioned in alignment with the die (1), the deformable body (2) is compressed between the elements (1) and (24) by means of the press (23). recover the shape of said deformable body (2).
[0209]
[0210] It is important to note that the restoration is also expected to be carried out in a place other than that of fiber adaptation (20), in which case, as set forth in claim 7a, the matrix (1) has a system that allows it to disengage from the press. (23) to be moved to the position occupied by the additional restoration mold (24).
[0211]
[0212] Figure 13 shows a partial plan view showing two elements (42) that are part of the fiber fastening system (5). The fiber structure (4) is fastened in those areas where necessary by at least one element (42), which have a closure system (28) that acts at least one point of each element (42). Alternatively, other types of closure are contemplated, such as pliers, pins or threads. The upper or closing frame (31) is the element that gives consistency to the fastening system together with the lower frame (29) located below, so it is not visualized in the present figure.
[0213]
[0214] Figure 14 shows a sectional view of section 14-14, indicated in Figure 13, of an element (42) of the fiber fastening system. It shows the lower frame (29) that, together with the upper or closing frame (31) provide consistency to the fastening system, and can be manufactured based on any material, according to the requirements of each preform, for example sheet aluminum, steel, or a material polymeric Between both frames (29) and (31), separation sheets (30) are placed on both sides of each fiber layer (13). Said sheets (30) are preferably made of a flexible material coated with a non-stick medium, such as Teflon or non-stick silicone, to allow the fiber layers to slide. Alternatively they can be manufactured directly based on said non-stick material.
[0215]
[0216] Between each of the frames (29) and (31) and the adjacent separation sheets (30) an elastic element (32) is placed, such as a flexible polymer foam or an elastomer, covering a larger area (37) or equal to the effective fastening area (36), that is, the region of the fibers (13) that is covered by the fastener (42) at the initial instant of the preforming. Said flexible material (32) envelops the fibers (13) and its objective is to distribute the pressure exerted by the frames on the fibers (13) in a homogeneous manner, thus avoiding pressure concentrations that can cause distortions in the fiber directions ( 13) when sliding with respect to the sheets (30) due to excessive frictional force.
[0217]
[0218] To ensure the consistency of each fastener (42), a hook system is placed so that the lower frame (29), the separation sheets (30) and the upper or closing frame (31) do not have relative displacement relative to to your plane This hooking system is, according to the present figure, a hooking element (33) (cylindrical pin) integral with the lower frame (29) and which crosses the custom holes located in the sheets (30) and the upper frame (31) , so that the only allowed movement of the elements with each other is according to the normal to the plane of the fibers.
[0219]
[0220] Additionally, the closure (28) of the fastening system is located, whose objective is to exert adequate pressure on the fibers (13) in order to generate the necessary tension in the fibers by friction phenomena. In the present figure, said closure (28) is an element in which the coupling element (33) is inserted, being retained relative to each other, for example by means of a threaded joint, a pin, etc. In this way the closure (28) exerts the required force on the upper or closing frame (31).
[0221] It is important to note that it is planned that the lower (29) and upper (30) frames have anchoring elements that are not detailed, and that are used for fixing them in the different areas of the adaptation machine, as well as for transport or storage .
[0222] Figure 15 shows a sectional view of section 15-15, indicated in Figure 13, of an element (42) of the fiber fastening system, and is similar to Figure 14. In this case the coupling element ( 33) and the closure (28) are not displayed since they are located in another section of the fastener (42).
[0223]
[0224] The fiber structure (4) protrudes (43) from the fastening system to allow a greater sliding distance of the fibers during the preforming process, in areas that require it. Note that the elastic element (32) covers the entire area (37) of the lower (29) and upper (31) frames.
[0225]
[0226] Figure 16 shows the same section as Figure 14 at a later time, specifically, during the preforming process, in which it is seen how each of the fiber layers (13) have independently slipped from the fastener (42), to the extent required by the process.
[0227]
[0228] Figure 17 shows the same section as Figure 14, presenting in this case an additional element, namely, an elastic film (34), which is fastened by a fixing system (35) that is not detailed, such as for example pliers or a tensioning frame, and which may or may not allow said film to slide (34).
[0229]
[0230] Figure 18 shows a perspective view of a fiber fastener (42) according to the present invention, in which the fiber layers (13) positioned between the separation sheets (30) located in turn between the lower frame (29) and the upper or closing frame (31). The closing elements (28) provide the closing force that is transmitted to the fibers through the frames (29) and (31), thanks to which the tensioning effect is achieved by friction phenomena.
[0231]
[0232] Figure 19 shows a disassembled fiber clamping system (5), where the ease of automation of said fastening concept is appreciated. For mounting, first, the lower frame (29) is placed on a surface or tooling (40) located in the lower area (19B) of stacking layers (13) and mounting the fiber fastening system, in that there is a support element (41) that prevents the layers (13) from sinking during stacking. Subsequently, preferably by means of an automated system containing the remaining elements of the fastening system (5), a separation sheet (30) is positioned. Then, preferably by an automated system, such as the robot (21), a layer of fibers (5) is placed in the desired position. The process is continued by placing so many layers (13) and sheets (30) alternately as necessary for each preform, placing a last sheet (30) followed by the upper or closing frame (31). Finally, the closure (28) is installed to apply the necessary force on the fibers (13), so that there is the tension required therein during its adaptation to the forming mold (3).
[0233]
[0234] Figure 20 shows a section of the restoration system indicated in claim 13a, wherein the additional restoration mold (24) and the matrix (1) are positioned such that the deformable body (2) is positioned between them. . The elastic film (44) positioned by means of fastening or tooling (45), separates the deformable body (2) so that it does not adhere to the additional mold (24) for restoring. Said film (44) has perforations (47) that allow the evacuation of the air that would otherwise be enclosed between the deformable body (2) and the film (44), said perforations being small enough to prevent the deformable body ( 2) be extruded through them.
[0235]
[0236] Thus, when compressing the matrix (1) against the additional mold (24), the deformable body (2) is forced to acquire the form of said additional restoration mold (24), which is the one required to re-perform the adaptation process.
[0237]
[0238] The system also has an elastic seal (46) located on the edge of the additional mold (24) and on the elastic film (44). Said elastic seal (46) is compressed together with the deformable body (2) to prevent said deformable body from falling out of the volume between matrix (1) and additional mold (24).
[0239]
[0240] Figure 21 is similar to Figure 20, showing in this case a joint (46) integral with the matrix (1) and having a skirt (49) that is enclosed between said matrix and the deformable body (2), according to claim 14a.
[0241]
[0242] Figure 22 is similar to Figure 20, in this case showing a section during compression of the deformable body (2) on the additional mold (24).
[0243]
[0244] Figure 23 shows a sectional view of the fastening and guiding apparatus of the elements (42) of the fiber fastening system (5) (4), as described in claim 27. This system comprises a displacement mechanism. (52) that can be operated by a robotic system, or pushed by an actuator (53) integral with the die (1), and which allows the clamping element (42) to be positioned in the right place during adaptation. For this, there is a flexible arm (50) that is anchored at one of the ends to the movable element (54) of the movement mechanism (52), the other end being anchored to the fiber fastening element (42). This arm can deform to bending and torsion, allowing the fastener (42) to align freely with the direction of tension of the fibers, which is essential to prevent the fiber layers (13) from adhering to each other before have adapted to the shape of the mold (3) correctly. Since the arm is flexible, before adaptation, in which the fibers are arranged in a two-dimensional plane, the fasteners (42) could fall by their own weight. To avoid this, a rigid support (51) is placed under the flexible arm (50) and is anchored to the movable element (54) of the movement mechanism (52).
[0245]
[0246] Figures 24.A and 24.B show possible embodiments of the hitch system linked to the fastening system (5) of the fibers, according to claim 1. A sectional view of a fastener (42) of said fastener system (5) is shown.
[0247]
[0248] A mixed embodiment of the coupling system between the lower frame (29), separation sheets (30) and upper frame (31) is shown in Figure 24.A, in which the lower and upper frame (29,31) are linked by a first hinge mechanism (55) that allows a relative rotation movement, while the separation sheets (30) are linked to the lower frame (29) by a pin (33) that crosses them. The closure system is not shown in this figure, and it can be a rotary actuator that acts on the first hinge mechanism (55) exerting the necessary force to compress the fibers (13) between the lower and upper frames (29,31) .
[0249]
[0250] Figure 24.B shows a hitch system composed of a first hinge mechanism (55) that joins the upper and lower frames (31.29) on the one hand, and a second hinge mechanisms (55 ') that link the separation sheets (30) with the lower frame (29) on the other hand. The closing system is also not represented in this figure.
[0251]
[0252] Industrial Application
[0253] Manufacture of composite structural parts that require high quality and high productivity.
权利要求:
Claims (27)
[1]
1.- Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , comprising:
- a solid matrix (1);
- a deformable body (2) that is attached to the surface of said matrix (1), which can have several shapes and that covers an area greater than or equal to the area of the piece to be formed;
- a forming mold (3);
- a fastening system (5) of the fiber structure (4);
where:
- said matrix (1) is a solid element that has a functional face whose geometry depends on the piece to be manufactured; where the deformable body (2) is connected to the functional face of the die (1), which is configured to move towards the forming mold (3) by a linear guidance system driven by an actuator;
- said deformable body (2) is of a material that has a stiffness at least 100 times lower than the matrix (1) and the forming mold (3), where the deformable body (2) has an initial geometry dependent on the geometry that it is desired to confer to the fiber structure (4); and where the progressive compression of the deformable body (2) against said forming mold (3), is the one that causes the effect of adapting the fiber structure (4) to the forming mold (3);
- said forming mold (3) has the geometry that it is desired to confer to the fiber structure (4) in the adaptation process on the forming mold (3), and the forming mold (3) is positioned in such a way that the deformable body (2) is located between said forming mold (3) and the matrix (1); characterized by:
- said fastening system (5) of the fiber structure (4) comprises at least a part of the contour of the fiber structure (4) by means of at least one fastening element (42) that is configured to be able to move during the adaptation of the fiber structure (4) to the forming mold (3);
where each clamping element (42) comprises:
- a lower frame (29) covering an area (38) greater than or equal to an effective clamping area (36); wherein said lower frame (29) includes an anchoring system to an element such as a tooling or a robotic mechanism that allows the clamping element (42) to be displaced during adaptation;
two
- separation sheets (30), covering at least the effective clamping area (36), located on said lower frame (29); wherein the planes of said separation sheets (30) and the plane of said lower frame (29) are parallel; wherein between said separation sheets (30) layers (13) that are part of the fiber structure (4) to be fastened are placed; and where each layer (13) is always separated from another adjacent layer (13) by one of said separation sheets (30);
- an upper closing frame (31), which covers at least the effective clamping area (36), located on the separation sheets (30); wherein the plane of said upper frame (31) and the planes of the separation sheets (30) are parallel; wherein said separation sheets (30) are located between the lower frame (29) and the upper frame (31); and where the upper frame (31) includes an anchoring system to an element such as a tooling or a robotic mechanism that allows the clamping element (42) to be displaced during adaptation;
- a hitch system that links the lower frame (29), separation sheets (30) and upper frame (31); wherein said coupling system is configured to prevent relative displacement relative to the planes in which said elements are located (29, 30, 31);
- a closure system that prevents the relative displacement between the lower frame (29), the separation sheets (30) and the upper frame (31) with respect to the normal direction to the planes in which said elements (29, 30, 31); where said closing system is configured to exert the required closing force.
[2]
2. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 1, characterized in that it includes an elastic film (34) that is configured to be placed between the deformable body (2) and the fiber structure (4); where the deformable body (2) is a material of high plasticity by virtue of which it permanently deforms plastically during the adaptation process on the forming mold (3).
[3]
3. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 1, characterized in that the deformable body (2) includes in its interior a series of watertight cavities (6), filled with a fluid selected from a gas and a liquid; where the deformable body (2) is an elastic body by virtue of which it does not suffer permanent deformations during the adaptation process on the forming mold (3).
[4]
4. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 1, characterized in that the deformable body (2) includes in its interior a series of watertight cavities (6), filled with a fluid selected from a gas and a liquid; wherein said hollow watertight structure (6) connects with a fluid injection and evacuation system configured to vary the volume of the deformable body (2) and to vary the degree of compression of the deformable body (2) on the fiber structure (4) against the forming mold (3); and where the deformable body (2) is an elastic body by virtue of which it does not suffer permanent deformations during the adaptation process on the forming mold (3).
[5]
5. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 2, characterized in that it comprises an additional mold (24) configured to return the deformable body (2) to its shape initial by pressing the additional mold (24) on said deformable body (2) against the die (1); wherein said deformable body (2) is located between the die (1) and the additional mold (24); and where the additional mold (24) is required when the deformable body (2) is not a body of elastic material but a body of plastic material that undergoes permanent deformations during the adaptation process.
[6]
6. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 5, characterized in that the additional restoration mold (24) and the forming mold (3) include systems of displacement (27) that are configured to allow both molds (3, 24) to be positioned alternately in alignment with the die (1).
[7]
7. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 5, characterized in that the matrix (1) includes a displacement system configured to move said matrix (1) , by means of a robotic mechanism, to a position in which the additional restoration mold (24) is located; and wherein said matrix (1) is compressed against said additional mold (24).
[8]
8. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any one of the preceding claims 5, 6 or 7, characterized in that the functional face of the matrix (1) that is It is in contact with the deformable body (2), and an additional mold surface (24) for restoration, they have surface textures with a degree of adhesion between the deformable body (2) and the matrix (1) that is greater than the degree of adhesion that exists between said deformable body (2) and said additional restoration mold (24); wherein said deformable body (2) when separating the matrix (1) from the additional mold (24), is adhered to said matrix (1) and not to said additional mold (24).
[9]
9. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any one of the preceding claims 5, 6 or 7 , characterized in that it further comprises a film (44) of elastic material, such as latex, which is located on the surface of the additional restoration mold (24); wherein said film (44) is placed between the deformable body (2) and said additional restoration mold (24); wherein the film (44) is secured by a fixing system (45) that does not invade the space of said additional mold (24); and where the film (44) is a body selected between a porous body and a body that has perforations (47) that allow the air enclosed between said film (44) and the deformable body (2) to be evacuated.
[10]
10. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 9, characterized in that the fixing system (45) of the film (44) is integral with the additional mold (24 ) reset.
[11]
11. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 9, characterized in that the fixing system (45) of the film (44) is integral with the matrix (1 ).
[12]
12. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 9, characterized in that the fixing system (45) of the film (44) is an independent system configured to move relatively with respect to the mold
two
additional (24) and with respect to the matrix (1); where the fixing of the film (44) is independent with respect to the additional mold (24) and with respect to the film itself (44).
[13]
13. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any one of the preceding claims 5, 6, 7, 8, 9, 10, 11 or 12 characterized in that it further comprises an elastic seal (46) based on an elastic material; wherein said elastic seal (46) is located on the contour of the additional mold (24); and where said elastic seal (46) may contain cavities, or reinforcements therein.
[14]
14. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any one of the preceding claims 5, 6, 7, 8, 9, 10, 11 or 12, characterized in that it comprises additionally an elastic seal (46) based on an elastic material; where the elastic seal (46) is integral with the die (1), along its contour; wherein said elastic joint (46) has a skirt (49) towards an interior space of said matrix (1) that is enclosed between said matrix (1) and the deformable body (2); where said elastic seal (46) is configured to contain cavities, or reinforcements inside.
[15]
15. - Machine for adapting a structure of fibers to a mold for the manufacture of pieces of composite material , according to any one of the preceding claims 13 or 14, characterized in that the additional mold (24) has on its contact surface a air evacuation structure (48) formed by grooves or pores that allows the evacuation of the air enclosed between the film (44) and said additional mold (24) during the recovery of the geometry of the deformable body (2) that faces the contact surface of the air evacuation structure (48).
[16]
16. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any one of the preceding claims, characterized in that the fastening system (5) of the fiber structure (4) comprises additionally an elastic element (32), such as an elastic polymer foam, which is located between the upper frame (31) and the separation sheet (30), and between the lower frame (29) and the separation sheet (30) ; wherein said elastic element (32) covers an area (37) greater than or equal to the effective clamping area (36).
two
[17]
17. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any of the preceding claims, characterized in that the separation sheets (30) comprise a material selected from a non-stick material, and any flexible material coated with said nonstick material.
[18]
18. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 2, characterized in that the elastic film (34) is fixed to an element selected from the matrix (1) and the forming mold (3).
[19]
19. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 2, characterized in that the fastening system (5) of the fiber structure (4) additionally comprises the film elastic (34); wherein said elastic film (34) is fixed either to the lower frame (29), or to the upper frame (31) to both elements (29, 31); where said elastic film (34) is held by a fixing system (35), such as tweezers.
[20]
20. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any one of the preceding claims, characterized in that the coupling system that links the lower frame (29), separation sheets (30) and upper frame (31), comprises at least one coupling element (33) selected between a cylindrical pin and a threaded rod; where
said hooking element (33) is integral with either the upper frame (31) or the lower frame (29);
said hooking element (33) is arranged in a direction perpendicular to the planes of the lower frame (29), separation sheets (30) and upper frame (31); The coupling element (33) passes through the separation sheets (30) and the respective frame (29 or 31) through holes included in said separation sheets (30) and in the respective frame (29 or 31).
[21]
21. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any of the preceding claims 1 to 19, characterized in that the coupling system that links the lower frame (29), separation sheets (30) and upper frame (31) comprises a first hinge mechanism (55) and a second hinge mechanism (55 '); where the upper frame (31) is connected to the lower frame (29) by the first hinge mechanism (55); and where the separation sheets (30) are connected to the lower frame (29) by the second hinge mechanisms (55 ').
[22]
22. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any of the preceding claims 1 to 19, characterized in that the coupling system linking the lower frame (29), sheets of separation (30) and upper frame (31) comprises a first hinge mechanism (55) and a coupling element (33) such as a cylindrical pin or a threaded rod; where the upper frame (31) is connected to the lower frame (29) by the first hinge mechanism (55); and where the coupling element (33) crosses the separation sheets (30) and is attached to the lower frame (29).
[23]
23. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 20, characterized in that the closure system (28) is linked to the cylindrical pin (33).
[24]
24. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any one of the preceding claims, characterized in that the matrix (1) is formed by several moving parts (8) that are configured to move towards the forming mold (3); where said parts (8) compress the deformable body material (2) and are driven by at least one mechanical actuator (9).
[25]
25. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 24, characterized in that the moving parts (8) are independently coupled to two mechanical actuators (9).
[26]
26. - Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to claim 24, characterized in that the movable parts (8) are coupled together to a
one
single mechanical actuator (9) through an intermediate mechanism (10) that links the moving parts (8) to the mechanical actuator (9).
[27]
27.- Machine for adapting a fiber structure to a mold for the manufacture of pieces of composite material , according to any of the preceding claims, characterized in that the fasteners (42) of the fiber fastening system (5) ( 4) are subject to a system that includes:
- a displacement mechanism (52) that is operated by a robotic system, or pushed by an actuator (53) integral with the matrix (1);
- a flexible arm (50) that is anchored at one of its ends to a movable element (54) of the movement mechanism (52); where the other end of the flexible arm (50) is anchored to the fiber fastener (42);
- a rigid support (51) located under the flexible arm (50); wherein said rigid support (51) is configured to prevent said flexible arm (50) and the fiber fastener (42) from falling by its own weight; and where said rigid support (51) is anchored to the movable element (54) of the movement mechanism (52).
two
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同族专利:
公开号 | 公开日
ES2734598B2|2020-05-04|
WO2020074757A1|2020-04-16|
CA3115026A1|2020-04-16|
EP3865287A1|2021-08-18|
EP3865287A4|2021-12-08|
US20210379845A1|2021-12-09|
JP2022508736A|2022-01-19|
引用文献:
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EP2419260A1|2009-04-14|2012-02-22|Airbus Operations GmbH|Apparatus and method for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material|
DE102011012500A1|2011-02-25|2012-08-30|Benteler Sgl Gmbh & Co. Kg|Device for manufacturing fiber composite work piece, particularly from fibrous material sheet, has upper tool, lower tool and clamping frame, where clamping frame is moveably separated from upper tool and lower tool|
US20140103571A1|2011-05-05|2014-04-17|Compositence Gmbh|Method and apparatus for producing laid fibre fabrics and component preforms made of fibres|
DE102012021738A1|2012-10-27|2014-04-30|Daimler Ag|Producing preform, comprises providing fiber semifinished product formed as fiber mat comprising two layers, clamping fiber mat, in which individual layers of fiber mat are separately clamped, and forming fiber mat using forming device|
DE102013007382A1|2013-04-26|2014-10-30|Volkswagen Aktiengesellschaft|Device and method for draping flat semi-finished products for producing a fiber composite material|
ES2648562T3|2013-10-30|2018-01-04|Airbus Operations S.L.|Device for the manufacture of omega-shaped stringers|
FR2741936B1|1995-12-01|1998-02-06|Gaztransport Et Technigaz|METHOD FOR MANUFACTURING A THERMALLY INSULATING PANEL COMPRISING AN INCORPORATED WATERPROOFING SHEET|
DE102014205479A1|2014-03-25|2015-10-01|Bayerische Motoren Werke Aktiengesellschaft|Process for producing a fiber preform for a fiber composite component|
法律状态:
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优先权:
申请号 | 申请日 | 专利标题
ES201830979A|ES2734598B2|2018-10-10|2018-10-10|Machine for adapting a fiber structure to a mold for the manufacture of composite material parts|ES201830979A| ES2734598B2|2018-10-10|2018-10-10|Machine for adapting a fiber structure to a mold for the manufacture of composite material parts|
PCT/ES2019/070618| WO2020074757A1|2018-10-10|2019-09-19|Machine for adapting a fibre structure to a mould for manufacturing parts of composite material|
JP2021545330A| JP2022508736A|2018-10-10|2019-09-19|Equipment for adapting fiber structures to molds for manufacturing composite parts|
US17/283,750| US20210379845A1|2018-10-10|2019-09-19|Machine for adapting a fibre structure to a mould formanufacturing parts of composite material|
EP19871561.7A| EP3865287A4|2018-10-10|2019-09-19|Machine for adapting a fibre structure to a mould for manufacturing parts of composite material|
CA3115026A| CA3115026A1|2018-10-10|2019-09-19|Machine for adapting a fibre structure to a mould for manufacturing parts of composite material|
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