DEVICE AND METHOD FOR PRODUCING A CURVED FIBER PREFORM FROM A BI- OR MULTIDIRECTIONAL FIBER SEMI-FINISHED PRODUCT
20190030841 · 2019-01-31
Inventors
- Julian Kuntz (Augsburg, DE)
- Ralph Männich (Aichach, DE)
- Enzo de Santis Mühlberger (Augsburg, DE)
- Francois Tremblay (Augsburg, DE)
- Margarita Wanner (Friedberg, DE)
- Christoph Stehncken (Uslar, DE)
Cpc classification
B29C70/545
PERFORMING OPERATIONS; TRANSPORTING
B29C66/1122
PERFORMING OPERATIONS; TRANSPORTING
B29C53/06
PERFORMING OPERATIONS; TRANSPORTING
B29B11/16
PERFORMING OPERATIONS; TRANSPORTING
B29C70/56
PERFORMING OPERATIONS; TRANSPORTING
B29C70/742
PERFORMING OPERATIONS; TRANSPORTING
Y02T50/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29C70/682
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C70/68
PERFORMING OPERATIONS; TRANSPORTING
B29C70/56
PERFORMING OPERATIONS; TRANSPORTING
B29C53/06
PERFORMING OPERATIONS; TRANSPORTING
B29C70/74
PERFORMING OPERATIONS; TRANSPORTING
B29C70/54
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A device for producing a curved fiber preform from a bi- or multidirectional fiber semi-finished product, in particular for an aircraft or spacecraft fuselage component has first lamellae and second lamellae formed to be couplable to one another criss-cross such that they are positioned on a shared plane and thus form a grid. The lamellae at least in part are formed resiliently bendable about an axis intersecting the shared plane such that a local orientation of the lamellae in the grid changes. An adhesion device or structure is formed for temporarily adhering the fiber semi-finished product and is configured such that the local fiber orientation of the fiber semi-finished product also changes accordingly when the lamellae bend.
Claims
1. A device for producing a curved fiber preform from a bi- or multidirectional fiber semi-finished product, in particular for a fuselage component of an aircraft or spacecraft, comprising: a plurality of first lamellae and a plurality of second lamellae which are formed to be couplable to one another criss-cross such that they are positioned on a shared plane and thus form a grid, the lamellae at least in part being formed resiliently bendable about an axis intersecting the shared plane such that a local orientation of the lamellae in the grid changes; and an adhesion structure formed for temporarily adhering the fiber semi-finished product to the grid and configured such that local fiber orientation of the fiber semi-finished product also changes accordingly when the lamellae bend.
2. The device of claim 1, wherein for coupling to one another the first and second lamellae comprise corresponding plug sockets which can be plugged into one another.
3. The device of claim 2, wherein corresponding plug sockets are combined and form a depth corresponding to a thickness of at least one of the first and second lamellae.
4. The device of claim 1, wherein a neutral lamella is introduced into the grid, and is arranged in a region of a theoretical or actual neutral fiber of the curved fiber preform to be produced, and is formed such that cells of the grid positioned on a first side of the neutral lamella are stretched during bending and cells of the grid which are positioned on a second side of the neutral lamella are compressed during bending.
5. The device of claim 4, wherein the neutral lamella is irregular.
6. The device of claim 1, wherein a deformable membrane provided as a support face for the fiber semi-finished product is provided on the grid.
7. The device of claim 6, wherein the deformable membrane is a resiliently biased membrane for compensating bending of the lamellae.
8. The device of claim 1, wherein the adhesion structure comprises an underpressure box which fluidically contacts the grid and which is formed such that an underpressure can thus be applied in each cell of the grid provided for supporting the fiber semi-finished product.
9. The device of claim 8, wherein the underpressure can be applied by an underpressure connection, which is provided on the underpressure box and to which an underpressure source can be connected.
10. The device of claim 8, wherein the underpressure box is perforated to form a perforation in a region of cells of the grid provided for supporting the fibers, and at least one of sealing for sealing the perforation and the grid are provided in at least one of the regions without fiber semi-finished product support and in edge regions of the fiber semi-finished product support, such that an underpressure is present substantially at the fiber semi-finished product.
11. The device of claim 10, wherein the perforation is provided in a first region, where the cells of the grid provided for supporting the fiber semi-finished product are located when the lamellae are detensioned, and in a second region, where the cells of the grid which are provided for supporting the fiber semi-finished product are located when the lamellae are bent.
12. The device of claim 10, wherein the sealing seals the perforation which is positioned alongside the cells of the grid which are provided for supporting the fiber semi-finished product in each state of the grid.
13. The device of claim 12, wherein the sealing has at least one of an air-impermeable local covering and selectively actuable valves of at least one of the perforation and the grid.
14. The device of claim 1, wherein the adhesion structure comprises a bonding of the grid itself.
15. The device of claim 14, wherein bonding of the grid itself is in a form of at least one of sticky, rough, jagged and needle portions in an application region, provided on the grid, which is non-critical for the fiber semi-finished product.
16. The device of claim 15, wherein bonding of the grid itself is provided at an edge of the fiber semi-finished product.
17. The device of claim 1, wherein the adhesion structure has a contact face which contacts the fiber semi-finished product on a side opposite the grid, a coefficient of friction between the contact face and the fiber semi-finished product being configured to be less than a coefficient of friction between the grid and the semi-finished product.
18. The device of claim 1, wherein at least one of the grid and the adhesion structure are formed as part of an end effector for transporting the previously curved fiber preform when the lamellae are bent.
19. A method for producing a curved fiber preform, comprising: applying a bi- or multi-directional fiber semi-finished product to a grid of a plurality of first lamellae and a plurality of second lamellae, which are coupled to one another criss-cross and positioned on a shared plane; temporarily adhering the fiber semi-finished product to the grid; and resiliently bending the lamellae at least in part about an axis intersecting the shared plane, a local orientation of the lamellae in the grid changing and a local fiber orientation of the fiber semi-finished product also changing accordingly when the lamellae bend.
20. The method of claim 19, wherein the fiber semi-finished product is oriented on the grid such that the bi- or multidirectional fibers of the fiber semi-finished product at least in part extend parallel to at least one of the lamellae and a theoretical or actual neutral fiber of the fiber semi-finished product is arranged and oriented on a neutral lamella of the grid, and, during the resilient bending, fibers positioned on the first side of the neutral lamella are deformed in accordance with a stretching of the cells of the grid which acts there, and fibers positioned on a second side of the neutral lamella deform in accordance with a compression of the cells of the grid which acts there.
21. The method of claim 20, wherein the neutral lamella is irregular.
22. The method of claim 19, wherein the temporary adhesion is provided by mechanical pressure acting on the fiber semi-finished product or fluidic underpressure acting on the fiber semi-finished product.
23. The method of claim 19, further comprising transporting the curved fiber preform by at least one of the grid when the lamellae are bent and an adhesion structure used for adhesion is provided.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0059] Hereinafter, the disclosure herein is described in greater detail by way of the embodiments set out in the schematic and example drawings, in which:
[0060]
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[0073] The accompanying drawings are intended to convey an improved understanding of the embodiments of the disclosure herein. They illustrate embodiments and serve in conjunction with the description to explain principles and concepts of the disclosure herein. Other embodiments and many of the stated advantages may be derived from the drawings. The elements of the drawings are not necessarily shown to scale with one another.
[0074] In the drawings, unless stated otherwise, like, functionally equivalent and identically acting elements, features and components are provided with like reference numerals.
DETAILED DESCRIPTION
[0075]
[0076] This is a device 1 for producing a curved fiber preform from a bi- or multidirectional fiber semi-finished product (not shown here) for a fuselage component of an aircraft or spacecraft, for example a former portion.
[0077] The device 1 comprises a plurality of first lamellae 2 and a plurality of second lamellae 3, which are configured to be pluggable into one another criss-cross in such a way that they are positioned on a shared plane and thus together form a grid 4. An axis 5, which intersects the shared plane of the grid 4 and about which the lamellae 2, 3 are resiliently bent, is further illustrated schematically. In this way, the local orientation of the lamellae 2, 3 deforms continuously, in such a way that the cells of the grid 4, which are square when detensioned, recognisably change to stretched or compressed rhombuses.
[0078] A fiber semi-finished product 9, not shown here, can be adhered temporarily on the grid 4 by an adhesion device or structure 6, here formed by way of example as an adhesive coating of the lamellae. The adhesion device or structure 6 is configured in such a way that the local fiber orientation of the fiber semi-finished product also changes accordingly when the lamellae 2, 3 bend. A corresponding coefficient of friction is therefore provided between the grid and the adhesion device or structure 6.
[0079] Purely by way of example, the adhesive coating shown here is an adhesive strip permitted for fiber materials. For example, the adhesive strip is formed to be thermally resistant.
[0080] In further embodiments, however, the adhesion device or structure 6 may have additional elements and/or measures for adhering the fiber semi-finished product, which are discussed in greater detail in reference to the following embodiments. In this case, an adhesive strip permitted for fiber materials may also be provided as an anti-adhesive coating so as to reduce the friction and/or as a contact face so as to provide reliable contact.
[0081] The deformation or shaping of the fiber semi-finished product 9 using a device 1 of this type is performed by a carrier, which comprises the grid 4 which is formed using the lamellae 2, 3 plugged into one another in the form of shearable bars plugged into one another. The bars may have the same orientation (for example 45) as the fiber orientation of at least some of the layers of the fiber semi-finished product 9 to be shaped. The fiber semi-finished product is therefore applied before the deformation in a fiber orientation corresponding to the orientation of the lamellae.
[0082] If the grid together with the fiber semi-finished product adhering thereto is sheared by bending, the fiber semi-finished product is also sheared together. By stops, the maximum deformation/shearing of the grid 4 and thus also the desired curved shape, for example a required curvature of a former shape, can also be established.
[0083]
[0084] This drawing likewise shows a bent state of the grid 4, which can be seen clearly here.
[0085] Further,
[0086]
[0087] The device can be seen to comprise a plurality of first and second lamellae 2, 3. These are oriented in a 45 orientation. For example, the lamellae may each be a flexible bar. As the material, a wide range of bendable materials are suitable, such as high-grade steel, spring steel, glass-fiber-reinforced plastics material, carbon-fiber-reinforced plastics material, thermoplastics or the like. By way of example, in the embodiment shown over 100 lamellae, which are highly flexible, are plugged into one another. The resulting grid is planar on both sides.
[0088] In the grid 4, a neutral lamella 8 in the form of an individual bar is introduced in a third direction, and has a 0 orientation. The neutral lamella 8 is likewise formed using plug sockets, the lamellae 2, 3 of the grid 4 likewise being formed with additional plug sockets for receiving the neutral lamella 8.
[0089] The neutral lamella 8 defines a neutral fiber of the deformation, in other words a line along which no shear deformation takes place. This may apply equally to the deformation of the grid 4 and of the fiber semi-finished product 9. Cells of the grid 4 which are positioned on a first side of the neutral lamella 8 are thus stretched when the lamellae 2, 3 bend, whilst cells of the grid positioned on a second side of the neutral lamella 8 are compressed.
[0090] The fiber semi-finished product 9 can be sucked onto the grid 4 when an underpressure is applied by holes or ducts in the grid. For this purpose, in this embodiment the cells formed by the lamellae 2, 3 are fluidically connected via additional holes arranged between the plug sockets so as to make air circulation or pressure compensation possible between the cells.
[0091]
[0092] In this embodiment, the device 1 also has a grid 4 as explained in reference to
[0093] However, the adhesion device or structure 6A of this embodiment additionally comprises a hollow box which is arranged under the grid and which is formed as an underpressure box 16. Sealing 13 for sealing regions without fiber semi-finished product support is further provided.
[0094] For applying underpressure to the grid 4, a connection 12 to an underpressure source, for example for connecting a vacuum cleaner tube as shown in
[0095] On the upper face of the underpressure box 16, a perforation 14 as shown in
[0096] In this way, the fiber semi-finished product 9 placed on the grid 4 is sucked onto the grid 4, as is symbolised by the perpendicular thick arrows in
[0097]
[0098] As a result of the deformation of the grid during bending, the face covered by the grid 4 is also displaced on the underpressure box 16. Thus, there are holes of the perforation 14 of the underpressure box 16 which are only positioned below the grid 4 when detensioned as in
[0099] For sealing the holes positioned alongside the grid 4 in each case, the perforation 14 is also covered by the covering in regions positioned alongside the grid. Otherwise, holes positioned outside the grid 4 would suck up false air and reduce the suction force available for the fiber semi-finished product 9 positioned on the grid 4. The covering provided as sealing 13 is accordingly formed so as to be displaced together with the deformation of the grid 4, as is indicated in
[0100] Since the shape and the lengths of the outer edges of the grid 4 change during bending, the covering is further formed flexibly, in this case for example in the form of a flexible film. Further, in this case the covering consists of or comprises for example a plurality of sub-pieces which are displaceable with respect to one another.
[0101]
[0102] It can be seen that at the edge of the fiber semi-finished product there are cells of the grid 4 which are merely covered in part. For these regions, in the embodiment shown an additional sealing 13 is provided, which is shown in
[0103]
[0104] The additional sealing 13 serve to prevent false air from being sucked up at the edge of the grid 4, in particular in the gap shown in
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[0106] This embodiment differs from the embodiments described previously in relation to
[0107] In this embodiment, which is based on suction by way of underpressure, the membrane 11 is formed air-permeable and deformable. It serves to brace the fiber semi-finished product in compressed regions of the grid, so as to prevent local swelling into grid gaps, in other words into cavities of the individual cells.
[0108]
[0109] In this case the membrane 11 is formed as a metal grid by way of example. The threads of the metal grid have an identical orientation to the lamellae 2, 3 of the grid 4.
[0110] By the additional metal grid, the fiber semi-finished product 9 is braced from below in the grid gaps. Since the threads of the metal grid extend in the lamellae direction, the metal grid and thus also the lamellar grid 4 still remain deformable, however.
[0111] In other embodiments, however, instead of a metal grid a rubber membrane, for example perforated or slitted, may be used. For example, this is biased in accordance with a predetermined curvature of the fiber preform to be produced, so as to compensate the deformation of the grid 4 without swellings. The rubber membrane would subsequently have to be tensioned onto the grid 4 in such a way that the deformation of the rubber membrane is defined by the grid and thus subsequently also corresponds to the deformation of the textile (in other words not to the natural deformation of rubber).
[0112] In a further embodiment, instead of a membrane 11 of this type it is also conceivable to make the grid 4 itself narrower-mesh, in other words from much smaller lamellae, in such a way that the grid 4 has smaller cells or smaller gaps and the fiber semi-finished product 9 is thus better supported.
[0113]
[0114] The distinguishing adhesion device or structure 6B of this embodiment comprises a planar bed, which supports the grid, and has a contact face 15, which contacts the fiber semi-finished product 9 on a side opposite the grid 4.
[0115] The contact face 15 is for example formed as a stamp which covers the size of the grid in both states, which is for example in the form of a solid body plate, and which has an anti-adhesive coating. In this way, a coefficient of friction between the contact face 15 and the fiber semi-finished product 9 is less than a coefficient of friction between the grid 4 and the fiber semi-finished product 9. When mechanical pressure, symbolised by vertical arrows in
[0116] Further, in this case a membrane 11 for supporting the fiber semi-finished product 9 on the grid 4 may optionally also be provided. For example, in this case an (optionally biased) rubber membrane is used, but this does not need to be perforated.
[0117] By a device in accordance with one of the above-described embodiments, in particular fiber preforms for C profiles for formers can be produced, for example for producing 90 portions of a former. Accordingly, the produced fiber preform may subsequently be processed further to form the desired component, for example by cutting away edge regions, optionally by further shaping to form the subsequent component shape. For example, this may include collaring the flange of the C profile for a former portion.
[0118] Although the disclosure herein has been described entirely by way of several embodiments in the above, it is not limited thereto, but can be modified in various ways.
[0119] For example, a fiber semi-finished product may also be heated while positioned on the bent grid 4 so as to activate a binder which is located in the textile of the fiber semi-finished product and which fixes the deformation. In this case, after cooling, the curved fiber preform can subsequently be received by a conventional gripper and transported onwards and/or processed further.
[0120] A further conceivable embodiment of the device in the context of the disclosure herein is a simultaneous formation of the device as an end effector. For this purpose, the device 1 is for example rotated together with the suction substructure of an adhesion device or structure 6A, in other words together with the underpressure box 16 and the sealing 13, after deformation together with the curved fiber preform. The fiber preform is subsequently transported onwards, for example directly positioned on a further component preform, by the end effector formed integrally with the device. Therefore, in this embodiment, the curved fiber preform may also only be heated once it is on the component preform, in such a way that the shape of the fiber preform is fixed simultaneously with fixing on the component preform. For example, the component preform may be in the form of already deposited but not yet connected further layers for the component which is to be produced.
[0121] If elastomer or rubber membranes are used on the grid 4, either below or above the fiber semi-finished product 9, a further embodiment may involve applying this membrane biased only in part or in portions to the grid. As a result of the different deformation of the grid and of the material of the membrane, for example rubber, the grid 4 is prevented from shortening on the radially inner side in the longitudinal direction, for example on the inside of the bending in the direction of the inner flange of a former preform. The membrane is thus compressed and can buckle in the absence of bias. As a result of the membrane being biased, it instead always remains planar, in such a way that buckling is prevented and the fiber semi-finished product is always optimally supported.
[0122] In one embodiment, the bias of the rubber membrane can be provided in such a way that on the inner side of the curvature the tension is at a maximum at the start of the deformation and is near-zero when the end state of the deformation is reached. On the outside of the curvature, the bias may accordingly be provided the other way around, in such a way that there it is near-zero at the start of the deformation and becomes a maximum when the end state of the deformation is achieved.
[0123] In a further embodiment, however, the bias of the membrane may also be provided to be exactly as great on the outside as on the inside, in such a way that when the grid is non-deformed or relaxed it also remains straight in the absence of external forces.
[0124] While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms comprise or comprising do not exclude other elements or steps, the terms a, an or one do not exclude a plural number, and the term or means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.