The present invention relates to the general field of fiber preforms obtained by three-dimensional weaving and comprising two distinct portions that present outlines of different shapes and that are connected together by a zone of non-interlinking.
Certain fiber preforms obtained by three-dimensional weaving include zones of non-interlinking that make it possible, using a single flat-woven preform, to make parts out of composite material that are complex in shape. For example, they might be fan blade platforms for an aviation turbine engine that can be obtained from n-shaped fiber preforms having a base and two legs forming stiffeners, the base constituting one portion and the two legs constituting another portion that is distinct from the base portion, the portions being connected together by a zone of non-interlinking.
One of the problems encountered with making such preforms is that the profiles as cut out from the two non-interlinked portions of the preforms (constituting their final outlines) are not necessarily the same. In such a situation, it is not possible to envisage using waterjet cutting, so it is necessary to cut out the profiles of the two portions of the preform manually, one after the other.
However, it is difficult to control manual cutting out of a fiber preform, which can lead to cutting inaccuracies, and to problems of reproducibility and of loss of fibers.
An object of the invention is thus to provide a cutting table and a cutting method that do not present the above-mentioned drawbacks.
In accordance with the invention, this object is achieved by a cutting table for cutting out a fiber preform obtained by three-dimensional weaving and having two portions that are connected together by at least one zone of non-interlinking and that present outlines of different shapes, the cutting table comprising: a tabletop provided with a recess for receiving flat one of the portions of the preform to be cut out; sacrificial plates for interposing between the portions of the preform for cutting out and for being fastened to the tabletop; at least one cutting template designed to be pressed against the portion of the fiber preform that is not positioned in the recess; and means for applying compacting pressure against the cutting template.
The cutting table of the invention is remarkable in that it incorporates multiple constraints within a single piece of tooling, such as uniform and accurate compacting of the preform portion while it is being cut out, accurate cutting out of its portions without risk of deformation or fiber removal, and a limited risk of injury for the operator. Thus, the cutting table of the invention makes it easier to cut out fiber preforms and limits problems of reproducibility.
The cutting table may include an actuator mounted vertically above the tabletop and designed to receive the cutting template in order to apply compacting pressure thereagainst.
Each sacrificial plate may be suitable for fastening on the tabletop by means of indexing screws. The recess of the tabletop may present a profile that corresponds to an outline that is common to the two preform portions that are to be cut out.
Advantageously, the cutting template has at least two indexing fingers for positioning it on the preform. Likewise, the cutting template advantageously has a bevelled edge for facilitating the passage of a cutting tool. Finally, the cutting template advantageously has a compacting lip at its periphery for the purpose of optimizing retention of the preform while it is being cut out.
The tabletop is preferably rotary, circular, horizontal, and includes a top surface that is provided with the recess, thereby facilitating the cutting work of the operator.
Another object of the invention is to provide a method of cutting out a fiber preform by means of a cutting table as defined above, the method comprising:
The method may include a prior step of pre-cutting the preform by water jet around a common outline covering the outlines of both portions of the preform.
Other characteristics and advantages of the present invention appear from the following description made with reference to the accompanying drawings, which show an embodiment having no limiting character. In the figures:
The invention relates to cutting out a fiber preform obtained by three-dimensional (3D) weaving and having two portions that are connected together by at least one zone of non-interlinking and that present outlines of different shapes. Such fiber preforms make it possible to make composite material parts of complex shape from a single flat-woven preform. A non-limiting example application is that of fiber preforms used for fabricating fan blade platforms for an aviation turbine engine, such as the preform shown in
These figures are diagrams showing a fiber preform 10 that is obtained by 3D weaving and that, after shaping, injecting resin or densifying with a matrix, and possibly machining, serves to obtain a fan blade platform.
The term “3D weaving” should be understood as meaning that the warp yarns of the preform follow sinuous paths in order to interlink weft yarns belonging to different weft yarn layers, excepting zones of non-interlinking, it being understood that a 3D weave, in particular an interlock weave, may include 2D weaves at the surface. Various 3D weaves may be used, such as interlock, multi-satin, or multi-plain weaves, for example, as described in particular in document WO 2006/136755.
The fiber preform 10 presents two distinct portions in its thickness direction, namely a top portion 12 and a bottom portion 14, each of which is formed by a plurality of superposed layers of yarns, and which are connected together by a zone of non-interlinking 16 so as to form a single fiber structure. In this zone of non-interlinking 16, the layers of yarns of the top portion of the fiber preform are interlinked with the layers of yarns of the bottom portion (and vice versa).
Furthermore, the portions 12 and 14 of the fiber preform present outlines that are different.
With reference to
The initial step of the cutting method is making a fiber structure 20 by 3D weaving, such as that shown in
Starting from this fiber structure, the following step consists in pre-cutting the fiber structure with a waterjet along a common outline C that covers the outlines of both of the fiber preform portions that are to be obtained. This operation makes it possible to obtain the pre-cut preform 30 shown in
The preform 30 as pre-cut in this way is then positioned on the cutting table 100 in accordance with the invention, as shown diagrammatically in
This cutting table 100 comprises in particular a stand 102 on which a horizontal tabletop 104 is mounted to rotate about a vertical axis A-A and that has a top surface 106 provided with a recess 108 that is to receive flat one of the preform portions to be cut out. For this purpose, the recess 108 presents a profile that corresponds to the outline C that is common to both of the preform portions that are to be cut out.
In the example shown in
Sacrificial plates 110 (there are two in this example) are then interposed between the two preform portions for cutting out (
Once the sacrificial plates 110 are positioned in this way on the cutting table, they are fastened to its tabletop 104, e.g. each by means of two indexing screws 112 (
The following step is shown in
Advantageously, the cutting template 114 has two indexing fingers 116 relative to the sacrificial plates 110 in order to ensure that the cutting template is properly positioned on the pre-cut preform 30.
Thereafter, compacting pressure is applied on the cutting template 114 in order to enable the fibers of the preform at the margin of the cutting template to be held so as to prevent them from moving during the cutting operation proper.
For this purpose, the cutting template 114 is fastened horizontally to the free end of an actuator 118 mounted vertically above the tabletop 104 of the cutting table. The compacting pressure applied by the actuator on the cutting template typically lies in the range 3 bars to 5 bars.
Once the cutting template has been applied, it is possible to begin cutting out the portion 34 of the preform along the outline of the cutting template. This cutting can be performed in various ways that are themselves known, for example manually using a blade made of steel or of ceramic.
In the example shown in
When cutting is finished, the portion 34 of the fiber preform 30 corresponds to the top portion 12 of the cut-out preform 10 as shown in
The fiber preform 30 is thus placed on the cutting table 100′ with its top portion 12 positioned in the recess 108′ of the tabletop 104′.
The operations then follow on in the same manner as for cutting out the portion 34 of the preform. In particular, the same sacrificial plates 110 are mounted and fastened to the tabletop 104′ and another cutting template 114′ is applied against the preform portion 32 to be cut out, this cutting template presenting an outline 114′a that corresponds to the outline of the bottom portion 12 of the cut-out preform (
Once it has been cut out, the portion 32 of the fiber preform 30 corresponds to the bottom portion 14 of the cut-out preform 10 as shown in
In another advantageous provision of the invention, as shown in
In another advantageous provision of the invention, also shown in
Number | Date | Country | Kind |
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1362408 | Dec 2013 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2014/053092 | 12/1/2014 | WO | 00 |