The present invention relates to the general field of composite material parts.
Classically, a composite material part comprises a reinforcement (for example a fibrous reinforcement) and a matrix (for example a polymer resin).
The manufacturing method of such a part comprises various operations.
First, an operation referred to as “weaving” consists of flat-weaving a flat preform by means of a loom from strands of fibres (for example strands of carbon fibres). The preform is intended to form the reinforcement of the composite part.
Secondly, an operation referred to as “cutting” consists of cutting the flat preform using a cutting mould.
Thirdly, an operation referred to as “forming” consists of forming the flat preform in three dimensions using a forming mould.
Fourth, an operation referred to as “injecting” consists of injecting the matrix into an injection mould in which the preform is located in three dimensions, so as to obtain the composite part.
During the weaving operation, it is known to incorporate at least one strand comprising fibres of a light coloured material (e.g. glass fibres) forming a tracer, and in other words a reference that can be used throughout the manufacturing method. In the case of a tracer comprising glass fibres, the tracer is visually identifiable by the white colour of the glass fibres. Classically, the preform comprises several tracers.
As mentioned above, during the manufacturing method, it is known to use this tracer as a reference. For example, a tracer can be used to position the preform relative to a mould.
In the case of manual positioning of the preform and to locate a tracer arranged in an area of the preform that is not directly visible to the operator, for ergonomic reasons, it is known to use a camera filming the desired area and a screen on which the filmed images are displayed live. To position the preform in relation to the mould, the operator must position the tracer in relation to a reference frame, using the screen.
However, in practice, it has been found that the operator cannot correctly distinguish the tracer on the screen, despite the white colour of the glass fibres. Indeed, the optical properties of the carbon (specular reflection) considerably attenuate the white colour of the glass fibres.
Thus, in practice, the operators do not use the screen and position the tracer of the preform approximately in relation to the reference frame. Such a positioning considerably increases the number of defective preforms and does not allow to have a traceability of the preforms.
The objective of the present invention is therefore to provide a simple, effective and economical solution to the above-mentioned problem.
The invention thus proposes a system for locating at least one strand comprising fibres of a first material of a woven preform of a part made of composite material, the preform comprising strands of fibres of a second material on its surface and at least the strand comprising fibres of the first material forming a tracer, the system comprising a camera;
Such a system allows to easily locate the tracer of the preform from the images filmed by the camera, in order for example to position or control the preform. Such a system thus allows to significantly reduce the number of defective preforms, and consequently of defective parts.
Indeed, the system exploits the differences of optical properties between the first material and the second material, to highlight the fibres of the first material on the images filmed by the camera. The camera thus only films the light rays reflected by the fibres of the first material of the tracer.
Such a system also allows to guarantee the traceability of the preforms, and more generally of the composite material parts.
The system according to the invention may comprise one or more of the following characteristics and/or steps, taken alone or in combination with each other:
The present invention further relates to a method for positioning a woven preform of a composite material part with respect to a mould, the preform comprising on its surface at least one strand comprising fibres of a first material forming a tracer and strands of fibres of a second material, by means of the system as previously described, the first material being selected from glass, aramid and alumina oxide, the second material being selected from carbon and silicon carbide, the method comprising a step consisting in:
The positioning method according to the invention may comprise one or more of the following characteristics and/or steps, taken alone or in combination with each other:
The present invention also relates to a method for controlling a woven preform of a composite material part, the preform comprising on its surface at least one strand comprising fibres of a first material forming a tracer and strands of fibres of a second material, by means of the system as previously described, the first material being selected from glass, aramid and alumina oxide, the second material being selected from carbon and silicon carbide, the method comprising a step consisting in:
The control method according to the invention may comprise one or more of the following characteristics and/or steps, taken alone or in combination with each other:
The invention will be better understood and other details, characteristics and advantages of the present invention will become clearer from the following description made by way of non-limiting example and with reference to the attached drawings, in which:
The composite material part is, for example, a part of an aircraft turbomachine, such as a vane of a fan or a casing of a fan.
The composite material part comprises a reinforcement in the form of a woven fibrous preform 3, 3a, 3b and an organic matrix such as a polymer resin.
Such a part is manufactured according to a manufacturing method comprising various operations.
First, a weaving operation consists of flat-weaving a flat preform by means of a loom from strands of fibres. The woven preform then comprises warp strands (i.e. strands extending along the length of the preform) and weft strands (i.e. strands extending along the width of the preform).
The preform is for example woven by means of a Jacquard loom.
Advantageously, the weaving of the preform is a three-dimensional weaving.
Secondly, a cutting operation consists of cutting the flat preform using a cutting mould.
Thirdly, a forming operation consists of forming the flat preform in three dimensions using a forming mould.
The forming mould has an indentation whose shape corresponds substantially to that of the part to be produced.
Fourth, an injection operation consists of injecting the matrix (e.g., a polymer resin) into an injection mould in which the three-dimensional preform is located.
Advantageously, the injection operation is obtained via a method known by the English acronym RTM for “Resin Transfer Moulding”. Such an RTM method uses an injection mould comprising two opposing shells that are movable relative to each other. The shells each comprise an indentation, the indentations delimiting a cavity in which the preform is placed and the matrix injected.
Advantageously, the different operations of the manufacturing method are performed in the order defined above. The different operations of the manufacturing method can be performed manually and/or automatically.
The preform 3, 3a, 3b comprises on its surface at least the strand 2 comprising fibres of a first material forming a tracer and strands 4 of fibres of a second material. A tracer corresponds to a reference (or a mark) that can be used throughout the manufacturing method of the part, in order for example to position or control the preform 3, 3a, 3b during an operation.
The first material is selected from glass, aramid and alumina oxide. The second material is selected from carbon and silicon carbide.
Advantageously, to facilitate the identification of a tracer, the fibres of the first material are light and the fibres of the second material are dark.
In a first preferred combination, the first material is glass and the second material is carbon. Classically, the carbon fibres are black and the glass fibres are white.
In a second preferred combination, the first material is aramid and the second material is carbon. Classically, the carbon fibres are black and the aramid fibres are yellow.
In a third preferred combination, the first material is silicon carbide and the second material is alumina oxide. Classically, the silicon carbide fibres are black in colour and the alumina oxide fibres are yellowish white.
To facilitate its identification, a tracer is located on the surface of the preform 3, 3a, 3b.
As an example, a tracer may comprise two-thirds fibres of the first material and one-third fibres of the second material. A tracer may also comprise one hundred percent fibre of the first material.
The preform 3, 3a, 3b can of course comprise several tracers. Advantageously, the tracer is integrated into the preform 3, 3a, 3b during the weaving operation.
A tracer can be a warp strand (hereinafter referred to as warp tracer or longitudinal tracer) or a weft strand (hereinafter referred to as weft tracer or transverse tracer).
According to the invention, the system 1 for locating at least one tracer of the woven preform 3, 3a, 3b comprises:
The camera 5 is adapted to film a reflected beam f3 resulting from the interaction of the polarized incident beam f2 with the preform 3, 3a, 3b, the reflected beam f3 having previously passed through the cross analyser 8, so as to locate the tracer of the preform 3, 3a, 3b.
Such a system 1 allows to easily locate the tracer or the tracers in the preform. The tracer or the tracers appear distinctly on the images filmed by the camera 5. The system 1 allows to significantly accentuate the colour of the fibres of the first material on the images filmed by the camera 5.
For this purpose, the system 1 exploits the differences in optical properties between the first material and the second material, in order to highlight the fibres of the first material on the images filmed by the camera 5. The second material has a specular reflection while the first material has a diffuse reflection. Unlike the diffuse reflection, a specular reflection has the particularity of preserving the polarization. The cross analyser 8 thus allows to stop the light rays reflected by the fibres of the second material and to let pass only the light rays reflected by the fibres of the first material of the tracer, so as to make the fibres of the first material appear distinctly on the images filmed by the camera 5. In other words, the camera 5 only films the light rays reflected by the fibres of the first material of the tracer.
The polarizer 7 has a first polarization direction (or first transmission direction), the polarizer 7 allows the light rays of the incident beam to be polarized linearly (or straight) along the first polarization direction. For this reason, such a polarizer 7 is referred to as “linear polarizer” or “rectilinear polarizer”.
Advantageously, the cross analyser 8 has a second direction of polarization (or second direction of transmission), perpendicular or substantially perpendicular to the first direction of polarization of the polarizer 7, the analyser 8 being as such crossed with the polarizer 7. The polarization directions are defined in a plane perpendicular to the propagation direction of the beam.
Advantageously, the system 1 comprises a diffuser (not shown), the unpolarized incident beam f1 passing through the diffuser before passing through the polarizer 7. Such a diffuser allows to obtain a homogeneous lighting.
The system 1 can comprise a screen 9 on which images filmed by the camera 5 are displayed live. Such a screen 9 can for example allow an operator to locate the tracer, so as to position or control the preform.
The system 1 may comprise a control device configured to control the light source 6 and the camera 5. In the event that the system comprises a screen 9, the control device can also be configured to control the screen 9. The control device can be configured to automatically process the images filmed by the camera 5. In order to automatically process the images taken by the camera 5, the control device can comprise, for example, a computer (or an information processing system) and an image processing software.
Advantageously, the images filmed by the camera 5 are recorded in order to guarantee the traceability of the preforms, and more generally of the composite material parts obtained by the manufacturing method.
Advantageously, the camera 5 has a variable field of view, the latter is set to cover the desired field.
Advantageously, the light source 6 comprises a plurality of light emitting diodes (LED). The light emitting diodes are, for example, in the form of an LED bar.
The invention also relates to a method for positioning a woven preform 3, 3a, 3b with respect to a mould 11a, 11b, the preform 3, 3a, 3b comprising on its surface at least one strand 2 comprising fibres of the first material forming a tracer and strands 4 of fibres of the second material, by means of the system 1.
The positioning method comprises a step a) consisting of positioning the preform 3, 3a, 3b with respect to the mould 11a, 11b from the images filmed by the camera 5 by positioning the tracer of the preform 3, 3a, 3b with respect to a reference frame.
The step a) of the positioning method can be performed by an operator using a screen 9 of the system 1 on which the images filmed by the camera 5 are displayed live.
The step a) of the positioning method can be performed automatically, in particular by means of a control device of the system 1.
The positioning method can be implemented throughout the manufacturing method of a composite material part, and in particular during the cutting operation and/or during the forming operation and/or during the injection operation.
The invention also relates to a method for controlling a woven preform 3, 3a, 3b, the preform 3, 3a, 3b comprising on its surface at least one strand 2 comprising fibres of the first material forming a tracer and strands 4 of fibres of the second material, by means of the system 1.
The control method comprises a step a) of controlling that the tracer of the preform 3, 3a, 3b is within a predefined interval from the images filmed by the camera 5.
The step a) of the control method can be performed by an operator using a screen 9 of the system 1 on which the images filmed by the camera 5 are displayed live.
The step a) of the control method can be performed by a control device of the system 1 configured to automatically process images filmed by the camera 5.
The control method can be implemented throughout the manufacturing method of a composite material part, and in particular during the cutting operation and/or during the forming operation and/or during the injection operation.
As shown in
In particular, the vane preform 3a comprises a lower transverse tracer 2a on the surface at the level of the junction 15.
As shown in
The forming mould 11a also comprises a slit 12 opening both on a lower face of the mould 11a and into the indentation 16. The slit 12 is located at the level of the junction stretch 19 and forms a reference frame used in particular for positioning the vane preform 3a relative to the mould 11a.
The forming mould 11a also comprises a wedge 21 adapted to be attached to two projecting supports 22 bordering the indentation 16 at the level of the root stretch 17. The wedge 21 allows to immobilize the root portion 13 and the junction 15 of the vane preform 3a by compression.
As illustrated in
During the forming operation, the positioning method described above is implemented to position the vane preform 3a relative to the forming mould 11a.
An operator manually positions the lower transverse tracer 2a of the vane preform 3a in the slit 12 forming the reference frame, using the screen 9 of the system 1 on which the images filmed by the camera 5 are displayed live. To do this, using the screen 9, the operator displaces the vane preform 3a on the mould 11a until the lower transverse tracer 2a is comprised in the slit 12.
It is noted that the vane preform 3a is positioned relative to the forming mould 11a not only by positioning the lower transverse tracer 2a in the slit 12 but also by making coincide an upper transverse tracer (not shown) of the vane preform 3a with a reference projected onto the mould 11a by one or more lasers. The upper transverse tracer is for example placed at the level of the junction 15. The reference projected by the laser or the lasers defines the theoretical position of the upper transverse tracer. Following the positioning of the vane preform 3a, the operator immobilizes the root portion 13 and the junction 15 of the vane preform 3a by attaching the wedge 21 on the two supports 22 of the mould 11a, the root portion 13 and the junction 15 being then compressed between the indentation 16 and the wedge 21.
During the forming operation, the control method described above is implemented to control the position of the vane preform 3a following its positioning, and in other words following the placement of the wedge 21 on the two supports 22.
Indeed, an operator controls that the lower transverse tracer 2a is well within the interval defined by the slit 12, with the help of the screen 9 of the system 1 on which the images filmed by the camera 5 are displayed live.
It is noted that the vane preform 3a is here shaped by an operator who spreads the preform 3a into the indentation 16 until upper longitudinal tracers (not shown) of the preform 3a coincide with references projected onto the mould 11a by one or more lasers. The references projected by the laser or the lasers define the theoretical positions of each of the upper longitudinal tracers.
As shown in
As shown in
As illustrated in
It is noted that the casing preform 3b is here shaped by an operator who wraps the preform 3b around the indentation 23 by making coincide the upper longitudinal tracer 2b of the preform 3b with a reference projected onto the mould 11b by one or more lasers. The reference projected by the laser or the lasers defines the theoretical position of the upper longitudinal tracer 2b.
During the forming operation, the control method described above is implemented to control the forming of the casing preform 3b.
The control device 10 automatically controls that the upper longitudinal tracer 2b is within a predefined range. For this purpose, the control device 10 compares the actual position of the upper longitudinal tracer 2b and the predefined interval. The actual position of the upper longitudinal tracer 2b is determined, for example, from the images taken by the camera 5 and from an image processing software.
In the present application, the terms “lower” and “upper” associated with the preforms 3a, 3b and the moulds 11a, 11b are defined with respect to the positions of the latter in the figures.
It can be seen that the system 1 according to the invention allows to significantly accentuate the white colour of the tracers, and thus to easily locate the tracers of the preform 3, for the purpose, for example, of positioning or controlling the preform 3.
Number | Date | Country | Kind |
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2002177 | Mar 2020 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2021/050345 | 3/1/2021 | WO |