DEVICE AND METHOD FOR SHAPING A BLANK FOR THE FORMATION OF A STRUCTURAL THERMOPLASTIC PART
20210237376 · 2021-08-05
Assignee
Inventors
Cpc classification
B29C70/465
PERFORMING OPERATIONS; TRANSPORTING
B29C35/0272
PERFORMING OPERATIONS; TRANSPORTING
B29C70/506
PERFORMING OPERATIONS; TRANSPORTING
B29C31/004
PERFORMING OPERATIONS; TRANSPORTING
B29D99/0003
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
B29C70/085
PERFORMING OPERATIONS; TRANSPORTING
B29C70/24
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A device for shaping a blank for forming a thermoplastic structural part, the blank comprising reinforcing fibres embedded in a thermoplastic matrix, said shaping device comprising a support member for supporting a blank along a longitudinal axis, at least one heating member, at least one inclination member configured to modify the inclination of at least one part of the longitudinal portion of the blank at an angle of inclination that can be parameterised with respect to the horizontal plane in a plane transverse to the longitudinal axis, and a movement system from upstream to downstream along the longitudinal axis of the heating member and of the inclination member relative to the support member so as to successively modify the inclination of a part of each longitudinal portion of the blank.
Claims
1-10. (canceled)
11. A device for shaping a blank for the formation of a structural thermoplastic part, intended to be integrated in a primary structure of an airplane, the blank comprising reinforcing fibres embedded in a thermoplastic matrix, said shaping device comprising: a member for supporting a blank, the support member extending along a longitudinal axis; at least one heating member configured to heat a longitudinal portion of the blank to a temperature making it possible to render the thermoplastic matrix of the blank malleable; at least one inclination member configured to modify the inclination of at least one part of the longitudinal portion of the blank according to an angle of inclination parameterizable with respect to the horizontal plane in a plane transversal to the longitudinal axis; at least one module comprising a frame configured to be displaced by the displacement system, the heating member and the inclination member being connected to said frame; and a system for displacing from upstream to downstream along the longitudinal axis the frame so as to modify successively the inclination of a part of each longitudinal portion of the blank.
12. The shaping device according to claim 11, wherein each inclination member comprises at least one rolling member so as to enable a compression during its displacement by the displacement system.
13. The shaping device according to claim 12, wherein the rolling member extends in a plane transversal to the longitudinal axis.
14. The shaping device according to claim 12, wherein each inclination member comprises at least one parameterizable device for modifying the angle of inclination of the rolling member.
15. The shaping device according to claim 11, comprising at least two inclination members configured to modify the inclination of two side parts of a longitudinal portion of the blank.
16. The shaping device according to claim 11, comprising at least one cooling member configured to cool the local portion of the blank to a temperature making it possible to solidify the thermoplastic matrix of the blank.
17. The shaping device according to claim 11, wherein the heating member has a section hollowed out towards the support member so as to enable uniform heating of a local portion of the blank in the course of its shaping.
18. A method for shaping a structural thermoplastic part, intended to be integrated in a primary structure of an airplane, the blank comprising reinforcing fibres embedded in a thermoplastic matrix, the blank being shaped by the shaping device according to claim 11, the blank being supported on the support member, the method comprising: a step of heating a local portion of the blank to a temperature making it possible to melt the thermoplastic matrix of the blank; then a step of modifying the inclination of at least one part of the longitudinal portion of the blank according to an angle of inclination defined with respect to the horizontal plane in a plane transversal to the longitudinal axis; and a step of displacing from upstream to downstream along the longitudinal axis the heating member and the inclination member relatively to the support member so as to modify successively the inclination of a part of each longitudinal portion of the blank according to the angle of inclination.
19. The shaping method according to claim 18, wherein the method comprises a repetition of the steps of heating, modification of the inclination and displacement, the angle of inclination being increased at each repetition.
20. The shaping method according to claim 18 wherein the support member having a transversal section defining a horizontal upper surface and at least one side surface which is inclined with respect to said horizontal upper surface, the blank is supported on the horizontal upper surface and a part of the blank is progressively inclined up to being pressed against the side surface.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0034] The invention will be better understood on reading the description that follows, given uniquely as an example, and by referring to the appended drawings in which:
[0035]
[0036]
[0037]
[0038]
[0039]
[0040]
[0041]
[0042] It should be noted that the figures set out the invention in a detailed manner for implementing the invention, said figures obviously being able to serve to better define the invention if need be.
DETAILED DESCRIPTION
[0043] In a known manner, a structural thermoplastic part, intended to be integrated in a primary structure of an airplane, is formed from a blank comprising reinforcing fibres embedded in a thermoplastic matrix. As indicated previously, in order to obtain a finished part, the blank has to be heated to a temperature above the melting temperature of the thermoplastic matrix while being compressed in order to increase its density and to make it rigid. As an example, the reinforcing fibres are made of carbon and the matrix is PEEK or PEKK. A blank 1 is not consolidated and is porous.
[0044] In this example, the blank 1 is produced by flat draping of reinforcing fibres pre-impregnated with PEEK or PEKK matrix. Such a draping method is faster and less expensive than three-dimensional draping. After draping, the blank 1 is planar and rigid. The blank 1 is not consolidated.
[0045] As an example, with reference to
[0046] With reference to
[0047] In this example, the shaping device 2 comprises a member for supporting 20 a blank 1 which extends from upstream to downstream along the X axis, a heating member 3, two inclination members 4, 4′ and a system for displacing 9 from upstream to downstream along the longitudinal X axis the heating member 3 and inclination members 4, 4′ relatively to the support member 20 so as to modify successively the inclination of a part of each longitudinal portion of the blank 1.
[0048] With reference to
[0049] Hereafter, the shaping device 2 is defined in an orthogonal reference system X, Y, Z in which the X axis extends longitudinally from upstream to downstream, the Y axis extends laterally from the left to the right and the Z axis extends vertically from the bottom to the top.
[0050] In order to enable optimal shaping of the blank 1 by the shaping device 2, the support member 20 has a rigid structure, in particular, made of metal material in order not to deform during the manufacture. The support member 20 is also called anvil. In this example, the support member 20 has a length greater than 2 m. To facilitate handling, the support member 20 has a length greater than that of the blank 1.
[0051] With reference to
[0052] The heating member 3 is configured to produce heating by induction by circulating a current in a metal element or directly in the reinforcing fibres, but it goes without saying that other heating technologies could be suitable, in particular, by infrared or resistive. In this example, the heating member 3 makes it possible to induce a current in the reinforcing fibres of the blank 1.
[0053] As illustrated in
[0054] It goes without saying that the structure of the heating member 3 could be different as a function of the heating technology employed, for example, resistive or infrared.
[0055] In a preferred manner, the heating member 3 may be coupled to one or more members for measuring the temperature in order to control the temperature during manufacture.
[0056] As illustrated in
[0057] In this example, the inclination members 4, 4′ are configured to fold back the side arms 11, 11′ of the blank 1 against the side surfaces 21, 21′ of the support member 20. The maximum desired angle of inclination is 90°, which corresponds to the angle formed between each side surface 21, 21′ and the horizontal upper surface 22 of the support member 20. It goes without saying that the angles of inclination θ, θ′ of the inclination members 4, 4′ could be different as a function of the desired shaping.
[0058] The inclination members 4, 4′ are all oriented in a plane transversal to the X axis so as to deform successively each longitudinal portion during the relative displacement with respect to the support member 20.
[0059] In this example, with reference to
[0060] In a preferred manner, the rolling member 40, 40′ is in the form of a roller. The parameterizable modification device 41, 41′ is configured to incline gradually the rolling member 40, 40′. Each inclination member 4, 4′ is configured to exert an oblique compression along an oblique axis with respect to the Y and Z axes. In this example, the parameterizable modification device 41, 41′ is in the form of cylinder with a pivot system or an angular variator (electric, hydraulic or pneumatic). Each inclination member 4, 4′ can deform the blank 1 while being displaced longitudinally along the longitudinal X axis on the blank 1.
[0061] As illustrated in
[0062] The pressing members 5, 6 are all oriented in a plane transversal to the X axis so as to compress successively each longitudinal portion.
[0063] In this example, each pressing member 5, 6 comprises a rolling member 50, 60, a pressing member 52, 62 to press the rolling member 50, 60 onto the blank 1 and several members for guiding 51, 61 the rolling member 52, 62. In a preferred manner, the rolling member 50, 60 is in the form of a roller and the pressing member 52, 62 is in the form of a pressure cylinder. The guiding members 51, 61 are for their part in the form of slides so as to allow a displacement of the rolling member 50, 60 uniquely in translation along the axis of the pressing member 50, 60 without turning around said axis. Thus, each pressing member 5, 6 can press the blank 1 while being displaced longitudinally along the X axis on the blank 1. Each pressing member 5, 6 carries out a pressing in a plane transversal to the longitudinal X axis so as to press successively each longitudinal portion of the blank 1.
[0064] With reference to
[0065] The compressive force of each pressing member 5, 6 and each inclination member 4, 4′ may advantageously be adjusted in an individual manner.
[0066] Optionally, with reference to
[0067] The cooling member 7 is in the form of an air discharge pipe oriented vertically downwards so as to cool the base 10 of the blank 1 as well as the side arms 11, 11′ of the blank 1 of which the inclination has been modified. Thus, when a longitudinal portion of the blank 1 is situated under the cooling member 7, it is cooled locally so as to make it rigid and set its structure.
[0068] According to the invention, with reference to
[0069] In an embodiment not represented, the displacement system 9 could be configured to displace the support member 20 whereas the heating member 3, the inclination members 4, 4′, the pressing members 5, 6 and the cooling member 7 remain fixed. Only a relative movement must be carried out to enable the consecutive deformation of each longitudinal portion.
[0070] In this exemplary embodiment, the different members are grouped together into several modules.
[0071] With reference to
[0072] The downstream module 81 comprises a frame 810 which has an inverted U-shape defining a concavity in which is mounted the downstream pressing member 5. The downstream pressing member 5 comprises a rolling member 50, a pressing member 52 connecting the rolling member 50 to the frame 810 and two guiding members 51 connecting the rolling member 50 to the frame 810, in particular, on either side of the pressing member 52. As indicated previously, each rolling member 50 is in the form of a roller, each pressing member 52 is in the form of a cylinder and each guiding member 51 is in the form of a slide.
[0073] The frame 810 of the downstream module 81 is connected to the displacement system 9 in order to enable the displacement of the downstream module 81 along the longitudinal direction X. During the longitudinal displacement along the X axis, the base 10 of the blank 1 is forced by the downstream pressing member 5 against the support member 20, which makes it possible to immobilise it.
[0074] The upstream module 82 comprises a frame 820 which has an inverted U-shape defining a concavity in which are mounted, from downstream to upstream, the heating member 3, the inclination members 4, 4′, the cooling member 7 and the upstream pressing member 6.
[0075] In an analogous manner to the downstream pressing member 5, the upstream pressing member 6 comprises a rolling member 60, a pressing member 62 connecting the rolling member 60 to the frame 820 and two guiding members 61 connecting the rolling member 60 to the frame 820, in particular, on either side of the pressing member 62. As indicated previously, each rolling member 60 is in the form of a roller, each pressing member 62 is in the form of a cylinder and each guiding member 61 is in the form of a slide.
[0076] In an analogous manner to previously, the frame 820 of the upstream module 82 is connected to the displacement system 9 in order to enable the displacement of the upstream module 82 along the longitudinal direction X. During the longitudinal displacement along the X axis, a local portion of the blank 1 is heated by the heating member 3 to a temperature above the melting temperature of the thermoplastic matrix so as to render the blank 1 malleable then directly stressed by the inclination members 4, 4′ in order to fold back in a progressive manner the side arms 11, 11′ of the blank 1 without inducing weaknesses in the blank 1. After deformation, the blank 1 is cooled to a temperature below the glass transition temperature of the thermoplastic matrix in order to fix the deformation obtained. The deformation is controlled in an optimal manner while avoiding any undesired deformation. The upstream pressing member 6 makes it possible, in the same way as the downstream pressing member 5, to immobilise the longitudinal portion which is deformed.
[0077] An exemplary embodiment of a method for shaping a structural thermoplastic part, intended to be integrated in a primary structure of an airplane, will henceforth be described.
[0078] The blank 1 comprises reinforcing fibres embedded in a thermoplastic matrix. The blank 1 is planar and is supported on the support member 20, in particular, on the upper surface 22 as illustrated in
[0079] With reference to
[0080] Each longitudinal portion of the blank 1 is treated consecutively by the downstream module 81 and the upstream module 82. The downstream module 81 presses in a preliminary manner the blank 1 as a whole in order to prepare it for heating. The blank 1 is thus immobilised.
[0081] Then, the heating member 3 of the upstream module 82 heats the local portion of the blank 1 to a temperature above the melting temperature of the thermoplastic matrix (temperature of the order of 360° C.-380° C.) in order to soften the blank 1.
[0082] Next, the inclination members 4, 4′ modify respectively the inclination of the side arms 11, 11′ of the heated longitudinal portion of the blank 1 according to a first angle of inclination θ.sub.1 defined with respect to the horizontal plane in a plane transversal to the longitudinal X axis. The first angle of inclination θ.sub.1 is less than an angular threshold, here of value 15°, so as not to induce weaknesses at the junction of the base 10 and the side arms 11, 11′ of the blank 1. The angular deformation threshold further makes it possible to limit any weakness between two successive longitudinal portions of the blank 1. In the course of the method, the side arms 11, 11′ are further away from the side surfaces 21, 21′ of the support member 20 upstream of the inclination members 4, 4′ than downstream. Thus, the inclination is progressive, which makes it possible to benefit from the thermoplastic matrix which may be rendered malleable in a repeated manner without affecting the mechanical properties of the blank 1. The integrity of the reinforcing fibres is preserved.
[0083] The integration of the inclination members 4, 4′ and a heating member 3 in a same upstream module 82 advantageously enables the inclination members 4, 4′ to deform in an optimal manner the blank 1 which has been rendered malleable. The steps of heating and deformation are directly sequenced together, the thermoplastic matrix not having the time to cool to a temperature below the glass transition temperature of the thermoplastic matrix. In other words, the upstream module 82 makes it possible to modify progressively the inclination of the side arms 11, 11′.
[0084] The cooling member 7 makes it possible to cool the local portion by setting the thermoplastic matrix, said matrix being cooled to a temperature below the glass transition temperature of the thermoplastic matrix. In an analogous manner to the downstream pressing member 5, the upstream pressing member 6 compresses and presses the blank 1 in order to give it its final shape. Any undesired folding or torsion of the blank 1 is thus avoided. Thus, each local portion of the blank 1 is successively heated, deformed and cooled.
[0085] As illustrated in
[0086] In this example, the side arms 11, 11′ are inclined progressively up to being pressed against the side surfaces 21, 21′ of the support part 20. In a preferred manner, between 3 and 5 repetitions are necessary to obtain the desired U-shape. Such a shaping method is thus rapid to implement.
[0087] Moreover, thanks to the invention, each longitudinal portion of the blank 1 may be shaped in a local manner. This is particularly advantageous for the manufacture of parts of large dimensions, it is not necessary to provide an equipment having dimensions greater than the part to manufacture. There thus no long exist constraints linked to the dimensions of the part to shape.
[0088] The invention applies to different structural parts and has an important interest for those of large dimensions, that is to say, having at least one dimension greater than 1 m and, preferably, greater than 5 m.
[0089] Once the blank 1 shaped in a three-dimensional manner, it may be consolidated in order to decrease its porosity, in particular, by means of a device such as described in the patent application FR1852432 of the Applicant. The use of a shaping device and a manufacturing device has synergic effects to reach industrial production throughputs for the manufacture of structural thermoplastic parts.