Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
  • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
  • B22F10/20—Direct sintering or melting
  • B22F10/22—Direct deposition of molten metal
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F12/00—Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
  • B22F12/30—Platforms or substrates
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F12/00—Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
  • B22F12/90—Means for process control, e.g. cameras or sensors
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K15/00—Electron-beam welding or cutting
  • B23K15/0046—Welding
  • B23K15/0086—Welding welding for purposes other than joining, e.g. built-up welding
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
  • B23K26/34—Laser welding for purposes other than joining
  • B23K26/342—Build-up welding
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K31/00—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
  • B23K31/003—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups relating to controlling of welding distortion
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
  • B23K9/00—Arc welding or cutting
  • B23K9/04—Welding for other purposes than joining, e.g. built-up welding
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
  • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
  • B23P17/00—Metal-working operations, not covered by a single other subclass or another group in this subclass
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B33—ADDITIVE MANUFACTURING TECHNOLOGY
  • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
  • B33Y10/00—Processes of additive manufacturing
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B33—ADDITIVE MANUFACTURING TECHNOLOGY
  • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
  • B33Y30/00—Apparatus for additive manufacturing; Details thereof or accessories therefor
• • Y—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
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
  • Y02P10/00—Technologies related to metal processing
  • Y02P10/25—Process efficiency

Definitions

• the present invention relates to the technical field of additive manufacturing.
• additive manufacturing processes are the opposite of material removal or subtractive processes, which make it possible to obtain metallic objects from thick plates or hollow cylinders.
• Metallic objects can also be obtained from rough roughed in forging or foundry rough close to the coast.
• the solidification of the metal after its deposition causes strong constraints linked to the phase change and to the temperature gradients, and therefore to deformations of the support.
• Another solution consists in clamping the support on a tool to contain the deformation of the support during the deposition of the wire or the powder, the assembly then undergoing a stress relieving heat treatment.
• This solution therefore requires specific tools made of a material chosen to hold mechanically during the heat treatment. It is expensive because of this tool. Indeed, it has a large amount of material to ensure its rigidity and its cost is therefore high.
• the tooling must be present during the heat treatment of the support and this treatment during several hours, a large number of tools must be provided, which increases the manufacturing cost.
• the object of the invention is to overcome these drawbacks by proposing a radically different and highly efficient additive manufacturing process.
• the invention relates to a method of manufacturing at least one blank of a final metallic object from a digital object, said blank comprising at least two separate stacks of layers superimposed on a metallic support, the method comprising successive stages of depositing molten metallic material on said support by local supply of metallic material, combined with a local supply of energy, said support defining two opposite faces, the method being characterized in that the deposit of material is produced on both sides of the support to produce at least one stack on each face, in that the support is at least partially integrated into said blank and in that all of the material in at least one stack is absent from the final object obtained after machining the blank.
• This process thus makes it possible to control the overall deformation of the support by appropriately depositing the material on the two surfaces of the support and without the need to increase its thickness.
• the method can be implemented to produce two blanks.
• the support is then separated into two parts, each of which includes one of the faces of the support and the stack (s) produced on this face of the support and forming a blank.
• the latter will be at least partially part of the blank leading to the production of a final object after machining.
• all of the material deposited on one side is absent from the final object obtained after machining the blank including the other side of the support.
• this material absent from the final object played the function of a rectifier for this draft from which this final object came.
• At least one face of the support is made at least one stack which will at least partially form part of the final object as well as at least one stack forming a rectifier.
• all of the material of the stack corresponding to the rectifier is absent from the final object obtained after machining the blank, while the stack present on the first face will be at least partially part of the blank .
• At least one stack forming a rectifier will also be produced on the first face of the support and all of the material of the stack corresponding to the rectifier will be absent from the final object obtained after machining the blank.
• a deposit of material on one side is carried out to compensate for the deformations linked to a deposit of material on the other side.
• the invention relates to a method of manufacturing at least one blank of a final metallic object from a digital object, said blank comprising at least two separate stacks of layers superimposed on a metallic support, the method comprising successive stages of depositing molten metallic material on said support by local supply of metallic material, combined with a local supply of energy, said support defining two opposite faces, the method being characterized in that the deposit of material is produced on both sides of the support to produce at least one stack on each side, in that at least one of the stacks produced on one side will be at least partially part of the final object and in that at at least one stack forms a rectifier, all of the material of which is absent from the final object obtained after machining the blank.
• the method is implemented with a support which is permanently free on its two faces.
• a large part of the surface of each face of the support is devoid of tools, this part being between 60 and 100%.
• the tooling is essentially intended to maintain the support in a determined frame of reference. It is not designed to prevent it from deforming. This is why the tooling can be provided on the periphery of the support, or even on its edge, which makes it possible to free the two faces of the support. It is also designed to adapt to deformations of the support.
• the two faces of the support can therefore receive a deposit of material without it being necessary to dismantle a tool beforehand.
• one or more of the following provisions is used:
• the successive steps of depositing metallic material can be carried out at least in part simultaneously on the two faces of the support
• At least one of said stacks is constructed in a direction which is not opposite to that of gravity
• the support is arranged substantially horizontally or vertically
• the metallic material is brought in the form of wire or powder the deposition steps are carried out by one device or by a plurality of additive manufacturing devices
• At least one additive manufacturing device is controlled according to pre-established control software
• At least one additive manufacturing device is controlled by measurements from sensors arranged near the support.
• the invention also relates to a blank manufacturing system comprising a metal support which will be at least partially integrated in the blank and at least one additive manufacturing device designed to deposit a metallic material on said support in a direction which is not opposite to that of gravity.
• FIG. 1 schematically illustrates a first example of implementation of the method according to the invention.
• FIG. 2 schematically illustrates a second example of implementation of the method according to the invention.
• FIG. 3 which corresponds to FIGS. 3A to 3D, schematically illustrates a third example of implementation of the method according to the invention.
• FIG. 4 is a perspective view illustrating an example of a final part produced from a crude obtained with a method according to the invention.
• FIG. 5 includes FIGS. 5A and 5B which are perspective views of a theoretical blank corresponding to the final part illustrated in FIG. 4.
• FIG. 6 comprises FIGS. 6A and 6B which are perspective views of a blank obtained by a conventional additive manufacturing process, on the basis of the theoretical blank illustrated in FIG. 5.
• Figure 7 includes Figures 7A and 7B which are sectional views along lines A-A and B-B of Figure 6B respectively.
• FIG. 9 is a perspective view showing a variant of Figure 6B, with a longer support.
• FIG. 9 comprises FIGS. 9A and 9B which are sectional views along lines AA and BB respectively of FIG. 8.
• Figure 10 is a perspective view of a blank obtained by a manufacturing process according to the invention, providing for the formation of rectifiers.
• Figure 11 is a perspective view of a blank obtained by a manufacturing process according to the invention, providing for the formation of rectifiers.
• FIG. 12 includes FIGS. 12A and 12B which are sectional views corresponding to FIGS. 7A and 7B as well as FIGS. 12C and 12D which are sectional views along lines C-C and D-D of FIG. 11.
• FIG. 13 is a perspective view of a variant of the blank illustrated in FIGS. 10 and 11.
• FIG. 14 is a perspective view of a variant of the blank illustrated in FIGS. 10 and 11.
• FIG. 15 is a graph schematically illustrating the deformations of a support after implementation of the method according to the invention.
• FIG. 1 illustrates a metal support 1, for example made of TA6V.
• the thickness of this substrate is less than 20 mm.
• the support 1 is substantially planar and defines two opposite faces 10 and 11 also substantially planar.
• the invention is not however limited to this embodiment and the support is not necessarily planar. On the other hand, it must have facing surfaces.
• the thickness of the support is not necessarily constant.
• the support may result from the slanting of a plate.
• the support 1 is arranged substantially horizontally. In other words, it defines a plane that is substantially perpendicular to the direction of the force of gravity (illustrated by arrow G).
• FIG. 1 also illustrates two devices 20 and 21 for additive manufacturing.
• the first device 20 is arranged above the upper face 10 of the support, while the second device 21 is arranged below the lower face 11 of the support.
• energy source for example electron beam, laser, plasma, electric arc or hot carrier gas. If one of these devices has several sources of energy, these can be different from each other.
• each of these devices includes means for bringing the metal onto the support, in the form of powder or wire.
• This metal will be melted thanks to the energy source present in the device 20 or 21, in order to deposit it on the support 1.
• the support 1 is fixed in rotation.
• the support 1 and the devices 20 and 21 are movable in translation relative to each other. In the example shown, it is the devices 20 and 21 which are movable in translation, the support 1 being fixed.
• the first device 20 was controlled to produce a stack 12 formed here of four layers superimposed 120 to 23, while the second device 21 has been piloted to produce on the lower face 11 of the support 1 a stack 13, itself formed of successive layers 130 to 133.
• the arrow F12 indicates the direction in which the stack 12 is constructed, or in other words, the direction defined by the succession or the progression of the layers 120 to 123 from the support 1.
• Each layer corresponds to a deposition cycle during which the entire desired surface of the support or of the previous layer is covered with a bead of metallic material of a determined height, this height being defined in a direction perpendicular to the support. This height can vary from one layer to another, this variation being generally of small amplitude.
• the direction of construction of the stack 12 is therefore opposite to the direction of gravity, this opposite direction being materialized by the arrow G ’.
• the direction of construction of the stack 13 is, for its part, materialized by the arrow F13 and it corresponds to the direction of gravity, materialized by the arrow G.
• the stacks 12 and 13 constitute two distinct stacks, that is to say that they are produced independently of one another or that there is a discontinuity between the material forming the first layer 120 of the stack 12 and the material forming the first layer 130 of the stack 13.
• the invention is of course not limited to this mode of implementation and several separate stacks could be made on one face of the support or on both.
• the direction of construction of the stacks is not necessarily perpendicular to the support but may form an angle to the support which is less than 90 °.
• the control of the two devices 20 and 21 is carried out to minimize the deformation of the support 1.
• the layers of the same rank of each of the stacks 12 and 13 can be produced simultaneously both to compensate for the deformations of the support and to obtain greater productivity in the manufacture of the blanks.
• a simultaneous deposition of material on both sides of the support requires prior knowledge of the deformations caused by the deposition of material.
• the method according to the invention does not provide for limiting or eliminating the deformations of the support, by stiffening it either by increasing the thickness of the support or by clamping it with suitable tools. Its effect is to compensate for a deformation occurring in one direction by a deformation occurring in an opposite direction in order to control the overall deformation of the support.
• the two devices 20 and 21 can be controlled so as to alternate the simultaneous deposition of layers on each face of the support and a deposition shifted in time.
• the number of successive layers constructed by a device 20 or 21 on the same face, between two deposition phases on the other face of the support is determined as a function of the blank to be constructed, taking into account its geometry, the temperature constraints and the tolerances fixed for the deformations.
• an additive manufacturing device is provided for each face of the substrate 1.
• the invention is not limited to this method of implementing the method and it could be implemented with a single device.
• more than one additive manufacturing device can also be provided for each face of the substrate. These devices can be the same or different.
• the devices 20 and 21 can be different.
• the additive manufacturing devices can be identical or different.
• energy sources can be different from one device to another.
• the nature and composition of the filler materials may differ from one additive manufacturing device to another.
• the method according to the invention is not however limited to these applications. It can also be implemented to produce at least one stack on each face of the support, a cut in the plane of the support then being carried out to obtain two blanks, each of which therefore comprises a part of the support. If the stacks are symmetrical with respect to the support, they will also make it possible to obtain two substantially symmetrical parts, after machining.
• the support material is at least partially integrated into the blank.
• the method effectively allows the support to be cut into two parts, while the thickness of the support is reduced compared to conventional methods.
• the method according to the invention can be implemented on supports the thickness of which is globally or locally less than 10 mm even if the length of the support reaches 500 mm for example, with a width of 400 mm.
• supports with a thickness greater than 15 mm or even 20 mm must otherwise be used in this case.
• the invention could achieve the same effects with greater lengths, for example equal to 1 m.
• FIG. 2 illustrates another embodiment of the method according to the invention in which the support 3 is arranged substantially vertically or even substantially in the direction of the force of gravity.
• the support 3 remains fixed in rotation throughout the implementation of the method.
• the support 3 on the one hand, and the devices 40 and 41 on the other hand are relatively mobile in translation.
• the support 3 is fixed and the devices are movable in translation.
• the invention is not limited to this mode of implementation of the method and the support could be movable in rotation about an axis.
• the method according to the invention has the advantage of being able to be implemented with a fixed support both in rotation and in translation.
• the support 3 is substantially planar and defines two opposite faces 30 and 31 whose spacing corresponds to the thickness of the support.
• An additive manufacturing device is provided on the side of each lateral face of the support.
• a device 40 is provided on the side of the left side face 30 of the support and another additive manufacturing device 41 is provided on the side of the right side face 31 of the support.
• the device 40 allows the construction 32 to be carried out on the face 30 of the support 3 and the device 41 allows the construction 33 to be carried out on the face 31 of the support.
• Each of these constructions is formed by a succession of layers 320 to 323 for the stack 32 and 330 to 333 for the stack 33.
• a construction direction is defined which corresponds to the direction in which the height of the stack increases relative to the support.
• the direction of construction of the stack 32 is illustrated by the arrow F32. This arrow is horizontal and it starts from the left lateral face 30 of the support 3 towards the outside.
• the arrow F33 illustrates the direction of construction of the stack 33. It is horizontal and starts from the right lateral face 31 of the support 3 while going outwards.
• the method according to the invention is not limited to the two modes of implementation illustrated in FIGS. 1 and 2, that is to say to a support arranged substantially in the direction of the force of gravity or in a perpendicular direction. to this force.
• FIG. 3 illustrates in more detail the mode of implementation of the method in which the different layers are deposited alternately on each face of a support.
• FIGS. 3A to 3D illustrate a support 5 arranged substantially horizontally, like the support 1 illustrated in FIG. 1.
• This support defines two planar opposite faces, the upper face 50 and the lower face 51.
• FIG. 3A illustrates a first step in which a first layer 520 is deposited on the upper face 50 of the support 5.
• FIG. 3B illustrates a second step of the method in which a first layer 530 is deposited on the lower face 51 of the support.
• FIG. 3C illustrates a third step in implementing the method in which a second layer 521 is deposited on the first layer 520 previously deposited on the upper face 50 of the support.
• FIG. 3D illustrates a fourth step in implementing the method in which a second layer 531 is deposited on the first layer 530 previously deposited on the underside 51 of the support 5.
• the stacks 52 and 53 obtained are symmetrical with respect to the support 5.
• the direction of construction F52 of the stack 52 is therefore opposite to the direction of gravity, this opposite direction being materialized by the arrow G ’.
• the direction of construction F53 of the stack 53 is, for its part, materialized by the arrow F53 and it corresponds to the direction of gravity, materialized by the arrow G.
• the method according to the invention is not limited to this mode of implementation.
• it is possible to control the deformations of the support, even in the case where the stacks are not symmetrical with respect to the support. This will be illustrated in the following description.
• It can be a single device, two devices each provided for one face of the support or a plurality of devices provided on at least one face of the support.
• FIGS. 4 to 12 describe another embodiment of the invention in which a stack is produced on one face of the support, this stack being intended to form at least partially the final part, l 'other side of the support receiving stacks which have a rectifier function, that is to say intended to compensate for the deformations of the support linked to the formation of the stack. These rectifiers will be absent from the final part.
• a theoretical blank can be designed which can be produced by forging or by additive manufacturing.
• the design of the blank integrates the manufacturing constraints of the blank, for example the undercuts or the joint planes, depending on the process used.
• FIG. 5 illustrates how the theoretical outline of the part 6 illustrated in FIG. 4 is designed, when the latter is intended to be produced by additive manufacturing.
• FIG. 5A illustrates a planar support 7 defining an upper face 70 also planar on which a stack 8 of four layers is provided, each layer forming a square.
• the stack 8 comprises two pairs of facing walls: the walls 80,81, on the one hand and the walls 82,83, on the other hand.
• FIG. 5B is a view similar to FIG. 5A in which the final part 6 is drawn in dotted lines inside the stack and the support.
• the thickness of the support in the theoretical blank will be 10 mm (an additional thickness of 0.5 mm is required on each face to carry out the machining, an additional thickness of 3 mm is also necessary on each face to carry out a control by ultrasound).
• the deformation of the support can be so great that the desired part cannot be obtained after machining.
• FIG. 6A shows that the support 7 now has a concave shape and that the walls of the stack 8 are also deformed.
• FIG. 6B illustrates the relative position of the blank and of the final part 6.
• the shaded areas correspond to the parts of part 6 which cannot be obtained due to the deformation of the support 7.
• Figures 7A and 7B provide a better view of the locations where the material is lacking to obtain the final part. It should be emphasized that this phenomenon is even more accentuated when the length of the support increases.
• FIG. 8 shows that the support 7 ’, which has the same width as the support 7 but a greater length, has a concave shape more accentuated than that of the support 7.
• FIGS. 9A and 9B make it possible to better visualize the locations where the material is lacking to obtain the final part.
• the method according to the invention consists in producing not only the stack 8 on the upper face 70 of the support, as provided in the theoretical blank illustrated in FIG. Figure 5, but also several stacks 90 to 97 on the opposite face 71 of the support.
• These stacks have a rectifier function, that is to say that they are provided to compensate for the deformation of the support during the formation of the stack 8 on the face 70 of the support.
• the direction of construction Fs of the stack 8 is therefore opposite to the direction of gravity, this opposite direction being materialized by the arrow G ’.
• the direction of construction F9 of the rectifiers is, in turn, materialized by the arrow F9 and it corresponds to the direction of gravity, materialized by the arrow G.
• two rectifiers 90 and 91 are substantially in line with the walls 80 and 81 of the stack and centered with respect to them, while two other rectifiers 92 and 93 are substantially in line walls 82 and 83 of the stack and centered with respect thereto.
• a pair of rectifiers 94.95 and 96.97 respectively is provided between an edge 72.73 of the support 7 and the rectifiers 90 to 93.
• FIGS. 12A and 12C make it possible to compare the deformations of the support along its length, with a conventional method (FIG. 12A) and with the method according to the invention (FIG. 12C) which provides for the production of rectifiers 90, 91 on the face of the support. opposite stacking.
• FIGS. 12B and 12D make it possible to compare the deformations of the support according to its width, with a conventional method (FIG. 12B) and with the method according to the invention (FIG. 12D). In both cases, the thickness of the support is that calculated for the theoretical blank.
• FIGS. 13 and 14 illustrate a variant implementation of the method illustrated in FIGS. 10 and 11.
• the method according to the invention here consists in making the stack 8 on the upper face 70 of the support, as provided in the theoretical blank illustrated in FIG. 5, but also several stacks 90 'to 93' inside the stack 8 and several stacks 94 'to 97' on the opposite face 71 of the support.
• These stacks 90 ’to 97’ again have a rectifier function, that is to say that they are provided to compensate for the deformation of the support during the formation of the stack 8 on the face 70 of the support.
• the rectifiers placed inside the stack form two pairs, respectively 90 ', 91' and 92 ', 93', arranged along two diagonals of the square formed by the stack 8 and perpendicular to each other.
• a pair of rectifiers 94 ', 95' and 96 ', 97' respectively is provided between an edge 72,73 of the support 7 and the rectifiers 90 'to 93'.
• FIG. 15 schematically illustrates the deformations of the support when the method according to the invention is implemented.
• This figure thus illustrates (in dotted lines) a support 7 used in the context of the method according to the invention to produce stacks therein by additive manufacturing (these stacks are not illustrated in the figure).
• This support is substantially identical to that of the theoretical blank, for example that illustrated in FIG. 5.
• This thickness is for example substantially equal to 10 mm, like that provided in the theoretical blank, while that required for a conventional process is at least 15 mm.
• part 6 of the support which will be present in the finished part, after machining.
• the upper face 60, respectively the lower face 61 are located at a distance e from the upper face 70 of the support, respectively from its lower face 71. This distance e corresponds to the additional thickness provided for in the theoretical blank.
• the support is shown in solid lines at the end of the implementation of the method, that is to say when both the stacks and the rectifiers have been formed, as illustrated for example in FIGS. 10 , 11 and 13.14.
• This support 7A is deformed. However, at any point on the upper face 70A or on the lower face 71 A of the support, its deformation dy is less than the value e of the additional thickness.
• the deformations dy 0 and dy n are illustrated in FIG. 15 at two different points on the support. These two deformations occur in opposite directions.
• the support 7A has alternating deformations, which gives it a general shape of a sinusoid while the support illustrated for example in Figures 12A and 12B is deformed in one direction and has a general shape in a bowl.
• the faces of the deformed support frame the faces of the support after machining or, in other words, stay away from these faces 60 and 61, which makes it possible to effectively obtain this support after machining. Therefore, inside the support, even deformed, can be obtained the part of the support intended to be present in the final part.
• the rectifiers can be made of a material whose cost is lower than that of the material actually forming the, final part since they are intended to be eliminated during the machining of the blank.
• a material distributed in a specific way in the space which will be present in the final object after machining with the exception of the part of the material forming extra thicknesses and extra lengths compared to the final object or planned to take into account the constraints linked to the process used. For example, it may be an undercut necessary to ensure the release of the part when it is obtained by forging.
• the blank may include a stack, the material of which will be completely absent from the final object. This is the case when this stack constitutes a rectifier whose presence is provided to compensate for the deformation of the support.
• the latter type of software allows continuous adjustment of the control of additive manufacturing devices.
• some areas of the blank can be built more or less quickly and the amount of energy delivered by the additive manufacturing devices can also be limited if necessary.
• This software can implement known digital simulation tools such as the SYSWELD software from the company ESI or the ABAQUS software.
• the SYSWELD software is a multi-physical software for analyzing finite elements which is conventionally used for welding and is therefore suitable for the additive manufacturing technique with the addition of wire.
• the ABAQUS software also makes it possible to model the deformations and the stresses.

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• Engineering & Computer Science (AREA)
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• Analytical Chemistry (AREA)
• Automation & Control Theory (AREA)
• Optics & Photonics (AREA)
• Plasma & Fusion (AREA)
• Powder Metallurgy (AREA)

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• 2018
  • 2018-12-20 FR FR1873679A patent/FR3090438B1/fr active Active
• 2019
  • 2019-12-20 EP EP19845696.4A patent/EP3898072A1/de active Pending
  • 2019-12-20 WO PCT/FR2019/000213 patent/WO2020128169A1/fr unknown

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