• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Assembly 4 for densification under load 2, comprising: at least one volume to be densified 5 of pulverulent and / or porous composition, at least one counterform 6 of pulverulent and / or porous composition, having at least one face 7 opposite at least a portion 5 'of said volume 5, said assembly 4 being characterized in that said portion 5' and said face 7 are separated by at least one movable interfacial layer 9.
    公开号:FR3042992A1
    申请号:FR1560564
    申请日:2015-11-04
    公开日:2017-05-05
    发明作者:Claude Estournes；Charles Maniere；Lise Durand
    申请人:Centre National de la Recherche Scientifique CNRS；Universite Paul Sabatier Toulouse III；
    IPC主号:
    专利说明:

    Implementation of a mobile interface for the manufacture of complex parts 1. Domain
    The field of the invention is that of the manufacture of mechanical parts by densification of pulverulent or porous materials.
    More particularly, the invention relates to the improvement of an assembly of pulverulent or porous materials adapted to be densified under load, both in its implementation and in the technical characteristics of the mechanical parts obtained. 2. Prior Art
    Many processes for densifying powders or porous materials are now known and used daily in the industry. These processes include forging, hot pressing, Hot Isostatic Pressing and flash sintering, also known as Spark Plasma Sintering (SPS). ) in the following description and are intended to consolidate a defined volume of metal powders, ceramics, or polymers, by heating the latter and application of a uniaxial or multiaxial pressure.
    The SPS in particular is known for subjecting a cylindrical volume of compressed powders to a pulsed current making it possible to significantly increase the densification kinetics of these powders and thus to obtain mechanical parts whose fine microstructures are preserved. However, the densification methods implemented by the SPS have the disadvantage of causing densification inhomogeneities in the case of parts of complex shapes with significant differences in thicknesses. Thus, according to the publication "A Numerical Model for Powder Densification by SPS Technique", by P. Mondalek, L. Silva, M. Bellet, Advanced Engineering Materials. 13 (2011), a cylindrical T shape has at the end of sintering a porous zone of relative density of the order of 70%. To better understand this phenomenon, a simulation involving a cylindrical piece having a step is implemented. The initial assembly geometry of the SPS, as well as the densification field and the vertical displacement field at the end of the cycle, are illustrated in FIGS. 1 to 3. The simulation consists of a purely mechanical model, with a prescribed temperature cycle. on all geometry. The boundary conditions consist of a displacement fixed along the z axis of the cylinder of the lower piston and a compressive force is applied to the top face of a cylindrical volume of alumina powder. Lateral conditions are conditions of non-penetration. The thermal cycle is defined according to a temperature rise of 100 K / min up to 1400 ° C, followed by a 5 minute step. The applied force is 18000 N. It is observed that in the final state, the zone of smaller thickness is dense and the zone of high height is porous with a relative density of the order of 80% (FIG. 2). The vertical displacement field (Figure 3) results in strongly curved iso-displacement lines that contrast with the lines of a cylindrical sample without friction, where the iso-displacement lines are horizontal. This result is explained by the non-uniformity of the withdrawal observed between the two zones of different heights. Thus, the low-rise zone densifies more rapidly because, with equal displacement, its maximum retraction distance is reached more quickly than within the high-rise zone. Thus, once the area of low height completely densified, the sintering stops and the high-rise area requiring more removal can not complete its densification process. The heterogeneity of the densification field highlighted by the simulation results from this phenomenon. In the context of such an assembly, the production of parts of complex shapes by the conventional SPS process is therefore made difficult when the geometries of the parts to be manufactured have height differences involving different withdrawals.
    There is therefore a need to overcome the densification heterogeneity of known densification processes under load. 3. Summary
    The proposed technique does not have these disadvantages of the prior art. More particularly, in at least one embodiment, the proposed technique relates to an assembly for densification under load, comprising: at least one volume to be densified with a powdery and / or porous composition, at least one counter-form of composition pulverulent and / or porous, having at least one face facing at least a portion of said volume, said assembly being characterized in that said portion and said face are separated by at least one movable interfacial layer.
    The term "densification process under load" is understood to mean any method of sintering under load or creep aimed at consolidating a defined volume of metal powders, ceramics, or polymers, by heating the latter and applying a uniaxial, multiaxial pressure. or isostatic. These methods include forging, hot pressing, hot isostatic pressing, SPS, or any other known method according to this same general principle of operation. The invention thus relates to an assembly adapted to the implementation of such densification processes under load, and having specific technical characteristics (melting point, thermal capacity, activation energy, etc.) enabling it to withstand important thermal constraints (ex: sudden rise in temperature, of the order of a thousand degrees) and mechanical (compression of the order of tens of thousands of Newtons).
    The terms "volume to be densified" denote a volume of powders and / or porous material intended to form a mechanical part following the implementation of the densification process, hence an equivalent designation by the terms "part to be formed" in the present description. A portion of this volume, that is to say all or part of its outer surface, has a shape complementarity with at least one face of a counterform. According to a particular embodiment, the assembly may also comprise a plurality of counterforms. An interfacial layer acts as a separation between this portion of the workpiece to form against the form. The movability of the interfacial layer results in a negligible thickness, chemical reactivity and compaction capacity with respect to the materials used in the respective compositions of the volume to be densified and counterformed. During the densification of the assembly, this mobile interfacial layer will thus move and follow the shrinkage of the volume to be densified to form a counter-shape of the relevant portion of the part to be manufactured, once the densification process completed. The displacement of the interfacial layer makes it possible to distribute homogeneously over the part to be formed all the stresses transmitted by the counterform and the tooling used for densification under load (piston-matrix). The resulting part consequently has a shrinkage homothety over its entire surface (portion) in contact with the interfacial layer. In a complementary manner, the faults and fractures that can be generated within the counter-form during the densification process and / or a subsequent fracturing step are all or partly blocked by the mobile interfacial layer and therefore do not propagate. not in the part to be formed, whose surface appearance, and more generally the microstructure, are preserved. Finally, such an assembly allows the simultaneous manufacture of one or more pieces of potentially complex shape, in the context of a densification process under load whose compression directions are limited (example: uniaxial compression).
    The present invention thus relies on a novel and inventive concept which consists in providing an assembly for densification under load, implementing a mobile interfacial layer, allowing the simultaneous manufacture of one or more pieces of potentially complex shape, said parts having a densification homothety and a preserved microstructure. Such an assembly has the particular advantage of being able to be implemented in the context of a densification process under load of limited complexity.
    According to a particular characteristic of the invention, the counter-form encompasses the volume in its entirety.
    According to another particular characteristic of the invention, the counter-form includes only part of the volume to be densified.
    Such a configuration thus allows the manufacture of parts whose entire periphery has densification homothétie.
    According to a particular characteristic, the volume to be densified and the counter-form are of identical composition.
    The use of materials of the same composition for the workpiece and the counterform (s) has the advantage of facilitating the prediction of material withdrawals generated during the densification step.
    Alternatively, the volume to be densified and the counterform are of different compositions.
    The use of materials of different compositions makes it possible to broaden the possibilities presented to the designer in the choice of materials used in the composition of the part to be formed or in that of the counter-form. It is thus possible to implement, for the constitution of the workpiece, a material having advanced technical properties, while selecting, for the constitution of the counterform, a material at reduced cost.
    Advantageously, the rate of densification of the material constituting said volume is greater than the rate of densification of the material constituting said counter-form.
    In the context of the implementation of two different materials for the volume to be densified and counterformed, it is advantageous to prefer a densifying counterform material at the same speed or more slowly than the material of the part to be formed. , in order to keep a good control of the densification of the part to be formed. It should also be ensured that these materials do not interact chemically with the interface material, an interaction that could potentially affect the separability of the final pieces.
    According to a particular characteristic, said portion and said face are separated by a plurality of mobile interfacial layers.
    According to one particular characteristic, the assembly comprises a plurality of volumes to be densified and at least one counterform, all of powdery and / or porous composition, said counterform having at least one face facing at least a portion of each of said volumes, and said faces and each of said portions are separated by at least one mobile interfacial layer.
    The simultaneous manufacture of a plurality of parts thus makes it possible to increase the hourly efficiency of the manufacturing method implementing such an assembly. The invention also relates to a method for manufacturing at least one part, characterized in that it comprises at least one step of densification under load of an assembly comprising: at least one volume to be densified with a powder composition and or porous, at least one counterform of pulverulent and / or porous composition, having at least one face facing at least a portion of said volume, at least one movable interfacial layer separating said portion from said face. The invention also relates to a method for manufacturing at least one part, characterized in that it comprises: a step of incorporation within an assembly for densification under load, of a mobile interfacial layer separating at least a portion of a volume to be densified of powdery and / or porous composition, of at least one face of a counterform of pulverulent and / or porous composition, • a step of densification under load of said assembly.
    The implementation of such a step of incorporating the mobile interfacial layer is particularly complex, given the need to adapt the latter to the different materials constituting the workpiece, against-shape, and this interfacial layer.
    Thus, according to a particular embodiment, said incorporation step is carried out by pulverulent deposition of said interfacial layer (s) on the zone (s) of said counterpart (s). form (s) placed next to the piece to be formed but also between counterforms if necessary.
    According to an alternative embodiment, said step of incorporation is carried out by insertion within said assembly of one or more solid interfacial layer, preferably a flexible graphite sheet (ex: Papyex ®), prior to a step filling said assembly with the materials respectively constituting the workpiece and the counterform (s).
    According to a particular embodiment, the manufacturing method comprises a step of extracting said part from said assembly, by sacrificial destruction of said counter-form (s) and / or the said one (s) interfacial layer (s) moving (s).
    In the context of an assembly known from the state of the art, the risks of embrittlement of the part to be formed caused by the propagation of cracks from the counterform (s) to the part to be formed, following the fracturing step, are known to those skilled in the art. In the context of the invention, knowledge of these risks would have diverted the skilled person from this technical solution, and encouraged the latter to consider an alternative means of extraction of the formed part since assembly.
    Although not described explicitly, the various embodiments described above can be implemented in any combination, or sub-combination. 4. Figures Other characteristics and advantages of the invention will emerge more clearly on reading the following description of particular embodiments, given as simple illustrative and non-limiting examples, and the appended figures, namely:
    Figure 1 - Schematic view of an initial assembly for SPS of the state of the art using a cylindrical piece having a step.
    Figure 2 - Simulation illustrating the relative density field at the end of sintering of a cylindrical piece having a step.
    FIG. 3 - Simulation illustrating the vertical displacement field at the end of sintering of a cylindrical part having a step,
    FIG. 4 - Schematic view of the successive steps of shaping an assembly according to a particular embodiment of the invention,
    FIG. 5 - Series of photographs illustrating the step of extracting a mechanical part following the densification under load of an assembly according to a particular embodiment of the invention,
    Figure 6 - Series of photographs illustrating the imprint that can generate the initial shape of the workpiece and the formed part after densification of an assembly according to a particular embodiment of the invention.
    Figure 7 - Schematic view of the successive steps of shaping an assembly according to an alternative embodiment of the invention.
    Figure 8 - Photograph illustrating a conical piece, as well as fragments of the counter-form, obtained following the densification under load of an assembly according to a particular embodiment of the invention,
    Figure 9 - Photograph illustrating a pyramidal piece with a square base, as well as fragments of the counter-form, obtained following the densification under load of an assembly according to a particular embodiment of the invention,
    FIG. 10 - Photograph illustrating a piece of pyramidal shape with a star base obtained after densification under load of an assembly according to a particular embodiment of the invention,
    FIG. 11 - Photograph illustrating two fragments of the counter-form obtained following the densification under load of an assembly according to a particular embodiment of the invention,
    Figure 12 - Image performed via a scanning electron microscope (SEM) of the microstructure of a fracture present on a pyramid sacrificial portion following the densification under load of an assembly according to a particular embodiment of the invention.
    Figure 13 - Photograph illustrating a cone of 99% dense zirconia and part of the counter-form (98% dense alumina), obtained following the densification under load of an assembly according to a particular embodiment of the invention. 'invention,
    Figure 14 - SEM image of the microstructure of a deliberately induced fracture in the center of a zirconia cone following the densification under load of an assembly according to a particular embodiment of the invention.
    Figure 15 - SEM image of the microstructure of a fracture voluntarily provoked at the edge in the thin zones of a zirconia cone following the densification under load of an assembly according to a particular embodiment of the invention.
    The various elements illustrated by the figures are not necessarily represented on a real scale, the emphasis being more on the representation of the general operation of the invention. 5. Detailed Description of Particular Embodiments of the Invention
    Several particular embodiments of the invention are presented hereinafter and relate to the manufacture 1 via a SPS 2 process of mechanical parts 3 in the shape of a hemisphere, cone, square-based pyramid, and pyramid with starry base. It is understood that the present invention is not limited by these particular embodiments and that other embodiments can be implemented perfectly.
    Thus, and according to alternative embodiments, the invention relates to the manufacture 1 of parts 3 may have a wide variety of shapes, with possible adaptations of the manufacturing method 1 according to the degree of complexity of these forms. The complexity of shape increases for parts with: • A flat base, no difference in height • A constant thickness, but a non-flat base, • A flat base with differences in heights and remains (easy to unmold) • A non-planar base with differences in heights and undercuts (easy to unmold) • A flat base with differences in height but without stripping (needs to segment the sacrificial part) • A non-planar base without stripping (needs to segment the sacrificial part) • A hollow form (two or more parts requiring an additional assembly step).
    Similarly, the densification step 2 is not limited to the SPS, but also relates to forging, hot pressing, hot isostatic pressing, or any other known method of consolidation and / or creep of pulverulent materials. and / or porous. 5.1 SPS sintering of a half-sphere
    FIG. 4 illustrates the subsequent steps of a manufacturing method 1 aimed at densifying an assembly 4 by the implementation of an SPS 2 process, in order to obtain a half-sphere 3 made of poly methyl methacrylate (PMMA) .
    It should be pointed out that obtaining a dense semi-sphere by SPS technology is very difficult, within the limits of the manufacturing processes known in the state of the art, especially in view of the rapid densification of the periphery of the volume. 5 of powder intended to form the half-sphere 3 which prematurely blocks the densification process 2. The approach adopted by the inventors consists in placing in a cylindrical mold 8 a half-ellipsoid 5 of PMMA powder and a counterpoise porous sacrificial form 6 integrating a face 7 facing the half-ellipsoid, with a movable interfacial layer 9 for demolding the obtained part 3 and the sacrificial counterform 6 after sintering.
    According to alternative embodiments of the invention, the PMMA powder used in the composition of the part to be formed can be replaced by alumina powder, zirconia powder, or by any other known pulverulent and / or porous composition. . Similarly, the counterform 6 may consist of any type of known powdery and / or porous material, preferably having a densification curve close to that of the material constituting the workpiece 5 and that, preferably, the formed pair is composed of two materials of the same class (eg metal / metal or ceramic / ceramic or polymer / polymer).
    According to the present embodiment, the half-ellipsoid shape has been chosen because it is the stretched shape of the desired half-sphere. In the case of uniaxial compression, shape and counter-form with close densification properties, the stretching height (h |) is related to the initial and final relative densities of the part (d ,, df) and at the desired final height (hf), by the following formula: h / = h /, d // d /
    In a complementary way, the COMSOL multiphysics® simulation software makes it possible to simulate the shrinkage distances and the deformations induced on a given volume following the implementation of a densification process. The publications "Temperature Control in Spark Plasma Sintering: an FEM Approach", by G. Molenat, L. Durand, J. Galy, A. Couret, Journal of Metallurgy, 2010 (2010), "Electro-thermal measurements and finite element method simulations of a spark plasma sintering device "by A. Pavia, L. Durand, F. Ajustron, V. Bley, A. Peigney, C. Estournès, Journal of Materials Processing Technology, 213 (8), (2013), 1327 -1336, and "Temperature control during Spark Plasma Sintering and application to up-scaling and complex shaping" by T. Voisin, L. Durand, N. Karnatak, S. Le Gallet, M. Thomas, Y. Le Berre, et al. , Journal of Materials Processing Technology, 213 (2013) also deal with this issue, and in view of this simulation software and the three articles above, a skilled person thus has the necessary elements to determine the conformation of the volume of powder. initial 5 depending on the desired shape of the part 3 to manufacture and the ratio of densities.
    During a first phase of the manufacturing process 1, the PMMA powder is introduced into a graphite mold 8. Preferably, one or more binders such as water, Rhodoviol ™, may be incorporated into the powder mixture in order to improve the technical characteristics. Subsequently, an imprint is formed (step 10a) on the powder bed using a semi-elliptical counter-form obtained by 3D printing. According to an alternative embodiment, the counterform can also be formed via a machining method.
    A layer 9 of boron nitride powder (sintered inert powder) is then deposited (step 10b) in the form of a spray on the surface of the cavity. Alternatively, this boron nitride powder may be replaced by graphite powder or any other material that is inert on consolidation and non-chemically reactive with the material constituting the part to be formed.
    The inner cavity is then filled with PMMA powder (step 10c), thereby forming the volume 5 for forming the desired part 3. Finally, the assembly closed by two graphite pistons is placed in an SPS device for the sintering step 2. During this step, the interfacial layer 9 of boron nitride will thus move and follow the half-ellipsoid which will crash as sintering to form a half-sphere 3 once the material densified. The displacement of the interfacial layer 9 along the lower portion 5 'of the half-ellipse 5 makes it possible to distribute there homogeneously all the stresses transmitted by the counter-form 6. The half-sphere 3 obtained in consequently, a withdrawal homothety over the entire surface 5 'in contact with the interfacial layer 9. The final step is the extraction 11 of the piece 3 in the form of a half-sphere from the sacrificial counterform 6, carried out by fracturing the sacrificial counterform 6 and the interfacial layer 9. It has been observed that following this extraction step 11, the cracks stop clearly at the level of the interfacial layer 9 of boron nitride, thus preserving the piece 3 in half-sphere which remains intact.
    FIG. 5 presents a series of photographs illustrating the extraction step of the part 3 of the assembly 4, and in particular of the interfacial layer 9. FIG. 6 illustrates the induced shape change of the interfacial layer 9 following the implementation of the SPS 2 process. 5.2 SPS sintering of a cone, a square-based pyramid and a star-shaped pyramid
    According to alternative embodiments of the invention, a cone, a square-based pyramid and a star-based pyramid are sintered from an aluminum powder using a graphite sheet (papyex®) as an interfacial layer 9 As shown in FIG. 7, in the context of the use of papyex, the step 10 of placing the assembly 4 consists in folding the desired shape of the interfacial layer 9 with the papyex, and then to position (step 10'a) the papyex 9 in the assembly 4, before filling with a powdery and / or porous material the areas corresponding to the workpiece 5 (step 10'c), and at the counterform 6 (step 10'b).
    FIGS. 8 to 11 are photographs illustrating parts 3 of conical and pyramidal shape as well as the counterform fragments, obtained following the densification under load of an assembly according to these particular embodiments of the invention. As indicated in these photographs, the respective densities of the pieces obtained are between 97% and 99%. It is observed that the two pyramidal shapes both have well-defined straight edges. This result is obviously difficult to achieve by the known mold casting processes without machining. FIG. 12 is an image made via a Scanning Electron Microscope (SEM) of the microstructure of a fracture present on a sacrificial portion of the pyramid. This image notably reflects the low porosity and the satisfactory ductility of the interfacial layer 9. 5.3 Implementation of different materials in the respective compositions of the workpiece 5 and the counterform 6
    According to one particular embodiment of the invention, the respective compositions of the volume 5 intended to form the part and the counterform 6 are different. Although the use of materials of the same nature has the advantage of facilitating the prediction of the material withdrawals generated during the densification step, the use of materials of different natures makes it possible to expand the possibilities presented to the designer in the choice of materials used in the composition of the workpiece 5 or in the counterform 6. It is thus possible to implement, for the constitution of the workpiece 5, a material having advanced technical properties, while selecting, for the constitution of the sacrificial counter-form 6, a material at reduced cost.
    Thus, according to a particular embodiment, a conical volume 5 is composed of zirconia powder (ZrO 2) when the counterform 6 is composed of alumina powder. The coupling of these two powders is based on their relatively similar sintering behavior (temperature and densification curve).
    FIG. 13 is a photograph illustrating a 99% dense zirconia cone and a 98% dense alumina fragment obtained following the implementation of SPS sintering. FIGS. 14 and 15 are fracture SEM images obtained at the center and at the edge of the zirconia cone 3. These SEM images make it possible, in particular, to observe that the microstructure in the center and at the edge of the cone 3 is homogeneous and has an average grain size of 200 nanometers.
    权利要求:
    Claims (9)
    [1" id="c-fr-0001]
    An assembly (4) for densification under load (2), comprising: at least one volume to be densified (5) of pulverulent and / or porous composition, at least one counterform (6) of pulverulent composition and / or porous, having at least one face (7) facing at least a portion (5 ') of said volume (5), said assembly (4) being characterized in that said portion (5') and said face (7) are separated by at least one mobile interfacial layer (9).
    [2" id="c-fr-0002]
    2. Assembly (4) according to claim 1, characterized in that said against-shape (6) encompasses said volume (5) in its entirety.
    [3" id="c-fr-0003]
    3. Assembly (4) according to any one of claims 1 and 2, characterized in that said volume (5) and said against-shape (6) are of identical composition.
    [4" id="c-fr-0004]
    4. Assembly (4) according to any one of claims 1 and 2, characterized in that said volume (5) and said against-shape (6) are of different compositions.
    [5" id="c-fr-0005]
    5. Assembly (4) according to claim 4, characterized in that the densification rate of the material constituting said volume (5) is greater than the rate of densification of the material constituting said counter-form (6).
    [6" id="c-fr-0006]
    6. An assembly (4) according to any one of claims 1 to 5, characterized in that said portion (5 ') and said face (7) are separated by a plurality of movable interfacial layers (9).
    [7" id="c-fr-0007]
    7. Assembly (4) according to any one of claims 1 to 5, characterized in that: • said assembly (4) comprises a plurality of volumes to be densified (5) of powdery and / or porous composition, • said counter form (6) has at least one face (7) facing at least a portion (5 ') of each of said volumes (5), • said face (7) and each of said portions (5') are separated by at least one mobile interfacial layer (9).
    [8" id="c-fr-0008]
    8. A method of manufacturing (1) at least one part (3), characterized in that it comprises: • an incorporation step (10b, 10'a) within an assembly (4) for densification under load (2), a movable interfacial layer (9) separating at least a portion (5 ') of a volume to be densified (5) of powdery and / or porous composition, of at least one face (7) a counterform (6) of powdery and / or porous composition, • a step of densification under load (2) of said assembly (4).
    [9" id="c-fr-0009]
    9. Manufacturing process (1) according to claim 8, characterized in that it comprises a step (11) for extracting said workpiece (3) from said assembly (4) by sacrificial destruction of said counterform ( 6) and / or said movable interfacial layer (9).
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    同族专利:
    公开号 | 公开日
    JP2019502027A|2019-01-24|
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    EP3370902A1|2018-09-12|
    US20180318931A1|2018-11-08|
    FR3042992B1|2021-09-10|
    EP3370902B1|2019-09-18|
    CA3003545A1|2017-05-11|
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    US20210016499A1|2018-03-27|2021-01-21|UNITED STATES OF AMERICA has certain rights in the invention from DOE Grant No. DE-SC0008581|In situ partially degradable separation interface for fabrication of complex near net shape objects by pressure assisted sintering|
    FR3088017B1|2018-11-02|2020-11-13|Univ Paul Sabatier Toulouse 3|MANUFACTURING PROCESS OF A PART BY DENSIFICATION UNDER LOAD|
    FR3088016B1|2018-11-02|2021-01-29|Univ Paul Sabatier Toulouse 3|MANUFACTURING PROCESS OF A PART BY DENSIFICATION UNDER LOAD|
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    优先权:
    申请号 | 申请日 | 专利标题
    FR1560564A|FR3042992B1|2015-11-04|2015-11-04|IMPLEMENTATION OF A MOBILE INTERFACE FOR THE MANUFACTURING OF COMPLEX PARTS|FR1560564A| FR3042992B1|2015-11-04|2015-11-04|IMPLEMENTATION OF A MOBILE INTERFACE FOR THE MANUFACTURING OF COMPLEX PARTS|
    US15/773,791| US20180318931A1|2015-11-04|2016-11-04|Use of a deformable interface for the fabrication of complex parts|
    EP16794970.0A| EP3370902B1|2015-11-04|2016-11-04|Use of a deformable interface for the production of complex parts|
    CA3003545A| CA3003545A1|2015-11-04|2016-11-04|Use of a deformable interface for the fabrication of complex parts|
    JP2018541552A| JP2019502027A|2015-11-04|2016-11-04|Use of deformable interfaces to manufacture complex parts|
    PCT/EP2016/076657| WO2017077028A1|2015-11-04|2016-11-04|Use of a deformable interface for the production of complex parts|
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