EP3250336A1 - Procédé et machine de décochage pour grappe de pièces de fonderie à modèle perdu - Google Patents
Procédé et machine de décochage pour grappe de pièces de fonderie à modèle perduInfo
- Publication number
- EP3250336A1 EP3250336A1 EP16703566.6A EP16703566A EP3250336A1 EP 3250336 A1 EP3250336 A1 EP 3250336A1 EP 16703566 A EP16703566 A EP 16703566A EP 3250336 A1 EP3250336 A1 EP 3250336A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cluster
- blade
- shell
- machine
- pieces
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 37
- 238000005266 casting Methods 0.000 title claims abstract description 22
- 239000002184 metal Substances 0.000 claims abstract description 15
- 239000012634 fragment Substances 0.000 claims abstract description 10
- 238000004519 manufacturing process Methods 0.000 claims description 11
- 238000006073 displacement reaction Methods 0.000 claims description 6
- 238000004891 communication Methods 0.000 description 5
- 238000001816 cooling Methods 0.000 description 5
- 238000004138 cluster model Methods 0.000 description 3
- 239000000919 ceramic Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007730 finishing process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D29/00—Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
- B22D29/04—Handling or stripping castings or ingots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D29/00—Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C7/00—Patterns; Manufacture thereof so far as not provided for in other classes
- B22C7/02—Lost patterns
Definitions
- the invention relates to the unhinging of clusters of cast metal parts lost model.
- the lost-model (or lost-wax) foundry process is a well-known foundry process used in particular for the manufacture of turbine blades, especially aeronautical turbines, in particular turbomachines. This process is described, for example, in WO2014 / 049223.
- this foundry process for the manufacture of a cluster of parts we obtain a cluster of parts formed in a shell or shell.
- This shell is typically ceramic. It is here called indifferently carapace or shell mold.
- the stall is done by striking on the shell with a hammer so as to break it and detach from the bunch of pieces.
- this technique has two disadvantages: firstly, it is painful and tiring for the operators in charge of these operations; moreover, it can create mechanical stresses in foundry pieces. These mechanical stresses may, during the subsequent heat treatment, result in the appearance of metallurgical defects called 'recrystallized grains'. These recrystallized metal grains are areas of weakness that reduce the life of the parts obtained and may lead to the scrapping thereof.
- the object of the invention is to propose a process for unclamping clusters of lost-model foundry metal parts in which the two disadvantages indicated above are eliminated or at least reduced.
- This object is achieved according to the invention by means of a method of unhinging a cluster of lost-model foundry metal parts in which, the cluster of parts being formed in a shell, at least one blade is displaced using a machine, without contact with the cluster, so that the blade engages the shell, breaks it into a plurality of fragments, and detaches from the cluster at least a portion of the shell.
- blade is meant a tooling surface provided to engage an outer body, particularly in this case the shell of the cluster.
- the displacement of the blade or blades for the shakeout of the cluster of parts occurs at a reduced speed; for example, at a speed less than 0.2 m / s, or even less than 0.05 m / s. This reduces the impact between the blade and the shell and the risk of damage to the parts.
- the invention can also be implemented without impact with the shell; that is to say that during the first contact between the blade (s) and the shell, the speed of the blades is almost zero.
- the movement of the stall blade (s) can be done without stopping.
- the speed of movement of the blade or blades may for example be substantially constant.
- the method is implemented by means of a machine to ensure that the blade (s) move under the conditions (including no contact with the bunch at the parts) indicated.
- the machine advantageously avoids the tiring operation of shaking the clusters with the hammer.
- the efficiency of the process results from the fact that the shell formed around foundry pieces is a fragile piece, having a relatively low adhesion on the foundry parts constituting the cluster. Also advantageously, even if the blade or blades of the tool do not come into contact, far from it, with all parts of the shell, their engagement with some protruding parts or 'protuberances' of the shell is enough to fracture almost completely this one, and consequently to uncheck the castings.
- the projecting parts or protuberances at which the mold-shell is fractured may for example be formed around a heat shield provided in the mold-shell.
- Such a heat shield serves to improve the cooling of the cluster during and after casting (An example of a heat shield is described in document FR2874340). In particular, it serves to maintain the solidification front (solid / liquid interface during the cooling of the foundry cluster in the mold) as horizontal as possible.
- the blade or blades engage protrusions of the shell mold and only these (excluding the cluster itself), it is not necessary that the blade approaches close to the parts to be unchecked. On the contrary, to reduce as much as possible the mechanical stresses applied to the surface of the parts, it is even preferable that the displacement of the blade and the contact with the shell is made at a certain distance from the parts.
- the method according to the invention can often be implemented with one or more blade (s) and / or movements of this or these blade (s) extremely simple.
- the speed of the blade may be constant.
- the displacement of the at least one blade for unhitching the part bundle consists solely of a translational movement.
- This movement can in particular be carried out in a direction parallel to an axis of the cluster (the axis of casting, or the axis of symmetry or axisymmetry of the cluster).
- This axis is generally oriented vertically during the casting of the cluster.
- this movement of said at least one blade may also comprise a movement that is not parallel to an axis of the cluster, for example a rotational movement. It can thus possibly be constituted solely by a rotational movement.
- the displacement can be any, depending on the possibilities (number of degrees of freedom or number of axes) of the machine on which the blade is fixed, and the geometry of the cluster.
- the movement of said at least one blade includes a passage between any pair of adjacent pieces of said pieces. Indeed, in the case of a pair of adjacent parts, the passage of a blade between the two parts of the pair of adjacent parts ensures that the carapace portion possibly connecting these parts is fractured, which facilitates the separation between the carapace and the cluster.
- the parts of the cluster are distributed around a casting axis
- the parts are distributed over a circle around the casting axis. They are then adjacent two by two along the circumference of said circle.
- said at least one blade is constituted by a plurality of blades, and when moving said plurality of blades, all said blades come into contact with the shell at substantially the same time. This makes it easier to detach the shell from the cluster.
- the invention also relates to a process for manufacturing castings comprising the following steps: a cluster of lost-model foundry pieces is produced, the part-bundle being formed in a shell, and then at least a portion of the pieces are discarded. of the carapace by the process of unplugging the foundry cluster defined previously.
- the invention also relates to a machine of shakeout of cluster of pieces of foundry to lost model, the cluster of pieces being formed in a carapace, the machine comprising
- At least one actuator adapted to move said at least one blade relative to the frame, in a space provided for fixing the cluster.
- the actuator is provided for moving said at least one blade relative to the frame in the space provided for fixing the cluster at a speed of less than 0.2 m / s, or even less than 0.05 m / sec. s.
- the machine can be a relatively simple press.
- the actuator (s) may include an actuator adapted to move at least one blade for unhitching the part bundle only by a translational movement or only by a rotational movement.
- the actuator (s) may include in particular a jack. This jack can ensure the displacement of said at least one blade, in particular in translation.
- Said at least one blade is preferably non-rotating (it is neither a drill nor a mill).
- said at least one blade is constituted by a plurality of blades integrated into a tool.
- These blades can in particular be rigidly fixed to each other within the tooling.
- They can in particular be oriented (extend) in directions substantially perpendicular to the direction of movement of the tool.
- They may in particular be elongated and be formed on tooling portions, for example in the form of fingers, directed in radial directions relative to a center of the tooling.
- the machine is provided for the unhinging of a cluster of pieces formed in a shell.
- the actuator or actuators are provided, depending on the configuration of the cluster, so as to move the blade or blades without shock relative to the cluster and without contact with the blades so as to separate at least a portion of the shell of the bunch.
- the invention also relates to an assembly comprising a shake machine as defined above, and a cluster of lost model casting parts, the cluster of parts being formed in a shell ;
- the shakeout machine is adapted to allow the attachment of said cluster on the frame;
- said at least one actuator is adapted, when the cluster is fixed on the frame, to move said at least one blade relative to the cluster and without contact with the cluster, so that said at least one blade engages the shell, breaks it into a plurality of fragments, and detaches from the cluster at least a portion of the shell.
- the shell in the vicinity of each piece of the cluster, has at least one protuberance that said at least one blade engages during said movement.
- This or these protuberance (s) are one or portions (s) of the shell containing no part of the cluster; thus, the lamé (s) can engage the protrusion (s) without risk of hitting the cluster.
- This or these protuberance (s) preferably extend to at least 6 mm, and preferably at least 8 mm, of the room in the vicinity of which it is located.
- At least one of the protuberances surrounds at least one of the parts of the cluster 360 ° in view along an axis of the cluster.
- This protuberance may in particular be a heat shield to improve the cooling of the cluster during the casting and cooling of the metal.
- the protuberances are disposed substantially in a plane.
- At least a portion of the protuberances are formed around or from a tray-shaped piece pierced with holes.
- This part is mostly intended to form a heat shield.
- FIG. 1 shows schematically the steps of a method of manufacturing parts according to the invention by lost pattern foundry.
- FIG. 2 schematically illustrates a wax core used for the implementation of the blade manufacturing process of Figure 1;
- FIG. 3 is a side view of a shell mold and tooling used in the blade manufacturing process of FIG. 1;
- FIG. 4 is a schematic perspective view of a shake machine according to a first embodiment of the invention, used for carrying out the method illustrated in Figures 1 to 3;
- FIG. 5A is a half-view in axial section of the shell mold and the tool shown in Figure 3;
- Figure 5B is a view of a detail of Figure 5A;
- FIG. 6 is a perspective view of the tooling used in the process illustrated in FIGS. 1 to 5B;
- FIG. 7A is a detail axial section of a shell mold containing a foundry cluster, and the tooling of a shake machine according to a second embodiment of the invention.
- Figure 7B is a cross-section of the tooling shown partially in Figure 7A.
- Figure 7C is a schematic axial section of the shake machine illustrated in Figures 7A and 7B.
- FIGS. 1 to 5 An example of a shakeout machine and method according to a first embodiment of the invention will now be presented in connection with FIGS. 1 to 5. This machine and this shake-out method will be presented in the context of a blade manufacturing method according to the invention.
- the blade production process presented is a lost-model foundry process (FIG. 1).
- the first step SI of this method consists in manufacturing a model of cluster 21 in wax (FIG. 2), also called 'non-permanent cluster'. Then, around the wax cluster model, a shell mold 1 is manufactured in a manner known per se.
- the cluster model 21 comprises a plurality of blade models 22, connected by auxiliary parts 23.
- These auxiliary parts 23 comprise two additional parts 14 in the form of a disc, made waxen.
- Each of these additional pieces 14 is in the form of a plate pierced with holes through which the blade patterns 22 pass.
- the dawn patterns 22 are all identical to each other. They are arranged in a circle axisymmetrically about an axis X, said casting axis.
- the X axis is disposed in the vertical direction during the foundry operation, when molten metal is poured into the shell mold 1 (operation discussed in more detail below).
- the blade models 22 are arranged parallel to the X axis.
- the blade models 22 will be used to develop molding cavities 7 for the blade molding 32;
- the additional parts 14 will be used to build an upper heat shield 13 and a lower heat shield 13 ';
- the other functional parts 23 will be used to develop including a casting cup 5, supply channels 8, stiffeners 20, and selectors 9.
- a second step S2 the shell mold 1 is manufactured from the wax cluster 21 (this step is described in more detail by the document WO2014 / 049223).
- this step is described in more detail by the document WO2014 / 049223.
- step S2 consists of removing the wax from the bunch model from the mold. This removal of the wax is achieved by wearing the shell mold in an autoclave mold (or other) at a temperature above the melting temperature of the wax.
- the additional carapace portions define cavities, referred to herein as 'additional cavities'.
- a third step S3 the blade cluster 32 is formed in the shell mold 1 by casting molten metal into the shell mold 1.
- the result of the casting differs according to whether or not the additional cavities are connected to the main cavity:
- the additional cavities are not in communication with the main cavity; the communication between these cavities and the main cavity has for example been deliberately blocked. These cavities then remain empty during casting and do not fill with metal.
- the additional cavities are in communication with the main cavity. They fill up then during the casting.
- a fourth step S4 after cooling and solidification of the metal in the shell mold 1, the cluster 30 is unchecked from the shell mold 1.
- the shakeout consists in breaking up the shell by acting on the additional shell parts. During this step, contact with the solidified metal should be avoided.
- each of the blades 32 is separated from the rest of the cluster 30 and finished by finishing processes, for example machining processes.
- the invention particularly relates to the shakeout method implemented in the fourth step S4 indicated above.
- This stalling process is implemented by means of a shakeout machine 40 (FIG. 4).
- This machine 40 comprises a frame or structure 42, a tooling 50 and an actuator 46.
- the frame 42 comprises fixing lugs or pins 44 (of the valet type), which make it possible to rigidly fix the shell mold 1 containing the blade cluster 30 on a perforated plate 41 of the frame 42.
- the perforated portions of this plate which serve to evacuate the fragments of the shell mold during the shakeout operation, are not shown.
- the pins 44 make it possible to fix the shell mold 1 so that the axis of symmetry (X) of this mold is oriented in the vertical direction.
- the actuator 46 is a linear jack. It is arranged to move the tooling 50 vertically in the downward direction along the X axis of the shell mold 1.
- the tooling 50 (FIG. 6) has a cage shape, with an upper disc 54, and a lower disc 52 fixed on the disc 54 by four vertical metal bars 56.
- the tooling 50 is fixed on the output shaft 48 of the jack 46 by a sleeve 58 fixed on the upper outer surface of the disk 54, and in which the end of the shaft 48 is fixed.
- the upper disk 54 is therefore the driven part of the tooling 50.
- the lower disc 52 is the working part of the tooling 50, namely the part that includes the blade 64 which engages the shell mold 1 to allow the shaving of the blade cluster 30.
- the disc 52 has in its central part a wide opening 60 of generally circular shape (Fig.6). On the periphery of this opening 60 are provided shaking fingers 62. These fingers are disc portions which extend from the peripheral ring 61 of the disc 52 in a radial direction reentrant towards the axis X of the machine 40 .
- the lower surface of the disk 52 (under the fingers 62 and under the peripheral ring 61) constitutes the blade 64.
- This blade 64 is provided to engage the shell mold 1, when the cylinder 46 moves the tooling 50 downwards ( arrows A, Fig. 3).
- the jack 46 is provided to move the tool 50 - and therefore the blade 64 - in translation relative to the frame at a constant speed of less than 0.2 m / s.
- the choice of a rather low speed makes it possible to avoid creating too large constraints of stress on the casting cluster when the blades are unstuck, and thus to avoid creating mechanical stresses capable of generating grains recrystallized during the treatment. thermal.
- the shakeout machine 40 is designed such that during the downward movement of the tooling 50, the jack 46 moves the blade 64 (and more generally, the tooling 50) without contact with the cluster 30, particularly without contact. with the blades.
- the disk 52 is arranged so that the blade cluster 30 can pass without contact in its opening 60.
- the shake machine 40 is further designed so that during the downward movement of the tooling 50, the blade 64 engages different parts of the shell mold 1, said protuberances, and detaches from the cluster 30 most of the carapace .
- these protuberances are constituted by the additional parts of shell forming the heat shields 13 and 13 '.
- the disc 52 is intended to come into contact with the shell mold 1 at the level of the protuberances (the heat shields 13 and 13. However, the disc 52 (and therefore the blade 64) must not come into contact with the cluster (metallic) 30.
- the protuberances are constituted by the additional parts of the shell, that is to say the heat shields 13 and 13 '. Depending on the mode of implementation, these additional parts are empty, or filled or partially filled with metal:
- the protuberances are empty. In this case, so that the disk 52 can descend without coming into contact with the cluster 30, it suffices that the disk 52 engages or interferes with the additional part of the shell, while maintaining a sufficient safety distance with respect to The disk 30. In this case, the disk 52 can come into extensive contact with the additional parts of the shell (heat shields 13 and 13 7 ).
- the protuberances or heat shields 13, 13 ' are partially or completely filled with metal.
- the zone of radial interference between the disk 52 and the heat shield 13 can extend only over a short distance d1 between the disk 52 and the shell mold 1.
- the trajectory of the disk 52 is intended to allow in no case a contact between the disk and the cluster 30; for this purpose, it is provided that a safety distance d2 at all times separates the disk 52 from the cluster 30.
- the shape of the disc 52 is provided so that the contact between the latter and the shell mold occurs first on the upper heat shield 13. This implies in particular that the disk 52 is arranged inversely so as to do not come into contact with parts of the mold 1 situated above the screen 13, such as in particular the upper projections 38 of the shell mold 1 (FIG. 5B).
- the screen 13 constitutes a "protuberance" that the blade 64 engages during the movement of the tooling 50 according to the invention, which is not the case with the protrusions 38.
- the heat shield 13 is situated at a certain distance from the blades, the mechanical stresses applied to the blades during the contact between the blades 64 and the shell mold are relatively small and do not create zones capable of creating recrystallized grains.
- the blade 64 then applies on the surface of the screen 13 (as protuberance) a force that tends to split the ceramic shell into fragments; the rupture lines propagate and extend from the protuberance to the rest of the shell.
- the descent of the tool 50 continues, it hits the mold-shell 1 (moderate speed) and continues its descent movement by exerting a force on the mold-shell.
- the shell-mold 1 which is fragile, breaks into a large number of fragments; under the effect of gravity, most of these fragments are detached from the cluster 30 and fall. The bulk of the shake-out of the cluster is thus achieved in a single simple and fast operation.
- the blade 64 After striking the heat shield 13 constituting an upper protrusion, continuing its descent the blade 64 strikes the heat shield 13 ', which constitutes a lower protuberance. It then breaks the remaining parts of the carapace mold and thus completes the stall of it (except for some remaining parts eventually).
- the tooling 50 presented above has the advantage of being implemented by a simple translational movement. This is made possible by the fact that the shape of the shell mold 1 allows the passage of the tool when it descends in the vertical direction (X axis).
- a more complex shake machine including including different shake tools, may be necessary when the shape of the shell mold does not allow to achieve the disengagement of the cluster by moving a tool by a simple translational movement.
- FIGS. 7A, 7B and 7C An example of such a situation is illustrated by FIGS. 7A, 7B and 7C.
- the vanes of a cluster 130 which must be unchecked from a shell mold 101 have protrusions 138 very prominent. These projections 138 are incompatible with tools down vertically without hitting the shell mold 101 to the right of these projections, but by engaging the heat shield 113 (Fig.7A).
- This movement can be performed by means of the machine 140 shown in FIGS. 7B and 7C, which constitutes another embodiment of the invention.
- the parts of the machine 140 or the mold 101 which have a structure and / or a function identical or similar to that (s) of the corresponding part of the machine 40 or the mold 1 bear the reference of this corresponding part, increased by 100 .
- the stalling machine 140 comprises a frame 142 with a perforated plate 141 on which the shell mold 101 can be fixed, a tool 150, and actuators 146.
- the tooling 150 is not constituted in a single rigid part as the tooling 50, but in four parts (It can naturally be made in any number of parts, other than four). Each of these four parts comprises a plate 152 in the general shape of disk quarter, these four plates being identical.
- the shake machine 140 comprises four rotary actuators 146 identical to each other.
- Each actuator 146 is a rotary jack adapted to rotate one of the trays 152 about a horizontal axis.
- each of the trays 152 includes a flange portion 158 provided to allow the tray 152 to be fixed to one of the actuators 146.
- the actuators 146 drive the four plates 152 in rotation simultaneously.
- trays 152 engage the carapace mold 101 at the upper heat shield 113 thereof, fragment the mold 101 into a large number of pieces, and thus separate a large part of the mold 101 of the blade cluster.
- the different parts of the tooling can naturally be moved not simultaneously, but in any conceivable sequence, for example one after the other, or successively in diametrically opposed pairs, etc.
- the movement of the trays 152 is a rotational movement, carried out in such a way that they do not come into contact with the cluster 130.
- This rotational movement makes it possible to bring the ends of the fingers 162 of the tool 150 closer to the X axis of the carapace mold 101 (arrows in Figure 7B). With this, the fingers 162 pass between each pair of adjacent blades, and thus ensure that the shell mold 101 is fractured between all pairs of adjacent blades. By thus fragmenting the shell mold 101 in at least as many portions as there are blades 132, the tooling 150 thus ensures the unhinging of a very large portion of the shell mold 101.
- Each cylinder 146 is controlled so that it moves the end of the plate 152 which it drives, that is to say the end of the finger 162, at a substantially constant speed, less than 0.2 m / s.
- a machine or a stalling method according to the invention can be made according to many other embodiments than those presented above. Many possibilities exist as regards the arrangement of stall blades and the tooling that supports them, as regards the kinetics or the path of movement of the blade or blades.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1550595A FR3031921B1 (fr) | 2015-01-27 | 2015-01-27 | Procede et machine de decochage pour grappe de pieces de fonderie a modele perdu |
PCT/FR2016/050039 WO2016120538A1 (fr) | 2015-01-27 | 2016-01-11 | Procédé et machine de décochage pour grappe de pièces de fonderie à modèle perdu |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3250336A1 true EP3250336A1 (fr) | 2017-12-06 |
EP3250336B1 EP3250336B1 (fr) | 2019-03-06 |
Family
ID=53758285
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16703566.6A Active EP3250336B1 (fr) | 2015-01-27 | 2016-01-11 | Procédé et machine de décochage pour grappe de pièces de fonderie à modèle perdu |
Country Status (5)
Country | Link |
---|---|
US (1) | US10632531B2 (fr) |
EP (1) | EP3250336B1 (fr) |
CN (1) | CN107427910B (fr) |
FR (1) | FR3031921B1 (fr) |
WO (1) | WO2016120538A1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3056994B1 (fr) * | 2016-09-30 | 2021-01-22 | Safran | Four de cristallisation pour la production d'aubes de turboreacteur avec ecran thermique embarque |
FR3062588B1 (fr) * | 2017-02-06 | 2019-04-26 | Safran Aircraft Engines | Systeme de raccordement d'une sole de four a une embase de moule carapace pour la fabrication d'un element aubage |
FR3089438B1 (fr) | 2018-12-11 | 2020-12-25 | Safran | Barbotine de fonderie améliorée pour la fabrication de moules carapaces |
FR3094655B1 (fr) * | 2019-04-08 | 2021-02-26 | Safran | Procédé de fabrication d’une pluralité de secteurs de distributeur par fonderie |
FR3127904B1 (fr) | 2021-10-07 | 2024-04-19 | Safran | Procédé amélioré de fabrication d’un moule carapace pour la fabrication de pièces métalliques aéronautiques par fonderie à cire perdue |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US471158A (en) * | 1892-03-22 | Theodore westerman | ||
FR2460736A1 (fr) * | 1979-07-09 | 1981-01-30 | Renault | Installation de decochage selectif de pieces de fonderie |
RU1770072C (ru) * | 1990-02-14 | 1992-10-23 | Центральный научно-исследовательский институт материалов | Способ выбивки при литье в вакуумно-пленочные формы |
US5678583A (en) * | 1995-05-22 | 1997-10-21 | Howmet Research Corporation | Removal of ceramic shell mold material from castings |
US7207375B2 (en) * | 2004-05-06 | 2007-04-24 | United Technologies Corporation | Investment casting |
FR2874340B1 (fr) | 2004-08-20 | 2008-01-04 | Snecma Moteurs Sa | Procede de fonderie de pieces en carapace, grappe et carapace pour sa mise en oeuvre, aube de turboreacteur obtenue par un tel procede, et moteur d'aeronef comportant de telles aubes |
DE102005055876B4 (de) * | 2004-11-23 | 2016-11-24 | Künkel Wagner Germany Gmbh | Vorrichtungskombination und Verfahren zum Trennen von Gusskörper und Form durch ein selektives Auspacken |
US7231955B1 (en) * | 2006-01-30 | 2007-06-19 | United Technologies Corporation | Investment casting mold design and method for investment casting using the same |
JP2012050990A (ja) * | 2010-08-31 | 2012-03-15 | Shiga Yamashita:Kk | 振動砂落とし装置 |
FR2995807B1 (fr) | 2012-09-25 | 2015-10-09 | Snecma | Moule carapace a ecran thermique |
TW201433384A (zh) * | 2013-02-22 | 2014-09-01 | Alloymax Prec Casting Co Ltd | 鑄造殼模脫除機與鑄造殼模脫除方法 |
CN203390188U (zh) * | 2013-07-08 | 2014-01-15 | 黄冈市钰丰精密五金有限公司 | 一种震壳机 |
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2015
- 2015-01-27 FR FR1550595A patent/FR3031921B1/fr active Active
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2016
- 2016-01-11 US US15/546,545 patent/US10632531B2/en active Active
- 2016-01-11 CN CN201680012704.8A patent/CN107427910B/zh active Active
- 2016-01-11 WO PCT/FR2016/050039 patent/WO2016120538A1/fr active Application Filing
- 2016-01-11 EP EP16703566.6A patent/EP3250336B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
CN107427910B (zh) | 2019-12-06 |
CN107427910A (zh) | 2017-12-01 |
FR3031921A1 (fr) | 2016-07-29 |
FR3031921B1 (fr) | 2017-02-10 |
WO2016120538A1 (fr) | 2016-08-04 |
US20180178280A1 (en) | 2018-06-28 |
EP3250336B1 (fr) | 2019-03-06 |
US10632531B2 (en) | 2020-04-28 |
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