EP2846948A2 - Outillage de fabrication d'un noyau de fonderie pour une aube de turbomachine et son procédé de fabrication - Google Patents
Outillage de fabrication d'un noyau de fonderie pour une aube de turbomachine et son procédé de fabricationInfo
- Publication number
- EP2846948A2 EP2846948A2 EP13728448.5A EP13728448A EP2846948A2 EP 2846948 A2 EP2846948 A2 EP 2846948A2 EP 13728448 A EP13728448 A EP 13728448A EP 2846948 A2 EP2846948 A2 EP 2846948A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- core
- mold
- rod
- tooling according
- notch
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C13/00—Moulding machines for making moulds or cores of particular shapes
- B22C13/12—Moulding machines for making moulds or cores of particular shapes for cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/103—Multipart cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C21/00—Flasks; Accessories therefor
- B22C21/12—Accessories
- B22C21/14—Accessories for reinforcing or securing moulding materials or cores, e.g. gaggers, chaplets, pins, bars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/18—Finishing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/22—Moulds for peculiarly-shaped castings
- B22C9/24—Moulds for peculiarly-shaped castings for hollow articles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/21—Manufacture essentially without removing material by casting
Definitions
- the present invention relates to a tool for manufacturing a foundry core for producing a cooling circuit of a turbomachine blade.
- a turbomachine blade and in particular a wheel of a turbomachine turbine, comprises a cooling circuit which is supplied with air by orifices formed in the blade root, these orifices opening into internal cavities of the turbine engine.
- dawn that communicate with a bathtub from the top of the blade of dawn.
- This bath is formed by a recess of the top of the blade which is separated from the internal cavities of the blade by a bath bottom wall and which is in fluid communication with the internal cavities through the through holes of this wall.
- air enters the openings of the blade root, circulates in the internal cavities of the dawn and is then expelled, partly into the tub through the aforementioned orifices and partly into the vein of the turbine through air outlets of the blade of the dawn.
- the cooling circuit of a blade of this type includes in particular the bathtub, the internal cavities of the blade, and the holes in the bottom wall of the bathtub which ensure fluid communication between the bathtub and the internal cavities.
- This cooling circuit has a complex shape and is generally obtained by means of a foundry core which is inserted in a mold in which is cast a molten metal for the realization of the blade.
- EP-A1-1,661,642, EP-B1-1,754,555 and EP-A1-1,980,343 describe nuclei of this type.
- the core is generally made from a paste having ceramic fillers and a polymer-based binder which is injected into a mold of a tool and which is then heated to solidify the core.
- the mold of the tooling includes indentations of a first portion of the core for forming the dawn tub, and one or more other portions of the core for forming one or more internal cavities, respectively, of dawn.
- the mold has a wall separating the first part of the cavity from the other part or parts of the core, this wall being intended to define a space in the core, between its first and its other part or parts.
- this bath bottom wall is pierced with orifices.
- orifices are obtained from foundry by means of ceramic rods which are positioned in the mold, before the manufacture of the core, and which form an integral part of the core after its manufacture.
- Each ceramic rod generally connects the first part of the core to one of the other aforementioned parts (EP-B1 -1 754 555).
- the core manufacturing mold comprises means for supporting and / or embedding the end portions of each rod.
- One of these means is formed on the aforementioned wall of the mold and the other means is formed on another part of the mold, which is opposite to the aforementioned wall relative to the cavity of the first part of the core.
- Each rod thus passes through the impression of the first part of the mold.
- the diameter of the orifices of the bath bottom wall is in particular a function of the diameter of the ceramic rods of the core. To reduce the diameter of these holes, it is possible to reduce the diameter of the rods.
- the stems of small diameter for example of the order of 0.6 mm
- the present invention is intended in particular to provide a simple, effective and economical solution to this problem.
- a tool for manufacturing a foundry core for the realization of a cooling circuit of a turbomachine blade
- the core comprising a first part intended to define a dawn tub and at least another part intended to define an internal cavity of the blade, and at least one rod which extends between the first part and the other or each other part and which is intended to define a fluid passage means between the tub and the corresponding internal cavity of the blade
- the tool comprising an injection mold of a paste having impressions of the first part and the other or of each other part of the core, and support means and and / or embedding the end portions of the or each rod, one of these means being formed in a wall of the mold separating the impression of the first part of the core of the impression of the or each other part of the core, characterized in that it compresses end, in the cavity of the first part of the core, means for supporting a substantially central portion of the or each rod.
- the median part of the or each rod which is the part of the rod most stressed by buckling during the injection of the dough into the mold, is supported by means holding in position the or each rod to prevent it from being deformed and breaks under the effect of the forces applied during the injection of the dough.
- the invention makes it possible to produce a foundry core for a turbomachine blade, whose rod or rods have a relatively small diameter, less than 0.8 mm, and for example about 0.6 mm.
- the support means of a rod may be independent of the support means of the other rods.
- the support means of the rods may be spaced from each other and the support means of a rod may be located midway between the support means and / or embedding this rod.
- the support means comprise for example at least one member projecting from the bottom of the cavity of the first part of the core, this member having for example a substantially semi-ovoid shape.
- the or each member may comprise at its apex a notch in which the median portion of a rod is intended to be engaged.
- the notch may have a substantially L-shaped section preferably comprising two plane and intersecting faces which are intended to be substantially parallel to the longitudinal axis of the corresponding rod.
- the rod is intended to be supported on each of these faces via a bearing line which is substantially parallel to the axis of the rod.
- the notch may also have a substantially U-shaped or C-shaped section comprising two plane lateral faces substantially parallel to each other and to the longitudinal axis of the corresponding rod.
- the dough can exert a lateral force on the rod which can then move and break. This is particularly the case when the paste exerts on the rod a force directed towards the side where the rod is not completely supported by its support member.
- the notch section U or C of each member receives the middle part of the rod, which is supported on each side by this body.
- this rod is held in position by the member and can not be moved or broken.
- This particular U-shaped or C-shaped shape provides better support than the L shape.
- Each of the lateral faces of the notch is connected to an upper face of the member by a convex rounded edge in particular to facilitate the insertion of the rod into the notch.
- the rod is thus intended to be supported on these lateral faces via a bearing line which is substantially parallel to the axis of the rod.
- the rod may be, in the mounting position, at a small distance (less than 0.1 mm) from one of these faces or both faces.
- One of the faces of the notch may be substantially perpendicular to a direction of injection of the paste in the mold, and in particular in its print of the first part of the core. When the paste is injected into the mold, the rod bears against this face, which opposes the flow of flow of the dough and ensures that the rod is properly held in position.
- the side faces may be substantially perpendicular to a direction of injection of the dough into the mold so that during the injection of the dough into the mold, the rod either in support on these faces which oppose the flow of flow of the dough and ensure a good maintenance of the rod in position.
- the or each member may be formed integrally with the mold or be attached and fixed on the mold.
- the tool may also include a counter mold which also comprises means for supporting a middle portion of the or each rod.
- the tooling according to the invention comprises a counter mold which comprises means for immobilizing the or each rod in the notch of the corresponding member, these immobilizing means comprising at least one wedge formed protruding in an impression against the mold and having at its top a finger engagement in the upper part of the notch and / or bearing on the portion of the rod housed in this notch.
- the or each shim In the mounting position of the mold and against the mold, the or each shim is intended to be positioned vis-à-vis the corresponding member to prevent the rod from leaving the notch of the body, especially when the paste injected into the tooling exerts on the rod a force tending to dislodge it from the notch (for example a force directed from the bottom upwards).
- the rod is then held in position by a member and a wedge that prevent movement of the rod in a plane perpendicular to its longitudinal axis, and therefore limit the risk of breakage.
- the or each shim preferably comprises support and positioning means on the top of the corresponding member.
- the against-mold may include a number of shims smaller than the number of mold members so that only some of the mold members are associated with wedges against the mold.
- the support means may comprise at least three or four protruding members.
- the against-mold may comprise a single shim intended, in the mounting position, to cooperate with a mold member located on the side of the trailing edge of the core to be produced.
- the present invention also relates to a process for manufacturing a foundry core by means of the tooling as described above, comprising steps for injecting a paste comprising ceramic fillers into the tooling, the solidification and the extraction of the core, characterized in that it comprises an additional step consisting, after the extraction of the core, filling the or the recesses of the core defined by the tool support means, for example with a ceramic material .
- the core made by means of the tool according to the invention has at least a slight recess or recess, in its first part intended to define the bath of the blade, because of the presence of the support means in the mold. In a simple way, this recess is filled with a material close to that of the core.
- FIG. 1 is a schematic perspective view of a rotor blade of a turbomachine
- FIG. 2 is a schematic sectional view along the line ll-ll of Figure 1 and shows a cooling circuit of the blade;
- FIG. 3 is a very schematic view of a foundry core for producing a turbomachine blade;
- FIGS. 4 and 5 are partial schematic views in perspective of the tool according to the invention for manufacturing by molding a foundry core, the tool carrying a ceramic core rod;
- FIG. 6 is a partial schematic perspective view of another tool according to the invention for manufacturing by molding a foundry core, the tool carrying four ceramic rods of the core;
- Figure 7 is a view similar to that of Figure 5 and showing a tool according to the invention for manufacturing by molding a foundry core;
- FIG. 8 is a very schematic perspective view of the rod support members in a tool according to the invention, and also comprises a schematic cross-sectional view of the core to be formed in this tool;
- FIG. 9 is a view on a larger scale of a part of FIG. 8 and also shows a wedge of a counter-mold of the tooling.
- FIG. 10 is a sectional view along the line X-X of Figure 9.
- FIG. 1 shows a rotor blade 10 of a compressor or turbomachine turbine, the rotor blade comprising a blade 12 connected by a platform 14 to a foot 16.
- the blade 10 comprises an internal cooling circuit which is partially visible in FIG. 2, this circuit being fed with air through orifices 18 of the blade root 16. These orifices open into internal cavities 20 of the blade in which circulates the cooling air of dawn. This air is then expelled through orifices 22 of the trailing edge of the blade 12 and through orifices 24 of the top of the blade.
- the orifices 24 of the blade tip open into a bath 26 which is formed by a recess at the top of the blade 12 and which is separated from the internal cavities 20 by a bath bottom wall 28, in which the orifices 24 are formed.
- the cooling circuit of the blade 10 is obtained from casting by means of a core which is mounted in the ceramic shell mold in which a molten metal alloy is cast. After solidification and extraction of the blade, the core is removed for example by etching.
- FIG. 3 very schematically shows a core 30 of this type, this core 30 having a first part 32 intended to form the bath 26 of the blade, other parts 34 intended respectively to form the internal cavities 20 of the dawn, and ceramic rods 36 each connecting the first portion 32 to one of the other portions 34.
- the first portion 32 of the core 30 has a shape and dimensions complementary to those of the bath 26 to be formed and the other parts 34 also have a shape and dimensions complementary to those of the cavities 20 to form.
- the ceramic rods 36 provide two functions, the mechanical connection between the different parts of the core 30 and the maintenance of these parts in predetermined positions and with predetermined spacings.
- the first part 32 of the core is separated from the other parts 34 by a space 38 whose thickness depends on the length of the parts of rods 36 extending between the first part and the other parts of the core .
- part of this alloy is intended to penetrate into the space 38 of the core 30 to form the bath bottom wall 28, the thickness of which is imposed. by the thickness of the space 38.
- the ceramic rods 36 of the core 30 are intended to form the orifices 24 of the wall 28, which provide the fluidic communication between the bath 26 and the internal cavities 20 of the blade.
- the diameter of these orifices 24 is in particular a function of the diameter of the ceramic rods 36 of the core 30.
- These ceramic rods 36 are mounted in the mold of the tooling of the core, before the injection of the paste into this mold.
- the mold comprises a first impression of the first part 32 and a second impression of the other parts 34 of the core 30, these impressions being separated from each other by a wall which is intended to form the space 38 supra of the core.
- the ceramic rods 36 are mounted in the mold so that they completely pass through the first cavity, an end portion of each rod being embedded in a recess of the mold and the opposite end portion of the rod extending into the cavity. second mold cavity and bearing on the aforementioned wall of the mold.
- the ceramic rods 36 in particular those of small diameter (for example of the order of 0.6 mm), have a tendency to break during the injection of the paste into the mold. mold, which leads to the disposal of the core.
- the present invention provides a solution to this problem by means of support means of the middle portions of the ceramic rods mounted in the mold tooling.
- FIGS. 4 and 5 show an embodiment of the tooling according to the invention, this tool comprising a mold 40 comprising a first cavity 42 of the first part 32 of the core 30 and a second cavity 44 of the other parts 34 of the core, these cavities 42, 44 being separated from each other by a wall 46 which is intended to form at least part of the aforementioned space 38 of the core.
- a single ceramic rod 36 is shown in Figures 4 and 5, this rod having an end portion 48 embedded in a recess 50 of the mold and an opposite end portion 52 extending into the second cavity 44 of the mold and being bearing on the wall 46 of the mold.
- the wall 46 of the mold has a notch 54 with a U or C section substantially complementary to that of a portion of the rod 36, which is substantially cylindrical in the example shown.
- the recess 50 of the mold 40 also has a shape substantially complementary to that of the rod 36. This prevents dough passing between the rod 36 and the walls of the notch 54 and the recess 50, during its injection in the mold 40.
- the tool according to the invention may comprise a counter-mold, not shown, which also comprises a first impression of the first part 32 of the core 30 and a second impression of the other parts 34 of the core, these impressions being separated from each other. the other by a wall which is intended to form part of the aforementioned space 38 of the core.
- This wall of the counter mold has a free edge of complementary shape to that of the free edge of the wall 46 of the mold, so that these walls are aligned with each other and fit into one another in the assembly of tools.
- the wall 46 may comprise projecting means 56 intended to cooperate by connection of shapes with means complementary to the wall of the counter-mold to ensure proper positioning of the walls during assembly.
- the middle part of the rod 36 extends through the first cavity 42 of the mold 40.
- support means 58 are provided in this cavity 42 to support the portion median of the rod 36 and hold it in position in order to limit its deformations during the injection of the paste into the mold.
- the support means of the rod comprise a member 58 projecting from the bottom of the first cavity 42 of the mold, this member being located substantially midway between the recess 50 and the notch 54 of the mold.
- This member 58 can be attached and fixed on the mold 40, as is the case in the example shown, or be formed in one piece with the mold. It may be made of the same material as the mold, that is to say of metal alloy.
- the member 58 here has a semi-ovoid shape and has at its top a notch 60 for mounting the rod 36.
- this notch has an L-shaped cross-section and comprises two flat faces 62, 64 and secant extending substantially parallel to the longitudinal axis of the rod 36, when the latter is mounted in the mold. These faces 62, 64 form an angle of the order of 90 degrees.
- the ceramic rod 36 is intended to bear on these faces 62,
- the paste is injected into the mold and is intended to flow into the first cavity 42 of the mold in the direction indicated by the arrow 66.
- the face 64 of the notch 60 is substantially perpendicular to this direction, which makes it possible to retain effectively the rod 36 in position when the dough flows around the rod, and limit its deformations.
- FIG. 6 represents another embodiment of the invention in which the mold of the tooling comprises means 58 for supporting four ceramic rods 36, these support means being similar to those described in the foregoing and being independent and at a distance from each other.
- the core 30 has in its first part 32 as many recesses as support means present in the manufacturing mold of this core.
- the core will have a recess and in the case of Figure 6, the core will have four recesses. These recesses have complementary shapes to those of the support means.
- the present invention provides a method comprising a step in which these recesses are filled with a ceramic charging material whose composition is preferably close to that of the core material.
- the paste injected into the mold of FIG. 5 can exert a force on the rod 36 in a direction opposite to that of the arrow 66. Due to the shape of the notch 60 of the member 58, the rod is not supported by the member of the opposite side to the face 64 and can move or even break under the force exerted by the dough.
- FIG. 7 represents a first embodiment in which the elements already described in the foregoing are designated by the same references.
- the member 58 differs from that shown in FIG. 5 in that its notch 60 'comprises two lateral faces 64, 65 which are substantially parallel to each other and to the longitudinal axis of the rod 36 and whose lower ends are interconnected. by a face 62 of the bottom of the notch.
- the rod 36 is intended to bear on the faces 62, 64 and 65.
- a game of a few tenths or hundredths of a millimeter can exist between the rod and the faces 62, 64 and 65.
- the rod 36 is thus supported on each side by the member 58 and is held in place even if the paste injected into the tool exerts on the rod lateral forces on both sides of the rod (arrows 66 and 66 ').
- Figures 8 to 10 show an alternative embodiment of the invention wherein the tool comprises four rods 36, the middle portions are supported by members having notches 60 'U-section or C housing rods.
- the lateral faces 64, 65 of the notch 60 'of each member 58 are connected by rounded edges 70 convex to upper faces 72 of the member ( Figures 9 and 10).
- the faces 64, 65 are here slightly inclined with respect to each other, these faces being further apart from each other at their upper ends than at their lower ends.
- the against-mold (not shown) of the tooling comprises a shim 74 which is formed protruding into a mold cavity and which, in the mounting position, is intended to face one of the members 58 of the mold 40 .
- This shim 74 has an elongated shape whose apex comprises a finger 76 which is intended to be engaged in the upper part of the notch 60 'of the member 58 and to bear on the median part of the rod 36.
- the top of the shim 74 has a shape that is substantially complementary to the top of the member 58 and bears on the above-mentioned upper faces 72 of this member.
- a section 78 of the core to be formed is schematically represented in FIGS. 8 to 10.
- the wedge 74 of the counter-mold cooperates with a member 58 of the mold which is situated on the side of the trailing edge of the core.
- the spacer 74 prevents the rod 36 supported by this member 58 from moving and coming out of the notch of this member because it has been found that the paste injected into the tooling can exert a force on this rod directed from the bottom upwards. and capable of dislodging the rod from the notch of the organ.
- the paste injected into the tooling does not exert such force on the rods 36 supported by the other members 58, which can therefore not be associated with wedges 74 of the counter-mold.
- the members 58 preferably have rounded external profiles so as to provide a deflection and damping function for the effort of the flow of pulp undergone by the rods 36.
Abstract
Description
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1254350A FR2990367B1 (fr) | 2012-05-11 | 2012-05-11 | Outillage de fabrication d'un noyau de fonderie pour une aube de turbomachine |
FR1258282A FR2990368B1 (fr) | 2012-05-11 | 2012-09-05 | Outillage de fabrication d'un noyau de fonderie pour une aube de turbomachine |
PCT/FR2013/051028 WO2013167847A2 (fr) | 2012-05-11 | 2013-05-07 | Outillage de fabrication d'un noyau de fonderie pour une aube de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2846948A2 true EP2846948A2 (fr) | 2015-03-18 |
EP2846948B1 EP2846948B1 (fr) | 2016-06-15 |
Family
ID=47049311
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13728448.5A Active EP2846948B1 (fr) | 2012-05-11 | 2013-05-07 | Outillage de fabrication d'un noyau de fonderie pour une aube de turbomachine et son procédé de fabrication |
Country Status (10)
Country | Link |
---|---|
US (1) | US9505052B2 (fr) |
EP (1) | EP2846948B1 (fr) |
JP (1) | JP6236066B2 (fr) |
CN (1) | CN104271286B (fr) |
BR (1) | BR112014027831B1 (fr) |
CA (1) | CA2872066C (fr) |
FR (2) | FR2990367B1 (fr) |
IN (1) | IN2014DN09458A (fr) |
RU (1) | RU2627084C2 (fr) |
WO (1) | WO2013167847A2 (fr) |
Cited By (1)
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RU2726171C2 (ru) * | 2016-03-01 | 2020-07-09 | Сафран Эркрафт Энджинз | Стержень для литья лопатки газотурбинного двигателя |
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FR3022810B1 (fr) * | 2014-06-30 | 2019-09-20 | Safran Aircraft Engines | Procede de fabrication d'un noyau pour le moulage d'une aube |
CN104338905B (zh) * | 2014-10-16 | 2016-06-01 | 沈阳黎明航空发动机(集团)有限责任公司 | 一种定向凝固叶片陶瓷型芯成形装置 |
US10280761B2 (en) * | 2014-10-29 | 2019-05-07 | United Technologies Corporation | Three dimensional airfoil micro-core cooling chamber |
FR3037829B1 (fr) | 2015-06-29 | 2017-07-21 | Snecma | Noyau pour le moulage d'une aube ayant des cavites superposees et comprenant un trou de depoussierage traversant une cavite de part en part |
FR3047767B1 (fr) * | 2016-02-12 | 2019-05-31 | Safran | Procede de formation de trous de depoussierage pour aube de turbine et noyau ceramique associe |
US20180298765A1 (en) * | 2017-04-14 | 2018-10-18 | General Electric Company | Engine component with replaceable tip element |
FR3065660B1 (fr) * | 2017-04-28 | 2019-06-14 | Safran Aircraft Engines | Ensemble pour la fabrication d'une aube de turbomachine |
FR3065662B1 (fr) | 2017-04-28 | 2020-11-13 | Safran Aircraft Engines | Noyau pour la fabrication d'une aube de turbomachine |
FR3065661B1 (fr) * | 2017-04-28 | 2019-06-14 | Safran Aircraft Engines | Noyau pour la fabrication par moulage a la cire perdue d'une aube de turbomachine |
FR3070624B1 (fr) | 2017-09-06 | 2019-09-13 | Safran Aircraft Engines | Carter en materiau composite a geometrie raidissante |
KR101955858B1 (ko) * | 2018-09-07 | 2019-03-08 | 국방과학연구소 | 중공형 가스터빈 블레이드 내에 유로를 형성하기 위한 유로 형성 가이드 및 유로 형성 가이드 제작 장치 |
US10913106B2 (en) | 2018-09-14 | 2021-02-09 | Raytheon Technologies Corporation | Cast-in film cooling hole structures |
US11759850B2 (en) | 2019-05-22 | 2023-09-19 | Siemens Energy Global GmbH & Co. KG | Manufacturing aligned cooling features in a core for casting |
FR3100143B1 (fr) * | 2019-08-30 | 2021-11-12 | Safran | Procédé amélioré de fabrication d’un noyau céramique pour la fabrication d’aubes de turbomachine |
CN111036839B (zh) * | 2019-12-31 | 2021-03-23 | 无锡市铭腾模具科技有限公司 | 便于脱模的砂芯成型模具 |
FR3108540B1 (fr) * | 2020-03-25 | 2022-04-08 | Safran | Moule pour la fabrication d’un noyau céramique de fonderie |
FR3121372B1 (fr) * | 2021-03-30 | 2023-03-31 | Safran | Système d’insertion de tiges dans une ébauche de noyau céramique pour la fabrication d’aubes de turbomachine |
FR3126894A1 (fr) * | 2021-09-15 | 2023-03-17 | Safran | Dispositif et procede de fabrication d’un noyau en ceramique pour aube |
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US5733102A (en) * | 1996-12-17 | 1998-03-31 | General Electric Company | Slot cooled blade tip |
US6637500B2 (en) * | 2001-10-24 | 2003-10-28 | United Technologies Corporation | Cores for use in precision investment casting |
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US6929054B2 (en) * | 2003-12-19 | 2005-08-16 | United Technologies Corporation | Investment casting cores |
FR2878458B1 (fr) | 2004-11-26 | 2008-07-11 | Snecma Moteurs Sa | Procede de fabrication de noyaux ceramiques de fonderie pour aubes de turbomachines, outil pour la mise en oeuvre du procede |
FR2889088B1 (fr) * | 2005-07-29 | 2008-08-22 | Snecma | Noyau pour aubes de turbomachine |
FR2914871B1 (fr) | 2007-04-11 | 2009-07-10 | Snecma Sa | Outillage pour la fabrication de noyaux ceramiques de fonderie pour aubes de turbomachines |
FR2957828B1 (fr) * | 2010-03-26 | 2012-10-05 | Snecma | Extraction des tiges d'alumine utilisees pour le maintien du noyau lors de la fabrication d'aubes de turbine. |
CN201855923U (zh) * | 2010-10-31 | 2011-06-08 | 东风汽车零部件(集团)有限公司 | 内冷油道活塞盐芯定位装置 |
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2012
- 2012-05-11 FR FR1254350A patent/FR2990367B1/fr active Active
- 2012-09-05 FR FR1258282A patent/FR2990368B1/fr active Active
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2013
- 2013-05-07 US US14/400,457 patent/US9505052B2/en active Active
- 2013-05-07 BR BR112014027831-8A patent/BR112014027831B1/pt active IP Right Grant
- 2013-05-07 CA CA2872066A patent/CA2872066C/fr active Active
- 2013-05-07 CN CN201380024670.0A patent/CN104271286B/zh active Active
- 2013-05-07 IN IN9458DEN2014 patent/IN2014DN09458A/en unknown
- 2013-05-07 WO PCT/FR2013/051028 patent/WO2013167847A2/fr active Application Filing
- 2013-05-07 RU RU2014150082A patent/RU2627084C2/ru active
- 2013-05-07 JP JP2015510863A patent/JP6236066B2/ja active Active
- 2013-05-07 EP EP13728448.5A patent/EP2846948B1/fr active Active
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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RU2726171C2 (ru) * | 2016-03-01 | 2020-07-09 | Сафран Эркрафт Энджинз | Стержень для литья лопатки газотурбинного двигателя |
Also Published As
Publication number | Publication date |
---|---|
US20150122445A1 (en) | 2015-05-07 |
RU2014150082A (ru) | 2016-07-10 |
FR2990367A1 (fr) | 2013-11-15 |
WO2013167847A2 (fr) | 2013-11-14 |
FR2990368A1 (fr) | 2013-11-15 |
CA2872066C (fr) | 2020-06-23 |
EP2846948B1 (fr) | 2016-06-15 |
WO2013167847A3 (fr) | 2014-07-03 |
CN104271286B (zh) | 2016-09-21 |
FR2990368B1 (fr) | 2014-04-25 |
JP2015520677A (ja) | 2015-07-23 |
JP6236066B2 (ja) | 2017-11-22 |
RU2627084C2 (ru) | 2017-08-03 |
BR112014027831B1 (pt) | 2019-10-29 |
US9505052B2 (en) | 2016-11-29 |
CA2872066A1 (fr) | 2013-11-14 |
BR112014027831A2 (pt) | 2017-06-27 |
FR2990367B1 (fr) | 2014-05-16 |
IN2014DN09458A (fr) | 2015-07-17 |
CN104271286A (zh) | 2015-01-07 |
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