EP3953082A1 - Verfahren zur herstellung einer mehrzahl von leitschaufelabschnitten durch giessen - Google Patents
Verfahren zur herstellung einer mehrzahl von leitschaufelabschnitten durch giessenInfo
- Publication number
- EP3953082A1 EP3953082A1 EP20731165.5A EP20731165A EP3953082A1 EP 3953082 A1 EP3953082 A1 EP 3953082A1 EP 20731165 A EP20731165 A EP 20731165A EP 3953082 A1 EP3953082 A1 EP 3953082A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cavity
- blade
- cluster
- shell
- mold
- 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.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 33
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 20
- 238000005266 casting Methods 0.000 title claims description 5
- 238000007711 solidification Methods 0.000 claims abstract description 30
- 230000008023 solidification Effects 0.000 claims abstract description 30
- 239000002184 metal Substances 0.000 claims abstract description 28
- 239000000919 ceramic Substances 0.000 claims abstract description 11
- 238000010438 heat treatment Methods 0.000 claims abstract description 4
- 230000002250 progressing effect Effects 0.000 claims abstract description 4
- 238000011144 upstream manufacturing Methods 0.000 claims description 9
- 239000013078 crystal Substances 0.000 claims description 7
- 239000012212 insulator Substances 0.000 claims description 7
- 238000004891 communication Methods 0.000 claims description 3
- 238000000465 moulding Methods 0.000 abstract description 6
- 238000005495 investment casting Methods 0.000 abstract description 2
- 239000008186 active pharmaceutical agent Substances 0.000 abstract 1
- 210000002105 tongue Anatomy 0.000 description 5
- 230000003071 parasitic effect Effects 0.000 description 4
- 101100327917 Caenorhabditis elegans chup-1 gene Proteins 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 230000003471 anti-radiation Effects 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 229910010293 ceramic material Inorganic materials 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling the mould
- B22D27/045—Directionally solidified castings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/06—Permanent moulds for shaped castings
-
- 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
Definitions
- manufacture of metal turbomachine parts by foundry It relates more particularly to a method of manufacturing a plurality of monocrystalline distributor sectors each comprising at least one blade extending between two platforms.
- FIG. 1 shows for example a single-bladed distributor sector 1.
- FIG. 2 shows for example a two-bladed distributor sector 2.
- a distributor sector generally comprises one or more blades 3 which extend between two platforms 4 delimiting the duct. flow of the gas stream. Due to their complex shape, and in order to obtain a monocrystalline part, it is often necessary to develop ceramic molds comprising artifices such as grain supply conduits connecting a single crystal grain supply device to different parts of the mold cavity, and in particular to the part intended to form the blade (s) of the distributor sector.
- FIG. 3 shows a view of the internal volume of a mold 5 for manufacturing a two-bladed distributor sector 2 such as that of FIG. 2, comprising a grain supplier device 6 housing here a monocrystalline seed connected to the parts 7 of the mold cavity intended to form the blades 3 by grain supply ducts 8.
- the invention relates to a method of manufacturing a plurality of monocrystalline distributor sectors each comprising at least a first blade extending between two platforms, the method comprising the casting of a molten metal in a plurality of molds ceramics distributed in a cluster around an axis, and the directed solidification of the metal cast in a furnace comprising a radiating heating element configured to be disposed around the cluster, a solidification front of the metal progressing in each mold in a direction parallel to the axis of the cluster during directed solidification, in which each mold comprises:
- a first shell delimiting a first mold cavity of a distributor sector, the first cavity having parts forming the platforms of the distributor sector, and a part forming a first blade having a external face with respect to the axis of the cluster corresponding to an extrados face of the first blade, a first edge and a second edge corresponding respectively to a leading edge and to a trailing edge of the first blade, the first edge being located upstream of the second edge with respect to the direction of progression of the solidification front, and
- each mold further comprises a second shell separated from the first shell and located upstream of the latter with respect to the direction of progression of the solidification front, the second shell defining a second mold cavity of a blade dummy connected to the grain supply device, the second cavity having a face corresponding to an extrados face of the dummy blade parallel to the external face of the first cavity.
- the method according to the invention differs in particular from the methods of the prior art by the use of molds provided with mold cavities of dummy blades.
- the presence of these dummy blades makes it possible to form an anti-radiation heat shield for each sector of the molded distributor, in particular for the blade or blades thereof, during the directed solidification of the cast metal.
- the separation between the first and the second shell prevents thermal bridges between them.
- the aforementioned characteristics second molding shell of a dummy blade, and separation of the first and second shell), in particular, thus make it possible to drastically reduce the formation of parasitic grains and the number of parts rejected because of them. .
- each dummy blade can be independent, that is to say is not connected to platforms.
- the part of each first cavity forming a first blade can only be in communication with the parts of said cavity forming the platforms.
- each mold may be devoid of a grain supply duct between the grain supplying device and the part forming the first blade, and between the grain supplying device and a second blade, if applicable.
- each dummy blade may have the shape of a curved strip. This shape makes it possible to obtain a dummy blade of reduced mass maintaining a heat shield function with little impact on the mass and strength of the cluster.
- each dummy blade may include part of a lower surface face so that each second shell forms a tongue extending inside the cluster.
- the shell formed around this tab can be used to hold, for example, a thermal insulator inside the cluster.
- a thermal insulator can be placed at
- thermal insulation being held over at least one tongue of a second shell.
- the presence of such a thermal insulator makes it possible to improve the temperature homogeneity during directed solidification, to obtain a more stable solidification front, and thus further reduce the appearance of parasitic grains.
- the thermal insulation can be a carbon felt.
- each mold may further comprise a supply cavity having a triangular shape, the ducts
- the feeder and the single crystal grain feeder device being connected to said cavity at the tops of the feed cavity, the second cavity being connected to the feed cavity at one side thereof located between the two supply ducts.
- a junction can connect the cavity
- each distributor sector can further comprise a second blade, the part of the first cavity forming the second blade being located downstream of the part of the first cavity forming the first blade relative to the direction of progression of the solidification front. This arrangement makes it possible to manufacture a two-bladed distributor sector.
- each grain supplier device may comprise a housing in which a single crystal seed is present.
- the cluster may comprise between four and twelve ceramic molds, for example six ceramic molds.
- Figure 1 shows an example of a single-bladed distributor sector.
- Figure 2 shows a two-bladed distributor sector.
- Figure 3 shows a mold for making a two-bladed distributor sector used in a prior art process.
- Figure 4 shows a cluster comprising several molds for manufacturing two-bladed distributor sectors in a method according to the invention.
- Figure 5 shows a perspective view of a mold of the bunch of Figure 4.
- Figure 6 shows a detailed front view of the mold of Figure 5.
- Figure 7 shows a detailed rear view of the mold of the
- Figure 8 shows an enlarged view of Figure 6 at the level of the second cavity.
- Figure 9 shows an enlarged side view of the mold of the
- Figure 10 shows a sectional view along the X plane identified in Figure 6.
- Figure 1 1 shows the main steps of a
- Figure 12 illustrates the placement of a cluster in a furnace to achieve directed solidification of the cast metal.
- Figure 4 shows an installation or cluster 10 comprising a plurality of molds 100 for molding two-bladed distributor sectors 2 like that of Figure 2 by a method according to the invention, here the molds are six in number.
- the cluster 10 can include a different number of molds, for example a number between four and twelve.
- the cluster 10 has a central axis A around which the molds 100 are distributed.
- the cluster 10 comprises a cup 1 1 through which a liquid metal can be introduced into the cluster 10.
- the cup 1 1 overcomes a vertical or downward central duct 12.
- Near the opening of the cup 1 1 is a plurality of ducts 13 which make it possible to extract the wax before the step of casting a molten metal for each of the molds 100.
- a ring 14 connected to the descendant 12 by stiffeners 15 makes it possible to distribute the molten metal cast between the molds 100 and to feed them via supply conduits 16. In this example, there are two feed conduits 16 per mold 100.
- the entire cluster 10 can be placed on a horizontal sole 17 provided to support the 'together throughout the manufacturing process which will be described later in connection with FIG. 1 1.
- the sole 17 also makes it possible to avoid the complete fusion of the monocrystalline seed.
- a direction D s is defined corresponding to the direction of propagation of the solidification front of the metal progressing in the cluster during the directed solidification.
- the direction D s is parallel to the axis A of the cluster 10. In the figures, such a front will progress from the sole 17 to the bucket 1 1.
- a direction DR is defined corresponding to a radial direction with respect to the axis A of cluster 10, which defines the terms “interior” and “exterior” in relation to cluster 10.
- Figures 5 to 9 show different views of a mold 100 corresponding to a sector of the cluster 10.
- the mold 100 comprises a first shell which defines a first cavity 1 10 for molding the distributor sector 2.
- the first cavity 110 comprises parts 1 1 1 forming the platforms 4 of the distributor sector 2, a part 1 12 forming a first blade 3 ( Figures 6 and 7) and a part 1 13 forming a second blade 3.
- the parts 112 and 113 are thus each in communication only with the parts 11 11 forming the platforms.
- the conduits 13 for removing the wax, and the supply conduits 17 are connected to the parts 11 1 of the first cavity 1 10.
- the part 1 12 forming the first blade is located upstream with respect to the direction. D s of the part 112 forming the second blade.
- Each part 1 12 and 1 13 forming a first and a second blade is oriented so that the first and the second blade have an extrados face which is located radially (in the direction DR) on the outside with respect to their intrados face.
- the part 1 12 forming the first blade and the part 1 13 forming the second blade each have an external face 1 12a and 1 13a relative to the axis A of the cluster 10 which corresponds to the extrados face of the first or the second blade.
- the part 112 forming the first blade and the part 1 13 forming the second blade each have a first edge 112b and 1 13b corresponding to the leading edge of the corresponding blade and a second edge 112c and 1 13c corresponding at the trailing edge of the corresponding blade.
- the sector of distributor is oriented such that the first edges 112b and 1 13b are located upstream with respect to the direction D s of the second edges 1 12c and 1 13c.
- the mold 100 further comprises a grain supplier device
- monocrystalline 120 which may for example comprise a monocrystalline seed in a housing, connected by a triangular supply cavity 121 and two supply conduits 122 to the parts 11 of the first cavity 110 forming the platforms.
- the device 120 and the supply conduits 121 are connected to the tops of the triangular supply cavity 121.
- each mold 100 also has a second shell, separated from the first shell and located upstream of the latter with respect to the direction D s , defining a second mold cavity 130 d 'a dummy blade.
- a “dummy” blade because it simulates the presence of a blade in the distributor sector, but is not part of it.
- the dummy blade which will be molded in the second cavity will be separated from the distributor sector (or withdrawn or eliminated) at the end of the manufacturing process. It is in fact only used during directed solidification, where it acts as an anti-radiation heat shield to reduce the appearance of parasitic grains.
- the second cavity 130 is connected by a junction 131 only to the triangular supply cavity 121 at a middle part of one of its sides.
- the junction 131 has, in this example, a length L ( Figure 9) of at least 12 mm.
- the second cavity 130 has part of the aerodynamic profile
- the dummy blade (and therefore the cavity for molding it) here has the shape of a curved strip.
- the dummy blade also comprises a part of a lower surface of the blade so that the second shell forms a tongue 132 (FIG. 10) extending inside the cluster 10.
- the second cavity 130 is oriented so that the external face 1 12a of the part 1 12 of the first cavity 110 forming the first blade and the external face 130a are parallel (FIG. 9).
- the second cavity 130 can be separated by a minimum distance DO ( Figure 8) of at least 8 mm from the first cavity 1 10.
- Figure 10 shows a sectional view along the X plane identified in Figure 6.
- the ceramic shell of the mold 100 there is shown the ceramic shell of the mold 100.
- the mold 100 can be arranged so that the distance D1 separating the first edge 130b from the second cavity of the first edge 112b, and the distance D2 separating the first edge 112b from the first edge 113b can be roughly equal.
- the cluster 10 and the molds 100 which compose it can be made of ceramic material.
- a wax model of cluster 10 is first obtained.
- this wax model is covered with a ceramic shell by successive quenching in a suitable slip and sanding (tempering-stucco).
- the covered model is finally dewaxed and fired.
- FIG. 11 illustrates the main steps of a process for manufacturing a single crystal distributor sector 1 or 2 according to the invention using several molds 100 arranged in a cluster 10 such as that presented above.
- the first step E1 of the process consists in filling the molds 100 of the cluster 10 by pouring a molten metal in the cluster 10. To do this, the metal can be poured directly into the cup 11 of the installation, and it can travel by gravity until filling the molds 100.
- the second step E2 of the process comprises the directed solidification of the metal present in the molds.
- the cluster 10 filled with molten metal is placed in an oven 200 (figure 2) having a radiating heating element 210 arranged around the cluster 10.
- a thermal insulator 220 inside the cluster, for example a carbon felt, which is held on the tongues 132 of the second shells 130c forming the dummy blades.
- the thermal insulator 220 can take a cylindrical or conical shape and be placed in the cluster around the central channel 12.
- the solidification of the part is controlled by means of a thermal gradient in the oven 200. thermal gradient generally extends in the direction D s .
- the solidification front moves in the direction D s from the monocrystalline grain supply devices 120 to the bucket 1 1.
- the solidification front can be moved by for example moving the cluster 10 vertically (this is also referred to as “draw”) in the oven 200 (arrow 230).
- draw the oven 200
- the method comprises a step of removing the dummy blade from the solidified assembly to obtain the distributor sector (in other words, the dummy blade is separated from the distributor sector thus manufactured).
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1903733A FR3094655B1 (fr) | 2019-04-08 | 2019-04-08 | Procédé de fabrication d’une pluralité de secteurs de distributeur par fonderie |
PCT/FR2020/050613 WO2020208325A1 (fr) | 2019-04-08 | 2020-03-20 | Procede de fabrication d'une pluralite de secteurs de distributeur par fonderie |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3953082A1 true EP3953082A1 (de) | 2022-02-16 |
Family
ID=67514879
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20731165.5A Pending EP3953082A1 (de) | 2019-04-08 | 2020-03-20 | Verfahren zur herstellung einer mehrzahl von leitschaufelabschnitten durch giessen |
Country Status (5)
Country | Link |
---|---|
US (1) | US11712737B2 (de) |
EP (1) | EP3953082A1 (de) |
CN (1) | CN113677454B (de) |
FR (1) | FR3094655B1 (de) |
WO (1) | WO2020208325A1 (de) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113042713B (zh) * | 2021-02-26 | 2023-05-12 | 贵阳航发精密铸造有限公司 | 一种大尺寸或多联单晶导向叶片的引晶结构及制造装置 |
CN113042687A (zh) * | 2021-02-26 | 2021-06-29 | 贵阳航发精密铸造有限公司 | 晶体取向可控的大尺寸单晶导向叶片的铸造模组 |
CN114682734B (zh) * | 2022-03-18 | 2023-03-24 | 江西亿丰精密铸造有限公司 | 一种用于消失模铸造的设备 |
CN115121768B (zh) * | 2022-04-26 | 2024-04-05 | 湘潭大学 | 型壳结构及其制备方法和热裂倾向性判定方法 |
CN117047041B (zh) * | 2023-10-12 | 2023-12-19 | 中国航发沈阳黎明航空发动机有限责任公司 | 一种三联体实心导向叶片柱晶铸造系统结构及铸造工艺 |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2724857B1 (fr) * | 1980-12-30 | 1997-01-03 | Snecma | Procede de fabrication d'aubes cristallines |
GB2259660A (en) * | 1991-09-17 | 1993-03-24 | Rolls Royce Plc | A mould for casting components |
FR2927270B1 (fr) * | 2008-02-08 | 2010-10-22 | Snecma | Procede de fabrication d'aubes a solidification dirigee |
FR2985924B1 (fr) * | 2012-01-24 | 2014-02-14 | Snecma | Carapace pour la fabrication par moulage a cire perdue d'elements aubages de turbomachine d'aeronef, comprenant des ecrans formant accumulateurs de chaleur |
FR2995235B1 (fr) * | 2012-09-11 | 2016-12-09 | Snecma | Modele de fonderie |
FR2995807B1 (fr) * | 2012-09-25 | 2015-10-09 | Snecma | Moule carapace a ecran thermique |
FR3031921B1 (fr) * | 2015-01-27 | 2017-02-10 | Snecma | Procede et machine de decochage pour grappe de pieces de fonderie a modele perdu |
FR3034128B1 (fr) * | 2015-03-23 | 2017-04-14 | Snecma | Noyau ceramique pour aube de turbine multi-cavites |
FR3052088B1 (fr) * | 2016-06-02 | 2018-06-22 | Safran | Moule pour la fabrication d'une aube monocristalline par fonderie, installation et procede de fabrication le mettant en oeuvre |
FR3070286B1 (fr) * | 2017-08-31 | 2022-01-21 | Safran Aircraft Engines | Arbre de coulee pour procede de fabrication par fonderie a modele perdu et procede de fabrication |
CN107745093B (zh) * | 2017-12-06 | 2023-06-06 | 安徽应流航源动力科技有限公司 | 一种精铸模组及利用其制备可精控晶体取向的镍基单晶导叶的铸造方法 |
-
2019
- 2019-04-08 FR FR1903733A patent/FR3094655B1/fr active Active
-
2020
- 2020-03-20 WO PCT/FR2020/050613 patent/WO2020208325A1/fr unknown
- 2020-03-20 CN CN202080027385.4A patent/CN113677454B/zh active Active
- 2020-03-20 US US17/598,672 patent/US11712737B2/en active Active
- 2020-03-20 EP EP20731165.5A patent/EP3953082A1/de active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Also Published As
Publication number | Publication date |
---|---|
FR3094655B1 (fr) | 2021-02-26 |
CN113677454B (zh) | 2022-08-16 |
US20220193761A1 (en) | 2022-06-23 |
WO2020208325A1 (fr) | 2020-10-15 |
US11712737B2 (en) | 2023-08-01 |
FR3094655A1 (fr) | 2020-10-09 |
CN113677454A (zh) | 2021-11-19 |
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