EP2794147A2 - Process for manufacturing a ceramic core for a rotor blade, ceramic core, rotor blade - Google Patents
Process for manufacturing a ceramic core for a rotor blade, ceramic core, rotor bladeInfo
- Publication number
- EP2794147A2 EP2794147A2 EP12824903.4A EP12824903A EP2794147A2 EP 2794147 A2 EP2794147 A2 EP 2794147A2 EP 12824903 A EP12824903 A EP 12824903A EP 2794147 A2 EP2794147 A2 EP 2794147A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- core
- ceramic
- manufacturing
- rod
- rods
- 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
- 239000000919 ceramic Substances 0.000 title claims abstract description 52
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 19
- 238000000034 method Methods 0.000 title claims description 18
- 239000000463 material Substances 0.000 claims abstract description 25
- 238000000576 coating method Methods 0.000 claims abstract description 21
- 239000011248 coating agent Substances 0.000 claims abstract description 20
- 238000000465 moulding Methods 0.000 claims abstract description 12
- 238000010304 firing Methods 0.000 claims abstract description 11
- 239000002966 varnish Substances 0.000 claims description 28
- 238000010411 cooking Methods 0.000 claims description 12
- 238000002347 injection Methods 0.000 claims description 7
- 239000007924 injection Substances 0.000 claims description 7
- 229920005989 resin Polymers 0.000 claims description 7
- 239000011347 resin Substances 0.000 claims description 7
- 238000012423 maintenance Methods 0.000 claims description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 4
- 229910002804 graphite Inorganic materials 0.000 claims description 4
- 239000010439 graphite Substances 0.000 claims description 4
- 230000008021 deposition Effects 0.000 claims description 3
- 238000005266 casting Methods 0.000 claims 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 6
- 229910010293 ceramic material Inorganic materials 0.000 description 5
- 238000005336 cracking Methods 0.000 description 5
- 230000010339 dilation Effects 0.000 description 5
- 206010061218 Inflammation Diseases 0.000 description 4
- 230000004054 inflammatory process Effects 0.000 description 4
- 239000000243 solution Substances 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- VJYFKVYYMZPMAB-UHFFFAOYSA-N ethoprophos Chemical compound CCCSP(=O)(OCC)SCCC VJYFKVYYMZPMAB-UHFFFAOYSA-N 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 239000000020 Nitrocellulose Substances 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000008246 gaseous mixture Substances 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229920001220 nitrocellulos Polymers 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 239000011505 plaster Substances 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
- 230000009974 thixotropic effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 239000001993 wax Substances 0.000 description 1
Classifications
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28B—SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
- B28B1/00—Producing shaped prefabricated articles from the material
- B28B1/24—Producing shaped prefabricated articles from the material by injection moulding
-
- 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
-
- 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
-
- 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
- F05D2230/211—Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment casting
Definitions
- the field of the invention relates to the processes for manufacturing ceramic cores used in lost-wax foundry for the manufacture of complex hollow blades for the circulation of moving blades.
- the invention relates in particular to the field of aeronautics in which such blades can be used in aircraft engines.
- the ceramic core is a removable part which serves to obtain in particular the cooling circuit of the metal blading.
- the cores are made by injecting a polymer-ceramic mixture into an injection tool.
- the cores are baked to remove the polymer and sinter the ceramic.
- the cores are deburred and impregnated with resin which gives them mechanical strength.
- Figure 1 shows a ceramic core body having an upper portion 2 forming a bath and a lower portion 1 forming a core core.
- the ceramic core is used for the blades, in particular of turbine for an aircraft engine. Generally, this type of blade is coupled to a circular vane surrounding the blades.
- the part forming a bath forms a cavity opening at the end of the blade.
- the tub is used to reduce centrifugal forces at the blade root and reduce heat transfer at the blade tip. It is integral with the core body by the use of rods 3 which connect the body of the core to the bathtub.
- the rods can also be ceramic. In general, any material having a coefficient greater than the coefficient of expansion of the cores is suitable for producing the rods. A problem during the manufacture of such nuclei is encountered during the cooking step of said nuclei.
- the baking step follows the step of molding the ceramic in a mold in which the rods are pre-positioned before the injection of material.
- FIG. 2 shows a consequence of the expansion of a rod in the ceramic after firing, in particular by the generation of a crack 20 forming an emergent cracking of the bath 2.
- One solution is to set up a local extra thickness on the core facing the alumina rod.
- Figure 3 shows a thickening 30 introduced to consolidate the portion forming a crack after firing the ceramic along the bath at the rods located in the interior of the ceramic. The extra thickness is then removed. Before the shaving of the local extra thickness, there were no visible cracks along the stem.
- a disadvantage of this solution is that it is necessary to remove after baking, for example by manual sanding, this extra thickness. During this operation, it appears that the crack is likely to appear again on the bathtub. It then forms a crack opening on the surface of the bath.
- a major disadvantage is that the core is then unusable and potentially put off.
- the invention solves the aforementioned drawbacks.
- the object of the invention relates to a method of manufacturing a ceramic core for blade having a lower portion forming a core body, an upper part forming a bath and a set of rods contributing to the maintenance of the upper part with the part lower.
- the method of the invention comprises: • a coating step (also called coating step) rods by a material having a flash point less than a temperature threshold beyond which the expansion of the rod is greater than a predefined proportion;
- a step of firing the ceramic core is
- the temperature threshold is
- the proportion of dilation of the rod is 1%.
- the method of manufacturing ceramic core avoids cracking of the ceramic caused by the presence of the rods during cooking.
- the method of the invention comprises in particular a preliminary step of coating at least one rod such as a varnishing.
- the varnishing of the stem prevents cracking of the bathtub.
- Each rod may be alumina or be made of a ceramic material having a coefficient greater than the coefficient of expansion of the cores.
- the steps are carried out successively.
- a demolding step (DEM) of the nucleus precedes the cooking step (CUI) of the latter.
- each rod is coated on the surface likely to be surrounded by the tub.
- the coating of a portion of the rods is a varnish of a layer of varnish.
- the coating of the stems comprises either:
- the subject of the invention also relates to a ceramic core for a turbine blade comprising a lower part forming a core body, an upper part forming a bath and a set of rods making it possible to contribute to the maintenance of the upper and lower parts between them, characterized in that the core is manufactured according to a method of the invention.
- the invention further relates to a turbine blade made by a foundry method having used a core made by the method of the invention.
- FIG. 1 is a representation of a ceramic core for moving blades
- FIG. 2 a representation of a ceramic core after curing and forming an inlet of the core bath
- FIG. 3 a representation of a ceramic core comprising an extra thickness to support the formation of a crack
- FIG. 4 a diagram showing the main steps of the inventive method.
- flash point also called “flash point” or “flash point” in the English terminology, the lowest temperature at which a body or a combustible material emits enough vapors to form, with the ambient air, a gaseous mixture which ignites under the effect of a source of heat energy.
- a ceramic core for turbine blade has a lower portion forming a core body, an upper portion forming a tub and a set of rods to help maintain the upper and lower parts therebetween.
- the upper and lower parts are joined together.
- at least one rod makes it possible to contribute to the maintenance of the two parts of the core.
- the lower and upper portions may comprise a common zone also contributing to the maintenance of the two parts together.
- FIG. 1 shows such an embodiment in which parts 1 and 2 are also maintained by a common zone 4 situated on the side of the core.
- the method of manufacturing a ceramic core of the invention comprises a coating step, denoted END in Figure 4, rods prior to their introduction into a mold for molding ceramic parts.
- the varnish is deposited on the part of the stem that will be surrounded by the tub of the core.
- the portion of the stem which is encircled by the core body is not coated with varnish.
- the coating of the rods can be performed when the rods are already positioned in the mold. But preferably, the rods are coated before their introduction into the mold so as to cover uniformly the entire surface of the rod.
- the coating of the rods can be achieved in different ways depending on: the type of material that is applied, the thickness of the desired layer of material and / or the part of the rod, or rods, which it is desired to cover.
- the entire rod is covered with a material whose flash point is less than 1000 ° C.
- each rod encircled by the bath is covered with plaster.
- the part of the stem encircled by the core body is not coated with varnish.
- the temperature limit of 1000 ° C. corresponds to the starting temperature of transformation of the ceramic materials constituting the core. This limit thus constitutes a particularly advantageous temperature for the material applied to the rod to ignite before the cooking temperature reaches this limit. It is also possible to choose lower limits that work a fortiori also from the moment when the temperature of the flash point of the material is lower than this limit.
- a temperature threshold will be chosen which makes it possible to obtain an inflammation of the coated material, such as a varnish, before the rod expands.
- the dilation is considered to be substantially zero before a certain limit.
- this limit is set at 1%, which corresponds to a 1% expansion of the dimensions of the rod.
- the predefined proportion defining the limit of a so-called “consequent" expansion may be greater than 1% is up to 2% or more depending on the materials used and their dimensions.
- the application of the material can be carried out either by dipping the stems or by applying the material from a brush for example on the stems.
- the applied material is a varnish.
- the latter may for example be of the "nail polish" type.
- the varnish application process can then be applied to the rod of conventional way by a brush as one would apply a varnish on a nail of a woman's hand.
- a suitable varnish includes solvents, resin, nitrocellulose and plasticizers.
- a varnish such as "Thixotropic base” marketed under the trade name: "Peggy Sage Nail Polish All Formulas” can be used in the process of the present invention.
- the rod is positioned according to a process step denoted POS, after drying of the varnish.
- POS process step denoted POS
- the method comprises a molding step, denoted MOU in FIG. 4, comprising an injection of the ceramic into the mold.
- the injection of the ceramic forms the core in the housing provided for this purpose thus forming the body and the bathtub according to the shape of the mold.
- the step of molding the ceramic comprises molding the lower portion forming the core body and molding an upper portion forming a bath.
- the molding of the two parts is preferably done at the same time.
- the stems are positioned to include a portion of the stem in the upper portion of the core and a portion of the stem in the lower portion of the core.
- the ceramic material injected into the portion of the mold forming the tub surrounds the portion of the rod present in the tub and the ceramic material injected into the mold portion forming the core body surrounds the portion of the rod positioned in this portion of the mold.
- the rod holds the two parts of the core.
- the core is then demolded, this step is denoted DEM in Figure 4.
- the rod or rods integral (s) of the two parts of the core are also output (s) of the mold.
- a firing step of the core thus demolded denoted CUI in FIG. 4, can then be engaged.
- the varnish covering the stems reaches its flash point before the dilation of the stem reaches consequent proportions.
- the coefficient of expansion of alumina at 1200 ° C. is 1.03%.
- the burn or inflammation of the varnish corresponding to the achievement of the flash point of the varnish takes place at a temperature lower than the firing temperature resulting in expansion of the alumina rod.
- tests make it possible to choose the type of material used to cover the rods and to choose the appropriate thickness of said layers when they are affixed to the rods. These tests make it possible to perfectly adapt the space released by the burnt material and the space required for the expansion of the rod during cooking.
- the steps of the process of the invention are preferably carried out sequentially. But in one embodiment, it can be envisaged that the coating step of each rod is carried out while the latter are already arranged in the mold. On the other hand, it seems inevitable to perform the molding and baking in a sequential order for the good realization of the invention.
- All the products that can be used in the present invention allow a deposition of a thin layer, for example of a few hundredths of a millimeter. It is necessary that the products applied to the stems are eliminated by cooking before the expansion of the alumina stem. In preferred embodiments of the invention, it is also important that those products used as rod coatings leave no undesirable chemical residues.
- the following products can be used: wax, resin, paint and / or graphite.
- a homogeneous deposit can be made on the entire surface of the rod;
- the combustion can be advantageously controlled so as to avoid or limit carbon monoxide emissions.
- the combustion can be controlled from to ensure a sufficiently oxidizing atmosphere during cooking.
- An advantage of the wax is its plasticity and malleability at room temperature which gives it a particular interest for the coating of a rod. Its melting point at 45 ° C makes it possible to free a space around the stem before the dilation of the stem. Another advantage lies in its low viscosity when it is melted, which allows to leave a homogeneous space around the stem.
- the method of the invention may include steps of sintering the ceramic and recovering resin after core firing.
- the invention relates to a ceramic core obtained by the method of the invention.
- the ceramic core of the invention has the particularity of being manufactured by the use of rods coated with a material having a lower flammability temperature than the expansion temperature of alumina.
- the invention also relates to a mobile turbine blade having a ceramic core obtained by the method of the invention.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Ceramic Engineering (AREA)
- Architecture (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Cookers (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1162358A FR2984880B1 (en) | 2011-12-23 | 2011-12-23 | METHOD FOR MANUFACTURING A CERAMIC CORE FOR MOBILE DREAM, CERAMIC CORE, MOBILE AUB |
PCT/FR2012/053010 WO2013093352A2 (en) | 2011-12-23 | 2012-12-20 | Method of manufacturing a ceramic core for a blade, ceramic core and blade |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2794147A2 true EP2794147A2 (en) | 2014-10-29 |
EP2794147B1 EP2794147B1 (en) | 2019-04-03 |
Family
ID=47741153
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12824903.4A Active EP2794147B1 (en) | 2011-12-23 | 2012-12-20 | Process for manufacturing a ceramic core for a rotor blade |
Country Status (9)
Country | Link |
---|---|
US (1) | US9890643B2 (en) |
EP (1) | EP2794147B1 (en) |
JP (1) | JP6097307B2 (en) |
CN (1) | CN104039476B (en) |
BR (1) | BR112014015655B1 (en) |
CA (1) | CA2860290C (en) |
FR (1) | FR2984880B1 (en) |
RU (1) | RU2642228C2 (en) |
WO (1) | WO2013093352A2 (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104647586B (en) * | 2013-11-19 | 2017-09-22 | 中国科学院金属研究所 | A kind of preparation method of labyrinth single crystal hollow blade composite ceramic core |
CN104232934B (en) * | 2014-08-22 | 2016-01-20 | 石家庄金刚凯源动力科技有限公司 | Casting Aluminum Piston Sweet natural gas holding furnace |
CN104338905B (en) * | 2014-10-16 | 2016-06-01 | 沈阳黎明航空发动机(集团)有限责任公司 | A kind of directional solidification blade ceramic core shaping device |
FR3048374B1 (en) * | 2016-03-01 | 2018-04-06 | Snecma | CORE FOR MOLDING A DAWN WITH SUPERIOR CAVITIES AND COMPRISING A DEDUSTING LINE CONDUCTING A CAVITY FROM PART TO SHARE |
CN107584084A (en) * | 2017-09-12 | 2018-01-16 | 东方电气集团东方汽轮机有限公司 | Hollow blade essence casting ceramic shell mould forming method |
CN110773706B (en) * | 2019-09-30 | 2021-09-21 | 北京航空材料研究院有限公司 | Casting and forming method thereof |
CN111266525A (en) * | 2020-03-17 | 2020-06-12 | 黄国莲 | Investment casting equipment utilizing wax fluidity |
FR3108540B1 (en) * | 2020-03-25 | 2022-04-08 | Safran | Mold for the manufacture of a foundry ceramic core |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4532974A (en) * | 1981-07-03 | 1985-08-06 | Rolls-Royce Limited | Component casting |
US6637500B2 (en) * | 2001-10-24 | 2003-10-28 | United Technologies Corporation | Cores for use in precision investment casting |
US6929054B2 (en) * | 2003-12-19 | 2005-08-16 | United Technologies Corporation | Investment casting cores |
FR2878458B1 (en) * | 2004-11-26 | 2008-07-11 | Snecma Moteurs Sa | METHOD FOR MANUFACTURING CERAMIC FOUNDRY CORES FOR TURBOMACHINE BLADES, TOOL FOR IMPLEMENTING THE METHOD |
US7326030B2 (en) * | 2005-02-02 | 2008-02-05 | Siemens Power Generation, Inc. | Support system for a composite airfoil in a turbine engine |
FR2889088B1 (en) * | 2005-07-29 | 2008-08-22 | Snecma | CORE FOR BLADE OF TURBOMACHINE |
US7610946B2 (en) * | 2007-01-05 | 2009-11-03 | Honeywell International Inc. | Cooled turbine blade cast tip recess |
FR2914871B1 (en) * | 2007-04-11 | 2009-07-10 | Snecma Sa | TOOLS FOR THE MANUFACTURE OF CERAMIC FOUNDRY CORES FOR TURBOMACHINE BLADES |
CN100560248C (en) * | 2007-06-19 | 2009-11-18 | 西安交通大学 | A kind of core and shell integrated ceramic casting mold manufacture method |
-
2011
- 2011-12-23 FR FR1162358A patent/FR2984880B1/en active Active
-
2012
- 2012-12-20 BR BR112014015655A patent/BR112014015655B1/en active IP Right Grant
- 2012-12-20 CA CA2860290A patent/CA2860290C/en active Active
- 2012-12-20 WO PCT/FR2012/053010 patent/WO2013093352A2/en active Application Filing
- 2012-12-20 JP JP2014548157A patent/JP6097307B2/en active Active
- 2012-12-20 US US14/368,215 patent/US9890643B2/en active Active
- 2012-12-20 EP EP12824903.4A patent/EP2794147B1/en active Active
- 2012-12-20 RU RU2014130211A patent/RU2642228C2/en not_active Application Discontinuation
- 2012-12-20 CN CN201280066793.6A patent/CN104039476B/en active Active
Non-Patent Citations (1)
Title |
---|
See references of WO2013093352A2 * |
Also Published As
Publication number | Publication date |
---|---|
CN104039476B (en) | 2016-06-22 |
US9890643B2 (en) | 2018-02-13 |
WO2013093352A3 (en) | 2013-08-29 |
BR112014015655B1 (en) | 2020-01-28 |
JP6097307B2 (en) | 2017-03-15 |
US20140369842A1 (en) | 2014-12-18 |
CA2860290A1 (en) | 2013-06-27 |
BR112014015655A2 (en) | 2017-06-13 |
BR112014015655A8 (en) | 2017-07-04 |
WO2013093352A2 (en) | 2013-06-27 |
RU2014130211A (en) | 2016-02-20 |
CA2860290C (en) | 2019-10-22 |
RU2642228C2 (en) | 2018-01-24 |
JP2015506840A (en) | 2015-03-05 |
CN104039476A (en) | 2014-09-10 |
FR2984880B1 (en) | 2014-11-21 |
EP2794147B1 (en) | 2019-04-03 |
FR2984880A1 (en) | 2013-06-28 |
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