EP2938448B1 - Noyau de moulage de précision à modèle perdu contenant de la mullite - Google Patents
Noyau de moulage de précision à modèle perdu contenant de la mullite Download PDFInfo
- Publication number
- EP2938448B1 EP2938448B1 EP13868294.3A EP13868294A EP2938448B1 EP 2938448 B1 EP2938448 B1 EP 2938448B1 EP 13868294 A EP13868294 A EP 13868294A EP 2938448 B1 EP2938448 B1 EP 2938448B1
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- EP
- European Patent Office
- Prior art keywords
- mullite
- core body
- investment casting
- core
- recited
- Prior art date
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- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 title claims description 102
- 229910052863 mullite Inorganic materials 0.000 title claims description 102
- 238000005495 investment casting Methods 0.000 title claims description 36
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 33
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 30
- 239000000843 powder Substances 0.000 claims description 25
- 239000000463 material Substances 0.000 claims description 22
- 238000009826 distribution Methods 0.000 claims description 17
- 238000000034 method Methods 0.000 claims description 17
- 239000000203 mixture Substances 0.000 claims description 17
- RUDFQVOCFDJEEF-UHFFFAOYSA-N yttrium(III) oxide Inorganic materials [O-2].[O-2].[O-2].[Y+3].[Y+3] RUDFQVOCFDJEEF-UHFFFAOYSA-N 0.000 claims description 17
- ODINCKMPIJJUCX-UHFFFAOYSA-N Calcium oxide Chemical compound [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 claims description 16
- 239000000292 calcium oxide Substances 0.000 claims description 16
- 235000012255 calcium oxide Nutrition 0.000 claims description 16
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 15
- 239000000395 magnesium oxide Substances 0.000 claims description 15
- 239000000377 silicon dioxide Substances 0.000 claims description 15
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims description 15
- 239000002245 particle Substances 0.000 claims description 11
- 239000011230 binding agent Substances 0.000 claims description 6
- 238000005266 casting Methods 0.000 claims description 4
- 238000005245 sintering Methods 0.000 claims description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 3
- 238000005304 joining Methods 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 229910052750 molybdenum Inorganic materials 0.000 claims description 3
- 239000011733 molybdenum Substances 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims description 3
- 229910052758 niobium Inorganic materials 0.000 claims description 3
- 239000010955 niobium Substances 0.000 claims description 3
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 3
- 229910052702 rhenium Inorganic materials 0.000 claims description 3
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 claims description 3
- 229910052715 tantalum Inorganic materials 0.000 claims description 3
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 3
- 229910052721 tungsten Inorganic materials 0.000 claims description 3
- 239000010937 tungsten Substances 0.000 claims description 3
- 229910052845 zircon Inorganic materials 0.000 claims description 2
- 239000000853 adhesive Substances 0.000 description 6
- 230000001070 adhesive effect Effects 0.000 description 6
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 4
- 239000003870 refractory metal Substances 0.000 description 4
- 239000002002 slurry Substances 0.000 description 4
- 238000007711 solidification Methods 0.000 description 4
- 230000008023 solidification Effects 0.000 description 4
- 239000008119 colloidal silica Substances 0.000 description 3
- 239000006057 Non-nutritive feed additive Substances 0.000 description 2
- 230000002902 bimodal effect Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 239000004115 Sodium Silicate Substances 0.000 description 1
- BOTDANWDWHJENH-UHFFFAOYSA-N Tetraethyl orthosilicate Chemical compound CCO[Si](OCC)(OCC)OCC BOTDANWDWHJENH-UHFFFAOYSA-N 0.000 description 1
- 230000037237 body shape Effects 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000004814 ceramic processing Methods 0.000 description 1
- 239000011362 coarse particle Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000003966 growth inhibitor Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 1
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 1
- 229910052911 sodium silicate Inorganic materials 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
- 239000012815 thermoplastic material Substances 0.000 description 1
- 239000004034 viscosity adjusting agent Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C1/00—Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
-
- 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
Definitions
- This disclosure relates to investment casting and, more particularly, to investment casting cores.
- Investment casting is known and used to cast metallic components with relatively complex geometries.
- gas turbine engine components such as airfoils that have internal passages
- a core is provided which represents a positive projection of negative features that are to be formed in the casting process.
- a wax material is then provided around the core in the shape of the component to be cast.
- a shell is then formed around the wax and the wax is removed to form a cavity between the core and the surrounding shell into which molten metal is poured to form the shape of the component. After solidification of the metal, the core is removed using known techniques to provide the cast component.
- US 2005/070651 discloses an investment casting core comprising a mullite-containing core body.
- An investment casting core includes a mullite-containing core body and characterised by the investment casting core comprising a metallic core body joined to the mullite-containing core body, wherein the coefficient of thermal expansion of the mullite-containing core body is within 2% of the coefficient of thermal expansion of the metallic core body.
- the mullite-containing core body has, by weight, 40% or greater of mullite.
- the mullite-containing core body has, by weight, 40-90% of mullite.
- the mullite-containing core body has a material selected from the group consisting of alumina, silica, magnesia, yttria, calcia, zirconium silicate and combinations thereof.
- the mullite-containing core body has, by weight, 40-90% of mullite and 60-5% of silica.
- the mullite-containing core body has a material selected from the group consisting of magnesia, yttria, calcia and combinations thereof.
- the mullite-containing core body has zirconium silicate.
- the metallic core body is selected from the group consisting of molybdenum, tungsten, tantalum, rhenium, niobium and combinations thereof.
- the mullite-containing core body has, by weight, 80-90% mullite, 15-5% silica, 2.5- 10% alumina, 0-2.5% zircon, 0-5% of one or more of: calcia, magnesia and yttria.
- the mullite-containing core body has a multi-modal or bi-modal grain size distribution.
- a method of making an investment casting core includes: providing a mullite-containing powder; forming the mullite-containing powder into a green body; and sintering the green body to form a mullite-containing core body; and characterised by joining the mullite-containing core body to a metallic core body, wherein the coefficient of thermal expansion of the mullite-containing core body has a coefficient of thermal expansion within 2% of the coefficient of thermal expansion of the metallic core body.
- a further non-limiting embodiment of any of the foregoing examples includes providing the mullite-containing powder in a blend with a binder, and the forming includes molding the blend into the green body.
- the mullite-containing powder has at least a bi-modal particle size distribution of mullite particles.
- the mullite-containing powder has a material selected from alumina, silica, magnesia, yttria, calcia, zirconium silicate and combinations thereof in a powder with at least a bi-modal particle size distribution.
- a further non-limiting embodiment of any of the foregoing examples includes selecting a composition of the mullite-containing powder to obtain a coefficient of thermal expansion in the mullite-containing core body that matches a coefficient of thermal expansion of the metallic core body.
- a method of investment casting according to an exemplary aspect of the present disclosure includes: casting a metallic component at least partially around an investment casting core that has a mullite-containing core body; and characterised by the investment casting core further comprising a metallic core body joined to the mullite-containing core body, wherein the coefficient of thermal expansion of the mullite-containing core body is within 2% of the coefficient of thermal expansion of the metallic core.
- a further non-limiting embodiment of any of the foregoing examples includes the mullite-containing core body that has a material selected from the group consisting of alumina, silica, magnesia, yttria, calcia, zirconium silicate and combinations thereof.
- Figure 1 schematically illustrates selected portions of an example investment casting core 20 (hereafter "core 20").
- core 20 is shown schematically for purposes of description and the actual geometry will depend on the design features of the cast component.
- the cast component can be an airfoil for a gas turbine engine, however, the examples herein are also applicable to other engine components or non-engine components.
- the core 20 includes a mullite-containing core body 22.
- a "body” is a main or central foundational part, distinct from subordinate features, such as coatings or the like that are supported by the underlying body and depend primarily on the shape of the underlying body for their own shape.
- the mechanical characteristics of a core influence the quality of the investment casting process and component.
- solidification of the metallic material exerts a force on the core. If the Young's Modulus is to high, the core will resist the solidification forces and may undesirably cause high internal stresses in the cast component or "hot tearing" of the component.
- the mullite-containing core body 22 has a composition that provides "crushability" of the core 20 during investment casting. That is, the core 20 is tailored to "crush" under the solidification forces to reduce internal stresses and hot tearing.
- the mullite-containing core body 22 has a composition that has, by weight, 40% or greater of mullite. In a further example, the mullite-containing core body 22 has, by weight, 40-90% of mullite.
- additional materials are used with the mullite to adjust a coefficient of thermal expansion ("CTE") of the mullite-containing core body 22 and/or as processing aids.
- the mullite-containing core body 22 has one or more materials selected from: alumina, silica, magnesia, yttria, calcia, zirconium silicate or combinations thereof.
- the alumina, silica, magnesia, yttria and calcia may be added to adjust the CTE.
- the yttria, calcia and zirconium silicate may be added as processing aids (yttria and calcia) to facilitate sintering when making the mullite-containing core body 22 or as grain growth inhibitors (zirconium silicate).
- the mullite-containing core body 22 has, by weight, 40-90% of mullite and 60 - 5 % silica.
- the mullite-containing core body can also include up to 25% by weight of alumina, up to 5% by weight of magnesia, up to 5% by weight of yttria, up to 5% by weight of calcia and up to 10% by weight of zirconium silicate.
- the mullite-containing core body 22 can have a grain size that has a grain size distribution that is equal to or approximately equal to a powder size distribution, such as a bi-modal or multi-modal particle size distribution as discussed below. This, the grain size distribution can be multi-modal or bi-modal.
- the core 20 has a shape that corresponds to negative features that are to be formed in the investment cast component, such as gas turbine engine airfoils.
- the illustrated core 20 has elongated limbs 24 and branches 26 that extend off of the limbs 24. It is to be understood, however, that the core 20 may alternatively have different geometries than shown, depending upon the features that are to be formed in the investment cast component.
- the core 20 can be a multi-material core that, in addition to the mullite-containing core body 22, also has a metallic core body 28 that is joined with the mullite-containing core body 22.
- the metallic core body 28 is a refractory metal core.
- the refractory metal is selected from molybdenum, tungsten, tantalum, rhenium, niobium and combinations thereof.
- the metallic core body 28 can be joined to the mullite-containing core body 22 using an adhesive material.
- the adhesive material is applied the joining surface of the mullite-containing core body 22, the metallic core body 28 or both in the form of slurry, such as a colloidal silica-based slurry.
- the colloidal silica based adhesive slurry will be comprised of materials of similar composition to the main core body: mullite, alumina, zirconia silicate to act as filler material as well as to ensure compatibility with the main body core.
- the colloidal silica serves as a binder adhesive to secure the mullite-containing core body 22 and the metallic core body 28 together.
- other types of adhesives and ceramic materials could be used including adhesive systems based upon, ethyl silicate, sodium silicate, collidial alumina, colloidal yttria, colloidal zirconia.
- the composition of the mullite-containing core body 22 can be tailored with regard to CTE to closely match the CTE of the metallic core body 28.
- mullite provides a relatively close match in CTE.
- the mullite composition can be modified with the alumina, silica, magnesia or combinations thereof to modify the CTE of the mullite-containing core body 22 in accordance with the CTE of the selected refractory metal of the metallic core body 28.
- the CTE of the mullite-containing core body 22 is within about 2% of the CTE of the metallic core body 28.
- Figure 2 illustrates an example method 30 of making the investment casting core 20.
- the method 30 includes steps 32, 34 and 36.
- Step 32 includes providing a mullite-containing powder
- step 34 includes forming the mullite-containing powder into a green body
- step 36 includes sintering the green body to form the mullite-containing core body 22.
- step 32 includes providing the mullite-containing powder in a blend with a binder and then in step 34 molding the blend to form the green body.
- the binder can be a thermoplastic material, a wax material or a wax material with viscosity modifiers, such as stearate.
- the blend includes approximately 10-20% by weight of the binder material and a remainder of the mullite-containing powder.
- the composition of the mullite-containing powder can be tailored according to the desired composition of the mullite-containing core body 22. That is, the mullite-containing powder can include mullite powder and powders of any or all of the other above-described materials of alumina, silica, magnesia, yttria, calcia and zirconium silicate.
- the mullite-containing powder has at least a bi-modal particle size distribution.
- the bi-modal distribution provides a blend of coarse and fine particles that facilitate forming the green body with relatively large sections and also with relatively thin sections. That is, the multi-modal particle size distribution facilitates filling a mold to form a relatively complex green body shape.
- Powders of the added materials in addition to the mullite can also include a multi-modal particle size distribution for similar purposes. Given this description, one of ordinary skill in the art will be able to determine a bimodal or multi-modal distribution to meet their particular needs. As examples, multi-modal distributions are described in " Fitting Bimodal Particle Size Distribution Curves" J. M. Dallavalle et. al., Ind. Eng. Chem., 1951, 43 (6), pp 1377-1380 , and Reed, James, Introduction to the principles of ceramic processing, New York, A Wiley-Interscience publication, 1995 .
- a method 40 of investment casting can be implemented after forming the mullite-containing core body 22.
- the method 40 includes casting a metallic component at least partially around the investment casting core 20 that has the mullite-containing core body 22.
- the details of investment casting, aside from the core 20 and mullite-containing core body 22, are generally known and therefore will not be described in further detail herein.
- the methods 30 and 40 need not be conducted together. That is, the methods 30 and 40 can be mutually independent.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Mold Materials And Core Materials (AREA)
Claims (14)
- Noyau de moulage de précision à modèle perdu (20) comprenant :
un corps de noyau contenant de la mullite (22) ; et caractérisé par le noyau de moulage de précision à modèle perdu comprenant un corps de noyau métallique (28) joint au corps de noyau contenant de la mullite, dans lequel le coefficient d'expansion thermique du corps de noyau contenant de la mullite (22) ne dépasse pas 2 % du coefficient d'expansion thermique du corps de noyau métallique. - Noyau de moulage de précision à modèle perdu selon la revendication 1, dans lequel le corps de noyau contenant de la mullite présente en poids 40 % ou plus de mullite, de préférence dans lequel le corps de noyau contenant de la mullite présente, en poids, 40 à 90 % de mullite.
- Noyau de moulage de précision à modèle perdu selon la revendication 1 ou 2, dans lequel le corps de noyau contenant de la mullite présente un matériau sélectionné dans le groupe composé d'alumine, de silice, de magnésie, d'yttrium, de calcium, de silicate de zirconium et de combinaisons de ceux-ci .
- Noyau de moulage de précision à modèle perdu selon une quelconque revendication précédente, dans lequel le corps de noyau contenant de la mullite présente en poids 40 à 90 % de mullite et 60 à 5 % de silice.
- Noyau de moulage de précision à modèle perdu selon une quelconque revendication précédente, dans lequel le corps de noyau contenant de la mullite présente un matériau sélectionné dans le groupe composé de magnésie, d'yttrium, de calcium et de combinaisons de ceux-ci, ou dans lequel le corps de noyau contenant de la mullite présente du silicate de zirconium.
- Noyau de moulage de précision à modèle perdu selon une quelconque revendication précédente, dans lequel le corps de noyau métallique est sélectionné dans le groupe composé de molybdène, de tungstène, de tantale, de rhénium, de niobium et de combinaisons de ceux-ci.
- Noyau de moulage de précision à modèle perdu selon une quelconque revendication précédente, dans lequel le corps de noyau contenant de la mullite présente en poids 80 à 90 % de mullite, 15 à 5 % de silice, 2,5 à 10 % d'alumine, 0 à 2,5 % de zircon, 0 à 5 % d'un ou de plusieurs de : calcium, magnésie et yttrium.
- Noyau de moulage de précision à modèle perdu selon une quelconque revendication précédente, dans lequel le corps de noyau contenant de la mullite présente une distribution granulométrique multimodale ou bimodale.
- Procédé de fabrication d'un noyau de moulage de précision à modèle perdu (20), le procédé comprenant :la fourniture d'une poudre contenant de la mullite ;la formation de la poudre contenant de la mullite dans un corps vert ; etle frittage du corps vert pour former un corps de noyau contenant de la mullite (22) ;et caractérisé par la jonction du corps de noyau contenant de la mullite à un corps de noyau métallique (28), dans lequel le coefficient d'expansion thermique du corps de noyau contenant de la mullite (22) présente un coefficient d'expansion thermique qui ne dépasse pas 2 % du coefficient d'expansion thermique du corps de noyau métallique.
- Procédé selon la revendication 9, incluant la fourniture de la poudre contenant de la mullite dans un mélange avec un liant, et la formation inclut le moulage du mélange dans le corps vert, et/ou dans lequel la poudre contenant de la mullite présente au moins une distribution granulométrique bimodale de particules de mullite.
- Procédé selon la revendication 9 ou 10, dans lequel la poudre contenant de la mullite présente un matériau sélectionné parmi l'alumine, la silice, la magnésie, l'yttrium, le calcium, le silicate de zirconium et des combinaisons de ceux-ci dans une poudre avec au moins une distribution granulométrique bimodale.
- Procédé selon l'une quelconque des revendications 9 à 11, comprenant en outre la sélection d'une composition de la poudre contenant de la mullite pour obtenir un coefficient d'expansion thermique dans le corps de noyau contenant de la mullite qui correspond à un coefficient d'expansion thermique du corps de noyau métallique.
- Procédé de moulage de précision à modèle perdu, le procédé comprenant :
le moulage d'un composant métallique au moins partiellement autour d'un noyau de moulage de précision à modèle perdu (20) qui présente un corps de noyau contenant de la mullite (22) ; et caractérisé par le noyau de moulage de précision à modèle perdu comprenant en outre un corps de noyau métallique (28) joint au corps de noyau contenant de la mullite, dans lequel le coefficient d'expansion thermique du corps de noyau contenant de mullite (22) ne dépasse pas 2 % du coefficient d'expansion thermique du noyau métallique. - Procédé selon la revendication 13, dans lequel le corps de noyau contenant de la mullite présente un matériau sélectionné dans le groupe composé d'alumine, de silice, de magnésie, d'yttrium, de calcium, de silicate de zirconium et de combinaisons de ceux-ci.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/729,077 US20140182809A1 (en) | 2012-12-28 | 2012-12-28 | Mullite-containing investment casting core |
PCT/US2013/074555 WO2014105436A1 (fr) | 2012-12-28 | 2013-12-12 | Noyau de moulage de précision à modèle perdu contenant de la mullite |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2938448A1 EP2938448A1 (fr) | 2015-11-04 |
EP2938448A4 EP2938448A4 (fr) | 2016-08-31 |
EP2938448B1 true EP2938448B1 (fr) | 2018-07-04 |
Family
ID=51015809
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13868294.3A Active EP2938448B1 (fr) | 2012-12-28 | 2013-12-12 | Noyau de moulage de précision à modèle perdu contenant de la mullite |
Country Status (3)
Country | Link |
---|---|
US (1) | US20140182809A1 (fr) |
EP (1) | EP2938448B1 (fr) |
WO (1) | WO2014105436A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9950358B2 (en) | 2015-11-19 | 2018-04-24 | General Electric Company | Compositions for cores used in investment casting |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3833385A (en) * | 1971-12-28 | 1974-09-03 | Corning Glass Works | Preform core bodies |
US4164424A (en) * | 1977-10-06 | 1979-08-14 | General Electric Company | Alumina core having a high degree of porosity and crushability characteristics |
US4837187A (en) * | 1987-06-04 | 1989-06-06 | Howmet Corporation | Alumina-based core containing yttria |
US4767479A (en) * | 1987-09-21 | 1988-08-30 | United Technologies Corporation | Method for bonding ceramic casting cores |
JP2663392B2 (ja) * | 1992-06-19 | 1997-10-15 | 工業技術院長 | チタン及びその合金の鋳造用中子 |
US5612393A (en) * | 1993-12-24 | 1997-03-18 | Nissan Motor Co., Ltd. | Casting core composition |
US6637500B2 (en) * | 2001-10-24 | 2003-10-28 | United Technologies Corporation | Cores for use in precision investment casting |
US7287573B2 (en) * | 2003-09-30 | 2007-10-30 | General Electric Company | Silicone binders for investment casting |
US7207374B2 (en) * | 2004-10-26 | 2007-04-24 | United Technologies Corporation | Non-oxidizable coating |
FR2889088B1 (fr) * | 2005-07-29 | 2008-08-22 | Snecma | Noyau pour aubes de turbomachine |
US7802613B2 (en) * | 2006-01-30 | 2010-09-28 | United Technologies Corporation | Metallic coated cores to facilitate thin wall casting |
US7905273B2 (en) * | 2007-09-05 | 2011-03-15 | Pcc Airfoils, Inc. | Method of forming a cast metal article |
US8100165B2 (en) * | 2008-11-17 | 2012-01-24 | United Technologies Corporation | Investment casting cores and methods |
US8286689B1 (en) * | 2011-08-30 | 2012-10-16 | United Technologies Corporation | Porous ceramic body and method therfor |
-
2012
- 2012-12-28 US US13/729,077 patent/US20140182809A1/en not_active Abandoned
-
2013
- 2013-12-12 EP EP13868294.3A patent/EP2938448B1/fr active Active
- 2013-12-12 WO PCT/US2013/074555 patent/WO2014105436A1/fr active Application Filing
Non-Patent Citations (1)
Title |
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Also Published As
Publication number | Publication date |
---|---|
EP2938448A1 (fr) | 2015-11-04 |
EP2938448A4 (fr) | 2016-08-31 |
WO2014105436A1 (fr) | 2014-07-03 |
US20140182809A1 (en) | 2014-07-03 |
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