US20120043046A1 - Process for casting columnar grain airfoil with preferential primary orientation - Google Patents
Process for casting columnar grain airfoil with preferential primary orientation Download PDFInfo
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- US20120043046A1 US20120043046A1 US13/289,115 US201113289115A US2012043046A1 US 20120043046 A1 US20120043046 A1 US 20120043046A1 US 201113289115 A US201113289115 A US 201113289115A US 2012043046 A1 US2012043046 A1 US 2012043046A1
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- 238000005266 casting Methods 0.000 title abstract description 17
- 238000000034 method Methods 0.000 title abstract description 16
- 239000012768 molten material Substances 0.000 claims abstract description 23
- 238000007711 solidification Methods 0.000 claims abstract description 12
- 230000008023 solidification Effects 0.000 claims abstract description 12
- 239000000463 material Substances 0.000 claims description 10
- 238000004891 communication Methods 0.000 claims description 4
- 239000007769 metal material Substances 0.000 claims description 4
- 239000002131 composite material Substances 0.000 claims description 3
- 238000000465 moulding Methods 0.000 abstract description 5
- 239000000919 ceramic Substances 0.000 description 6
- 239000013078 crystal Substances 0.000 description 3
- 239000000155 melt Substances 0.000 description 3
- 230000006911 nucleation Effects 0.000 description 3
- 238000010899 nucleation Methods 0.000 description 3
- 239000000956 alloy Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000007858 starting material Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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Classifications
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- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B11/00—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B11/00—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
- C30B11/14—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method characterised by the seed, e.g. its crystallographic orientation
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B29/00—Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
- C30B29/10—Inorganic compounds or compositions
- C30B29/52—Alloys
Definitions
- This disclosure generally relates a preferential grain casting process. More particularly, this disclosure describes a method and device for preferential grain casting utilizing a seed to control orientation of a columnar grain casting.
- Processes for orientating a grain structure in a cast article are known to provide either a columnar structure or a single crystal structure.
- a ceramic casting mold that is heated to a temperature above the melting point of the alloy is filled with molten material within a furnace.
- This mold is subsequently withdrawn from a hot chamber to a cold chamber of the casting furnace in a controlled manner to control solidification and obtain directional alignment of the crystals.
- a starter block provides a starting point for the solidification of a molten material.
- the starter block facilitates the nucleation and growth of several columns that will grow in the direction opposite of heat extraction as opposed to the formation of a random grain structure without directionality.
- a columnar grain structure is an improvement over random grain structures, the column grain structure is only orientated in one direction identified as the primary orientation. Adjacent columns would possess the same primary orientation but possess different secondary orientations denoting a crystal structure that is rotated about the primary growth axis.
- a process that promotes the nucleation and growth of many directional columns is preferred to optimize mechanical properties within a cast component. Because of component and mold geometries or furnace design limitations, obtaining many directional columns that progress from the bottom to the top of the casting is not always easily achievable. In many instances, only a few columns will nucleate and grow compromising part integrity.
- a disclosed example molding process utilizes a seed with a predetermined columnar grain structure for defining a desired grain structure in a completed casting.
- the example process utilizes a mold that defines the geometric features of a molded part, such as for example an airfoil.
- the seed is received or embedded within a seed cavity of the ceramic mold having a plurality of preferentially orientated columns.
- the molten material is poured into the ceramic mold, melts a small portion of the prefabricated metal seed, and solidifies adopting the orientation of the columns defined within the seed during solidification to form a completed molded article having a desired columnar grain structure.
- the example method and device provides for the preferential orientation of columnar grain structures within a completed molded article.
- the example columnar grain structures are defined within a seed that is received within each mold cavity prior to receiving molten metal material.
- the preferential defined columnar grain structure provides for tailoring of grain structure to obtain desired mechanical characteristics and properties in the completed molded article.
- FIG. 1 is a schematic view of an example casting process.
- FIG. 2 is a sectional view of an example columnar grain structure.
- FIG. 3 is schematic view of an orientation of an example columnar grain.
- FIG. 4 is a schematic view of a prior art equiax grain structure.
- FIG. 5 is a schematic view of an example casting.
- FIG. 6 is perspective view of an example airfoil including a columnar grain structure.
- an example casting process utilizes a casting furnace assembly 10 having an induction coil 12 for heating a ceramic mold to a temperature in excess of the melting point of the alloy to be cast.
- the example casting assembly further includes a hot zone 22 and a susceptor 16 which translates heat from the induction coil to the ceramic casting mold 20 .
- a lid 14 is placed on top of the hot zone to prevent the escape of heat.
- a ceramic mold 20 is supported on a cold chillplate 18 .
- the cold chillplate 18 is movable out of the hot zone 22 in a direction indicated by arrow 32 .
- a baffle 21 separates the hot zone which resides above the baffle 21 from the colder portion of the furnace into which the cast mold is withdrawn. It is within the contemplation of this disclosure that other casting furnace assembly 10 configurations could be utilized.
- the mold 20 defines the geometric features of a molded part, such as for example an airfoil.
- a seed 28 is received within a seed cavity 34 of the mold 20 .
- the seed 28 includes a plurality of preferentially orientated columns 30 .
- the molten material adopts the orientation of the columns 30 defined within the seed 28 during solidification to form a completed molded article having a desired columnar grain structure.
- the molding method proceeds by forming the mold 20 to define the desired geometric shape.
- the mold 20 is defined with the seed cavity 34 for receiving the seed 28 .
- the seed 28 is a pre-molded block having the desired columnar grain structure.
- the seed 28 comprises similar material content and mixture as is utilized to cast the article.
- the material comprising the seed 28 can be identical to that of the molten material for the cast article.
- the seed 28 could be fabricated from a metallic material or composite material similar, but different than the material utilized for the cast article.
- any material or composite utilized for the seed 28 is selected to provide the desired results and compatibility in view of the material utilized for the cast article.
- the solid seed 28 is inserted into the seed cavity 34 prior to the introduction of molten metal and prior to insertion of the mold 20 within the furnace assembly 10 .
- the mold 20 With the seed 28 disposed within the mold 20 , the mold 20 is placed within the hot zone 22 . Molten material is then poured into the mold 20 . The molten material 20 remains in a molten state within the hot zone 22 . The seed 28 comes into contact with the molten material and partially melts at the interface with the molten material.
- the mold 20 is removed from the hot zone 22 into a cooler environment that provides for solidification of the molten material 24 .
- the mold 20 is supported on the cold plate 18 .
- the example cold plate 18 is supported for movement out of the hot zone 22 in a controlled manner to control the solidification of the molten material.
- a solidification front 26 forms as the mold 20 is lowered from the hot zone 22 .
- the solidified material adopts the columnar orientations and structure of the seed 28 .
- the columnar orientations are defined by those created and defined in the seed 28 .
- the orientation of the grains within the completed molded article is thereby defined by the columnar structure fabricated into the seed 28 .
- a section 36 is shown that illustrates the interface between the seed 28 and the molded article.
- the seed 28 is shown with defined columns 30 .
- a portion of the seed 28 melts back and forms a mixed zone 38 .
- the added molten material 24 ( FIG. 1 ) mixes with a portion of the seed 28 .
- the material from the original seed 28 freezes in a mixture with the molten material. It is in this mixed zone 38 that the columnar grain structure and orientation is adopted by the solidifying molten material.
- the molded article 40 includes the columnar structure 30 that was defined in the original seed 28 .
- This columnar structure 30 includes fine dendritic structures to start the growth of columnar structures within the molten material.
- the columnar structures are numbered and orientated to provide the desired strength, durability or other mechanical properties desired in the completed molded article. Additional mechanical properties that can be defined and provided by the example process includes durability, fatigue strength, dampening and also the preferential orientation of stresses on the completed part.
- each of the grained structures 44 are vertically orientated along a vertical axis 46 . Further, the grained structures 44 are commonly orientated in a rotational direction indicated by arrow 48 about the vertical axis 46 . The orientations vertically along the axis 46 and rotationally is provided by the orientations defined in the columnar grained seed 28 . Each block 44 defines the orientation of one column 30 .
- a prior art equiax grain structure 50 is schematically illustrated and includes a grain structure where the grains possess different primary and secondary orientations. Each adjacent column represented by the block is facing a different rotational direction as indicated by arrows 52 .
- an example mold 54 for the fabrication of an airfoil such as a turbine vane includes several cavities 56 .
- Each cavity 56 defines the geometry and shape of a completed turbine blade. All the cavities 56 are in communication such that molten material flows to each cavity from a common inlet.
- Each of the cavities 56 includes a seed cavity portion 58 .
- Once of the example seed cavities 58 are partially sectioned to show an example seed 60 received therein.
- the seed 60 is cast, solidified and heat-treated prior to insertion into the seed cavity 58 .
- the casting process of the seed 60 provides the desired columnar grain orientations that are to be adopted by the completed turbine blade.
- the seed 60 includes a size that corresponds with each individual cavity 56 .
- the seed 60 is as wide or wider than the corresponding cavity 56 to provide for columnar growth in a vertical manner without disruptions. Further, the height of the seed 60 is such that upon encountering the molten material, at least some portion of the seed 60 will remain in a solid form. The height of the seed 60 is therefore provided such that sufficient original solidified material with the defined grain structure survives the molding and solidification process.
- an example turbine blade assembly 62 includes a columnar grain structure with columns 64 throughout.
- the columns 64 within the blade assembly 62 are uniform and generated by columns 66 defined by the seed 60 .
- the seed 60 is removed by a machining process as is known.
- the example method and device provides for the preferential orientation of columnar grain structures within a completed cast article.
- the example columnar grain structures are defined within a seed that is received within each mold cavity prior to receiving molten metal material.
- the preferential defined columnar grain structure provides for tailoring of grain structure to obtain desired mechanical characteristics and properties in the completed molded article.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
A molding process utilizes a seed with a columnar grain structure for defining a desired grain structure in a completed casting. The seed is received within a seed cavity of a mold. The molten material adopts the orientation of the columns defined within the seed during solidification to form a completed molded article having a desired columnar grain structure.
Description
- This application is a divisional of U.S. application Ser. No. 12/244,203 filed on Oct. 2, 2008.
- This disclosure generally relates a preferential grain casting process. More particularly, this disclosure describes a method and device for preferential grain casting utilizing a seed to control orientation of a columnar grain casting.
- Processes for orientating a grain structure in a cast article are known to provide either a columnar structure or a single crystal structure. In such processes, a ceramic casting mold that is heated to a temperature above the melting point of the alloy is filled with molten material within a furnace. This mold is subsequently withdrawn from a hot chamber to a cold chamber of the casting furnace in a controlled manner to control solidification and obtain directional alignment of the crystals. A starter block provides a starting point for the solidification of a molten material. For a columnar grain structure, the starter block facilitates the nucleation and growth of several columns that will grow in the direction opposite of heat extraction as opposed to the formation of a random grain structure without directionality. Although a columnar grain structure is an improvement over random grain structures, the column grain structure is only orientated in one direction identified as the primary orientation. Adjacent columns would possess the same primary orientation but possess different secondary orientations denoting a crystal structure that is rotated about the primary growth axis.
- Accordingly, it is desirable to design and develop a method and device for providing a preferential columnar grain structure for a cast article. A process that promotes the nucleation and growth of many directional columns is preferred to optimize mechanical properties within a cast component. Because of component and mold geometries or furnace design limitations, obtaining many directional columns that progress from the bottom to the top of the casting is not always easily achievable. In many instances, only a few columns will nucleate and grow compromising part integrity.
- It is desirable to develop a method that promotes the nucleation and growth of as many directional columns as possible to optimize part integrity.
- A disclosed example molding process utilizes a seed with a predetermined columnar grain structure for defining a desired grain structure in a completed casting.
- The example process utilizes a mold that defines the geometric features of a molded part, such as for example an airfoil. The seed is received or embedded within a seed cavity of the ceramic mold having a plurality of preferentially orientated columns. The molten material is poured into the ceramic mold, melts a small portion of the prefabricated metal seed, and solidifies adopting the orientation of the columns defined within the seed during solidification to form a completed molded article having a desired columnar grain structure.
- The example method and device provides for the preferential orientation of columnar grain structures within a completed molded article. The example columnar grain structures are defined within a seed that is received within each mold cavity prior to receiving molten metal material. The preferential defined columnar grain structure provides for tailoring of grain structure to obtain desired mechanical characteristics and properties in the completed molded article.
- These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
-
FIG. 1 is a schematic view of an example casting process. -
FIG. 2 is a sectional view of an example columnar grain structure. -
FIG. 3 is schematic view of an orientation of an example columnar grain. -
FIG. 4 is a schematic view of a prior art equiax grain structure. -
FIG. 5 is a schematic view of an example casting. -
FIG. 6 is perspective view of an example airfoil including a columnar grain structure. - Referring to
FIG. 1 , an example casting process utilizes acasting furnace assembly 10 having aninduction coil 12 for heating a ceramic mold to a temperature in excess of the melting point of the alloy to be cast. The example casting assembly further includes ahot zone 22 and asusceptor 16 which translates heat from the induction coil to theceramic casting mold 20. Alid 14 is placed on top of the hot zone to prevent the escape of heat. Aceramic mold 20 is supported on acold chillplate 18. Thecold chillplate 18 is movable out of thehot zone 22 in a direction indicated byarrow 32. Abaffle 21 separates the hot zone which resides above thebaffle 21 from the colder portion of the furnace into which the cast mold is withdrawn. It is within the contemplation of this disclosure that othercasting furnace assembly 10 configurations could be utilized. - The
mold 20 defines the geometric features of a molded part, such as for example an airfoil. Aseed 28 is received within aseed cavity 34 of themold 20. Theseed 28 includes a plurality of preferentiallyorientated columns 30. The molten material adopts the orientation of thecolumns 30 defined within theseed 28 during solidification to form a completed molded article having a desired columnar grain structure. - The molding method proceeds by forming the
mold 20 to define the desired geometric shape. Themold 20 is defined with theseed cavity 34 for receiving theseed 28. Theseed 28 is a pre-molded block having the desired columnar grain structure. Theseed 28 comprises similar material content and mixture as is utilized to cast the article. The material comprising theseed 28 can be identical to that of the molten material for the cast article. Further, theseed 28 could be fabricated from a metallic material or composite material similar, but different than the material utilized for the cast article. As appreciated, any material or composite utilized for theseed 28 is selected to provide the desired results and compatibility in view of the material utilized for the cast article. - The
solid seed 28 is inserted into theseed cavity 34 prior to the introduction of molten metal and prior to insertion of themold 20 within thefurnace assembly 10. With theseed 28 disposed within themold 20, themold 20 is placed within thehot zone 22. Molten material is then poured into themold 20. Themolten material 20 remains in a molten state within thehot zone 22. Theseed 28 comes into contact with the molten material and partially melts at the interface with the molten material. - Once the
mold 20 is filled, it is removed from thehot zone 22 into a cooler environment that provides for solidification of themolten material 24. Themold 20 is supported on thecold plate 18. The examplecold plate 18 is supported for movement out of thehot zone 22 in a controlled manner to control the solidification of the molten material. Asolidification front 26 forms as themold 20 is lowered from thehot zone 22. The solidified material adopts the columnar orientations and structure of theseed 28. The columnar orientations are defined by those created and defined in theseed 28. The orientation of the grains within the completed molded article is thereby defined by the columnar structure fabricated into theseed 28. - Referring to
FIG. 2 with continued reference toFIG. 1 , asection 36 is shown that illustrates the interface between theseed 28 and the molded article. Theseed 28 is shown with definedcolumns 30. Upon exposure to the molten material, a portion of theseed 28 melts back and forms amixed zone 38. In themixed zone 38 the added molten material 24 (FIG. 1 ) mixes with a portion of theseed 28. Upon solidification, the material from theoriginal seed 28 freezes in a mixture with the molten material. It is in thismixed zone 38 that the columnar grain structure and orientation is adopted by the solidifying molten material. - The molded
article 40 includes thecolumnar structure 30 that was defined in theoriginal seed 28. Thiscolumnar structure 30 includes fine dendritic structures to start the growth of columnar structures within the molten material. The columnar structures are numbered and orientated to provide the desired strength, durability or other mechanical properties desired in the completed molded article. Additional mechanical properties that can be defined and provided by the example process includes durability, fatigue strength, dampening and also the preferential orientation of stresses on the completed part. - Referring to
FIG. 3 ,several columns 30 of grained structures is schematically depicted as blocks 44. Each of thegrained structures 44 are vertically orientated along avertical axis 46. Further, thegrained structures 44 are commonly orientated in a rotational direction indicated byarrow 48 about thevertical axis 46. The orientations vertically along theaxis 46 and rotationally is provided by the orientations defined in the columnargrained seed 28. Eachblock 44 defines the orientation of onecolumn 30. - Referring to
FIG. 4 , a prior artequiax grain structure 50 is schematically illustrated and includes a grain structure where the grains possess different primary and secondary orientations. Each adjacent column represented by the block is facing a different rotational direction as indicated byarrows 52. - Referring to
FIG. 5 , anexample mold 54 for the fabrication of an airfoil such as a turbine vane includesseveral cavities 56. Eachcavity 56 defines the geometry and shape of a completed turbine blade. All thecavities 56 are in communication such that molten material flows to each cavity from a common inlet. Each of thecavities 56 includes aseed cavity portion 58. Once of theexample seed cavities 58 are partially sectioned to show anexample seed 60 received therein. Theseed 60 is cast, solidified and heat-treated prior to insertion into theseed cavity 58. The casting process of theseed 60 provides the desired columnar grain orientations that are to be adopted by the completed turbine blade. - The
seed 60 includes a size that corresponds with eachindividual cavity 56. Theseed 60 is as wide or wider than the correspondingcavity 56 to provide for columnar growth in a vertical manner without disruptions. Further, the height of theseed 60 is such that upon encountering the molten material, at least some portion of theseed 60 will remain in a solid form. The height of theseed 60 is therefore provided such that sufficient original solidified material with the defined grain structure survives the molding and solidification process. - Referring to
FIG. 6 , an exampleturbine blade assembly 62 includes a columnar grain structure withcolumns 64 throughout. Thecolumns 64 within theblade assembly 62 are uniform and generated bycolumns 66 defined by theseed 60. After the molding process is complete and theblade assembly 62 has solidified, theseed 60 is removed by a machining process as is known. - The example method and device provides for the preferential orientation of columnar grain structures within a completed cast article. The example columnar grain structures are defined within a seed that is received within each mold cavity prior to receiving molten metal material. The preferential defined columnar grain structure provides for tailoring of grain structure to obtain desired mechanical characteristics and properties in the completed molded article.
- Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
Claims (10)
1. A mold assembly for fabricating a cast article, the mold assembly comprising:
a mold cavity including a shape defining a desired geometry of a cast article and a bottom opening including a width;
a seed cavity in communication with the mold cavity for receiving a seed, the seed cavity including width substantially equal to the bottom opening;
a seed receivable within the seed cavity, the seed including a defined columnar grain orientation for adoption within the molded article.
2. The assembly as recited in claim 1 , wherein the seed comprises a material identical to molten material utilized for fabricating the molded article.
3. The assembly as recited in claim 1 , wherein the seed comprises one of a metallic material and a composite material different than the material utilized for fabricating the molded article.
4. The assembly as recited in claim 1 , wherein the seed comprises a vertical grain orientation parallel with a vertical axis through the mold cavity and a fixed rotational grain orientation along the column.
5. The assembly as recited in claim 1 , including a cooled plate for supporting the mold cavity within a heated chamber, wherein the cooled plate is movable in a controlled manner to remove the mold cavity to control solidification of molten material.
6. A mold assembly for fabricating a cast article, the mold assembly comprising:
a mold cavity including a shape defining a desired geometry of a cast article;
a seed cavity in communication with the mold cavity for receiving a seed;
a seed receivable within the seed cavity, the seed defining a plurality of columns each defining a primary grain orientation for defining a corresponding plurality of columnar grains within a molded article that include the primary grain orientations defined by the seed; and
a cooled plate for supporting the mold cavity within a heated chamber, wherein the cooled plate is movable in a controlled manner to remove the mold cavity to control solidification of molten material.
7. The mold assembly for fabricating a cast article as recited in claim 6 , including a baffle that separates the mold cavity from the seed cavity.
8. The mold assembly for fabricating a cast article as recited in claim 6 , wherein the mold cavity includes a top opening and a bottom opening, the bottom opening having a width substantially equal to a width of the seed cavity.
9. The mold assembly for fabricating a cast article as recited in claim 6 , wherein the mold cavity comprises several cavities that are in communication with each other through a common inlet for molten material.
10. The mold assembly for fabricating a cast article as recited in claim 9 , wherein each of the several cavities includes a corresponding seed cavity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/289,115 US20120043046A1 (en) | 2008-10-02 | 2011-11-04 | Process for casting columnar grain airfoil with preferential primary orientation |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/244,203 US8079400B2 (en) | 2008-10-02 | 2008-10-02 | Process for casting columnar grain airfoil with preferential primary orientation |
| US13/289,115 US20120043046A1 (en) | 2008-10-02 | 2011-11-04 | Process for casting columnar grain airfoil with preferential primary orientation |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US12/244,203 Division US8079400B2 (en) | 2008-10-02 | 2008-10-02 | Process for casting columnar grain airfoil with preferential primary orientation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20120043046A1 true US20120043046A1 (en) | 2012-02-23 |
Family
ID=41453951
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US12/244,203 Active 2029-07-23 US8079400B2 (en) | 2008-10-02 | 2008-10-02 | Process for casting columnar grain airfoil with preferential primary orientation |
| US13/289,115 Abandoned US20120043046A1 (en) | 2008-10-02 | 2011-11-04 | Process for casting columnar grain airfoil with preferential primary orientation |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US12/244,203 Active 2029-07-23 US8079400B2 (en) | 2008-10-02 | 2008-10-02 | Process for casting columnar grain airfoil with preferential primary orientation |
Country Status (2)
| Country | Link |
|---|---|
| US (2) | US8079400B2 (en) |
| EP (1) | EP2182098A3 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170136535A1 (en) * | 2014-06-25 | 2017-05-18 | Halliburton Energy Services, Inc. | Insulation enclosure incorporating rigid insulation materials |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8079400B2 (en) * | 2008-10-02 | 2011-12-20 | United Technologies Corporation | Process for casting columnar grain airfoil with preferential primary orientation |
| JP5844361B2 (en) | 2010-06-29 | 2016-01-13 | コーニング インコーポレイテッド | Multi-layer glass plate manufactured by co-stretching using overflow, downdraw and fusion methods |
| US9718127B2 (en) | 2014-05-09 | 2017-08-01 | United Technologies Corporation | Method for forming components using additive manufacturing and re-melt |
| US9435211B2 (en) | 2014-05-09 | 2016-09-06 | United Technologies Corporation | Method for forming components using additive manufacturing and re-melt |
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| US20040231822A1 (en) * | 1998-11-20 | 2004-11-25 | Frasier Donald J. | Method and apparatus for production of a cast component |
| US6837299B2 (en) * | 2002-04-26 | 2005-01-04 | Sky+Ltd. | Heating to control solidification of cast structure |
| US8079400B2 (en) * | 2008-10-02 | 2011-12-20 | United Technologies Corporation | Process for casting columnar grain airfoil with preferential primary orientation |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3532155A (en) | 1967-12-05 | 1970-10-06 | Martin Metals Co | Process for producing directionally solidified castings |
| US4133368A (en) | 1977-08-01 | 1979-01-09 | United Technologies Corporation | Single crystal casting mold and method for making same |
| US4714101A (en) | 1981-04-02 | 1987-12-22 | United Technologies Corporation | Method and apparatus for epitaxial solidification |
| US4605452A (en) | 1981-12-14 | 1986-08-12 | United Technologies Corporation | Single crystal articles having controlled secondary crystallographic orientation |
| US4412577A (en) | 1982-01-27 | 1983-11-01 | United Technologies Corporation | Control of seed melt-back during directional solidification of metals |
| US4475582A (en) | 1982-01-27 | 1984-10-09 | United Technologies Corporation | Casting a metal single crystal article using a seed crystal and a helix |
| US4548255A (en) | 1982-03-01 | 1985-10-22 | United Technologies Corporation | Mold with starter and selector sections for directional solidification casting |
| US4450889A (en) | 1982-08-20 | 1984-05-29 | United Technologies Corporation | Mold having a helix for casting single crystal articles |
| EP0171343A1 (en) * | 1984-05-11 | 1986-02-12 | United Technologies Corporation | Polygon cross section seed for directional solidification |
| US5810552A (en) | 1992-02-18 | 1998-09-22 | Allison Engine Company, Inc. | Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same |
| EP0637476B1 (en) | 1993-08-06 | 2000-02-23 | Hitachi, Ltd. | Blade for gas turbine, manufacturing method of the same, and gas turbine including the blade |
| US5404930A (en) | 1994-01-06 | 1995-04-11 | Pcc Airfoils, Inc. | Method and apparatus for casting an airfoil |
| CN1226291A (en) | 1996-06-05 | 1999-08-18 | 通用电气公司 | Method and apparatus for making directionally solidified castings |
| EP1076119A1 (en) | 1999-08-11 | 2001-02-14 | ABB Alstom Power (Schweiz) AG | Apparatus and method for manufacture a directionally solidified columnar grained article |
-
2008
- 2008-10-02 US US12/244,203 patent/US8079400B2/en active Active
-
2009
- 2009-10-02 EP EP09252356A patent/EP2182098A3/en not_active Withdrawn
-
2011
- 2011-11-04 US US13/289,115 patent/US20120043046A1/en not_active Abandoned
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040231822A1 (en) * | 1998-11-20 | 2004-11-25 | Frasier Donald J. | Method and apparatus for production of a cast component |
| US6837299B2 (en) * | 2002-04-26 | 2005-01-04 | Sky+Ltd. | Heating to control solidification of cast structure |
| US8079400B2 (en) * | 2008-10-02 | 2011-12-20 | United Technologies Corporation | Process for casting columnar grain airfoil with preferential primary orientation |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170136535A1 (en) * | 2014-06-25 | 2017-05-18 | Halliburton Energy Services, Inc. | Insulation enclosure incorporating rigid insulation materials |
| US10195662B2 (en) * | 2014-06-25 | 2019-02-05 | Halliburton Energy Services, Inc. | Insulation enclosure incorporating rigid insulation materials |
Also Published As
| Publication number | Publication date |
|---|---|
| US8079400B2 (en) | 2011-12-20 |
| EP2182098A3 (en) | 2010-08-04 |
| EP2182098A2 (en) | 2010-05-05 |
| US20100084106A1 (en) | 2010-04-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |