US20050230077A1 - Casting process and cast product - Google Patents
Casting process and cast product Download PDFInfo
- Publication number
- US20050230077A1 US20050230077A1 US10/503,698 US50369805A US2005230077A1 US 20050230077 A1 US20050230077 A1 US 20050230077A1 US 50369805 A US50369805 A US 50369805A US 2005230077 A1 US2005230077 A1 US 2005230077A1
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- Prior art keywords
- stator
- mould
- cast
- canceled
- rotor
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- Abandoned
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- 238000005266 casting Methods 0.000 title claims abstract description 26
- 239000000463 material Substances 0.000 claims abstract description 22
- 238000000034 method Methods 0.000 claims abstract description 21
- 230000008569 process Effects 0.000 claims abstract description 21
- 239000010935 stainless steel Substances 0.000 claims abstract description 21
- 229910001220 stainless steel Inorganic materials 0.000 claims abstract description 21
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 8
- 239000012768 molten material Substances 0.000 claims abstract description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 7
- 238000007528 sand casting Methods 0.000 claims abstract description 6
- 229910000861 Mg alloy Inorganic materials 0.000 claims abstract description 4
- 238000011065 in-situ storage Methods 0.000 claims abstract description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- 239000004576 sand Substances 0.000 claims description 6
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 3
- 239000011777 magnesium Substances 0.000 claims description 3
- 229910052749 magnesium Inorganic materials 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 claims 2
- 239000002184 metal Substances 0.000 claims 2
- 239000004411 aluminium Substances 0.000 abstract description 4
- 239000000047 product Substances 0.000 description 37
- 238000005260 corrosion Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 239000012530 fluid Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
Images
Classifications
-
- 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
- B22C9/28—Moulds for peculiarly-shaped castings for wheels, rolls, or rollers
Definitions
- the invention comprises a casting process for forming a cast product from one material incorporating preformed inserts of another material, and a cast product incorporating inserts within the cast product of a different material which are integral in the finished product.
- Casting processes such as sand casting are well known and commonly used in industry for forming a wide range of products and product components for numerous applications. Without intending to be limiting, many of the components of water jet propulsions systems for watercraft are produced by casting, typically from aluminium or an aluminium alloy.
- the invention comprises a process for forming a cast production component, including one or more parts having a passage or cavity on at least one side, comprising supporting a preformed insert or inserts in association with a mould part or parts which define(s) the passage or cavities during the casting process, surrounding the mould part(s) with one or more other mould parts which define the balance of the product or component shape, filling the mould with molten material, and allowing the product to cool and removing the mould parts to leave the cast product with the preformed inserts cast in situ as an integral part or parts of the cast product or component.
- the invention comprises a cast product including one or more parts having a passage or cavity on at least one side, at least a portion of which part(s) are formed by a preformed insert or inserts about which the balance of the production component has been cast.
- the part or parts of the cast product or component (hereinafter: product) of which at least a portion is formed by a preformed insert may be one or more vanes, blades, ribs, or wall sections for example.
- a portion such as a leading edge, trailing edge, or a central portion of the part(s) may comprise a preformed insert of a stronger or more wear resistant material than the material from which the balance of the product is cast.
- the preformed inserts may be formed from stainless steel while the balance of the product is cast from aluminum or an aluminium alloy (or any other material such as magnesium or a magnesium alloy for example).
- the parts such as vanes, blades, ribs or wall sections may have a passage or cavity on one or both sides.
- a stator or rotor component the parts may be vanes or blades of the stator or rotor, on either side of which fluid flows in use.
- the leading edge for example, or a greater part of the stator or rotor vane or blade, may be formed from stainless steel, in a body of the stator or rotor which is otherwise cast from aluminium or aluminium alloy. The leading edge for example will thus be formed of a more wear resistant material.
- a center part of a stator or rotor vane or blade may be formed of a preformed stainless steel component to give the stator or rotor blade increased strength.
- the product need not necessarily be a product in which vanes or blades radiate from a center core as in a stator or rotor, but may comprise vanes, blades, ribs or the leading edges of corner wall sections, which extend in the finished product generally parallel to each other, across a fluid flow for example.
- Corner wall sections or similar may have a passage on one side through which fluid flows, or cavity, vanes or ribs may have a passage on both sides.
- FIG. 1 is a side view of a stator component
- FIG. 2 is a view from one end of a conventionally cast stator component, in the direction of arrow A in FIG. 1 ,
- FIG. 3 is a view similar to FIG. 2 but of a stator component of the invention
- FIGS. 4 a to d are views from different angles of one of the preferred form stainless steel inserts, which are preformed and incorporated into the stator of FIG. 3 during casting,
- FIGS. 5 to 10 show mould parts and illustrate the casting process of the invention
- FIG. 11 is a view of a cast stator component with a single mould core insert part unremoved
- FIG. 12 is a view of the cast stator component similar to FIG. 11 but with all of the mould core insert parts unremoved, and
- FIGS. 13 to 16 show forming of a core insert mould part carrying a preformed stainless steel insert.
- the stator component comprises a generally tapered cylindrical body having external wall 1 and a center part 2 which are joined by a series of radial vanes 3 . Passages 5 pass through the stator between the angled vanes 3 .
- the stator component is entirely formed by casting from a material such as aluminium or aluminium alloy for example.
- FIG. 3 shows a product of the invention, which is a stator similar to that of FIG. 2 except that the leading edge of each vane 3 is formed from stainless steel.
- Each stator vane 4 is formed partly by a stainless steel insert 6 , which is preformed and incorporated in the product during the casting process so as to be an integral part of the final product.
- a single preformed insert 6 is shown in more detail in FIGS. 4 a to 4 d .
- the insert forms the leading edge of a vane 4 .
- the forward edge 6 a of the insert 6 forms the tip of the leading edge of the stator vane, and a rear edge 6 b abuts so as to be flush and integral with the balance of the vane which is formed from aluminium alloy during the casting process.
- the particular preformed leading edge vane insert shown has a base 7 incorporating protrusion 7 a , which is surrounded by cast material during the casting process so that the top surface of the base 7 is flush with the interior surface of the stator.
- the preformed insert has grooves 8 to assist in fixing the other end of the preformed component in the cast material.
- the preformed insert is shown by way of example only and could be of any desired shape for any desired application, such as a corner shaped insert for example.
- a preformed insert has height as shown, at its either end it may comprise a base 7 and optionally a protrusion 7 a , ribs or depressions 8 , or any other irregularity or means for fixing the preformed component so that in the finished cast product the preformed insert is an integral part of the product.
- a tail pipe stator of the invention formed as described with stainless steel inserts will have substantially greater life due to the increased wear resistance and resistance to galvanic corrosion of the stainless steel leading edges of the stator vanes. Similar advantages are likely to be obtained with product or components for other applications which are cast by the process of the invention, with an insert or inserts formed of a different material having different wear characteristics or other desirable properties for the particular application, relative to the material from which the balance of the component is cast.
- FIGS. 5 to 12 The casting process of the invention as applied to forming the stator of FIG. 3 is illustrated by FIGS. 5 to 12 .
- the stator component is cast using a number of mould components which define the external and internal shapes including internal passages of the stator component, which are formed of sand in a sand casting process.
- FIG. 5 shows a base mould part 10 .
- Portions 10 b and 10 c of the mould base part 10 define the shape of the center 2 of the stator.
- a number of core insert mould parts 11 one of which is shown in FIG. 7 , and which are formed from sand if the product is to be formed using sand casting, are assembled together on the base component as shown in FIGS. 6, 8 and 9 .
- Each of the core insert part 11 defines the passage space between two vanes during the casting process.
- a number of the core insert parts 11 are mounted on the mould base 10 in assembly of the mould— FIG. 6 shows a first core insert part 1 in position on the mould base 10 , FIG. 8 shows three core insert parts 1 in position, and FIG. 9 shows all of the core inserts in position on the mould base part.
- FIG. 11 which shows a cast stator with a single core insert part unremoved (before breaking out of the final core insert part)
- FIG. 12 which shows a cast stator with all of the core insert parts in situ, before breaking out of the core inserts.
- each core insert part 11 When the mould is assembled before filling the mould with molten material to carry out the casting process, one of the preformed stainless steel inserts 6 is carried by each core insert part 11 , as shown, so that each core insert part 11 holds a preformed stainless steel insert 6 in the correct position during casting, when the cavities between the mould base 10 mould top 13 —see FIG. 10 , and core insert part 11 of the mould are filled with molten material. It is apparent from FIGS. 8 and 9 how the core insert parts 11 when assembled together each carry a preformed insert 6 in the correct position around the mould from the center of the mould, so that in the finished cast product the preformed inserts will form the leading edges of the radiating stator vanes. Referring to FIGS. 8 and 9 , the shaped spaces 14 between each two adjacent mould insert parts 11 form the stator vanes, with the preformed stainless steel inserts as the leading edges thereof.
- the mould base 10 includes recesses 10 a into which protrusions 11 b on the bottom end 11 a of the core inserts 11 fit to assist in retaining the core insert parts 11 in position on the mould base 10 .
- the top part 13 of the mould is placed over the mould base and core inserts, as shown in FIG. 10 . Beneath the mould top part 13 and exterior surfaces of the assembled core insert part 11 is defined the cavity which forms the outer tapered circular wall section 1 of the stator.
- the mould is then filled with molten material, through port 15 for example, the molten material is allowed to cool, and the mould is disassembled, in a sand casting process by breaking the mould components away from around the cooled stator product formed by the casting process.
- the core inserts parts 11 are removed, and in the finished cast product the preformed inserts 6 will form the leading edges of the stator vanes 3 as shown in FIG. 3 .
- FIGS. 13 to 16 show how, in the preferred form, the sand core insert mould parts 11 are formed around the preformed stainless steel inserts 6 so as to carry the inserts during the moulding process, until the sand core inserts 11 are broken away from around the cooled stator product formed by the casting process.
- Each sand core insert mould part 11 is formed in a mould 16 having an internal cavity 17 , which generally comprises a base surface 16 and side walls 17 and 19 .
- a preformed stainless steel insert 6 is first inserted into the mould 16 , as shown in FIG. 14 .
- FIG. 16 shows a core insert 11 in the mould 16 after removal of the mould top 21 and prior to removal of the core insert 11 from the mould.
- the core insert parts 11 are formed around the stainless steel preformed inserts 6 , they hold the preformed inserts in the correct position and securely during the casting process. Subsequently in disassembly of the mould the core insert parts 11 are broken away from within the cast product, leaving the stainless steel inserts, now an integral part of the cast product, behind.
- the preformed inserts 6 may simply be slotted or placed into mould parts which hold the preformed parts during the casting process, rather than the mould parts (such as the core inserts 11 ) being first formed around the preformed inserts (stainless steel inserts 6 ) as described.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacture Of Motors, Generators (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Rotary Pumps (AREA)
Abstract
A process for forming a cast product or component, including one or more parts having a passage or cavity on at least one side such as a stator or rotor from aluminium or magnesium alloy, comprises supporting one or more preformed insert or inserts for example stainless steel in association with a mould part or parts which define(s) the passage or cavities during the casting process, surrounding the mould part(s) with one or more other mould parts which define the balance of the product or component shape, filling the mould with molten material, and allowing the product to cool and removing the mould parts to leave the cast product with the preformed inserts cast in situ as an integral part or parts of the cast product or component. Typically the process is a sand casting process. Typically the preformed insert(s) are formed of a stronger or more wear-resistant material than the material from which the balance of the product is cast, such as stainless steel.
Description
- The invention comprises a casting process for forming a cast product from one material incorporating preformed inserts of another material, and a cast product incorporating inserts within the cast product of a different material which are integral in the finished product.
- Casting processes such as sand casting are well known and commonly used in industry for forming a wide range of products and product components for numerous applications. Without intending to be limiting, many of the components of water jet propulsions systems for watercraft are produced by casting, typically from aluminium or an aluminium alloy.
- In a first aspect the invention comprises a process for forming a cast production component, including one or more parts having a passage or cavity on at least one side, comprising supporting a preformed insert or inserts in association with a mould part or parts which define(s) the passage or cavities during the casting process, surrounding the mould part(s) with one or more other mould parts which define the balance of the product or component shape, filling the mould with molten material, and allowing the product to cool and removing the mould parts to leave the cast product with the preformed inserts cast in situ as an integral part or parts of the cast product or component.
- In broad terms in another aspect the invention comprises a cast product including one or more parts having a passage or cavity on at least one side, at least a portion of which part(s) are formed by a preformed insert or inserts about which the balance of the production component has been cast.
- The part or parts of the cast product or component (hereinafter: product) of which at least a portion is formed by a preformed insert may be one or more vanes, blades, ribs, or wall sections for example. A portion such as a leading edge, trailing edge, or a central portion of the part(s) may comprise a preformed insert of a stronger or more wear resistant material than the material from which the balance of the product is cast. For example the preformed inserts may be formed from stainless steel while the balance of the product is cast from aluminum or an aluminium alloy (or any other material such as magnesium or a magnesium alloy for example).
- The parts such as vanes, blades, ribs or wall sections may have a passage or cavity on one or both sides. For example in a stator or rotor component the parts may be vanes or blades of the stator or rotor, on either side of which fluid flows in use. The leading edge for example, or a greater part of the stator or rotor vane or blade, may be formed from stainless steel, in a body of the stator or rotor which is otherwise cast from aluminium or aluminium alloy. The leading edge for example will thus be formed of a more wear resistant material. Alternatively a center part of a stator or rotor vane or blade may be formed of a preformed stainless steel component to give the stator or rotor blade increased strength. The product need not necessarily be a product in which vanes or blades radiate from a center core as in a stator or rotor, but may comprise vanes, blades, ribs or the leading edges of corner wall sections, which extend in the finished product generally parallel to each other, across a fluid flow for example. Corner wall sections or similar may have a passage on one side through which fluid flows, or cavity, vanes or ribs may have a passage on both sides. For example it may be desired to incorporate in a cast product a harder insert at the corner of an internal passage around which fluid passes in use, and which is prone to wear or corrosion damage or similar. Numerous variations of products may be formed by the process of the invention are possible.
- The process and a product of the invention are described with reference to the accompanying drawings, by way of example and without intending to be limiting, in which:
-
FIG. 1 is a side view of a stator component, -
FIG. 2 is a view from one end of a conventionally cast stator component, in the direction of arrow A inFIG. 1 , -
FIG. 3 is a view similar toFIG. 2 but of a stator component of the invention, -
FIGS. 4 a to d are views from different angles of one of the preferred form stainless steel inserts, which are preformed and incorporated into the stator ofFIG. 3 during casting, - FIGS. 5 to 10 show mould parts and illustrate the casting process of the invention,
-
FIG. 11 is a view of a cast stator component with a single mould core insert part unremoved, -
FIG. 12 is a view of the cast stator component similar toFIG. 11 but with all of the mould core insert parts unremoved, and - FIGS. 13 to 16 show forming of a core insert mould part carrying a preformed stainless steel insert.
- The casting process of the invention is described in detail with reference to the casting of a stator component, by way of example only and as previously indicated the process of the invention may be used to form a wide range of cast products and components.
- Referring to FIGS. 1 to 3, and also
FIGS. 11 and 12 , the stator component comprises a generally tapered cylindrical body havingexternal wall 1 and acenter part 2 which are joined by a series ofradial vanes 3.Passages 5 pass through the stator between theangled vanes 3. Conventionally the stator component is entirely formed by casting from a material such as aluminium or aluminium alloy for example. -
FIG. 3 shows a product of the invention, which is a stator similar to that ofFIG. 2 except that the leading edge of eachvane 3 is formed from stainless steel. Eachstator vane 4 is formed partly by astainless steel insert 6, which is preformed and incorporated in the product during the casting process so as to be an integral part of the final product. - A single
preformed insert 6 is shown in more detail inFIGS. 4 a to 4 d. The insert forms the leading edge of avane 4. Theforward edge 6 a of theinsert 6 forms the tip of the leading edge of the stator vane, and arear edge 6 b abuts so as to be flush and integral with the balance of the vane which is formed from aluminium alloy during the casting process. In the preferred form the particular preformed leading edge vane insert shown has abase 7 incorporatingprotrusion 7 a, which is surrounded by cast material during the casting process so that the top surface of thebase 7 is flush with the interior surface of the stator. At its other end the preformed insert hasgrooves 8 to assist in fixing the other end of the preformed component in the cast material. The preformed insert is shown by way of example only and could be of any desired shape for any desired application, such as a corner shaped insert for example. Where a preformed insert has height as shown, at its either end it may comprise abase 7 and optionally aprotrusion 7 a, ribs ordepressions 8, or any other irregularity or means for fixing the preformed component so that in the finished cast product the preformed insert is an integral part of the product. - In relation to water jet propulsion systems it is well known that the leading edges of the vanes of the tail pipe stator are prone to damage from cavitation, abrasion, and galvanic corrosion, and that it is necessary to inspect, repair, and if necessary replace the tail pipe stators of water jet propulsion systems periodically. A tail pipe stator of the invention formed as described with stainless steel inserts will have substantially greater life due to the increased wear resistance and resistance to galvanic corrosion of the stainless steel leading edges of the stator vanes. Similar advantages are likely to be obtained with product or components for other applications which are cast by the process of the invention, with an insert or inserts formed of a different material having different wear characteristics or other desirable properties for the particular application, relative to the material from which the balance of the component is cast.
- The casting process of the invention as applied to forming the stator of
FIG. 3 is illustrated by FIGS. 5 to 12. As is conventional, the stator component is cast using a number of mould components which define the external and internal shapes including internal passages of the stator component, which are formed of sand in a sand casting process.FIG. 5 shows abase mould part 10. 10 b and 10 c of thePortions mould base part 10 define the shape of thecenter 2 of the stator. A number of coreinsert mould parts 11, one of which is shown inFIG. 7 , and which are formed from sand if the product is to be formed using sand casting, are assembled together on the base component as shown inFIGS. 6, 8 and 9. Each of thecore insert part 11 defines the passage space between two vanes during the casting process. A number of thecore insert parts 11 are mounted on themould base 10 in assembly of the mould—FIG. 6 shows a firstcore insert part 1 in position on themould base 10,FIG. 8 shows threecore insert parts 1 in position, andFIG. 9 shows all of the core inserts in position on the mould base part. The way in which the core insert parts define the passages between the vanes in the finished stator product is illustrated byFIG. 11 which shows a cast stator with a single core insert part unremoved (before breaking out of the final core insert part), andFIG. 12 which shows a cast stator with all of the core insert parts in situ, before breaking out of the core inserts. - When the mould is assembled before filling the mould with molten material to carry out the casting process, one of the preformed
stainless steel inserts 6 is carried by eachcore insert part 11, as shown, so that eachcore insert part 11 holds a preformedstainless steel insert 6 in the correct position during casting, when the cavities between themould base 10mould top 13—seeFIG. 10 , andcore insert part 11 of the mould are filled with molten material. It is apparent fromFIGS. 8 and 9 how thecore insert parts 11 when assembled together each carry apreformed insert 6 in the correct position around the mould from the center of the mould, so that in the finished cast product the preformed inserts will form the leading edges of the radiating stator vanes. Referring toFIGS. 8 and 9 , theshaped spaces 14 between each two adjacentmould insert parts 11 form the stator vanes, with the preformed stainless steel inserts as the leading edges thereof. - In the preferred form the
mould base 10 includesrecesses 10 a into whichprotrusions 11 b on thebottom end 11 a of thecore inserts 11 fit to assist in retaining thecore insert parts 11 in position on themould base 10. After all of the core inserts have been put in position as shown inFIG. 9 , thetop part 13 of the mould is placed over the mould base and core inserts, as shown inFIG. 10 . Beneath the mouldtop part 13 and exterior surfaces of the assembledcore insert part 11 is defined the cavity which forms the outer taperedcircular wall section 1 of the stator. - The mould is then filled with molten material, through
port 15 for example, the molten material is allowed to cool, and the mould is disassembled, in a sand casting process by breaking the mould components away from around the cooled stator product formed by the casting process. Thecore inserts parts 11 are removed, and in the finished cast product thepreformed inserts 6 will form the leading edges of thestator vanes 3 as shown inFIG. 3 . - FIGS. 13 to 16 show how, in the preferred form, the sand core
insert mould parts 11 are formed around the preformedstainless steel inserts 6 so as to carry the inserts during the moulding process, until thesand core inserts 11 are broken away from around the cooled stator product formed by the casting process. Each sand coreinsert mould part 11 is formed in amould 16 having aninternal cavity 17, which generally comprises abase surface 16 and 17 and 19. In the preferred form, in forming the core insert 11 a preformedside walls stainless steel insert 6 is first inserted into themould 16, as shown inFIG. 14 . The end of theinsert 6 opposite thebase 7 engages into a complementary shapedslot 21 in thebase surface 16 of the insert mould to hold the preformedinsert 6 in position while themould 16 is filled with sand and binder to form the core insert, and thebase 7 of theinsert 6 similarly engages into the underside of the top 21 of the mould. The top 21 which has a suitably shaped undersurface to complete the interior surfaces of the mould cavity, is placed on themould 16 as shown and the mould is filled with sand and binder.FIG. 16 shows acore insert 11 in themould 16 after removal of themould top 21 and prior to removal of the core insert 11 from the mould. Referring to the description of the casting process of the invention as applied to forming a stator as described above, prior to assembly of the stator mould parts the required number of sand core inserts 11 are formed as described immediately above with reference to FIGS. 13 to 16. - Because the core insert
parts 11 are formed around the stainless steel preformedinserts 6, they hold the preformed inserts in the correct position and securely during the casting process. Subsequently in disassembly of the mould the core insertparts 11 are broken away from within the cast product, leaving the stainless steel inserts, now an integral part of the cast product, behind. In an alternative arrangement, it is possible that the preformedinserts 6 may simply be slotted or placed into mould parts which hold the preformed parts during the casting process, rather than the mould parts (such as the core inserts 11) being first formed around the preformed inserts (stainless steel inserts 6) as described. - The foregoing describes the process of the invention in the application of forming a cast stator component, in which the preformed inserts form the leading edges of the stator vanes, by way of example only and as previously indicated the process of the invention may be used to form a wide range of products or components in which it is desired to provide inserts of a different material having different properties for any desired reason such as to obtain increased resistance to wear, corrosion, or similar for part of the cast product.
- The foregoing describes the invention including a preferred form thereof. Alterations and modifications as will be obvious to those skilled in the art are intended to be incorporated in the scope thereof as defined in the accompanying claims.
Claims (26)
1. (canceled)
2. (canceled)
3. (canceled)
4. (canceled)
5. (canceled)
6. (canceled)
7. (canceled)
8. (canceled)
9. (canceled)
10. (canceled)
11. (canceled)
12. (canceled)
13. (canceled)
14. A process for forming a cast stator or rotor component, which includes a number of radially extending vanes or blades, comprising supporting preformed inserts, each of which in the cast stator or rotor component will form a leading portion of a vane or blade of the rotor or stator component, in association with a mould part or parts which define(s) passages between the vanes or blades during the casting process, surrounding the mould part(s) with one or more other mould parts which define the balance of the stator or rotor component shape, filling the mould with molten material, and allowing the molten material to cool and removing the mould parts to leave the cast stator or rotor component with each preformed insert cast in situ as an integral leading portion of a vane or blade with a trailing portion of the vane or blade being formed of the material from which the balance of the stator or rotor component is cast, said preformed inserts being formed of a stronger or more wear-resistant material than the material from which the balance of the product is cast.
15. A process according to claim 14 wherein at least some of said mould parts are formed of sand by sand casting.
16. A process according to claim 15 wherein the preformed inserts are formed from stainless steel.
17. A process according to claim 16 wherein the balance of the stator or rotor is cast from a metal selected from the group consisting of aluminum, an aluminum alloy, magnesium, and a magnesium alloy.
18. A process according to claim 14 wherein the stator or rotor component is a stator component which comprises a center part, a generally cylindrical body around the center part, and a series of said vanes spaced around the center part and extending radially from the center part to the cylindrical body.
19. A process according to claim 18 wherein the preformed inserts extend the length of the vanes in a radial direction and include an enlarged end at either end of the preformed inserts, which enlarged ends are surrounded by the material of the balance of the stator during casting of the product.
20. A process according to claim 19 including the steps of positioning the preformed inserts in a mould base, positioning one or more core insert parts of the mould in association with the mould base and so as to hold or assist in holding the preformed inserts in position, and fitting a mould top part to the mould.
21. A process according to claim 20 including positioning the preformed inserts in the mould base by fitting the preformed inserts into one or more recesses in the mould base.
22. A stator or rotor including a number of radially extending vanes or blades, the leading portions of which are formed by preformed inserts about which a trailing portion of each of the vanes or blades and the balance of stator or rotor have been cast, the preformed inserts being formed of a stronger or more wear-resistant material than the material from which the trailing portions of the vanes or blades and balance of the stator or rotor has been cast.
23. A stator or rotor according to claim 22 wherein the preformed inserts are formed from stainless steel.
24. A stator or rotor according to claim 23 wherein the balance of the stator or rotor is cast from a metal selected from the group consisting of aluminum, an aluminum alloy, magnesium, and a magnesium alloy.
25. A stator according to claim 24 which comprises a center part, a generally cylindrical body around the center part, and a series of said vanes spaced around the center part and extending radially from the center part to the cylindrical body.
26. A stator according to claim 22 wherein the preformed inserts extend the length of the vanes in a radial direction and include an enlarged end at either end of the preformed inserts which enlarged ends are surrounded by the material of the balance of the stator during casting of the product.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NZ517037 | 2002-02-05 | ||
| NZ517037A NZ517037A (en) | 2002-02-05 | 2002-02-05 | A casting process and cast product |
| PCT/NZ2003/000015 WO2003066255A1 (en) | 2002-02-05 | 2003-02-05 | A casting process and cast product |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20050230077A1 true US20050230077A1 (en) | 2005-10-20 |
Family
ID=27731024
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/503,698 Abandoned US20050230077A1 (en) | 2002-02-05 | 2003-02-05 | Casting process and cast product |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20050230077A1 (en) |
| AU (1) | AU2003206469A1 (en) |
| NZ (1) | NZ517037A (en) |
| WO (1) | WO2003066255A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090176126A1 (en) * | 2008-01-09 | 2009-07-09 | Jiing Tung Tec. Metal Co., Ltd. | Magnesium metal product with reinforcing structure |
| CN110614347A (en) * | 2019-11-06 | 2019-12-27 | 晋江渠成机械有限公司 | Investment casting process of fan-shaped impeller |
| CN114393177A (en) * | 2022-01-25 | 2022-04-26 | 烟台路通精密科技股份有限公司 | A casting process and device for a large thin-walled aluminum alloy supercharger impeller |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007014352A1 (en) * | 2007-03-26 | 2008-10-02 | Robert Bosch Gmbh | Method for casting a housing element for an electrical device comprises placing a stator into a model of the housing element, molding the model with the stator and casting the housing element |
| US8708425B2 (en) | 2010-10-12 | 2014-04-29 | GM Global Technology Operations LLC | Bimetallic casting |
| CN104325091B (en) * | 2014-10-24 | 2016-08-24 | 刘加兴 | A kind of method of casting of automobile hub and mould |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4574865A (en) * | 1984-11-05 | 1986-03-11 | The Air Preheater Company, Inc. | Method of making a finned cast recuperator tube |
| US5290143A (en) * | 1992-11-02 | 1994-03-01 | Allied Signal | Bicast vane and shroud rings |
| US5351395A (en) * | 1992-12-30 | 1994-10-04 | General Electric Company | Process for producing turbine bucket with water droplet erosion protection |
| US5433511A (en) * | 1993-10-07 | 1995-07-18 | Hayes Wheels International, Inc. | Cast wheel reinforced with a metal matrix composite |
| US6032720A (en) * | 1997-01-14 | 2000-03-07 | Tecumseh Products Company | Process for making a vane for a rotary compressor |
| US6516869B2 (en) * | 2001-02-15 | 2003-02-11 | Teksid Aluminum S.P.A. | Mould structure for producing light metal alloy casts and a low pressure precision casting method in a semi permanent mould |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0035913B1 (en) * | 1980-03-12 | 1984-10-17 | Gkn Technology Limited | A wheel for a track-laying vehicle |
| US5259486A (en) * | 1992-02-12 | 1993-11-09 | The Budd Company | Integral casted labrynth ring for brake drum |
-
2002
- 2002-02-05 NZ NZ517037A patent/NZ517037A/en not_active IP Right Cessation
-
2003
- 2003-02-05 US US10/503,698 patent/US20050230077A1/en not_active Abandoned
- 2003-02-05 AU AU2003206469A patent/AU2003206469A1/en not_active Abandoned
- 2003-02-05 WO PCT/NZ2003/000015 patent/WO2003066255A1/en not_active Ceased
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4574865A (en) * | 1984-11-05 | 1986-03-11 | The Air Preheater Company, Inc. | Method of making a finned cast recuperator tube |
| US5290143A (en) * | 1992-11-02 | 1994-03-01 | Allied Signal | Bicast vane and shroud rings |
| US5351395A (en) * | 1992-12-30 | 1994-10-04 | General Electric Company | Process for producing turbine bucket with water droplet erosion protection |
| US5433511A (en) * | 1993-10-07 | 1995-07-18 | Hayes Wheels International, Inc. | Cast wheel reinforced with a metal matrix composite |
| US6032720A (en) * | 1997-01-14 | 2000-03-07 | Tecumseh Products Company | Process for making a vane for a rotary compressor |
| US6516869B2 (en) * | 2001-02-15 | 2003-02-11 | Teksid Aluminum S.P.A. | Mould structure for producing light metal alloy casts and a low pressure precision casting method in a semi permanent mould |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090176126A1 (en) * | 2008-01-09 | 2009-07-09 | Jiing Tung Tec. Metal Co., Ltd. | Magnesium metal product with reinforcing structure |
| CN110614347A (en) * | 2019-11-06 | 2019-12-27 | 晋江渠成机械有限公司 | Investment casting process of fan-shaped impeller |
| CN114393177A (en) * | 2022-01-25 | 2022-04-26 | 烟台路通精密科技股份有限公司 | A casting process and device for a large thin-walled aluminum alloy supercharger impeller |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2003066255A1 (en) | 2003-08-14 |
| NZ517037A (en) | 2004-11-26 |
| AU2003206469A1 (en) | 2003-09-02 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: CWF HAMILTON & CO LIMITED, NEW ZEALAND Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MEDURIC, MLADEN;HAMILTON, MICHAEL;REEL/FRAME:016551/0945 Effective date: 20040816 |
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| STCB | Information on status: application discontinuation |
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