CA2747878A1 - Method of manufacturing components - Google Patents
Method of manufacturing components Download PDFInfo
- Publication number
- CA2747878A1 CA2747878A1 CA2747878A CA2747878A CA2747878A1 CA 2747878 A1 CA2747878 A1 CA 2747878A1 CA 2747878 A CA2747878 A CA 2747878A CA 2747878 A CA2747878 A CA 2747878A CA 2747878 A1 CA2747878 A1 CA 2747878A1
- Authority
- CA
- Canada
- Prior art keywords
- metallic material
- manufacturing
- component
- cavity
- metallic
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 18
- 238000000034 method Methods 0.000 claims abstract description 22
- 238000005299 abrasion Methods 0.000 claims abstract description 10
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 8
- 239000000956 alloy Substances 0.000 claims abstract description 8
- 239000007769 metal material Substances 0.000 claims description 47
- 239000000463 material Substances 0.000 claims description 28
- 229910001037 White iron Inorganic materials 0.000 claims description 18
- 238000010438 heat treatment Methods 0.000 claims description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 9
- 229910052804 chromium Inorganic materials 0.000 claims description 9
- 239000011651 chromium Substances 0.000 claims description 9
- 239000000470 constituent Substances 0.000 claims description 7
- 230000003647 oxidation Effects 0.000 claims description 6
- 238000007254 oxidation reaction Methods 0.000 claims description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 4
- 238000003754 machining Methods 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 3
- 230000000295 complement effect Effects 0.000 claims description 3
- 230000004927 fusion Effects 0.000 claims description 3
- 150000001247 metal acetylides Chemical class 0.000 claims description 3
- 239000010936 titanium Substances 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- 229910000967 As alloy Inorganic materials 0.000 claims description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 2
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 claims description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 239000011733 molybdenum Substances 0.000 claims description 2
- 229910052759 nickel Inorganic materials 0.000 claims description 2
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 239000010955 niobium Substances 0.000 claims description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 2
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- 239000010937 tungsten Substances 0.000 claims description 2
- 229910052720 vanadium Inorganic materials 0.000 claims description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 2
- 239000007789 gas Substances 0.000 abstract description 12
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract description 5
- 239000001301 oxygen Substances 0.000 abstract description 5
- 229910052760 oxygen Inorganic materials 0.000 abstract description 5
- 239000000758 substrate Substances 0.000 abstract description 3
- 238000000605 extraction Methods 0.000 abstract 1
- 229910000831 Steel Inorganic materials 0.000 description 8
- 230000015572 biosynthetic process Effects 0.000 description 8
- 239000010959 steel Substances 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 230000003466 anti-cipated effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 235000000396 iron Nutrition 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000002283 diesel fuel Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000003779 heat-resistant material Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000001473 noxious effect Effects 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical class [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E02—HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
- E02F—DREDGING; SOIL-SHIFTING
- E02F9/00—Component parts of dredgers or soil-shifting machines, not restricted to one of the kinds covered by groups E02F3/00 - E02F7/00
- E02F9/28—Small metalwork for digging elements, e.g. teeth scraper bits
- E02F9/2808—Teeth
- E02F9/285—Teeth characterised by the material used
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/06—Casting in, on, or around objects which form part of the product for manufacturing or repairing tools
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/08—Casting in, on, or around objects which form part of the product for building-up linings or coverings, e.g. of anti-frictional metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D23/00—Casting processes not provided for in groups B22D1/00 - B22D21/00
- B22D23/06—Melting-down metal, e.g. metal particles, in the mould
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/011—Layered products comprising a layer of metal all layers being exclusively metallic all layers being formed of iron alloys or steels
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
- C22C29/067—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds comprising a particular metallic binder
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C37/00—Cast-iron alloys
Abstract
A method of forming a wear resistant component is disclosed. The method includes the metallurgical bonding of an abrasion resistant alloy to a substrate within a furnace. A gas flow restricting means is used to restrict the flow of gaseous oxygen into the region of the metallurgical bond, allowing a furnace to be used without vacuum extraction.
Description
METHOD OF MANUFACTURING COMPONENTS
FIELD OF THE INVENTION
The present invention relates to the formation of components having a shell formed from a first metallic material and an inner body formed from a second metallic material. It has particular application to the formation of wear resistant metallic components.
BACKGROUND TO THE INVENTION
Parts of earth moving machinery and related equipment are subject to significant wear during use, principally due to abrasion. In an attempt to reduce the effects of this abrasion, wear components are often mounted to earth moving buckets and similar machinery. Typical wear components include wear bars, bucket heel shrouds and edge components. The wear components are arranged to protect the parts of the machinery which would otherwise wear most rapidly.
The wear components are designed to be relatively easy to replace, when worn.
It is desirable to make these wear components from abrasive resistant materials, in order to extend their working life and provide an enhanced benefit. It is also necessary to use materials which can withstand substantial impact forces, and the resulting stresses within the material. In general, it has been found that materials of high resistance to abrasive wear, such as chromium white irons and tungsten carbide composites, are generally too brittle to withstand the impact forces to which the wear components are frequently subjected.
Additional difficulties have been experienced in successfully attaching components made of these materials to heavy equipment. The materials are generally incapable of being welded, and the provision of holes and the like in the component for mechanical attachment can lead to unacceptable stress concentrations and resultant failure when in use.
As a result, most wear members are made from quenched and tempered steel, as this provides excellent strength properties along with a degree of resistance to abrasion. Nonetheless, it has long been considered desirable to provide wear members with a higher resistance to abrasive wear than that provided by quenched and tempered steel.
Attempts have been made to overcome the limitations of more highly abrasion resistant materials by bonding these materials to base metals such as steel. In one such process, white iron is cast to a block, which is then machined to a highly smooth finish. A steel substrate is similarly machined to a highly smooth finish. The steel substrate can then be vacuum brazed to the white iron block using a copper filler. This method requires very high machining tolerances, equating to a fraction of a millimetre. Additionally, the copper braze can provide a structural weak point in the wear member.
An alternative process has been proposed in International PCT publication number WO 02/13996. This application describes a process for forming a component from two metallic materials, where the materials form a metallic bond.
The method requires an inner material to have a liquidus temperature which is lower than the solidus temperature of an outer material. The materials are bonded within a furnace, where the materials are heated above the liquidus temperature of the inner material and are then maintained at this elevated temperature for sufficient time to allow fusing of the materials.
The conditions within the furnaces used in the above processes are tightly controlled to prevent oxidation of either the first or the second metal. The furnace employed is a vacuum furnace, which is firstly evacuated of oxygen and may then be purged with an appropriate quantity of an inert gas such as nitrogen. Such a furnace is expensive both to install and operate. Additionally, such furnaces frequently have adverse environmental impacts, with potential for noxious emissions. There are often limits to where vacuum furnaces can be sited.
In another process, white iron has been cast directly onto a steel plate in a foundry mould.
These processes result in a white iron block having a steel plate bonded on one side. It is then possible to attach the white iron to a wearing structure by welding of the steel block to the structure. Such an operation can be problematic, as care must be taken not to `pick up' any of the white iron in the weld, as this will compromise weld integrity.
The present invention seeks to provide a method for manufacturing components such as wear resistant components which provides some of the advantages of WO 02/13996 without requiring the evacuation and purging of a vacuum furnace.
FIELD OF THE INVENTION
The present invention relates to the formation of components having a shell formed from a first metallic material and an inner body formed from a second metallic material. It has particular application to the formation of wear resistant metallic components.
BACKGROUND TO THE INVENTION
Parts of earth moving machinery and related equipment are subject to significant wear during use, principally due to abrasion. In an attempt to reduce the effects of this abrasion, wear components are often mounted to earth moving buckets and similar machinery. Typical wear components include wear bars, bucket heel shrouds and edge components. The wear components are arranged to protect the parts of the machinery which would otherwise wear most rapidly.
The wear components are designed to be relatively easy to replace, when worn.
It is desirable to make these wear components from abrasive resistant materials, in order to extend their working life and provide an enhanced benefit. It is also necessary to use materials which can withstand substantial impact forces, and the resulting stresses within the material. In general, it has been found that materials of high resistance to abrasive wear, such as chromium white irons and tungsten carbide composites, are generally too brittle to withstand the impact forces to which the wear components are frequently subjected.
Additional difficulties have been experienced in successfully attaching components made of these materials to heavy equipment. The materials are generally incapable of being welded, and the provision of holes and the like in the component for mechanical attachment can lead to unacceptable stress concentrations and resultant failure when in use.
As a result, most wear members are made from quenched and tempered steel, as this provides excellent strength properties along with a degree of resistance to abrasion. Nonetheless, it has long been considered desirable to provide wear members with a higher resistance to abrasive wear than that provided by quenched and tempered steel.
Attempts have been made to overcome the limitations of more highly abrasion resistant materials by bonding these materials to base metals such as steel. In one such process, white iron is cast to a block, which is then machined to a highly smooth finish. A steel substrate is similarly machined to a highly smooth finish. The steel substrate can then be vacuum brazed to the white iron block using a copper filler. This method requires very high machining tolerances, equating to a fraction of a millimetre. Additionally, the copper braze can provide a structural weak point in the wear member.
An alternative process has been proposed in International PCT publication number WO 02/13996. This application describes a process for forming a component from two metallic materials, where the materials form a metallic bond.
The method requires an inner material to have a liquidus temperature which is lower than the solidus temperature of an outer material. The materials are bonded within a furnace, where the materials are heated above the liquidus temperature of the inner material and are then maintained at this elevated temperature for sufficient time to allow fusing of the materials.
The conditions within the furnaces used in the above processes are tightly controlled to prevent oxidation of either the first or the second metal. The furnace employed is a vacuum furnace, which is firstly evacuated of oxygen and may then be purged with an appropriate quantity of an inert gas such as nitrogen. Such a furnace is expensive both to install and operate. Additionally, such furnaces frequently have adverse environmental impacts, with potential for noxious emissions. There are often limits to where vacuum furnaces can be sited.
In another process, white iron has been cast directly onto a steel plate in a foundry mould.
These processes result in a white iron block having a steel plate bonded on one side. It is then possible to attach the white iron to a wearing structure by welding of the steel block to the structure. Such an operation can be problematic, as care must be taken not to `pick up' any of the white iron in the weld, as this will compromise weld integrity.
The present invention seeks to provide a method for manufacturing components such as wear resistant components which provides some of the advantages of WO 02/13996 without requiring the evacuation and purging of a vacuum furnace.
SUMMARY OF THE INVENTION
In accordance with the present invention there is provided a method for manufacturing a component, the method comprising the steps of:
(i) providing an outer shell formed by a first metallic material, the outer shell having a base and side walls defining a cavity, the cavity being open at an upper end thereof;
(ii) providing a second metallic material above the base of the cavity;
(iii) providing a gas flow restricting means to restrict the flow of gas into the cavity;
(iv) heating the first and second metallic materials to above the solidus temperature of the second metallic material so that the second metallic material flows and covers the base of the cavity;
(v) heating the metallic materials above the liquidus temperature of the second metallic material;
(vi) cooling the materials below the solidus temperature of the second metallic material so that a metallurgical bond is formed between the first and second metallic materials.
The invention envisages a possible additional step of machining of the outside of the shell following cooling to remove any oxidation which occurs during the heating.
The invention is based on the understanding that the existence of a small quantity of oxygen in the interface between the first and second metallic materials may still allow for the formation of a sufficiently strong metallurgical bond.
With this understanding, the present invention proposes not to remove all oxygen from the environment in which the metals are being heated, but rather to restrict the flow of oxygen into the actual location of the bond. It is understood that this may result in oxidation occurring away from the bond location, but such oxidation is likely to be only to the surface of the component and hence can be machined away.
The method may include an additional step of maintaining the metallic materials above the liquidus temperature of the second metallic material for a sufficient period of time to allow at least partial fusion of the second material to the first material. It is expected that the materials will be held at this temperature sufficiently for substantially complete fusion to occur about the boundary between the first and second metallic materials. This time may be in the order of 15 minutes to 120 minutes.
In its simplest form, the gas flow restricting means may be a cover sized and shaped to locate across the open end of the cavity. In a preferred embodiment, the gas flow restricting means may be a container within which some or all of the second metallic material is located. In this embodiment, the steps of providing the second metallic material and of providing the gas flow restricting means may be achieved through providing the second metallic material in a container, the container having an opening complementary to the open end of the cavity, and then inverting the container and locating it above the cavity.
Melting of the second metallic material will cause it to flow from the container into the cavity.
The present invention may be used in conjunction with the methods of co-pending PCT application PCT/AU2009/000816, the contents of which are incorporated herein by reference. When performed in this manner, the second metallic material may be provided as alloy constituents, chosen so that during the process of the present invention the alloy constituents melt and mix to form a desired alloy composition, bonded to the outer shell.
The second metallic material may be an abrasion resistant metal, such as an abrasion resistant white cast iron. It is anticipated that white cast irons containing carbides of one or more of chromium, molybdenum, tungsten, niobium, vanadium and boron, or other suitable carbides, may be suitable for use in the method of the present invention.
It is anticipated that the present invention will allow wear resistant components to be produced using relatively small and inexpensive kilns or furnaces, operating with a significantly smaller environmental impact than vacuum furnaces. The types of kiln which may be suitable for the method include kilns generally used for the firing of pottery, provided they have a sufficiently high operating temperature. The kiln may be heated by any convenient heat source, including conventional sources such as gas or electricity, or alternatively by sources such as oil or diesel fuel. Heating could also be provided by non-traditional means, such as induction heating or microwave heating.
BRIEF DESCRIPTION OF THE DRAWINGS
It will be convenient to further describe the invention with reference to preferred embodiments of the method of the present invention. Other embodiments are possible, and consequently, the particularity of the following 5 discussion is not to be understood as superseding the generality of the preceding description of the invention. In particular, although the drawings and the discussion below discuss the use of the present invention in the formation of a wear resistant heel shroud, it will be understood that the present invention is applicable for the formation of a wide range of components. In the drawings:
Figure 1 is a perspective of a wear resistant heel shroud formed using a method in accordance with the present invention;
Figure 2 is a perspective of an outer shell of the heel shroud of Figure 1, shown prior to the operation of the present invention;
Figure 3(a) is a cross sectional schematic view of a container used in one embodiment of the present invention;
Figures 3(b) and 3(c) are sequential, cross sectional schematic views of the outer shell of Figure 2 and the container of Figure 3(b) during formation of the heel shroud;
Figures 4(a) and 4(b) are cross sectional schematic views of the heel shroud of Figure 1 during formation in accordance with a second embodiment of the present invention.
DESCRIPTION OF PREFERRED EMBODIMENT
Figure 1 shows a wear resistant mechanical component, being a heel shroud 10. The heel shroud 10 has an outer shell 12, which may be formed from a high strength, weldable material such as a ferrous based material, or a nickel or titanium based alloy. The heel shroud 10 has an inner body 14, which is formed from an abrasion resistant material such as a chromium white iron. The following discussion refers to the method of manufacturing such an article.
Figure 2 shows the outer shell 12 of the heel shroud 10, before the formation of the inner body 14. The outer shell 10 defines a cavity 16, having a base 18 and side walls 20. The cavity 16 has an opening 22 at an upper end thereof. The opening 22 is substantially square.
In accordance with the present invention there is provided a method for manufacturing a component, the method comprising the steps of:
(i) providing an outer shell formed by a first metallic material, the outer shell having a base and side walls defining a cavity, the cavity being open at an upper end thereof;
(ii) providing a second metallic material above the base of the cavity;
(iii) providing a gas flow restricting means to restrict the flow of gas into the cavity;
(iv) heating the first and second metallic materials to above the solidus temperature of the second metallic material so that the second metallic material flows and covers the base of the cavity;
(v) heating the metallic materials above the liquidus temperature of the second metallic material;
(vi) cooling the materials below the solidus temperature of the second metallic material so that a metallurgical bond is formed between the first and second metallic materials.
The invention envisages a possible additional step of machining of the outside of the shell following cooling to remove any oxidation which occurs during the heating.
The invention is based on the understanding that the existence of a small quantity of oxygen in the interface between the first and second metallic materials may still allow for the formation of a sufficiently strong metallurgical bond.
With this understanding, the present invention proposes not to remove all oxygen from the environment in which the metals are being heated, but rather to restrict the flow of oxygen into the actual location of the bond. It is understood that this may result in oxidation occurring away from the bond location, but such oxidation is likely to be only to the surface of the component and hence can be machined away.
The method may include an additional step of maintaining the metallic materials above the liquidus temperature of the second metallic material for a sufficient period of time to allow at least partial fusion of the second material to the first material. It is expected that the materials will be held at this temperature sufficiently for substantially complete fusion to occur about the boundary between the first and second metallic materials. This time may be in the order of 15 minutes to 120 minutes.
In its simplest form, the gas flow restricting means may be a cover sized and shaped to locate across the open end of the cavity. In a preferred embodiment, the gas flow restricting means may be a container within which some or all of the second metallic material is located. In this embodiment, the steps of providing the second metallic material and of providing the gas flow restricting means may be achieved through providing the second metallic material in a container, the container having an opening complementary to the open end of the cavity, and then inverting the container and locating it above the cavity.
Melting of the second metallic material will cause it to flow from the container into the cavity.
The present invention may be used in conjunction with the methods of co-pending PCT application PCT/AU2009/000816, the contents of which are incorporated herein by reference. When performed in this manner, the second metallic material may be provided as alloy constituents, chosen so that during the process of the present invention the alloy constituents melt and mix to form a desired alloy composition, bonded to the outer shell.
The second metallic material may be an abrasion resistant metal, such as an abrasion resistant white cast iron. It is anticipated that white cast irons containing carbides of one or more of chromium, molybdenum, tungsten, niobium, vanadium and boron, or other suitable carbides, may be suitable for use in the method of the present invention.
It is anticipated that the present invention will allow wear resistant components to be produced using relatively small and inexpensive kilns or furnaces, operating with a significantly smaller environmental impact than vacuum furnaces. The types of kiln which may be suitable for the method include kilns generally used for the firing of pottery, provided they have a sufficiently high operating temperature. The kiln may be heated by any convenient heat source, including conventional sources such as gas or electricity, or alternatively by sources such as oil or diesel fuel. Heating could also be provided by non-traditional means, such as induction heating or microwave heating.
BRIEF DESCRIPTION OF THE DRAWINGS
It will be convenient to further describe the invention with reference to preferred embodiments of the method of the present invention. Other embodiments are possible, and consequently, the particularity of the following 5 discussion is not to be understood as superseding the generality of the preceding description of the invention. In particular, although the drawings and the discussion below discuss the use of the present invention in the formation of a wear resistant heel shroud, it will be understood that the present invention is applicable for the formation of a wide range of components. In the drawings:
Figure 1 is a perspective of a wear resistant heel shroud formed using a method in accordance with the present invention;
Figure 2 is a perspective of an outer shell of the heel shroud of Figure 1, shown prior to the operation of the present invention;
Figure 3(a) is a cross sectional schematic view of a container used in one embodiment of the present invention;
Figures 3(b) and 3(c) are sequential, cross sectional schematic views of the outer shell of Figure 2 and the container of Figure 3(b) during formation of the heel shroud;
Figures 4(a) and 4(b) are cross sectional schematic views of the heel shroud of Figure 1 during formation in accordance with a second embodiment of the present invention.
DESCRIPTION OF PREFERRED EMBODIMENT
Figure 1 shows a wear resistant mechanical component, being a heel shroud 10. The heel shroud 10 has an outer shell 12, which may be formed from a high strength, weldable material such as a ferrous based material, or a nickel or titanium based alloy. The heel shroud 10 has an inner body 14, which is formed from an abrasion resistant material such as a chromium white iron. The following discussion refers to the method of manufacturing such an article.
Figure 2 shows the outer shell 12 of the heel shroud 10, before the formation of the inner body 14. The outer shell 10 defines a cavity 16, having a base 18 and side walls 20. The cavity 16 has an opening 22 at an upper end thereof. The opening 22 is substantially square.
Figure 3(a) shows a container 30, formed of a heat resistant material such as a ceramic material. The container 30 has an open top 32. The open top 32 is substantially complementary in shape to the opening 22 of the outer shell 12, such that, when the container 30 is inverted, it can be placed about the opening 22 of the outer shell 12 to substantially seal the opening as shown in Figure 3(b).
The container 30 is filled with an abrasion-resistant material such as a chromium white iron 34.
In order to form the heel shroud 10, the container 30 is inverted and placed atop the outer shell 12 as shown in Figure 3(b). The outer shell 12 and the container 30 are then heated in a furnace to a temperature above the solidus temperature of the chromium white iron 34.
Once it begins to melt, the chromium white iron flows from the container 30 into the cavity 16. The quantity of chromium white iron within the container 30 is chosen so as to fill the cavity 16. Furnace gases are precluded from entering into the cavity 16 due to a seal provided about the cavity opening 22 by the container 30. Even where this is not a gas-tight seal, its effect is to greatly diminish the propensity for gas to flow into the cavity 16. The container 30 thereby acts as a gas flow restricting means.
The covered shell 12 containing white iron 34 is then heated above the liquidus temperature of the chromium white iron. At this point the white iron begins to fuse with the internal shell walls, thus giving rise to a metallurgical bond.
This temperature is maintained for a predetermined time, which may be between 15 minutes and 120 minutes, depending on the particular metals used and the temperature to which the shell 12 is heated.
Once the shell has been heated for a sufficient period, the entire arrangement can be cooled, to solidify the white iron 34 as the inner body 14 of the heel shroud 10.
Depending on the nature of the gases present in the furnace, and on the nature of the outer shell 12, oxidation of the outer shell 12 may have occurred. In order to remove and oxidised parts, and to remove any burrs and the like, the heel shroud 10 may then be subjected to a machining operation.
Figures 4(a) and 4(b) show a different embodiment of the present invention, where constituent parts of the heel shroud inner body 14 are placed within the cavity 16, which is then covered by a cover 40. As in the embodiment of Figure 3, the cover 40 acts to restrict the flow of gases into the cavity 16. The covered shell 12 may then be heated to a level where enough of the constituent ingredients melt so as to form the required alloy, as described in co-pending application number PCT! AU2009/000816.
Modifications and variations as would be apparent to a skilled addressee are deemed to be within the scope of the present invention. For instance, it will be appreciated that some of the second material (or its constituents) can be provided within the cavity 16, with the remainder provided within the container 30.
The container 30 is filled with an abrasion-resistant material such as a chromium white iron 34.
In order to form the heel shroud 10, the container 30 is inverted and placed atop the outer shell 12 as shown in Figure 3(b). The outer shell 12 and the container 30 are then heated in a furnace to a temperature above the solidus temperature of the chromium white iron 34.
Once it begins to melt, the chromium white iron flows from the container 30 into the cavity 16. The quantity of chromium white iron within the container 30 is chosen so as to fill the cavity 16. Furnace gases are precluded from entering into the cavity 16 due to a seal provided about the cavity opening 22 by the container 30. Even where this is not a gas-tight seal, its effect is to greatly diminish the propensity for gas to flow into the cavity 16. The container 30 thereby acts as a gas flow restricting means.
The covered shell 12 containing white iron 34 is then heated above the liquidus temperature of the chromium white iron. At this point the white iron begins to fuse with the internal shell walls, thus giving rise to a metallurgical bond.
This temperature is maintained for a predetermined time, which may be between 15 minutes and 120 minutes, depending on the particular metals used and the temperature to which the shell 12 is heated.
Once the shell has been heated for a sufficient period, the entire arrangement can be cooled, to solidify the white iron 34 as the inner body 14 of the heel shroud 10.
Depending on the nature of the gases present in the furnace, and on the nature of the outer shell 12, oxidation of the outer shell 12 may have occurred. In order to remove and oxidised parts, and to remove any burrs and the like, the heel shroud 10 may then be subjected to a machining operation.
Figures 4(a) and 4(b) show a different embodiment of the present invention, where constituent parts of the heel shroud inner body 14 are placed within the cavity 16, which is then covered by a cover 40. As in the embodiment of Figure 3, the cover 40 acts to restrict the flow of gases into the cavity 16. The covered shell 12 may then be heated to a level where enough of the constituent ingredients melt so as to form the required alloy, as described in co-pending application number PCT! AU2009/000816.
Modifications and variations as would be apparent to a skilled addressee are deemed to be within the scope of the present invention. For instance, it will be appreciated that some of the second material (or its constituents) can be provided within the cavity 16, with the remainder provided within the container 30.
Claims (13)
1. A method of manufacturing a component, the method comprising the steps of:
(i) providing an outer shell formed by a first metallic material, the outer shell having a base and side walls defining a cavity, the cavity being open at an upper end thereof;
(ii) providing a second metallic material above the base of the cavity;
(iii) providing a gas flow restricting means to restrict the flow of gas into the cavity;
(iv) heating the first and second metallic materials to above the solidus temperature of the second metallic material so that the second metallic material flows and covers the base of the cavity;
(v) heating the metallic materials above the liquidus temperature of the second metallic material;
(vi) cooling the materials below the solidus temperature of the second metallic material so that a metallurgical bond is formed between the first and second metallic materials.
(i) providing an outer shell formed by a first metallic material, the outer shell having a base and side walls defining a cavity, the cavity being open at an upper end thereof;
(ii) providing a second metallic material above the base of the cavity;
(iii) providing a gas flow restricting means to restrict the flow of gas into the cavity;
(iv) heating the first and second metallic materials to above the solidus temperature of the second metallic material so that the second metallic material flows and covers the base of the cavity;
(v) heating the metallic materials above the liquidus temperature of the second metallic material;
(vi) cooling the materials below the solidus temperature of the second metallic material so that a metallurgical bond is formed between the first and second metallic materials.
2. A method of manufacturing a component as claimed in claim 1, including a further step of machining of the outside of the shell following cooling to remove any oxidation which occurs during the heating.
3. A method of manufacturing a component as claimed in claim 1 or claim 2, whereby following heating of the metallic materials, the temperature of the metallic materials is maintained above the liquidus temperature of the second metallic material for a sufficient period of time to allow at least partial fusion of the second material to the first material.
4. A method of manufacturing a component as claimed in claim 3, wherein the temperature of the metallic materials is maintained above the liquidus temperature for at least 15 minutes.
5. A method of manufacturing a component as claimed in any preceding claim, whereby the gas flow restricting means is a cover sized and shaped to locate across the open end of the cavity.
6. A method of manufacturing a component as claimed in any one of claims 1 to 4, wherein the gas flow restricting means is a container within which some or all of the second metallic material is located.
7. A method of manufacturing a component as claimed in claim 6, wherein the steps of providing the second metallic material and of providing the gas flow restricting means are achieved through providing the second metallic material in a container, the container having an opening complementary to the open end of the cavity, and then inverting the container and locating it above the cavity.
8. A method of manufacturing a component as claimed in any preceding claim, wherein the second metallic material is provided as alloy constituents, chosen so that during the process of the present invention the alloy constituents melt and mix to form a desired alloy composition, bonded to the outer shell.
9. A method of manufacturing a component as claimed in any preceding claim, wherein the first metallic material has a higher tensile strength than the second metallic material, and wherein the second metallic material is more resistant to abrasion than the first metallic material.
10. A method of manufacturing a component as claimed in claim 9, wherein the first metallic material is a ferrous based material.
11. A method of manufacturing a component as claimed in claim 9, wherein the first metallic material is a nickel or titanium based alloy.
12. A method of manufacturing a component as claimed in any one of claims 9 to 11, wherein the second metallic material is a white cast iron.
13. A method of manufacturing a component as claimed in claim 12, wherein the second metallic material is a white cast iron containing carbides of at least one of chromium, molybdenum, tungsten, titanium, niobium, vanadium or boron.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU2008906602 | 2008-12-23 | ||
| AU2008906602A AU2008906602A0 (en) | 2008-12-23 | Method of manufacturing components | |
| PCT/AU2009/001696 WO2010071940A1 (en) | 2008-12-23 | 2009-12-23 | Method of manufacturing components |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2747878A1 true CA2747878A1 (en) | 2010-07-01 |
Family
ID=42286801
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2747878A Abandoned CA2747878A1 (en) | 2008-12-23 | 2009-12-23 | Method of manufacturing components |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20110259541A1 (en) |
| AU (1) | AU2009329829B2 (en) |
| CA (1) | CA2747878A1 (en) |
| WO (1) | WO2010071940A1 (en) |
| ZA (1) | ZA201105114B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110153396A (en) * | 2012-01-31 | 2019-08-23 | 爱斯科集团有限责任公司 | Wear-resistant material and the system and method for forming wear-resistant material |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9027266B2 (en) * | 2010-06-28 | 2015-05-12 | Excalibur Steel Company Pty Ltd | Wear resistant component |
| KR102627470B1 (en) * | 2016-11-17 | 2024-01-19 | 에이치디현대인프라코어 주식회사 | Construction equipment bucket parts and methods of manufacturing the same |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1734313A (en) * | 1928-05-26 | 1929-11-05 | Malmborg Nils W Daniel Von | Casting apparatus |
| US2315876A (en) * | 1941-12-19 | 1943-04-06 | Baker & Co Inc | Casting of metal alloys |
| US4017480A (en) * | 1974-08-20 | 1977-04-12 | Permanence Corporation | High density composite structure of hard metallic material in a matrix |
| US4052802A (en) * | 1976-02-23 | 1977-10-11 | Caterpillar Tractor Co. | Ground-engaging tool with wear-resistant insert |
| US4933240A (en) * | 1985-12-27 | 1990-06-12 | Barber Jr William R | Wear-resistant carbide surfaces |
| JPS645701A (en) * | 1987-06-29 | 1989-01-10 | Kubota Ltd | Center for supporting rotor |
| US4823513A (en) * | 1987-10-13 | 1989-04-25 | Mermark, Inc. | Apparatus and process for vibratory finishing of parts |
| US4966222A (en) * | 1989-10-05 | 1990-10-30 | Paton Boris E | Method of and apparatus for producing shaped castings |
| AUPQ933400A0 (en) * | 2000-08-10 | 2000-08-31 | Huggett, Paul | A method of manufacturing metallic composites produced thereby |
| US6652814B1 (en) * | 2000-08-11 | 2003-11-25 | Lifescan, Inc. | Strip holder for use in a test strip meter |
| US7807099B2 (en) * | 2005-11-10 | 2010-10-05 | Baker Hughes Incorporated | Method for forming earth-boring tools comprising silicon carbide composite materials |
-
2009
- 2009-12-23 US US13/141,443 patent/US20110259541A1/en not_active Abandoned
- 2009-12-23 WO PCT/AU2009/001696 patent/WO2010071940A1/en active Application Filing
- 2009-12-23 CA CA2747878A patent/CA2747878A1/en not_active Abandoned
- 2009-12-23 AU AU2009329829A patent/AU2009329829B2/en not_active Ceased
-
2011
- 2011-07-12 ZA ZA2011/05114A patent/ZA201105114B/en unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110153396A (en) * | 2012-01-31 | 2019-08-23 | 爱斯科集团有限责任公司 | Wear-resistant material and the system and method for forming wear-resistant material |
Also Published As
| Publication number | Publication date |
|---|---|
| AU2009329829B2 (en) | 2016-06-02 |
| AU2009329829A1 (en) | 2011-07-28 |
| WO2010071940A1 (en) | 2010-07-01 |
| US20110259541A1 (en) | 2011-10-27 |
| ZA201105114B (en) | 2012-11-28 |
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