WO2009155655A1 - Manufacture of wear resistant composite components - Google Patents
Manufacture of wear resistant composite components Download PDFInfo
- Publication number
- WO2009155655A1 WO2009155655A1 PCT/AU2009/000816 AU2009000816W WO2009155655A1 WO 2009155655 A1 WO2009155655 A1 WO 2009155655A1 AU 2009000816 W AU2009000816 W AU 2009000816W WO 2009155655 A1 WO2009155655 A1 WO 2009155655A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- wear resistant
- shell
- manufacturing
- alloy
- constituents
- Prior art date
Links
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling 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
- C22C37/00—Cast-iron alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C37/00—Cast-iron alloys
- C22C37/06—Cast-iron alloys containing chromium
- C22C37/08—Cast-iron alloys containing chromium with nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C37/00—Cast-iron alloys
- C22C37/10—Cast-iron alloys containing aluminium or silicon
Definitions
- the present invention relates to the manufacture of wear resistant components including metal composites.
- the invention has been developed in relation to components for ground engaging tools. BACKGROUND TO THE INVENTION
- wear components are often mounted to earth moving buckets and similar machinery.
- Typical wear components include wear bars, bucket heel shrouds and ground engaging tools.
- 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.
- the present invention seeks to provide a method of manufacturing a wear resistant component from a wear resistant alloy and a weldable metal which provides a bond across more than a single surface.
- the invention further seeks to provide a method of manufacturing such components which does not require an initial step of creating a wear resistant alloy before the component can be formed.
- a method of manufacturing a wear resistant metal component having the steps of: providing a metal shell formed from a first metal, the metal shell defining an open receptacle; placing constituents of a metal alloy within the shell, one of the constituents being a primary binding constituent which has a lower melting point than that of the first metal; heating the shell and the constituents to an elevated temperature at which second metal melts; maintaining the shell at the elevated temperature for a time period sufficient for the alloy constituents to melt and diffuse within the primary binding constituent, and to bond to the shell; and cooling the shell to form a wear resistant metal component having an outer shell of the first metal and an inner body of the metal alloy, wherein the metal alloy has a greater resistance to abrasive wear than the first metal.
- a method of manufacturing a wear resistant metal component having the steps of: providing an outer shell, the outer shell defining an open receptacle; locating a body portion within the outer shell, the body portion being spaced from internal walls of the shell and protruding from an opening or the receptacle, the body portion being formed from a first metal; placing constituents of a metal alloy within the shell, one of the constituents being a primary binding constituent which has a lower melting point than that of the first metal; heating the shell and the constituents to an elevated temperature at which second metal melts; maintaining the shell at the elevated temperature for a time period sufficient for the alloy constituents to melt and diffuse within the primary binding constituent, and to bond to the first metal; cooling the shell; and removing the shell to leave a wear resistant metal component having an outer casing of the metal alloy and an inner body of the first metal, wherein the metal alloy has a greater resistance to abrasive wear than the first metal.
- these methods allow for
- the step of heating the shell and constituents may be conducted at around atmospheric pressure. It is preferred that this is done in a furnace arranged to have a relatively low oxygen concentration. This may be a gas fired furnace. The presence of a low oxygen concentration, preferably below 2% by volume, reduces the propensity for oxidation of the first metal.
- the first metal may be steel. It will be understood that this term includes a range of ferrous based alloys of various grades including but not limited to carbon steel, stainless steel, manganese steels, CrMo steels etc.
- the primary binding constituent may be iron, such as pig iron having a carbon content of about 4% by weight.
- the primary binding constituent may comprise at least 40% by weight of the metal alloy. Preferably, the primary binding constituent comprises 55-70% by weight of the metal alloy.
- the elevated temperature must be higher than the melting temperature of the metal alloy. Nonetheless, it will be appreciated that the alloy may include relatively high melting point constituents, with these constituents having melting points higher than the elevated temperature.
- the high melting point constituents are provided in particles having a diameter less than 15mm.
- the high melting point constituents it is preferred for them to be provided in particles having a diameter less than 5mm.
- One of the high melting point constituents may be ferrochrome.
- the elevated temperature may be in the range 1200°C to 1400°C, and in a preferred embodiment of the invention is in the range 1250°C to 1300°C.
- the time period at which this temperature is maintained may be between 15 minutes and 120 minutes, and in the preferred embodiment of the invention is greater than 30 minutes.
- a wear resistant component is formed having an outer steel shell and an inner body of a wear resistant alloy such as white iron.
- the white iron has a single exposed face, which will be the wearing face in use.
- the remainder of the component has steel on the outside, and can thus be readily welded to machinery.
- the steel shell provides impact resistance to the component. Firstly, the steel shell is cast, fabricated and/or machined so as to form a receptacle into which the alloy will be formed.
- the alloy includes a primary binding constituent, being pig iron (having about 4% carbon plus tramp material). It is anticipated that the primary binding constituent should constitute at least 40% by weight of the alloy. In the instant embodiment, the quantity of pig iron provided is in the range 55% to 70% by weight of the alloy. Other alloy constituents are provided in the quantities required to produce the desired composition in the final alloy.
- a typical desired composition could be:
- the maximum particle size of the constituents provided is dependent upon the melting temperature of each constituent. Where the melting temperature of a constituent is higher than the final alloy melting temperature, the particle size must be relatively small to allow for melting, mixing and diffusion of the constituent within the primary binding constituent. In the present embodiment, the maximum particle size of high melting point constituents is 25mm, although particle size less than 15mm is preferred as it allows for shorter hold times.
- the maximum particle size of the constituents may be set at 5mm.
- ferroalloys such as ferrochrome, ferromanganese and ferromolybdenum, represent such particularly high melting point constituents.
- the steel shell and alloy constituents are then placed within a furnace, and heated to an elevated temperature greater than the primary binding constituent and final alloy melting points (liquidus).
- the primary binding constituent's melting point is approximately 118O 0 C and final alloy melting point is about 121O 0 C
- the elevated temperature is between 125O 0 C and 1300 0 C.
- the desired composition could be:
- the elevated temperature is between 1300 0 C and 138O 0 C.
- the melting point of the final alloy composition may range typically from 1200 0 C and 1350 0 C, the elevated temperature will be between 25 0 C and 100°C above the melting point of the final alloy.
- the furnace may be operated substantially at atmospheric pressure. Nonetheless, it is important for a low oxygen atmosphere (for instance, oxygen to be less than 2% by volume) to be maintained within the furnace, in order to reduce the propensity for the steel shell or the alloy constituents to oxidize.
- the furnace is gas-fired, with appropriate gas flow management to cause most of the available oxygen to be consumed in the combustion process. It may be advantageous to provide physical barriers of suitable configuration within the furnace to restrict the flow of gasses about the shell and to the alloy material within the shell.
- the shell is maintained at the elevated temperature for a time period sufficient to permit melting and mixing of the alloy constituents.
- this time period is between 30 minutes and 120 minutes, although it is anticipated that the use of a different alloy may reduce the time period to as little as 15 minutes.
- the maintenance of the shell at this temperature for this time period promotes the creation of a metallurgical bond between the steel and the alloy, thus increasing the strength of the wear resistant composite component.
- the component is cooled to allow the alloy to solidify. Further machining can then be performed on the component if required.
- a wear resistant component is formed having an outer shell of a wear resistant alloy such as white iron, and an inner body of a steel substrate (or other suitable metal, such as a nickel or titanium based alloy). The substrate protrudes from a single face to provide a mounting portion of the component, for welding or other connection to machinery. The remainder of the component has the wear resistant alloy on the outside, and is thus resistant to wear.
- the method of forming such a component is largely similar to the first embodiment.
- the primary difference is that the shell is formed from a sacrificial material, such as a ceramic material.
- the substrate is located within the shell, extending outwardly from the receptacle opening. Alloy components are then provided around the substrate, within the receptacle, and the process continues as outlined in relation to the first embodiment.
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2729051A CA2729051A1 (en) | 2008-06-27 | 2009-06-26 | Manufacture of wear resistant composite components |
AU2009262357A AU2009262357B2 (en) | 2008-06-27 | 2009-06-26 | Manufacture of wear resistant composite components |
ZA2011/00443A ZA201100443B (en) | 2008-06-27 | 2011-01-14 | Manufacture of wear resistant composite components |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2008903278A AU2008903278A0 (en) | 2008-06-27 | Method of Manufacturing Wear Resistant Composite Components | |
AU2008903278 | 2008-06-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2009155655A1 true WO2009155655A1 (en) | 2009-12-30 |
Family
ID=41443910
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/AU2009/000816 WO2009155655A1 (en) | 2008-06-27 | 2009-06-26 | Manufacture of wear resistant composite components |
Country Status (4)
Country | Link |
---|---|
AU (1) | AU2009262357B2 (en) |
CA (1) | CA2729051A1 (en) |
WO (1) | WO2009155655A1 (en) |
ZA (1) | ZA201100443B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9561562B2 (en) | 2011-04-06 | 2017-02-07 | Esco Corporation | Hardfaced wearpart using brazing and associated method and assembly for manufacturing |
US10543528B2 (en) | 2012-01-31 | 2020-01-28 | Esco Group Llc | Wear resistant material and system and method of creating a wear resistant material |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3600201A (en) * | 1968-11-29 | 1971-08-17 | Borg Warner | Hard facing alloy composition and method of manufacture |
US4140170A (en) * | 1977-09-06 | 1979-02-20 | Baum Charles S | Method of forming composite material containing sintered particles |
JPS6256503A (en) * | 1985-09-05 | 1987-03-12 | Silver Roi:Kk | Composite sintered body of powder metallurgy and its production |
US5375759A (en) * | 1993-02-12 | 1994-12-27 | Eutectic Corporation | Alloy coated metal base substrates, such as coated ferrous metal plates |
WO2002013996A1 (en) * | 2000-08-10 | 2002-02-21 | Paul Graeme Huggett | A method of manufacturing metallic composites and composites produced thereby |
RU2202441C2 (en) * | 2001-05-14 | 2003-04-20 | Новосибирский государственный технический университет | Method for connecting hard alloy with cast base of tool |
WO2007059568A1 (en) * | 2005-11-22 | 2007-05-31 | Composite Alloy Products Pty Ltd | A method of manufacturing metallic composites in an inert atmosphere and composites produced thereby |
-
2009
- 2009-06-26 WO PCT/AU2009/000816 patent/WO2009155655A1/en active Application Filing
- 2009-06-26 AU AU2009262357A patent/AU2009262357B2/en not_active Ceased
- 2009-06-26 CA CA2729051A patent/CA2729051A1/en not_active Abandoned
-
2011
- 2011-01-14 ZA ZA2011/00443A patent/ZA201100443B/en unknown
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3600201A (en) * | 1968-11-29 | 1971-08-17 | Borg Warner | Hard facing alloy composition and method of manufacture |
US4140170A (en) * | 1977-09-06 | 1979-02-20 | Baum Charles S | Method of forming composite material containing sintered particles |
JPS6256503A (en) * | 1985-09-05 | 1987-03-12 | Silver Roi:Kk | Composite sintered body of powder metallurgy and its production |
US5375759A (en) * | 1993-02-12 | 1994-12-27 | Eutectic Corporation | Alloy coated metal base substrates, such as coated ferrous metal plates |
WO2002013996A1 (en) * | 2000-08-10 | 2002-02-21 | Paul Graeme Huggett | A method of manufacturing metallic composites and composites produced thereby |
RU2202441C2 (en) * | 2001-05-14 | 2003-04-20 | Новосибирский государственный технический университет | Method for connecting hard alloy with cast base of tool |
WO2007059568A1 (en) * | 2005-11-22 | 2007-05-31 | Composite Alloy Products Pty Ltd | A method of manufacturing metallic composites in an inert atmosphere and composites produced thereby |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9561562B2 (en) | 2011-04-06 | 2017-02-07 | Esco Corporation | Hardfaced wearpart using brazing and associated method and assembly for manufacturing |
US10730104B2 (en) | 2011-04-06 | 2020-08-04 | Esco Group Llc | Hardfaced wear part using brazing and associated method and assembly for manufacturing |
US10543528B2 (en) | 2012-01-31 | 2020-01-28 | Esco Group Llc | Wear resistant material and system and method of creating a wear resistant material |
Also Published As
Publication number | Publication date |
---|---|
ZA201100443B (en) | 2012-06-27 |
AU2009262357A1 (en) | 2009-12-30 |
AU2009262357B2 (en) | 2015-10-01 |
CA2729051A1 (en) | 2009-12-30 |
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