US20150246391A1 - Method for Manufacturing Steel Casts - Google Patents
Method for Manufacturing Steel Casts Download PDFInfo
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- US20150246391A1 US20150246391A1 US14/428,336 US201314428336A US2015246391A1 US 20150246391 A1 US20150246391 A1 US 20150246391A1 US 201314428336 A US201314428336 A US 201314428336A US 2015246391 A1 US2015246391 A1 US 2015246391A1
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- reinforcement insert
- micro
- steel
- mold
- melting
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- 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
- B22D19/02—Casting in, on, or around objects which form part of the product for making reinforced articles
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- 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
- B22D19/0081—Casting in, on, or around objects which form part of the product pretreatment of the insert, e.g. for enhancing the bonding between insert and surrounding cast metal
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/30—Process control
- B22F10/38—Process control to achieve specific product aspects, e.g. surface smoothness, density, porosity or hollow structures
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- B22F3/1055—
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/08—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/003—Making ferrous alloys making amorphous alloys
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/36—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.7% by weight of carbon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C45/00—Amorphous alloys
- C22C45/02—Amorphous alloys with iron as the major constituent
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Definitions
- chromium carbides have the tendency to precipitate to the grain edge, making the structure fragile and reducing the toughness of the steel.
- a heat treatment is therefore necessary, typically a solubilization annealing followed by water quenching, which is carried out after the cooling of the steel has been completed. The annealing and subsequent rapid cooling allow to make the carbides migrate from the grain edge to the austenitic matrix.
- annealing does not allow to obtain a complete solubilization of the carbides, and therefore it is intended to modify the form of the latter, so as to make them globular and therefore less inclined to form cracks. Furthermore, another function of annealing and quenching is to distribute the carbides present at the grain edge uniformly around the austenitic grain.
- Methods are known, from GB-A-2098112 and GB-A-2003932, for manufacturing wear elements reinforced by high-resistance inserts having a heterogeneous structure defined by sintered particles in a metal matrix.
- the above methods provide to make the inserts by uniting carbides, for example tungsten or titanium carbides, in the form of powders or granules, to metal matrixes containing alloys of iron or cobalt using sintering techniques carried out at temperatures above the melting temperature of the alloys.
- the melting of the alloys causes the carbides to be incorporated into the metal matrixes and possibly the sizes of the carbides to be reduced. Afterward, the inserts thus made are introduced into a mold and incorporated into the metal alloy that is cast onto them.
- EP-B1-0554682 describes a method for manufacturing an element subject to wear in which one or more planar inserts, conformed as plates, sheets or discs, are obtained by incorporating powders of materials with high resistance to wear, in particular carbides, for example tungsten carbides, in a metal matrix.
- the reinforcement inserts described in EP-B 1-0554682 can also include organic binders, plasticizers and hardening agents.
- the planar insert is subjected to high-temperature vacuum sintering and is then attached to a sand mold by means of pins or other anchoring elements made of the same material.
- sintering is carried out essentially at temperatures that come within the range of the melting temperature of the metal matrix, and lower than the melting temperatures of the carbides.
- the purpose of sintering is essentially to determine an interface contact, or uniformly distributed, between the carbides and the matrix, in order to obtain reinforcement inserts consisting of a conglomerate of carbides immersed in the metal matrix.
- the original carbides remain substantially unchanged, except for possible variations in size.
- DE-A1-4214524 describes a method for manufacturing a wear-resistant cast that provides to insert into the mold, before casting, a reinforcement insert made with balls of hard material, in particular carbides, housed in seatings made in holed sheets of steel and held in position by the same holed sheets of steel.
- Purpose of the present invention is to perfect a method that allows to obtain, by casting, casts of steel alloys, advantageously but not exclusively manganese steel, having throughout the toughness of manganese steel and, in localized zones, the hardness needed to resist stresses of wear and abrasion.
- the invention obtains steel casts that, throughout the localized zones, have a homogeneous micro-structure and a uniform distribution of the mechanical characteristics.
- the Applicant has devised, tested and embodied the present invention to overcome the shortcomings of the state of the art and to obtain these and other purposes and advantages.
- a method according to the present invention is used for manufacturing steel casts, in particular but not exclusively for manufacturing manganese steel casts intended to obtain wear elements.
- the method comprises at least a step of making at least a reinforcement insert, a step of preparing a mold for the cast to be manufactured, and a subsequent step of casting the steel inside the mold.
- the reinforcement insert is made by compacting an amorphous mass of hardening powder in a desired geometric shape.
- the compacting is obtained by means of sintering techniques with a selective and localized melting comprising one or another of the techniques identified as EBM (Electron Beam Melting), SLM (Selective Laser Melting), or other similar or comparable techniques.
- the amorphous mass of hardening powder is obtained by mixing powders of pure elements, or of compounds that form carbides and/or micro-structures of great hardness, which due to the effect of the melting generate carbides and/or micro-structures of great hardness.
- Making reinforcement inserts with EBM or SLM techniques or similar also has the other advantage of obtaining a rapid and accurate process, and also allows to obtain reinforcement inserts starting from powders of high-melting materials, for example tungsten, titanium, molybdenum, advantageously usable pure or alloyed in iron alloys, which, after the chemical reactions that are triggered due to the effect of the type of melting, give rise to carbides or other hard micro-structures.
- high-melting materials for example tungsten, titanium, molybdenum, advantageously usable pure or alloyed in iron alloys, which, after the chemical reactions that are triggered due to the effect of the type of melting, give rise to carbides or other hard micro-structures.
- the mold preparation step comprises a sub-step of positioning at least one reinforcement insert inside the mold.
- at least one appendix is also made in a piece therewith, with the function of anchoring the reinforcement insert to the mold.
- the sintering techniques melt the powders of pure elements, or compounds that form carbides and/or micro-structures of great hardness, triggering chemical reactions to generate carbides and/or micro-structures of great hardness, uniformly and homogeneously distributed inside the reinforcement insert and defining a homogeneous micro-structure of the latter.
- the carbides make the reinforcement insert uniformly hard and resistant to wear, and suitable to confer these properties throughout the volume of the zones of the cast into which it is inserted.
- the reinforcement insert is partly melted, which advantageously allows an intimate welding with the cast steel, to confer on the cast obtained a homogeneous macro-structure.
- the method 10 provides that in a preparation step 11 a mold 11 is made for every cast 110 , that in a subsequent casting step 12 molten manganese steel is cast inside the mold 111 and that in a standby step the cast 110 solidifies.
- the preparation step 11 comprises a sub-step 14 of positioning at least one reinforcement insert 115 inside the internal cavity 113 of the mold 111 .
- Sintering provides an initial compacting of the hardening powder 118 , which is then at least partly melted using high density energy, and subsequently re-solidified.
- a second formulation of the present invention provides that, as well as iron-based powder, the hardening powder 118 comprises the following components:
- molybdenum in a percentage comprised between 0.5% and 1.5%.
- the primary function of sintering by means of EBM or SLM is therefore to determine the micro-structure of the reinforcement insert 115 , triggering chemical reactions starting from the base components.
- an anchoring operation is also carried out, during which it is anchored at least to one of the perimeter walls 112 of the mold 111 .
- the reinforcement insert 115 comprises, at its ends, one or more appendixes 120 , which function as anchoring means and which are inserted inside the corresponding perimeter walls 112 .
- FIG. 3 shows an example of a cast 110 showing the incorporated position of the reinforcement insert 115 .
- the use of EBM or SLM techniques allows to obtain reinforcement inserts 115 which are not only micro-structurally homogeneous but also substantially without residual porosity and tensions, and therefore advantageously compact and resistant.
- the reinforcement inserts 115 thus obtained do not need heat treatments after they have been made, and therefore can be put into the mold 111 immediately after sintering.
- each reinforcement insert 115 can be subjected to partial melting which, during the subsequent solidification, allows to obtain a cast 110 that is macro-structurally homogeneous, due to the welding of the cast steel and the melted part of the reinforcement insert 115 .
- the cast 110 obtained maintains a generally heterogeneous micro-structure, which has a greater hardness in correspondence with the zones concerned with the reinforcement insert 115 , which is uniformly distributed in them and constant, that is, without point-by-point variations.
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- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Automation & Control Theory (AREA)
- Powder Metallurgy (AREA)
- Heat Treatment Of Steel (AREA)
- Coating By Spraying Or Casting (AREA)
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Abstract
Description
- The present invention concerns a method for manufacturing steel casts, advantageously but not exclusively of manganese steel, used to obtain wear elements, and casts thus manufactured.
- The wear elements are usable in all the applications where a high resistance to wear is required, even under impulsive loads, such as crushers, mills, grinding members, turbo-machine components or earth moving machines.
- It is known to manufacture, by casting, steel casts to obtain wear elements, used in a plurality of applications which require great resistance both to abrasion and to knocks. For example, such steels are used to make components for mills, crushers or safes, components for excavators or tracked means or turbo-machines etc.
- In a preferential formulation the steels in question contain up to 1.5% carbon and up to 20% manganese, and have an austenitic structure that allows to combine great hardness with considerable toughness. These steels also have a good tendency for work-hardening and great ductility.
- It is known to add elements that form complex carbides to these steels, in order to form manganese steel alloys that are more resistant to wear. Among these components the most commonly used is chromium which, as well as raising the yield point, induces the formation of chromium carbide in the austenitic matrix.
- However, chromium carbides have the tendency to precipitate to the grain edge, making the structure fragile and reducing the toughness of the steel. A heat treatment is therefore necessary, typically a solubilization annealing followed by water quenching, which is carried out after the cooling of the steel has been completed. The annealing and subsequent rapid cooling allow to make the carbides migrate from the grain edge to the austenitic matrix.
- For high chromium contents, annealing does not allow to obtain a complete solubilization of the carbides, and therefore it is intended to modify the form of the latter, so as to make them globular and therefore less inclined to form cracks. Furthermore, another function of annealing and quenching is to distribute the carbides present at the grain edge uniformly around the austenitic grain.
- Although these known steels are the best for resistance to wear with regard to materials to be ground having considerable toughness and abrasiveness, they also have the disadvantage that they have low heat-conductivity. Indeed, this has limited their use to thicknesses of not more than about 100 mm, because in products of greater thicknesses the water quenching process entails the creation of internal tensions such as to cause cracks. In this way, if such thicknesses are obtained with steels containing manganese comprised between 12% and 20%, the properties of toughness that are typical of such steels are compromised.
- It is also known that this limitation in the thicknesses can be overcome by introducing elements, such as for example titanium, able to give origin to hard compounds already in the liquid phase of the alloy. The hard compounds are rarely located at the grain edge, but remain uniformly distributed in the austenitic matrix, even after the solubilization treatment. The steel alloys that are obtained are therefore more resistant to abrasion and wear compared with steels containing chromium and without titanium, especially in the case of considerable thicknesses and particularly onerous conditions of use.
- One disadvantage of steels containing titanium is that they confer greater resistance to wear on the whole section of an article, even though it is necessary to have a particular resistance only in those parts that are most stressed. This makes the article less workable and causes a considerable increase in the costs of working, due to the removal of chip.
- Another disadvantage connected to the use of titanium and the manufacture of an article having uniformly optimum characteristics lies in the cost of said article, which is very high.
- Methods are known, from GB-A-2098112 and GB-A-2003932, for manufacturing wear elements reinforced by high-resistance inserts having a heterogeneous structure defined by sintered particles in a metal matrix. The above methods provide to make the inserts by uniting carbides, for example tungsten or titanium carbides, in the form of powders or granules, to metal matrixes containing alloys of iron or cobalt using sintering techniques carried out at temperatures above the melting temperature of the alloys.
- The melting of the alloys causes the carbides to be incorporated into the metal matrixes and possibly the sizes of the carbides to be reduced. Afterward, the inserts thus made are introduced into a mold and incorporated into the metal alloy that is cast onto them.
- EP-B1-0554682 describes a method for manufacturing an element subject to wear in which one or more planar inserts, conformed as plates, sheets or discs, are obtained by incorporating powders of materials with high resistance to wear, in particular carbides, for example tungsten carbides, in a metal matrix. The reinforcement inserts described in EP-B 1-0554682 can also include organic binders, plasticizers and hardening agents. The planar insert is subjected to high-temperature vacuum sintering and is then attached to a sand mold by means of pins or other anchoring elements made of the same material.
- In the three documents cited above, sintering is carried out essentially at temperatures that come within the range of the melting temperature of the metal matrix, and lower than the melting temperatures of the carbides. In these documents, the purpose of sintering is essentially to determine an interface contact, or uniformly distributed, between the carbides and the matrix, in order to obtain reinforcement inserts consisting of a conglomerate of carbides immersed in the metal matrix.
- The original carbides remain substantially unchanged, except for possible variations in size.
- DE-A1-4214524 describes a method for manufacturing a wear-resistant cast that provides to insert into the mold, before casting, a reinforcement insert made with balls of hard material, in particular carbides, housed in seatings made in holed sheets of steel and held in position by the same holed sheets of steel.
- WO-A1-2012/004654 describes a method for manufacturing elements subject to wear which provides to make reinforcement inserts to be incorporated in casts of melted steel. The reinforcement inserts comprise a porous support, like a sponge, impregnated with a liquid mixture consisting of a binder and metal powders containing hard elements, in particular carbides.
- The use of sintering techniques as described in GB-A-2098112, GB-A-2003932 and EP-B1-0554682 has the disadvantage that they need long working times, enormous energy consumption and a consequent increase in the costs of manufacturing the final cast. This is due to the fact that, to make the inserts with these known techniques, preliminary operations are needed to prepare a mixture, or “green”, to be sintered, and molds, in which the mixture is subjected to sintering.
- Another disadvantage of these known methods is that they are not very flexible in terms of possible shapes of the inserts obtainable, since the shapes are limited to planar objects or with a simple conformation, also because of the molds as described above.
- One disadvantage of all the known methods indicated above is connected to the micro-structural heterogeneity of the reinforcement inserts, and consists in the consequent discontinuity of the physical and mechanical properties, the distribution of which is not uniform.
- Purpose of the present invention is to perfect a method that allows to obtain, by casting, casts of steel alloys, advantageously but not exclusively manganese steel, having throughout the toughness of manganese steel and, in localized zones, the hardness needed to resist stresses of wear and abrasion. In particular, the invention obtains steel casts that, throughout the localized zones, have a homogeneous micro-structure and a uniform distribution of the mechanical characteristics.
- The Applicant has devised, tested and embodied the present invention to overcome the shortcomings of the state of the art and to obtain these and other purposes and advantages.
- The present invention is set forth and characterized in the independent claims, while the dependent claims describe other characteristics of the invention or variants to the main inventive idea.
- In accordance with the above purpose, a method according to the present invention is used for manufacturing steel casts, in particular but not exclusively for manufacturing manganese steel casts intended to obtain wear elements.
- The method comprises at least a step of making at least a reinforcement insert, a step of preparing a mold for the cast to be manufactured, and a subsequent step of casting the steel inside the mold.
- According to one feature of the present invention, the reinforcement insert is made by compacting an amorphous mass of hardening powder in a desired geometric shape. The compacting is obtained by means of sintering techniques with a selective and localized melting comprising one or another of the techniques identified as EBM (Electron Beam Melting), SLM (Selective Laser Melting), or other similar or comparable techniques. The amorphous mass of hardening powder is obtained by mixing powders of pure elements, or of compounds that form carbides and/or micro-structures of great hardness, which due to the effect of the melting generate carbides and/or micro-structures of great hardness.
- These techniques have the advantage that they allow to form almost any geometric shape, developed in three dimensions according to specific requirements.
- The techniques described above allow to obtain complex shapes with variable geometries, starting directly from the amorphous mass of powder, because they are techniques of the adaptive type and obtain localized melting of the powder only in the zones affected by a high energy beam.
- Thanks to the high energy intensity and the compacting to which the hardening powder is subjected, they also allow to obtain reinforcement inserts that are substantially without residual porosity and tensions.
- Making reinforcement inserts with EBM or SLM techniques or similar also has the other advantage of obtaining a rapid and accurate process, and also allows to obtain reinforcement inserts starting from powders of high-melting materials, for example tungsten, titanium, molybdenum, advantageously usable pure or alloyed in iron alloys, which, after the chemical reactions that are triggered due to the effect of the type of melting, give rise to carbides or other hard micro-structures.
- The method according to the present invention provides that the mold preparation step comprises a sub-step of positioning at least one reinforcement insert inside the mold. In order to allow a desired stable positioning of the reinforcement insert inside the mold, when the reinforcement insert is made, at least one appendix is also made in a piece therewith, with the function of anchoring the reinforcement insert to the mold.
- According to a variant of the present invention, during the making of the reinforcement insert, through or blind or reciprocally intersecting channels are made, to promote the anchoring of the reinforcement insert to the steel cast during the casting step.
- According to another feature of the invention, the sintering techniques melt the powders of pure elements, or compounds that form carbides and/or micro-structures of great hardness, triggering chemical reactions to generate carbides and/or micro-structures of great hardness, uniformly and homogeneously distributed inside the reinforcement insert and defining a homogeneous micro-structure of the latter.
- The carbides make the reinforcement insert uniformly hard and resistant to wear, and suitable to confer these properties throughout the volume of the zones of the cast into which it is inserted.
- The present invention also concerns a steel cast, in order to obtain a wear element, manufactured according to the method described above. The cast has overall a heterogeneous micro-structure and hardness, defined by at least one reinforcement insert integrated into the steel cast during the casting of the steel in a mold.
- According to a characteristic feature of the cast, the reinforcement insert has a homogeneous micro-structure comprising carbides and/or structures of great hardness, and is obtained with sintering techniques with a selective and localized melting comprising one or the other of the following techniques: EBM (Electron Beam Molding), SLM (Selective Laser Melting), or other similar or comparable techniques.
- The cast can comprise simple or mixed carbides, or complex aggregations of carbides. The carbides confer, uniformly in the zones where the insert is applied, hardness and resistance to wear on the cast that incorporates it, and consequently on the wear element that is made from it.
- During the casting step, the reinforcement insert is partly melted, which advantageously allows an intimate welding with the cast steel, to confer on the cast obtained a homogeneous macro-structure.
- These and other characteristics of the present invention will become apparent from the following description of a preferential form of embodiment, given as a non-restrictive example with reference to the attached drawings wherein:
-
FIG. 1 is a schematic representation of one form of embodiment of a method according to the present invention; -
FIG. 2 is a variant of a detail ofFIG. 1 ; -
FIG. 3 shows schematically a cast according to the present invention. - With reference to
FIG. 1 , amethod 10 for manufacturing steel casts 110, advantageously but not exclusively manganese steel, according to the present invention, allows to obtaincasts 110 having a heterogeneous micro-structure. - The
method 10 provides that in a preparation step 11 amold 11 is made for everycast 110, that in asubsequent casting step 12 molten manganese steel is cast inside themold 111 and that in a standby step thecast 110 solidifies. - During the
preparation step 11, a plurality ofperimeter walls 112 are made, in this case for example with olivine sand and binder additives, which delimit aninternal cavity 113. Anupper opening 114 puts theinternal cavity 113 in communication with the outside of themold 111 and allows the molten steel to enter into theinternal cavity 113 during the castingstep 12. - The
preparation step 11 comprises a sub-step 14 of positioning at least onereinforcement insert 115 inside theinternal cavity 113 of themold 111. - A
step 15 of making the reinforcement insert 115 (FIG. 1 ) is performed prior to thestep 11 of preparing themold 111, and provides that thereinforcement insert 115 is made by sintering a hardeningpowder 118. - Sintering provides an initial compacting of the hardening
powder 118, which is then at least partly melted using high density energy, and subsequently re-solidified. - The hardening
powder 118 is for example iron-based and also contains compounds containing chromium and/or titanium, or other elements similar to carbon, which, melting due to the high energy, can obtain alloys with simple or mixed carbides, or complex aggregations of carbides and/or micro-structures of great hardness. - The hardening
powder 118 can be defined, for example, by a mixture of powders of pure elements, such as for example carbon, tungsten, chromium, iron, or powders of iron alloys containing said elements and others, such as for example titanium, molybdenum, boron or vanadium. - A first formulation of the present invention provides that, as well as iron-based powder, the hardening
powder 118 comprises the following components: - carbon in a percentage comprised between 2.5% and 3.5%;
- chromium in a percentage comprised between 20% and 30%;
- to which can be added, depending on the other characteristics to be obtained, the following optional components:
- molybdenum in a percentage comprised between 0.1% and 1%;
- tungsten in a percentage comprised between 0.1% and 0.5%.
- A second formulation of the present invention provides that, as well as iron-based powder, the hardening
powder 118 comprises the following components: - carbon in a percentage comprised between 0.5% and 1.0%;
- chromium in a percentage comprised between 10% and 15%; to which can be added the following optional components:
- molybdenum in a percentage comprised between 0.1% and 1%;
- vanadium in a percentage comprised between 0.2% and 1.5%;
- boron in a percentage comprised between 0.001% and 0.015%.
- According to a third formulation of the present invention, as well as iron-based powder, the hardening
powder 118 comprises the following components: - carbon in a percentage comprised between 0.3% and 0.5%;
- chromium in a percentage comprised between 4% and 5%;
- molybdenum in a percentage comprised between 0.5% and 1.5%.
- Other formulations of the mixtures can be obtained as simple applications of the base lines indicated above.
- The formulation of the hardening
powder 118 can be established, according to specific requirements, by selecting on each occasion the powders of elements and/or compounds to be used, based on the carbides and/or micro-structures of great hardness that are to be obtained for thereinforcement insert 115. - The hardening
powder 118 is treated in a sintering machine, in which the structure and geometric shape of thereinforcement insert 115 are defined, starting from the hardeningpowder 118. - To this purpose, sintering techniques with a selective and localized melting, such as for example EBM (Electron Beam Melting), or SLM (Selective Laser Melting), but also other techniques of the additive type, or other techniques similar or comparable to these, may be used.
- Hereafter in the description, by way of example, we shall refer to EBM and SLM techniques, however the following considerations shall also apply to other similar techniques.
- EBM or SLM techniques allow to obtain the desired
reinforcement insert 115 with hardeningpowder 118, by the localized melting of specific areas of the latter, which is initially in the form of a mass of amorphous powder. - The high energy density reached with EBM or SLM techniques allows to melt and then sinter powders of high-melting materials, such as for example titanium, tungsten and molybdenum as above.
- Following melting, the elements or compounds that make up the hardening
powder 118 join together to make alloys. The compounds made due to the melting are the result of chemical reactions triggered by the high energy administered locally and which follow the laws of aggregation according to Gibbs' free energy. These compounds are essentially hard and made up of aggregations of carbides, simple or mixed, and/or micro-structures of great hardness, for example martensitic. - Since the EBM or SLM techniques allow to obtain carbides as indicated above, it is not necessary—and indeed it may even be disadvantageous—to use a hardening
powder 118 containing already formed carbides. - The primary function of sintering by means of EBM or SLM is therefore to determine the micro-structure of the
reinforcement insert 115, triggering chemical reactions starting from the base components. - This advantageously allows to obtain a hard micro-structure and at the same time homogeneous inside the
whole reinforcement insert 115. - Obtaining the
reinforcement insert 115 is controlled and managed by a control unit that cooperates with a melting device to obtain the desired geometric shapes. - The sintering techniques described above advantageously allow to make reinforcement inserts 115 of any geometric shape, developed in the three spatial dimensions according to the specific requirements of the
cast 110 to be obtained. In fact, since they are additive techniques, they allow to obtain, quickly and precisely, quite complex and difficult three-dimensional geometrical developments that are even impossible to obtain using chip-removal operations, or by molding, or using traditional sintering techniques. - In fact, according to the invention, the reinforcement inserts 115 can have internal channels, intersecting or not, in which the melted steel can penetrate during the casting
step 12, to create a better and more stable connection between thereinforcement insert 115 and molten steel. -
FIG. 2 shows, by way of example, a variant of thereinforcement insert 115, in this case shaped as a flat spiral. - Other spatial forms of
reinforcement insert 115 can be made, according to the point-by-point requirements of the final product. - During the
positioning sub-step 14 of thereinforcement insert 115, an anchoring operation is also carried out, during which it is anchored at least to one of theperimeter walls 112 of themold 111. To this purpose, thereinforcement insert 115 comprises, at its ends, one ormore appendixes 120, which function as anchoring means and which are inserted inside thecorresponding perimeter walls 112. - This stratagem allows the
reinforcement insert 115 to remain in the correct position also during thesubsequent casting step 12, during which it is completely incorporated in the manganese steel matrix that is cast into themold 111. -
FIG. 3 shows an example of acast 110 showing the incorporated position of thereinforcement insert 115. - By controlling the sintering process, the use of EBM or SLM techniques allows to obtain reinforcement inserts 115 which are not only micro-structurally homogeneous but also substantially without residual porosity and tensions, and therefore advantageously compact and resistant.
- Furthermore, the reinforcement inserts 115 thus obtained do not need heat treatments after they have been made, and therefore can be put into the
mold 111 immediately after sintering. - During the
casting step 12, depending on the components, eachreinforcement insert 115 can be subjected to partial melting which, during the subsequent solidification, allows to obtain acast 110 that is macro-structurally homogeneous, due to the welding of the cast steel and the melted part of thereinforcement insert 115. - The
cast 110 obtained maintains a generally heterogeneous micro-structure, which has a greater hardness in correspondence with the zones concerned with thereinforcement insert 115, which is uniformly distributed in them and constant, that is, without point-by-point variations. - The
reinforcement insert 115 can be analyzed using microscopic analysis, whether optical or, better, electronic, by scanning or transmission. - Once the solidification of the
cast 110 is terminated, after the stand-by step 13, subsequent heat treatments allow, for example by inducing martensitic transformations inside thecast 110, to confer more hardness on the zones that have the reinforcement inserts 115. - It is clear that modifications and/or additions of parts may be made to the
method 10 and cast 110 as described heretofore, without departing from the field and scope of the present invention. - It is also clear that, although the present invention has been described with reference to some specific examples, a person of skill in the art shall certainly be able to achieve many other equivalent forms of
cast 110, having the characteristics as set forth in the claims and hence all coming within the field of protection defined thereby.
Claims (5)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000159A ITUD20120159A1 (en) | 2012-09-14 | 2012-09-14 | PROCEDURE FOR THE MANUFACTURE OF STEEL JETS |
ITUD2012A000159 | 2012-09-14 | ||
PCT/IB2013/001904 WO2014041409A2 (en) | 2012-09-14 | 2013-09-04 | Method for manufacturing steel casts |
Publications (1)
Publication Number | Publication Date |
---|---|
US20150246391A1 true US20150246391A1 (en) | 2015-09-03 |
Family
ID=47138118
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14/428,336 Abandoned US20150246391A1 (en) | 2012-09-14 | 2013-09-04 | Method for Manufacturing Steel Casts |
Country Status (9)
Country | Link |
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US (1) | US20150246391A1 (en) |
EP (1) | EP2916978B1 (en) |
BR (1) | BR112015005687A2 (en) |
CA (1) | CA2884928C (en) |
ES (1) | ES2710100T3 (en) |
IT (1) | ITUD20120159A1 (en) |
PT (1) | PT2916978T (en) |
TR (1) | TR201901636T4 (en) |
WO (1) | WO2014041409A2 (en) |
Cited By (8)
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CN105618751A (en) * | 2015-12-16 | 2016-06-01 | 伊特克斯惰性气体系统(北京)有限公司 | Selective laser melting system protected by ultra-pure atmosphere |
CN106041031A (en) * | 2016-07-29 | 2016-10-26 | 河海大学常州校区 | Preparation method of high-entropy alloy coating layer on surface of casting |
DE102016211358A1 (en) * | 2016-06-24 | 2017-12-28 | Bayerische Motoren Werke Aktiengesellschaft | Casting component and method for producing a cast component |
US10173258B2 (en) | 2014-04-30 | 2019-01-08 | Daido Steel Co., Ltd. | Steel for mold, and mold |
WO2019094210A1 (en) | 2017-11-10 | 2019-05-16 | Divergent Technologies, Inc. | Structures and methods for high volume production of complex structures using interface nodes |
CN110090940A (en) * | 2018-01-31 | 2019-08-06 | 戴弗根特技术有限公司 | System and method for casting the interface node of increasing material manufacturing jointly |
CN113000822A (en) * | 2021-02-03 | 2021-06-22 | 邯郸慧桥复合材料科技有限公司 | Ceramic reinforced Fe-B alloy and preparation method thereof |
CN113290230A (en) * | 2020-02-24 | 2021-08-24 | 北京兆牌科技发展有限公司 | Design method for pre-arranged hard surfaces and hard points of cast product and corresponding casting |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2098112A (en) * | 1981-04-27 | 1982-11-17 | Kennametal Inc | Casting incorporating hard, e.g. wear-resistant, insert |
US5066546A (en) * | 1989-03-23 | 1991-11-19 | Kennametal Inc. | Wear-resistant steel castings |
US20040216860A1 (en) * | 2003-04-16 | 2004-11-04 | Rolf Pfeifer | Ceramic casting mold for casting metal and process for production thereof |
US20070128462A1 (en) * | 2003-08-20 | 2007-06-07 | F.A.R. - Fonderie Acciaierie Roiale-Spa | Method to produce an element subject to wear, and element subject to wear thus obtained |
US20080008894A1 (en) * | 2006-07-06 | 2008-01-10 | Siemens Power Generation, Inc. | Rapid prototyping of ceramic articles |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4140170A (en) * | 1977-09-06 | 1979-02-20 | Baum Charles S | Method of forming composite material containing sintered particles |
DE4214524A1 (en) * | 1991-05-06 | 1992-12-24 | Karl Lange | Casting insect to produce wear-protected castings - comprises perforated steel sheets with carbide balls in perforations between sheets |
US5267600A (en) * | 1992-01-21 | 1993-12-07 | Deere & Company | Hard facing casting surfaces with wear-resistant sheets |
US8007373B2 (en) * | 2009-05-19 | 2011-08-30 | Cobra Golf, Inc. | Method of making golf clubs |
IT1401763B1 (en) * | 2010-07-09 | 2013-08-02 | Far Fonderie Acciaierie Roiale S P A | PROCEDURE FOR THE PRODUCTION OF AN ELEMENT SUBJECT TO WEAR, ITEM SUBJECT TO WEAR AND TEMPORARY AGGREGATION STRUCTURE FOR THE MANUFACTURE OF SUCH ITEM SUBJECT TO WEAR |
-
2012
- 2012-09-14 IT IT000159A patent/ITUD20120159A1/en unknown
-
2013
- 2013-09-04 WO PCT/IB2013/001904 patent/WO2014041409A2/en active Application Filing
- 2013-09-04 ES ES13785597T patent/ES2710100T3/en active Active
- 2013-09-04 PT PT13785597T patent/PT2916978T/en unknown
- 2013-09-04 BR BR112015005687A patent/BR112015005687A2/en active IP Right Grant
- 2013-09-04 CA CA2884928A patent/CA2884928C/en active Active
- 2013-09-04 US US14/428,336 patent/US20150246391A1/en not_active Abandoned
- 2013-09-04 EP EP13785597.9A patent/EP2916978B1/en active Active
- 2013-09-04 TR TR2019/01636T patent/TR201901636T4/en unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2098112A (en) * | 1981-04-27 | 1982-11-17 | Kennametal Inc | Casting incorporating hard, e.g. wear-resistant, insert |
US5066546A (en) * | 1989-03-23 | 1991-11-19 | Kennametal Inc. | Wear-resistant steel castings |
US20040216860A1 (en) * | 2003-04-16 | 2004-11-04 | Rolf Pfeifer | Ceramic casting mold for casting metal and process for production thereof |
US20070128462A1 (en) * | 2003-08-20 | 2007-06-07 | F.A.R. - Fonderie Acciaierie Roiale-Spa | Method to produce an element subject to wear, and element subject to wear thus obtained |
US20080008894A1 (en) * | 2006-07-06 | 2008-01-10 | Siemens Power Generation, Inc. | Rapid prototyping of ceramic articles |
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DE102016211358A1 (en) * | 2016-06-24 | 2017-12-28 | Bayerische Motoren Werke Aktiengesellschaft | Casting component and method for producing a cast component |
CN106041031A (en) * | 2016-07-29 | 2016-10-26 | 河海大学常州校区 | Preparation method of high-entropy alloy coating layer on surface of casting |
EP3706981A4 (en) * | 2017-11-10 | 2021-10-27 | Divergent Technologies Inc. | Structures and methods for high volume production of complex structures using interface nodes |
WO2019094210A1 (en) | 2017-11-10 | 2019-05-16 | Divergent Technologies, Inc. | Structures and methods for high volume production of complex structures using interface nodes |
CN109759583A (en) * | 2017-11-10 | 2019-05-17 | 戴弗根特技术有限公司 | Structure and for using interface node come high yield production labyrinth method |
US11786971B2 (en) | 2017-11-10 | 2023-10-17 | Divergent Technologies, Inc. | Structures and methods for high volume production of complex structures using interface nodes |
JP2021502269A (en) * | 2017-11-10 | 2021-01-28 | ダイバージェント テクノロジーズ, インコーポレイテッドDivergent Technologies, Inc. | Structures and methods for mass production of complex structures using interface nodes |
JP7182620B2 (en) | 2017-11-10 | 2022-12-02 | ダイバージェント テクノロジーズ, インコーポレイテッド | Structures and methods for mass production of complex structures using interface nodes |
WO2019152100A1 (en) * | 2018-01-31 | 2019-08-08 | Divergent Technologies, Inc. | Systems and methods for co-casting of additively manufactured interface nodes |
US11420262B2 (en) | 2018-01-31 | 2022-08-23 | Divergent Technologies, Inc. | Systems and methods for co-casting of additively manufactured interface nodes |
JP2021511966A (en) * | 2018-01-31 | 2021-05-13 | ダイバージェント テクノロジーズ, インコーポレイテッドDivergent Technologies, Inc. | Systems and methods for co-casting additionally manufactured interface nodes |
CN110090940A (en) * | 2018-01-31 | 2019-08-06 | 戴弗根特技术有限公司 | System and method for casting the interface node of increasing material manufacturing jointly |
CN113290230A (en) * | 2020-02-24 | 2021-08-24 | 北京兆牌科技发展有限公司 | Design method for pre-arranged hard surfaces and hard points of cast product and corresponding casting |
CN113000822A (en) * | 2021-02-03 | 2021-06-22 | 邯郸慧桥复合材料科技有限公司 | Ceramic reinforced Fe-B alloy and preparation method thereof |
Also Published As
Publication number | Publication date |
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EP2916978A2 (en) | 2015-09-16 |
CA2884928C (en) | 2020-09-29 |
BR112015005687A2 (en) | 2017-10-10 |
PT2916978T (en) | 2019-02-08 |
ITUD20120159A1 (en) | 2014-03-15 |
TR201901636T4 (en) | 2019-02-21 |
WO2014041409A2 (en) | 2014-03-20 |
ES2710100T3 (en) | 2019-04-23 |
CA2884928A1 (en) | 2014-03-20 |
WO2014041409A3 (en) | 2014-06-12 |
EP2916978B1 (en) | 2018-11-07 |
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