EP2323770A1 - Composite impactor for percussion crushers - Google Patents
Composite impactor for percussion crushersInfo
- Publication number
- EP2323770A1 EP2323770A1 EP09814104A EP09814104A EP2323770A1 EP 2323770 A1 EP2323770 A1 EP 2323770A1 EP 09814104 A EP09814104 A EP 09814104A EP 09814104 A EP09814104 A EP 09814104A EP 2323770 A1 EP2323770 A1 EP 2323770A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- titanium carbide
- impactor
- micrometric
- granules
- zones
- 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.)
- Granted
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 17
- 238000009527 percussion Methods 0.000 title abstract description 5
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 claims abstract description 76
- 239000002245 particle Substances 0.000 claims abstract description 50
- 239000008187 granular material Substances 0.000 claims description 81
- 239000010936 titanium Substances 0.000 claims description 47
- 238000006243 chemical reaction Methods 0.000 claims description 36
- 230000002787 reinforcement Effects 0.000 claims description 27
- 229910052799 carbon Inorganic materials 0.000 claims description 25
- 229910052719 titanium Inorganic materials 0.000 claims description 25
- 229910045601 alloy Inorganic materials 0.000 claims description 24
- 239000000956 alloy Substances 0.000 claims description 24
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 22
- 238000005266 casting Methods 0.000 claims description 22
- 239000000203 mixture Substances 0.000 claims description 22
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 18
- 239000000843 powder Substances 0.000 claims description 18
- 230000015572 biosynthetic process Effects 0.000 claims description 17
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 claims description 16
- 238000003786 synthesis reaction Methods 0.000 claims description 15
- 238000001764 infiltration Methods 0.000 claims description 12
- 230000008595 infiltration Effects 0.000 claims description 12
- 238000004519 manufacturing process Methods 0.000 claims description 11
- 239000002243 precursor Substances 0.000 claims description 8
- 239000010439 graphite Substances 0.000 claims description 3
- 229910002804 graphite Inorganic materials 0.000 claims description 3
- -1 titanium carbides Chemical class 0.000 claims description 3
- 239000012141 concentrate Substances 0.000 claims 1
- 229910001021 Ferroalloy Inorganic materials 0.000 abstract 2
- 238000005056 compaction Methods 0.000 description 31
- 239000000463 material Substances 0.000 description 21
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 16
- 229910052751 metal Inorganic materials 0.000 description 14
- 239000002184 metal Substances 0.000 description 14
- 238000000034 method Methods 0.000 description 12
- 239000011159 matrix material Substances 0.000 description 8
- 230000003014 reinforcing effect Effects 0.000 description 7
- 239000003153 chemical reaction reagent Substances 0.000 description 6
- 239000010959 steel Substances 0.000 description 6
- 229910001018 Cast iron Inorganic materials 0.000 description 5
- 229910052742 iron Inorganic materials 0.000 description 5
- 239000011435 rock Substances 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 230000008602 contraction Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000008188 pellet Substances 0.000 description 4
- 238000004064 recycling Methods 0.000 description 3
- 239000004576 sand Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 229910001208 Crucible steel Inorganic materials 0.000 description 2
- 229910000760 Hardened steel Inorganic materials 0.000 description 2
- 235000019738 Limestone Nutrition 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 239000004568 cement Substances 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 239000010419 fine particle Substances 0.000 description 2
- 238000005469 granulation Methods 0.000 description 2
- 230000003179 granulation Effects 0.000 description 2
- 239000006028 limestone Substances 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000007873 sieving Methods 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910001311 M2 high speed steel Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 230000004807 localization Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000000376 reactant Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B02—CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
- B02C—CRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
- B02C13/00—Disintegrating by mills having rotary beater elements ; Hammer mills
- B02C13/26—Details
- B02C13/28—Shape or construction of beater elements
-
- 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
- B22D19/14—Casting in, on, or around objects which form part of the product the objects being filamentary or particulate in form
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B02—CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
- B02C—CRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
- B02C2210/00—Codes relating to different types of disintegrating devices
- B02C2210/02—Features for generally used wear parts on beaters, knives, rollers, anvils, linings and the like
Definitions
- the present invention relates to a composite impactor for impact crushers.
- Percussion crushers grouping crushing machines for rocks and hard materials such as hammer crushers, crushers, vertical axis crushers, etc. These machines are used extensively in the first and second stages of a production line designed to drastically reduce the dimension of rock in the extractive industries
- impactor for impact crushers is to be interpreted in the broad sense, namely a composite wear part whose function is to be in direct contact with the rock or the material to be grinded during the first phase. process where these rocks and materials are subjected to extremely violent impacts intended to fragment them.
- impactor therefore includes hammers and beaters but also fixed armor plates undergoing the impacts of materials projected against them.
- EP 0 476 496 proposes the use of a hard insert mechanically crimped into a hammer body made of a ductile steel.
- EP 1 651 389 (Mayer) also discloses a hammer making technique employing two different materials, one being arranged in the form of a prefabricated insert disposed in the other material at the place where the piece is the most solicited.
- Document US 2008/041993 proposes the use of inserts very hard material, fixed to the hammer on its working side.
- US 6,066,407 discloses a reinforced composite impactor with carbides.
- the present invention discloses a composite impactor for impact crushers having improved wear resistance while maintaining good impact resistance. This property is obtained by a composite reinforcement structure specifically designed for this application, a material that alternates on a millimeter scale dense zones in fine micrometric globular particles of metal carbides with zones that are practically free of them within the metallic matrix. of the impactor.
- the present invention also provides a method for obtaining said reinforcement structure.
- the present invention discloses a composite impactor for impact crushers, said impactor comprising a ferrous alloy reinforced at least in part with titanium carbide according to a defined geometry, wherein said reinforced portion comprises a macro- alternating microstructure of millimetric zones of millimetric zones concentrated in micrometric globular particles of titanium carbide separated by millimetric zones substantially free of micrometric globular particles of titanium carbide, micrometrically concentrated micrometric micrometric particles of micrometric titanium carbide particles in which the micrometric interstices between said globular particles are also occupied by said ferrous alloy.
- the composite impactor comprises at least one or a suitable combination of the following characteristics:
- said concentrated millimetric zones have a concentration of titanium carbides greater than 36.9% by volume
- said reinforced portion has an overall titanium carbide content of between 16.6 and 50.5% by volume;
- micrometric globular particles of titanium carbide have a size of less than 50 ⁇ m
- micrometric globular particles of titanium carbide have a size of less than 20 ⁇ m;
- zones concentrated in globular particles of titanium carbide comprise 36.9 to 72.2% by volume of titanium carbide
- said millimetric zones which are concentrated in titanium carbide, have a size ranging from 1 to 12 mm;
- said millimetric zones which are concentrated in titanium carbide, have a size ranging from 1 to 6 mm;
- said concentrated zones made of titanium carbide have a dimension varying from 1.4 to 4 mm.
- the present invention also discloses a method of manufacturing the composite impactor according to any one of claims 1 to 9 comprising the following steps:
- the method comprises at least one or a suitable combination of the following characteristics:
- compacted powders of titanium and carbon comprise a powder of a ferrous alloy
- said carbon is graphite.
- the present invention also discloses a composite impactor obtained according to the method of any one of claims 11 to 13. Brief description of the figures
- Figure 1 shows a horizontal axis crusher in which the impactors of the present invention are used.
- Figure 2 shows a vertical axis crusher in which the impactors of the present invention are also used.
- Figure 3 shows an impactor / hammer of the prior art without reinforcement.
- Figures 4a and 4b show a hammer with two types of reinforcement possible. This reinforcing geometry is of course not limiting.
- FIG. 5a-5h shows schematically the method of manufacturing a hammer according to the invention.
- step 5a shows the device for mixing the titanium and carbon powders;
- Step 5b shows the compaction of the powders between two rollers followed by crushing and sieving with recycling of the fine particles
- FIG. 5c shows a sand mold in which a dam has been placed to contain the granules of compacted powder at the location of the reinforcement of the impactor (hammer);
- FIG. 5d shows an enlargement of the reinforcement zone in which the compacted granules comprising TiC precursor reactants are found
- Step 5e shows the casting of the ferrous alloy in the mold
- FIG. 5g shows an enlargement of the zones with a high concentration of TiC nodules
- FIG. 5h shows an enlargement within the same zone with a high concentration of TiC nodules.
- the micrometric nodules are individually surrounded by the casting metal.
- FIG. 6 shows a binocular view of a polished, unengaged surface of a section of the reinforced portion of an impactor according to the invention with millimetric zones (in light gray) concentrated in titanium carbide.
- micrometric globular (nodules of TiC) The dark part represents the metal matrix (steel or cast iron) filling at the same time the space between these concentrated micrometric globular titanium carbide zones but also the spaces between the globules themselves.
- FIG. 7 and 8 show SEM electron microscope views of micrometric globular titanium carbide on polished and untouched surfaces at different magnifications. We see that in this particular case most of the globules of titanium carbide have a size less than 10 microns.
- FIG. 9 represents a view of micrometric globular titanium carbide on a fracture surface taken by SEM electron microscope. It can be seen that the globules of titanium carbide are perfectly incorporated in the metal matrix. This proves that the casting metal completely infiltrates (impregnates) the pores during casting once the chemical reaction between titanium and carbon is initiated.
- FIG. 10 schematically represents the zones of reinforcement on a hammer impactor.
- the reinforced corners are similar to those of FIG. 4b and the diagrammatic enlargement of the reinforcement zones makes it possible to show the reinforcement macro-microstructure according to the invention.
- the reactive powder mixtures comprise carbon powder and titanium powder and are compressed into plates and then crushed in order to obtain granules whose size varies from 1 to 12 mm, preferably from 1 to 12 mm. 6 mm, and particularly preferably from 1.4 to 4 mm. These granules are not 100% compacted. They are generally compressed between 55 and 95% of the theoretical density. These granules allow easy use / handling (see Fig. 3a-3h).
- These millimetric granules of mixed carbon and titanium powders obtained according to the diagrams of FIG. 3a-3h constitute the precursors of the titanium carbide to be created and make it possible to easily fill mold parts of various or irregular shapes. These granules can be held in place in the mold 15 by means of a dam 16, for example. The shaping or assembly of these granules can also be done using an adhesive.
- the composite impactor according to the present invention has a reinforcing macro-microstructure that can also be called alternating structure of concentrated zones in micrometric globular particles of titanium carbide separated by zones which are practically free. Such a structure is obtained by the reaction in the mold of the granules comprising a mixture of powders of carbon and titanium.
- This reaction is initiated by the heat of casting of the cast iron or steel used to pour the whole piece and thus both the unreinforced part and the reinforced part (see Fig. 3e).
- the casting therefore triggers an exothermic reaction of self-propagating synthesis at high temperature of the mixture of powders of carbon and titanium compacted in the form of granules (self-propagating high-temperature synthesis - SHS) and previously placed in the mold 15.
- SHS high temperature synthesis
- This high temperature synthesis allows easy infiltration of all millimetric and micrometric interstices by cast iron or casting steel (Fig. 5g & 5h). By increasing the wettability, the infiltration can be done on any thickness or depth of reinforcement of the impactor.
- the reinforcement zones with a high concentration of titanium carbide are composed of globular micrometer particles of TiC in significant percentage (between about 35 and about 70% by volume) and the ferrous alloy infiltration.
- micrometric globular particles are meant globally spheroidal particles which have a size ranging from microns to a few tens of microns at most, the vast majority of these particles having a size of less than 50 microns, and even at 20 microns. or even 10 ⁇ m.
- TiC globules This globular form is characteristic of a method for obtaining titanium carbide by self-propagating SHS synthesis (see Fig. 8).
- the process for obtaining the granules is illustrated in Figure 5a-5h.
- the granules of carbon / titanium reagents are obtained by compaction between rollers 10 in order to obtain strips that are then crushed in a crusher 11.
- the mixture of the powders is made in a mixer 8 consisting of a tank equipped with blades , to promote homogeneity.
- the mixture then passes into a granulation apparatus through a hopper 9.
- This machine comprises two rollers 10, through which the material is passed. Pressure is applied to these rollers 10, which compresses the material. We get at the exit a band of material compressed which is then crushed to obtain the granules.
- These granules are then sieved to the desired particle size in a sieve 13.
- the apparent density of the granules is 3.75 x 0.55, ie 2.06 g / cm 3 .
- a density on the bands of 90% of the theoretical density is obtained, ie an apparent density of 3.38 g / cm 3 .
- the granules obtained from the raw material Ti + C are porous. This porosity varies from 5% for highly compressed granules, to 45% for slightly compressed granules.
- the granules obtained overall a size between 1 and 12 mm, preferably between 1 and 6 mm, and particularly preferably between 1.4 and 4 mm.
- the granules are made as described above. To obtain a three-dimensional structure or superstructure / macro-microstructure with these granules, they are placed in the areas of the mold where it is desired to reinforce the workpiece. This is achieved by agglomerating the granules either by means of an adhesive, or by confining them in a container, or by any other means (dam 16).
- the bulk density of the stack of Ti + C granules is measured according to ISO 697 and depends on the level of compaction of the bands, the granulometric distribution of the granules and the crushing mode of the bands, which influences the shape of the granules .
- the bulk density of these Ti + C granules is generally of the order of 0.9 g / cm 3 to 2.5 g / cm 3 depending on the level of compaction of these granules and the density of the stack.
- Granulation was carried out with a Sahut-Conreur granulator.
- the compactness of the granules was obtained by varying the pressure between the rolls by 10 to 250 ⁇ 10 5 Pa.
- Example 1 The reinforcement was carried out by placing granules in a metal container, which is then judiciously placed in the mold where the impactor is likely to be reinforced. Then we cast the steel or cast in this mold.
- Example 1 The reinforcement was carried out by placing granules in a metal container, which is then judiciously placed in the mold where the impactor is likely to be reinforced. Then we cast the steel or cast in this mold.
- the granules are placed in the mold at the location of the part to be reinforced, which thus comprises 65% by volume of porous granules.
- a chromium cast iron (3% C, 25% Cr) is then cast at about 1500 ° C. in a non-preheated sand mold.
- the reaction between Ti and C is initiated by the heat of melting. This casting is done without a protective atmosphere.
- 65% by volume of zones with a high concentration of approximately 65% of globular titanium carbide are obtained, ie 42% by global volume of TiC in the reinforced part of the impactor.
- Example 2 it is intended to provide an impactor whose reinforced zones comprise an overall volume percentage of TiC of approximately 30%.
- a 70% compaction band is made of the theoretical density of a mixture of C and Ti.
- the granules are sieved to obtain a pellet size of between 1.4 and 4 mm.
- a bulk density of about 1.4 g / cm 3 (45% of space between the granules + 30% of porosity in the granules) is obtained.
- the granules are available in the section strengthen which thus comprises 55% by volume of porous granules.
- 55% by volume of zones with a high concentration of approximately 53% of globular titanium carbide is obtained, ie approximately 30% by global volume of TiC in the reinforced part of the impactor.
- Example 3 it is intended to provide an impactor whose reinforced zones comprise an overall volume percentage of TiC of about 20%.
- a band is made by compaction at 60% of the theoretical density of a mixture of C and Ti. After crushing, the granules are sieved so as to obtain a granule size of 1 and 6 mm. A bulk density of the order of 1.0 g / cm 3 (55% of space between the granules + 40% of porosity in the granules) is obtained. The granules are placed in the part to be reinforced, which thus comprises 45% by volume of porous granules. After reaction, in the reinforced part 45% by volume of concentrated zones with approximately 45% of globular titanium carbide is obtained, ie 20% by global volume of TiC in the reinforced part of the impactor.
- Example 2 it was sought to attenuate the intensity of the reaction between carbon and titanium by adding a ferrous alloy powder.
- it is intended to provide an impactor whose reinforced zones comprise a global volume percentage of TiC of about 30%.
- a compaction band is produced at 85% of the theoretical density of a mixture by weight of 15% of C, 63% of Ti and 22% of Fe.
- the granules are sieved to obtain a granule size between 1.4 and 4 mm.
- a bulk density of the order of 2 g / cm 3 (45% of space between the granules + 15% of porosity in the granules) is obtained.
- the granules are placed in the part to be reinforced, which thus comprises 55% by volume of porous granules. After reaction, 55% by volume of zones with a high concentration of approximately 55% of globular titanium carbide, ie 30% by volume of global titanium carbide in the reinforced macro-microstructure of the compound, are obtained in the reinforced part. impactor.
- part 70 1 .4 1 .6 1 .7 1 .8 2 2 1 2 2 2.4 2 5 reinforced part in% vol 65 1 .3 * 1 .5 1 .6 1 .7 1 .8 2 0 2 1 2.2 2 3
- millimetric granules are themselves composed of microscopic particles of TiC globular tendency also crimped in the alloy metallic infiltration. This system makes it possible to obtain an impactor with a reinforcement zone comprising a macrostructure within which there is an identical microstructure on a scale approximately a thousand times smaller.
- the reinforcing zone of the impactor comprises small globular particles of titanium carbide, hard and finely dispersed in a metal matrix which surrounds them, makes it possible to prevent the formation and propagation of cracks (see FIG. 4 & 6). There is thus a double dissipative system of cracks.
- the cracks generally originate at the most fragile places, which are in this case the TiC particle or the interface between this particle and the infiltration metal alloy. If a crack originates at the interface or in the micrometric particle of TiC, the propagation of this crack is then impeded by the infiltration alloy which surrounds this particle.
- the toughness of the infiltration alloy is greater than that of the TiC ceramic particle. The crack needs more energy to pass from one particle to another, to cross the micrometric spaces that exist between the particles.
- the coefficient of expansion of the TiC reinforcement is lower than that of the ferrous alloy matrix (TiC expansion coefficient: 7.5 10-6 / K and the ferrous alloy: approximately 12.0 10-6 / K).
- This difference in the expansion coefficients has the consequence of generating tensions in the material during the solidification phase and also during the heat treatment. If these voltages are too great, cracks may appear in the room and lead to scrapping it.
- a small proportion of TiC reinforcement (less than 50% by volume) is used, resulting in less stress in the workpiece.
- the presence of a more ductile matrix between the micrometric globular particles of TiC in alternating zones of low and high concentration makes it possible to better manage any local voltages.
- the boundary between the reinforced part and the unreinforced part of the impactor is not abrupt because there is a continuity of the metal matrix between the part reinforced and the unreinforced part, which allows to protect against a complete tearing of the reinforcement.
- Test 2 weight hammers 70 to 130 kgs crushed material: limestone rock stage: primary increase in the life of the hammer compared to a hardened steel hammer: 100 to 200%
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL09814104T PL2323770T3 (en) | 2008-09-19 | 2009-08-26 | Composite impactor for impact crusher |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE2008/0520A BE1018129A3 (en) | 2008-09-19 | 2008-09-19 | COMPOSITE IMPACTOR FOR PERCUSSION CRUSHERS. |
PCT/EP2009/060981 WO2010031663A1 (en) | 2008-09-19 | 2009-08-26 | Composite impactor for percussion crushers |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2323770A1 true EP2323770A1 (en) | 2011-05-25 |
EP2323770B1 EP2323770B1 (en) | 2013-11-27 |
Family
ID=40578583
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09814104.7A Active EP2323770B1 (en) | 2008-09-19 | 2009-08-26 | Composite impactor for impact crusher |
Country Status (18)
Country | Link |
---|---|
US (1) | US8651407B2 (en) |
EP (1) | EP2323770B1 (en) |
JP (1) | JP5503653B2 (en) |
KR (1) | KR101621996B1 (en) |
CN (1) | CN102176973B (en) |
AU (1) | AU2009294782B2 (en) |
BE (1) | BE1018129A3 (en) |
BR (1) | BRPI0913717B1 (en) |
CA (1) | CA2735877C (en) |
CL (1) | CL2011000576A1 (en) |
DK (1) | DK2323770T3 (en) |
EG (1) | EG26800A (en) |
ES (1) | ES2449440T3 (en) |
MX (1) | MX2011003028A (en) |
PL (1) | PL2323770T3 (en) |
PT (1) | PT2323770E (en) |
WO (1) | WO2010031663A1 (en) |
ZA (1) | ZA201101792B (en) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE1018130A3 (en) * | 2008-09-19 | 2010-05-04 | Magotteaux Int | HIERARCHICAL COMPOSITE MATERIAL. |
CN102310014B (en) * | 2011-08-22 | 2015-09-16 | 宁国市东方碾磨材料有限责任公司 | High performance composite metal hammer |
CN102423799B (en) * | 2011-12-12 | 2013-02-13 | 广东新劲刚超硬材料有限公司 | Method of in situ synthetic steel bond hard alloy casting composite hammerhead and hammerhead |
PL398770A1 (en) * | 2012-04-10 | 2013-01-07 | Akademia Górniczo-Hutnicza im. Stanislawa Staszica | Method for producing the cast composite zones |
US11045813B2 (en) * | 2013-10-28 | 2021-06-29 | Postle Industries, Inc. | Hammermill system, hammer and method |
WO2015117172A1 (en) | 2014-02-10 | 2015-08-13 | Lisec Austria Gmbh | Method for cutting laminated glass |
AU2016352319B2 (en) | 2015-11-12 | 2022-03-10 | Innerco Sp. Z O.O. | Powder composition for the manufacture of casting inserts, casting insert and method of obtaining local composite zones in castings |
PL414755A1 (en) | 2015-11-12 | 2017-05-22 | Innerco Spółka Z Ograniczoną Odpowiedzialnością | Method for producing local composite zones in castings and the casting insert |
US20170233986A1 (en) * | 2016-02-15 | 2017-08-17 | Caterpillar Inc. | Ground engaging component and method for manufacturing the same |
CA3029673A1 (en) | 2016-06-29 | 2018-01-04 | Superior Industries, Inc. | Vertical shaft impact crusher |
JP6804143B2 (en) * | 2016-09-30 | 2020-12-23 | 株式会社小松製作所 | Earth and sand wear resistant parts and their manufacturing methods |
US11001914B2 (en) | 2018-01-23 | 2021-05-11 | Dsc Materials Llc | Machinable metal matrix composite and method for making the same |
US10851020B2 (en) | 2018-01-23 | 2020-12-01 | Dsc Materials Llc | Machinable metal matrix composite and method for making the same |
CN110791677A (en) * | 2019-11-18 | 2020-02-14 | 中国科学院上海硅酸盐研究所 | High-performance wear-resistant bronze-based composite material and preparation method and application thereof |
BE1027444B1 (en) | 2020-02-11 | 2021-02-10 | Magotteaux Int | COMPOSITE WEAR PART |
EP3885061A1 (en) | 2020-03-27 | 2021-09-29 | Magotteaux International S.A. | Composite wear component |
EP3915699A1 (en) | 2020-05-29 | 2021-12-01 | Magotteaux International SA | Ceramic-metal composite wear part |
AU2020457247A1 (en) | 2020-07-07 | 2023-02-02 | Sandvik Srp Ab | A crushing or wear part having a localized composite wear zone |
WO2022122393A1 (en) | 2020-12-10 | 2022-06-16 | Magotteaux International S.A. | Hierarchical composite wear part with structural reinforcement |
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WO2010031663A1 (en) | 2010-03-25 |
CA2735877A1 (en) | 2010-03-25 |
CA2735877C (en) | 2015-12-22 |
MX2011003028A (en) | 2011-04-12 |
US8651407B2 (en) | 2014-02-18 |
PT2323770E (en) | 2014-02-24 |
BRPI0913717A2 (en) | 2015-10-13 |
CL2011000576A1 (en) | 2011-08-26 |
PL2323770T3 (en) | 2014-07-31 |
KR101621996B1 (en) | 2016-05-17 |
EG26800A (en) | 2014-09-17 |
JP2012502789A (en) | 2012-02-02 |
US20110226882A1 (en) | 2011-09-22 |
CN102176973A (en) | 2011-09-07 |
DK2323770T3 (en) | 2014-03-03 |
EP2323770B1 (en) | 2013-11-27 |
BRPI0913717B1 (en) | 2019-11-26 |
ES2449440T3 (en) | 2014-03-19 |
BE1018129A3 (en) | 2010-05-04 |
KR20110081151A (en) | 2011-07-13 |
AU2009294782A1 (en) | 2010-03-25 |
CN102176973B (en) | 2014-02-26 |
ZA201101792B (en) | 2012-08-29 |
JP5503653B2 (en) | 2014-05-28 |
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