EP0575685A1 - Moulage de précision ayant des surfaces d'usure - Google Patents

Moulage de précision ayant des surfaces d'usure Download PDF

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Publication number
EP0575685A1
EP0575685A1 EP92810477A EP92810477A EP0575685A1 EP 0575685 A1 EP0575685 A1 EP 0575685A1 EP 92810477 A EP92810477 A EP 92810477A EP 92810477 A EP92810477 A EP 92810477A EP 0575685 A1 EP0575685 A1 EP 0575685A1
Authority
EP
European Patent Office
Prior art keywords
ceramic
embedded
casting
casting according
porous ceramic
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
Application number
EP92810477A
Other languages
German (de)
English (en)
Other versions
EP0575685B1 (fr
Inventor
Fritz Staub
John Antony Dr. Peters
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sulzer Markets and Technology AG
Original Assignee
Sulzer Innotec AG
Sulzer AG
Gebrueder Sulzer AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sulzer Innotec AG, Sulzer AG, Gebrueder Sulzer AG filed Critical Sulzer Innotec AG
Priority to DE59207902T priority Critical patent/DE59207902D1/de
Priority to AT92810477T priority patent/ATE147669T1/de
Priority to EP92810477A priority patent/EP0575685B1/fr
Priority to JP5149583A priority patent/JPH06170514A/ja
Publication of EP0575685A1 publication Critical patent/EP0575685A1/fr
Application granted granted Critical
Publication of EP0575685B1 publication Critical patent/EP0575685B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/20—Specially-shaped blade tips to seal space between tips and stator
    • 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
    • B22D19/0054—Casting in, on, or around objects which form part of the product rotors, stators for electrical motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00—Casting in, on, or around objects which form part of the product
    • B22D19/08—Casting in, on, or around objects which form part of the product for building-up linings or coverings, e.g. of anti-frictional metal
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • 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
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/10—Alloys containing non-metals
    • C22C1/1036—Alloys containing non-metals starting from a melt

Definitions

  • the invention relates to a method for producing castings with ceramic embedded in composite form, and to castings which are produced by means of such a method.
  • first phase being formed by a base material and a second phase — in a special spatial arrangement — being embedded in the first phase.
  • the base material is often metallic (pure metal or alloy) and the deposits are made of ceramic material.
  • dispersion alloys dispersion-hardened materials
  • the first phase serves as a binder for the ceramic particles of the second phase, which, in terms of volume, makes up the main part of the composite.
  • Cermets are manufactured using powder metallurgy. They are suitable as wear-resistant materials.
  • the ceramic reinforcement of the cast must be provided in the webs, in the area that is worn away by the wear processes.
  • the ceramic inclusions have a macroscopic character in the castings according to the invention.
  • the casting according to the invention is carried out by means of an investment casting process in which meltable or burnable models are used for the production of the molded shell.
  • meltable or burnable models are used for the production of the molded shell.
  • wax is used for the unreinforced parts of the casting wax with advantage for the model.
  • the porous ceramic bodies intended for the reinforcement are integrated into the cast model, the pore spaces of the ceramic bodies being filled beforehand with wax - or instead of wax with a plastic which volatilizes without residue when the molded shell is fired.
  • the porous ceramic body which has a completely communicating pore space and whose ceramic structure forms a three-dimensional network, can be produced in various ways. Three examples of these manufacturing processes are described below.
  • the following ceramic structures result from these processes: 1. a pile of granular particles; 2. a ceramic structure consisting of rib-like and sintered grain-like particles; 3. a ceramic structure with an open-cell foam structure.
  • the base material used is advantageously a stainless steel, as is customary when casting such plates (ASTM CB-30 or X 35 CrMo 17).
  • Nickel-based or cobalt-based alloys can also be used.
  • the ceramic material must be inert to the melt.
  • aluminum oxide (corundum), zirconium oxide or magnesium oxide can be used; Silicon carbide, on the other hand, is unsuitable because this substance reacts with the melt.
  • a refiner plate 1 with webs 10 is shown in detail in FIG.
  • the web surface 15 (the grinding surface) is subjected to wear during the milling of the fibrous material.
  • the wear areas of the webs 10 consist of a steel / ceramic composite 20, in which a porous ceramic body 2 is embedded in cast steel.
  • the base body 11 of the refiner plate 1 and the web base areas have no embedded ceramic; this maintains the high toughness of the cast material in the web roots, where large bending moments occur during grinding.
  • the cross-sectional drawing in FIG. 2 shows part of the molded shell 30 (including a cast model with a base body 11 'and a wax-filled ceramic body 20').
  • the casting is advantageously carried out in the position shown in order to obtain a good filling of the pore space of the ceramic body 2 by the melt.
  • a ventilation duct 12 see FIG. 3, is provided below the webs 10, the air displacement from the pore spaces improves.
  • the poured channel 12 is, of course, removed during the reworking of the casting.
  • the molded shell 30 is heated before casting to at least a temperature customary for precision casting (around 1150 ° C.).
  • the melt whose liquidus temperature is between around 1300 and 1400 ° C, is overheated. As experience has shown, the pore spaces of the ceramic bodies 2 fill completely thanks to the overheating before the solidification of the melt occurs.
  • FIGS. 4, 5 and 6 relate to the production of a first porous ceramic body 2
  • Ceramic grains 21 for example corundum, diameter between 0.8 and 1.2 mm
  • a pile 2 'with a pore space 22 is formed.
  • This pore space 22 is filled with a free-flowing binder (eg silicate binder) and then emptied again via the outlet 32, bridges 21a of the binder material being formed between the grains.
  • a coherent ceramic body 2 is obtained, which can be removed from the trough 31 and solidified by firing.
  • the ceramic body 2 is filled with wax and installed in the casting model for the production of the molded shell 30.
  • the wax is removed from the surface 23 of the ceramic body 2, so that a direct connection between the grains 21 and the molded shell 30 is created. After the wax 35 has melted out, there is a connection between the ceramic body 2 and the molded shell 30.
  • a surface 23 is formed with the metallic phase 35 filling the pore space 22, from which tips of the grains 21 emerge.
  • a second porous ceramic body 2 is produced by means of an open-cell foam structure 50 made of plastic, see FIG. 7.
  • the two net layers are connected to one another by invisible rungs.
  • the average distance between adjacent ones Mesh layers can be equated to the average cell diameter, the cell diameter is in the range of around 1 to 5 mm 50 applied.
  • the diving and Subsequent sanding must be carried out several times - for example three times.
  • the resulting rib-like agglomerate of ceramic grains is sintered together by firing, the plastic of the original foam structure 50 evaporating at the same time.
  • this ceramic body 2 is again shown as in FIG. 7 with two net layers 25 and 25 '(on an enlarged scale), the ceramic grains being drawn only for the upper net layer 25, however somewhat too large.
  • the third ceramic body 2 shown in FIG. 9 consists of a commercially available ceramic structure which is used, for example, as a filter for molten metal.
  • the production of this ceramic framework with an open-cell foam structure is known for example from CH-PS 679394.
  • FIG. 9 shows a section through the walls of the ceramic foam structure 26. Thanks to openings 27 in the walls, the cells form a completely communicating pore space 22.
  • FIG. 10 shows the ceramic structure 26 of FIG. 9, the pore space of which is filled with the metallic phase 28 (or with wax or plastic) and forms the composite body 20.
  • the metallic phase 28 is washed out on the web surfaces, as indicated in FIG. 11.
  • the relief-like surface structure probably has an improved fibrillating effect when the pulp is ground.
  • FIG. 12 shows a turbine blade tip 100 with armor 102, which is designed as a casting according to the invention.
  • the Armor 102 is formed by a casting zone with embedded ceramic, while the main part 101 of the blade is an unreinforced casting (for example the product of a method with directional solidification).

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Dental Prosthetics (AREA)
  • Mold Materials And Core Materials (AREA)
  • Compositions Of Oxide Ceramics (AREA)
EP92810477A 1992-06-23 1992-06-23 Moulage de précision ayant des surfaces d'usure Expired - Lifetime EP0575685B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE59207902T DE59207902D1 (de) 1992-06-23 1992-06-23 Feinguss mit Verschleissflächen
AT92810477T ATE147669T1 (de) 1992-06-23 1992-06-23 Feinguss mit verschleissflächen
EP92810477A EP0575685B1 (fr) 1992-06-23 1992-06-23 Moulage de précision ayant des surfaces d'usure
JP5149583A JPH06170514A (ja) 1992-06-23 1993-06-21 セラミック挿入型複合構造を有する鋳物

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP92810477A EP0575685B1 (fr) 1992-06-23 1992-06-23 Moulage de précision ayant des surfaces d'usure

Publications (2)

Publication Number Publication Date
EP0575685A1 true EP0575685A1 (fr) 1993-12-29
EP0575685B1 EP0575685B1 (fr) 1997-01-15

Family

ID=8211944

Family Applications (1)

Application Number Title Priority Date Filing Date
EP92810477A Expired - Lifetime EP0575685B1 (fr) 1992-06-23 1992-06-23 Moulage de précision ayant des surfaces d'usure

Country Status (4)

Country Link
EP (1) EP0575685B1 (fr)
JP (1) JPH06170514A (fr)
AT (1) ATE147669T1 (fr)
DE (1) DE59207902D1 (fr)

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2718279A1 (fr) * 1994-03-30 1995-10-06 Electrovac Corps de forme.
WO1998015373A1 (fr) * 1996-10-01 1998-04-16 Hubert Francois Piece d'usure composite
EP0838288A1 (fr) * 1996-10-01 1998-04-29 Hubert Francois Pièce d'usure composite
EP0928654A1 (fr) * 1998-01-09 1999-07-14 Gut Giesserei Umwelt Technik GmbH Procédé de fabrication des pièces composites avec des matériaux liquides ou semi liquides
WO2003024648A1 (fr) * 2001-09-17 2003-03-27 Fundacion Inasmet Pieces de broyage d'agregats composees d'une matrice metallique avec un insert interne en ceramique et procede de fabrication
US7513295B2 (en) 2001-12-04 2009-04-07 Magotteaux International Sa Cast parts with enhanced wear resistance
US20110014060A1 (en) * 2009-07-17 2011-01-20 Rolls-Royce Corporation Substrate Features for Mitigating Stress
EP2309098A1 (fr) * 2009-09-30 2011-04-13 Siemens Aktiengesellschaft Profil et aube directrice, aube rotorique, turbine à gaz et turbomachine associées
ITUD20100135A1 (it) * 2010-07-09 2012-01-10 Far Fonderie Acciaierie Roiale S P A Procedimento per la produzione di un elemento soggetto ad usura, elemento soggetto ad usura e struttura di aggregazione temporanea per la realizzazione di tale elemento soggetto ad usura
ITUD20100134A1 (it) * 2010-07-09 2012-01-10 Far Fonderie Acciaierie Roiale S P A Procedimento per la produzione di un elemento soggetto ad usura, elemento soggetto ad usura e struttura di aggregazione temporanea per la realizzazione di tale elemento soggetto ad usura
WO2015015507A1 (fr) * 2013-07-30 2015-02-05 Balaji Industrial Products Ltd., Cylindre de broyage pour broyeur à cylindres vertical et son procédé de fabrication
WO2016008967A1 (fr) 2014-07-16 2016-01-21 Magotteaux International S.A. Grains de céramique et leur procédé de fabrication
US9713912B2 (en) 2010-01-11 2017-07-25 Rolls-Royce Corporation Features for mitigating thermal or mechanical stress on an environmental barrier coating
US10040094B2 (en) 2013-03-15 2018-08-07 Rolls-Royce Corporation Coating interface
CN108941517A (zh) * 2018-07-19 2018-12-07 柳州市创科复合金属陶瓷制品有限公司 一种金属陶瓷复合材料及其制备方法
US10328531B2 (en) 2014-10-31 2019-06-25 Rolls-Royce Plc Rotary device
WO2020032964A1 (fr) * 2018-08-10 2020-02-13 Siemens Energy, Inc. Fabrication additive par friction-malaxage et réparation de composants de turbine
CN110997148A (zh) * 2017-07-27 2020-04-10 蒂森克虏伯工业解决方案股份公司 具有磨损元件的破碎机和用于制造破碎机磨损元件的方法
WO2020244695A1 (fr) * 2019-06-07 2020-12-10 SAUKE.SEMRAU GmbH Matériau composite en métal et en céramique et procédé de production correspondant
EP3915684A1 (fr) 2020-05-29 2021-12-01 Magotteaux International SA Pièce d'usure composite
CN115518736A (zh) * 2022-06-30 2022-12-27 华能海南发电股份有限公司东方电厂 一种金属陶瓷的磨辊辊套和磨盘衬板及铸造方法

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0935009B1 (fr) * 1998-02-05 2002-04-10 Sulzer Markets and Technology AG Corps moulé revêtu d'une couche
JP2004317243A (ja) 2003-04-15 2004-11-11 Mitsutoyo Corp 測定機
DE10323720A1 (de) * 2003-05-24 2004-12-30 Daimlerchrysler Ag Verfahren zur Herstellung eines Werkstücks aus einem Verbundmaterial
JP4095584B2 (ja) 2004-06-15 2008-06-04 本田技研工業株式会社 セラミック成形体及び金属基複合部材
WO2015006406A1 (fr) 2013-07-09 2015-01-15 United Technologies Corporation Structure de réseau tubulaire plaqué
US20160158964A1 (en) * 2013-07-09 2016-06-09 United Technologies Corporation Ceramic-encapsulated thermopolymer pattern or support with metallic plating
US11268526B2 (en) 2013-07-09 2022-03-08 Raytheon Technologies Corporation Plated polymer fan
EP3019711B1 (fr) 2013-07-09 2023-11-01 RTX Corporation Nosecône en polymère plaqué pour turbine à gas
US10214824B2 (en) 2013-07-09 2019-02-26 United Technologies Corporation Erosion and wear protection for composites and plated polymers
US10227704B2 (en) 2013-07-09 2019-03-12 United Technologies Corporation High-modulus coating for local stiffening of airfoil trailing edges
US10927843B2 (en) 2013-07-09 2021-02-23 Raytheon Technologies Corporation Plated polymer compressor

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DE2131812B1 (de) * 1971-06-23 1972-11-23 Kanegafuchi Chemical Ind Verfahren zur aeroben Zuechtung von Mikroorganismen
GB2003932A (en) * 1977-09-06 1979-03-21 Permanence Corp Method of forming composite material containing sintered particles and composite material
WO1984002927A1 (fr) * 1983-01-18 1984-08-02 Ae Plc Renforcement d'articles en metal ou alliage metallique coule
US4735656A (en) * 1986-12-29 1988-04-05 United Technologies Corporation Abrasive material, especially for turbine blade tips
EP0324706A2 (fr) * 1988-01-11 1989-07-19 Lanxide Technology Company, Lp. Procédé de fabrication de matériaux composites à matrice métallique
EP0340957A2 (fr) * 1988-04-30 1989-11-08 Toyota Jidosha Kabushiki Kaisha Procédé de fabrication de métal composite promouvant l'infiltration d'une matrice métallique par des fines particules d'un troisième matériau
EP0365978A1 (fr) * 1988-10-17 1990-05-02 Chrysler Motors Corporation Procédé pour la préparation d'un matériel composite renforcé de céramique
DE4107416A1 (de) * 1990-04-25 1991-11-28 Gisag Ag Giesserei Masch Verfahren zur herstellung von partiell verschleissgeschuetzten gussstuecken

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2131812B1 (de) * 1971-06-23 1972-11-23 Kanegafuchi Chemical Ind Verfahren zur aeroben Zuechtung von Mikroorganismen
GB2003932A (en) * 1977-09-06 1979-03-21 Permanence Corp Method of forming composite material containing sintered particles and composite material
WO1984002927A1 (fr) * 1983-01-18 1984-08-02 Ae Plc Renforcement d'articles en metal ou alliage metallique coule
US4735656A (en) * 1986-12-29 1988-04-05 United Technologies Corporation Abrasive material, especially for turbine blade tips
EP0324706A2 (fr) * 1988-01-11 1989-07-19 Lanxide Technology Company, Lp. Procédé de fabrication de matériaux composites à matrice métallique
EP0340957A2 (fr) * 1988-04-30 1989-11-08 Toyota Jidosha Kabushiki Kaisha Procédé de fabrication de métal composite promouvant l'infiltration d'une matrice métallique par des fines particules d'un troisième matériau
EP0365978A1 (fr) * 1988-10-17 1990-05-02 Chrysler Motors Corporation Procédé pour la préparation d'un matériel composite renforcé de céramique
DE4107416A1 (de) * 1990-04-25 1991-11-28 Gisag Ag Giesserei Masch Verfahren zur herstellung von partiell verschleissgeschuetzten gussstuecken

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Title
M.K.AGHAJANIAN ET AL. 'The fabrication of metal matrix composites by a pressureless infiltration technique' 15. Januar 1991 , JOURNAL OF MATERIAL SCIENCE 26 (1991) NR. 2 , LONDON, GB *
PATENT ABSTRACTS OF JAPAN vol. 8, no. 276 (M-346)(1713) 18. Dezember 1984 & JP-A-59 147 769 ( HITACHI KINZOKU K.K. ) 24. August 1984 *

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2718279A1 (fr) * 1994-03-30 1995-10-06 Electrovac Corps de forme.
USRE39998E1 (en) 1996-10-01 2008-01-08 Magotteaux International S.A. Composite wear component
WO1998015373A1 (fr) * 1996-10-01 1998-04-16 Hubert Francois Piece d'usure composite
EP0838288A1 (fr) * 1996-10-01 1998-04-29 Hubert Francois Pièce d'usure composite
US6399176B1 (en) 1996-10-01 2002-06-04 Magotteaux International S.A. Composite wear component
US6520241B2 (en) 1996-10-01 2003-02-18 Magotteaux Inernational S.A. Composite wear component
EP0928654A1 (fr) * 1998-01-09 1999-07-14 Gut Giesserei Umwelt Technik GmbH Procédé de fabrication des pièces composites avec des matériaux liquides ou semi liquides
WO2003024648A1 (fr) * 2001-09-17 2003-03-27 Fundacion Inasmet Pieces de broyage d'agregats composees d'une matrice metallique avec un insert interne en ceramique et procede de fabrication
ES2190881A1 (es) * 2001-09-17 2003-08-16 Fundacion Inasmet Piezas para molienda de aridos compuestas de una matriz metalica con interno interno de material.
US7935431B2 (en) 2001-12-04 2011-05-03 Magotteaux International Sa Cast parts with enhanced wear resistance
US7513295B2 (en) 2001-12-04 2009-04-07 Magotteaux International Sa Cast parts with enhanced wear resistance
US9194243B2 (en) * 2009-07-17 2015-11-24 Rolls-Royce Corporation Substrate features for mitigating stress
US20110014060A1 (en) * 2009-07-17 2011-01-20 Rolls-Royce Corporation Substrate Features for Mitigating Stress
EP2275646A3 (fr) * 2009-07-17 2017-12-13 Rolls-Royce Corporation Extrémité d'aube comprenant des caractéristiques de réduction de la fatigue
EP2309098A1 (fr) * 2009-09-30 2011-04-13 Siemens Aktiengesellschaft Profil et aube directrice, aube rotorique, turbine à gaz et turbomachine associées
US9713912B2 (en) 2010-01-11 2017-07-25 Rolls-Royce Corporation Features for mitigating thermal or mechanical stress on an environmental barrier coating
US10357830B2 (en) 2010-07-09 2019-07-23 F.A.R.—Fonderie Acciaierie Roiale—SpA Method for the production of an element subject to wear, element subject to wear and temporary aggregation structure to produce said element subject to wear
CN103228381A (zh) * 2010-07-09 2013-07-31 F·A·R·罗亚力铸钢股份有限公司 制造受磨元件的方法、受磨元件以及用于制造受磨元件的临时聚集结构
CN103228381B (zh) * 2010-07-09 2015-06-24 F·A·R·罗亚力铸钢股份有限公司 制造受磨元件的方法、受磨元件以及用于制造受磨元件的临时聚集结构
WO2012004655A1 (fr) * 2010-07-09 2012-01-12 F.A.R. - Fonderie Acciaierie Roiale - Spa Procédé pour la production d'un élément sujet à usure, élément sujet à usure et structure à agrégation temporaire pour produire ledit élément sujet à usure
WO2012004654A1 (fr) * 2010-07-09 2012-01-12 F.A.R. - Fonderie Acciaierie Roiale - Spa Procédé pour la production d'un élément sujet à usure, élément sujet à usure et structure à agrégation temporaire pour produire ledit élément sujet à usure
AU2011275443B2 (en) * 2010-07-09 2016-10-06 F.A.R. - Fonderie Acciaierie Roiale - Spa Method for the production of an element subject to wear, element subject to wear and temporary aggregation structure to produce said element subject to wear
ITUD20100134A1 (it) * 2010-07-09 2012-01-10 Far Fonderie Acciaierie Roiale S P A Procedimento per la produzione di un elemento soggetto ad usura, elemento soggetto ad usura e struttura di aggregazione temporanea per la realizzazione di tale elemento soggetto ad usura
ITUD20100135A1 (it) * 2010-07-09 2012-01-10 Far Fonderie Acciaierie Roiale S P A Procedimento per la produzione di un elemento soggetto ad usura, elemento soggetto ad usura e struttura di aggregazione temporanea per la realizzazione di tale elemento soggetto ad usura
US10040094B2 (en) 2013-03-15 2018-08-07 Rolls-Royce Corporation Coating interface
WO2015015507A1 (fr) * 2013-07-30 2015-02-05 Balaji Industrial Products Ltd., Cylindre de broyage pour broyeur à cylindres vertical et son procédé de fabrication
WO2016008967A1 (fr) 2014-07-16 2016-01-21 Magotteaux International S.A. Grains de céramique et leur procédé de fabrication
US11465942B2 (en) 2014-07-16 2022-10-11 Magotteaux International S.A. Ceramic grains and method for their production
US10328531B2 (en) 2014-10-31 2019-06-25 Rolls-Royce Plc Rotary device
CN110997148A (zh) * 2017-07-27 2020-04-10 蒂森克虏伯工业解决方案股份公司 具有磨损元件的破碎机和用于制造破碎机磨损元件的方法
CN108941517A (zh) * 2018-07-19 2018-12-07 柳州市创科复合金属陶瓷制品有限公司 一种金属陶瓷复合材料及其制备方法
CN108941517B (zh) * 2018-07-19 2021-09-17 柳州市创科复合金属陶瓷制品有限公司 一种炉口的制备方法
WO2020032964A1 (fr) * 2018-08-10 2020-02-13 Siemens Energy, Inc. Fabrication additive par friction-malaxage et réparation de composants de turbine
WO2020244695A1 (fr) * 2019-06-07 2020-12-10 SAUKE.SEMRAU GmbH Matériau composite en métal et en céramique et procédé de production correspondant
EP3915684A1 (fr) 2020-05-29 2021-12-01 Magotteaux International SA Pièce d'usure composite
WO2021239295A1 (fr) 2020-05-29 2021-12-02 Magotteaux International S.A. Piece d'usure composite
CN115518736A (zh) * 2022-06-30 2022-12-27 华能海南发电股份有限公司东方电厂 一种金属陶瓷的磨辊辊套和磨盘衬板及铸造方法

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JPH06170514A (ja) 1994-06-21
ATE147669T1 (de) 1997-02-15
EP0575685B1 (fr) 1997-01-15
DE59207902D1 (de) 1997-02-27

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