EP0575685A1 - Investment casting with wear surfaces - Google Patents
Investment casting with wear surfaces Download PDFInfo
- 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
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- 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
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- 238000005495 investment casting Methods 0.000 title description 3
- 239000000919 ceramic Substances 0.000 claims abstract description 71
- 238000005266 casting Methods 0.000 claims abstract description 34
- 238000004519 manufacturing process Methods 0.000 claims abstract description 15
- 238000000034 method Methods 0.000 claims abstract description 13
- 239000011148 porous material Substances 0.000 claims abstract description 13
- 239000002131 composite material Substances 0.000 claims abstract description 12
- 239000006260 foam Substances 0.000 claims description 9
- 239000002245 particle Substances 0.000 claims description 8
- 239000000155 melt Substances 0.000 claims description 7
- 238000000227 grinding Methods 0.000 claims description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 4
- 239000010959 steel Substances 0.000 claims description 4
- 229910010293 ceramic material Inorganic materials 0.000 claims description 3
- 229910052593 corundum Inorganic materials 0.000 claims description 3
- 239000010431 corundum Substances 0.000 claims description 3
- 229910000531 Co alloy Inorganic materials 0.000 claims description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 2
- 239000000395 magnesium oxide Substances 0.000 claims description 2
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 claims description 2
- 229910052759 nickel Inorganic materials 0.000 claims description 2
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 claims description 2
- 229910001928 zirconium oxide Inorganic materials 0.000 claims description 2
- 238000000465 moulding Methods 0.000 abstract 3
- 238000010009 beating Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 description 8
- 239000011230 binding agent Substances 0.000 description 5
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 239000006185 dispersion Substances 0.000 description 3
- 230000003628 erosive effect Effects 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 230000002787 reinforcement Effects 0.000 description 3
- 229910001208 Crucible steel Inorganic materials 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 229910001149 41xx steel Inorganic materials 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000009189 diving Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000010297 mechanical methods and process Methods 0.000 description 1
- 230000005226 mechanical processes and functions Effects 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
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- 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)
- Compositions Of Oxide Ceramics (AREA)
- Dental Prosthetics (AREA)
- Mold Materials And Core Materials (AREA)
Abstract
Description
Die Erfindung bezieht sich auf ein Verfahren zum Herstellen von Gussstücken mit verbundartig eingelagerter Keramik sowie auf Gussstücke, die mittels eines derartigen Verfahrens hergestellt sind.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.
Bei Verbundwerkstoffen sind verschiedene Arten von Stoffgruppen zusammengefügt, wobei in vielen Fällen eine erste Phase durch einen Basiswerkstoff gebildet wird und eine zweiten Phase - in einer besonderen räumlichen Anordnung - in die erste Phase eingelagert ist. Oft ist der Basiswerkstoff metallisch (Reinmetall oder Legierung) und die Einlagerungen bestehen aus keramischem Material. Bei Dispersionslegierungen (dispersionsgehärteten Werkstoffen) sind harte Teilchen - gebildet beispielsweise durch Oxide, Karbide, Boride oder Nitride - in feindispersiver Form in die metallische erste Phase eingelagert. Bei einer anderen Art von Teilchenverbundwerkstoffen, nämlich den sogenannten Cermets (ceramics/metals), dient die erste Phase als Bindemittel für die keramischen Teilchen der zweiten Phase, welche volumenbezogen den Hauptteil des Verbundwerkstoffes ausmacht. Cermets werden pulvermetallurgisch hergestellt. Sie eignen sich als verschleissfeste Werkstoffe.In the case of composite materials, different types of material groups are put together, in many cases a 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. In the case of dispersion alloys (dispersion-hardened materials), hard particles - formed, for example, by oxides, carbides, borides or nitrides - are embedded in the metallic first phase in a finely dispersive form. In another type of particle composite, namely the so-called cermets (ceramics / metals), 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.
Bei verschiedenen mechanischen Verfahren werden Vorrichtungskomponenten, die als Gussstücke hergestellt sind, starkem Verschleiss unterworfen. Solche Gussstücke trifft man beispielsweise in Refinern bei der Papierherstellung an. In den Refinern wird der im Pulper aufgelöste Faserstoff zwischen Platten mit scharfkantigen Stegen gemahlen, wobei die Fasern zerschnitten und fibrilliert werden. Die Stege der Refinerplatten verlieren beim Mahlvorgang durch Abrasion, Erosion und Korrosion an Höhe und die Kanten werden durch plastische Verformung abgerundet. Um die Verschleissfestigkeit der Refinerplatten zu erhöhen, wird eine Verstärkung der Mahlflächen benötigt: Die Stege sollen - ähnlich wie bei den Cermets oder den Dispersionslegierungen - mittels Keramik verstärkt werden. Um die bei den bekannten Refinern gebene hohe Zähigkeit der Stegbasis zu erhalten, soll die Keramikeinlagerung auf den oberen Bereich der Stege bei den Mahlflächen beschränkt bleiben.In various mechanical processes, device components that are manufactured as castings are subjected to severe wear. Such castings can be found, for example, in refiners used in papermaking. In the refiners, the pulp dissolved in the pulper is ground between plates with sharp-edged webs, the fibers being cut and fibrillated. The ridges of the refiner plates lose height during the grinding process due to abrasion, erosion and corrosion, and the edges are rounded off by plastic deformation. In order to increase the wear resistance of the refiner plates, a reinforcement of the grinding surfaces is required: Similar to the cermets or the dispersion alloys, the webs should be reinforced with ceramics. In order to maintain the high toughness of the bar base given in the known refiners, the ceramic incorporation should be limited to the upper area of the bars at the grinding surfaces.
Es ist Aufgabe der Erfindung, ein Verfahren zur Herstellung von Gussstücken zu schaffen, bei dem das Gussstück zumindest teilweise durch verbundartig eingelagerte Keramik verstärkt wird. Diese Aufgabe wird durch die Merkmale des ersten Anspruchs gelöst. Beim Beispiel der Refinerplatten muss in den Stegen und zwar im Bereich, der durch die Verschleissvorgänge abgetragen wird, für die keramische Verstärkung des Gusses gesorgt werden. Anders als bei den Cermets und Dispersionslegierungen, wo die keramische Phase innerhalb der metallischen Phase mikroskopisch verteilt ist, weisen bei den erfindungsgemässen Gussstücken die keramischen Einlagerungen einen makroskopischen Charakter auf.It is an object of the invention to provide a method for producing castings, in which the casting is at least partially reinforced by ceramic embedded in a composite. This object is achieved by the features of the first claim. In the example of the refiner plates, the ceramic reinforcement of the cast must be provided in the webs, in the area that is worn away by the wear processes. In contrast to the cermets and dispersion alloys, where the ceramic phase is microscopically distributed within the metallic phase, the ceramic inclusions have a macroscopic character in the castings according to the invention.
Der erfindungsgemässe Guss wird mittels eines Feingussverfahrens ausgeführt, bei dem ausschmelzbare oder ausbrennbare Modelle für die Herstellung der Formschale benutzt werden. Für die unverstärkten Teile des Gussstücks wird für das Modell mit Vorteil Wachs verwendet. In das Gussmodell werden die für die Verstärkung vorgesehenen porösen Keramikkörper integriert, wobei die Porenräume der Keramikkörper zuvor mit Wachs gefüllt werden - oder statt Wachs mit einem Kunststoff, der sich beim Brennen der Formschale rückstandfrei verflüchtigt.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. For the unreinforced parts of the casting wax is used 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.
Der poröse Keramikkörper, der einen vollständig kommunizierenden Porenraum aufweist und dessen Keramikstrukur ein dreidimensionales Netz bildet, kann auf verschiedene Weisen hergestellt werden. Drei Beispiele für diese Herstellverfahren werden weiter unten beschrieben. Es ergeben sich bei diesen Verfahren folgende Keramikstrukturen: 1. ein Haufwerk von kornartigen Partikeln; 2. eine Keramikstrukur aus gerippeartig angeordneten und zusammengesinterten kornartigen Partikeln; 3. ein keramisches Gerippe mit offenzelliger Schaumstruktur.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.
Bei der Herstellung von Refinerplatten nimmt man als Basiswerkstoff mit Vorteil einen rostfreien Stahl, wie er beim Giessen solcher Platten üblich ist (ASTM CB-30 oder X 35 CrMo 17). Auch Nickelbasis- oder Kobaltbasis-Legierungen sind verwendbar. Das keramische Material muss sich gegenüber der Schmelze inert verhalten. Beim Stahlguss kommt beispielsweise Aluminiumoxid (Korund), Zirkonoxid oder Magnesiumoxid in Frage; Siliziumcarbid hingegen ist ungeeignet, da dieser Stoff mit der Schmelze reagiert.When manufacturing refiner plates, 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. For steel castings, for example, 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.
Da die Wärmeausdehung bei Keramik und Stahl verschieden ist, bestanden Bedenken gegenüber der Herstellung des erfindungsgemässen Verbundwerkstoffes. Die Versuche, die entgegen diesen Bedenken ausgeführt wurden, zeigten jedoch, dass die verwendeten Keramikstrukturen im Verbund mit Gussstahl intakt - zumindest ohne störende Schäden - blieben.Since the thermal expansion of ceramic and steel is different, there were concerns about the production of the composite material according to the invention. The tests that were carried out against these concerns, however, showed that the ceramic structures used in combination with cast steel remained intact - at least without any disturbing damage.
Das erfindungsgemässe Verfahren kann auch bei der Herstellung von beispielsweise Lagerteilen oder Dichtungen angewendet werden. In der vorliegenden Beschreibung wird auf die Erfindung hauptsächlich im Zusammenhang mit der erwähnten Refinerplatten eingegangen. Nachfolgend wird die Erfindung anhand der Zeichnungen im Detail erläutert. Es zeigen:
- Fig. 1
- einen Ausschnitt aus einer Refinerplatte, die nach dem erfindungsgemässen Verfahren hergestellt ist,
- Fig. 2
- einen Ausschnitt aus der Formschale und dem Modell für den Guss der Refinerplatte gemäss Fig.1,
- Fig. 3
- eine Variante zur Formschale der Fig.2,
- Fig. 4
- ein Hilfsmittel für die Herstellung eines ersten porösen Körpers,
- Fig. 5
- ein Haufwerk von keramischen Körnern,
- Fig. 6
- das in Gussstahl eingelagerte Haufwerk der Fig.5,
- Fig. 7
- eine offenzellige Schaumstruktur,
- Fig. 8
- eine Keramikstrukur aus gerippeartig angeordneten und zusammengesinterten kornartigen Partikeln,
- Fig. 9
- ein keramisches Gerippe mit offenzelliger Schaumstruktur
- Fig. 10
- einen Ausschnitt eines Gussstücks mit eingelagerter Keramikstruktur gemäss Fig.9,
- Fig. 11
- das gleiche Gussstück wie in Fig.10 nach teilweiser Erosion der Oberfläche und
- Fig. 12
- eine Turbinenschaufelspitze mit Panzerung.
- Fig. 1
- a section of a refiner plate which is produced by the method according to the invention,
- Fig. 2
- a section of the molded shell and the model for the casting of the refiner plate according to FIG. 1,
- Fig. 3
- a variant of the molded shell of Figure 2,
- Fig. 4
- an aid for the production of a first porous body,
- Fig. 5
- a pile of ceramic grains,
- Fig. 6
- the pile of cast iron stored in Fig. 5,
- Fig. 7
- an open-cell foam structure,
- Fig. 8
- a ceramic structure made up of rib-like and sintered grain-like particles,
- Fig. 9
- a ceramic structure with an open-cell foam structure
- Fig. 10
- a section of a casting with embedded ceramic structure according to Figure 9,
- Fig. 11
- the same casting as in Fig.10 after partial erosion of the surface and
- Fig. 12
- a turbine blade tip with armor.
In Fig.1 ist ausschnittsweise eine Refinerplatte 1 mit Stegen 10 dargestellt. Die Stegoberfläche 15 (die Mahlfläche) wird beim Mahlen des Faserstoffs dem Verschleiss unterworfen. Die Verschleissbereiche der Stege 10 bestehen erfindungsgemäss aus einem Stahl/Keramik-Verbund 20, in welchem ein poröser Keramikkörper 2 in gegossenem Stahl eingelagert ist. Der Grundkörper 11 der Refinerplatte 1 sowie die Stegbasisbereiche weisen keine eingelagerte Keramik auf; dadurch bleibt die hohe Zähigkeit des Gusswerkstoffs in den Stegwurzeln, wo grosse Biegemomente während des Mahlens auftreten, erhalten.A refiner plate 1 with
Die Querschnittszeichnung in Fig.2 zeigt einen Teil der Formschale 30 (einschliesslich Gussmodell mit Grundkörper 11' und wachsgefülltem Keramikkörper 20'). Der Guss erfolgt mit Vorteil in der gezeigten Lage, um eine gute Füllung des Porenraums des Keramikkörpers 2 durch die Schmelze zu erhalten. Wird ein Entlüftungskanal 12, siehe Fig.3, jeweils unterhalb der Stege 10 vorgesehen, so verbessert sich die Luftverdrängung aus den Porenräumen. (Der ausgegossene Kanal 12 wird selbstverständlich bei der Überarbeitung des Gussstücks entfernt.) Die Formschale 30 wird vor dem Giessen mindestens auf eine beim Präzisionsguss übliche Temperatur (rund 1150°C) aufgeheizt. Die Schmelze, deren Liquidustemperatur zwischen rund 1300 und 1400°C liegt, wird überhitzt. Wie die Erfahrung gezeigt hat, füllen sich die Porenräume der Keramikkörper 2 dank der Überhitzung vollständig, bevor die Erstarrung der Schmelze eintritt.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
Die Figuren 4, 5 und 6 betreffen die Herstellung eines ersten porösen Keramikkörpers 2. In eine Wanne 31 aus Wachs mit einem Ablauf 32 werden Keramikkörner 21 (beispielsweise Korund, Durchmesser zwischen 0,8 und 1,2 mm) eingeschüttet. Es bildet sich dabei ein Haufwerk 2' mit einem Porenraum 22. Dieser Porenraum 22 wird mit einem gut fliessfähigen Bindemittel (z.B. Silikatbinder) gefüllt und anschliessend über den Ablauf 32 wieder entleert, wobei zwischen den Körnern sich Brücken 21a aus dem Bindermaterial ausbilden. Durch Trocknen des Binders erhält man einen zusammenhängenden Keramikkörper 2, den man aus der Wanne 31 entfernen und mittels Brennens verfestigen kann.FIGS. 4, 5 and 6 relate to the production of a first porous
Der Keramikkörper 2 wird mit Wachs gefüllt und in das Gussmodell für die Herstellung der Formschale 30 eingebaut. An der Oberfläche 23 des Keramikkörpers 2 wird das Wachs entfernt, sodass eine unmittelbare Verbindung zwischen den Körnern 21 und der Formschale 30 entsteht. Nach dem Ausschmelzen des Wachses 35 liegt somit eine Verbindung zwischen dem Keramikkörper 2 und der Formschale 30 vor. Beim Giessen bildet sich mit der den Porenraum 22 füllenden metallischen Phase 35 eine Oberfläche 23 aus, aus welcher Spitzen der Körner 21 hervortreten.The
Ein zweiter poröser Keramikkörper 2 wird mittels einer offenzelligen Schaumstruktur 50 aus Kunststoff, siehe Fig.7, hergestellt. (Der Übersichtlichkeit halber sind in Fig.7 nur eine Netzlage 55, die an der Oberfläche der Schaumstruktur 50 liegt, und ein zweite, darunter liegende Netzlage 55' dargestellt. Die beiden Netzlagen sind durch nicht sichtbare Sprossen miteinander verbunden. Der mittlere Abstand zwischen benachbarten Netzlagen kann dem mittleren Zelldurchmesser gleichgesetzt werden. Der Zelldurchmesser liegt im Bereich von rund 1 bis 5 mm.) Feine Keramikkörner (beispielsweise Korund, Korndurchmesser 0,06 bis 0,15 mm) werden mittels eines Binders durch Tauchung und Besandung auf die Sprossen der Schaumstrukur 50 aufgebracht. Die Tauchung und anschliessende Besandung muss mehrfach - beispielsweise dreimal - ausgeführt werden. Nachfolgend wird das so erzeugte gerippeartige Agglomerat von Keramikkörnern durch Brennen zusammengesintert, wobei der Kunststoff der ursprünglichen Schaumstruktur 50 sich gleichzeitig verflüchtigt. In Fig.8 ist dieser Keramikkörper 2 wiederum wie in Fig.7 mit zwei Netzlagen 25 und 25' dargestellt (bei vergrössertem Massstab), wobei nur für die obere Netzlage 25 die Keramikkörner - allerdings etwas zu gross - gezeichnet sind.A second porous
Der dritte, in Fig.9 gezeigt Keramikkörper 2, besteht aus einer im Handel erhältlichen Keramikstruktur, die beispielsweise als Filter für Metallschmelzen verwendet wird. Die Herstellung dieses keramischen Gerippes mit offenzelliger Schaumstruktur ist beispielsweise aus der CH-PS 679394 bekannt. Fig.9 zeigt einen Schnitt durch die Wandungen der keramischen Schaumstruktur 26. Die Zellen bilden dank Durchbrüchen 27 in den Wandungen einen vollständig kommunizierenden Porenraum 22.The third
Das Schrägbild in Fig.10 stellt die Keramikstruktur 26 der Fig.9 dar, deren Porenraum mit der metallischen Phase 28 (bzw. mit Wachs oder Kunststoff) gefüllt ist und den Verbundkörper 20 bildet. Bei der Verwendung dieses Verbundkörpers 20 in Refinerplatten ergibt sich wegen der grösseren Widerstandsfähigkeit der Keramik 26 eine Auswaschung der metallischen Phase 28 an den Stegoberflächen, wie es in Fig.11 angedeutet ist. Die reliefartige Oberflächenstruktur weist wahrscheinlich eine verbesserte fibrillierende Wirkung beim Mahlen des Faserstoffs auf.10 shows the
Bei Schaufeln für Gasturbinen ist es vorteilhaft, wenn deren Spitzen gepanzert werden. Fig. 12 zeigt eine Turbinenschaufelspitze 100 mit einer Panzerung 102, die als erfindungsgemässes Gussstück ausgeführt ist. Die Panzerung 102 wird durch eine Gusszone mit eingelagerter Keramik gebildet, während der Hauptteil 101 der Schaufel ein unverstärkter Gusskörper (beispielsweise das Erzeugnis eines Verfahrens mit gerichteter Erstarrung) ist.In the case of blades for gas turbines, it is advantageous if their tips are armored. 12 shows a
Claims (10)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
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DE59207902T DE59207902D1 (en) | 1992-06-23 | 1992-06-23 | Investment casting with wear surfaces |
EP92810477A EP0575685B1 (en) | 1992-06-23 | 1992-06-23 | Investment casting with wear surfaces |
AT92810477T ATE147669T1 (en) | 1992-06-23 | 1992-06-23 | INVESTMENT CASTING WITH WEAR SURFACES |
JP5149583A JPH06170514A (en) | 1992-06-23 | 1993-06-21 | Casting with ceramic insertion type composite construction |
Applications Claiming Priority (1)
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EP92810477A EP0575685B1 (en) | 1992-06-23 | 1992-06-23 | Investment casting with wear surfaces |
Publications (2)
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EP0575685A1 true EP0575685A1 (en) | 1993-12-29 |
EP0575685B1 EP0575685B1 (en) | 1997-01-15 |
Family
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EP92810477A Expired - Lifetime EP0575685B1 (en) | 1992-06-23 | 1992-06-23 | Investment casting with wear surfaces |
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EP (1) | EP0575685B1 (en) |
JP (1) | JPH06170514A (en) |
AT (1) | ATE147669T1 (en) |
DE (1) | DE59207902D1 (en) |
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EP3915684A1 (en) | 2020-05-29 | 2021-12-01 | Magotteaux International SA | Composite wear part |
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Also Published As
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DE59207902D1 (en) | 1997-02-27 |
ATE147669T1 (en) | 1997-02-15 |
EP0575685B1 (en) | 1997-01-15 |
JPH06170514A (en) | 1994-06-21 |
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