DE2362469A1 - Joining sintered ceramic components - esp in the mfr of silicon nitride gas turbine impeller wheels - Google Patents
Joining sintered ceramic components - esp in the mfr of silicon nitride gas turbine impeller wheelsInfo
- Publication number
- DE2362469A1 DE2362469A1 DE2362469A DE2362469A DE2362469A1 DE 2362469 A1 DE2362469 A1 DE 2362469A1 DE 2362469 A DE2362469 A DE 2362469A DE 2362469 A DE2362469 A DE 2362469A DE 2362469 A1 DE2362469 A1 DE 2362469A1
- Authority
- DE
- Germany
- Prior art keywords
- components
- sintered
- hot
- silicon nitride
- powder
- 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.)
- Pending
Links
- 229910052581 Si3N4 Inorganic materials 0.000 title claims abstract description 11
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 title claims abstract description 10
- 239000000919 ceramic Substances 0.000 title claims description 9
- 238000005304 joining Methods 0.000 title claims description 3
- 239000000843 powder Substances 0.000 claims abstract description 12
- 238000005245 sintering Methods 0.000 claims abstract description 12
- 238000007731 hot pressing Methods 0.000 claims abstract description 10
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 9
- 239000000377 silicon dioxide Substances 0.000 claims abstract description 5
- 235000012239 silicon dioxide Nutrition 0.000 claims abstract description 5
- -1 silicon nitrile Chemical class 0.000 claims abstract description 4
- 238000000034 method Methods 0.000 claims description 19
- 239000000395 magnesium oxide Substances 0.000 claims description 4
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 4
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 claims description 4
- 230000003647 oxidation Effects 0.000 claims description 3
- 238000007254 oxidation reaction Methods 0.000 claims description 3
- SGPGESCZOCHFCL-UHFFFAOYSA-N Tilisolol hydrochloride Chemical compound [Cl-].C1=CC=C2C(=O)N(C)C=C(OCC(O)C[NH2+]C(C)(C)C)C2=C1 SGPGESCZOCHFCL-UHFFFAOYSA-N 0.000 claims 1
- 229910052710 silicon Inorganic materials 0.000 abstract description 2
- 239000010703 silicon Substances 0.000 abstract description 2
- 239000003795 chemical substances by application Substances 0.000 abstract 2
- 229910052681 coesite Inorganic materials 0.000 abstract 2
- 229910052906 cristobalite Inorganic materials 0.000 abstract 2
- 150000004760 silicates Chemical class 0.000 abstract 2
- 229910052682 stishovite Inorganic materials 0.000 abstract 2
- 229910052905 tridymite Inorganic materials 0.000 abstract 2
- 238000004519 manufacturing process Methods 0.000 description 7
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 239000007795 chemical reaction product Substances 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- FRWYFWZENXDZMU-UHFFFAOYSA-N 2-iodoquinoline Chemical compound C1=CC=CC2=NC(I)=CC=C21 FRWYFWZENXDZMU-UHFFFAOYSA-N 0.000 description 1
- 244000025254 Cannabis sativa Species 0.000 description 1
- FSVQVLHGIXXZGC-UHFFFAOYSA-N [Si].[U] Chemical compound [Si].[U] FSVQVLHGIXXZGC-UHFFFAOYSA-N 0.000 description 1
- LTPBRCUWZOMYOC-UHFFFAOYSA-N beryllium oxide Inorganic materials O=[Be] LTPBRCUWZOMYOC-UHFFFAOYSA-N 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- FUJCRWPEOMXPAD-UHFFFAOYSA-N lithium oxide Chemical compound [Li+].[Li+].[O-2] FUJCRWPEOMXPAD-UHFFFAOYSA-N 0.000 description 1
- 229910001947 lithium oxide Inorganic materials 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000001465 metallisation Methods 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000007493 shaping process 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
- 239000011863 silicon-based powder Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 238000007740 vapor deposition Methods 0.000 description 1
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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/58—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides
- C04B35/584—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on silicon nitride
- C04B35/593—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on silicon nitride obtained by pressure sintering
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/64—Burning or sintering processes
- C04B35/645—Pressure sintering
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B37/00—Joining burned ceramic articles with other burned ceramic articles or other articles by heating
- C04B37/003—Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of a combination of materials selected from glass, or ceramic material with metals, metal oxides or metal salts
- C04B37/005—Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of a combination of materials selected from glass, or ceramic material with metals, metal oxides or metal salts consisting of glass or ceramic material
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/02—Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
- C04B2237/04—Ceramic interlayers
- C04B2237/06—Oxidic interlayers
- C04B2237/062—Oxidic interlayers based on silica or silicates
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/341—Silica or silicates
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/34—Oxidic
- C04B2237/343—Alumina or aluminates
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/368—Silicon nitride
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/60—Forming at the joining interface or in the joining layer specific reaction phases or zones, e.g. diffusion of reactive species from the interlayer to the substrate or from a substrate to the joining interface, carbide forming at the joining interface
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/50—Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
- C04B2237/64—Forming laminates or joined articles comprising grooves or cuts
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Products (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
"Verfahren zum Verbinden keramischer Bauteile""Process for connecting ceramic components"
Die Erfindung bezieht sich auf ein Verfahren zum Verbinden keramischer Bauteile. Solche Bauteile, die beispielsweise aus Aluminiumoxyd bestehen, lassen sich nach bekannten Metallisierungs- und Lötverfahren zusammenfügen, bei denen die zu verbindenden Flächen durch Aufsintern oder Aufdampfen mit einer Metallschicht überzogen und danach zusammengelötet werden. Derartige Verbindungen sind jedoch nur begrenzt hitzebeständig. Für hohen Temperaturen ausgesetzte Werkstücke, wie z.B. Laufräder von Gasturbinen, lassen si· sich nicht verwenden. Gerade bei solchen hochbeanspruchten Maschinenteilen ist es jedoch vorteilhaft, Bauteil· verschiedener Eigenschaften miteinander zu kombinieren. Diese Möglichkeit entfällt bei den bisher bekannten Verfahren.The invention relates to a method for joining ceramic components. Such components, for example consist of aluminum oxide, can be according to known metallization and soldering processes, in which the surfaces to be connected by sintering or vapor deposition with coated with a metal layer and then soldered together. However, such compounds have only limited heat resistance. Workpieces exposed to high temperatures, such as the impellers of gas turbines, cannot be used. In the case of such highly stressed machine parts, however, it is advantageous to use components with different properties to combine with each other. This possibility does not apply to the previously known methods.
Der Erfindung liegt die Aufgabe zugrunde, diesen Mangel zu beheben und ein Verfahren anzugeben, das es erlaubt, keramische Bauteile so miteinander zu verbinden, daß die Verbindungsstelle hohe thermische und mechanische Beanspruchungen aushält. Dies geschieht nach der Erfindung dadurch, daß ein oder mehrere vorgesinterte Bauteile in eine Heißpreßmatrize eingesetzt werden, in der anschließend ein oder mehrere Bauteile aus einem sinterfähigen Pulver heißgepreßt und dabei gleichzeitig mit dem oder den vorgesinterten Bauteilen zu einem einstückigen Werkstück verbunden werden. Bei diesem Verfahren, bei dem Bauteile während ihrer Herstellung mit anderen bereits fertigen Bauteilen zu einem Werkstück ver-The invention is based on the object of eliminating this deficiency and specifying a method that allows ceramic To connect components to one another in such a way that the connection point is subject to high thermal and mechanical loads endures. This is done according to the invention in that one or more pre-sintered components in a hot press die are used, in which one or more components are then hot-pressed from a sinterable powder and thereby are simultaneously connected to the pre-sintered component or components to form a one-piece workpiece. With this one Process in which components are combined with other already finished components to form a workpiece during their manufacture.
509825/0568509825/0568
- » -- »- Paint 97OIAPaint 97OIA
bunden werden, das trotz unterschiedlicher Eigenschaften seiner Bestandteile eine Einheit bildet, ergeben sich Verbindungsstellen, die auch hohen thermischen und mechanischen Belastungen gewachsen sind. be bound, despite different properties of its If the components form a unit, there are connection points that can withstand high thermal and mechanical loads.
Weitere vorteilhafte Ausgestaltungen der Erfindung sind in der Beschreibung angegeben.Further advantageous embodiments of the invention are given in the description.
Die Zeichnung zeigt zur Erläuterung eines Aueführungebeispieles des erfindungsgemäßen Verfahrens eine Heißpreßform zur Herstellung eines aus keramischen Bauteilen zusammengesetzten Laufrades einer Gras turbine.The drawing shows to explain an example of execution of the method according to the invention a hot press mold for the production of an impeller of a grass turbine composed of ceramic components.
Die Heißpreßform besteht aus einem Bodenteil 1 und aus einem hohlzylindrischen Mantelteil 2, die zusammen die Matrize 3 bilden, sowie aus einem Stempel k. Das Bodenteil 1 hat an seiner Oberseite einen zylindrischen Ansatz 5, der in eine stufenförmige zylindrische Ausnehmung 6 an der Unterseite des Mantelteiles 2 eingreift und dieses dadurch zentriert» Der Ansatz 5 des Bodenteiles 1 erstreckt sich nur teilweise in die Ausnehmung 6, so daß am Grunde der Matrize 3 eine seitliche Ringnut 7 zur Aufnahme von vorgesinterten Laufschaufeln 8 gebildet wird. Die Stirnseite 9 des Ansatzes 5 des Bodenteiles 1 und die Stirnseite 10 des Stempels U weisen rotationssymmetrische Formen auf, die den Seitenflächen des strichpunktiert angedeuteten Radkörpers 11 des herzustellenden Turbinenlaufrades entsprechen. 12 sind die Schaufelfüße der Laufschaufeln 8, die an den Radkörper 11 angrenzen.The hot press mold consists of a bottom part 1 and a hollow cylindrical shell part 2, which together form the die 3, and a punch k. The bottom part 1 has a cylindrical extension 5 on its upper side, which engages in a step-shaped cylindrical recess 6 on the underside of the casing part 2 and thereby centers it the die 3 a lateral annular groove 7 for receiving presintered rotor blades 8 is formed. The end face 9 of the extension 5 of the bottom part 1 and the end face 10 of the stamp U have rotationally symmetrical shapes which correspond to the side surfaces of the wheel body 11, indicated by dash-dotted lines, of the turbine runner to be produced. 12 are the blade roots of the rotor blades 8, which adjoin the wheel body 11.
Das Turbinenlaufrad, dessen Pertigungs- und Verbindungsverfahren im folgenden beschrieben wird, ist beispielsweiseThe turbine runner, its manufacturing and connection processes will be described below is, for example
S09825/0588S09825 / 0588
Palm 9701APalm 9701A
aus Laufschaufeln 8 aus reaktionsgesintertem Siliziumnitrid und einem Radkörper 11 aus heißgepreßtem Siliziumnitrid zusammengesetzt. of rotor blades 8 made of reaction-sintered silicon nitride and a wheel body 11 composed of hot-pressed silicon nitride.
Die Herstellung der reaktiongesinterten Laufschaufeln 8 kann nach einem der bekannten Verfahren zur Hers-teilung von reaktionsgeeint er tem Siliziumnitrid erfolgen. Beispielsweise wird Siliziumpulver mit einem Bindemittel aus Kunststoff in die gewünschte Schaufelform gepreßt. Durch anschließendes Erhitzen der Laufschaufel 8 auf Temperaturen zwischen 1200 und 1Λ50 Grad Celsius in einer stickstoffhaltigen Atmosphäre wird das Silizium nitriert und gleichzeitig der Kunststoff ausgetrieben. Wird beim Erhitzen eine Temperatur von 13OO Grad Celsius nicht überschritten, bildet sich in bekannter Weise vorwiegend noch sinterfähiges <X - Siliziumnitrid*The production of the reaction-sintered rotor blades 8 can according to one of the known processes for the production of reaction-unified he tem silicon nitride. For example, silicon powder is made into the desired with a binder made of plastic Pressed blade shape. By subsequently heating the rotor blade 8 to temperatures between 1200 and 150 Degrees Celsius in a nitrogen-containing atmosphere, the silicon is nitrided and the plastic is expelled at the same time. When heated, a temperature of 13OO degrees Celsius is not exceeded, forms in a known manner predominantly still sinterable <X - silicon nitride *
Die vorgefertigten reaktionsgesinterten Laufschaufeln 8 werden in der Ringnut 7 der Matrize 3 entsprechend ihrer späteren Anordnung am Laufrad eingesetzt. Dazu werden Stempel k und Mantelteil 2 abgenommen und die Laufschaufeln 8 auf dem Bodenteil 1 fixiert. Die Unterseiten der Schaufelfüße 12 bilden dabei eine geschlossene Ringwand, die als Teil der Matrize 3 wirkt. Nachdem das Mantelteil 2 wieder auf dem Bpdenteil 1 zentriert ist, wird in die Matrize 3 die für die Bildung des Radkörpers 11 notwendige Menge Siliziumnitridpulver geschüttet, dem als Sinterhilfsmittel etwa ein bis fünf Prozent Magnesiumoxidpulver beigemischt ist. Darauf wird der Stempel %k in den Mantelteil 2 der Matrize 3 eingesetzt.The prefabricated reaction-sintered rotor blades 8 are inserted in the annular groove 7 of the die 3 according to their subsequent arrangement on the impeller. For this purpose, the punch k and the casing part 2 are removed and the rotor blades 8 are fixed on the base part 1. The undersides of the blade roots 12 form a closed ring wall that acts as part of the die 3. After the shell part 2 is centered on the base part 1 again, the amount of silicon nitride powder necessary for the formation of the wheel body 11 is poured into the die 3, to which about one to five percent magnesium oxide powder is added as a sintering aid. The punch % k is then inserted into the jacket part 2 of the die 3.
Beim Heißpressen wird das in der Matrize 3 befindliche Pulvergemisch bei einer Temperatur von etwa I65O Grad CelsiusDuring hot pressing, the powder mixture located in the die 3 becomes at a temperature of about 160 degrees Celsius
509825/Q.S68509825 / Q.S68
Palm 9701 APalm 9701 A
Λ-Λ-
unter dem Druck des Stempels h zum Radkörper 11 geformt und gesintert und dabei gleichzeitig mit den in der Ringnut 7 angeordneten reaktionsgesinterten Laufschaufeln 8 zu einem einstückigen Turbinenlaufrad verbunden. Das als Sinterhilfsmittel verwendete Magnesiumoxid hat die Aufgabe, sich mit dem neben dem Siliziumnitrid noch im Pulvergemisch vorhandene Siliziumdioxid zu einem Silikat zu verbinden. Die Silikatteilchen schmelzen beim Überschreiten einer Temperatur von 1500 Grad Celsius und ermöglichen damit das Sintern der Siliziumnitridteilchen zu einem gut verdichteten, porenfreien Radkörper 11, der mit den Laufschaufeln 8 fest verbunden ist.Formed and sintered under the pressure of the punch h to form the wheel body 11 and at the same time connected to the reaction-sintered rotor blades 8 arranged in the annular groove 7 to form a one-piece turbine impeller. The magnesium oxide used as a sintering aid has the task of combining with the silicon dioxide still present in the powder mixture in addition to the silicon nitride to form a silicate. The silicate particles melt when a temperature of 1500 degrees Celsius is exceeded and thus enable the silicon nitride particles to be sintered to form a well-compacted, pore-free wheel body 11 which is firmly connected to the rotor blades 8.
Das durch das beschriebene Verbindungsverfahren aus verschiedenen Bauteilen hergestellte Laufrad vereinigt in vorteilhafter Weise jeweils die günstigsten Eigenschaften sowohl eines reaktionsgesinterten als auch eines heißgepreßten Laufrades in sich. Die guten Pormgebungsmöglichkeiten reaktionsgesinterter Bauteile werden für eine wirtschaftliche Herstellung der komplizierten Gestalt der Laufschaufeln 8 nutzbar gemacht. Besonders wertvoll ist die Eigenschaft der reaktionsgesinterten Laufschaufeln 8, ihre Festigkeit auch bei Erwärmung auf sehr hohe Temperaturen beizubehalten. Dies ist auf das Fehlen von Sinterhilfsmitteln zurückzuführen, die bzw. deren Reaktionsprodukte bei höheren Temperaturen erweichen und damit erheblich an Festigkeit einbüßen. Der durch Zentrifugalkräfte am stärksten beanspruchte Radkörper 11 wird durch Heißpressen hergestellt, das dem Bauteil eine hohe Festigkeit verleiht. Ein wesentliche· Absinken dieser Festigkeit unter die zulässigen Werte bei höherer Temperaturen infolge der beim Heißpressen verwendeten SinterhilfsBittel tritt nicht «in, da der Radkörper 11 im Betrieb nicht so stark erhitzt wird wie die dem heißen Gasstrom un-The impeller produced from various components by the connection method described combines in an advantageous manner Way the most favorable properties of both a reaction-sintered and a hot-pressed one Impeller in itself. The good shaping possibilities Reaction sintered components are used for an economical production of the complicated shape of the rotor blades 8 harnessed. The property of the reaction-sintered rotor blades 8, their strength, is particularly valuable Maintain even when heated to very high temperatures. This is due to the lack of sintering aids, the reaction products or their reaction products soften at higher temperatures and thus lose a considerable amount of strength. The one most exposed to centrifugal forces Wheel body 11 is produced by hot pressing, which gives the component high strength. A substantial · drop This strength falls below the permissible values at higher temperatures as a result of the sintering aids used in hot pressing does not occur because the wheel body 11 is in operation is not heated as much as the one exposed to the hot gas flow
509825/0568509825/0568
- fr- Dft im 9701/4 - fr- Dft in the 9701/4
•Χ*• Χ *
mittelbar ausgesetzten Laufschaufeln 8. Die einfache Form des Radkörpers 11 eignet sich sehr gut für das Heißpressverfahren, da· dagegen beim Herstellen verwickelter Formen sehr aufwendig und damit teuer ist.indirectly exposed blades 8. The simple shape of the wheel body 11 is very suitable for the hot pressing process, on the other hand, when producing intricate shapes is very complex and therefore expensive.
Das nach dem beschriebenen Verfahren zum Verbinden keramischer Bauteile hergestellte integrale Laufrad einer Gasturbine zeichnet sich durch eine wirtschaftliche Herstellung und durch sehr gute Betriebseigenschaften aus. Gegenüber Laufrädern, die aus verschiedenen Werkstoffen zusammengesetzt sind, hat das aus einem Werkstoff hergestellte Laufrad nach der Erfindung infolge seines einheitlichen Wärmeausdehnungskoeffizienten den Vorteil, daß übermäßige Wärmespannungen vermieden werden.The integral impeller of a gas turbine manufactured according to the method described for connecting ceramic components is characterized by economical production and very good operating properties. Opposite to Impellers composed of different materials are, has the impeller made of one material according to the invention due to its uniform coefficient of thermal expansion the advantage that excessive thermal stresses are avoided.
Nach einer weiteren Ausgestaltung des Verfahrens können die vorgesinterten Bauteile vor dem Heißpressen eine Oxydationsbehandlung, beispielsweise bei einer Temperatur von 13ΟΟ Grad Celsius, erhalten. Dies führt zu einer besonders guten Verbindung des reaktionsgesinterten Bauteiles mit dem heißgepreßten Bauteil. Versuche haben gezeigt, daß bei einer Steigerung der mechanischen Belastung bis zum Bruch, dieser nicht von der Verbindungsschicht der Bauteile ausgeht.According to a further embodiment of the method, the pre-sintered components can undergo an oxidation treatment before hot pressing, for example at a temperature of 130 degrees Celsius, received. This leads to a particularly good connection between the reaction-sintered component and the hot-pressed component Component. Tests have shown that if the mechanical load is increased to the point of rupture, the latter does not starts from the connecting layer of the components.
Zur weiteren Verbesserung des Zusammensinterns der Bauteile kann das reaktionsgesinterte und gegebenenfalls durch Oxidieren nachbehandelte Bauteil zusätzlich mit einem Sinterhilfemittel, z.B. durch Einpudern, überzogen werden. Dazu eignen sich Verbindungen und Elemente, die mit Siliziumdioxid Silikat« bilden, z.B. Magnesiumoxid, Bortrioxid, Alurainuraoxid, Lithiumoxid und Berylliumoxid.To further improve the sintering together of the components the reaction-sintered component, which may have been post-treated by oxidation, can also be treated with a sintering aid, e.g. by powdering. Compounds and elements that contain silicon dioxide are suitable for this purpose Form silicate «, e.g. magnesium oxide, boron trioxide, alurainura oxide, Lithium oxide and beryllium oxide.
- 6 509825/0.56« - 6 509825 / 0.56 «
Palm 9701APalm 9701A
reaktionsgesintertem heißgepreßtem Siliziuranitrid, sondern kann sinngemäß auch auf andere Systeme, z.B. rekristallisiertes oder reaktionsgesintertes und heißgepreßtes Siliziumkarbid, übertragen werden. Voraussetzung für eine gute Haltbarkeit ist, daß die zu verbindenden keramischen Bauteile gleiche oder annähernd gleiche Wärmeausdehnungskoeffizienten haben.reaction-sintered hot-pressed silicon uranium nitride, but can also be applied to other systems, e.g. recrystallized or reaction-sintered and hot-pressed silicon carbide, be transmitted. A prerequisite for good durability is that the ceramic to be joined Components have the same or approximately the same coefficient of thermal expansion to have.
50S825/0SG850S825 / 0SG8
Claims (5)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2362469A DE2362469A1 (en) | 1973-12-15 | 1973-12-15 | Joining sintered ceramic components - esp in the mfr of silicon nitride gas turbine impeller wheels |
| JP14206274A JPS5095310A (en) | 1973-12-15 | 1974-12-12 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2362469A DE2362469A1 (en) | 1973-12-15 | 1973-12-15 | Joining sintered ceramic components - esp in the mfr of silicon nitride gas turbine impeller wheels |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE2362469A1 true DE2362469A1 (en) | 1975-06-19 |
Family
ID=5900891
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE2362469A Pending DE2362469A1 (en) | 1973-12-15 | 1973-12-15 | Joining sintered ceramic components - esp in the mfr of silicon nitride gas turbine impeller wheels |
Country Status (2)
| Country | Link |
|---|---|
| JP (1) | JPS5095310A (en) |
| DE (1) | DE2362469A1 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2317502A1 (en) * | 1975-06-27 | 1977-02-04 | Special Metals Corp | COMPOSITE BLADDER WHEELS, ESPECIALLY INTENDED FOR GAS TURBINES, AND THEIR MANUFACTURING PROCESS |
| FR2375696A1 (en) * | 1976-12-21 | 1978-07-21 | Asea Ab | PROCESS FOR ENCLOSING USED NUCLEAR FUEL OR WASTE NUCLEAR FUEL |
| EP0002918A1 (en) * | 1977-12-23 | 1979-07-11 | Ford Motor Company Limited | Method of treating a ceramic body prior to hot pressing and ceramic body thus treated; method of manufacturing a ceramic assembly, and ceramic assembly thereby produced |
| EP0036202A3 (en) * | 1980-03-18 | 1981-10-07 | Mtu Muenchen Gmbh | Container for hot isostatic pressing and hot isostatic pressing process using this container |
| EP0789007A1 (en) * | 1996-02-10 | 1997-08-13 | Forschungszentrum Jülich Gmbh | Joining of non-oxide ceramic, cermets or metallic articles |
| DE102004044942A1 (en) * | 2004-09-16 | 2006-03-30 | Esk Ceramics Gmbh & Co. Kg | Method for low-deformation diffusion welding of ceramic components |
| WO2010121966A1 (en) * | 2009-04-24 | 2010-10-28 | Snecma | Method for manufacturing an assembly including a plurality of blades mounted in a platform |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3241926A1 (en) * | 1982-11-12 | 1984-05-17 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | CONNECTION OF A CERAMIC ROTATION COMPONENT TO A METAL ROTATION COMPONENT FOR FLOW MACHINES, IN PARTICULAR GAS TURBINE ENGINES |
-
1973
- 1973-12-15 DE DE2362469A patent/DE2362469A1/en active Pending
-
1974
- 1974-12-12 JP JP14206274A patent/JPS5095310A/ja active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2317502A1 (en) * | 1975-06-27 | 1977-02-04 | Special Metals Corp | COMPOSITE BLADDER WHEELS, ESPECIALLY INTENDED FOR GAS TURBINES, AND THEIR MANUFACTURING PROCESS |
| FR2375696A1 (en) * | 1976-12-21 | 1978-07-21 | Asea Ab | PROCESS FOR ENCLOSING USED NUCLEAR FUEL OR WASTE NUCLEAR FUEL |
| EP0002918A1 (en) * | 1977-12-23 | 1979-07-11 | Ford Motor Company Limited | Method of treating a ceramic body prior to hot pressing and ceramic body thus treated; method of manufacturing a ceramic assembly, and ceramic assembly thereby produced |
| EP0036202A3 (en) * | 1980-03-18 | 1981-10-07 | Mtu Muenchen Gmbh | Container for hot isostatic pressing and hot isostatic pressing process using this container |
| EP0789007A1 (en) * | 1996-02-10 | 1997-08-13 | Forschungszentrum Jülich Gmbh | Joining of non-oxide ceramic, cermets or metallic articles |
| DE102004044942A1 (en) * | 2004-09-16 | 2006-03-30 | Esk Ceramics Gmbh & Co. Kg | Method for low-deformation diffusion welding of ceramic components |
| US8087567B2 (en) | 2004-09-16 | 2012-01-03 | Esk Ceramics Gmbh & Co., Kg | Process for the low-deformation diffusion welding of ceramic components |
| WO2010121966A1 (en) * | 2009-04-24 | 2010-10-28 | Snecma | Method for manufacturing an assembly including a plurality of blades mounted in a platform |
| FR2944724A1 (en) * | 2009-04-24 | 2010-10-29 | Snecma | METHOD FOR MANUFACTURING AN ASSEMBLY COMPRISING A PLURALITY OF AUBES MOUNTED IN A PLATFORM |
| US9145782B2 (en) | 2009-04-24 | 2015-09-29 | Snecma | Method for manufacturing an assembly including a plurality of blades mounted in a platform |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5095310A (en) | 1975-07-29 |
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