DE1296069B - High temperature resistant molded body - Google Patents
High temperature resistant molded bodyInfo
- Publication number
- DE1296069B DE1296069B DES83320A DES0083320A DE1296069B DE 1296069 B DE1296069 B DE 1296069B DE S83320 A DES83320 A DE S83320A DE S0083320 A DES0083320 A DE S0083320A DE 1296069 B DE1296069 B DE 1296069B
- Authority
- DE
- Germany
- Prior art keywords
- carbide
- base body
- coating
- layer
- graphite
- 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
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 32
- 239000011248 coating agent Substances 0.000 claims description 18
- 238000000576 coating method Methods 0.000 claims description 18
- 229910002804 graphite Inorganic materials 0.000 claims description 18
- 239000010439 graphite Substances 0.000 claims description 18
- 229910052751 metal Inorganic materials 0.000 claims description 15
- 239000002184 metal Substances 0.000 claims description 15
- 229910052799 carbon Inorganic materials 0.000 claims description 13
- 239000000126 substance Substances 0.000 claims description 12
- 150000001247 metal acetylides Chemical class 0.000 claims description 8
- 150000002739 metals Chemical class 0.000 claims description 6
- 229910021332 silicide Inorganic materials 0.000 claims description 6
- FVBUAEGBCNSCDD-UHFFFAOYSA-N silicide(4-) Chemical compound [Si-4] FVBUAEGBCNSCDD-UHFFFAOYSA-N 0.000 claims description 6
- 239000013078 crystal Substances 0.000 claims description 4
- 238000002844 melting Methods 0.000 claims description 4
- 150000004767 nitrides Chemical class 0.000 claims description 3
- 229910052845 zircon Inorganic materials 0.000 claims description 3
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 2
- -1 Titans Chemical compound 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 239000011651 chromium Substances 0.000 claims description 2
- 238000010310 metallurgical process Methods 0.000 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 239000011733 molybdenum Substances 0.000 claims description 2
- 239000000843 powder Substances 0.000 claims description 2
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 2
- 229910052715 tantalum Inorganic materials 0.000 claims description 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 2
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- 239000010937 tungsten Substances 0.000 claims description 2
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 claims 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims 1
- 229910052776 Thorium Inorganic materials 0.000 claims 1
- 229910052790 beryllium Inorganic materials 0.000 claims 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims 1
- 229910052796 boron Inorganic materials 0.000 claims 1
- 239000010410 layer Substances 0.000 description 30
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 16
- 239000011241 protective layer Substances 0.000 description 11
- 239000007789 gas Substances 0.000 description 10
- 229910052786 argon Inorganic materials 0.000 description 8
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 8
- 229910010271 silicon carbide Inorganic materials 0.000 description 8
- 239000000203 mixture Substances 0.000 description 7
- 238000000465 moulding Methods 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 5
- 239000002245 particle Substances 0.000 description 5
- 239000010936 titanium Substances 0.000 description 5
- 229910052719 titanium Inorganic materials 0.000 description 5
- 150000001875 compounds Chemical class 0.000 description 4
- 229910052758 niobium Inorganic materials 0.000 description 4
- 239000010955 niobium Substances 0.000 description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 4
- 239000011148 porous material Substances 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 3
- 229910026551 ZrC Inorganic materials 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 230000006378 damage Effects 0.000 description 3
- UNASZPQZIFZUSI-UHFFFAOYSA-N methylidyneniobium Chemical compound [Nb]#C UNASZPQZIFZUSI-UHFFFAOYSA-N 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000012071 phase Substances 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 229910052726 zirconium Inorganic materials 0.000 description 3
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 2
- OTCHGXYCWNXDOA-UHFFFAOYSA-N [C].[Zr] Chemical compound [C].[Zr] OTCHGXYCWNXDOA-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- NEHMKBQYUWJMIP-UHFFFAOYSA-N chloromethane Chemical compound ClC NEHMKBQYUWJMIP-UHFFFAOYSA-N 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 238000007598 dipping method Methods 0.000 description 2
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 description 1
- 206010010144 Completed suicide Diseases 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910019142 PO4 Inorganic materials 0.000 description 1
- 229910000147 aluminium phosphate Inorganic materials 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 239000007900 aqueous suspension Substances 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000006399 behavior Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 description 1
- 239000004327 boric acid Substances 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 239000012159 carrier gas Substances 0.000 description 1
- 239000003610 charcoal Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000003958 fumigation Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000007770 graphite material Substances 0.000 description 1
- 229910052735 hafnium Inorganic materials 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229940050176 methyl chloride Drugs 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 235000021317 phosphate Nutrition 0.000 description 1
- 150000003013 phosphoric acid derivatives Chemical class 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000035484 reaction time Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000004071 soot Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- YOUIDGQAIILFBW-UHFFFAOYSA-J tetrachlorotungsten Chemical compound Cl[W](Cl)(Cl)Cl YOUIDGQAIILFBW-UHFFFAOYSA-J 0.000 description 1
- 238000005382 thermal cycling Methods 0.000 description 1
- XJDNKRIXUMDJCW-UHFFFAOYSA-J titanium tetrachloride Chemical compound Cl[Ti](Cl)(Cl)Cl XJDNKRIXUMDJCW-UHFFFAOYSA-J 0.000 description 1
- ZOYFEXPFPVDYIS-UHFFFAOYSA-N trichloro(ethyl)silane Chemical compound CC[Si](Cl)(Cl)Cl ZOYFEXPFPVDYIS-UHFFFAOYSA-N 0.000 description 1
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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- C04B14/00—Use of inorganic materials as fillers, e.g. pigments, for mortars, concrete or artificial stone; Treatment of inorganic materials specially adapted to enhance their filling properties in mortars, concrete or artificial stone
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Description
1 21 2
Die Erfindung bezieht sich auf einen hochtempera- Schädigungen der Schutzschicht durch Temperaturturbeständigen Formkörper aus einem Grundkörper Wechselbeanspruchung auf, deren Ursachen imunter- und einem Überzug, bei dem der Grundkörper aus schiedlichen Verhalten des Graphitmaterials des Kohle oder Graphit und darin feinverteilt einem oder Grundkörpers und des Materials der Schutzschicht mehreren der hochschmelzenden Karbide des Beryl- 5 gegenüber Temperaturen zu suchen sind. Dünne Hums, Bors, Siliziums, Titans, Zirkons, Vanadins, Schutzschichten sind außerdem sehr empfindlich Niobs, Tantals, Chroms, Molybdäns, Wolframs, Tho- gegen mechanische Beschädigungen, riums, eines Elementes der seltenen Erden zusam- Es ist auch schon bekannt, poröse Graphitform-The invention relates to high-temperature damage to the protective layer by temperature-turbo-resistant Molded body from a base body to alternating stress, the causes of which sometimes and a coating in which the base body consists of different behaviors of the graphite material Carbon or graphite and finely divided therein a or base body and the material of the protective layer several of the high-melting carbides of Beryl-5 are to be looked for in relation to temperatures. Thin Hums, Bors, Silicon, Titans, Zircon, Vanadins, protective layers are also very sensitive Niobium, tantalum, chromium, molybdenum, tungsten, tho- against mechanical damage, rium, a rare earth element, it is also known that porous graphite forms
mengesetzt ist. körper derart mit Metall zu bedampfen, daß dieis set. body to be vaporized with metal that the
Graphit besitzt eine gute Wärmeleitfähigkeit, eine io Poren oder die Porenwände des Graphitformkörpers geringe thermische Ausdehnung, eine hohe, mit stei- durch das Karbid des aufgedampften Metalls ausgegender Temperatur noch zunehmende Festigkeit und füllt bzw. bedeckt werden, so daß den ganzen Graeine sehr gute Temperaturwechselbeständigkeit. phitkörper Karbidschichten durchdringen. Hierdurch Diese Eigenschaften machen ihn zu einem geschätz- wird jedoch in keiner Weise die Festigkeit gegenüber ten Hochtemperaturwerkstoff. Bei Anwendung höhe- 15 Temperaturwechselbeanspruchungen erhöht. Zwar ist rer Temperaturen ist allerdings eine neutrale oder die auf den Graphitkörper aufgebrachte Karbidreduzierende Atmosphäre notwendig, da Graphit ab schicht mit den aus dem gleichen Stoff bestehenden etwa 500° C mit Sauerstoff oder sauerstoffhaltigen Ausfüllungen der Poren verbunden, die sehr inhomo-Gasen zu reagieren beginnt, so z. B. mit Luft, CO2, gene Zusammensetzung des Formkörpers aus Gra-Wasserdampf u. a. Die Geschwindigkeit der Oxy- 20 phit einerseits und Karbid andererseits mit ihren dation — im technischen Sinn wird hier von Ab- unterschiedlichen Ausdehnungskoeffizienten führt jebrand gesprochen — nimmt mit steigender Tempe- doch bei einer Temperaturwechselbeanspruchung zu ratur zu. einer schnellen Zerstörung des Formkörpers.Graphite has good thermal conductivity, 10 pores or the pore walls of the graphite molding have low thermal expansion, high strength, which increases with the temperature rising through the carbide of the vapor-deposited metal, and is filled or covered, so that the whole of the graphite is very resistant to temperature changes . phite bodies penetrate carbide layers. These properties make it an appreciated one, but in no way is the strength compared to the high-temperature material. When used, 15 thermal cycling increases. Although rer temperatures are, however, a neutral atmosphere or the carbide-reducing atmosphere applied to the graphite body is necessary, since graphite from layer with the approximately 500 ° C consisting of the same substance is connected with oxygen or oxygen-containing fillings of the pores, which begins to react with very inhomo gases , so z. B. with air, CO 2 , the composition of the molded body from Gra water vapor, etc. The speed of the oxyphite on the one hand and carbide on the other hand with their dation - in the technical sense here of different expansion coefficients leads jebrand - increases with increasing temperature - but too rature when exposed to temperature fluctuations. rapid destruction of the molding.
Man kennt eine Reihe von Maßnahmen, die Ab- Der vorliegenden Erfindung liegt die Aufgabe zu-A number of measures are known which, from the present invention, the task is to-
brandfestigkeit von Graphitformkörpern zu erhöhen. 25 gründe, eine bessere Gasdichtheit der Schutzschich-Technisch gebräuchlich ist die Verwendung ab- ten zu erreichen und damit ihre Haltbarkeit zu verbrandvermindernder Mittel, wie Phosphorsäure, größern und dadurch bedingt eine bessere Verhaf-Phosphate, Borsäure und ähnlicher Verbindungen, tung dieser Schichten mit dem Grundkörper zu erdie entweder auf die Oberfläche des Graphitgrund- halten.to increase the fire resistance of graphite moldings. 25 reasons for a better gas tightness of the protective layer It is common to use abten and thus reduce their shelf life by reducing burns Means, like phosphoric acid, increase and therefore better arresting phosphates, Boric acid and similar compounds to earth these layers with the base body either on the surface of the graphite base.
körpers aufgetragen oder in seine oberflächennahen 30 Dies wird bei einem hochtemperaturbeständigen Bereiche imprägniert werden. Dieser Schutz wirkt Formkörper der eingangs genannten Art dadurch ernur innerhalb eines gewissen Temperaturbereichs, reicht, daß erfindungsgemäß der Grundkörper aus vor allem unterhalb 1000° C und da nur temporär. 40 bis 99,5 Volumprozent Kohlenstoff und aus 60 Für höhere Temperaturen hat es sich zum Teil be- bis 0,5 Volumprozent Karbid besteht und nach währt, Schutzschichten aus verschiedenen Stoffen, 35 pulvermetallurgischen Verfahren hergestellt ist und vorwiegend aus Karbiden und Suiziden, auf die daß der — gasdichte — Überzug aus der oder den Oberfläche des Graphitgrundkörpers aufzubringen Karbidkomponenten, wie sie der Grundkörper auf- und damit die zerstörende Einwirkung der Luft vom weist, oder aus einem Stoff besteht, der mit den Graphit fernzuhalten. Karbidkomponenten des Grundkörpers Misch-applied to the body or in its near-surface 30 This will be impregnated at a high temperature-resistant area. This protection acts moldings of the type mentioned at the beginning only within a certain temperature range, sufficient that according to the invention the base body from above all below 1000 ° C. and there only temporarily. 40 to 99.5 percent by volume of carbon and from 60. For higher temperatures it has partly been made up to 0.5 percent by volume of carbide and according to it, protective layers are made from various substances, 35 powder-metallurgical processes and mainly from carbides and suicides, on which that the - gas-tight - coating from the surface or surfaces of the graphite base body is to be applied carbide components, as they are applied by the base body and thus the destructive effect of the air, or consists of a substance that can be kept away with the graphite. Carbide components of the base body mixed
Diese Schichten wurden bereits auf verschiedene 40 kristalle bildet.These layers have already been formed on 40 different crystals.
Weise aufgebracht: durch Tauchen, Aufstreichen, Auf diese Weise erhält man eine chemische Affini-Applied in a way: by dipping, brushing on, in this way one obtains a chemical affinity
Spritzen, Aufschmelzen oder Imprägnieren, mit dem tat zwischen dem Überzugsmaterial und dem Mate-Plasmabrenner oder durch Abscheiden der Verbin- rial des Grundkörpers und damit die Möglichkeit zur düngen aus der Gasphase. Während bei den erst- Bildung chemischer Verbindungen aus den Stoffen genannten Verfahren noch ein nachträgliches Ein- 45 des Überzugs und des Grundkörpers, brennen der Schutzschicht notwendig ist, erübrigt Verwendet man zum Bilden des Überzugs einenSpraying, melting or impregnating, with the tat between the coating material and the Mate plasma torch or by depositing the connector of the base body and thus the possibility of fertilize from the gas phase. While at the first- formation of chemical compounds from the substances a subsequent insertion of the coating and the base body, If the protective layer needs to be fired, it is not necessary to use a to form the coating
sich dies beim Aufbringen der Schutzschichten mit stoff oder ein Stoffgemisch, das ein Metall oder dem Plasmabrenner und bei Abscheidung der Ver- mehrere Metalle der im Grundkörper enthaltenen bindungen aus der Gasphase. Karbidkomponente (Komponenten) rein oder in che-This is the case when the protective layers are applied using a substance or a mixture of substances containing a metal or the plasma torch and when separating the several metals contained in the base body bonds from the gas phase. Carbide component (s) pure or in chemical
Die Verwendung von Schutzschichten erweitert 50 mischer Verbindung enthält, und bringt man diesen zwar den Anwendungsbereich des Graphits bis auf stoff auf die Oberfläche des Grundkörpers, so kann etwa 1500° C, doch treten dabei immer noch eine sich bei Temperpaturen oberhalb 1200° C ein Über-Reihe von Schwierigkeiten auf. ZUg bilden, der aus einem oder mehreren KarbidenThe use of protective layers extends 50 mixer compound contains, and if you bring this the area of application of the graphite down to the surface of the base body, about 1500 ° C, but still occur at temperatures above 1200 ° C over -Base of difficulties. TO form that of one or more carbides
Die Wärmeausdehnung der Graphitformkörper der in dem Stoff enthaltenen Metalle besteht. Ist die und der aufgebrachten Schichten ist im allgemeinen 55 im Grundkörper enthaltene Karbidkomponente idenverschieden. Um dies auszugleichen, dürfen die tisch mit dem Material des Überzugs, so wird eine Schichten nur wenige Mikron stark sein. Es ist aber Verankerung des Überzugs mit der in feiner Verteischwierig, bei dieser geringen Dicke eine hin- lung im Grundkörper vorliegenden Karbidkomporeichende Gasdichtheit zu erreichen. Außerdem be- nente erreicht und eine Verfestigung und Verdichdarf es vieler technischer Kunstgriffe, um sie absolut 60 tung des Überzugs erzielt. Man kann bei dieser Art homogen und ohne Risse aufzubringen. Im Lauf der von Verankerung von einer dübelartigen Befestigung Zeit, bei längerer Beanspruchung unter höheren des Überzugs sprechen. Es tritt daneben noch eine Temperaturen, wandelt sich die Schutzschicht lang- Verschweißung der Karbidpartikeln des Überzugs sam in ein Karbid oder in Karbide mit höherem mit denen des Grundkörpers ein, und dies nicht nur C-Gehalt um. Diese Modifikationsänderung, oft ver- 65 an den Berührungsflächen von Grundkörper und bunden mit Änderungen im Kristallsystem, verändert Überzug, sondern infolge von Festkörperdiffusion die physikalische Beschaffenheit der Schicht, sie wird auch noch innerhalb der oberflächennahen Bereiche spröde und undicht. In vielen Fällen treten auch Be- des Grundkörpers. Ferner wird dabei erreicht, daßThe thermal expansion of the graphite moldings consists of the metals contained in the substance. If the and the applied layers are generally 55 carbide components contained in the base body are identical. To compensate for this, the tables with the material of the coating are allowed, so one layer will only be a few microns thick. It is, however, difficult to anchor the coating with the fine-grained gas-tightness in this small thickness, which is sufficient for the carbide in the base body. In addition, benent is achieved and a solidification and condensation is required of many technical tricks in order to achieve absolute formation of the coating. With this type you can apply homogeneously and without cracks. In the course of anchoring, speak of a dowel-like fastening, in the case of prolonged stress under higher levels of the coating. In addition, there is a temperature, the protective layer long-welding of the carbide particles of the coating is transformed into a carbide or into carbides with a higher level than those of the base body, and this is not just a carbon content. This modification change, often comparable 6 5 brittle at the contact surfaces of the base body and connected with changes in the crystal system changed coating, but as a result of solid state diffusion, the physical nature of the layer, it is also within the near-surface regions and leaking. In many cases, the main body also occurs. It is also achieved that
3 43 4
die thermischen Ausdehnungskoeffizienten von Über- stoff und 24 Volumprozent Siliziumkarbid mit einerthe thermal expansion coefficients of overstock and 24 percent by volume silicon carbide with a
zug und Grundkörper einander angeglichen werden. Porosität von 15% wird auf folgende Weise mit einer Dadurch erhält man eine hohe Temperaturwechsel- gasdichten Siliziumkarbidschicht innen und außentrain and base body are matched to each other. Porosity of 15% is obtained in the following way with a This results in a silicon carbide layer inside and outside that is gas-tight to a high level of temperature change
beständigkeit des Formkörpers. Sinngemäß gilt das gleichmäßig überzogen: Das Kohlerohr wird in einemresistance of the molding. The same applies accordingly: The carbon pipe is in one
gleiche für mischkristallbildende Karbide. 5 Vakuumofen auf 1500° C erhitzt und dann mit Me-same for solid solution forming carbides. 5 vacuum furnace heated to 1500 ° C and then with
Die Aufbringung des Überzugs kann bei Vorliegen thyltrichlorsilan (H3CSiCl3) bei 0,1 AtmosphärenThe application of the coating can be carried out in the presence of ethyltrichlorosilane (H 3 CSiCl 3 ) at 0.1 atmospheres
des Stoffes in flüssiger Phase, beispielsweise durch Druck 2 Stunden begast. Während dieser Zeit schei-of the substance in the liquid phase, for example gassed by pressure for 2 hours. During this time,
Tauchen, Spritzen oder Lackieren des Grundkörpers, det sich auf dem ganzen Körper eine gleichmäßigeDipping, spraying or painting the base body creates a uniform effect on the whole body
geschehen. Verwendet man flüchtige Verbindungen grüne Siliziumkarbidschicht ab in einer Stärke vonhappen. If you use volatile compounds green silicon carbide layer from a thickness of
des Metalls oder der Metalle der obengenannten Art, io 200 bis 250 Mikron. Sie ist sehr dicht und fest inof the metal or metals of the above type, from 200 to 250 microns. It is very dense and tight in
so werden diese Verbindungen durch Erhitzung zer- den Poren des Grundkörpers verankert,
setzt und die betreffenden Komponenten aus derso these connections are anchored by heating the pores of the base body,
sets and the relevant components from the
Gasphase auf dem Grundkörper niedergeschlagen. Beispiel 3Deposited gas phase on the base body. Example 3
Besteht der Stoff zum Bilden des Überzugs ausThe fabric for forming the cover is made up of
dem Metall (den Metallen) der im Grundkörper ent- 15 Zur Erzeugung einer gasdichten Schutzschicht aufthe metal (s) in the base body. 15 To create a gas-tight protective layer
haltenen Karbidkomponente (Komponenten) oder einem Graphitstab (50 · 50 · 1000 mm), der ausholding carbide component (components) or a graphite rod (50 x 50 x 1000 mm), which is made of
aus dem Oxyd, Silizid, Nitrid oder Borid dieses Me- 70 Volumprozent Graphit, 25 Volumprozent Titan-from the oxide, silicide, nitride or boride of this Me- 70 percent by volume graphite, 25 percent by volume titanium
talls (dieser Metalle), so scheidet sich eine Schicht karbid und 5 Volumprozent Wolframkarbid besteht,talls (of these metals), a layer of carbide separates and 5 percent by volume of tungsten carbide consists,
aus dem gewählten Stoff auf dem Grundstoff ab, wird folgendes Verfahren angewandt:from the selected material on the base material, the following procedure is used:
doch bildet sich bei der hohen Abscheidungstempe- 20 Der Stab wird in einem Rohrofen mit 100 mmhowever, at the high separation temperature, the rod is placed in a 100 mm tube furnace
ratur und auch noch während des Betriebs des Form- Innendurchmesser und 3 m Länge in Wasserstoff auftemperature and also during operation of the mold inner diameter and 3 m length in hydrogen
körpers bei höheren Temperaturen eine Zwischen- 1350° C erhitzt. Nach Erreichen dieser TemperaturThe body is heated to an intermediate 1350 ° C at higher temperatures. After reaching this temperature
schicht, die aus dem oder den Karbiden des in dem wird durch eine Zweigleitung ein mit Titanchloridlayer, which is made up of the carbide or carbides of the in which is branched off with titanium chloride
gewählten Stoff enthaltenen Metalls oder der Me- und Wolframchlorid gesättigtes Propan-Wasserstoff-selected substance contained metal or the Me- and tungsten chloride saturated propane-hydrogen
talle besteht. Ein derart behandelter Grundkörper 35 Gemisch (1:100) in den Reaktionsraum eingeleitet,talle exists. A base body treated in this way 35 mixture (1: 100) is introduced into the reaction chamber,
weist sodann einen Überzug aus Karbiden und Nach dreistündiger wechselseitiger Begasung hat sichthen has a coating of carbides and after three hours of mutual fumigation has
außerdem noch eine weitere Schicht, die sogenannte eine 300 bis 400 Mikron starke gasdichte Schicht,In addition, another layer, the so-called a 300 to 400 micron thick gas-tight layer,
Deckschicht, aus dem Metall (den Metallen) oder bestehend aus Titankarbid und Wolframkarbid, ab-Cover layer, made of the metal (s) or consisting of titanium carbide and tungsten carbide,
dessen (deren) Oxyd, Silizid, Nitrid oder Borid auf. geschieden.its oxide, silicide, nitride or boride. divorced.
Die Verdichtung und Verfestigung des Überzugs und 30 Be-ςη'el 4The compaction and solidification of the coating and 30 Be - ςη'el 4
der Deckschicht ist dann besonders gut. "the top layer is then particularly good. "
Bei besonders hohen Anforderungen an die Gas- Zur Erzielung einer gut haftenden und gasdichtenWith particularly high demands on the gas To achieve a well-adhering and gas-tight
dichtigkeit des Formkörpers hat es sich als günstig Oxyddeckschicht auf einem Karbidüberzug geht mantightness of the molded body has proven to be beneficial
erwiesen, wenn die Deckschicht aus einem Oxyd des folgendermaßen vor:proven when the top layer is made of an oxide of the following:
oder der Metalle der im Grundkörper enthaltenen 35 Ein Graphitrohr (Durchmesser 20/10 · 500 mm),or the metals of the 35 contained in the base body a graphite tube (diameter 20/10 500 mm),
Karbidkomponente besteht und in amorpher, glas- 10 Volumprozent Siliziumkarbid enthaltend, wirdThere is a carbide component and an amorphous, glass-containing 10 percent by volume silicon carbide is
artiger Konsistenz vorliegt. Derartige Formkörper mit Siliziumpaste angestrichen und in Argon auflike consistency is present. Such moldings are coated with silicon paste and put in argon
zeichnen sich durch besonders gute Oxydations- 1450° C aufgeheizt und dann mit einem Argon-Me-are characterized by particularly good oxidation 1450 ° C and then heated with an argon
beständigkeit aus, da die Diffusion des Sauerstoffs thylchlorid-Gasgemisch (50:1) etwa 1 Stunde begast.resistance, because the diffusion of the oxygen thyl chloride gas mixture (50: 1) fumigates for about 1 hour.
durch diese wie eine Sperrschicht wirkende Deck- 40 Danach ist der Körper oberflächig mit einer gasdich-through this cover, which acts like a barrier layer, the body is then covered with a gas-tight
schicht auch bei höchsten Verwendungstemperaturen ten Siliziumkarbidschicht überzogen. Nun wird daslayer coated with silicon carbide even at the highest temperatures. Now that will
praktisch unterbunden ist. Methylchlorid abgeschaltet und der Argonstromis practically prevented. Turned off methyl chloride and the argon flow
„ . . T durch eine Waschflasche mit Wasser von 5° C ge-". . T by a washing bottle with water at 5 ° C
ö ei spiel 1 leitet }md über den Siliziumkarbid beschichteten ö ei game 1 leads } md over the silicon carbide coated
EinGraphit-Zirkonkarbidblock(100· 100· 500mm), 45 Körper geleitet. Nach einer Reaktionsdauer von
bestehend aus 85 Volumprozent Graphit 15 Volum- 10 Minuten ist der ganze Körper oberflächig mit
prozent Zirkonkarbid mit einer Porosität von 20% einer sehr dichten, etwa 10 Mikron starken, Siliziumsoll
mit einer Zirkonkarbidschicht überzogen werden. dioxydschicht überzogen.
Dazu wird der Formkörper in einem Tunnelofen auf . .A graphite-zirconium carbide block (100 x 100 x 500mm), 45 bodies passed. After a reaction time of 85 percent by volume graphite 15 percent by volume 10 minutes, the entire body is superficially coated with percent zirconium carbide with a porosity of 20% of a very dense, about 10 micron thick silicon should be coated with a zirconium carbide layer. coated with a layer of dioxide.
For this purpose, the molded body is placed in a tunnel furnace. .
500° C erhitzt und in einem Schutzgasbehälter unter 50 Beispiel 5500 ° C and heated in a protective gas container below 50 Example 5
Argon mit einer Lichtbogen-Spritzpistole oder einem Ein Formkörper, bestehend aus 85 VolumprozentArgon with an arc spray gun or a molded body consisting of 85 percent by volume
Plasmabrenner mit Zirkon gleichmäßig überzogen. Kohlenstoff, 5 Volumprozent Siliziumkarbid und Zur Umwandlung des aufgetragenen Zirkons in Zir- 10 Volumprozent Niobkarbid, wird in Argonatmokonkarbid wird der Formkörper in einen Graphit- Sphäre auf 400° C aufgeheizt. Mit einem Plasmastabbeheizten Ofen eingesetzt, mit Ruß umschüttet 55 brenner wird in bekannter Weise Niobsilizidpulver und in Co bis auf 1600° C erhitzt. Nach Erreichen unter Verwendung von Argon als Trägergas gedieser Temperatur wird dem CO-Gas Methan im Ver- schmolzen und auf den vorgewärmten Körper in hältnis 100:1 zugemischt. Nach einstündiger Tem- feiner Schicht aufgetragen. Dabei reagieren die perung ist alles Zirkon in Karbid umgewandelt. Der schmelzflüssigen Partikelchen des Niobsilizids bei unursprünglich silbrig glänzende Überzug hat nach der 60 mittelbarer Berührung mit der Oberfläche des Grund-Temperung eine dunkelgraue Farbe angenommen. körpers mit dem Kohlenstoff unter Bildung von Er haftet außerordentlich fest auf dem Grundkörper Niobkarbid und Siliziumkarbid. Die darauffolgenden und platzt selbst bei starker Temperaturwechselbean- — äußeren — Teilchen verbleiben in ihrer ursprüngspruchung nicht ab. liehen Zusammensetzung und bilden eine gasdichtePlasma torch evenly coated with zirconium. Carbon, 5 volume percent silicon carbide and To convert the applied zirconium into zirconium 10 percent by volume niobium carbide, argon atomic carbide is used the shaped body is heated to 400 ° C. in a graphite sphere. With a plasma rod heated Oven used, covered with soot 55 burner is niobium silicide powder in a known manner and heated in Co up to 1600 ° C. After reaching this using argon as the carrier gas Temperature is melted into the CO gas methane and on the preheated body in ratio 100: 1 added. Apply a fine layer after an hour. They react perung, all zircon is converted to carbide. Molten particles of niobium silicide at unoriginal Silvery shining coating has after the 60 indirect contact with the surface of the basic tempering assumed a dark gray color. body with the carbon to form It adheres extremely firmly to the base body of niobium carbide and silicon carbide. The following and bursts even with strong temperature changes - - external - particles remain in their original state not off. borrowed composition and form a gas-tight
Beisoiel2 6s Deckschicht aus Niobsilizid.Example2 6s top layer made of niobium silicide.
Um die Gasdichtheit dieser Deckschicht nochTo the gas tightness of this top layer
Ein Kohlerohr (Durchmesser 100/80 · 1000 mm) weiter zu verbessern, wird sie durch die Plasmamit der Zusammensetzung 76 Volumprozent Kohlen- flamme nochmals erweicht, so daß sich durch dasA carbon tube (diameter 100/80 x 1000 mm) is further improved by the Plasmamit of the composition 76 percent by volume of the charcoal flame is softened again, so that the
Zusammenschmelzen der Partikelchen eine porenfreie Schicht auf dem Formkörper bildet.Melting together of the particles forms a pore-free layer on the shaped body.
Ein zylindrischer Körper, Durchmesser 250-300 mm der Zusammensetzung 60 fl/o Kohlenstoff und 40% NbC wird mit einer gut haftenden, dichten Schicht aus HfC folgendermaßen überzogen:A cylindrical body, diameter 250-300 mm with the composition 60 fl / o carbon and 40% NbC is coated with a well-adhering, dense layer of HfC as follows:
Hafnium-Pulver (Teilchengröße 40 μ) wird als wäßrige Suspension auf den Körper oberflächlich aufgestrichen und anschließend bei 110° C getrocknet. Anschließend wird der Körper unter Argon durch einen Hochfrequenzofen oberflächlich kurzzeitig bis auf 2000° C erhitzt. Während dieser Temperaturbehandlung kommt das vorher aufgetragene *5 Hafnium zum Schmelzen und reagiert mit dem Kohlenstoff zum HfC. Letzteres bildet mit demNiobkarbid Mischkristalle vom Typ NbC · HfC.Hafnium powder (particle size 40 μ) is applied as an aqueous suspension on the body superficially brushed on and then dried at 110 ° C. Then the body is under argon The surface is briefly heated up to 2000 ° C by a high-frequency furnace. During this temperature treatment the previously applied * 5 hafnium melts and reacts with the Carbon to the HfC. The latter forms with the niobium carbide Mixed crystals of the type NbC · HfC.
Ein Rohr Durchmesser 70/50 · 2000 mm aus 52«/o Kohlenstoff und 48°/o TiC wird mit einer glatten und gasdichten Schicht aus TiC und Titan auf folgende Weise beschichtet:A tube with a diameter of 70/50 x 2000 mm made of 52% carbon and 48% TiC is fitted with a smooth and gas-tight layer of TiC and titanium coated in the following way:
Mit einer Drahtflammspritzpistole wird auf der Rohroberfläche eine Titanschicht von 0,1 mm Dicke aufgetragen. Anschließend wird diese poröse Schicht mit einem Argonarc-Brenner aufgeschmolzen. Dabei verläuft das Titan zu einer porenfreien Schutzschicht, die durch die Reaktion mit dem Kohlenstoff des Körpers aus einer TiC-Grundschicht und einer Titan-Deckschicht besteht.With a wire flame spray gun, a titanium layer 0.1 mm thick is applied to the pipe surface applied. This porous layer is then melted using an argon arc burner. Included the titanium runs into a pore-free protective layer that reacts with the carbon of the Body consists of a TiC base layer and a titanium top layer.
Claims (2)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DES83320A DE1296069B (en) | 1963-01-18 | 1963-01-18 | High temperature resistant molded body |
CH47564A CH481851A (en) | 1963-01-18 | 1964-01-16 | High-temperature-resistant molded body and process for its production |
GB227364A GB1002790A (en) | 1963-01-18 | 1964-01-17 | Improvements in or relating to carbon bodies |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DES83320A DE1296069B (en) | 1963-01-18 | 1963-01-18 | High temperature resistant molded body |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1296069B true DE1296069B (en) | 1969-05-22 |
Family
ID=7510950
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DES83320A Pending DE1296069B (en) | 1963-01-18 | 1963-01-18 | High temperature resistant molded body |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH481851A (en) |
DE (1) | DE1296069B (en) |
GB (1) | GB1002790A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3990686A (en) * | 1975-02-14 | 1976-11-09 | Toshin Seiko Kabushiki Kaisha | Furnace for producing steel from scrap steel and the like |
US5577596A (en) * | 1993-03-01 | 1996-11-26 | U.S. Philips Corporation | Sorting device with a field of transport units |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4518702A (en) * | 1983-01-19 | 1985-05-21 | Director-General Of The Agency Of Industrial Science And Technology | Silicon carbide-boron carbide carbonaceous body |
GB8804174D0 (en) * | 1988-02-23 | 1988-03-23 | T & N Technology Ltd | Coatings |
CN112341229B (en) * | 2020-11-09 | 2022-09-20 | 航天特种材料及工艺技术研究所 | Gradient C/ZrC-SiC superhigh temperature ceramic matrix composite and preparation method thereof |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2991192A (en) * | 1958-10-30 | 1961-07-04 | Frank A Halden | Process of coating graphite with niobium-titanium carbide |
US2992901A (en) * | 1958-04-29 | 1961-07-18 | Union Carbide Corp | Production of artificial graphite |
US3007805A (en) * | 1957-08-22 | 1961-11-07 | Carborundum Co | Carbide-bonded graphite bodies and method of making the same |
US3017286A (en) * | 1958-09-08 | 1962-01-16 | James S Kane | Method for coating graphite with niobium carbide |
GB903260A (en) * | 1958-12-31 | 1962-08-15 | Atomic Energy Commission | Improvements in or relating to a graphite or carbon article |
-
1963
- 1963-01-18 DE DES83320A patent/DE1296069B/en active Pending
-
1964
- 1964-01-16 CH CH47564A patent/CH481851A/en not_active IP Right Cessation
- 1964-01-17 GB GB227364A patent/GB1002790A/en not_active Expired
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3007805A (en) * | 1957-08-22 | 1961-11-07 | Carborundum Co | Carbide-bonded graphite bodies and method of making the same |
US2992901A (en) * | 1958-04-29 | 1961-07-18 | Union Carbide Corp | Production of artificial graphite |
US3017286A (en) * | 1958-09-08 | 1962-01-16 | James S Kane | Method for coating graphite with niobium carbide |
US2991192A (en) * | 1958-10-30 | 1961-07-04 | Frank A Halden | Process of coating graphite with niobium-titanium carbide |
GB903260A (en) * | 1958-12-31 | 1962-08-15 | Atomic Energy Commission | Improvements in or relating to a graphite or carbon article |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3990686A (en) * | 1975-02-14 | 1976-11-09 | Toshin Seiko Kabushiki Kaisha | Furnace for producing steel from scrap steel and the like |
US5577596A (en) * | 1993-03-01 | 1996-11-26 | U.S. Philips Corporation | Sorting device with a field of transport units |
Also Published As
Publication number | Publication date |
---|---|
GB1002790A (en) | 1965-08-25 |
CH481851A (en) | 1969-11-30 |
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