DE1293401B - Process for the production of firmly adhering, gas-tight coatings on molded bodies made of niobium or tantalum or alloys of these metals - Google Patents
Process for the production of firmly adhering, gas-tight coatings on molded bodies made of niobium or tantalum or alloys of these metalsInfo
- Publication number
- DE1293401B DE1293401B DEB82521A DEB0082521A DE1293401B DE 1293401 B DE1293401 B DE 1293401B DE B82521 A DEB82521 A DE B82521A DE B0082521 A DEB0082521 A DE B0082521A DE 1293401 B DE1293401 B DE 1293401B
- Authority
- DE
- Germany
- Prior art keywords
- tantalum
- niobium
- metals
- glaze
- gas
- 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
- 229910052751 metal Inorganic materials 0.000 title claims description 34
- 239000002184 metal Substances 0.000 title claims description 34
- 150000002739 metals Chemical class 0.000 title claims description 22
- 238000000576 coating method Methods 0.000 title claims description 20
- 239000010955 niobium Substances 0.000 title claims description 18
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 title claims description 18
- 229910052758 niobium Inorganic materials 0.000 title claims description 17
- 229910052715 tantalum Inorganic materials 0.000 title claims description 17
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 title claims description 17
- 238000000034 method Methods 0.000 title claims description 16
- 229910045601 alloy Inorganic materials 0.000 title claims description 4
- 239000000956 alloy Substances 0.000 title claims description 4
- 238000004519 manufacturing process Methods 0.000 title claims description 4
- 239000011248 coating agent Substances 0.000 claims description 15
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 11
- 229910052710 silicon Inorganic materials 0.000 claims description 11
- 239000010703 silicon Substances 0.000 claims description 11
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 11
- 229910052720 vanadium Inorganic materials 0.000 claims description 10
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 8
- 229910052748 manganese Inorganic materials 0.000 claims description 8
- 239000011572 manganese Substances 0.000 claims description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 5
- 210000003298 dental enamel Anatomy 0.000 claims description 5
- 229910052750 molybdenum Inorganic materials 0.000 claims description 5
- 239000011733 molybdenum Substances 0.000 claims description 5
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 5
- 229910052721 tungsten Inorganic materials 0.000 claims description 5
- 239000010937 tungsten Substances 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 230000001590 oxidative effect Effects 0.000 claims description 4
- 229910052845 zircon Inorganic materials 0.000 claims description 4
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 239000011651 chromium Substances 0.000 claims description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- XUIMIQQOPSSXEZ-NJFSPNSNSA-N silicon-30 atom Chemical compound [30Si] XUIMIQQOPSSXEZ-NJFSPNSNSA-N 0.000 claims description 2
- 239000010410 layer Substances 0.000 description 22
- 239000002002 slurry Substances 0.000 description 11
- 239000000843 powder Substances 0.000 description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 229910052719 titanium Inorganic materials 0.000 description 6
- 239000010936 titanium Substances 0.000 description 6
- 238000000465 moulding Methods 0.000 description 5
- 239000007921 spray Substances 0.000 description 5
- 238000009792 diffusion process Methods 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 239000002344 surface layer Substances 0.000 description 4
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- 229910052786 argon Inorganic materials 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000005422 blasting Methods 0.000 description 3
- 238000005238 degreasing Methods 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 229910044991 metal oxide Inorganic materials 0.000 description 3
- 150000004706 metal oxides Chemical class 0.000 description 3
- 238000002407 reforming Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 238000004031 devitrification Methods 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 238000007654 immersion Methods 0.000 description 2
- NROKBHXJSPEDAR-UHFFFAOYSA-M potassium fluoride Chemical compound [F-].[K+] NROKBHXJSPEDAR-UHFFFAOYSA-M 0.000 description 2
- 239000004925 Acrylic resin Substances 0.000 description 1
- 229920000178 Acrylic resin Polymers 0.000 description 1
- ZOXJGFHDIHLPTG-BJUDXGSMSA-N Boron-10 Chemical compound [10B] ZOXJGFHDIHLPTG-BJUDXGSMSA-N 0.000 description 1
- 101100492787 Caenorhabditis elegans mai-1 gene Proteins 0.000 description 1
- 229910001257 Nb alloy Inorganic materials 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 229910001362 Ta alloys Inorganic materials 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- DJPURDPSZFLWGC-UHFFFAOYSA-N alumanylidyneborane Chemical compound [Al]#B DJPURDPSZFLWGC-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- SVPXDRXYRYOSEX-UHFFFAOYSA-N bentoquatam Chemical class O.O=[Si]=O.O=[Al]O[Al]=O SVPXDRXYRYOSEX-UHFFFAOYSA-N 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000010288 cold spraying Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000012217 deletion Methods 0.000 description 1
- 230000037430 deletion Effects 0.000 description 1
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 description 1
- 238000007688 edging Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- AMWRITDGCCNYAT-UHFFFAOYSA-L manganese oxide Inorganic materials [Mn].O[Mn]=O.O[Mn]=O AMWRITDGCCNYAT-UHFFFAOYSA-L 0.000 description 1
- PPNAOCWZXJOHFK-UHFFFAOYSA-N manganese(2+);oxygen(2-) Chemical class [O-2].[Mn+2] PPNAOCWZXJOHFK-UHFFFAOYSA-N 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 229910052863 mullite Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 235000003270 potassium fluoride Nutrition 0.000 description 1
- 239000011698 potassium fluoride Substances 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229910052851 sillimanite Inorganic materials 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- -1 tantalum or niobium Chemical class 0.000 description 1
- 229910001935 vanadium oxide Inorganic materials 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23D—ENAMELLING OF, OR APPLYING A VITREOUS LAYER TO, METALS
- C23D5/00—Coating with enamels or vitreous layers
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C4/00—Compositions for glass with special properties
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C27/00—Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
- C22C27/02—Alloys based on vanadium, niobium, or tantalum
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C24/00—Coating starting from inorganic powder
- C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
- C23C24/10—Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
- C23C26/02—Coating not provided for in groups C23C2/00 - C23C24/00 applying molten material to the substrate
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/18—After-treatment
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/02—Pretreatment of the material to be coated
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/936—Chemical deposition, e.g. electroless plating
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/937—Sprayed metal
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/938—Vapor deposition or gas diffusion
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/939—Molten or fused coating
Description
1 21 2
Die vorliegende Erfindung betrifft ein Verfahren zur vorwiegend aus Metall besteht, eine geringe Menge
Herstellung festhaftender, gasdichter Überzüge durch Metalloxid kann selbstverständlich darin vorhanden
Aufbringen einer siliziumhaltigen metallischen Schicht sein, ohne daß dadurch die Eigenschaften des Überauf
Formkörper aus Niob oder Tantal oder Legie- zuges, selbst nachdichtend zu sein, verlorengeht,
rungen, welche mindestens 50 Gewichtsprozent Niob 5 Erfindungsgemäß muß die metallische Schicht
oder Tantal enthalten. Vanadium oder Mangan enthalten, um gute Haft-Aus der deutschen Patentschrift 895 848 ist ein Ver- festigkeit zwischen den Partikeln der Metallschicht
fahren zur Herstellung festhaftender, gasdichter Über- und zwischen der Metallschicht und der Unterlage
züge auf Formkörper aus vorzugsweise hochschmel- zu gewährleisten.The present invention relates to a method for mainly consisting of metal, a small amount of production of firmly adhering, gas-tight coatings by metal oxide can of course be present therein, application of a silicon-containing metallic layer, without thereby affecting the properties of the over-molded body made of niobium or tantalum or alloy, to be self-proofing is lost,
ments which contain at least 50 percent by weight niobium 5 According to the invention, the metallic layer or tantalum must contain. Vanadium or manganese are contained in order to ensure good adhesion between the particles of the metal layer to produce firmly adhering, gas-tight overlay and between the metal layer and the underlay on molded bodies, preferably of high melting point.
zenden Metallen, wie Tantal oder Niob, bekannt. io (Der Ausdruck »Metall« in dieser Beschreibung soll
Hierbei wird zunächst eine auf dem Formkörper auch Silizium und Bor mit umfassen.)
haftende Oxidschicht durch Oxydation eines auf den Dadurch, daß man den Überzug in Form einer
Formkörper aufgebrachten metallischen Überzuges Glasur herstellt, wird eine bessere Beständigkeit gegen
hergestellt. Als metallischer Überzug wird eine Zwischenraumdurchdringung durch solche Gase, wie
Siliziumlegierung aufgebracht, die oxydiert wird; nach 15 Sauerstoff, Stickstoff oder Wasserstoff, erzielt, wie sie
Aufbringen einer weiteren Oxidschicht wird so stark mit unglasierten Überzügen erreicht werden könnte,
erhitzt, daß die Oxidschicht glasurartig niederschmilzt. Es ist jedoch erforderlich, daß die Glasur gegen Ent-Ein
derartiger Überzug hat den Nachteil, daß, wenn glasung beständig ist. Im allgemeinen ist die Glasur
die Emailschicht reißt oder porös wird, eine auto- um so beständiger gegen Entglasung, je komplexer
matische Ausbildung der Email nicht möglich ist. 20 ihre Zusammensetzung ist; das ist sehr wichtig für
Der vorliegenden Erfindung liegt nun die Aufgabe Glasuren, welche bei relativ niedrigen Temperaturen,
zugrunde, ein Verfahren zu schaffen, durch das dieser wie etwa 11000C oder weniger, einer Entglasung ausNachteil
behoben wird. Die Erfindung betrifft somit gesetzt sind. Ein hinreichendes Maß an Beständigkeit
ein Verfahren zur Herstellung festhaftender, gasdichter wird dadurch erzielt, daß man mindestens fünf EIe-Überzüge
durch Aufbringen einer siliziumhaltigen 25 mente einbezieht. Die Gegenwart von Silizium und
metallischen Schicht auf Formkörper aus Niob oder entweder Vanadium oder Mangan (oder beiden) ist
Tantal oder Legierungen, welche mindestens 50 Ge- erforderlich, da zunächst eine gesinterte Schicht der
wichtsprozent Niob oder Tantal enthalten. Es ist Elemente in metallischer Form auf dem Gegenstand
dadurch gekennzeichnet, daß die metallische Schicht gebildet und dann oxydiert und glasiert wird, weil das
die nachstehend aufgeführten Metalle innerhalb der 30 Silizium, Vanadium und Mangan eine flüssige Phase
angegebenen Mengenbereiche enthält (in Gewichts- von relativ niedrigem Schmelzpunkt bilden, welche das
prozent): . Sintern der anderen Bestandteile unter Bildung einesedging metals, such as tantalum or niobium, are known. io (The term “metal” in this description is intended to initially include silicon and boron on the molded body.)
Adhesive oxide layer by oxidation of a metallic coating applied to the glaze by producing the coating in the form of a molded body, a better resistance to glaze is produced. As a metallic coating, a gap penetration is applied by such gases as silicon alloy, which is oxidized; after 15 oxygen, nitrogen or hydrogen, achieved, as it could be achieved with unglazed coatings, the application of a further oxide layer is so strong that the oxide layer melts down like a glaze. It is necessary, however, that the glaze against deletion. Such a coating has the disadvantage that if glaze is resistant. In general, the glaze is the enamel layer cracks or becomes porous, automatically more resistant to devitrification, the more complex the matic formation of the enamel is not possible. 20 is their composition; this is very important for the present invention It is an object glazes, which at relatively low temperatures, the invention to provide a method by which this or about 1100 0 C or less, devitrification ausNachteil is resolved. The invention relates to are thus set. A sufficient degree of resistance in a process for the production of firmly adhering, gas-tight ones is achieved by including at least five EIe coatings by applying a silicon-containing element. The presence of silicon and metallic layer on shaped bodies made of niobium or either vanadium or manganese (or both) is tantalum or alloys, which at least 50 Ge are required, since initially a sintered layer contains the weight percent niobium or tantalum. Elements in metallic form on the object are characterized in that the metallic layer is formed and then oxidized and glazed because it contains the metals listed below within the quantity ranges indicated in a liquid phase (in weight from relative low melting point, which is the percentage):. Sintering the other components to form one
(a) Silizium 30 bis 50; festhaftenden Überzuges erleichtern. Es wurde auch(a) silicon 30 to 50; make it easier to use a firmly adhering coating. It was too
(b) Vanadium oder Mangan 5 bis 25 oder sowohl gefunden, daß das nachfolgende Einverleiben von Vanadium als auch Mangan, insgesamt 10 bis 25, 35 Vanadium und/oder Manganoxiden in die Ober- und flächenschicht zur Bildung einer homogenen Glasur(b) Vanadium or Manganese 5 to 25 or both found that the subsequent incorporation of Vanadium and manganese, a total of 10 to 25, 35 vanadium and / or manganese oxides in the upper and surface layer to form a homogeneous glaze
(c) mindestens drei der nachfolgenden Elemente: beiträgt.(c) at least three of the following: contributes.
j t 1 51- 5Q Bei einer bevorzugten Ausführungsform des erfin-j t 1 51-5Q In a preferred embodiment of the
2^0J3 5 bis 50 dungsgemäßen Verfahrens wird ein festhaftender Über-2 ^ 0 J 3 5 to 50 according to the method, a firmly adhering over-
WoIfram 3 bis 25 4° zu^ aus den Metallbestandteilen der Glasur oderWoIfram 3 to 25 4 ° zu ^ from the metal components of the glaze or
Molybdän 3 bis 25 zumindest aus solchen Metallen, die noch nicht in derMolybdenum 3 to 25 at least from those metals that are not yet in the
Chrom 3 bis 25 Grundmasse des Formkörpers vorhanden sind, aufChromium 3 to 25 basic mass of the shaped body are present
jjt 3 bis 25 ^e Oberfläche des Formkörpers dadurch aufgetragen,jj t 3 to 25 ^ e surface of the molding applied thereby,
Zirkon' 3 bis 25 da^ mai1 denselben in eine Aufschlämmung eintauchtZircon '3 to 25 ^ since mai1 same into a slurry dips
Aluminium '.".'.'.''.'.'.'.'.'.'.'.'.'.'.'. 3 bis 25 45 oder einem r Kalt" 0?er Heißsprühverfahren unter-Aluminum '. ".'. '.''.'.'.'.'.'.'.'.'.'.'.'. 3 to 25 45 or a r cold " 0 ? he hot spray process
g α bis 15 wirft, worauf man erhitzt, um den Überzug aui deng α to 15 throws, whereupon it is heated to the coating aui
Formkörper aufzuschmelzen, ihn zu oxydieren und zuTo melt molded body, to oxidize it and to
wobei der Gesamtgehalt an Tantal und Niob glasieren. Dieses Verfahren kann auch dazu verwendetthe total content of tantalum and niobium glaze. This procedure can also be used
50 Gewichtsprozent nicht überschreitet, und daß werden, um Formkörper zu überziehen, welche früherDoes not exceed 50 percent by weight, and that will be used to coat molded articles, which earlier
nach dem Trocknen der metallischen Schicht der 50 einer schützenden metallisierenden Behandlung nachafter the drying of the metallic layer of the 50 a protective metallizing treatment
Formkörper in oxydierender Atmosphäre so stark der gleichen oder einer anderen Methode unterworfenShaped body in an oxidizing atmosphere so strongly subjected to the same or a different method
erhitzt wird, daß die Metalle in der Außenschicht wurden, wobei die abschließende Behandlung ent-is heated so that the metals in the outer layer have become, the final treatment being
des Überzuges in Oxide umgewandelt werden und weder deshalb vorgenommen wird, um den allgemeinenof the coating are converted into oxides and neither is therefore made to the general
die Oxide unter Bildung eines Emails schmelzen. Schutz zu verstärken, oder um Teile des früher gebil-the oxides melt to form an enamel. To reinforce protection, or to remove parts of
Im Gegensatz zu dem bekannten Verfahren wird 55 deten Überzuges, welcher abgenutzt oder entferntIn contrast to the known method, the coating is worn or removed
erfindungsgemäß keine Metalloxidschicht, sondern wurde, auszubessern.according to the invention no metal oxide layer, but was to be repaired.
zuerst eine Metallschicht aufgebracht, durch welche Nach einer anderen Ausführungsform des erfindungseine
automatische Nachbildung der Emailschicht gemäßen Verfahrens werden die metallischen Bestandmöglich ist. Wird diese rissig oder porös, so wird die teile der Glasur oder zumindest solche, welche nicht
Metallschicht darunter ausreichend hoch erhitzt, daß 60 in der Grundmasse des Formkörpers enthalten sind,
sich örtlich Oxide bilden, welche dann emailliert in die Oberfläche des Gegenstandes unter Bildung einer
werden. Bei der Oxydation der Außenschicht wird modifizierten Oberflächenschicht eindiffundiert, und
wahrscheinlich in der darunterliegenden Schicht ein der Formkörper wird dann unter oxydierenden Bedinmehr
oder weniger kleiner Teil des Metalls zum Oxid gungen erhitzt, um die Metalle in mindestens der
mit oxydiert, da einige in der Schicht vorhandenen 65 Außenschicht in die Oxide überzuführen und um die
Metalle bei einer gegebenen Oxydationsbehandlung Oxide unter Bildung einer Glasur zu schmelzen,
schneller und bis zu einer größeren Tiefe oxydiert Die nachfolgenden Beispiele dienen der Erläuterung
werden als andere. Wesentlich ist, daß diese Schicht der Erfindung und ihrer Ausführung.First a metal layer is applied, through which, according to another embodiment of the method according to the invention, an automatic replica of the enamel layer is possible, the metallic constituents are possible. If this becomes cracked or porous, the parts of the glaze or at least those that do not have a metal layer underneath are heated sufficiently high that 60 are contained in the basic mass of the molded body, locally formed oxides, which are then enamelled in the surface of the object to form a will. During the oxidation of the outer layer, a modified surface layer is diffused in, and probably in the layer below one of the shaped bodies is then heated under oxidizing conditions to form the oxide, in order to oxidize the metals in at least one of them, as some are present in the layer 65 to convert the outer layer into the oxides and to melt the metals with a given oxidation treatment oxides to form a glaze,
oxidized faster and to a greater depth The examples below are illustrative than others. It is essential that this layer of the invention and its implementation.
Ein aus Niob bestehender Formkörper wird einem Dampfentfettungsverfahren und einem Dampfstrahlverfahren unter Anwendung eines milden Schmiergels unterworfen, um eine feine matte Oberfläche zu erzielen.A molded body made of niobium is subjected to a vapor degreasing method and a steam jet method subjected using a mild lubricating gel to a fine matte surface achieve.
Nach dem Entfetten und Dampfstrahlen wird der Formkörper, welcher gegebenenfalls schon einer Diffusionsbehandlung mit Silizium und/oder anderen Metallen unterworfen wurde, in eine Aufschlämmung eingetaucht, welche aus den metallischen Bestandteilen der Glasur einschließlich Silizium, Vanadium und/oder Mangan in der Form eines Pulvers von 0,075 mm Korngröße und aus einem suspensionsfördernden Mittel, wie modifiziertem Bentonit, und einem Bindemittel, wie einem Acrylharz, in Toluol besteht. Das Eintauchen mit dazwischengeschobenem Trockenen wird nötigenfalls wiederholt, um einen trockenen Überzug von 0,075 bis 0,125 mm Dicke zu erzielen.After degreasing and steam blasting, the molded body, which may already be one Diffusion treatment with silicon and / or other metals has been subjected to a slurry immersed, which consists of the metallic components of the glaze including silicon, vanadium and / or manganese in the form of a powder of 0.075 mm grain size and of a suspension-promoting Agents such as modified bentonite and a binder such as an acrylic resin in toluene consists. The immersion with dryness in between is repeated if necessary to obtain a dry coating of 0.075 to 0.125 mm thickness.
Nach einer anderen Methode kann die Aufschlämmung mittels einer druckluftbetriebenen Spritzpistole auf den Formkörper aufgesprüht werden, wobei dazwischen nötigenfalls getrocknet wird.Another method is to use a compressed air spray gun to spray the slurry be sprayed onto the shaped body, drying if necessary in between.
Der Formkörper mit dem trockenen haftenden Überzug wird dann in einem Vakuum von mindestens 10~4 mm Quecksilber oder in Argon 3 Stunden auf 135O0C erwärmt oder auf eine etwas höhere Temperatur für eine kürzere Zeit, um den Überzug zu schmelzen und teilweise in den Formkörper eindiffundieren zu lassen, wobei dieser Vorgang durch die Gegenwart des Siliziums und Vanadiums und/oder Mangans erleichtert wird. Abschließend wird der Formkörper in Luft 1 bis 3 Stunden auf 13000C erhitzt, um die Oxydation und das Glasieren des Überzuges zu bewirken.The molded body with the dry adhesive coating is then heated in a vacuum of at least 10 -4 mmHg or in argon for 3 hours at 135 ° 0 C and to melt at a somewhat higher temperature for a shorter time to the coating and partially into the shaped body to diffuse in, this process is facilitated by the presence of the silicon and vanadium and / or manganese. Finally, the molded body in air for 1 to 3 hours at 1300 0 C is heated to the oxidation and glazing effect of the coating.
Wenn es sich um einen Formkörper handelt, welcher früher mit Silizium und/oder anderen Metallen unter Bildung eines schützenden Überzuges behandelt worden ist, kann das erste Erwärmen in Vakuum oder Argon unterbleiben, so daß die Behandlung aus einem Erhitzen in Luft für etwa 3 Stunden bei 1300 bis 1350° C besteht.If it is a shaped body, which earlier with silicon and / or other metals under Formation of a protective coating has been treated, the first heating in vacuum or Argon is omitted, so the treatment consists of heating in air for about 3 hours at 1300 to 1350 ° C.
Die folgende Tabelle gibt die Zusammensetzung von zwei Auf schlämmungen wieder:The following table gives the composition of two slurries:
GewichtsA.
Weight
ProzentB.
percent
733
7th
1333
13th
77th
7th
420
42
7
722nd
7th
7th
0
07th
0
0
05
0
00
0
05
0
50
5
5555
6060
Die Mengenanteile der Metalle in der Aufschlämmung entsprechen denen der Metalle in der endgültigen Glasur, abgesehen von der Diffusion von Metallen aus dem Formkörper.The proportions of metals in the slurry correspond to those of the metals in the final Glaze, apart from the diffusion of metals from the molded body.
Durch Variieren der Mengenanteile der Bestandteile der Aufschlämmung ist es möglich, die Reformierungstemperatur der Glasur zu steuern. Die Bedeutung dieser Erscheinung liegt darin, daß, falls die Glasur rissig oder durchlöchert wird, die dann frei werdende Oberfläche, die aus Metallen oder einem Gemisch von Metallen und Metalloxiden bestehen kann, automatisch erneut glasiert wird, sobald der Gegenstand während seines Gebrauches auf eine Temperatur oberhalb der Glasurreformierungstemperatur erwärmt wird.By varying the proportions of the components of the slurry, it is possible to adjust the reforming temperature to control the glaze. The significance of this phenomenon is that, if the glaze is cracked or perforated, the surface that is then exposed, which is made of metals or a mixture of Metals and metal oxides can be automatically re-glazed as soon as the object is during its use is heated to a temperature above the glaze reforming temperature.
Die Glasurreformierungstemperatur der Metalle von Aufschlämmung A beträgt etwa 12000C, während die der Metalle von Aufschlämmung B etwa 14000C beträgt.The glaze reforming temperature of the metals of slurry A is about 1200 ° C., while that of the metals of slurry B is about 1400 ° C.
Nach diesem Verfahren hergestellte Formkörper haben eine Lebensdauer von 150 bis 200 Stunden bei 13000C in oxydierenden Gasen.According to this method moldings produced a lifetime of 150 to 200 hours at 1300 0 C in oxidizing gases have.
Formkörper aus Tantal können in der gleichen Weise behandelt werden, wobei jedoch der Tantalgehalt in der Aufschlämmung durch Niob ersetzt wird, damit die Glasur die gleiche komplexe Zusammensetzung hat.Moldings made of tantalum can be treated in the same way, but the tantalum content in the slurry is replaced with niobium so that the glaze has the same complex composition.
Ebenso ist es bei Formkörpern aus Niob- oder Tantallegierungen, die Metalle, wie Wolfram und Titan, enthalten, welche in der Glasur erwünscht sind, nicht notwendig, diese Metalle in die Aufschlämmung einzubeziehen. Indem man jedoch einen Anteil dieser Metalle oder einiger von ihnen in die Aufschlämmung aufnimmt, ist es möglich, ihren Mengenanteil, mit welchem sie in der Glasur vorhanden sind, zu erhöhen.It is the same with moldings made of niobium or tantalum alloys, the metals such as tungsten and Titanium, which are desirable in the glaze, do not need to contain these metals in the slurry to be included. However, by adding a proportion of these metals or some of them to the slurry absorbs, it is possible to increase their proportion with which they are present in the glaze.
Dieses Beispiel entspricht dem Beispiel 1 mit der Ausnahme, daß der festhaftende Überzug durch Heißsprühen, z. B. durch Schlammsprühen oder mittels eines Plasmabogens aufgetragen wird. Außerdem kann das anfängliche Wärmen im Vakuum oder in Argon unterbleiben, so daß das Schmelzen, Diffundieren und Glasieren in einer einzigen Erwärmungsperiode in Luft in etwa 3 Stunden bei 13000C durchgeführt wird.This example is the same as Example 1 with the exception that the adherent coating is hot sprayed, e.g. B. is applied by mud spray or by means of a plasma arc. In addition, the initial heating in a vacuum or in argon can be omitted, so that the melting, diffusing and glazing is carried out in a single heating period in air in about 3 hours at 1300 ° C.
Das Heiß- oder Kaltsprühen ist besonders für Formkörper von einfacher Gestalt geeignet, z. B. für Gasturbinenschaufeln, während das Eintauchen bei Gegenständen von komplizierter Gestalt vorzusehen ist, z. B. für Verbrennungskammern von Gasturbinenantriebswerken. Hot or cold spraying is particularly suitable for moldings of simple shape, e.g. B. for gas turbine blades, while immersion is to be provided for objects of complex shape, z. B. for combustion chambers of gas turbine engines.
Nach dem Entfetten und Dampfstrahlen wird ein Formkörper aus Niob in ein Gemisch aus Metallpulvern von etwa 0,1 bis 0,075 mm Korngröße zusammen mit etwa 0,5 Gewichtsprozent Kaliumfiuorid gepackt, welches sich in einem feuerfesten Behälter befindet, z. B. aus Aluminiumoxid, Sillimanit oder Mullit, welcher einen locker sitzenden Deckel hat. Das Metallpulver enthält (in Gewichtsprozent) 33 Silizium, 7 Vanadium, 7 Mangan, 7 Tantal, 22 Wolfram, 7 Molybdän, 7 Chrom, 5 Titan und 5 Aluminium.After degreasing and steam blasting, a molded body made of niobium is converted into a mixture of metal powders from about 0.1 to 0.075 mm grain size together with about 0.5 weight percent potassium fluoride packed, which is in a refractory container, e.g. B. made of aluminum oxide, sillimanite or Mullite, which has a loosely fitting lid. The metal powder contains (in percent by weight) 33 silicon, 7 vanadium, 7 manganese, 7 tantalum, 22 tungsten, 7 molybdenum, 7 chromium, 5 titanium and 5 aluminum.
Der Behälter wird dann in Vakuum von mindestens ΙΟ"4 mm Quecksilber 3 Stunden auf eine Temperatur von 1350° C oder eine längere Zeit auf 1300° C erwärmt, damit das Metallpulver in dem Formkörper diffundiert. Der Formkörper erhält dadurch einen Überzug, welcher aus Niob, aus dem Formkörper stammend, und aus den Metallbestandteilen des Behandlungspulvers besteht. The container is then heated in a vacuum of at least ΙΟ " 4 mm of mercury for 3 hours to a temperature of 1350 ° C or a longer time to 1300 ° C so that the metal powder diffuses in the molded body. The molded body receives a coating that consists of niobium , originating from the molded body, and consists of the metal components of the treatment powder.
Nachdem sich der Behälter auf Handhabungstemperatur abgekühlt hat, wird der Formkörper herausgenommen und durch Abbürsten des lockeren Pulvers und Waschen in heißem Wasser gereinigt. ErAfter the container has cooled to handling temperature, the molded body taken out and cleaned by brushing off the loose powder and washing in hot water. He
wird darauf 1 bis 3 Stunden in Luft auf eine Temperatur von 1300° C erhitzt, bis die Oberfläche oxydiert ist und die Oxide unter Bildung einer Oberflächenschicht in Form einer Glasur geschmolzen sind.is then 1 to 3 hours in air at a temperature heated from 1300 ° C until the surface is oxidized and the oxides forming a surface layer melted in the form of a glaze.
Dieses Beispiel unterscheidet sich vom Beispiel III dadurch, daß nach dem Reinigen und Dampfstrahlen, jedoch vor dem Durchführen der Diffusion und der Glasierungsbehandlung, eine Oberflächenschicht des Gegenstandes dadurch modifiziert wird, daß man Titan hineindiffundieren läßt. Es wurde gefunden, daß diese Vorbehandlung die nachfolgende Bildung einer gleichmäßigen Glasur erleichtert.This example differs from Example III in that after cleaning and steam blasting, however, before performing the diffusion and glazing treatment, a surface layer of the Object is modified by allowing titanium to diffuse into it. It was found that this Pretreatment facilitates the subsequent formation of an even glaze.
Das Diffundieren von Titan in den Formkörpern wird vorzugsweise durch Erwärmen im Vakuum in der vorstehend beschriebenen Weise durchgeführt, mit der Ausnahme, daß das komplexe Metallpulver durch Titanpulver von etwa 0,4 mm Korngröße ersetzt wird und daß das Erwärmen 5 bis 10 Stunden bei etwa 11600C durchgeführt wird.The diffusion of titanium in the shaped bodies is preferably carried out by heating in vacuo in the manner described above, with the exception that the complex metal powder is replaced by titanium powder of about 0.4 mm grain size and that the heating is carried out at about 1160 for 5 to 10 hours 0 C is carried out.
Während bei den Beispielen I und II die verschiedenen Bestandteile eines Bades oder einer Sprühlösung innerhalb der gleichen Bereiche liegen können, wie sie für die Metallbestandteile der Glasur angegeben wird, bestehen für die in beiden Beispielen III und IV angewendeten Gemische herabgesetzte obere Grenzen für einige Metalle, nämlich (in Gewichtsprozent)While in Examples I and II the various components of a bath or a spray solution can lie within the same ranges as specified for the metal components of the glaze, there are reduced upper limits for the mixtures used in both Examples III and IV for some metals, namely (in percent by weight)
Mangan 15Manganese 15
Tantal 25Tantalum 25
Niob 25Niobium 25
Tantal und Niob zusammen 25Tantalum and niobium together 25
Wolfram 10Tungsten 10
Molybdän 10Molybdenum 10
Chrom 10Chrome 10
Titan 10Titanium 10
Zirkon 10Zircon 10
Aluminium 15Aluminum 15
Bor 10Boron 10
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB24103/64A GB1113066A (en) | 1964-06-24 | 1964-06-24 | Improvements in refractory metal articles |
Publications (1)
Publication Number | Publication Date |
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DE1293401B true DE1293401B (en) | 1969-04-24 |
Family
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---|---|---|---|
DEB82521A Pending DE1293401B (en) | 1964-06-24 | 1965-06-23 | Process for the production of firmly adhering, gas-tight coatings on molded bodies made of niobium or tantalum or alloys of these metals |
Country Status (3)
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US (1) | US3446655A (en) |
DE (1) | DE1293401B (en) |
GB (1) | GB1113066A (en) |
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Publication number | Priority date | Publication date | Assignee | Title |
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US3664884A (en) * | 1968-03-11 | 1972-05-23 | Concept Research Corp | Method of coloring metals by the application of heat |
US5786031A (en) * | 1995-06-07 | 1998-07-28 | Engelhard Corporation | Barrier for a metal substrate |
US6521356B2 (en) * | 2001-02-02 | 2003-02-18 | General Electric Company | Oxidation resistant coatings for niobium-based silicide composites |
CN103215614B (en) * | 2013-04-27 | 2015-05-27 | 中国船舶重工集团公司第七二五研究所 | Preparation method of metallic oxide anode containing cold spraying tantalum intermediate layer |
CN105483596B (en) * | 2015-11-14 | 2018-08-07 | 河南永业环保工程有限公司 | A kind of preparation method of inorganic coating |
CN110551878B (en) * | 2019-10-12 | 2021-06-08 | 东北大学 | Ultrahigh-strength ultrahigh-toughness low-density dual-phase layered steel plate and preparation method thereof |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
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DE895848C (en) * | 1950-01-11 | 1953-11-05 | Metallwerk Plansee G M B H | Process for the production of firmly adhering, gas-tight coatings on molded bodies made of preferably high-melting metals |
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US2809127A (en) * | 1948-11-19 | 1957-10-08 | Metal Gas Company Ltd | Surface treatment of metals |
GB676913A (en) * | 1950-04-25 | 1952-08-06 | Metro Cutanit Ltd | Improvements relating to the production of adherent coatings on metallic bodies |
US3037883A (en) * | 1959-02-18 | 1962-06-05 | Chromalloy Corp | Diffusion coating of non-ferrous metals |
US3317343A (en) * | 1963-02-01 | 1967-05-02 | Richard A Jefferys | Activated coating of columbium metal |
US3293068A (en) * | 1963-08-19 | 1966-12-20 | United Aircraft Corp | Coatings for columbium base alloys |
-
1964
- 1964-06-24 GB GB24103/64A patent/GB1113066A/en not_active Expired
-
1965
- 1965-06-22 US US466113A patent/US3446655A/en not_active Expired - Lifetime
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DE895848C (en) * | 1950-01-11 | 1953-11-05 | Metallwerk Plansee G M B H | Process for the production of firmly adhering, gas-tight coatings on molded bodies made of preferably high-melting metals |
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