DE1170748B - Process for coating a molybdenum wire with a carbon layer by thermal decomposition of volatile compounds - Google Patents
Process for coating a molybdenum wire with a carbon layer by thermal decomposition of volatile compoundsInfo
- Publication number
- DE1170748B DE1170748B DEN21817A DEN0021817A DE1170748B DE 1170748 B DE1170748 B DE 1170748B DE N21817 A DEN21817 A DE N21817A DE N0021817 A DEN0021817 A DE N0021817A DE 1170748 B DE1170748 B DE 1170748B
- Authority
- DE
- Germany
- Prior art keywords
- coating
- carbon layer
- molybdenum wire
- wire
- thermal decomposition
- 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
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B1/00—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
- H01B1/02—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
-
- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/02—Pretreatment of the material to be coated
- C23C16/0272—Deposition of sub-layers, e.g. to promote the adhesion of the main coating
-
- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
- C23C16/26—Deposition of carbon only
-
- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/54—Apparatus specially adapted for continuous coating
- C23C16/545—Apparatus specially adapted for continuous coating for coating elongated substrates
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J19/00—Details of vacuum tubes of the types covered by group H01J21/00
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2893/00—Discharge tubes and lamps
- H01J2893/0001—Electrodes and electrode systems suitable for discharge tubes or lamps
- H01J2893/0012—Constructional arrangements
- H01J2893/0019—Chemical composition and manufacture
- H01J2893/0022—Manufacture
- H01J2893/0023—Manufacture carbonising and other surface treatments
-
- 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
- Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
- Y10S264/19—Inorganic fiber
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2918—Rod, strand, filament or fiber including free carbon or carbide or therewith [not as steel]
- Y10T428/292—In coating or impregnation
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/294—Coated or with bond, impregnation or core including metal or compound thereof [excluding glass, ceramic and asbestos]
- Y10T428/2942—Plural coatings
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/294—Coated or with bond, impregnation or core including metal or compound thereof [excluding glass, ceramic and asbestos]
- Y10T428/2958—Metal or metal compound in coating
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/294—Coated or with bond, impregnation or core including metal or compound thereof [excluding glass, ceramic and asbestos]
- Y10T428/296—Rubber, cellulosic or silicic material in coating
Landscapes
- Chemical & Material Sciences (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Resistance Heating (AREA)
- Chemical Vapour Deposition (AREA)
- Carbon And Carbon Compounds (AREA)
Description
DEUTSCHESGERMAN
PATENTAMTPATENT OFFICE
AUSLEGESCHRIFTEDITORIAL
Internat. Kl.: C 23 cBoarding school Class: C 23 c
Deutsche Kl.: 48 b-11/10 German class: 48 b -11/10
Nummer: 1170748Number: 1170748
Aktenzeichen: N 21817 VI b / 48 bFile number: N 21817 VI b / 48 b
Anmeldetag: 10. Juli 1962Filing date: July 10, 1962
Aüslegetag: 21. Mai 1964Lay-out day: May 21, 1964
Die Erfindung bezieht sich auf ein Verfahren zum Überziehen eines Molybdändrahtes mit einer gut haltenden Kohlenstoffschicht bei niedriger Temperatur (etwa 1100° C) und auf eine mit einem solchen Draht versehene Gitterelektrode für eine elektrische Entladungsröhre. The invention relates to a method for coating a molybdenum wire with a well-holding one Carbon layer at low temperature (about 1100 ° C) and on one with such a wire provided grid electrode for an electric discharge tube.
Es ist bekannt, daß eine Kohlenstoffschicht bei etwa 900 bis 1000° C mit einer Molybdänunterlage reagiert, so daß der Kohlenstoff in die Oberfläche verschwindet. Um dies zu verhüten, ist bereits vorgeschlagen worden, eine Zwischenschicht aus einem Karbid, z. B. Siliziumkarbid, dadurch anzubringen, daß der Kern mit Siliziumoxyd und einem kohlenstoffhaltigen Stoff überzogen und daß dann auf 1700 bis 2000° C in einer inerten Atmosphäre erhitzt wird, um die Oxyde zu reduzieren und eine Karbidschicht zu bilden. Auf dieser Schicht konnte eine Kohlenstoffschicht angebracht werden, z. B. in Form von pulvrigem Graphit. Es stellt sich aber heraus, daß der Molybdänkern infolge der starken Erhitzung sehr spröde wird. Im allgemeinen müssen beim bekannten Verfahren denn auch erst die Elektroden gebildet werden, bevor die Karbidschicht und die Kohlenstoffschicht angebracht werden. Dabei war stets eine starke Erhitzung erforderlich, da sonst keine Karbid-Zwischenschicht gebildet wurde. Wurden die Karbide als solche auf der Elektrode angebracht, war eine Erhitzung auf Temperaturen oberhalb 2000° C erforderlich, um die Karbide zu schmelzen zur Erzielung einer guten Haftung der Karbidschicht.It is known that a carbon layer at about 900 to 1000 ° C with a molybdenum underlay reacts so that the carbon disappears into the surface. To prevent this, it has already been suggested an intermediate layer of a carbide, e.g. B. silicon carbide, thereby attaching that the core was coated with silicon oxide and a carbonaceous substance and that then on 1700 is heated to 2000 ° C in an inert atmosphere to reduce the oxides and create a carbide layer to build. A layer of carbon could be applied to this layer, e.g. B. in the form of powdery graphite. It turns out, however, that the molybdenum core as a result of the strong heating becomes brittle. In general, the electrodes must first be formed in the known method before applying the carbide layer and the carbon layer. There was always one strong heating required, otherwise no intermediate carbide layer would be formed. Were the carbides attached as such on the electrode, heating to temperatures above 2000 ° C was necessary, to melt the carbides to achieve good adhesion of the carbide layer.
Jeder Erwartung zuwider hat es sich aber herausgestellt, daß die Bildung einer gut haftenden Zwischenschicht unter einer Kohlenstoffschicht auf einem Molybdändraht bereits bei einer Temperatur von etwa 1100° C möglich ist, so daß der überzogene Molybdändraht seine mechanischen Eigenschaften völlig beibehält und ohne weiteres zu Gitterelektroden verarbeitet werden kann, wenn nach der Erfindung der Molybdändraht zunächst bei einer Temperatur von etwa 900° C durch eine Atmosphäre von Siliziumchlorid (SiCl4) und dann bei etwa 1100° C durch eine Atmosphäre von Tetrachlorkohlenstoff (CCl4) hindurchgeführt wird.Contrary to all expectations, however, it has been found that the formation of a well-adhering intermediate layer under a carbon layer on a molybdenum wire is already possible at a temperature of about 1100 ° C, so that the coated molybdenum wire completely retains its mechanical properties and is easily processed into grid electrodes can be if, according to the invention, the molybdenum wire is first passed through an atmosphere of silicon chloride (SiCl 4 ) at a temperature of about 900 ° C. and then at about 1100 ° C. through an atmosphere of carbon tetrachloride (CCl 4 ).
Es zeigt sich dann, daß der Molybdänkern nach dieser Behandlung mit einer sehr gut haftenden
Zwischenschicht aus Silizium mit einer Kohlenstoffschicht darauf überzogen ist und daß dieser Kern
ohne weiteres zu Gittern gewickelt werden kann, da die aufgebrachten Schichten so dünn sind, daß sie
die mechanischen Eigenschaften des Molybdäns im wesentlichen nicht beeinflussen. Es wird angenommen,
daß die gute Haftung dadurch erhalten wird, Verfahren zum Überziehen eines Molybdändrahtes
mit einer Kohlenstoffschicht durch
thermische Zersetzung flüchtiger VerbindungenIt then turns out that after this treatment the molybdenum core is covered with a very well adhering intermediate layer of silicon with a carbon layer on it and that this core can easily be wound into grids, since the applied layers are so thin that they impair the mechanical properties of the molybdenum essentially do not affect. It is believed that the good adhesion is obtained by methods of coating a molybdenum wire with a carbon layer
thermal decomposition of volatile compounds
Anmelder:Applicant:
N.V. Philips' Gloeilampenfabrieken, EindhovenN.V. Philips' Gloeilampenfabrieken, Eindhoven
(Niederlande)(Netherlands)
Vertreter:Representative:
Dr. rer. nat. P. Roßbach, Patentanwalt,Dr. rer. nat. P. Roßbach, patent attorney,
Hamburg 1, Mönckebergstr. 7Hamburg 1, Mönckebergstr. 7th
Als Erfinder benannt:Named as inventor:
Popko Reinder Dijksterhuis,Popko Reinder Dijksterhuis,
Hans Melsert,Hans Melsert,
Poppe Zuidema, Eindhoven (Niederlande)Poppe Zuidema, Eindhoven (Netherlands)
Beanspruchte Priorität:Claimed priority:
Niederlande vom 14. Juli 1961 (267 095)Netherlands of July 14, 1961 (267 095)
daß vom Mo-Kern her nach der Außenseite die folgenden Schichten vorhanden sind: MoSi2; Si; SiC; C. Es ist überraschend, daß die Reaktion zwischen Si und C, die im allgemeinen nur bei hoher Temperatur stattfindet, jetzt bereits bei etwa 1100° C auftreten kann, wahrscheinlich infolge einer reinigenden Wirkung des Tetrachlorkohlenstoffes.that the following layers are present from the Mo core to the outside: MoSi 2 ; Si; SiC; C. It is surprising that the reaction between Si and C, which generally only takes place at high temperature, can now occur at around 1100 ° C., probably as a result of a cleaning effect of the carbon tetrachloride.
Das Überziehen kann sehr schnell erfolgen. Ein Aufenthalt von IV2 Sekunde in jeder Gasatmosphäre genügt, um den Draht mit einem Gebilde der erwähnten Schichten mit einer Gesamtstärke von etwa μ zu überziehen. Der Draht kann nämlich eine Geschwindigkeit von etwa 1000 bis 2000 m in der Stunde haben, während die Länge der öfen, in denen die Gasatmosphären vorherrschen, etwa 1 m ist.The coating can be done very quickly. A stay of IV2 seconds in any gas atmosphere is sufficient to the wire with a structure of the layers mentioned with a total thickness of about μ to overlay. The wire can namely a speed of about 1000 to 2000 m in the Hours, while the length of the ovens in which the gas atmospheres prevail is about 1 m.
Bei einer geringeren Durchlaufgeschwindigkeit werden die Schichten selbstverständlich stärker.With a lower throughput speed, the layers naturally become thicker.
Die Erfindung wird an Hand einer Zeichnung näher erläutert, in derThe invention is explained in more detail with reference to a drawing in which
Fig. 1 schematisch das Verfahren illustriert undFig. 1 schematically illustrates the method and
Fig. 2 ein mit einem nach der Erfindung überzogenen Molybdändraht hergestelltes Gitter zeigt.Figure 2 shows a grid made with a molybdenum wire coated in accordance with the invention.
In Fig. 1 bezeichnet 1 den Mo-Draht, der von einer Vorratsspule 2 nach einer Vorratsspule 3 läuft und dabei die öfen 4 und 5 passiert. Die ErhitzungIn FIG. 1, 1 denotes the Mo wire which runs from a supply reel 2 to a supply reel 3 passing ovens 4 and 5. The heating
409 590/254409 590/254
des Drahtes erfolgt durch Stromdurchgang durch den Draht 1, z.B. mittels Schleif kontakte 6. Eine geeignete Geschwindigkeit, mit der der Draht die öfen passiert, ist etwa 2000 m/Stunde, wobei die Stärke der Schicht auf dem Draht etwa 1 μ beträgt. Im Ofen 4 wird Siliziumtetrachlorid (SiCl4) und im Ofen 5 Tetrachlorkohlenstoff (CCl4) in Gasform zugeführt. Die Drahtstärke kann 40 bis 150 μ sein.of the wire is carried out by passing current through the wire 1, for example by means of sliding contacts 6. A suitable speed at which the wire passes the ovens is about 2000 m / hour, the thickness of the layer on the wire being about 1 μ. In furnace 4 silicon tetrachloride (SiCl 4 ) and in furnace 5 carbon tetrachloride (CCl 4 ) are fed in gas form. The wire thickness can be 40 to 150 μ.
Das Gitter 9 von F i g. 2 besitzt eine gute Wärmeausstrahlung und eine geringe Primär-und Sekundäremission infolge der schwarzen Kohlenstoffschicht 8 auf der Oberfläche des Drahtes 1. Die Siliziumzwischenschicht ist mit 7 bezeichnet. Die nicht dargestellten Grenzschichten zwischen dem Kern und der Schicht 7 und zwischen den Schichten 7 und 8 bestehen wahrscheinlich aus den Verbindungen MoSi., und SiC, wie bereits angegeben wurde.The grid 9 of FIG. 2 has good heat radiation and low primary and secondary emissions due to the black carbon layer 8 on the surface of the wire 1. The silicon intermediate layer is denoted by 7. The boundary layers, not shown, between the core and of layer 7 and between layers 7 and 8 probably consist of the compounds MoSi., And SiC, as previously indicated.
Claims (1)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NL267095 | 1961-07-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1170748B true DE1170748B (en) | 1964-05-21 |
Family
ID=19753160
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DEN21817A Pending DE1170748B (en) | 1961-07-14 | 1962-07-10 | Process for coating a molybdenum wire with a carbon layer by thermal decomposition of volatile compounds |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3177094A (en) |
| DE (1) | DE1170748B (en) |
| GB (1) | GB979467A (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3479205A (en) * | 1966-10-14 | 1969-11-18 | Gen Electric | Process for producing boron filament |
| US3604970A (en) * | 1968-10-14 | 1971-09-14 | Varian Associates | Nonelectron emissive electrode structure utilizing ion-plated nonemissive coatings |
| US3549413A (en) * | 1969-07-28 | 1970-12-22 | Gen Technologies Corp | Reinforcing filaments comprising coated tungsten wires |
| GB1592063A (en) * | 1978-05-08 | 1981-07-01 | Chloride Silent Power Ltd | Sodium sulphur cells |
| GB9007273D0 (en) * | 1990-03-31 | 1990-05-30 | British Petroleum Co Plc | Process for the manufacture of ceramic fibres |
| US5252359A (en) * | 1990-03-31 | 1993-10-12 | The British Petroleum Company P.L.C. | CVD process for the manufacture of ceramic fibers |
| GB9022267D0 (en) * | 1990-10-13 | 1990-11-28 | British Petroleum Co Plc | Process for depositing a coating on a fibre |
| FR2682125A1 (en) * | 1991-10-07 | 1993-04-09 | Nitruvid | PROCESSING PROCESS FOR DEPOSITING A CARBON LAYER IN A STEAM PHASE ON THE SURFACE OF A METAL PART AND A PART THUS OBTAINED. |
| US7575039B2 (en) * | 2003-10-15 | 2009-08-18 | United Technologies Corporation | Refractory metal core coatings |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US876331A (en) * | 1906-11-30 | 1908-01-14 | Parker Clark Electric Company | Process of making electric-lamp filaments. |
| AT219925B (en) * | 1960-04-02 | 1962-02-26 | Philips Nv | Process for coating molybdenum wire with a layer of carbon |
-
1962
- 1962-06-15 US US202829A patent/US3177094A/en not_active Expired - Lifetime
- 1962-07-10 DE DEN21817A patent/DE1170748B/en active Pending
- 1962-07-11 GB GB26662/62A patent/GB979467A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB979467A (en) | 1965-01-06 |
| US3177094A (en) | 1965-04-06 |
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