US3772096A - Method for the manufacture of an element of watch case and element of watch case obtained by this method - Google Patents
Method for the manufacture of an element of watch case and element of watch case obtained by this method Download PDFInfo
- Publication number
- US3772096A US3772096A US00216275A US3772096DA US3772096A US 3772096 A US3772096 A US 3772096A US 00216275 A US00216275 A US 00216275A US 3772096D A US3772096D A US 3772096DA US 3772096 A US3772096 A US 3772096A
- Authority
- US
- United States
- Prior art keywords
- watch case
- hardening
- fact
- molybdenum
- carried out
- 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.)
- Expired - Lifetime
Links
Classifications
-
- G—PHYSICS
- G04—HOROLOGY
- G04D—APPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
- G04D3/00—Watchmakers' or watch-repairers' machines or tools for working materials
- G04D3/0074—Watchmakers' or watch-repairers' machines or tools for working materials for treatment of the material, e.g. surface treatment
- G04D3/0097—Watchmakers' or watch-repairers' machines or tools for working materials for treatment of the material, e.g. surface treatment for components of the means protecting the mechanism against external influences, e.g. cases
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B37/00—Cases
- G04B37/22—Materials or processes of manufacturing pocket watch or wrist watch cases
-
- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
-
- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
-
- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
-
- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
- Y10T428/265—1 mil or less
Definitions
- ABSTRACT [30] Foreign Application Priority Data Method of making a watch case element by forming J 13 1971 S it 1 d 446/71 same of molybdenum and hardenmg by carbunzatlon w zer an producing a surface layer of molybdenum carbide, said carburization being carried out during the final [52] Cl 0 3 manufacturing stage.
- a further treatment of the car- Int Cl 5 5 c23c /6 burized element with hydrogen sulphide results in the Field of Search" U 148/203 6 formation of a dark coloured pol1shab1e surface wh1ch has fine brilliance.
- Watch cases resulting from sintering are strictly limited in their forms and moreover, are very fragile.
- a watch case in stainless steel hardened by nitriding requires, in order to obtain a sufficient corrosion resistance, to be further protected by stainless steel hardened through a layer of chrome such processes imply numerous difficulties.
- the present invention proceeds from the idea of machining a watch case from a material capable of being hardened as a last operation. It is understood that this material must be non magnetic, corrosion resistant, particularly in respect of sea water, easily machinable and capable of either hot or cold forming.
- the method according to the invention is characterized by the fact that one fashions the element of watch case of molybdenum and that one hardens it during the finishing stage by a carburizing treatment, thereby producing on the surface thereof a layer of molybdenum carbide.
- the element of the watch case so obtained is characterized by the fact that it comprises molybdenum having a surface covering of molybdenum carbide.
- Molybdenum has shown itself to respond to the requirements mentioned hereinbefore. It is to be noted that the hardening of the watch case element obtained during final stages of manufacture does not comprise a cementation in the usual sense of this term, i.e. comprising a very hard surface zone united to the interior by a transitional zone. Instead a carburization occurs producing molybdenum carbide at the surface.
- the hardening operation by carburization, is effected by burying the otherwise finished items in a cement of the classic type, by welding shut the container in order to assure a complete sealing thereof, and by bringing this cement to and holding it at a temperature from 1 100 to 1300C for a duration of to hours or still longer should one wish to obtain a very deep carburization.
- the cooling must be effected in the oven and very slowly in order to prevent the carbide zone from becoming fragile. Once the element has reached the room temperature, one can reheat it at a temperature of about 1000C during about two hours, letting it then to cool again very slowly. This improves the diffusion of the hardening layer and reduces the fragility of the element.
- the hardness thus obtained is of the order of 1500 to 1700 Vickers measured by micro-hardness at a load of 500 g.
- the depth of carburization is in the order of 10 to 300 microns according to the temperature and the time. There will be no deformation since molybdenum at 1000C has the same resistance as iron at 20C. A simple polishing will give the desired brilliance.
- the hardening by carburization also can be carried out in a vessel made of a ceramic, the cement of which is constituted by 60 percent of active carbon, 30 percent of graphite and 10 percent of charcoal.
- the duration of the operation will be of about 20 hours, at a temperature of about 1300C, for obtaining a hard layer of a thickness of microns.
- the hardness of such layer is of the order of 1500 to 1600 Vickers at a load of 500 g.
- the hardening also can be carried out under a controlled atmosphere containing 98 percent of hydrogenous and 2 percent of methanol.
- a dark coloured surface having a very fine brilliance and capable of being polished without difficulty may be obtained by treating the carburized items in an atmosphere of hydrogen sulphide at a temperature of about 850C during about 20 minutes, thereby forming a compound molbydenum-sulphide on the surface.
- molybdenum has the property of being easily oxydizable above 500C, various colours such as blue and organge may be obtained through modifying the chemical composition of the surrounding atmosphere or by means of a galvanic oxydation in baths hardly acid or alkaline, even caustic, i.e. other than neutral.
- Method according to claim 1 characterized by the fact that the hardening is carried out in a cement at a temperature of 1100' to l300C, for a duration of 10 to 15 hours.
- Method according to claim 1 characterized by the fact that the hardening is carried out in a cement constituted by 60 percent of active carbon, 30 percent of graphite and 10 percent of powder of charcoal.
- Method according to claim 1 characterized by the fact that the hardening is carried out during about 20 hours, at a temperature of about 1300C.
- Method according to claim 1 characterized by the fact that once the hardening is effected, the element is reheated at a temperature of about l000C, for a duration of about two hours, and then cooled very slowly.
- Method according to claim 1 characterized by the fact that the element is coloured either by changing the composition of the surrounding atmosphere, or by a galvanic treatment in a bath other than neutral.
- a watch case element formed of molybdenum and having a surface layer of molybdenum carbide formed by hardening during the final manufacturing stage by carburization.
- a watch case element as claimed in claim in which said molybdenum carbide surface layer has an outer layer formed of a compound of molybdenumsulfide.
- a watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a hardness in the range of the order of 1500 to 1700 Vickers measured by micro-hardness at a load of 500 grams.
- a watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a thickness of the order of from 10 to 300 microns.
- a watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a hardness in the range of the order of 1500 to 1700 Vickers measured by micro-hardness at a load of 500 grams and a thickness of the order of from l0 to 300 microns.
- a watch case element as claimed in claim 10 in which said surface layer has a colour which is the result of changing the chemical composition of the surrounding atmosphere in the course of heat-treating same.
- Method according to claim 3 characterized by the fact that the hardening is carried out for a duration of about 20 hours, at a temperature of about l300C.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
- Carbon And Carbon Compounds (AREA)
Abstract
Method of making a watch case element by forming same of molybdenum and hardening by carburization producing a surface layer of molybdenum carbide, said carburization being carried out during the final manufacturing stage. A further treatment of the carburized element with hydrogen sulphide results in the formation of a dark coloured polishable surface which has fine brilliance.
Description
United States Maquelin Nov. 13, 1973 [5 METHOD FOR THE MANUFACTURE OF AN [56] References Cited ELEMENT OF WATCH CASE AND UNITED T S PATENTS ELEMENT 0F WATCH CASE OBTAINED 2,823,151 2/1958 Yntema et al. 148/315 BY THIS METHOD 2,804,406 8/1957 Yntema et al. 148/31.5 Inventor: Charles Maquelin, chemin 2,665,475 l/l954 Campbell 148/315 Gabriel, Peseux, Switzerland Primary Examiner-W. W. Stallard Filed: Jan. 7, 197 Attorneyl. Irving Silverman et al. [21] Appl. No.: 216,275
[57] ABSTRACT [30] Foreign Application Priority Data Method of making a watch case element by forming J 13 1971 S it 1 d 446/71 same of molybdenum and hardenmg by carbunzatlon w zer an producing a surface layer of molybdenum carbide, said carburization being carried out during the final [52] Cl 0 3 manufacturing stage. A further treatment of the car- Int Cl 5 5 c23c /6 burized element with hydrogen sulphide results in the Field of Search" U 148/203 6 formation of a dark coloured pol1shab1e surface wh1ch has fine brilliance.
18 Claims, No Drawings METHOD FOR THE MANUFACTURE OF AN ELEMENT OF WATCH CASE AND ELEMENT OF WATCH CASE OBTAINED BY THIS METHOD The present invention provides a method for manufacturing an element of a watch case and the element of watch case so obtained.
For the past several years research has been carried out in order that the watch-making industry might have available watch cases presenting a hard surface which would conserve their beauty and brilliance over the longest possible time. Several solutions already have been proposed, among which are the sintering of carhides, the utilization of stainless steel hardened by nitriding and covered by hard chrome, the application of carbides by spattering as well as the utilization of ordinary steel hardened by chemical vapour deposition of carbides.
All of these solutions present certain disadvantages.
Watch cases resulting from sintering are strictly limited in their forms and moreover, are very fragile.
A watch case in stainless steel hardened by nitriding requires, in order to obtain a sufficient corrosion resistance, to be further protected by stainless steel hardened through a layer of chrome such processes imply numerous difficulties.
The application of carbide by spattering produces a surface layer much too porous to permit the type of surface which one wishes to obtain through simple polishing.
Finally, the utilization of ordinary steel hardened by chemical vapour deposition of carbides produces a superficial layer of a hardness such that the final polishing thereof is almost impossible.
The present invention proceeds from the idea of machining a watch case from a material capable of being hardened as a last operation. It is understood that this material must be non magnetic, corrosion resistant, particularly in respect of sea water, easily machinable and capable of either hot or cold forming.
The method according to the invention is characterized by the fact that one fashions the element of watch case of molybdenum and that one hardens it during the finishing stage by a carburizing treatment, thereby producing on the surface thereof a layer of molybdenum carbide.
The element of the watch case so obtained is characterized by the fact that it comprises molybdenum having a surface covering of molybdenum carbide.
Molybdenum has shown itself to respond to the requirements mentioned hereinbefore. It is to be noted that the hardening of the watch case element obtained during final stages of manufacture does not comprise a cementation in the usual sense of this term, i.e. comprising a very hard surface zone united to the interior by a transitional zone. Instead a carburization occurs producing molybdenum carbide at the surface.
The hardening operation, by carburization, is effected by burying the otherwise finished items in a cement of the classic type, by welding shut the container in order to assure a complete sealing thereof, and by bringing this cement to and holding it at a temperature from 1 100 to 1300C for a duration of to hours or still longer should one wish to obtain a very deep carburization.
The cooling must be effected in the oven and very slowly in order to prevent the carbide zone from becoming fragile. Once the element has reached the room temperature, one can reheat it at a temperature of about 1000C during about two hours, letting it then to cool again very slowly. This improves the diffusion of the hardening layer and reduces the fragility of the element.
The hardness thus obtained is of the order of 1500 to 1700 Vickers measured by micro-hardness at a load of 500 g. The depth of carburization is in the order of 10 to 300 microns according to the temperature and the time. There will be no deformation since molybdenum at 1000C has the same resistance as iron at 20C. A simple polishing will give the desired brilliance.
The hardening by carburization also can be carried out in a vessel made of a ceramic, the cement of which is constituted by 60 percent of active carbon, 30 percent of graphite and 10 percent of charcoal. The duration of the operation will be of about 20 hours, at a temperature of about 1300C, for obtaining a hard layer of a thickness of microns. The hardness of such layer is of the order of 1500 to 1600 Vickers at a load of 500 g.
The hardening also can be carried out under a controlled atmosphere containing 98 percent of hydrogenous and 2 percent of methanol.
A dark coloured surface having a very fine brilliance and capable of being polished without difficulty may be obtained by treating the carburized items in an atmosphere of hydrogen sulphide at a temperature of about 850C during about 20 minutes, thereby forming a compound molbydenum-sulphide on the surface.
Since molybdenum has the property of being easily oxydizable above 500C, various colours such as blue and organge may be obtained through modifying the chemical composition of the surrounding atmosphere or by means of a galvanic oxydation in baths hardly acid or alkaline, even caustic, i.e. other than neutral.
I claim:
1. Method of manufacturing an element of a watch case, characterized by the fact that the said element is formed of molybdenum and is hardened during the final manufacturing stage by carburization thereby to produce a surface layer of molybdenum carbide.
2. Method according to claim 1, characterized by the fact that the hardening is carried out in a cement at a temperature of 1100' to l300C, for a duration of 10 to 15 hours.
3. Method according to claim 1, characterized by the fact that the hardening is carried out in a cement constituted by 60 percent of active carbon, 30 percent of graphite and 10 percent of powder of charcoal.
4. Method according to claim 1, characterized by the fact that the hardening is carried out during about 20 hours, at a temperature of about 1300C.
5. Method according to claim 1, characterized by the fact that the hardening is carried out under a controlled atmosphere contained 98 percent of hydrogenous and 2 percent of methanol.
6. Method according to claim 1, characterized by the fact that once the hardening is effected, the element is reheated at a temperature of about l000C, for a duration of about two hours, and then cooled very slowly.
7. Method according to claim 1, characterized by the fact that the element, after the hardening, is further treated in an atmosphere of hydrogen sulphide in order to form on the surface thereof a compound of molybdenum-sulphide so as to give a darkened colour to the said element.
8. Method according to claim 7, characterized by the fact that the treatment in the hydrogen sulphide atmosphere is carried out at a temperature of approximately 850C and for a duration of approximately 20 minutes.
9. Method according to claim 1 characterized by the fact that the element is coloured either by changing the composition of the surrounding atmosphere, or by a galvanic treatment in a bath other than neutral.
10. A watch case element formed of molybdenum and having a surface layer of molybdenum carbide formed by hardening during the final manufacturing stage by carburization.
11. A watch case element as claimed in claim in which said molybdenum carbide surface layer has an outer layer formed of a compound of molybdenumsulfide.
12. A watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a hardness in the range of the order of 1500 to 1700 Vickers measured by micro-hardness at a load of 500 grams.
13. A watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a thickness of the order of from 10 to 300 microns.
14. A watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a hardness in the range of the order of 1500 to 1700 Vickers measured by micro-hardness at a load of 500 grams and a thickness of the order of from l0 to 300 microns.
15. A watch case element as claimed in claim 10 in which said surface layer has a colour which is the result of changing the chemical composition of the surrounding atmosphere in the course of heat-treating same.
16. A watch case element as claimed in claim 15 in which the colour is the result of changing the surrounding atmosphere following hardening thereof.
17. A watch case element as claimed in claim 15 in which the colour is the result of galvanic oxidation above 500 Centigrade.
18. Method according to claim 3 characterized by the fact that the hardening is carried out for a duration of about 20 hours, at a temperature of about l300C.
Patent No, 3,772 November 13, 1973 Dated Charles Maquelin Inventor(s) It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
In the grant (only) cancel the two sheet of drawings bearing Patent No 3,772 ,097 On the cover sheet [76] "Charles Maquelin, 16 chemin Gabriel Peseujc, Switzerland" should read Charles Maquelin, chemin Gabriel 2034 Peseux,
Neuchatel, Switzerland Signed and sealed this 16th day of July 1974.
(SEAL) Attestz.
MCCOY 'M. GIBSON, J'R. c. MARSHALL DANN Attesting Officer Commissioner of Patents RM PO-105O (10-69) USCOMM-DC 60376-P69 us. GOVERNMENT wnnmus OFFICE: 19" 0-366-334.
Claims (17)
- 2. Method according to claim 1, characterized by the fact that the hardening is carried out in a cement at a temperature of 1100* to 1300*C, for a duration of 10 to 15 hours.
- 3. Method according to claim 1, characterized by the fact that the hardening is carried out in a cement constituted by 60 percent of active carbon, 30 percent of graphite and 10 percent of powder of charcoal.
- 4. Method according to claim 1, characterized by the fact that the hardening is carried out during about 20 hours, at a temperature of about 1300*C.
- 5. Method according to claim 1, characterized by the fact that the hardening is carried out under a controlled atmosphere contained 98 percent of hydrogenous and 2 percent of methanol.
- 6. Method according to claim 1, characterized by the fact that once the hardening is effected, the element is reheated at a temperature of about 1000*C, for a duration of about two hours, and then cooled very slowly.
- 7. Method according to claim 1, characterized by the fact that the element, after the hardening, is further treated in an atmosphere of hydrogen sulphide in order to form on the surface thereof a compound of molybdenum-sulphide so as to give a darkened colour to the said element.
- 8. Method according to claim 7, characterized by the fact that the treatment in the hydrogen sulphide atmosphere is carried out at a temperature of approximately 850*C and for a duration of approximately 20 minutes.
- 9. Method accOrding to claim 1 characterized by the fact that the element is coloured either by changing the composition of the surrounding atmosphere, or by a galvanic treatment in a bath other than neutral.
- 10. A watch case element formed of molybdenum and having a surface layer of molybdenum carbide formed by hardening during the final manufacturing stage by carburization.
- 11. A watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has an outer layer formed of a compound of molybdenum-sulfide.
- 12. A watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a hardness in the range of the order of 1500 to 1700 Vickers measured by micro-hardness at a load of 500 grams.
- 13. A watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a thickness of the order of from 10 to 300 microns.
- 14. A watch case element as claimed in claim 10 in which said molybdenum carbide surface layer has a hardness in the range of the order of 1500 to 1700 Vickers measured by micro-hardness at a load of 500 grams and a thickness of the order of from 10 to 300 microns.
- 15. A watch case element as claimed in claim 10 in which said surface layer has a colour which is the result of changing the chemical composition of the surrounding atmosphere in the course of heat-treating same.
- 16. A watch case element as claimed in claim 15 in which the colour is the result of changing the surrounding atmosphere following hardening thereof.
- 17. A watch case element as claimed in claim 15 in which the colour is the result of galvanic oxidation above 500* centigrade.
- 18. Method according to claim 3 characterized by the fact that the hardening is carried out for a duration of about 20 hours, at a temperature of about 1300*C.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH44671 | 1971-01-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3772096A true US3772096A (en) | 1973-11-13 |
Family
ID=4187208
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00216275A Expired - Lifetime US3772096A (en) | 1971-01-13 | 1972-01-07 | Method for the manufacture of an element of watch case and element of watch case obtained by this method |
Country Status (7)
Country | Link |
---|---|
US (1) | US3772096A (en) |
JP (1) | JPS5431975B1 (en) |
DE (1) | DE2201349A1 (en) |
FR (1) | FR2121884B1 (en) |
GB (1) | GB1344582A (en) |
HK (1) | HK62376A (en) |
IT (1) | IT948106B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3982970A (en) * | 1972-01-24 | 1976-09-28 | United Kingdom Atomic Energy Authority | Ductility of molybdenum and its alloys |
US4746375A (en) * | 1987-05-08 | 1988-05-24 | General Electric Company | Activation of refractory metal surfaces for electroless plating |
US6905758B1 (en) * | 1987-08-12 | 2005-06-14 | Citizen Watch Co., Ltd. | Decorative item and process for producing the same |
US20180046141A1 (en) * | 2016-08-15 | 2018-02-15 | Rolex Sa | Device for winding a timepiece movement |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2665475A (en) * | 1950-03-18 | 1954-01-12 | Fansteel Metallurgical Corp | Highly refractory body |
US2804406A (en) * | 1952-09-26 | 1957-08-27 | Fansteel Metallurgical Corp | Method of making refractory metal bodies |
US2823151A (en) * | 1953-10-14 | 1958-02-11 | Fansteel Metallurgical Corp | Highly refractive molybdenum bodies |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1056564A (en) * | 1952-05-15 | 1954-03-01 | Onera (Off Nat Aerospatiale) | Process for the formation of extra hard layers on metals and their alloys |
CH455856A (en) * | 1966-06-27 | 1968-07-15 | Suisse De Rech S Horlogeres La | Process for the production of hard coatings on watch components |
-
1972
- 1972-01-04 FR FR7201481A patent/FR2121884B1/fr not_active Expired
- 1972-01-05 GB GB53472A patent/GB1344582A/en not_active Expired
- 1972-01-05 IT IT47567/72A patent/IT948106B/en active
- 1972-01-07 DE DE19722201349 patent/DE2201349A1/en active Pending
- 1972-01-07 US US00216275A patent/US3772096A/en not_active Expired - Lifetime
- 1972-01-13 JP JP610872A patent/JPS5431975B1/ja active Pending
-
1976
- 1976-10-07 HK HK623/76*UA patent/HK62376A/en unknown
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2665475A (en) * | 1950-03-18 | 1954-01-12 | Fansteel Metallurgical Corp | Highly refractory body |
US2804406A (en) * | 1952-09-26 | 1957-08-27 | Fansteel Metallurgical Corp | Method of making refractory metal bodies |
US2823151A (en) * | 1953-10-14 | 1958-02-11 | Fansteel Metallurgical Corp | Highly refractive molybdenum bodies |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3982970A (en) * | 1972-01-24 | 1976-09-28 | United Kingdom Atomic Energy Authority | Ductility of molybdenum and its alloys |
US4746375A (en) * | 1987-05-08 | 1988-05-24 | General Electric Company | Activation of refractory metal surfaces for electroless plating |
US6905758B1 (en) * | 1987-08-12 | 2005-06-14 | Citizen Watch Co., Ltd. | Decorative item and process for producing the same |
US20180046141A1 (en) * | 2016-08-15 | 2018-02-15 | Rolex Sa | Device for winding a timepiece movement |
US11144011B2 (en) * | 2016-08-15 | 2021-10-12 | Rolex Sa | Device for winding a timepiece movement |
Also Published As
Publication number | Publication date |
---|---|
FR2121884B1 (en) | 1977-01-14 |
DE2201349A1 (en) | 1972-07-27 |
FR2121884A1 (en) | 1972-08-25 |
JPS5431975B1 (en) | 1979-10-11 |
HK62376A (en) | 1976-10-15 |
IT948106B (en) | 1973-05-30 |
GB1344582A (en) | 1974-01-23 |
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