US2206662A - Fabricating article of beryllium copper - Google Patents
Fabricating article of beryllium copper Download PDFInfo
- Publication number
- US2206662A US2206662A US188080A US18808038A US2206662A US 2206662 A US2206662 A US 2206662A US 188080 A US188080 A US 188080A US 18808038 A US18808038 A US 18808038A US 2206662 A US2206662 A US 2206662A
- Authority
- US
- United States
- Prior art keywords
- beryllium copper
- strip
- cadmium
- article
- coating
- 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
- DMFGNRRURHSENX-UHFFFAOYSA-N beryllium copper Chemical compound [Be].[Cu] DMFGNRRURHSENX-UHFFFAOYSA-N 0.000 title description 19
- 229910052793 cadmium Inorganic materials 0.000 description 16
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 16
- 239000011248 coating agent Substances 0.000 description 11
- 238000000576 coating method Methods 0.000 description 11
- 229910052751 metal Inorganic materials 0.000 description 11
- 239000002184 metal Substances 0.000 description 11
- 238000000034 method Methods 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 9
- 238000005520 cutting process Methods 0.000 description 6
- 239000000314 lubricant Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910001369 Brass Inorganic materials 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- MOFOBJHOKRNACT-UHFFFAOYSA-N nickel silver Chemical compound [Ni].[Ag] MOFOBJHOKRNACT-UHFFFAOYSA-N 0.000 description 2
- 229910000753 refractory alloy Inorganic materials 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- 229940058494 beryllium Drugs 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000010956 nickel silver Substances 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/22—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
- B23K20/233—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded without ferrous layer
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/02—Contact members
- H01R13/03—Contact members characterised by the material, e.g. plating, or coating materials
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/40—Securing contact members in or to a base or case; Insulating of contact members
- H01R13/42—Securing in a demountable manner
- H01R13/428—Securing in a demountable manner by resilient locking means on the contact members; by locking means on resilient contact members
- H01R13/432—Securing in a demountable manner by resilient locking means on the contact members; by locking means on resilient contact members by stamped-out resilient tongue snapping behind shoulder in base or case
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49117—Conductor or circuit manufacturing
- Y10T29/49204—Contact or terminal manufacturing
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49117—Conductor or circuit manufacturing
- Y10T29/49204—Contact or terminal manufacturing
- Y10T29/49224—Contact or terminal manufacturing with coating
Definitions
- This invention relates to a method of preparing metals which are to be fabricated into articles of manufacture by cutting, forming, stamping or like operations. More particularly, the
- -Beryllium copper having a beryllium content of from 2.0% to 2.25% is commonly referred to as 10 a refractory alloy, because of the dimculty with which it is fabricated and machined.
- This difficulty is encountered in mills where the cast material is fabricated into bar, tube, sheet and strip form and also in the fabricating processes which the manufacturer of articles employs, such as blanking, forming, swaging, shaving and shearing. In all of these manufacturing processes, whether used by the mill or factory, the wear and tear on tools and dies when processing these 20 alloys is far greater than when ordinary commercial free-cutting brass is processed.
- the machinability of the refractory alloys 25 such as phosphor bronze and nickel silver may be classed as 20.
- the machinability of beryllium copper may be classed as under 20 which classes it as even more refractory than phosphor bronzes and nickel silvers.
- beryllium copper has qualities such as strength, wear resistance, conductivity and corrosion-resistance which make it very desirable for use in the manufacture of various articles
- the difficulty encountered in working the metal resulting in excessive wear on the tools, overbalances the advantages derived from its better qualities and has threatened to force discontinuance of its use in the manufacture of particular articles because of the high cost incident to w the frequent replacement of tools and dies.
- a beryllium copper strip by applying thereto a coating of cadmium of uni- I form thickness which will prevent direct contact 56 between the beryllium copper and the tool and serve as a lubricant between the two.
- Fig. 1 represents a strip of beryllium copper coated with cadmium and illustrating the various 7 5 steps of fabricating.
- Fig. 2 is an isometric view showing the completely fabricated article.
- Fig. 3 is an enlarged cross-sectional view of the coated strip, the section being taken on lines 3-3 of Fig. 1. v
- Fig. 4 is a similar view taken on lines 4-4 of Fig. 1 showing the manner in which the cadmium coating is drawn over the surfaces of the base material by the forming tools.
- Fig. 5 is a diagrammatic representation of a multiple-tool machine through which a strip of metal is fed.
- Fig. 2 there is shown at a greatly enlarged scale a small part which has been fabricated automatically from a strip of material. A multiplicity of these parts is mounted on a panel of insulating material termed a "plug board panel" and employed in the well known electric accounting machines. Such a panel is described and illustrated in the copending application of Clair D. Lake, Serial No. 10,299, filed March 9, 1935, and allowed September 1'7, 1937, for a Plug board.
- beryllium copper in the production of these parts is highly desirable because of the corrosion resistance properties of the metal and its excellent electrical conductivity.
- the strip I is subjected to seven distinct operations in the cutting, forming and blanking of a single part from the strip after which the blank is bent and rolled to complete the article.
- Fig. is shown a turret type of machine with a die portion I l and a toolcarrying turret l2, although other types of machine may be employed in which the tools are arranged in tandem for concurrent operation.
- the beryllium copper strip ill in the form of a continuous web is cadmium plated in either individual still tanks, semi-auto matic tank or full tank equipment, or full automatic equipment may be used throughout for the cleaning as well as the plating and subsequent 55 rinsing operation. Best results have been obtained when the coating of cadmium is deposited with a thickness between a minimum of two ten.- thousandths and a maximum of five ten-thou.- sandths of an inch.
- Fig. 3 is shown a crosssection of the coated beryllium copper with an even distribution of cadmium.
- the cadmium acts as a lubricant avoiding intimate contact between the tool and the beryllium copper and because of its ductility, as the tool pierces the strip, the cadmium is drawn by the tool into the pierced sections and coats the newly formed inner surfaces so that a section, such as shown in Fig. 4, would disclose cadmium on the inner surfaces though of a lesser thickness than on the surfaces to which it was initially applied.
- the great ductility and malleability of the cadmium permits the coating to be stretched and dragged over the cut and formed edges, thus maintaining a film of the metal between the tool and the edge of the strip being out.
- the completed article shown in Fig. 2 when it leaves the machine, has the original coating on its outer and inner surfaces and in addition the narrow edges have also a thinner coating of cadmium.
- the cadmium coating having served its purpose may thereafter be removed in a suitable bath, leaving an article of bright beryllium copper.
- the lubricating effect of the coating has in actual production increased the life of the tools and dies from fifteen thousand pieces to one hundred and sixty thousand pieces or, in other words, it has increased the life of the tools over ten and a half times so that the use of beryllium copper in the production of small parts has been rendered more economical and satisfactory.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
Description
July 2, 1940. 2,206,662
FABRICATING ARTICLE OF BERYLLIUM COPPER L. C. CONRAD! El AL- Filed Feb; 1, 1958- v 22225 mmriou zzjikwm Eff 6H2/EITITO25 m 5225: M Tll Patented July 2, 1940 UNITED STATES PATENT oFFlcE FABRIOATING ARTICLE OF BER-YLLIUM COPPER poration of New York Application February 1, 1938, Serial No. 188,086-
2 Claims.
This invention relates to a method of preparing metals which are to be fabricated into articles of manufacture by cutting, forming, stamping or like operations. More particularly, the
5 invention relates to the preparation of the metal known as beryllium copper whose hardness renders it difiicult to fabricate and machine.
-Beryllium copper having a beryllium content of from 2.0% to 2.25% is commonly referred to as 10 a refractory alloy, because of the dimculty with which it is fabricated and machined. This difficulty is encountered in mills where the cast material is fabricated into bar, tube, sheet and strip form and also in the fabricating processes which the manufacturer of articles employs, such as blanking, forming, swaging, shaving and shearing. In all of these manufacturing processes, whether used by the mill or factory, the wear and tear on tools and dies when processing these 20 alloys is far greater than when ordinary commercial free-cutting brass is processed.
Generally speaking and arbitrarily taking the machinability of commercial free-cutting brass as 100, the machinability of the refractory alloys 25 such as phosphor bronze and nickel silver may be classed as 20. The machinability of beryllium copper may be classed as under 20 which classes it as even more refractory than phosphor bronzes and nickel silvers.
While beryllium copper has qualities such as strength, wear resistance, conductivity and corrosion-resistance which make it very desirable for use in the manufacture of various articles, the difficulty encountered in working the metal, resulting in excessive wear on the tools, overbalances the advantages derived from its better qualities and has threatened to force discontinuance of its use in the manufacture of particular articles because of the high cost incident to w the frequent replacement of tools and dies.
It is accordingly proposed to prepare the beryl- .lium copper stock before processing operations are performed thereon with a coating of a softer ductile metal which will act as a lubricant dur- 5 ing the processing operations.
More specifically, it is the object of the invention to prepare a beryllium copper strip by applying thereto a coating of cadmium of uni- I form thickness which will prevent direct contact 56 between the beryllium copper and the tool and serve as a lubricant between the two.
' Various other objects and advantages of the invention will be obvious from the following particular description of a method of procedure w embodying the invention as applied to the manufacture of a selected article or from an inspection of the drawing.
In the drawing:
Fig. 1 represents a strip of beryllium copper coated with cadmium and illustrating the various 7 5 steps of fabricating.
Fig. 2 is an isometric view showing the completely fabricated article.
Fig. 3 is an enlarged cross-sectional view of the coated strip, the section being taken on lines 3-3 of Fig. 1. v
Fig. 4 is a similar view taken on lines 4-4 of Fig. 1 showing the manner in which the cadmium coating is drawn over the surfaces of the base material by the forming tools.
Fig. 5 is a diagrammatic representation of a multiple-tool machine through which a strip of metal is fed.
In Fig. 2 there is shown at a greatly enlarged scale a small part which has been fabricated automatically from a strip of material. A multiplicity of these parts is mounted on a panel of insulating material termed a "plug board panel" and employed in the well known electric accounting machines. Such a panel is described and illustrated in the copending application of Clair D. Lake, Serial No. 10,299, filed March 9, 1935, and allowed September 1'7, 1937, for a Plug board.
The use of beryllium copper in the production of these parts is highly desirable because of the corrosion resistance properties of the metal and its excellent electrical conductivity.
It has been found under actual production conditions that the tools and dies used to fabricate this part required replacement after the making of about fifteen thousand pieces. In other words, the abrasive effect of the beryllium copper on the tools was so great that the use of the metal for this purpose was economically unsound.
As indicated in Fig. 1, the strip I is subjected to seven distinct operations in the cutting, forming and blanking of a single part from the strip after which the blank is bent and rolled to complete the article. In Fig. is shown a turret type of machine with a die portion I l and a toolcarrying turret l2, although other types of machine may be employed in which the tools are arranged in tandem for concurrent operation.
In carrying out the invention the beryllium copper strip ill in the form of a continuous web, after the usual cleaning processes, is cadmium plated in either individual still tanks, semi-auto matic tank or full tank equipment, or full automatic equipment may be used throughout for the cleaning as well as the plating and subsequent 55 rinsing operation. Best results have been obtained when the coating of cadmium is deposited with a thickness between a minimum of two ten.- thousandths and a maximum of five ten-thou.- sandths of an inch. In Fig. 3 is shown a crosssection of the coated beryllium copper with an even distribution of cadmium. As the coated strip is worked, the cadmium acts as a lubricant avoiding intimate contact between the tool and the beryllium copper and because of its ductility, as the tool pierces the strip, the cadmium is drawn by the tool into the pierced sections and coats the newly formed inner surfaces so that a section, such as shown in Fig. 4, would disclose cadmium on the inner surfaces though of a lesser thickness than on the surfaces to which it was initially applied. In other words, the great ductility and malleability of the cadmium permits the coating to be stretched and dragged over the cut and formed edges, thus maintaining a film of the metal between the tool and the edge of the strip being out.
As a result the completed article shown in Fig. 2, when it leaves the machine, has the original coating on its outer and inner surfaces and in addition the narrow edges have also a thinner coating of cadmium. The cadmium coating having served its purpose may thereafter be removed in a suitable bath, leaving an article of bright beryllium copper. The lubricating effect of the coating has in actual production increased the life of the tools and dies from fifteen thousand pieces to one hundred and sixty thousand pieces or, in other words, it has increased the life of the tools over ten and a half times so that the use of beryllium copper in the production of small parts has been rendered more economical and satisfactory.
Although one method for obtaining the improved results has been set forth and described, it is obvious that various changes may be made in the separate steps thereof without modifying or changing the essential features and characteristics of the method employed and that such methods remain substantially the same, although slight modifications may be made in the physical and chemical characteristics of the metals used.
What is claimed is:
1. The method of forming an article of beryl lium copper which consists in coating a strip of beryllium copper with cadmium to a thickness of approximately .00035 of an inch and then operating upon the coated strip with cutting, pressing and stamping tools so the cadmium is drawn by the tool over the cut edges of the strip.
2. The method of forming an article of a metal having a substantial hardness of beryllium copper which consists in coating a strip of said metal with cadmium to a thickness between .0002 and .0005 of an inch and then operating upon the coated strip with a cutting tool so the cadmium is drawn by the tool over the cut edges of the. strip.
LEO C. CONRADI. HAROLD F. BARNES.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US188080A US2206662A (en) | 1938-02-01 | 1938-02-01 | Fabricating article of beryllium copper |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US188080A US2206662A (en) | 1938-02-01 | 1938-02-01 | Fabricating article of beryllium copper |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2206662A true US2206662A (en) | 1940-07-02 |
Family
ID=22691698
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US188080A Expired - Lifetime US2206662A (en) | 1938-02-01 | 1938-02-01 | Fabricating article of beryllium copper |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2206662A (en) |
Cited By (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2476886A (en) * | 1943-05-29 | 1949-07-19 | Westinghouse Electric Corp | Contact construction |
| US2557126A (en) * | 1946-06-27 | 1951-06-19 | Aircraft Marine Prod Inc | Electrical connector |
| US2563761A (en) * | 1945-09-20 | 1951-08-07 | Bendix Aviat Corp | Socket connector having an indented solder wall |
| US2576528A (en) * | 1948-08-07 | 1951-11-27 | Burndy Engineering Co Inc | Connector with hard particle lining |
| US2627192A (en) * | 1950-09-25 | 1953-02-03 | Res Eng & Mfg | Process of making driver bits |
| US2627649A (en) * | 1948-08-07 | 1953-02-10 | Burndy Engineering Co Inc | Method for making connectors with hard particle lining |
| US2655641A (en) * | 1948-10-29 | 1953-10-13 | Aircraft Marine Prod Inc | Electrical connector having a mercury amalgam coating on its inner surface |
| US2659871A (en) * | 1949-10-03 | 1953-11-17 | Aircraft Marine Prod Inc | Electrical connector strip having laterally displaced strip feeding edges |
| US2681439A (en) * | 1949-06-20 | 1954-06-15 | Aircraft Marine Prod Inc | Insulated electrical connector |
| US2706760A (en) * | 1951-11-09 | 1955-04-19 | Clarostat Mfg Co Inc | Variable electric control |
| US2708741A (en) * | 1952-11-20 | 1955-05-17 | Orsini William | Attaching clip for two-prong electric plug |
| US2724098A (en) * | 1952-04-09 | 1955-11-15 | Thomas & Betts Corp | Electric connectors |
| US2738693A (en) * | 1951-11-19 | 1956-03-20 | Thomas & Betts Corp | Hand tool for crimping electrical connectors |
| US2776255A (en) * | 1955-07-07 | 1957-01-01 | Rockwell Spring & Axle Co | Method of making formed, plated articles |
| US2786191A (en) * | 1948-05-14 | 1957-03-19 | Amp Inc | Electrical connector |
| US2802257A (en) * | 1949-02-01 | 1957-08-13 | Amp Inc | Method of forming an electrical connection |
| US2886498A (en) * | 1957-09-06 | 1959-05-12 | Republic Steel Corp | Process of preparing steel for enameling |
| US3331049A (en) * | 1964-05-25 | 1967-07-11 | Gen Electric | Busway stab contact |
| US3406376A (en) * | 1966-09-26 | 1968-10-15 | Itt | Socket contact and method of manufacture |
| US4612703A (en) * | 1985-03-18 | 1986-09-23 | Pylon Company, Inc. | Production of metal-plated areas on selected interior portions of deep-drawn tubular parts |
| US6305067B1 (en) * | 2000-01-04 | 2001-10-23 | Chin Fu Horng | Elastic plate structure for preventing electromagnetic interference and manufacturing method for the same |
| US20070207635A1 (en) * | 2005-11-29 | 2007-09-06 | Gailus Mark W | Electronic component with high density, low cost attachment |
| US20070205497A1 (en) * | 2005-11-29 | 2007-09-06 | Gailus Mark W | Lead(Pb)-free electronic component attachment |
-
1938
- 1938-02-01 US US188080A patent/US2206662A/en not_active Expired - Lifetime
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2476886A (en) * | 1943-05-29 | 1949-07-19 | Westinghouse Electric Corp | Contact construction |
| US2563761A (en) * | 1945-09-20 | 1951-08-07 | Bendix Aviat Corp | Socket connector having an indented solder wall |
| US2557126A (en) * | 1946-06-27 | 1951-06-19 | Aircraft Marine Prod Inc | Electrical connector |
| US2786191A (en) * | 1948-05-14 | 1957-03-19 | Amp Inc | Electrical connector |
| US2576528A (en) * | 1948-08-07 | 1951-11-27 | Burndy Engineering Co Inc | Connector with hard particle lining |
| US2627649A (en) * | 1948-08-07 | 1953-02-10 | Burndy Engineering Co Inc | Method for making connectors with hard particle lining |
| US2655641A (en) * | 1948-10-29 | 1953-10-13 | Aircraft Marine Prod Inc | Electrical connector having a mercury amalgam coating on its inner surface |
| US2802257A (en) * | 1949-02-01 | 1957-08-13 | Amp Inc | Method of forming an electrical connection |
| US2681439A (en) * | 1949-06-20 | 1954-06-15 | Aircraft Marine Prod Inc | Insulated electrical connector |
| US2659871A (en) * | 1949-10-03 | 1953-11-17 | Aircraft Marine Prod Inc | Electrical connector strip having laterally displaced strip feeding edges |
| US2627192A (en) * | 1950-09-25 | 1953-02-03 | Res Eng & Mfg | Process of making driver bits |
| US2706760A (en) * | 1951-11-09 | 1955-04-19 | Clarostat Mfg Co Inc | Variable electric control |
| US2738693A (en) * | 1951-11-19 | 1956-03-20 | Thomas & Betts Corp | Hand tool for crimping electrical connectors |
| US2724098A (en) * | 1952-04-09 | 1955-11-15 | Thomas & Betts Corp | Electric connectors |
| US2708741A (en) * | 1952-11-20 | 1955-05-17 | Orsini William | Attaching clip for two-prong electric plug |
| US2776255A (en) * | 1955-07-07 | 1957-01-01 | Rockwell Spring & Axle Co | Method of making formed, plated articles |
| US2886498A (en) * | 1957-09-06 | 1959-05-12 | Republic Steel Corp | Process of preparing steel for enameling |
| US3331049A (en) * | 1964-05-25 | 1967-07-11 | Gen Electric | Busway stab contact |
| US3406376A (en) * | 1966-09-26 | 1968-10-15 | Itt | Socket contact and method of manufacture |
| US4612703A (en) * | 1985-03-18 | 1986-09-23 | Pylon Company, Inc. | Production of metal-plated areas on selected interior portions of deep-drawn tubular parts |
| US6305067B1 (en) * | 2000-01-04 | 2001-10-23 | Chin Fu Horng | Elastic plate structure for preventing electromagnetic interference and manufacturing method for the same |
| US20070207635A1 (en) * | 2005-11-29 | 2007-09-06 | Gailus Mark W | Electronic component with high density, low cost attachment |
| US20070205497A1 (en) * | 2005-11-29 | 2007-09-06 | Gailus Mark W | Lead(Pb)-free electronic component attachment |
| WO2008094135A3 (en) * | 2005-11-29 | 2008-10-30 | Amphenol Corp | Electronic component with high density, low cost attachment |
| US7484971B2 (en) * | 2005-11-29 | 2009-02-03 | Amphenol Corporation | Electronic component with high density, low cost attachment |
| US7630210B2 (en) * | 2005-11-29 | 2009-12-08 | Amphenol Corporation | Lead(Pb)-free electronic component attachment |
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