GB1301524A - - Google Patents
Info
- Publication number
- GB1301524A GB1301524A GB1301524DA GB1301524A GB 1301524 A GB1301524 A GB 1301524A GB 1301524D A GB1301524D A GB 1301524DA GB 1301524 A GB1301524 A GB 1301524A
- Authority
- GB
- United Kingdom
- Prior art keywords
- conduits
- brazing
- section
- annular
- spacers
- 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
Links
Classifications
-
- 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
- B23K11/00—Resistance welding; Severing by resistance heating
- B23K11/30—Features relating to electrodes
- B23K11/3009—Pressure electrodes
- B23K11/3018—Cooled pressure electrodes
-
- 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
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/40—Making wire or rods for soldering or welding
- B23K35/402—Non-consumable electrodes; C-electrodes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Ceramic Products (AREA)
Abstract
1301524 Brazing; making electrodes; casting composite articles WESTINGHOUSE ELECTRIC CORP 22 May 1970 24811/70 Headings B3A B3F and B3R A method of producing an annular electrode tip having a series of radially directed U-shaped coolant passages comprises placing a series of radially directed U-shaped conduits 29, 30 within an annular U-section shell 24, placing a series of spacer elements 31 between those portions of adjacent conduits which lie against the outer wall of the shell, placing an inner shell 22 which is also of annular shape and U-section within the annular U-section space defined by the conduits and brazing together the shells, conduits and spacers to form a substantially integral unified structure, having the desired coolant passages. The conduits may be of circular, square or rectangular cross-section. Brazing may be effected by winding turns of brazing material 51 around the upper part of the inner shell, and heating the assembled unit in a furnace with or without flux 47 and possibly under vacuum or in a reducing atmosphere to a temperature sufficient to melt the brazing material and cause it to penetrate all the spaces between the conduits, shells and spacers. Alternatively the assembled unit with an asbestos cover 34 and superimposed weight 35 covering the inner shell is heated to a predetermined temperature in one furnace and separately heated brazing material from another furnace is poured into the spaces 21, 33 at the upper part of the assembled unit. The shells, conduits and spacers may be of copper and the brazing alloy may have the following compositions:
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2481170 | 1970-05-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1301524A true GB1301524A (en) | 1972-12-29 |
Family
ID=10217605
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1301524D Expired GB1301524A (en) | 1970-05-22 | 1970-05-22 |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1301524A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4137619A (en) * | 1977-10-03 | 1979-02-06 | General Electric Company | Method of fabricating composite structures for water cooled gas turbine components |
US4249291A (en) * | 1979-06-01 | 1981-02-10 | General Electric Company | Method for forming a liquid cooled airfoil for a gas turbine |
WO2005113186A1 (en) * | 2004-05-21 | 2005-12-01 | Alexander Binzel Schweisstechnik Gmbh & Co. Kg | Method and device for cleaning an electrode used in resistance point welding or a cap and device for resistance point welding |
-
1970
- 1970-05-22 GB GB1301524D patent/GB1301524A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4137619A (en) * | 1977-10-03 | 1979-02-06 | General Electric Company | Method of fabricating composite structures for water cooled gas turbine components |
US4249291A (en) * | 1979-06-01 | 1981-02-10 | General Electric Company | Method for forming a liquid cooled airfoil for a gas turbine |
WO2005113186A1 (en) * | 2004-05-21 | 2005-12-01 | Alexander Binzel Schweisstechnik Gmbh & Co. Kg | Method and device for cleaning an electrode used in resistance point welding or a cap and device for resistance point welding |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |