GB882317A - Improvements relating to the joining of metals - Google Patents
Improvements relating to the joining of metalsInfo
- Publication number
- GB882317A GB882317A GB13471/57A GB1347157A GB882317A GB 882317 A GB882317 A GB 882317A GB 13471/57 A GB13471/57 A GB 13471/57A GB 1347157 A GB1347157 A GB 1347157A GB 882317 A GB882317 A GB 882317A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nickel
- parts
- chromium
- joined
- turbine blade
- 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
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/001—Interlayers, transition pieces for metallurgical bonding of workpieces
- B23K35/004—Interlayers, transition pieces for metallurgical bonding of workpieces at least one of the workpieces being of a metal of the iron group
-
- 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
- B23K20/16—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating with interposition of special material to facilitate connection of the parts, e.g. material for absorbing or producing gas
-
- 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
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/001—Turbines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Abstract
882,317. Making turbines; welding by pressure. WIGGIN & CO. Ltd., HENRY. April 28, 1958 [April 26, 1957], No. 13471/57. Classes 83 (2) and 83 (4). In joining preformed parts of chromium containing alloy a very thin layer or layers of nickel is interposed between the parts, the parts are forced together and the assembly is heated in a non-oxidizing atmosphere to 1000- 1100‹ C. to diffuse the nickel substantially completely into the parts. The parts may have spigot and socket connection when one is forced into the other in a press and heated without maintenance of the applied pressure. If the parts have other shapes they may be held under an external pressure during the initial heating e.g. to 700‹ C. to promote initial diffusion and the pressure may then be released. The pressure may be obtained by interfitting after shrinking in dry ice. The nickel may be in foil, powder, sprayed or plated form. In embodiments the trapezoidal section root 2 of a gas turbine blade 1, Fig. 1, of nickel-chromium or nickel-chromium-cobalt alloy is covered with nickel foil 5 or is coated with nickel and is joined to the slot 3 machined in the rim of a rotor 4 of the same nickel-chromium or nickel-chromium-cobalt alloy. The sides of the slot which may be cut by spark erosion and the root sides may be parallel. A frusto-conical root 2, Fig. 2, of a turbine blade of 20% chomium, 20% cobalt, 2.4% titanium, 1.5% aluminium, 0.07% carbon, balance nickel is forced into a socket 3 in a rotor 4 of the same alloy with an intermediate layer of nickel 5 and the assembly heated in hydrogen to 1100‹ C. for 8 hours. The nickel foil covered or plated ends of a section of turbine blade 6, Fig. 4, with holes 7 formed by extruding a billet having inserts of filler metal, subsequently removed, are secured in sockets cut by spark erosion in root and shroud 8, 9. These parts may be assembled by shrinkage fitting. A number of sleeves are shrink fitted on turbine blade stock coated with nickel and joined thereto and the assembly is cut into blades with roots. Stainless-steel cutlery blades may be joined to stainless-steel shanks. According to the Provisional Specification if the surfaces to be joined are of superlative quality the interposed layer may be dispensed with-preliminary heating at 600‹ C. is then effected before pressing the parts together.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13471/57A GB882317A (en) | 1957-04-26 | 1957-04-26 | Improvements relating to the joining of metals |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13471/57A GB882317A (en) | 1957-04-26 | 1957-04-26 | Improvements relating to the joining of metals |
Publications (1)
Publication Number | Publication Date |
---|---|
GB882317A true GB882317A (en) | 1961-11-15 |
Family
ID=10023568
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13471/57A Expired GB882317A (en) | 1957-04-26 | 1957-04-26 | Improvements relating to the joining of metals |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB882317A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2566842A1 (en) * | 1984-06-30 | 1986-01-03 | Messerschmitt Boelkow Blohm | Fixing nozzles in injection head |
GB2419836A (en) * | 2004-11-09 | 2006-05-10 | Eads Deutschland Gmbh | Welding using a shaped portion of welding filler |
US7735223B2 (en) | 2003-11-27 | 2010-06-15 | Rolls-Royce Plc | Method of fabricating or repairing a blisk |
FR3004698A1 (en) * | 2013-04-17 | 2014-10-24 | Snecma | DEVICE FOR CONTROLLING BLADE SETTING AND PROPELLER |
-
1957
- 1957-04-26 GB GB13471/57A patent/GB882317A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2566842A1 (en) * | 1984-06-30 | 1986-01-03 | Messerschmitt Boelkow Blohm | Fixing nozzles in injection head |
US7735223B2 (en) | 2003-11-27 | 2010-06-15 | Rolls-Royce Plc | Method of fabricating or repairing a blisk |
GB2419836A (en) * | 2004-11-09 | 2006-05-10 | Eads Deutschland Gmbh | Welding using a shaped portion of welding filler |
GB2419836B (en) * | 2004-11-09 | 2010-02-03 | Eads Deutschland Gmbh | Welding process using a filler |
FR3004698A1 (en) * | 2013-04-17 | 2014-10-24 | Snecma | DEVICE FOR CONTROLLING BLADE SETTING AND PROPELLER |
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