GB1438842A - Liquid interface diffusion method of bonding parts made of titanium or titanium based alloy - Google Patents
Liquid interface diffusion method of bonding parts made of titanium or titanium based alloyInfo
- Publication number
- GB1438842A GB1438842A GB3938573A GB3938573A GB1438842A GB 1438842 A GB1438842 A GB 1438842A GB 3938573 A GB3938573 A GB 3938573A GB 3938573 A GB3938573 A GB 3938573A GB 1438842 A GB1438842 A GB 1438842A
- Authority
- GB
- United Kingdom
- Prior art keywords
- copper
- nickel
- titanium
- diffusion
- silver
- 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
- 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
-
- 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
- B23K35/005—Interlayers, transition pieces for metallurgical bonding of workpieces at least one of the workpieces being of a refractory metal
-
- 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
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Laminated Bodies (AREA)
Abstract
1438842 Brazing and welding ROHR INDUSTRIES Inc 21 Aug 1973 39385/73 Heading B3R In liquid interface diffusion bonding of articles of titanium or titanium based alloy an alloy of nickel and copper or layers of copper, nickel and copper in that order, or an alloy of nickel, copper and silver or layers of nickel, copper, silver, copper and nickel in that order are deposited as a diffusion bridge between the articles, the assembly is heated to form by solid state diffusion a eutectic comprising titanium, and the diffusion bridge, the eutectic melting and then as a result of further diffusion, solidifiying, the temperature is maintained to cause further solid phase diffusion and then the assembly is cooled. In an embodiment of bonding a sheet to a honeycomb core or a sheet to a sheet, the parts to be joined both being of titanium or titanium based alloy, an alloy of nickel, copper and silver or layers, viz nickel, copper, silver, copper and nickel, are deposited on at least one of the parts by, e.g. brushing, electroplating, vapour deposition or powder flame spray to provide 1-5 grams. /square foot of honeycomb core or 6-12 grams./square foot for sheet material the amounts of the metals are 38-45% nickel, 38-45% copper and 10-24% silver. The parts are assembled and in a vacuum are heated at 100‹F./min.to 1400‹ F., at 20‹ F./min to 1600‹ F. when a copper/silver mush forms at 2‹F/min. to 1700-1750‹ F. when the titanium, nickel and copper eutectic composition is reached by solid state diffusion and the eutectic melts. Continuing diffusion produces enriched titanium composition and solidification of the alloy. Further heating at 1700-1750‹ F. causes solid state diffusion at the interfaces and finally the assembly is cooled, the final cooling taking place in inert atmosphere. In an alternative embodiment the coated layers are of copper, nickel and copper (40-60% nickel 60-40% copper). In both embodiments the heating steps are the same. The assembly is held at 1700‹ F. for 90 minutes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3938573A GB1438842A (en) | 1973-08-21 | 1973-08-21 | Liquid interface diffusion method of bonding parts made of titanium or titanium based alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3938573A GB1438842A (en) | 1973-08-21 | 1973-08-21 | Liquid interface diffusion method of bonding parts made of titanium or titanium based alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1438842A true GB1438842A (en) | 1976-06-09 |
Family
ID=10409267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3938573A Expired GB1438842A (en) | 1973-08-21 | 1973-08-21 | Liquid interface diffusion method of bonding parts made of titanium or titanium based alloy |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1438842A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2134832A (en) * | 1983-02-15 | 1984-08-22 | Messerschmitt Boelkow Blohm | Method of etablishing a bond between titanium and an iron-nickel alloy |
US4703159A (en) * | 1980-07-02 | 1987-10-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of manufacturing lightweight thermo-barrier material |
US9120173B2 (en) | 2011-07-19 | 2015-09-01 | Rolls-Royce Plc | Bonding of metal components |
CN110823768A (en) * | 2019-11-21 | 2020-02-21 | 中国核动力研究设计院 | Device and method for researching interface compatibility of solid material |
-
1973
- 1973-08-21 GB GB3938573A patent/GB1438842A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4703159A (en) * | 1980-07-02 | 1987-10-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of manufacturing lightweight thermo-barrier material |
GB2134832A (en) * | 1983-02-15 | 1984-08-22 | Messerschmitt Boelkow Blohm | Method of etablishing a bond between titanium and an iron-nickel alloy |
US9120173B2 (en) | 2011-07-19 | 2015-09-01 | Rolls-Royce Plc | Bonding of metal components |
CN110823768A (en) * | 2019-11-21 | 2020-02-21 | 中国核动力研究设计院 | Device and method for researching interface compatibility of solid material |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PE20 | Patent expired after termination of 20 years |
Effective date: 19930820 |