CN103990907A - High-temperature vacuum hard alloy welding method - Google Patents
High-temperature vacuum hard alloy welding method Download PDFInfo
- Publication number
- CN103990907A CN103990907A CN201410145484.9A CN201410145484A CN103990907A CN 103990907 A CN103990907 A CN 103990907A CN 201410145484 A CN201410145484 A CN 201410145484A CN 103990907 A CN103990907 A CN 103990907A
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- CN
- China
- Prior art keywords
- welding
- vacuum
- hard alloy
- temperature
- welding method
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- 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.)
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Classifications
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- 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
- B23K20/14—Preventing or minimising gas access, or using protective gases or vacuum during welding
-
- 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
-
- 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
- B23K20/24—Preliminary treatment
-
- 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
- B23K33/00—Specially-profiled edge portions of workpieces for making soldering or welding connections; Filling the seams formed thereby
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Powder Metallurgy (AREA)
Abstract
A high-temperature vacuum hard alloy welding method is characterized by including the steps of (1) surface treatment of welding faces, wherein one end of a hard alloy bar is grinded to form an angle of 15 degrees-25 degrees, and the welding end faces of two welded block materials are ground and polished to form mirror surfaces; (2) shaping treatment, wherein the welding faces are cleaned up through anhydrous alcohol and coated with an anaerobic adhesive, and then the two welding faces are bonded to be shaped; (3) vacuum welding, the shaped welded product is contained in a graphite boat and placed in a sintering area of a vacuum sintering furnace, and a welded opening is compressed through the gravity. The problem that an overlength and overlarge hard alloy is difficult to weld is solved in a bevel angle welding mode.
Description
Technical field:
The present invention relates to carbide alloy welding technology field, be specifically related to a kind of high temperature, vacuum carbide alloy welding method.
Background technology:
Along with scientific and technical development, the demand of carbide alloy is constantly had to new requirement.Especially in overlength super large carbide alloy demand, owing to being subject to the restriction of current general compacting, agglomerating plant, for example cannot produce overlength (hard alloy strip more than 1000mm): the hard alloy strip thin slice of the 1700mm * 22mm * 3mm producing now, can only weld with the rectangular of two 850mm; Super large (the above hard alloy blocks material of 50kg) is for example: the hard alloy blocks material of the long 200mm * wide 200mm * high 150mm producing now, can only be welded by two block length 200mm * wide 100mm * high 150mm, disposable compacting sintering cannot meet the market demand of current carbide alloy.
Summary of the invention:
The object of this invention is to provide a kind of high temperature, vacuum carbide alloy welding method, the mode that it welds by oblique angle, has solved overlength, super large carbide alloy welds difficult problem.
In order to solve the existing problem of background technology, the present invention is by the following technical solutions: its welding method is:
Step 1: the surface treatment of solder side
For hard alloy strip, weld: first the different thickness of root Ju goes out the angle of 15 °-25 ° in wherein one end grinding of two soldered carbide alloy bars, the welding end surface of two blocks of soldered piece material is polished, require flatness≤5 micron, be then polished to minute surface;
Step 2: heat treatment
Solder side is cleaned up with absolute alcohol, more a kind of anaerobic glue is coated on solder side surface, then two solders side are bonded together its sizing;
Step 3: vacuum welding
Welding product after sizing is installed in the sintering zone that is placed on vacuum sintering furnace with graphite boat, and by soldering opening gravitational compaction.Then according to different Hard alloys at 1380 ℃--select a temperature spot to carry out high-temperature vacuum welding for 1420 ℃, then according to product individual hour of the insulation 1-2 that varies in size after arriving welding temperature point.
The present invention has following beneficial effect: the mode that it welds by oblique angle, has solved overlength, super large carbide alloy welds difficult problem.
Accompanying drawing explanation:
Fig. 1 is that welding fabrication of the present invention is widened alloy sheets schematic diagram;
Fig. 2 be in Fig. 1 of the present invention a to schematic diagram;
Fig. 3 is that welding fabrication of the present invention lengthens alloy sheets schematic diagram;
Fig. 4 be in Fig. 3 of the present invention b to schematic diagram;
The specific embodiment:
Referring to Fig. 1-4, this specific embodiment by the following technical solutions: its welding method is:
Step 1: the surface treatment of solder side
For hard alloy strip, weld: first the different thickness of root Ju goes out the angle of 15 °-25 ° in wherein one end grinding of two soldered carbide alloy bars, the welding end surface of two blocks of soldered piece material is polished, require flatness≤5 micron, be then polished to minute surface;
Step 2: heat treatment
Solder side is cleaned up with absolute alcohol, more a kind of anaerobic glue is coated on solder side surface, then two solders side are bonded together its sizing;
Step 3: vacuum welding
Welding product after sizing is installed in the sintering zone that is placed on vacuum sintering furnace with graphite boat, and by soldering opening gravitational compaction.Then according to different Hard alloys at 1380 ℃--select a temperature spot to carry out high-temperature vacuum welding for 1420 ℃, then according to product individual hour of the insulation 1-2 that varies in size after arriving welding temperature point.
This specific embodiment has following beneficial effect: the mode that it welds by oblique angle, has solved overlength, super large carbide alloy welds difficult problem.
Claims (1)
1. high temperature, a vacuum carbide alloy welding method, is characterized in that its welding method is:
Step 1: the surface treatment of solder side
For hard alloy strip, weld: first the different thickness of root Ju goes out the angle of 15 °-25 ° in wherein one end grinding of two soldered carbide alloy bars, the welding end surface of two blocks of soldered piece material is polished, require flatness≤5 micron, be then polished to minute surface;
Step 2: heat treatment
Solder side is cleaned up with absolute alcohol, more a kind of anaerobic glue is coated on solder side surface, then two solders side are bonded together its sizing;
Step 3: vacuum welding
Welding product after sizing is installed in the sintering zone that is placed on vacuum sintering furnace with graphite boat, and by soldering opening gravitational compaction, then according to different Hard alloys at 1380 ℃--select a temperature spot to carry out high-temperature vacuum welding for 1420 ℃, then according to product individual hour of the insulation 1--2 that varies in size after arriving welding temperature point.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410145484.9A CN103990907A (en) | 2014-04-14 | 2014-04-14 | High-temperature vacuum hard alloy welding method |
Applications Claiming Priority (1)
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CN201410145484.9A CN103990907A (en) | 2014-04-14 | 2014-04-14 | High-temperature vacuum hard alloy welding method |
Publications (1)
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CN103990907A true CN103990907A (en) | 2014-08-20 |
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CN201410145484.9A Pending CN103990907A (en) | 2014-04-14 | 2014-04-14 | High-temperature vacuum hard alloy welding method |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110524080A (en) * | 2019-09-03 | 2019-12-03 | 无锡钻探工具厂有限公司 | A kind of vacuum soldering process of hard alloy and steel |
CN112122727A (en) * | 2020-09-27 | 2020-12-25 | 淄博晨启电子有限公司 | Forming process of high-reliability high-surge impact capability semiconductor protection device |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59159283A (en) * | 1983-03-01 | 1984-09-08 | Sumitomo Electric Ind Ltd | Hot joining method of sintered hard alloy |
US6155755A (en) * | 1998-03-02 | 2000-12-05 | Sumitomo Electric Industries, Ltd. | Hard sintered body tool |
CN102747242A (en) * | 2012-07-26 | 2012-10-24 | 株洲金鼎硬质合金有限公司 | Method for preparing large-size hard alloy |
CN102814532A (en) * | 2012-08-02 | 2012-12-12 | 泰兴市信达克刀具有限公司 | Method of V-shaped welding of solid carbide drill and solid carbide drill thereof |
CN103228393A (en) * | 2010-11-26 | 2013-07-31 | 住友电气工业株式会社 | Joint |
CN103691960A (en) * | 2013-12-25 | 2014-04-02 | 苏州新锐合金工具股份有限公司 | Double-layer hard alloy matrix and production method thereof |
-
2014
- 2014-04-14 CN CN201410145484.9A patent/CN103990907A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59159283A (en) * | 1983-03-01 | 1984-09-08 | Sumitomo Electric Ind Ltd | Hot joining method of sintered hard alloy |
US6155755A (en) * | 1998-03-02 | 2000-12-05 | Sumitomo Electric Industries, Ltd. | Hard sintered body tool |
CN103228393A (en) * | 2010-11-26 | 2013-07-31 | 住友电气工业株式会社 | Joint |
CN102747242A (en) * | 2012-07-26 | 2012-10-24 | 株洲金鼎硬质合金有限公司 | Method for preparing large-size hard alloy |
CN102814532A (en) * | 2012-08-02 | 2012-12-12 | 泰兴市信达克刀具有限公司 | Method of V-shaped welding of solid carbide drill and solid carbide drill thereof |
CN103691960A (en) * | 2013-12-25 | 2014-04-02 | 苏州新锐合金工具股份有限公司 | Double-layer hard alloy matrix and production method thereof |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110524080A (en) * | 2019-09-03 | 2019-12-03 | 无锡钻探工具厂有限公司 | A kind of vacuum soldering process of hard alloy and steel |
CN110524080B (en) * | 2019-09-03 | 2021-09-14 | 中地装(无锡)钻探工具有限公司 | Vacuum welding process for hard alloy and steel |
CN112122727A (en) * | 2020-09-27 | 2020-12-25 | 淄博晨启电子有限公司 | Forming process of high-reliability high-surge impact capability semiconductor protection device |
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Application publication date: 20140820 |