CN105171321A - Whole installing and welding tool for FT15 missile launcher - Google Patents
Whole installing and welding tool for FT15 missile launcher Download PDFInfo
- Publication number
- CN105171321A CN105171321A CN201510282988.XA CN201510282988A CN105171321A CN 105171321 A CN105171321 A CN 105171321A CN 201510282988 A CN201510282988 A CN 201510282988A CN 105171321 A CN105171321 A CN 105171321A
- Authority
- CN
- China
- Prior art keywords
- group
- pair
- column
- interior lining
- crossbeam
- 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.)
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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
- B23K37/00—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups
- B23K37/04—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work
- B23K37/047—Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work moving work to adjust its position between soldering, welding or cutting steps
Abstract
The invention provides a whole installing and welding tool for an FT15 missile launcher. The whole installing and welding tool comprises a frame (1), a set of vertical columns (2), a set of positioning columns (3), a set of jacking screws (4), a pair of weld joint plates (5), a set of beams (6), a set of expanding rods (7), a pair of liner plates (8), a set of expanding blocks (9) and a pair of turnover discs (10). The welding tool is reasonable in design, convenient to operate, simple in structure and accurate in positioning, and good welding performance and the tiny welding deformation amount are guaranteed.
Description
Technical field
The present invention relates to missile launcher production equipment field, be specifically related to FT15 missile launcher integral assembly welding frock.
Background technology
fT15missile launcher is thin-walled group welding piece, and its design size and appearance and size require extremely strict, and when welding, because welding bead is long, high to welding performance requirement, so the dimensional requirement after needing a kind of weld clip prodigiosin to meet welding requirements and welding.
Summary of the invention
Object of the present invention is exactly for above-mentioned requirement, and provides FT15 missile launcher integral assembly welding frock.
The present invention includes framework, one group of column, one group of locating dowel, one group of fastening screw, one butt welded seam plate, one group of crossbeam, one group of tighting rod, a pair interior lining panel, one group of tightening piece and a pair turnover disc, one group of column is respectively equipped with one group of screwed hole, one group of column and one group of locating dowel are fixedly mounted on framework respectively, one group of fastening screw lays respectively in one group of screwed hole on one group of column, one butt welded seam plate is respectively equipped with weld seam and dodges hole, one butt welded seam plate lays respectively between one group of column and one group of locating dowel, one group of crossbeam is respectively equipped with one group of tighting rod passing hole, one group of crossbeam is fixedly mounted on framework respectively, one group of tighting rod is each passed through one group of tighting rod passing hole on one group of crossbeam, a pair interior lining panel is respectively equipped with weld seam escape groove, a pair interior lining panel lays respectively between a butt welded seam plate, one group of tightening piece is fixedly mounted on one group of tighting rod respectively, and one group of tightening piece lays respectively between a pair interior lining panel, a pair turnover disc is respectively equipped with square passing hole, a pair turnover disc is fixedly mounted on the two ends of framework respectively.
Advantage of the present invention is: welding tooling is reasonable in design, easy to operate, and structure is simple, accurate positioning, the welding performance that ensure that and the welding deformation amount of trace.
accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is structural representation of the present invention.
Fig. 3 is structural representation of the present invention.
Fig. 4 is structural representation of the present invention.
Detailed description of the invention
As Fig. 1, 2, 3, shown in 4, the present invention includes framework 1, one group of column 2, one group of locating dowel 3, one group of fastening screw 4, one butt welded seam plate 5, one group of crossbeam 6, one group of tighting rod 7, a pair interior lining panel 8, one group of tightening piece 9 and a pair turnover disc 10, one group of column 2 is respectively equipped with one group of screwed hole, one group of column 2 and one group of locating dowel 3 are fixedly mounted on framework 1 respectively, one group of fastening screw 4 lays respectively in one group of screwed hole on one group of column 2, one butt welded seam plate 5 is respectively equipped with weld seam and dodges hole, one butt welded seam plate 5 lays respectively between one group of column 2 and one group of locating dowel 3, one group of crossbeam 6 is respectively equipped with one group of tighting rod passing hole, one group of crossbeam 6 is fixedly mounted on framework 1 respectively, one group of tighting rod 7 is each passed through one group of tighting rod passing hole on one group of crossbeam 6, a pair interior lining panel 8 is respectively equipped with weld seam escape groove, a pair interior lining panel 8 lays respectively between a butt welded seam plate 5, one group of tightening piece 9 is fixedly mounted on one group of tighting rod 7 respectively, and one group of tightening piece 9 lays respectively between a pair interior lining panel 8, a pair turnover disc 10 is respectively equipped with square passing hole, a pair turnover disc 10 is fixedly mounted on the two ends of framework 1 respectively.
Working method: FT15 missile launcher (hereinafter referred to as workpiece) to be welded is inserted between a butt welded seam plate 5 and a pair interior lining panel 8, a pair interior lining panel 8 is made to be positioned at inside workpiece, weld seam on one butt welded seam plate 5 is dodged hole and is positioned at workpiece commissure, the weld seam escape groove of a pair interior lining panel 8 is positioned at workpiece commissure, one group of tightening piece 9 is placed between a pair interior lining panel 8, and by one group of tighting rod 7 by one group of tightening piece 9 tensioner downwards, one group of fastening screw 4 is by butt welded seam plate 5 and a workpiece pre-tightening, can weld workpiece, can be welded each welding position of workpiece to facilitate by rotation a pair turnover disc 10 in welding process, after having welded, after work-piece cools, open frock again take out workpiece.
Claims (1)
1.FT15 missile launcher integral assembly welding frock, it is characterized in that it comprises framework (1), one group of column (2), one group of locating dowel (3), one group of fastening screw (4), one butt welded seam plate (5), one group of crossbeam (6), one group of tighting rod (7), a pair interior lining panel (8), one group of tightening piece (9) and a pair turnover disc (10), one group of column (2) is respectively equipped with one group of screwed hole, one group of column (2) and one group of locating dowel (3) are fixedly mounted on framework (1) respectively, one group of fastening screw (4) lays respectively in one group of screwed hole on one group of column (2), one butt welded seam plate (5) is respectively equipped with weld seam and dodges hole, one butt welded seam plate (5) lays respectively between one group of column (2) and one group of locating dowel (3), one group of crossbeam (6) is respectively equipped with one group of tighting rod passing hole, one group of crossbeam (6) is fixedly mounted on framework (1) respectively, one group of tighting rod (7) is each passed through one group of tighting rod passing hole on one group of crossbeam (6), a pair interior lining panel (8) is respectively equipped with weld seam escape groove, a pair interior lining panel (8) lays respectively between a butt welded seam plate (5), one group of tightening piece (9) is fixedly mounted on one group of tighting rod (7) respectively, and one group of tightening piece (9) lays respectively between a pair interior lining panel (8), a pair turnover disc (10) is respectively equipped with square passing hole, a pair turnover disc (10) is fixedly mounted on the two ends of framework (1) respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510282988.XA CN105171321B (en) | 2015-05-29 | 2015-05-29 | Whole installing and welding tool for FT15 missile launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510282988.XA CN105171321B (en) | 2015-05-29 | 2015-05-29 | Whole installing and welding tool for FT15 missile launcher |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105171321A true CN105171321A (en) | 2015-12-23 |
| CN105171321B CN105171321B (en) | 2017-05-10 |
Family
ID=54893994
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510282988.XA Expired - Fee Related CN105171321B (en) | 2015-05-29 | 2015-05-29 | Whole installing and welding tool for FT15 missile launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105171321B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106392448A (en) * | 2016-12-09 | 2017-02-15 | 范璐璐 | Integral assembly welding tool of missile ejection rack and use method |
| CN106425260A (en) * | 2016-12-09 | 2017-02-22 | 荆楚理工学院 | Tooling for overall group welding of missile ejection rack |
| CN109079397A (en) * | 2018-10-16 | 2018-12-25 | 哈电集团（秦皇岛）重型装备有限公司 | A kind of large-size stainless steel welded H section steel group weldering positioning device |
| CN110340597A (en) * | 2019-06-27 | 2019-10-18 | 西安建筑科技大学 | A kind of inflatable rectangular beam splicing mould and technique |
| CN108857117B (en) * | 2018-05-23 | 2020-11-27 | 武汉船用机械有限责任公司 | Manufacturing method of high-strength launching well fence structural member |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05185222A (en) * | 1992-01-14 | 1993-07-27 | Tomoe Corp | Welding equipment for pillar steel-frame joint part |
| JPH05318109A (en) * | 1992-05-25 | 1993-12-03 | Kobe Steel Ltd | Device for welding steel frame structure |
| CN201552408U (en) * | 2009-11-13 | 2010-08-18 | 天津振汉机械装备有限公司 | Rotating machine used for welding box-type structural part |
| CN201702537U (en) * | 2010-03-16 | 2011-01-12 | 叶宏洪 | Crane girder tipping and positioning device |
| CN202591902U (en) * | 2012-05-07 | 2012-12-12 | 长沙建鑫机械制造有限公司 | Welding positioning tool for weld joints inside fixing support legs of automobile crane |
| CN203371212U (en) * | 2013-05-28 | 2014-01-01 | 中国十七冶集团有限公司 | Overturn support for welding H-shaped steel |
| CN204725079U (en) * | 2015-05-29 | 2015-10-28 | 荆门诺恒科技有限公司 | FT15 missile launcher integral assembly welding frock |
-
2015
- 2015-05-29 CN CN201510282988.XA patent/CN105171321B/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05185222A (en) * | 1992-01-14 | 1993-07-27 | Tomoe Corp | Welding equipment for pillar steel-frame joint part |
| JPH05318109A (en) * | 1992-05-25 | 1993-12-03 | Kobe Steel Ltd | Device for welding steel frame structure |
| CN201552408U (en) * | 2009-11-13 | 2010-08-18 | 天津振汉机械装备有限公司 | Rotating machine used for welding box-type structural part |
| CN201702537U (en) * | 2010-03-16 | 2011-01-12 | 叶宏洪 | Crane girder tipping and positioning device |
| CN202591902U (en) * | 2012-05-07 | 2012-12-12 | 长沙建鑫机械制造有限公司 | Welding positioning tool for weld joints inside fixing support legs of automobile crane |
| CN203371212U (en) * | 2013-05-28 | 2014-01-01 | 中国十七冶集团有限公司 | Overturn support for welding H-shaped steel |
| CN204725079U (en) * | 2015-05-29 | 2015-10-28 | 荆门诺恒科技有限公司 | FT15 missile launcher integral assembly welding frock |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106392448A (en) * | 2016-12-09 | 2017-02-15 | 范璐璐 | Integral assembly welding tool of missile ejection rack and use method |
| CN106425260A (en) * | 2016-12-09 | 2017-02-22 | 荆楚理工学院 | Tooling for overall group welding of missile ejection rack |
| CN108857117B (en) * | 2018-05-23 | 2020-11-27 | 武汉船用机械有限责任公司 | Manufacturing method of high-strength launching well fence structural member |
| CN109079397A (en) * | 2018-10-16 | 2018-12-25 | 哈电集团（秦皇岛）重型装备有限公司 | A kind of large-size stainless steel welded H section steel group weldering positioning device |
| CN110340597A (en) * | 2019-06-27 | 2019-10-18 | 西安建筑科技大学 | A kind of inflatable rectangular beam splicing mould and technique |
| CN110340597B (en) * | 2019-06-27 | 2021-09-28 | 西安建筑科技大学 | Inflatable rectangular beam splicing mould and process |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105171321B (en) | 2017-05-10 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170510 |
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| CF01 | Termination of patent right due to non-payment of annual fee |