CN105171321B - Whole installing and welding tool for FT15 missile launcher - Google Patents
Whole installing and welding tool for FT15 missile launcher Download PDFInfo
- Publication number
- CN105171321B CN105171321B CN201510282988.XA CN201510282988A CN105171321B CN 105171321 B CN105171321 B CN 105171321B CN 201510282988 A CN201510282988 A CN 201510282988A CN 105171321 B CN105171321 B CN 105171321B
- Authority
- CN
- China
- Prior art keywords
- group
- pair
- missile
- weld seam
- launcheies
- 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 - Fee Related
Links
- 238000003466 welding Methods 0.000 title claims abstract description 30
- 230000007306 turnover Effects 0.000 claims abstract description 13
- 238000000034 method Methods 0.000 claims description 8
- 238000001816 cooling Methods 0.000 claims description 3
- 239000011324 bead Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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 for a procedure covered by only one of the other main groups of this subclass
- B23K37/04—Auxiliary devices or processes, not specially adapted for a procedure covered by only one of the other main groups of this subclass for holding or positioning work
- B23K37/047—Auxiliary devices or processes, not specially adapted for a procedure covered by only one of the other main groups of this subclass for holding or positioning work moving work to adjust its position between soldering, welding or cutting steps
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automatic Assembly (AREA)
- Arc Welding In General (AREA)
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 (7), a set of expanding rods (6), 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, and in particular to FT15 missile launcher integral assembly welding frocks.
Background technology
Missile launcher is thin-walled group welding piece, and its design size and appearance and size requirement are extremely strict, and in welding,
Due to welding bead it is long, it is high to welding performance requirement, so needing a kind of weld jig to meet after welding requirements and welding
Dimensional requirement.
The content of the invention
The purpose of the present invention is aiming at above-mentioned requirement, and provides FT15 missile launcher integral assembly welding frocks.
The present invention include framework, one group of column, one group of locating dowel, one group of fastening screw, a pair of weld seam plates, one group of crossbeam,
One group of tighting rod, a pair of interior lining panels, one group of tightening piece and a pair of turnover discs, are respectively equipped with one group of screwed hole on one group of column, and one
Group column and one group of locating dowel are respectively and fixedly installed on framework, and one group of fastening screw is located at respectively one group of spiral shell on one group of column
In pit, weld seam is respectively equipped with a pair of weld seam plates and avoids hole, a pair of weld seam plates are located at respectively one group of column and one group of locating dowel
Between, one group of tighting rod is respectively equipped with one group of crossbeam by hole, one group of crossbeam is respectively and fixedly installed on framework, one group of tensioner
Bar is each passed through one group of tighting rod on one group of crossbeam by hole, weld seam escape groove is respectively equipped with a pair of interior lining panels, in one pair
Liner plate is located between a pair of weld seam plates respectively, and one group of tightening piece is respectively and fixedly installed on one group of tighting rod, and one group of tightening piece
It is located between a pair of interior lining panels respectively, is respectively equipped with square by hole on a pair of turnover discs, a pair of turnover discs is fixedly mounted respectively
At the two ends of framework.Using method：By FT15 missile launcheies to be welded insert a pair of weld seam plates 5 and a pair of interior lining panels 8 it
Between so that a pair of interior lining panels 8 are located inside FT15 missile launcheies, and the weld seam on a pair of weld seam plates 5 avoids hole position and leads in FT15
Launcher commissure is played, the weld seam escape groove of a pair of interior lining panels 8 is located at FT15 missile launcheies commissure, by one group of tightening piece 9
It is placed between a pair of interior lining panels 8, and by one group of tighting rod 6 by one group of downward tensioner of tightening piece 9, one group of fastening screw 4 is by one
Weld seam plate 5 and FT15 missile launcheies are held out against, you can FT15 missile launcheies are welded, can be passed through in welding process
A pair of turnover discs 10 are rotated to facilitate each welding position to FT15 missile launcheies to weld, after the completion of welding, FT15 is treated
Frock is opened again after missile launcher cooling takes out FT15 missile launcheies.
The method have the advantages that：Welding tooling is reasonable in design, easy to operate, simple structure, accurate positioning, it is ensured that good
Welding performance and micro welding deformation amount.
Description of the drawings
Fig. 1 is schematic structural view of the invention.
Fig. 2 is schematic structural view of the invention.
Fig. 3 is schematic structural view of the invention.
Fig. 4 is schematic structural view of the invention.
Specific embodiment
As shown in Figure 1,2,3, 4, the present invention include 1, one group of framework, 2, one group of column, 3, one group of fastening screw 4 of locating dowel,
A pair of 5, one group of weld seam plate, 7, one group of crossbeam tighting rods 6, a pair of interior lining panels, 8, one group of tightening piece 9 and a pair of turnover discs 10, one group
One group of screwed hole is respectively equipped with column 2, one group of column 2 and one group of locating dowel 3 are respectively and fixedly installed on framework 1, one group of top
Tight screw rod 4 is located at respectively in one group of screwed hole on one group of column 2, weld seam is respectively equipped with a pair of weld seam plates 5 and avoids hole, a pair
Weld seam plate 5 is located between one group of column 2 and one group of locating dowel 3 respectively, one group of tighting rod is respectively equipped with one group of crossbeam 7 and is passed through
Hole, one group of crossbeam 7 is respectively and fixedly installed on framework 1, and one group of tighting rod 6 is each passed through one group of tighting rod on one group of crossbeam 7
By hole, weld seam escape groove is respectively equipped with a pair of interior lining panels 8, a pair of interior lining panels 8 are located at respectively between a pair of weld seam plates 5, one
Group tightening piece 9 is respectively and fixedly installed on one group of tighting rod 6, and one group of tightening piece 9 is located at respectively between a pair of interior lining panels 8, and one
Square by hole to being respectively equipped with turnover disc 10, a pair of turnover discs 10 are respectively and fixedly installed to the two ends of framework 1.
Working method：FT15 missile launcheies to be welded are inserted between a pair of weld seam plates 5 and a pair of interior lining panels 8 so that
A pair of interior lining panels 8 are located inside FT15 missile launcheies, and the weld seam on a pair of weld seam plates 5 avoids hole position in FT15 missile launcheies
Commissure, the weld seam escape groove of a pair of interior lining panels 8 is located at FT15 missile launcheies commissure, and one group of tightening piece 9 is placed in into a pair
Between interior lining panel 8, and by one group of tighting rod 6 by one group of downward tensioner of tightening piece 9, one group of fastening screw 4 is by a pair of weld seam plates 5
Hold out against with FT15 missile launcheies, you can FT15 missile launcheies are welded, can be by rotating a pair in welding process
Turnover disc 10 after the completion of welding, treats FT15 MISSILE LAUNCHINGs to facilitate each welding position to FT15 missile launcheies to weld
Frock is opened again after frame cooling takes out FT15 missile launcheies.
Claims (1)
1. the using method of FT15 missile launcheies integral assembly welding frock, FT15 missile launcher integral assembly weldings frock includes frame
Frame（1）, one group of column（2）, one group of locating dowel（3）, one group of fastening screw（4）, a pair of weld seam plates（5）, one group of crossbeam（7）, one
Group tighting rod（6）, a pair of interior lining panels（8）, one group of tightening piece（9）With a pair of turnover discs（10）, one group of column（2）On be respectively equipped with
One group of screwed hole, one group of column（2）With one group of locating dowel（3）It is respectively and fixedly installed to framework（1）On, one group of fastening screw（4）
One group of column is located at respectively（2）On one group of screwed hole in, a pair of weld seam plates（5）On be respectively equipped with weld seam avoid hole, a butt welding
Seam plate（5）One group of column is located at respectively（2）With one group of locating dowel（3）Between, one group of crossbeam（7）On be respectively equipped with one group of tighting rod
By hole, one group of crossbeam（7）It is respectively and fixedly installed to framework（1）On, one group of tighting rod（6）It is each passed through one group of crossbeam（7）On
One group of tighting rod by hole, a pair of interior lining panels（8）On be respectively equipped with weld seam escape groove, a pair of interior lining panels（8）One is located at respectively
To weld seam plate（5）Between, one group of tightening piece（9）It is respectively and fixedly installed to one group of tighting rod（6）On, and one group of tightening piece（9）Point
Wei Yu not a pair of interior lining panels（8）Between, a pair of turnover discs（10）On be respectively equipped with square by hole, a pair of turnover discs（10）Respectively
It is fixedly mounted on framework（1）Two ends;It is characterized in that using method is：FT15 missile launcheies to be welded are inserted a pair
Between weld seam plate (5) and a pair of interior lining panels (8) so that a pair of interior lining panels (8) inside FT15 missile launcheies, a pair of weld seams
Weld seam on plate (5) avoids hole position in FT15 missile launcheies commissure, and the weld seam escape groove of a pair of interior lining panels (8) is located at FT15
Missile launcher commissure, one group of tightening piece (9) is placed between a pair of interior lining panels (8), and by one group of tighting rod (6) by one
The downward tensioner of group tightening piece (9), one group of fastening screw (4) holds out against a pair of weld seam plates (5) and FT15 missile launcheies, you can right
FT15 missile launcheies are welded, and by rotating a pair of turnover discs (10) FT15 guided missiles can be sent out with facilitating in welding process
Penetrate each welding position of frame to be welded, after the completion of welding, open frock again after the cooling of FT15 missile launcheies and take out FT15
Missile launcher.
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 CN105171321A (en) | 2015-12-23 |
| CN105171321B true 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) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106425260A (en) * | 2016-12-09 | 2017-02-22 | 荆楚理工学院 | Tooling for overall group welding of missile ejection rack |
| CN106392448A (en) * | 2016-12-09 | 2017-02-15 | 范璐璐 | Integral assembly welding tool of missile ejection rack and use method |
| CN108857117B (en) * | 2018-05-23 | 2020-11-27 | 武汉船用机械有限责任公司 | A kind of manufacturing method of high-strength launch silo fence structure |
| CN109079397B (en) * | 2018-10-16 | 2024-08-06 | 哈电集团（秦皇岛）重型装备有限公司 | Large-scale stainless steel welding H shaped steel assembly welding positioner |
| CN110340597B (en) * | 2019-06-27 | 2021-09-28 | 西安建筑科技大学 | Inflatable rectangular beam splicing mould and process |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2539129B2 (en) * | 1992-01-14 | 1996-10-02 | 株式会社巴コーポレーション | Welding equipment for column steel joints |
| JP2534215B2 (en) * | 1992-05-25 | 1996-09-11 | 株式会社神戸製鋼所 | Steel column welding equipment |
| 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
Also Published As
| Publication number | Publication date |
|---|---|
| CN105171321A (en) | 2015-12-23 |
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| 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 |