CN2765708Y - Oil oven radiating fin circumferential spot welder - Google Patents
Oil oven radiating fin circumferential spot welder Download PDFInfo
- Publication number
- CN2765708Y CN2765708Y CN 200520054360 CN200520054360U CN2765708Y CN 2765708 Y CN2765708 Y CN 2765708Y CN 200520054360 CN200520054360 CN 200520054360 CN 200520054360 U CN200520054360 U CN 200520054360U CN 2765708 Y CN2765708 Y CN 2765708Y
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- fuselage
- cylinder
- soldering tip
- lifting
- welding machine
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Abstract
The utility model discloses an oil oven radiating fin circumferential spot welder, which comprises a host machine and a control cabinet which is connected with the host machine, wherein the host machine comprises a body which is composed of a left body, a right body and a back body, one side of each of the left and the right bodies is a fixed body, and the other side is a movable body. The left body or the right body is fixed on a body base, the front wall of the back body is provided with a slide way, the left body or the right body is movably connected with the slide way, and the left body or the right body can slide along the slide way. The inner side walls of the left body and the right body are respectively fixed with a set of welding device, the upper parts of the left and the right bodies are used for lifting and pressing a left and a right lifting pressing mechanisms of heat radiating fins. The utility model has the advantages of high automation, convenient operation and high product qualified rate.
Description
Technical field
The utility model relates to a kind of electroplating equipment wielding machine, more particularly, relates to a kind of resistance-type circumferential point welding machine that boss between the oil-filled stove fin is welded automatically.
Background technology
Traditional to be used between the oil-filled stove fin that boss welds be to adopt argon arc welding or gas welding welding, and human factor is more, the welding quality instability, more than two kinds of welding also have following defective: the welding operation complexity, the welding cost height, product structure intensity is low, and product percent of pass is low.
The utility model content
The purpose of this utility model is to overcome above-mentioned defective, provides a kind of welding operation easy, and welding cost is low, product structure intensity height, the oil-filled stove fin circumferential point welding machine that product percent of pass is high.
For achieving the above object, the technical scheme that the utility model provides is as follows: a kind of oil-filled stove fin circumferential point welding machine is provided, comprise main frame, the switch board that is connected with main frame, be provided with PLC control system and microcomputer controller in the switch board, described main frame comprises fuselage, this fuselage is made of left and right fuselage and rear body, on one side left and right fuselage is a fixed main body, another side is movable fuselage; Left side fuselage or right fuselage are installed on the fuselage base, and the antetheca of rear body is provided with slide rail, and left fuselage or right fuselage and slide rail flexibly connect, and movable fuselage can slide along slide rail; Respectively be installed with a cover welder on the madial wall of left side fuselage, right fuselage; Left and right back is provided with the left and right lifting hold-down mechanism that is used to promote, compress fin.
Described welder is by lift cylinder, the casing that is connected with lift cylinder, be arranged on casing top soldering tip, be arranged on the weld cylinder that is connected with soldering tip in the casing and be arranged on soldering tip off normal cylinder formation on the wall box, soldering tip is connected with intermediate frequency or power frequency supply, bottom half is provided with drive motors, drive motors is connected with reduction box, bottom half is provided with through hole, the rotating shaft of reduction box is inserted in the case from through hole, rotating shaft is floated with the soldering tip parts and is connected, rotatable and upper and lower the floating of soldering tip.
Described lifting hold-down mechanism is by the bearing of fixedlying connected with left and right fuselage, be arranged on the workpiece lifting cylinder that covers on the bearing, the lifting compact heap formation that is arranged on the Work-sheet pressing cylinder in the bearing and is connected with workpiece lifting cylinder, Work-sheet pressing cylinder, bearing is provided with and is used for the left and right inductive switch that the workpiece lifting compresses.
Oil-filled stove fin circumferential point welding machine described in the utility model adopts the intermediate frequency or the power frequency source of welding current, is controlled by microcomputer controller and PLC, has the automaticity height, and is easy and simple to handle, the advantage that product percent of pass is high.
Description of drawings
Fig. 1 is the front view of the oil-filled stove fin of the utility model circumferential point welding machine main frame;
Fig. 2 is the left view of Fig. 1;
Fig. 3 is the front view of the oil-filled stove fin of the utility model circumferential point welding machine switch board;
Fig. 4 is the front view of the oil-filled stove fin of the utility model circumferential point welding machine welder;
Fig. 5 is the left view of Fig. 3;
Fig. 6 is the front view of the oil-filled stove fin of the utility model circumferential point welding machine hoisting mechanism;
The specific embodiment
With reference to Fig. 1, Fig. 2, a kind of oil-filled stove fin circumferential point welding machine is provided, comprise main frame 1, the switch board 2 that is connected with main frame 1, be provided with PLC control system and microcomputer controller in the switch board 2, described main frame 1 comprises fuselage, and this fuselage is made of left and right fuselage 3,4 and rear body 5, left and right fuselage 3,4 is a fixed main body on one side, and another side is movable fuselage; Left side fuselage 3 is installed on the fuselage base 6, and the antetheca of rear body 5 is provided with slide rail 7, and right fuselage 4 flexibly connects with slide rail 7, and right fuselage 4 Din Rails 7 are along sliding; Respectively be installed with a cover welder 8,30 on the madial wall of left side fuselage 3, right fuselage 4; Left and right fuselage 3,4 tops are provided with the left and right lifting hold-down mechanism 10,11 that is used to promote, compress fin.
Described welder 8,30 by lift cylinder 12, the casing 13 that is connected with lift cylinder 12, be arranged on the soldering tip 14 on casing 13 tops, the soldering tip off normal cylinder 16 that is arranged on the weld cylinder 15 that is connected with soldering tip 14 in the casing 13 and is arranged on casing 13 sidewalls constitutes, soldering tip 14 is connected with intermediate frequency or power frequency supply, casing 13 bottoms are provided with drive motors 17, drive motors 17 is connected with reduction box 18, casing 13 bottoms are provided with through hole, rotating shaft in the reduction box 18 is inserted in the case from through hole, rotating shaft connects with drive block 19, and drive block 19 adopts to float with soldering tip swivel head 20 and connects.
Described lifting hold-down mechanism 10,11 is by the bearing 24 of fixedlying connected with left and right fuselage 3,4, be arranged on lifting compact heap 27 formations that the workpiece that covers on the bearing 24 promotes cylinder 25, is arranged on the Work-sheet pressing cylinder 26 in the bearing 24 and is connected with workpiece lifting cylinder 25, Work-sheet pressing cylinder 26, bearing 24 is provided with the left and right cylinder 28,29 that is used for the workpiece alignment, compresses.
When welding, adjust right fuselage 4 (movable fuselage), right fuselage 4 can adopt manual adjustment, also can adopt electronic adjustment, manual last first fin, a left side, right inductive switch 31,32 sense fin after, promoting cylinder 25 actions mentions fin, manual last second workpiece, a left side, right inductive switch 31,32 sense fin after, clamping cylinder 26 action compresses first fin, then, promote hold-down mechanism 10,11 lifting compact heap 27 makes first, the alignment of second fin compresses welder 8, a left side of 30, right lift cylinder 12 actions make a left side, backhand welding 14 rise simultaneously, a left side, 16 actions of right avertence position cylinder, make soldering tip 14 off normals, a left side, backhand welding connects cylinder 15 actions, makes a left side, backhand welding 14 welding simultaneously a bit; After first means of spot welds is finished, casing 13 bottoms of the lift cylinder 12 of welder 8,30 are provided with drive motors 17 actions, left and right soldering tip 14 is rotated to an angle simultaneously, weld down then a bit, after the last point welding is finished, soldering tip off normal cylinder 16 on casing 13 sidewalls of welder 8,30 makes left and right soldering tip return original position partially, left and right lift cylinder 12 actions of welder 8,30, make left and right soldering tip 14 drop to original position simultaneously, the lifting cylinder 25 that promotes hold-down mechanism 10,11 is mentioned the fin that welds.More than constantly circulation of action after an oil-filled stove fin is finished in welding, is taken out the fin that welds, and then carries out the welding of next oil-filled stove fin again.
Claims (4)
1, a kind of oil-filled stove fin circumferential point welding machine comprises main frame, the switch board that is connected with main frame, it is characterized in that, described main frame comprises fuselage, this fuselage is made of left and right fuselage and rear body, on one side left and right fuselage is a fixed main body, another side is movable fuselage; Left side fuselage or right fuselage are installed on the fuselage base, and the antetheca of rear body is provided with slide rail, and left fuselage or right fuselage and slide rail flexibly connect, and right fuselage can slide along slide rail; Respectively be installed with a cover welder on the madial wall of left side fuselage, right fuselage; The top of left and right fuselage is provided with the left and right lifting hold-down mechanism that is used to promote, compress fin.
2, according to the described oil-filled stove fin circumferential point welding machine of claim 1, it is characterized in that, described welder is by lift cylinder, the casing that is connected with lift cylinder, be arranged on the soldering tip on casing top, the soldering tip off normal cylinder that is arranged on the weld cylinder that is connected with soldering tip in the casing and is arranged on the wall box constitutes, soldering tip is connected with intermediate frequency or power frequency supply, bottom half is provided with drive motors, drive motors is connected with reduction box, bottom half is provided with through hole, the rotating shaft of reduction box is inserted in the case from through hole, rotating shaft and soldering tip parts float and connect, soldering tip rotatable with fluctuate.
3, according to the described oil-filled stove fin circumferential point welding machine of claim 1, it is characterized in that, described lifting hold-down mechanism is arranged on the lifting compact heap formation that the workpiece that covers on the bearing promotes cylinder, is arranged on the Work-sheet pressing cylinder in the bearing and is connected with workpiece lifting cylinder, Work-sheet pressing cylinder by the bearing of fixedlying connected with left and right fuselage.
According to the described oil-filled stove fin circumferential point welding machine of claim 3, it is characterized in that 4, bearing is provided with and is used for the left and right inductive switch that the workpiece lifting compresses.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200520054360 CN2765708Y (en) | 2005-02-02 | 2005-02-02 | Oil oven radiating fin circumferential spot welder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200520054360 CN2765708Y (en) | 2005-02-02 | 2005-02-02 | Oil oven radiating fin circumferential spot welder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2765708Y true CN2765708Y (en) | 2006-03-22 |
Family
ID=36606369
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200520054360 Expired - Fee Related CN2765708Y (en) | 2005-02-02 | 2005-02-02 | Oil oven radiating fin circumferential spot welder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2765708Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100540207C (en) * | 2007-05-22 | 2009-09-16 | 黄卓明 | A kind of novel straight seam welding machine |
| CN102528351A (en) * | 2012-02-17 | 2012-07-04 | 常熟市友邦散热器有限责任公司 | Radiating fin edge welding machine for transformer finned radiator |
| CN102554527A (en) * | 2012-02-17 | 2012-07-11 | 常熟市友邦散热器有限责任公司 | Edge welding machine for radiating fins of radiator |
-
2005
- 2005-02-02 CN CN 200520054360 patent/CN2765708Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100540207C (en) * | 2007-05-22 | 2009-09-16 | 黄卓明 | A kind of novel straight seam welding machine |
| CN102528351A (en) * | 2012-02-17 | 2012-07-04 | 常熟市友邦散热器有限责任公司 | Radiating fin edge welding machine for transformer finned radiator |
| CN102554527A (en) * | 2012-02-17 | 2012-07-11 | 常熟市友邦散热器有限责任公司 | Edge welding machine for radiating fins of radiator |
| CN102554527B (en) * | 2012-02-17 | 2014-06-11 | 常熟市友邦散热器有限责任公司 | Edge welding machine for radiating fins of radiator |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20060322 Termination date: 20140202 |