CN208628735U - A kind of aircraft plate face welding positioning tool - Google Patents
A kind of aircraft plate face welding positioning tool Download PDFInfo
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- CN208628735U CN208628735U CN201820928621.XU CN201820928621U CN208628735U CN 208628735 U CN208628735 U CN 208628735U CN 201820928621 U CN201820928621 U CN 201820928621U CN 208628735 U CN208628735 U CN 208628735U
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- fixedly connected
- leg
- plate face
- plate
- welding
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Abstract
The utility model relates to welding tooling technical fields, and disclose a kind of aircraft plate face welding positioning tool, including supporting leg, two opposite sides of the supporting leg are fixedly connected to fixed link, the inner wall of two supporting legs is fixedly connected to slideway, lifting leg is fixedly connected on the inside of four slideways, the outside of two lifting legs is fixedly connected to gear bar.The aircraft plate face welds positioning tool, the gear outside bull stick is driven by rotation turning handle, lifting leg on the inside of gear rotation driven gear item and two slideways, lifting leg will move up from the inside of supporting leg and change the height of support frame, rotational positioning nut makes regulating part, connecting rod and welding location-plate change soldering angle, aircraft plate face is located in welding location-plate by fixing clamp, rotation regulation handle makes anti-collision body fix aircraft plate face downwards, height and soldering angle can be arbitrarily adjusted, thus user-friendly.
Description
Technical field
The utility model relates to welding tooling technical field, specially a kind of aircraft plate face welds positioning tool.
Background technique
Three-dimension flexible welding tooling is widely used in steel construction, the manufacture of various automobile bodies, rail traffic welding, bicycle
Motorcycle manufacture, engineering machinery, frame and cabinet, pressure vessel, robot welding, panel beating, metal furniture, equipment assembly
With welding and the detection system such as industrial pipeline (flange).
Welding tooling is a set of fixture flexible for being welded and fixed, compressing and positioning, and is mainly used for welding various solderable
The welding of material, welding that is big, neutralizing small-sized material, but general welding positioning tool is too integrated, it cannot basis
It needs to increase to be adjusted and causes certain damage to property and manpower waste, so propose that a kind of aircraft plate face welding is fixed
Position tooling solves the problems, such as above-mentioned propose.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of aircraft plate face welding positioning tool, has adjusting
Height and the advantages of adjust welding panel angle, it is too integrated to solve general welding positioning tool, cannot be according to need
To be adjusted, the problem of causing certain damage to property and manpower to waste is increased.
(2) technical solution
To realize above-mentioned adjusting height and adjusting the purpose of welding panel angle, the utility model provides following technical side
Case: a kind of aircraft plate face welding positioning tool, including supporting leg, two opposite sides of the supporting leg are fixedly connected to solid
Fixed pole, the inner wall of two supporting legs are fixedly connected to slideway, are fixedly connected to lifting on the inside of four slideways
The outsides of leg, two lifting legs are fixedly connected to gear bar, and the external contact of two gear bars has a gear, and two
The inside of the gear is fixedly connected to bull stick, and the front of two bull sticks is fixedly connected to turning handle, two liters
It is fixedly connected to support frame at the top of drop leg, positioning plate, two positioning plates are fixedly connected at the top of support frame as described above
Inside be fixedly connected with connecting rod, two opposite sides of the positioning plate are fixedly connected to regulating part and welding positioning
Plate, the outside of two regulating parts are fixedly connected to location nut, and the inside of the welding location-plate is fixedly connected with
To determine screw, offers ventilation opening at the top of the welding location-plate, the external contact of the welding location-plate has a fixing clamp, and four
Regulation handle is fixedly connected at the top of the fixing clamp, the bottom of four regulation handles is fixedly connected to anti-collision body.
Preferably, the inside of two supporting legs is hollow, and the top of two supporting legs offers through-hole,
The front of two supporting legs offers circular through hole.
Preferably, four slideways include sliding rail and limited block, and one end of sliding rail is fixedly connected with the inner wall of supporting leg,
The other end of sliding rail is fixedly connected with the outside of lifting leg.
Preferably, the bull stick includes connecting rod and active joint, the circle that the outside and supporting leg front of active joint open up
Shape through-hole wall is fixedly connected, and connecting rod runs through active joint and extends to the inside of supporting leg.
Preferably, support frame as described above is " returning " font, and the left and right ends of support frame bottom are fixed with the top of lifting leg
It connects, the front-end and back-end at the top of support frame are fixedly connected with the bottom of positioning plate.
Preferably, the regulating part includes " L " type frame and bar, and the top of " L " type frame is and the bottom of welding location-plate
It is fixedly connected, bar runs through positioning plate and extends to the inside of location nut.
(3) beneficial effect
Compared with prior art, the utility model provides a kind of aircraft plate face welding positioning tool, has following beneficial
Effect:
The aircraft plate face welds positioning tool, drives the gear outside bull stick, gear rotation band movable tooth by rotation turning handle
The lifting leg on the inside of item and two slideways is taken turns, lifting leg will move up from the inside of supporting leg and change the height of support frame,
Rotational positioning nut makes regulating part, connecting rod and welding location-plate to change soldering angle, and the ventilation opening in welding location-plate can
Prevent aircraft plate face from overheating with available ventilation, aircraft plate face is located in welding location-plate by fixing clamp, and rotation regulation handle makes
Anti- collision body fixes downwards aircraft plate face, height and soldering angle can be arbitrarily adjusted, thus user-friendly.
Detailed description of the invention
Fig. 1 is the utility model structural front view；
Fig. 2 is the partial enlarged view of the utility model structure A.
In figure: 1 supporting leg, 2 fixed links, 3 lifting legs, 4 slideways, 5 gear bars, 6 gears, 7 bull sticks, 8 turning handles, 9 support frames,
10 positioning plates, 11 connecting rods, 12 regulating parts, 13 location nuts, 14 welding location-plates, 15 fixed screws, 16 ventilation openings, 17 are fixed
Folder, 18 regulation handles, 19 anti-collision bodies.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
A kind of aircraft plate face welding positioning tool referring to FIG. 1-2, including supporting leg 1, the inside of two supporting legs 1 are equal
To be hollow, the top of two supporting legs 1 offers through-hole, and the front of two supporting legs 1 offers circular through hole, two branch
The opposite side of support leg 1 is fixedly connected to fixed link 2, and the inner wall of two supporting legs 1 is fixedly connected to slideway 4, four cunnings
Road 4 includes sliding rail and limited block, and one end of sliding rail is fixedly connected with the inner wall of supporting leg 1, the other end and the lifting leg 3 of sliding rail
Outside is fixedly connected, and the inside of four slideways 4 is fixedly connected to lifting leg 3, and the outside of two lifting legs 3 is fixedly connected to
Gear bar 5, the external contact of two gear bars 5 have gear 6, and the inside of two gears 6 is fixedly connected to bull stick 7, and bull stick 7 wraps
Connecting rod and active joint are included, the outside of active joint is fixedly connected with the circular through hole inner wall that 1 front of supporting leg opens up, and connecting rod passes through
It wears active joint and extends to the inside of supporting leg 1, the front of two bull sticks 7 is fixedly connected to turning handle 8, two lifting legs 3
Top be fixedly connected to support frame 9, support frame 9 is " returning " font, and the left and right ends of 9 bottom of support frame and go up and down leg 3
Top be fixedly connected, the front-end and back-end at the top of support frame 9 are fixedly connected with the bottom of positioning plate 10, the top of support frame 9
Portion is fixedly connected with positioning plate 10, and the inside of two positioning plates 10 is fixedly connected with connecting rod 11, and two positioning plates 10 are opposite
Side is fixedly connected to regulating part 12 and welding location-plate 14, and regulating part 12 includes " L " type frame and bar, the top of " L " type frame
Portion is fixedly connected with the bottom of welding location-plate 14, and bar runs through positioning plate 10 and extends to the inside of location nut 13, and two
The outside of a regulating part 12 is fixedly connected to location nut 13, and the inside of welding location-plate 14 is fixedly connected with fixed screw
15, the top of welding location-plate 14 offers ventilation opening 16, and the external contact of welding location-plate 14 has fixing clamp 17, four fixations
The top of folder 17 is fixedly connected with regulation handle 18, and the bottom of four regulation handles 18 is fixedly connected to anti-collision body 19.
When in use, the gear 6 outside bull stick 7,6 rotation driven gear item 5 of gear and two are driven by rotation turning handle 8
The lifting leg 3 of 4 inside of slideway, lifting leg 3 will move up from the inside of supporting leg 1 and change the height of support frame 9, and rotation is fixed
Position nut 13 makes regulating part 12, connecting rod 11 and welding location-plate 14 to change soldering angle, the ventilation in welding location-plate 14
Mouth 16 can prevent aircraft plate face from overheating with available ventilation, and aircraft plate face is located in welding location-plate 14 by fixing clamp 17, rotate
Regulation handle 18 makes anti-collision body 19 fix aircraft plate face downwards, can arbitrarily adjust height and soldering angle, thus convenient
User uses.
In conclusion the aircraft plate face welds positioning tool, the gear 6 outside bull stick 7, tooth are driven by rotation turning handle 8
The lifting leg 3 of 6 rotation driven gear items 5 and two 4 insides of slideway is taken turns, lifting leg 3 will move up simultaneously from the inside of supporting leg 1
Change the height of support frame 9, rotational positioning nut 13 makes regulating part 12, connecting rod 11 and welding location-plate 14 to change welding angle
It spends, the ventilation opening 16 in welding location-plate 14 can prevent aircraft plate face from overheating with available ventilation, and fixing clamp 17 determines aircraft plate face
In welding location-plate 14, rotation regulation handle 18 makes anti-collision body 19 fix aircraft plate face downwards for position, can arbitrarily adjust
Height and soldering angle, thus user-friendly, it is too integrated to solve general welding positioning tool, Bu Nenggen
According to needs to be adjusted, the problem of causing certain damage to property and manpower to waste is increased.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that
There is also other identical elements in process, method, article or equipment including the element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of aircraft plate face welds positioning tool, including supporting leg (1), it is characterised in that: two supporting legs (1) are opposite
Side be fixedly connected to fixed link (2), the inner wall of two supporting legs (1) is fixedly connected to slideway (4), four institutes
It states and is fixedly connected to lifting leg (3) on the inside of slideway (4), the outside of two liftings leg (3) is fixedly connected to gear
The external contact of item (5), two gear bars (5) has gear (6), and the inside of two gears (6) is fixedly connected to
The front of bull stick (7), two bull sticks (7) is fixedly connected to turning handle (8), and the top of two liftings leg (3) is solid
Surely it is connected with support frame (9), is fixedly connected at the top of support frame as described above (9) positioning plate (10), two positioning plates (10)
Inside be fixedly connected with connecting rod (11), two opposite sides of the positioning plate (10) are fixedly connected to regulating part (12)
It is fixedly connected to location nut (13) with the outside of welding location-plate (14), two regulating parts (12), the welding is fixed
The inside of position plate (14) is fixedly connected with fixed screw (15), offers ventilation opening at the top of the welding location-plate (14)
(16), the external contact of the welding location-plate (14) has fixing clamp (17), and the top of four fixing clamps (17) is fixed to be connected
It is connected to regulation handle (18), the bottom of four regulation handles (18) is fixedly connected to anti-collision body (19).
2. a kind of aircraft plate face according to claim 1 welds positioning tool, it is characterised in that: two supporting legs
(1) inside be it is hollow, the top of two supporting legs (1) offers through-hole, the front of two supporting legs (1)
Offer circular through hole.
3. a kind of aircraft plate face according to claim 1 welds positioning tool, it is characterised in that: four slideways (4)
Including sliding rail and limited block, one end of sliding rail is fixedly connected with the inner wall of supporting leg (1), the other end of sliding rail and lifting leg (3)
Outside be fixedly connected.
4. a kind of aircraft plate face according to claim 1 welds positioning tool, it is characterised in that: the bull stick (7) includes
The outside of connecting rod and active joint, active joint is fixedly connected with the circular through hole inner wall that supporting leg (1) front opens up, and connecting rod passes through
It wears active joint and extends to the inside of supporting leg (1).
5. a kind of aircraft plate face according to claim 1 welds positioning tool, it is characterised in that: support frame as described above (9) is
" returning " font, the left and right ends of support frame (9) bottom and go up and down and are fixedly connected at the top of leg (3), at the top of support frame (9) before
End is fixedly connected with the bottom of positioning plate (10) with rear end.
6. a kind of aircraft plate face according to claim 1 welds positioning tool, it is characterised in that: regulating part (12) packet
" L " type frame and bar are included, the top of " L " type frame is fixedly connected with the bottom of welding location-plate (14), and bar runs through positioning plate
(10) and the inside of location nut (13) is extended to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820928621.XU CN208628735U (en) | 2018-06-15 | 2018-06-15 | A kind of aircraft plate face welding positioning tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820928621.XU CN208628735U (en) | 2018-06-15 | 2018-06-15 | A kind of aircraft plate face welding positioning tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208628735U true CN208628735U (en) | 2019-03-22 |
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ID=65734645
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820928621.XU Active CN208628735U (en) | 2018-06-15 | 2018-06-15 | A kind of aircraft plate face welding positioning tool |
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| Country | Link |
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| CN (1) | CN208628735U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116214241A (en) * | 2023-05-06 | 2023-06-06 | 沈阳宝隆飞机零部件有限公司 | Feeding and discharging device and method for processing airplane parts |
-
2018
- 2018-06-15 CN CN201820928621.XU patent/CN208628735U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116214241A (en) * | 2023-05-06 | 2023-06-06 | 沈阳宝隆飞机零部件有限公司 | Feeding and discharging device and method for processing airplane parts |
| CN116214241B (en) * | 2023-05-06 | 2023-07-07 | 沈阳宝隆飞机零部件有限公司 | Feeding and discharging device and method for processing airplane parts |
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