CN108581282A - A kind of unmanned machining welder of General Aviation - Google Patents
A kind of unmanned machining welder of General Aviation Download PDFInfo
- Publication number
- CN108581282A CN108581282A CN201810392000.9A CN201810392000A CN108581282A CN 108581282 A CN108581282 A CN 108581282A CN 201810392000 A CN201810392000 A CN 201810392000A CN 108581282 A CN108581282 A CN 108581282A
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- babinet
- movable plate
- block
- movable
- 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
-
- 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
- B23K37/0426—Fixtures for other work
- B23K37/0435—Clamps
- B23K37/0443—Jigs
-
- 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
- B23K37/0461—Welding tables
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- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
The invention discloses a kind of unmanned machining welders of General Aviation, including babinet, the both sides of the bottom of box have been fixedly connected with supporting leg, the bottom of the supporting leg is fixedly connected with non-slip mat, the both sides of the top of the box have been fixedly connected with fixed plate, and top plate is fixedly connected at the top of the fixed plate.The present invention is by being arranged the first sliding groove, second sliding slot, electric telescopic rod, movable block, first sliding block, pull rod, fixed block, movable plate, second sliding block, telescopic mast, spring, movable plate, snap-gauge, cushion pad and controller cooperate, the good advantage of clamping effect is reached, it is bad to solve the unmanned machining welder clamping effect of existing General Aviation, unmanned plane workpiece is caused the problem of welding damage occur, make General Aviation unmanned plane when being welded, it is not in sliding, improve the accuracy of welding position, reduce the defect ware of unmanned plane workpiece.
Description
Technical field
The present invention relates to General Aviation technical field, the unmanned machining welder of specially a kind of General Aviation.
Background technology
General Aviation, refer to be engaged in Civil Aviation Activities other than public air transport using civil aircraft, including from
Thing industry, agricultural, forestry, fishery and the operation flight of construction industry and health care, rescue and relief work, meteorological detection, ocean prison
The flying activity of survey, scientific experiment, education and training, culture and sports etc., General Aviation industry are with General Aviation Flight activity
For core, cover the strategic of the full industrial chains such as all purpose aircraft research and development manufacture, the market operation, comprehensive coverage and Extension Services
New industry system.
It in the unmanned machining process of General Aviation, needs to use welder, in order to process General Aviation unmanned plane
When use, the unmanned machining welder of current existing General Aviation, clamping effect is bad, and General Aviation unmanned plane is made to exist
It when being welded, is easy to cause unmanned plane workpiece and slides, cause unmanned plane workpiece welding damage occur, reduce welding position
The accuracy set increases the defect ware of unmanned plane workpiece, to reduce the unmanned machining welder of General Aviation
Practicability.
Invention content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the present invention provides a kind of unmanned machining welder of General Aviation, have
The good advantage of clamping effect, it is bad to solve the unmanned machining welder clamping effect of existing General Aviation, causes nothing
There is the problem of welding damage in man-machine workpiece.
(2) technical solution
To achieve the above object, the present invention provides the following technical solutions：A kind of General Aviation unmanned machining welding dress
It sets, including babinet, the both sides of the bottom of box have been fixedly connected with supporting leg, and the bottom of the supporting leg is fixedly connected with anti-skidding
Pad, the both sides of the top of the box have been fixedly connected with fixed plate, top plate, the top are fixedly connected at the top of the fixed plate
It is fixedly connected with welder ontology at the center in board bottom portion, mounting table is fixedly connected at the center of the top of the box；
The both sides of the cabinet wall bottom offer the first sliding groove, and the top of the cabinet wall both sides offers
Second sliding slot, the bottom of the cabinet wall both sides and has been fixedly connected with electric telescopic rod, and the electric telescopic rod is far from case
One end of internal wall is fixedly connected with movable block, and the bottom of the movable block is fixedly connected with the be used cooperatively with the first sliding groove
The front of one sliding block, the movable block is connected with pull rod by movable axis, passes through movable axis at the top of the pull rod back side
It is connected with fixed block, movable plate is fixedly connected at the top of the fixed block, the both sides of the movable plate are fixedly connected with
There is the second sliding block being used cooperatively with second sliding slot, telescopic mast is fixedly connected at the center of the movable plate bottom, it is described to stretch
It is fixedly connected at the bottom of contracting column and the center of cabinet wall bottom, the surface of the telescopic mast is arranged with spring, the spring
Top and bottom be fixedly connected respectively at the center of the movable plate bottom and center of cabinet wall bottom, the movable plate
The both sides at top have been fixedly connected with movable plate, and the top of babinet, the top of the movable plate are through at the top of the movable plate
Portion is fixedly connected with snap-gauge.
Preferably, the bottom of the snap-gauge is fixedly connected with cushion pad, and the inner cavity of the cushion pad is provided with buffer layer.
Preferably, the inner cavity of the first sliding groove and the junction of the first sliding block are provided with wearing layer, the second sliding slot
The junction of inner cavity and the second sliding block be provided with wearing layer.
Preferably, be fixedly connected with controller on the right side of the babinet, the controller respectively with welder ontology and
Electric telescopic rod is electrically connected, the model MAM-200 of the controller.
(3) advantageous effect
Compared with prior art, the present invention provides a kind of unmanned machining welder of General Aviation, have following
Advantageous effect：
1, the present invention is by being arranged the first sliding groove, second sliding slot, electric telescopic rod, movable block, the first sliding block, pull rod, consolidating
Determine block, movable plate, the second sliding block, telescopic mast, spring, movable plate, snap-gauge, cushion pad and controller to cooperate, reaches card
The tight good advantage of effect, it is bad to solve the unmanned machining welder clamping effect of existing General Aviation, causes nobody
There is the problem of welding damage in machine workpiece, makes General Aviation unmanned plane when being welded, and is not in sliding, improves welding
The accuracy of position reduces the defect ware of unmanned plane workpiece, to improve the unmanned machining welder of General Aviation
Practicability.
2, the present invention plays supporting leg anti-skidding effect, solves supporting leg and slide when in use by the way that non-slip mat is arranged
The problem of moving, babinet is caused to slide is stablized by the way that the first sliding groove and the first sliding block is arranged when playing mobile to movable block
Effect, solves the problems, such as that movable block shakes when moving, by the way that second sliding slot and the second sliding block is arranged, is risen to movable plate
To the effect stablized when movement, solve the problems, such as that movable plate shakes when moving, it is right by the way that telescopic mast and spring is arranged
Movable plate plays the role of stablizing when use, solves the problems, such as that movable plate rocks when moving, by the way that cushion pad is arranged,
Play the role of protecting unmanned plane workpiece, solves snap-gauge when carrying out clamping to unmanned plane workpiece, snap-gauge is to unmanned plane workpiece
The problem of causing damage.
Description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is right side structural representation of the present invention.
In figure：1 babinet, 2 supporting legs, 3 non-slip mats, 4 fixed plates, 5 top plates, 6 welder ontologies, 7 mounting tables, 8 first are slided
Slot, 9 second sliding slots, 10 electric telescopic rods, 11 movable blocks, 12 first sliding blocks, 13 pull rods, 14 fixed blocks, 15 movable plates, 16 second
Sliding block, 17 telescopic masts, 18 springs, 19 movable plates, 20 snap-gauges, 21 cushion pads, 22 controllers.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
- 2 are please referred to Fig.1, a kind of unmanned machining welder of General Aviation, including babinet 1, the right side of babinet 1 are solid
Surely it is connected with controller 22, controller 22 is electrically connected with welder ontology 6 and electric telescopic rod 10 respectively, controller 22
The both sides of model MAM-200,1 bottom of babinet have been fixedly connected with supporting leg 2, and the bottom of supporting leg 2 is fixedly connected with non-slip mat 3,
By the way that non-slip mat 3 is arranged, anti-skidding effect is played to supporting leg 2, supporting leg 2 is solved and slides when in use, babinet 1 is caused to go out
The both sides of the problem of now sliding, 1 top of babinet have been fixedly connected with fixed plate 4, and the top of fixed plate 4 is fixedly connected with top plate 5,
It is fixedly connected with welder ontology 6 at the center of 5 bottom of top plate, mounting table 7 is fixedly connected at the center at 1 top of babinet；
The both sides of 1 inner wall bottom of babinet offer the first sliding groove 8, and the top of 1 inner wall both sides of babinet offers second
Sliding slot 9, the bottom of 1 inner wall both sides of babinet and has been fixedly connected with electric telescopic rod 10, and electric telescopic rod 10 is far from 1 inner wall of babinet
One end be fixedly connected with movable block 11, the bottom of movable block 11 is fixedly connected with first be used cooperatively with the first sliding groove 8 and slides
Block 12, the inner cavity of the first sliding groove 8 and the junction of the first sliding block 12 are provided with wearing layer, by the way that the first sliding groove 8 and first is arranged
Sliding block 12 is stablized when playing the role of mobile to movable block 11, solves the problems, such as that movable block 11 shakes when moving, moves
The front of motion block 11 is connected with pull rod 13 by movable axis, and the top at 13 back side of pull rod is connected with admittedly by movable axis
Determine block 14, the top of fixed block 14 is fixedly connected with movable plate 15, and the both sides of movable plate 15 have been fixedly connected with and second sliding slot 9
The second sliding block 16 being used cooperatively, the inner cavity of second sliding slot 9 and the junction of the second sliding block 16 are provided with wearing layer, pass through setting
Second sliding slot 9 and the second sliding block 16, stablize when playing the role of mobile to movable plate 15, solve movable plate 15 and go out when moving
The problem of now shaking is fixedly connected with telescopic mast 17, bottom and 1 inner wall of babinet of telescopic mast 17 at the center of 15 bottom of movable plate
It is fixedly connected at the center of bottom, the surface of telescopic mast 17 is arranged with spring 18, by the way that telescopic mast 17 and spring 18 is arranged, to work
Movable plate 15 plays the role of stablizing when use, solves the problems, such as that movable plate 15 rocks when moving, the top of spring 18
It is fixedly connected respectively at the center of 15 bottom of movable plate and at the center of 1 inner wall bottom of babinet with bottom, 15 top of movable plate
Both sides be fixedly connected with movable plate 19, the top of movable plate 19 is through to the top of babinet 1, and the top of movable plate 19 is fixed
It is connected with snap-gauge 20, the bottom of snap-gauge 20 is fixedly connected with cushion pad 21, by the way that cushion pad 21 is arranged, plays protection unmanned plane work
The effect of part solves snap-gauge 20 when carrying out clamping to unmanned plane workpiece, and snap-gauge 20 causes damage to ask unmanned plane workpiece
Topic, the inner cavity of cushion pad 21 are provided with buffer layer, by the way that the first sliding groove 8, second sliding slot 9, electric telescopic rod 10, movable block is arranged
11, the first sliding block 12, pull rod 13, fixed block 14, movable plate 15, the second sliding block 16, telescopic mast 17, spring 18, movable plate 19, card
Plate 20, cushion pad 21 and controller 22 cooperate, and have reached the good advantage of clamping effect, solve existing General Aviation without
Man-machine processing is bad with welder clamping effect, cause unmanned plane workpiece occur welding damage the problem of, make General Aviation without
It is man-machine when being welded, be not in sliding, improve the accuracy of welding position, reduce the inferior of unmanned plane workpiece
Product, to improve the practicability of the unmanned machining welder of General Aviation.
In use, the top that worker will need the unmanned plane workpiece welded to be placed on mounting table 7 first, then passes through control
Device 22 opens electric telescopic rod 10, and electric telescopic rod 10, which starts, drives movable block 11 to start to move, and the movement of movable block 11 drives the
One sliding block 12 is slided in the inner cavity of the first sliding groove 8, is stablized when movable block 11 being made to move, while the movement of movable block 11 passes through movable axis
Pull rod 13 is driven to start to move, the movement of pull rod 13 drives movable plate 15 to start to move by movable axis, and the movement of movable plate 15 drives
Telescopic mast 17 starts to shrink at, and movable plate 15 is squeezed to spring 18 while telescopic mast 17 is shunk, and so that the movement of movable plate 15 is stablized, together
When movable plate 15 movement drive the second sliding block 16 second sliding slot 9 inner cavity slide, make movable plate 15 move when stablize, then live
The movement of movable plate 15 drives movable plate 19 to start to move, and the movement of movable plate 19 drives snap-gauge 20 to start to move, and the movement of snap-gauge 20 drives
Cushion pad 21 carries out clamping to unmanned plane workpiece, and then worker opens welder ontology 6 by controller 22, makes welder
Ontology 6 starts to weld unmanned plane workpiece, to reach the good advantage of clamping effect.
In conclusion the unmanned machining welder of the General Aviation, by the first sliding groove 8, second sliding slot 9, electronic
Telescopic rod 10, movable block 11, the first sliding block 12, pull rod 13, fixed block 14, movable plate 15, the second sliding block 16, telescopic mast 17, bullet
Spring 18, movable plate 19, snap-gauge 20, cushion pad 21 and controller 22 cooperate, and solve existing General Aviation unmanned plane and add
Work is bad with welder clamping effect, and unmanned plane workpiece is caused the problem of welding damage occur.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (4)
1. a kind of unmanned machining welder of General Aviation, including babinet (1), it is characterised in that：Babinet (1) bottom
Both sides be fixedly connected with supporting leg (2), the bottom of the supporting leg (2) is fixedly connected with non-slip mat (3), babinet (1) top
The both sides in portion have been fixedly connected with fixed plate (4), and top plate (5), the top plate are fixedly connected at the top of the fixed plate (4)
(5) it is fixedly connected with welder ontology (6) at the center of bottom, is fixedly connected with and puts at the center at the top of the babinet (1)
Set platform (7)；
The both sides of babinet (1) the inner wall bottom offer the first sliding groove (8), and the top of babinet (1) the inner wall both sides is equal
It offers second sliding slot (9), the bottom of babinet (1) the inner wall both sides and has been fixedly connected with electric telescopic rod (10), it is described
The one end of electric telescopic rod (10) far from babinet (1) inner wall is fixedly connected with movable block (11), the bottom of the movable block (11)
It is fixedly connected with the first sliding block (12) being used cooperatively with the first sliding groove (8), the front of the movable block (11) passes through movable axis
It is connected with pull rod (13), the top at pull rod (13) back side is connected with fixed block (14) by movable axis, described
Movable plate (15) is fixedly connected at the top of fixed block (14), the both sides of the movable plate (15) have been fixedly connected with to be slided with second
The second sliding block (16) that slot (9) is used cooperatively is fixedly connected with telescopic mast (17), institute at the center of movable plate (15) bottom
It states and is fixedly connected at the bottom and the center of babinet (1) inner wall bottom of telescopic mast (17), the surface of the telescopic mast (17) is arranged
Have a spring (18), the top and bottom of the spring (18) respectively at the center of movable plate (15) bottom and babinet (1) inner wall
It is fixedly connected at the center of bottom, the both sides at the top of the movable plate (15) have been fixedly connected with movable plate (19), the movement
It is through to the top of babinet (1) at the top of plate (19), snap-gauge (20) is fixedly connected at the top of the movable plate (19).
2. a kind of unmanned machining welder of General Aviation according to claim 1, it is characterised in that：The snap-gauge
(20) bottom is fixedly connected with cushion pad (21), and the inner cavity of the cushion pad (21) is provided with buffer layer.
3. a kind of unmanned machining welder of General Aviation according to claim 1, it is characterised in that：Described first
The inner cavity of sliding slot (8) is provided with wearing layer with the junction of the first sliding block (12), and the inner cavity of the second sliding slot (9) is slided with second
The junction of block (16) is provided with wearing layer.
4. a kind of unmanned machining welder of General Aviation according to claim 1, it is characterised in that：The babinet
(1) be fixedly connected with controller (22) on the right side of, the controller (22) respectively with welder ontology (6) and electric telescopic rod
(10) it is electrically connected, the model MAM-200 of the controller (22).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810392000.9A CN108581282A (en) | 2018-04-27 | 2018-04-27 | A kind of unmanned machining welder of General Aviation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810392000.9A CN108581282A (en) | 2018-04-27 | 2018-04-27 | A kind of unmanned machining welder of General Aviation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108581282A true CN108581282A (en) | 2018-09-28 |
Family
ID=63610079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810392000.9A Pending CN108581282A (en) | 2018-04-27 | 2018-04-27 | A kind of unmanned machining welder of General Aviation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108581282A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108994515A (en) * | 2018-10-15 | 2018-12-14 | 赵硕 | A kind of integral new-energy passenger welding clamp of vehicle frame |
| CN111451614A (en) * | 2020-04-30 | 2020-07-28 | 东莞合安机电有限公司 | Welding equipment for light alloy motor shell |
| CN112059499A (en) * | 2020-08-06 | 2020-12-11 | 东莞理工学院 | Unmanned aerial vehicle production is with welding frock that has polishing performance |
| CN115365637A (en) * | 2022-10-27 | 2022-11-22 | 成都市鸿侠科技有限责任公司 | Clamping system for aviation part welding |
-
2018
- 2018-04-27 CN CN201810392000.9A patent/CN108581282A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108994515A (en) * | 2018-10-15 | 2018-12-14 | 赵硕 | A kind of integral new-energy passenger welding clamp of vehicle frame |
| CN111451614A (en) * | 2020-04-30 | 2020-07-28 | 东莞合安机电有限公司 | Welding equipment for light alloy motor shell |
| CN112059499A (en) * | 2020-08-06 | 2020-12-11 | 东莞理工学院 | Unmanned aerial vehicle production is with welding frock that has polishing performance |
| CN112059499B (en) * | 2020-08-06 | 2022-01-07 | 东莞理工学院 | Unmanned aerial vehicle production is with welding frock that has polishing performance |
| CN115365637A (en) * | 2022-10-27 | 2022-11-22 | 成都市鸿侠科技有限责任公司 | Clamping system for aviation part welding |
| CN115365637B (en) * | 2022-10-27 | 2022-12-23 | 成都市鸿侠科技有限责任公司 | Clamping system for aviation part welding |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180928 |