CN206065875U - Aviation clamp automatic screw fixing machine - Google Patents
Aviation clamp automatic screw fixing machine Download PDFInfo
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- CN206065875U CN206065875U CN201621067081.8U CN201621067081U CN206065875U CN 206065875 U CN206065875 U CN 206065875U CN 201621067081 U CN201621067081 U CN 201621067081U CN 206065875 U CN206065875 U CN 206065875U
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- screw
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- fixing machine
- seat
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- 238000003780 insertion Methods 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 11
- 238000012545 processing Methods 0.000 description 4
- 238000004806 packaging method and process Methods 0.000 description 3
- 206010054949 Metaplasia Diseases 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000015689 metaplastic ossification Effects 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 210000003437 trachea Anatomy 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
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Abstract
This utility model is related to screw fixing machine technical field, refers in particular to a kind of aviation clamp automatic screw fixing machine；This utility model includes track, dolly is slidably equipped with track, crossbeam is installed above track, crossbeam is provided with the unit that screws, the unit that screws is furnished with can be with parallel beams movement, the screw seat for vertically moving, the screw hole that screw seat is opened up with longitudinal direction, the unit that screws is furnished with can be with the lead screw of rotation and lifting, and the screw hole of screw seat is inserted in the lower end of lead screw；When dolly of the present utility model is moved; the screw seat of unit of screwing can carry out parallel beams movement, vertically move; so as to screw is squeezed on base plate or panel and socle; complete automatic assembling work; realize automated production; and feeding, feeding, the time shut down, improve production efficiency can be reduced.
Description
Technical field
This utility model is related to aviation clamp automatic screw fixing machine technical field, refers in particular to a kind of aviation clamp automatic screw nailing
Machine.
Background technology
The Chinese patent literature of Patent No. " 200920185540.6 ", discloses a kind of light packing plate for logistics
Plate, including panel, base plate, are characterized in that the lower end of panel is uniformly arranged base plate, are connected by socle between panel and base plate, socle
For hollow-core construction, socle two ends are the connection sheet of three or more than three, and connection sheet is connected as a single entity with socle side, panel,
Connection sheet of the base plate respectively by self-drilling screw with socle two ends is fixed, or panel, base plate connection sheet directly with socle two ends
On through hole thorn fix, panel formed by flat board and hollow sheeting are cementing, and cavity is provided with hollow sheeting.
Existing production process, usually using socle is locked into panel and base plate manually, production efficiency is relatively low.With certainly
The development of dynamicization science and technology, if the light packaging clamp widelyd popularize by aforementioned documents, needs automation equipment, realize this
Packaging clamp ground automated production, improves work efficiency.
Therefore, the automated production demand based on above-mentioned existing light packaging clamp, applicant develop automatic metaplasia
Product equipment, proposes present patent application.
The content of the invention
The purpose of this utility model is to provide a kind of aviation clamp automatic screw fixing machine for the deficiencies in the prior art, should
Aviation clamp automatic screw fixing machine solves the defect of existing low production efficiency.
For achieving the above object, this utility model is achieved through the following technical solutions：
Aviation clamp automatic screw fixing machine, including track, are slidably equipped with dolly on track, crossbeam is provided with above track,
Crossbeam is provided with the unit that screws, and the unit that screws is furnished with can be with parallel beams movement, the screw seat for vertically moving, screw seat tool
The screw hole for having longitudinal direction to open up, the unit that screws is furnished with can be with the lead screw of rotation and lifting, the lower end insertion screw seat of lead screw
Screw hole.
Specifically, screw unit, including fixed plate, slide rail, slide block, cylinder, upper mounting blocks, lower mounting blocks, screws
Motor, lead screw；Fixed plate is fixed with crossbeam, and fixed plate is longitudinally provided with cylinder, mounting blocks in air cylinder driven；Fixed plate
Slide rail is vertically arranged with, on slide rail, is furnished with slide block, slide block is connected with upper mounting blocks；The drive that screws is installed above upper mounting blocks
Galvanic electricity machine, the rotating shaft of the motor that screws drive lead screw；Screw seat is installed on the lower section of lower mounting blocks.
Specifically, the unit that screws is furnished with the unit motor that screws, and the unit motor that screws drives screw mandrel,
The unit that screws is set on screw mandrel, is driven by screw mandrel, and the unit that can make to screw produces the effect of parallel beams movement.
Further, there are above screw seat two holes, one is the hole passed through for lead screw, and this hole is indulged with screw hole
To connection, another is feedhole, and feedhole is inclined with screw hole and connected, and screw is admitted to feedhole, and is snapped down to screw hole,
Positioned at the lower section of lead screw, the operation that screws is waited.
Further, dress panel area, dress base section are provided with dolly direction along ng a path, can be to filling panel, dress base plate
Operated in turn is carried out, the time for waiting feeding is reduced, is further improved efficiency.
Further, fill in base section and there are multiple socle seats.Dress has multiple auxiliary stopper blocks in base section.
Further, fill in panel area and there is multiple limited blocks, auxiliary stopper block, realize quick positioning assembling.
It is furnished with support by track, crossbeam is installed on support.
The beneficial effects of the utility model are：When dolly is moved, the screw seat of the unit that screws can carry out parallel horizontal stroke
Beam is moved, is vertically moved, and so as to screw is squeezed on base plate or panel and socle, is completed automatic assembling work, is realized automatic
Metaplasia is produced, and can reduce feeding, feeding, the time shut down, improve production efficiency.
Description of the drawings
Fig. 1 is structural representation of the present utility model.
Partial schematic diagrams of the Fig. 2 for Fig. 1.
Fig. 3 is the structural representation of the unit that screws of the present utility model.
Fig. 4 is the structural representation of base plate of the present utility model and socle.
Fig. 5 is the structural representation of clamp of the present utility model.
Track 1, dress panel area 2, dress base section 3, support 4, screw unit 5, fixed plate 6, slide rail 7, slide block 8, cylinder
9, upper mounting blocks 10, lower mounting blocks 11, screw motor 12, lead screw 13, screw seat 14, feedhole 15, screw hole 16,
Base plate 18, socle seat 17, socle 19, panel 20, screw unit motor 21, auxiliary stopper block 22.
Specific embodiment
Below in conjunction with the accompanying drawings this utility model is further described.
Seeing Fig. 1 --- Fig. 5, this utility model aviation clamp automatic screw fixing machine include：Track 1,1 both sides of track are furnished with
Frame 4, the top of support 4 are provided with crossbeam, and crossbeam is provided with the unit 5 that screws, and this utility model has three groups of units 5 that screw,
The unit 5 that screws is furnished with screw seat 14, and screw to be installed is sent to screw seat 14, screw seat 14 can with parallel beams movement,
Vertically move, screw is moved to predeterminated position carries out the operation that screws, it is assumed that dolly moving direction is X-direction, then screw
Seat 14 is Y direction along cross beam movement direction, and it is Z-direction that screw seat 14 vertically moves direction.
The unit 5 that screws of the present utility model, including fixed plate 6, slide rail 7, slide block 8, cylinder 9, upper mounting blocks 10, lower peace
Dress block 11, the motor 12 that screws, lead screw 13.Fixed plate 6 is fixed with crossbeam, and fixed plate 6 is longitudinally provided with cylinder 9, Gu
Fixed board 6 is vertically arranged with slide rail 7, is furnished with two slide blocks 8 on slide rail 7, and slide block 8 is connected with upper mounting blocks 10, lower mounting blocks 11 respectively
Connect, the top of upper mounting blocks 10 is provided with the motor 12 that screws, the rotating shaft of the motor 12 that screws drives has longitudinal direction to set
The lead screw 13 put, the lower end insertion screw seat 14 of lead screw 13, the lower section of lower mounting blocks 11 is provided with screw seat 14, cylinder 9
Driving on mounting blocks 10.Lower mounting blocks 11 can be by other air cylinder drivens.
See Fig. 4, Fig. 5, the clamp of this utility model processing, including base plate 18 and panel 20, base plate 18 is in strip, for dividing
The scattered external force acted on above panel 20, panel 20 are used for placing articles.
The motor 12 that screws of the present utility model can drive lead screw 13 to rotate, the upper mounting blocks 10 of the driving of cylinder 9,
Motor 12, the lead screw 13 of screwing is vertically moved, so as to screw is pressed into base plate 18, socle 19 by lead screw 13.
The unit 5 that screws of the present utility model is furnished with the unit motor 21 that screws, and screw unit motor 21
Driving has screw mandrel, and the unit 5 that screws is set on screw mandrel.
It is screw hole 16 below screw seat 14, screw can be passed from screw hole 16, with two holes above screw seat 14,
One is the hole passed through for lead screw 13, this hole and 16 vertical communication of screw hole, and another is feedhole 15, feedhole 15 with
Screw hole 16 inclines connection, meanwhile, 16 part of screw hole below feedhole 15 is highly greater than or is close to the length of screw,
The head of screw so can be just made to fall in the lower section of lead screw 13.
Screw hole 16 is connected by trachea with outside feed table, pneumatic transfer, and therefore not to repeat here.
Dolly is slidably equipped with track of the present utility model 1, dress panel area 2, dress base plate on dolly direction along ng a path, is provided with
Area 3, dress panel area 2 fill base section 3 for base plate 18 and socle 19 are assembled fixation for panel 20 is assembled fixation.
As dress panel area 2, the dress operating area of base section 3 two are provided with dolly, in practice, when dress base section 3
When carrying out base plate 18 and screwing, operator can carry out feeding to filling panel area 2, likewise, when dress panel area 2 carries out panel 20
When screwing, operator can carry out feeding to filling base section 3, reduce the time that feeding is waited, shut down, improve production efficiency.
The operation of this utility model application processing is base plate 18 to be installed with socle 19 first, then panel 20 is installed.
There are in dress base section of the present utility model 3 multiple socle seats 17, socle seat 17 can have three rows, three row, correspondence
, one piece of panel 20 matches somebody with somebody three pieces of base plates 18.The shape of socle seat 17 is matched with socle 19, and socle seat 17 can be by multiple barrier sheets
It is trapped among, therefore not to repeat here.
There are in dress panel area of the present utility model 2 multiple limited blocks, limited block can have three rows, three pieces of base plates of correspondence
18, there can also be auxiliary stopper block 22, carry out for counter plate 20 spacing, panel 20 can be fixed by operator exactly.
As shown in FIG., as each socle 19 respectively has multiple fixed screws with base plate 18, panel 20, each screw
X, Y-coordinate are different from, and in the direction parallel to crossbeam, arrange three row socle seats 17 altogether, meanwhile, and due to dolly it is complete
Into dress base plate 18, dress 20 two operations of panel, so, during work, dolly moves the distance of a length of wagon along track 1, because
This, the length of track 1 need to be pre-designed.
The idiographic flow that base plate 18 is installed with socle 19 is as follows, and socle 19 is first correspondingly placed into the socle seat of dress base section 3
In 17, then base plate 18 is positioned over above socle 17, and quickly will be base plate 18 spacing by auxiliary stopper block 22；Spiral shell is beaten in startup
Screw can be squeezed into base plate 18 and be fixed with socle 19 by silk unit 5, the unit 5 that screws.
Dress panel 20 idiographic flow it is as follows, base plate 18 is overturn, make base plate 18 down, socle 19 upward, be put into dress face
The relevant position in plate area 2, panel 20 is positioned over above socle 19, starts the unit 5 that screws, screw is squeezed into panel 20 and foot
Post 19 is fixed.
Dress base section 3 of the present utility model has very big accommodation space, and multiple socles 19 first can be poured into by operator
The dress base section 3, quickly can be put into socle 19 in corresponding socle seat 17 during processing, reduce come and go take socle 19 when
Between, improve production efficiency has multiple limited blocks in dress panel area 2, and with quickly spacing to base plate 18 and panel 20, here is not made
Repeat.
The shape of the socle 19 of this utility model processing is not limited, and the shape of the socle on a clamp can not
Together, so, the shape of socle seat 17 can also be different, as needed depending on.
This utility model also includes various control circuit boards, controlling switch etc., does not repeat in the present patent application.
Dolly of the present utility model is moved on path 1, motor, belt, and dolly stops for fixed point when moving
Sensor of car etc., is not repeated in the present patent application.
This utility model can reduce feeding, feeding, the time shut down, improve production efficiency, and can reduce work
Cost.
Certainly, the embodiment of the above, simply preferred embodiments of the present utility model, not limit this utility model
Practical range, therefore the equivalence changes done of all constructions according to described in this utility model claim, feature and principle or repair
Decorations, all should be included in this utility model claim.
Claims (9)
1. aviation clamp automatic screw fixing machine, it is characterised in that：Including track, dolly, the top peace of track on track, are slidably equipped with
Equipped with crossbeam, crossbeam is provided with the unit that screws, and the unit that screws is furnished with can be with parallel beams movement, the screw for vertically moving
Seat, the screw hole that screw seat is opened up with longitudinal direction, the unit that screws is furnished with can be with the lead screw of rotation and lifting, the lower end of lead screw
The screw hole of insertion screw seat.
2. aviation clamp automatic screw fixing machine according to claim 1, it is characterised in that：Screw unit, including fixation
Plate, slide rail, slide block, cylinder, upper mounting blocks, lower mounting blocks, the motor that screws, lead screw；Fixed plate is fixed with crossbeam, Gu
Fixed board is longitudinally provided with cylinder, mounting blocks in air cylinder driven；Fixed plate is vertically arranged with slide rail, is furnished with slide block, slide block on slide rail
It is connected with upper mounting blocks；The motor that screws is installed above upper mounting blocks, the rotating shaft of the motor that screws drives spiral shell
Screw mandrel；Screw seat is installed on the lower section of lower mounting blocks.
3. aviation clamp automatic screw fixing machine according to claim 1, it is characterised in that：The unit that screws is furnished with and screws
Unit motor, the unit motor that screws drives screw mandrel, and the unit that screws is set on screw mandrel.
4. aviation clamp automatic screw fixing machine according to claim 1, it is characterised in that：There are two above screw seat
Hole, one is the hole passed through for lead screw, this hole and screw hole vertical communication, and another is feedhole, feedhole and screw
Hole inclines connection.
5. aviation clamp automatic screw fixing machine according to claim 1, it is characterised in that：Arrange on dolly direction along ng a path
There are dress panel area, dress base section.
6. aviation clamp automatic screw fixing machine according to claim 5, it is characterised in that：Dress has multiple feet in base section
Column base.
7. aviation clamp automatic screw fixing machine according to claim 5, it is characterised in that：Have in dress base section multiple auxiliary
Help limited block.
8. aviation clamp automatic screw fixing machine according to claim 5, it is characterised in that：There are multiple limits in dress panel area
Position block, auxiliary stopper block.
9. aviation clamp automatic screw fixing machine according to claim 1, it is characterised in that：It is furnished with support, crossbeam by track
It is installed on support.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620737119 | 2016-07-14 | ||
| CN2016207371191 | 2016-07-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206065875U true CN206065875U (en) | 2017-04-05 |
Family
ID=58439761
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621067081.8U Expired - Fee Related CN206065875U (en) | 2016-07-14 | 2016-09-21 | Aviation clamp automatic screw fixing machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206065875U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110977395A (en) * | 2019-11-28 | 2020-04-10 | 铜陵市佳龙飞电容器有限公司 | Rapid Assembly device is used in condenser processing |
-
2016
- 2016-09-21 CN CN201621067081.8U patent/CN206065875U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110977395A (en) * | 2019-11-28 | 2020-04-10 | 铜陵市佳龙飞电容器有限公司 | Rapid Assembly device is used in condenser processing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170405 |