CN208991845U - A kind of planer aircraft panels clamping device - Google Patents
A kind of planer aircraft panels clamping device Download PDFInfo
- Publication number
- CN208991845U CN208991845U CN201821776117.9U CN201821776117U CN208991845U CN 208991845 U CN208991845 U CN 208991845U CN 201821776117 U CN201821776117 U CN 201821776117U CN 208991845 U CN208991845 U CN 208991845U
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- Prior art keywords
- movable plate
- plate
- planer
- fixed plate
- aircraft panels
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Abstract
The utility model discloses a kind of planer aircraft panels clamping devices, are related to planer technical field of mechanical processing, it is intended to solve the problem of aircraft panels be easy to happen offset can not effective guarantee cutting accuracy.Its key points of the technical solution are that being provided with the fixed fixed plate in position and moveable plate on mounting table, the fixed plate and movable plate are in be oppositely arranged, it is equipped with threaded rod jointly between the fixed plate and movable plate, the nut being threadedly engaged with threaded rod is provided on the threaded rod, the nut is located at side of the movable plate far from fixed plate；It is provided with the sliding slot that the axis direction of threadingly bar extends on the top surface of the mounting table, is provided with the support plate being bonded with mounting table on the movable plate bottom wall, is provided with the sliding block being in sliding fit with the sliding chute on the support plate bottom wall.The utility model, which has achieved the effect that facilitate, clamps aircraft panels to be processed.
Description
Technical field
The utility model relates to planer technical fields of mechanical processing, clamp and fill more particularly, to a kind of planer aircraft panels
It sets.
Background technique
Planer is the linear motion lathe planed with planing tool to the plane of workpiece, groove or forming surface.Planer is
Make to generate opposite straight reciprocating motion between cutter and workpiece to achieve the purpose that workpiece surface of planing.Reciprocating motion is planer
On main motion.Lathe is other than having main motion, and there are also synkinesias, also cries feed campaign, the feed campaign of planer is work
Make the intermittent movement of platform.Can plane horizontal plane, vertical plane, inclined-plane, curved surface, step surface, swallow-tail form workpiece, T shape on planer
Slot, V-shaped groove, can also plane hole, gear and rack gear etc..
Referring to Fig.1, existing planer is mainly made of driving device 5, cutter device 51 and workbench 52, by aircraft panels
It is placed on workbench 52, driving device 5 drives workbench 52 mobile, and cutter device 51 can process aircraft panels.
Prior art among the above has the following deficiencies: in use, directly by aircraft panels to be processed
It is placed on workbench 52, the platform 52 that then pushes the work forward allows aircraft panels to cut through towards 51 side of cutter device is mobile to realize
Journey, but due to lacking clamping device, aircraft panels, which are located at the top of workbench 52, is easy to happen offset, it can not effective guarantee cutting
Precision, the problem have to be solved.
Utility model content
The purpose of the utility model is to provide a kind of planer aircraft panels clamping devices, have and facilitate clamping to be processed
The effect of aircraft panels.
The above-mentioned purpose of utility model of the utility model has the technical scheme that
A kind of planer aircraft panels clamping device, including mounting table are provided with the fixed fixation in position on the mounting table
Plate and moveable plate, the fixed plate and movable plate are in being oppositely arranged, between the fixed plate and movable plate jointly
It is equipped with threaded rod, the nut being threadedly engaged with threaded rod is provided on the threaded rod, it is separate that the nut is located at movable plate
The side of fixed plate；The sliding slot that the axis direction of threadingly bar extends, the movable plate are provided on the top surface of the mounting table
It is provided with the support plate being bonded with mounting table on bottom wall, is provided with the sliding block being in sliding fit with the sliding chute on the support plate bottom wall.
By using above-mentioned technical proposal, turn nut keeps it mobile relative to threaded rod, and nut pushes away in moving process
Dynamic movable plate is mobile, makes it along sliding slot constantly close to fixed plate, to realize the clamping to aircraft panels.The setting of support plate
The contact area of movable plate and mounting table is increased, to improve the stability in the moving process of movable plate, avoids collapsing.
The glide direction of the movable plate of the restriction that is slidably matched of sliding slot and sliding block moves it towards the direction close to or far from fixed plate
It is dynamic, to keep the clamping of aircraft panels to be processed more convenient.
The utility model is further arranged to: the movable plate is provided with inverted u-shaped protection far from the side of fixed plate
Cover, the nut are located in shield.
By using above-mentioned technical proposal, shield prevents nut due to being exposed to the external world, by outer for protecting nut
The shock on boundary or unintentionally turn keep movable plate mobile, cause aircraft panels to be processed to loosen, influence processing quality.It is anti-
Shield enhances the stability of clamping device, to improve the success rate of processing.
The utility model is further arranged to: finite place piece is set on the mounting table, be provided in the support plate with
The limiting slot of locating part inlay card cooperation.
By using above-mentioned technical proposal, when movable plate slides into the end of mounting table, locating part is embedded in limiting slot,
The activity of movable plate is limited, movable plate is prevented to be detached from mounting table, on Crater face, causes machine breakdown and casualties,
To achieve the purpose that safety in production.
The utility model is further arranged to: the sliding slot is dovetail groove, and the section of the sliding block is trapezoidal.
By using above-mentioned technical proposal, the connective stability of sliding slot and sliding block is can be improved in dovetail groove, in active procedure
In both avoid being separated from each other so that the movement of movable plate is more stable, and then keep the fixation of aircraft panels more solid.
The utility model is further arranged to: more than one ball, the ball and sliding slot are provided on the sliding block
Contact.
By using above-mentioned technical proposal, the sliding friction between sliding slot and sliding block is become rolling friction by ball, thus
Frictional force between the two is reduced, a possibility that stuck is on the one hand reduced, so that the movement of movable plate is more smooth, it is another
Aspect reduces external force needed for moving active plate, moves it more convenient.
The utility model is further arranged to: the fixed plate is provided with card slot, the card on the side wall of movable plate
Slot is horizontally extending.
Aircraft panels are lifted by insertion card slot in aircraft panels one end to be processed by using above-mentioned technical proposal
The other end.Then rotating nut moves it on threaded rod, while the direction for pushing movable plate towards close fixed plate is mobile, directly
It offsets to the aircraft panels other end with movable plate, to complete the clamping of aircraft panels.
The utility model is further arranged to: the movable plate is provided with increasing on the side wall of fixed plate and rubs burr.
By using above-mentioned technical proposal, increases the burr that rubs and increases confficient of static friction between movable plate and aircraft panels,
After aircraft panels are stuck between movable plate and fixed plate, movable plate is bigger to the frictional force between aircraft panels, so that
Aircraft panels are not easy to fall between movable plate and fixed plate, and then improve the clamping device stabilization fixed to aircraft panels
Property.
The utility model is further arranged to: be provided with graduation mark on the mounting table, the graduation mark from fixed plate to
The directional spreding of movable plate.
By using above-mentioned technical proposal, when the hardness of aircraft panels is inadequate, the pressure of application is excessive to will lead to plate class
Part distortion.After the size of precognition aircraft panels, it can be estimated by moving range of the graduation mark to movable plate, from
And reduce a possibility that constantly squeezing aircraft panels and cause deformation.
In conclusion the advantageous effects of the utility model are as follows:
1. by the setting of movable plate, threaded rod, nut and sliding slot, the sliding matching structure of sliding block, to reach folder
The purpose of tight aircraft panels；
2. by the setting of shield, to achieve the effect that improve aircraft panels clamping stability；
3. by the setting of graduation mark, to reduce the probability of the deformation of aircraft panels.
Detailed description of the invention
Fig. 1 is the overall structure diagram of background technique；
Fig. 2 is the overall structure diagram of the utility model embodiment；
Fig. 3 is the cross-sectional view of the utility model embodiment.
In figure, 1, mounting table；11, sliding slot；12, mounting groove；13, ball；14, locating part；15, graduation mark；2, fixed plate；
21, card slot；3, movable plate；31, support plate；32, sliding block；33, shield；34, limiting slot；35；Nut；4, threaded rod；41, spiral shell
It is female；5；Driving device；51, cutter device；52, workbench.
Specific embodiment
The utility model is described in further detail below in conjunction with attached drawing.
It is a kind of planer aircraft panels clamping device disclosed by the utility model referring to Fig. 2, including to be processed for carrying
Aircraft panels mounting table 1.It is provided on mounting table 1 and exists in fixed plate 2 relatively disposed in parallel and movable plate 3, fixed plate 2
Position on mounting table 1 is fixed, and movable plate 3 moves on mounting table 1, has been wholely set and has been placed on the bottom wall of movable plate 3
The support plate 31 that platform 1 is bonded, for reinforcing the stability of movable plate 3.
Referring to Fig. 2 and Fig. 3, there are two sliding slots 11 for setting on the top surface of mounting table 1, are located at the both ends of mounting table 1, and
And extended along the direction perpendicular to fixed plate 2 from movable plate 3 to fixed plate 2, it is provided on the bottom wall of support plate 31 and sliding slot
11 sliding blocks 32 being slidably matched, enable movable plate 3 along sliding slot 11 close to or far from fixed plate 2.Sliding slot 11 is dovetail groove,
The section of sliding block 32 be it is trapezoidal, the connective stability of sliding slot 11 Yu sliding block 32 is improved, so that the movement of movable plate 3 is more
Stablize.11 extending direction offers mounting groove 12 along the chute on the bottom wall of sliding block 32, and multiple balls are placed in mounting groove 12
13, ball 13 is contacted with sliding block 32, for reducing the friction between sliding slot 11 and sliding block 32.
Referring to Fig. 2, perforation is offered through the thickness of plate in fixed plate 2 and movable plate 3, fixed plate 2 and movable plate 3
It is inserted with threaded rod 4 jointly in perforation, threaded rod 4 is fixedly connected close to one end of fixed plate 2 with fixed plate 2.In the present embodiment,
Threaded rod 4 is welded and fixed with fixed plate 2.There are two the settings of threaded rod 4, is located at two sliding slots, 11 top.It is set on threaded rod 4
It is equipped with the nut 41 being threadedly engaged with threaded rod 4, nut 41 is located at side of the movable plate 3 far from fixed plate 2.Turn nut 41 makes
It offsets with movable plate 3, continues turn nut 41, and movable plate 3 can be pushed close to fixed plate 2, is located at movable plate 3 to clamp
Aircraft panels between fixed plate 2 facilitate processing.Turn nut 41 keeps it mobile towards the direction far from fixed plate 2, then pushes away
Dynamic movable plate 3 makes it away from fixed plate 2, can discharge aircraft panels.
Referring to Fig. 2, movable plate 3 is provided with shield 33 far from the side of fixed plate 2, and shield 33 is by three pieces of plate head and the tail
Connect composition, and shield 33 is inverted u-shaped to be fixed on movable plate 3.Nut 41 is located in shield 33, prevents nut 41 due to sudden and violent
It is exposed at the external world, by extraneous shock or unintentionally turn, keeps movable plate 3 mobile, causes aircraft panels to loosen, influence to process
Quality.
Referring to Fig. 2, finite place piece 14 is arranged in the end far from fixed plate 2 on mounting table 1, is provided with and limits in support plate 31
The limiting slot 34 of position 14 inlay card of part cooperation.When movable plate 3 slides into the end of mounting table 1, locating part 14 is embedded in limiting slot 34
It is interior, the activity of movable plate 3 is limited, movable plate 3 is prevented to be detached from mounting table 1, to achieve the purpose that safety in production.In this reality
It applies in example, locating part 14 is the screw rod being threadedly secured on mounting table 1, and nut 35 is provided on screw rod, and the diameter of nut 35 is grown up
In the width of limiting slot 34, make nut 35 can not be by limiting slot 34.The bottom wall of nut 35 is equal at a distance from 1 roof of mounting table
The thickness of support plate 31.After locating part 14 is embedded in limiting slot 34,35 bottom wall of nut can be abutted against with 31 roof of support plate,
To improve the stability of movable plate 3.
Referring to Fig. 2, it is provided with card slot 21 on the side wall opposite with movable plate 3 of fixed plate 2, card slot 21 prolongs in the horizontal direction
It stretches.It is provided with increasing on the side wall opposite with fixed plate 2 of movable plate 3 to rub burr (not marking in figure), increases movable plate 3 and plate class portion
Frictional force between part, so that clamping device is more stable to the fixation of aircraft panels.
Referring to Fig. 2, the both ends of mounting table 1 are provided with graduation mark 15, and graduation mark 15 is from fixed plate 2 to the direction of movable plate 3
Distribution, for observing the distance between fixed plate 2 and movable plate 3.It is carried out by moving range of the graduation mark 15 to movable plate 3 pre-
Estimate, to improve the precision of processing a possibility that reducing aircraft panels deformation.
The implementation principle of the present embodiment are as follows: aircraft panels one end to be processed is inserted into card slot 21, the other end is raised up to plate
Base part is horizontal, and then turn nut 41 keeps it mobile relative to threaded rod 4, and nut 41 pushes movable plate 3 in moving process
It is mobile, make it along sliding slot 11 constantly close to fixed plate 2, thus the aircraft panels being fixedly clamped between plate 2 and movable plate 3.
The embodiment of present embodiment is the preferred embodiment of the utility model, and not limitation is originally practical new according to this
The protection scope of type, therefore: the equivalence changes that all structures, shape, principle according to the utility model are done should all be covered by practical
Within novel protection scope.
Claims (8)
1. a kind of planer aircraft panels clamping device, including mounting table (1), it is characterised in that: be provided on the mounting table (1)
The fixed fixed plate (2) in position and moveable plate (3), the fixed plate (2) and movable plate (3) are in be oppositely arranged,
It is equipped with threaded rod (4), is provided on the threaded rod (4) and threaded rod jointly between the fixed plate (2) and movable plate (3)
(4) nut (41) being threadedly engaged, the nut (41) are located at the side of movable plate (3) far from fixed plate (2)；The mounting table
(1) it is provided with the sliding slot (11) that the axis direction of threadingly bar (4) extends on top surface, is arranged on movable plate (3) bottom wall
There is a support plate (31) being bonded with mounting table (1), is provided on support plate (31) bottom wall and is slidably matched with sliding slot (11)
Sliding block (32).
2. a kind of planer aircraft panels clamping device according to claim 1, it is characterised in that: the movable plate (3) is remote
Side from fixed plate (2) is provided with inverted u-shaped shield (33), and the nut (41) is located in shield (33).
3. a kind of planer aircraft panels clamping device according to claim 2, it is characterised in that: on the mounting table (1)
It is arranged finite place piece (14), the limiting slot (34) with the cooperation of locating part (14) inlay card is provided on the support plate (31).
4. a kind of planer aircraft panels clamping device according to claim 1, it is characterised in that: the sliding slot (11) is swallow
Stern notch, the section of the sliding block (32) are trapezoidal.
5. a kind of planer aircraft panels clamping device according to claim 4, it is characterised in that: set on the sliding block (32)
It is equipped with more than one ball (13), the ball (13) contacts with sliding slot (11).
6. a kind of planer aircraft panels clamping device according to claim 1, it is characterised in that: the fixed plate (2) is leaned on
It is provided with card slot (21) on the side wall of nearly movable plate (3), the card slot (21) is horizontally extending.
7. a kind of planer aircraft panels clamping device according to claim 6, it is characterised in that: the movable plate (3) is leaned on
Increasing is provided on the side wall of nearly fixed plate (2) to rub burr.
8. a kind of planer aircraft panels clamping device according to claim 1, it is characterised in that: on the mounting table (1)
It is provided with graduation mark (15), the graduation mark (15) is from fixed plate (2) to the directional spreding of movable plate (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821776117.9U CN208991845U (en) | 2018-10-30 | 2018-10-30 | A kind of planer aircraft panels clamping device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821776117.9U CN208991845U (en) | 2018-10-30 | 2018-10-30 | A kind of planer aircraft panels clamping device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208991845U true CN208991845U (en) | 2019-06-18 |
Family
ID=66805921
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821776117.9U Expired - Fee Related CN208991845U (en) | 2018-10-30 | 2018-10-30 | A kind of planer aircraft panels clamping device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208991845U (en) |
-
2018
- 2018-10-30 CN CN201821776117.9U patent/CN208991845U/en not_active Expired - Fee Related
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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: 20190618 Termination date: 20201030 |