CN209441677U - A kind of unmanned plane wing pressure texture to be recycled - Google Patents
A kind of unmanned plane wing pressure texture to be recycled Download PDFInfo
- Publication number
- CN209441677U CN209441677U CN201821863571.8U CN201821863571U CN209441677U CN 209441677 U CN209441677 U CN 209441677U CN 201821863571 U CN201821863571 U CN 201821863571U CN 209441677 U CN209441677 U CN 209441677U
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- CN
- China
- Prior art keywords
- positioning seat
- substrate
- cylinder
- recycled
- compression
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Abstract
The utility model discloses a kind of unmanned plane wing pressure textures to be recycled, including substrate, base plate bottom is provided with support leg, positioning seat is provided on substrate, four angles of the bottom of positioning seat are connect by four support columns with substrate top, positioning seat upper end offers compression groove, and compression groove is slidably provided with compression blocks in the front end with positioning seat, compression groove；The first opening is offered along the length direction of compression groove, the first opening is slidably provided with link block, the bottom end gap setting on the top and positioning seat of pushing block and substrate；The first cylinder is provided on substrate, the first cylinder is fixed by the first cylinder mounting base with substrate, and the First piston bar on the first cylinder is connect with pushing block.On the one hand the utility model, is avoided injury while capable of effectively reducing the labor intensity of operator；On the other hand, compression efficiency and compression quality are improved, by wing compressed to slugs shape shape, is not only convenient for stacking and has saved parking space.
Description
Technical field
The utility model relates to a kind of recovery processing structures, specifically, in particular to a kind of be used for unmanned plane to be recycled
Wing pressure texture.
Background technique
With social development, unmanned plane is by more and more extensive use, when unmanned plane is integrally scrapped or wing damage needs
When replacing, then need to handle replaced wing, it is directly hand-held by operator when the mode of existing processing
Iron hammer pounded it is curved after be placed on warehouse and wait collection and uniform disposal, but existing way, on the one hand, labor intensity of operating staff
It is larger；And it is easy injury；On the other hand, compression efficiency and compression quality are poor, cause processing after wing volume still compared with
Greatly, memory space and transport space cannot effectively be saved.
Therefore those skilled in the art are dedicated to developing a kind of unmanned plane machine to be recycled that can effectively improve compression efficiency
Wing pressure texture.
Utility model content
In view of the above drawbacks of the prior art, the technical problem to be solved by the utility model is to provide one kind to have
Effect improves the unmanned plane wing pressure texture to be recycled of compression efficiency.
To achieve the above object, the utility model provides a kind of unmanned plane wing pressure texture to be recycled, including substrate,
The base plate bottom is provided with support leg, and positioning seat is provided on the substrate, and four angles of the bottom of the positioning seat pass through
Four support columns are connect with the substrate top, and the positioning seat upper end offers compression groove, the compression groove run through with it is described
The front end of positioning seat is slidably provided with compression blocks in the compression groove；
The first opening is offered along the length direction of the compression groove, first opening is slidably provided with connection
Block, the upper end of the link block are connect with the compression blocks, and the lower end of the link block is connect with pushing block, the pushing block with it is described
The bottom end gap setting on the top of substrate and the positioning seat；
The first cylinder is provided on the substrate, first cylinder is solid by the first cylinder mounting base and the substrate
Fixed, the First piston bar on first cylinder is connect with the pushing block；
The positioning base rear end offers the second opening with compression groove perforation, and second opening is slidable
It is provided with limited post, the rear end of the limited post is provided with limit plate, and the two sides of the positioning seat pass through the installation of the second cylinder
Seat is provided with the second cylinder, and the second piston bar on each second cylinder is connect with the both ends of the limit plate respectively.
Preferably, first opening is provided with triangle reinforcement block, the triangle reinforcement block simultaneously with it is described
Compression blocks are connected with the link block.
Preferably, two the first guide rods being parallel to each other are provided between the substrate and the positioning seat, it is described
First cylinder is located between two first guide rods, and the both ends of the pushing block are slidably set in each described first respectively
On guide rod, the both ends of first guide rod pass through locating piece while connecting with the substrate and the positioning seat.
Preferably, positioning seat back segment bottom open up it is jagged, the notch with it is described second opening runs through.
Preferably, offering third opening on the substrate, the third opening is located at the underface of the notch.
Preferably, being provided with pressing plate right above the compression groove, the two sides of the pressing plate are provided with sliding panel, described
Four second guide rods are provided on positioning seat, each sliding panel is mobilizable respectively to be set in each second guide rod
On；Each second guide rod upper end is connected with top plate, and each top plate passes through two locating rods and connect with the positioning seat,
Each second guide rod is located between two locating rods；
Screw thread is provided on wherein at least two second guide rods and is threadedly coupled with the sliding panel, has threaded the
Two guide rod lower ends rotatably pass through the positioning seat and the output axis connection with third motor, and the third motor passes through the
Three motor mounts are connect with the positioning seat bottom.
Preferably, the upper end of the pressing plate offers two limiting slots being parallel to each other, it is provided on the compression blocks
Two gag lever posts being used cooperatively with the limiting slot.
Preferably, being provided with two reinforcing rods immediately below the gag lever post, the other end of each reinforcing rod passes through
Triangle connecting plate is connect with the gag lever post.
The beneficial effects of the utility model are: on the one hand the utility model, can effectively reduce the labour of operator
It avoids injury while intensity；On the other hand, compression efficiency and compression quality are improved, by wing compressed to slugs shape shape,
It is not only convenient for stacking and has saved parking space.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of one specific embodiment of the utility model.
Fig. 2 is the left view structural representation of Fig. 1.
Fig. 3 is the right side structural representation of Fig. 1.
Fig. 4 is the overlooking structure diagram of Fig. 1.
Fig. 5 is the present invention looks up structural representation of Fig. 1.
Specific embodiment
The utility model is described in further detail with reference to the accompanying drawings and examples:
As shown in Figures 1 to 5, a kind of unmanned plane wing pressure texture to be recycled, including substrate 1,1 bottom of substrate are set
It is equipped with support leg 2, positioning seat 3 is provided on the substrate 1, four angles of the bottom of the positioning seat 3 pass through four support columns 5
It is connected at the top of the substrate 1,3 upper end of positioning seat offers compression groove 6, and the compression groove 6 runs through and the positioning seat 3
Front end, be slidably provided with compression blocks 7 in the compression groove 6；
The first opening 8 is offered along the length direction of the compression groove 6, the slidably company of being provided at first opening 8
Block 9 is connect, the upper end of the link block 9 is connect with the compression blocks 7, and the lower end of the link block 9 is connect with pushing block 10, described to push away
Block 10 and the top of the substrate 1 and the bottom end gap setting of the positioning seat 3；
Be provided with the first cylinder 11 on the substrate 1, first cylinder 11 by the first cylinder mounting base 12 with it is described
Substrate is fixed, and the First piston bar 13 on first cylinder 11 is connect with the pushing block 10；
3 rear end of positioning seat offers the second opening 15 with the compression groove 6 perforation, can at second opening 15
Sliding is provided with limited post 16, and the rear end of the limited post 16 is provided with limit plate 17, and the two sides of the positioning seat 3 pass through
Second cylinder mounting base 18 is provided with the second cylinder 19, the second piston bar 20 on each second cylinder 19 respectively with the limit
The both ends connection of position plate 17.
Be provided with triangle reinforcement block 21 at first opening 8, the triangle reinforcement block 21 simultaneously with the compression
Block 7 and the link block 9 connect.
Two the first guide rods 22 being parallel to each other, first gas are provided between the substrate 1 and the positioning seat 3
Cylinder 11 is located between two first guide rods 22, and the both ends of the pushing block 10 are slidably set in each described first respectively
On guide rod 22, the both ends of first guide rod 22 pass through locating piece 23 and connect simultaneously with the substrate 1 and the positioning seat 3
It connects.
The 3 back segment bottom of positioning seat opens up jagged 26, and the notch 26 runs through with second opening 15.
Third opening 27 is offered on the substrate 1, the third opening 27 is located at the underface of the notch 26.
Pressing plate 28 is provided with right above the compression groove 6, the two sides of the pressing plate 28 are provided with sliding panel 29, described fixed
Four second guide rods 30 are provided on the seat 3 of position, each sliding panel 29 is mobilizable respectively to be set in each second guiding
On bar 30；Each second guide rod, 30 upper end is connected with top plate 31, and each top plate 31 passes through two locating rods 32 and institute
The connection of positioning seat 3 is stated, each second guide rod 30 is located between two locating rods 32；
Screw thread is provided on wherein at least two second guide rods 30 and is threadedly coupled with the sliding panel 29, and there is screw thread
30 lower end of the second guide rod rotatably pass through the positioning seat 3 and the output axis connection with third motor 33, the third
Motor 33 is connect by third motor mount 35 with 3 bottom of positioning seat.
The upper end of the pressing plate 28 offers two limiting slots being parallel to each other 36, on the compression blocks 7 there are two settings
The gag lever post 37 being used cooperatively with the limiting slot 36.
The underface of the gag lever post 37 is provided with two reinforcing rods 38, and the other end of each reinforcing rod 38 passes through triangle
Shape connecting plate 39 is connect with the gag lever post 37.
The working principle of the utility model is as follows:
Wing to be compressed is placed in the compression groove 6 being provided on positioning seat 3；Start third motor 33, passes through third
Motor 33, which drives, has the threaded rotation of second guide rod 30, to make sliding panel 29 move down with dynamic pressure plate 28, until limit
Position slot 36 stops after being aligned with gag lever post 37；Start the first cylinder 11, pushing block 10 is pushed by the first cylinder 11, makes 10 band of pushing block
Dynamic compression blocks 7 are mobile to 16 direction of limited post, squeezed to treat compression wing with compression blocks 7 by limited post 16；It squeezes
Gag lever post 37 is slidably seated in limiting slot 36 while pressure；After the completion of extruding, starts the second cylinder 19, pass through the second gas
Cylinder 19 pushes limit plate 17, so that limited post 16 be made not to be located at the second opening 15, limited post 16 is also no longer to notch at this time
26 are blocked；Continuing the first cylinder 11 of starting drives compression blocks 7 mobile to 16 direction of limited post, will be squeezed by compression blocks 7
Later wing is fallen down by notch 26, then falls in the cart being placed under substrate 1 (figure by third opening 27
In be not shown).
The preferred embodiments of the present invention have been described in detail above.It should be appreciated that the ordinary skill people of this field
Member according to the present utility model can conceive without creative work makes many modifications and variations.Therefore, all this technology necks
Technical staff passes through logic analysis, reasoning or limited reality according to the design of the utility model on the basis of existing technology in domain
Available technical solution is tested, it all should be within the scope of protection determined by the claims.
Claims (8)
1. a kind of unmanned plane wing pressure texture to be recycled, it is characterized in that: including substrate (1), substrate (1) bottom is provided with
Support leg (2) is provided with positioning seat (3) on the substrate (1), and four angles of the bottom of the positioning seat (3) pass through four branch
It is connect at the top of dagger (5) and the substrate (1), positioning seat (3) upper end offers compression groove (6), and the compression groove (6) is passed through
The front end with the positioning seat (3) is worn, is slidably provided with compression blocks (7) in the compression groove (6)；
It offers the first opening (8) along the length direction of the compression groove (6), is slidably provided at first opening (8)
The upper end of link block (9), the link block (9) is connect with the compression blocks (7), the lower end of the link block (9) and pushing block
(10) it connects, the pushing block (10) and the top of the substrate (1) and the bottom end gap setting of the positioning seat (3)；
Be provided with the first cylinder (11) on the substrate (1), first cylinder (11) by the first cylinder mounting base (12) with
The substrate is fixed, and the First piston bar (13) on first cylinder (11) is connect with the pushing block (10)；
Positioning seat (3) rear end offers the second opening (15) with the compression groove (6) perforation, second opening (15)
Place is slidably provided with limited post (16), and the rear end of the limited post (16) is provided with limit plate (17), the positioning seat (3)
Two sides pass through the second cylinder mounting base (18) and be provided with the second cylinder (19), second on each second cylinder (19) is living
Stopper rod (20) is connect with the both ends of the limit plate (17) respectively.
2. unmanned plane wing pressure texture to be recycled as described in claim 1, it is characterized in that: being set at first opening (8)
It is equipped with triangle reinforcement block (21), the triangle reinforcement block (21) connects with the compression blocks (7) and the link block (9) simultaneously
It connects.
3. unmanned plane wing pressure texture to be recycled as described in claim 1, it is characterized in that: the substrate (1) with it is described fixed
It is provided with two the first guide rods (22) being parallel to each other between position seat (3), first cylinder (11) is located at two described the
Between one guide rod (22), the both ends of the pushing block (10) are slidably set in respectively on each first guide rod (22),
The both ends of first guide rod (22) pass through locating piece (23) while connecting with the substrate (1) and the positioning seat (3).
4. unmanned plane wing pressure texture to be recycled as described in claim 1, it is characterized in that: the positioning seat (3) back segment bottom
Portion opens up jagged (26), and the notch (26) is run through with second opening (15).
5. unmanned plane wing pressure texture to be recycled as claimed in claim 4, it is characterized in that: being offered on the substrate (1)
Third is open (27), and the third opening (27) is located at the underface of the notch (26).
6. unmanned plane wing pressure texture to be recycled as claimed in claim 1 to 5, it is characterized in that: the compression groove (6)
Surface is provided with pressing plate (28), and the two sides of the pressing plate (28) are provided with sliding panel (29), is arranged on the positioning seat (3)
There are four second guide rods (30), each sliding panel (29) is mobilizable respectively to be set in each second guide rod (30)
On；Each second guide rod (30) upper end is connected with top plate (31), and each top plate (31) passes through two locating rods (32)
It is connect with the positioning seat (3), each second guide rod (30) is located between two locating rods (32)；
Screw thread is provided on wherein at least two second guide rods (30) and is threadedly coupled with the sliding panel (29), and there is screw thread
The second guide rod (30) lower end rotatably pass through the positioning seat (3) and the output axis connection with third motor (33), institute
Third motor (33) are stated to connect by third motor mount (35) with the positioning seat (3) bottom.
7. unmanned plane wing pressure texture to be recycled as claimed in claim 6, it is characterized in that: the upper end of the pressing plate (28) is opened
Equipped with two limiting slots being parallel to each other (36), there are two make with the limiting slot (36) cooperation for setting on the compression blocks (7)
Gag lever post (37).
8. unmanned plane wing pressure texture to be recycled as claimed in claim 7, it is characterized in that: the gag lever post (37) just under
Side is provided with two reinforcing rods (38), and the other end of each reinforcing rod (38) passes through triangle connecting plate (39) and the limit
Bar (37) connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821863571.8U CN209441677U (en) | 2018-11-13 | 2018-11-13 | A kind of unmanned plane wing pressure texture to be recycled |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821863571.8U CN209441677U (en) | 2018-11-13 | 2018-11-13 | A kind of unmanned plane wing pressure texture to be recycled |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209441677U true CN209441677U (en) | 2019-09-27 |
Family
ID=68011069
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821863571.8U Expired - Fee Related CN209441677U (en) | 2018-11-13 | 2018-11-13 | A kind of unmanned plane wing pressure texture to be recycled |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209441677U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109436369A (en) * | 2018-11-13 | 2019-03-08 | 浙江云来集科技有限公司 | A kind of unmanned plane wing pressure texture to be recycled and its application method |
-
2018
- 2018-11-13 CN CN201821863571.8U patent/CN209441677U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109436369A (en) * | 2018-11-13 | 2019-03-08 | 浙江云来集科技有限公司 | A kind of unmanned plane wing pressure texture to be recycled and its application method |
| CN109436369B (en) * | 2018-11-13 | 2024-01-26 | 浙江云来集科技有限公司 | Unmanned aerial vehicle wing compression structure to be recycled and application method thereof |
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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: 20190927 Termination date: 20201113 |