CN218123932U - Unmanned aerial vehicle high altitude automatic wiring pincers - Google Patents
Unmanned aerial vehicle high altitude automatic wiring pincers Download PDFInfo
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- CN218123932U CN218123932U CN202222039192.XU CN202222039192U CN218123932U CN 218123932 U CN218123932 U CN 218123932U CN 202222039192 U CN202222039192 U CN 202222039192U CN 218123932 U CN218123932 U CN 218123932U
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Abstract
The utility model provides an automatic wiring pincers in unmanned aerial vehicle high altitude relates to automatic wiring technical field, which comprises an outer shell, the top fixed mounting of shell has the apron, the spout has been seted up to the bottom of shell, the first guide post of inner wall fixedly connected with of shell, the first spring of one end fixedly connected with of first guide post, the first slider of one end fixedly connected with of first spring, the passive clamping jaw of bottom fixedly connected with of first slider, the first fixed block of top fixedly connected with of first slider, the inside of first fixed block is pegged graft and is had the worm, the surface meshing of worm is connected with the worm wheel, the internal transmission of worm wheel is connected with the motor. The utility model has the advantages that: remove through first spring when removing control and compare rope traction remove control receive external force to disturb less, the device position is comparatively fixed, is difficult for taking place to change, is difficult to make the device drop when cooperation unmanned aerial vehicle removes the centre gripping, and stability is better, and the security is higher.
Description
Technical Field
The utility model relates to an automatic wiring technical field, in particular to unmanned aerial vehicle high altitude automatic wiring pincers.
Background
The overhead wiring clamp is a special tool for temporary wiring when an electric power system tests or overhauls electrical equipment, is suitable for detecting and wiring the overhead equipment on the ground, and transfers the traditional overhead operation to the ground for carrying out, so that the field working condition is greatly improved, and the safety and the working efficiency of the operation are greatly improved.
The unmanned aerial vehicle high-altitude automatic wiring clamp is disclosed in Chinese patent CN216956104U, and the driving structure is arranged on the mounting seat and used for driving the second clamping jaw component to move forwards and backwards. The utility model discloses aim at solving current high altitude jointing clamp and adopt people hand-held device to carry out the operation of working a telephone switchboard, the low and difficult problem of operation of work efficiency, nevertheless, this unmanned aerial vehicle high altitude automatic jointing clamp, in the solution problem, has following shortcoming:
elastic element exerts a jacking force, pushes up second clamping jaw subassembly to first clamping jaw subassembly, when removing clamping state, needs to drive the slider behind the first stay cord of pulling and drives second clamping jaw subassembly and remove the centre gripping, drives the device easily during the pulling stay cord and takes place to rotate along the cable, makes the device position change, makes the device drop easily when cooperation unmanned aerial vehicle removes the centre gripping, and stability is lower, and the security is relatively poor.
SUMMERY OF THE UTILITY MODEL
The purpose of the present invention is to solve at least one of the technical drawbacks.
Therefore, an object of the utility model is to provide an unmanned aerial vehicle high altitude automatic wiring pincers to solve the problem mentioned in the background art, overcome the not enough that exists among the prior art.
In order to achieve the above object, an embodiment of the utility model provides an automatic wire connection pincers in unmanned aerial vehicle high altitude, which comprises an outer shell, the top fixed mounting of shell has the apron, the spout has been seted up to the bottom of shell, the first guide post of inner wall fixedly connected with of shell, the first spring of one end fixedly connected with of first guide post, the first slider of one end fixedly connected with of first spring, the passive clamping jaw of bottom fixedly connected with of first slider, the first fixed block of top fixedly connected with of first slider, peg graft and have the worm in the inside of first fixed block, the surface meshing of worm is connected with the worm wheel, the internal drive of worm wheel is connected with the motor, the initiative clamping jaw of bottom fixedly connected with of shell, the inside sliding connection of shell has the second slider, the top fixedly connected with L shape fixed block of second slider, the inside fixedly connected with second guide post of shell, the one end fixedly connected with second spring of second guide post, the one end fixedly connected with second slider of second spring, second slider and initiative clamping jaw fixed connection, the inside and the worm that L shape fixed block peg graft.
An embodiment of the utility model provides an unmanned aerial vehicle high altitude automatic wiring pincers, which comprises an outer shell, the top fixed mounting of shell has the apron, the spout has been seted up to the bottom of shell, the first guide post of inner wall fixedly connected with of shell, the first spring of one end fixedly connected with of first guide post, the first slider of one end fixedly connected with of first spring, the passive clamping jaw of bottom fixedly connected with of first slider, the first fixed block of top fixedly connected with of first slider, the inside of first fixed block is pegged graft and is had the worm, the surface toothing of worm is connected with the worm wheel, the internal transmission of worm wheel is connected with the motor, the bottom fixedly connected with initiative clamping jaw of shell, the inside sliding connection of shell has the second slider, the top fixedly connected with L shape fixed block of second slider, the inside and the worm of L shape fixed block peg graft, the inside of shell is rotated and is connected with the screw thread post, the surface threaded connection of screw thread post has the second slider, the bottom and the initiative clamping jaw fixed connection of second slider, one side fixedly connected with the spring box of shell, the inside of spring box is provided with the screw thread post.
According to any one of the above schemes, preferably, the clamping surfaces of the passive clamping jaw and the active clamping jaw are provided with conductive anti-slip blocks, and the conductive anti-slip blocks are convenient for connecting the clamping jaws and a wire, so that the rotation is avoided.
Preferably, according to any one of the above schemes, a cable connecting ring is arranged on one side of the passive clamping jaw, and the cable connecting ring is convenient for fixing a conducting wire.
By any of the above-mentioned scheme preferred, the top fixedly connected with unmanned aerial vehicle go-between of apron, the unmanned aerial vehicle go-between is convenient for unmanned aerial vehicle and pulls the device.
By any of the above-mentioned scheme preferred, the one end joint of screw thread post has the energy storage rocking handle, the energy storage rocking handle is convenient for fill the ability for the clockwork spring.
Compared with the prior art, the utility model has the advantages and beneficial effects do:
1. the positive and negative rotation control worm through the motor moves to one side, remove the restriction back initiative clamping jaw of initiative clamping jaw and accomplish the centre gripping in the spout, the positive and negative rotation control worm through the motor moves to the opposite side, make passive clamping jaw remove the centre gripping through the second spring, remove through first spring when removing control and compare rope traction remove control receive external force to disturb less, the device position is comparatively fixed, difficult emergence changes, be difficult to make the device drop when cooperation unmanned aerial vehicle removes the centre gripping, stability is better, the security is higher.
2. The worm is controlled to move to one side through positive and negative rotation of the motor, the driving clamping jaw drives the threaded column to rotate through the torsional force of the clockwork spring after limitation of the driving clamping jaw is relieved, the second sliding block is controlled to slide, the second sliding block drives the driving clamping jaw to move to the driven clamping jaw, the driven clamping jaw is controlled to move through the threaded column, after the worm is fixed, the worm is not easily influenced by external force compared with a spring, the second sliding block is not easily moved on the threaded column, and clamping is more stable.
Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.
Drawings
The above and/or additional aspects and advantages of the present invention will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:
fig. 1 is a schematic structural diagram according to a first embodiment of the present invention;
fig. 2 is a schematic structural diagram of a top view according to an embodiment of the present invention;
fig. 3 is a schematic cross-sectional structural view according to an embodiment of the present invention;
fig. 4 is a schematic structural diagram according to a second embodiment of the present invention;
fig. 5 is a schematic cross-sectional structural view according to a second embodiment of the present invention;
fig. 6 is a schematic structural diagram of the second embodiment of the present invention viewed from the left.
Wherein: 1. the shell, 2, the spout, 3, first guide post, 4, first spring, 5, first slider, 6, passive clamping jaw, 7, first fixed block, 8, the worm, 9, the worm wheel, 10, the motor, 11, the second guide post, 12, the second spring, 13, the second slider, 14, initiative clamping jaw, 15, L shape fixed block, 16, the screw thread post, 17, the apron, 18, electrically conductive non slipping spur, 19, the cable go-between, 20, the unmanned aerial vehicle go-between, 21, the spring box, 22, the clockwork spring, 23, the energy storage rocking handle.
Detailed Description
Reference will now be made in detail to the embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present invention, and should not be construed as limiting the present invention.
In the present invention, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those of ordinary skill in the art.
The first embodiment is as follows:
as shown in fig. 1-3, the unmanned aerial vehicle high altitude automatic wiring clamp of this embodiment includes a housing 1, a cover plate 17 is fixedly mounted at the top of the housing 1, a sliding groove 2 is formed in the bottom of the housing 1, a first guide post 3 is fixedly connected to the inner wall of the housing 1, a first spring 4 is fixedly connected to one end of the first guide post 3, a first slider 5 is fixedly connected to one end of the first spring 4, a driven clamping jaw 6 is fixedly connected to the bottom of the first slider 5, a first fixing block 7 is fixedly connected to the top of the first slider 5, a worm 8 is inserted into the first fixing block 7, a worm wheel 9 is connected to the surface of the worm 8 in a meshed manner, a motor 10 is connected to the internal transmission of the worm wheel 9, a driving clamping jaw 14 is fixedly connected to the bottom of the housing 1, a second slider 13 is slidably connected to the inside of the housing 1, an L-shaped fixing block 15 is fixedly connected to the top of the second slider 13, the L-shaped fixing block 15 is inserted into the worm 8, when control is released, the control, the rope traction is less interfered by external force, and the device is fixed in position and is not easy to change.
The inside fixedly connected with second guide post 11 of shell 1, the one end fixedly connected with second spring 12 of second guide post 11, the one end fixedly connected with second slider 13 of second spring 12, second slider 13 and initiative clamping jaw 14 fixed connection hold initiative clamping jaw 14 through the elasticity top of spring 12, can accomplish the centre gripping of device fast.
The clamping surfaces of the passive clamping jaw 6 and the active clamping jaw 14 are provided with conductive anti-skidding blocks 18.
One side of the passive clamping jaw 6 is provided with a cable connecting ring 19, and the cable connecting ring 19 is connected with the passive clamping jaw 6 in a welding mode.
The top fixedly connected with unmanned aerial vehicle go-between 20 of apron 17, unmanned aerial vehicle go-between 20 is convenient for connect unmanned aerial vehicle.
The unmanned aerial vehicle high altitude automatic wiring pincers of this embodiment, theory of operation as follows:
the worm 8 is controlled to move to one side through positive and negative rotation of the motor 10, the driving clamping jaw 14 slides on the sliding groove 2 to complete clamping after the limitation of the driving clamping jaw 14 is released, and the worm 8 is controlled to move to the other side through positive and negative rotation of the motor 10, so that the driven clamping jaw 6 is released from clamping through the second spring 12.
The second embodiment:
as shown in fig. 4-6, the automatic high-altitude wiring clamp for unmanned aerial vehicles of this embodiment differs from embodiment one in that the inside of the housing 1 is rotatably connected with the threaded column 16, the driven clamping jaw 6 is controlled to move through the threaded column 16, after the fixing, the spring is less susceptible to external force, the second slider 13 is less susceptible to moving on the threaded column 16, the clamping is more stable, the surface thread of the threaded column 16 is connected with the second slider 13, the bottom of the second slider 13 is fixedly connected with the driving clamping jaw 14, one side of the housing 1 is fixedly connected with the spring barrel 21, the spring 22 is arranged inside the spring barrel 21, and the inside of the spring barrel 21 is in transmission connection with the threaded column 16.
The one end joint of screw post 16 has energy storage rocking handle 23, and energy storage rocking handle 23 is detachable construction, alleviates device weight, can save unmanned aerial vehicle's electric quantity.
The unmanned aerial vehicle high altitude automatic wiring pincers of this embodiment, theory of operation as follows:
the worm 8 is controlled to move to one side through positive and negative rotation of the motor 10, after the limitation of the driving clamping jaw 14 is released, the driving clamping jaw 14 drives the threaded column 16 to rotate through the torsional force of the spring 23, the second sliding block 13 is controlled to slide, and the second sliding block 13 drives the driving clamping jaw 14 to move towards the driven clamping jaw 6
Compared with the prior art, the utility model discloses for prior art have following beneficial effect:
1. positive and negative rotation control worm 8 through motor 10 moves to one side, remove the restriction back initiative clamping jaw 14 of initiative clamping jaw 14 and slide at spout 2 and accomplish the centre gripping, 8 move to the opposite side through motor 10 positive and negative rotation control worm, make passive clamping jaw 6 remove the centre gripping through second spring 12, it is less to receive external force to disturb to remove to compare rope traction removal control through first spring 4 during removal control, the device position is comparatively fixed, difficult emergence changes, it drops to be difficult to make the device when cooperation unmanned aerial vehicle removes the centre gripping, stability is better, and the security is higher.
2. The worm 8 is controlled to move to one side through positive and negative rotation of the motor 10, the driving clamping jaw 14 drives the threaded column 16 to rotate through the torsional force of the clockwork spring 23 after the limitation of the driving clamping jaw 14 is removed, the second sliding block 13 is controlled to slide, the second sliding block 13 drives the driving clamping jaw 14 to move towards the driven clamping jaw 6, the driven clamping jaw 6 is controlled to move through the threaded column 16, the spring is not easily influenced by external force after the fixing process, the second sliding block 13 is not easily moved on the threaded column 16, and the clamping is more stable
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
It will be understood by those skilled in the art that the invention, including any combination of the elements of the above description and the detailed description and illustrated in the accompanying drawings, is not limited to the details and should not be construed as limited to the embodiments set forth herein for the sake of brevity. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Although embodiments of the present invention have been shown and described, it is to be understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that changes, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art without departing from the principles and spirit of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (7)
1. The utility model provides an automatic wire connection pincers in unmanned aerial vehicle high altitude, a serial communication port, including shell (1), the top fixed mounting of shell (1) has apron (17), spout (2) have been seted up to the bottom of shell (1), the first guide post (3) of inner wall fixedly connected with of shell (1), the first spring (4) of one end fixedly connected with of first guide post (3), the first slider (5) of one end fixedly connected with of first spring (4), the bottom fixedly connected with of first slider (5) is passive clamping jaw (6), the first fixed block (7) of top fixedly connected with of first slider (5), the inside of first fixed block (7) is pegged graft and is had worm (8), the surface meshing of worm (8) is connected with worm wheel (9), the internal gearing of worm wheel (9) is connected with motor (10), the bottom fixedly connected with initiative clamping jaw (14) of shell (1), the inside sliding connection of shell (1) has second slider (13), the top fixedly connected with L shape fixed block (15) of second slider (13), the inside L shape fixed block (15) and worm (8) are pegged graft.
2. The unmanned aerial vehicle high altitude automatic wire connection clamp of claim 1, characterized in that, a second guide post (11) is fixedly connected to the inside of the housing (1), a second spring (12) is fixedly connected to one end of the second guide post (11), a second slider (13) is fixedly connected to one end of the second spring (12), and the second slider (13) is fixedly connected to the active clamping jaw (14).
3. The unmanned aerial vehicle high altitude automatic wire connection clamp of claim 1, characterized in that, the inside of shell (1) is connected with screw thread post (16) in a rotating manner, the surface screw thread of screw thread post (16) is connected with second slider (13), the bottom of second slider (13) and initiative clamping jaw (14) fixed connection, one side of shell (1) is fixedly connected with barrel (21), the inside of barrel (21) is provided with clockwork spring (22), the inside of barrel (21) and screw thread post (16) transmission connection.
4. The unmanned aerial vehicle high altitude automatic wiring clamp as claimed in any one of claims 1-3, characterized in that the clamping surfaces of the passive clamping jaw (6) and the active clamping jaw (14) are provided with conductive anti-skidding blocks (18).
5. The unmanned aerial vehicle high altitude automatic wiring clamp according to any one of claims 1-3, characterized in that one side of the passive clamping jaw (6) is provided with a cable connecting ring (19).
6. The unmanned aerial vehicle high altitude automatic wiring clamp of any one of claims 1-3, characterized in that the top of the cover plate (17) is fixedly connected with an unmanned aerial vehicle connecting ring (20).
7. The automatic overhead wire connecting clamp for unmanned aerial vehicles according to claim 3, wherein an energy storage rocking handle (23) is clamped at one end of the threaded column (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222039192.XU CN218123932U (en) | 2022-08-04 | 2022-08-04 | Unmanned aerial vehicle high altitude automatic wiring pincers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222039192.XU CN218123932U (en) | 2022-08-04 | 2022-08-04 | Unmanned aerial vehicle high altitude automatic wiring pincers |
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| Publication Number | Publication Date |
|---|---|
| CN218123932U true CN218123932U (en) | 2022-12-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222039192.XU Active CN218123932U (en) | 2022-08-04 | 2022-08-04 | Unmanned aerial vehicle high altitude automatic wiring pincers |
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| Country | Link |
|---|---|
| CN (1) | CN218123932U (en) |
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- 2022-08-04 CN CN202222039192.XU patent/CN218123932U/en active Active
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|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20231115 Address after: 010000 3001, Unit 3, Building 19, Lijing, Yongtai City, Saihan District, Hohhot City, Inner Mongolia Autonomous Region Patentee after: Inner Mongolia Guangtong Big Data Co.,Ltd. Address before: 528000 Room 701, No. 109, Jinyu Street, Baoan Neighborhood Committee, Zumiao Street, Chancheng District, Foshan, Guangdong Patentee before: Sheng Weixia |
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| TR01 | Transfer of patent right |