CN218887770U

CN218887770U - Unmanned aerial vehicle high altitude automatic wiring clamp

Info

Publication number: CN218887770U
Application number: CN202223521163.3U
Authority: CN
Inventors: 白晋飞; 段文博
Original assignee: Nanjing Ceewa Intelligent Technology Co ltd
Current assignee: Nanjing Ceewa Intelligent Technology Co ltd
Priority date: 2022-12-28
Filing date: 2022-12-28
Publication date: 2023-04-18
Anticipated expiration: 2032-12-28

Abstract

The utility model discloses an automatic wiring pincers in unmanned aerial vehicle high altitude of electric power wiring detection instrument technical field, including unmanned aerial vehicle, the install bin is installed to unmanned aerial vehicle's bottom, the lower surface central point of install bin puts and is provided with the bearing, motor A is installed to the inside top central point of install bin puts, and its is rational in infrastructure, the utility model discloses a be equipped with wiring mechanism, with wiring structure installs in the bearing on the install bin to with pivot on the motor A and the carousel fixed connection on the wiring mechanism, make motor A can drive wiring mechanism and carry out all-round rotation processing, have adjustable effect through utilizing wiring mechanism, can adjust according to high altitude circuit thickness, and carry out the centre gripping wiring, collocation motor A drives down, and the convenience is worked a telephone switchboard to the high altitude circuit, and its process is automatic operation simultaneously, and effectual realization is carried out automatic wiring processing to unmanned aerial vehicle to high altitude phenomenon, has improved wiring efficiency and effect.

Description

Unmanned aerial vehicle high altitude automatic wiring clamp

Technical Field

The utility model relates to an electric power wiring detects instrument technical field, specifically is automatic wiring pincers in unmanned aerial vehicle high altitude.

Background

The high-altitude 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 high-altitude equipment on the ground, and transfers the traditional high-altitude operation to the ground for wiring, so that the field working condition is greatly improved, and the safety and the working efficiency of the operation are greatly improved.

The existing unmanned aerial vehicle high-altitude automatic wiring clamp has the following defects: when high altitude line need carry out the wiring operation, because high altitude line height is higher, then need adopt unmanned aerial vehicle to carry out wiring processing, and to the installation wiring instrument on the unmanned aerial vehicle, receive high altitude line position influence very easily, and then lead to the wiring instrument to be difficult to take place with the condition that high altitude line meets, when the unable effective position adjustment of wiring instrument on the unmanned aerial vehicle was handled simultaneously, and then wiring efficiency discounts greatly, has reduced high altitude line's wiring efficiency.

Therefore, the development of unmanned aerial vehicle high-altitude automatic wiring clamp is necessary.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an automatic wiring pincers in unmanned aerial vehicle high altitude, through being equipped with wiring mechanism, to wiring the bearing of structural mounting on the install bin, and with pivot on the motor A and the carousel fixed connection on the wiring mechanism, make motor A can drive wiring mechanism and carry out all-round rotation processing, have adjustable effect through utilizing wiring mechanism, can adjust according to high altitude circuit thickness, and the centre gripping wiring, collocation motor A drives down, the convenience is worked a telephone switchboard to high altitude circuit, its process is automatic operation simultaneously, effectual realization is carried out automatic wiring processing to unmanned aerial vehicle to high altitude phenomenon, wiring efficiency and effect have been improved, with the problem of providing the unable effective position adjustment of unmanned aerial vehicle at high altitude wiring in-process and influence efficiency in solving above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle high-altitude automatic jointing clamp comprises an unmanned aerial vehicle, wherein an installation box is installed at the bottom of the unmanned aerial vehicle, a bearing is arranged at the central position of the lower surface of the installation box, a motor A is installed at the central position of the top end in the installation box, and a jointing mechanism is installed at the bottom of the installation box;

the wiring mechanism comprises a driving part and a wiring part, the driving part is connected with the bearing, and the wiring part is connected with the driving part.

Preferably, the pillar is all installed to the front end and the rear end of unmanned aerial vehicle bottom both sides, the bottom of pillar is provided with the rubber seat.

Preferably, the mounting seats are installed on the outer walls of the two sides of the motor A, the top of each mounting seat is fixedly connected with the top end of the inside of the mounting box through a fastening bolt, and an output shaft on the motor A is fixedly connected with one end of the rotating shaft through a coupler.

Preferably, the driving part comprises a rotary table, the outer wall of the rotary table is fixedly connected with the inner wall of the bearing, L-shaped supports are mounted on two sides of the bottom of the rotary table, and supporting rods are arranged above the two opposite sides of the L-shaped supports.

Preferably, the lower part is rotated between the relative one side of two sets of L type supports and is connected with about the threaded rod, and is a set of install motor B on the outer wall of one side of L type support, the last output shaft of motor B passes through shaft coupling and controls the one end fixed connection of threaded rod.

Preferably, the wiring component comprises a moving block, a threaded hole is formed in the center of the surface of the moving block, connecting rods are arranged on two sides of the top of the moving block, a limiting block is arranged at the top end of each connecting rod, and a through hole is formed in the center of the surface of each limiting block.

Preferably, the bottom of the moving block is provided with a wiring clamp, and the outer wall of one side of the wiring clamp is provided with a rubber pad.

Compared with the prior art, the beneficial effects of the utility model are that:

through being equipped with wiring mechanism, to be worked a telephone switchboard in the bearing of structrual installation on the install bin, and with the carousel fixed connection on the pivot on the motor A and the wiring mechanism, make motor A can drive wiring mechanism and carry out all-round rotation processing, have adjustable effect through utilizing wiring mechanism, can adjust according to high altitude circuit thickness, and carry out the centre gripping wiring, collocation motor A drives down, the convenience is worked a telephone switchboard to high altitude circuit, its process is automation mechanized operation simultaneously, the effectual unmanned aerial vehicle that has realized carries out automatic wiring to high altitude phenomenon and handles, wiring efficiency and effect have been improved.

Drawings

FIG. 1 is a front sectional view of the present invention;

fig. 2 is a front view provided by the present invention;

fig. 3 is an enlarged view of the structure at a in fig. 1 provided by the present invention;

FIG. 4 is a front sectional view of the wiring mechanism provided by the present invention;

fig. 5 is a perspective view of a part of the structure of the wiring mechanism provided by the present invention.

In the figure: 1. an unmanned aerial vehicle; 101. a pillar; 102. a rubber seat; 2. installing a box; 201. a bearing; 3. a motor A; 301. a mounting base; 302. a rotating shaft; 4. a wiring mechanism; 401. a turntable; 402. an L-shaped bracket; 403. a support bar; 404. a left threaded rod and a right threaded rod; 405. a motor B; 406. a moving block; 407. a threaded hole; 408. a connecting rod; 409. a limiting block; 410. a through hole; 411. a jointing clamp; 412. and (7) a rubber pad.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

The utility model provides a following technical scheme: an unmanned aerial vehicle high-altitude automatic wiring clamp can effectively carry out automatic wiring operation on an unmanned aerial vehicle in a high-altitude line in the using process, a motor A3 and a wiring mechanism 4 are additionally arranged, please refer to fig. 1-5, the unmanned aerial vehicle high-altitude automatic wiring clamp comprises an unmanned aerial vehicle 1, pillars 101 are respectively arranged at the front end and the rear end of two sides of the bottom of the unmanned aerial vehicle 1, a rubber seat 102 is arranged at the bottom end of each pillar 101, four groups of pillars 101 are uniformly distributed at the bottom of the unmanned aerial vehicle 1, a rubber seat 102 is arranged at the bottom end of each pillar 101, the rubber seat 102 has the effects of increasing friction and reducing abrasion, the unmanned aerial vehicle 1 is supported by the pillars 101 after descending, in the supporting process, the rubber seat 102 is used for anti-skidding and abrasion reduction treatment so as to avoid the occurrence of serious abrasion and damage of the pillars 101, a mounting box 2 is arranged at the bottom of the unmanned aerial vehicle 1, a bearing 201 is arranged at the central position of the lower surface of the mounting box 2, a motor A3 is arranged at the central position of the inner top end of the mounting box 2, mounting boxes 301 are respectively arranged at two outer walls of two sides of the motor A3, the mounting boxes are fixedly connected with a rotating shaft 302 through fastening bolts, and a rotating shaft 302 is arranged at the bottom of the mounting box 302, and a rotating shaft 302 which can drive the motor A2 or a reverse rotation mechanism which can drive the motor A4;

the wiring mechanism 4 comprises a driving part and a wiring part, the driving part is connected with the bearing 201, the wiring part is connected with the driving part, the driving part comprises a turntable 401, the outer wall of the turntable 401 is fixedly connected with the inner wall of the bearing 201, the turntable 401 is fixed in the bearing 201 on the installation box 2, the bearing 201 is fixedly arranged on the turntable 401 without influencing the rotation of the turntable 401, the bottom end of the rotating shaft 302 is fixedly connected with the turntable 401, the rotating shaft 302 rotates forwards or backwards, the turntable 401 can be driven to rotate synchronously, the two sides of the bottom of the turntable 401 are both provided with L-shaped supports 402, a support rod 403 is arranged above the opposite sides of the two L-shaped supports 402, a left threaded rod 404 and a right threaded rod 404 are rotatably arranged below the opposite sides of the two L-shaped supports 402, the left threaded rod 404 and the right threaded rod 404 are rotatably arranged between the two L-shaped supports 402, and the L-shaped supports 402 are fixedly arranged on the left side and the right side 404, the rotation of the left threaded rod and the right threaded rod 404 is not influenced, a motor B405 is installed on the outer wall of one side of one group of L-shaped supports 402, an output shaft on the motor B405 is fixedly connected with one end of the left threaded rod and the right threaded rod 404 through a coupler, the motor B405 can drive the left threaded rod 404 and the right threaded rod 404 to rotate forwards or backwards, the wiring component comprises moving blocks 406, threaded holes 407 are formed in the surface center positions of the moving blocks 406, connecting rods 408 are arranged on two sides of the top of the moving blocks 406, a limiting block 409 is arranged at the top end of each connecting rod 408, through holes 410 are formed in the surface center positions of the limiting blocks 409, the two groups of moving blocks 406 are arranged on two sides of the outer wall of the left threaded rod 404 and the right threaded rod 404 in a threaded connection mode through the threaded holes 407, the limiting blocks 409 on the top of the moving blocks 406 are arranged on the outer wall of the supporting rod 403 in a sliding mode through the through holes 410, the left threaded rod 404 and the right threaded rod 404 can rotate forwards or backwards, and the two groups of moving blocks 406 can be driven to move outwards or inwards, wiring pincers 411 are installed to the bottom of movable block 406, be provided with rubber pad 412 on one side outer wall of wiring pincers 411, make movable block 406 inwards or outwards move, can drive wiring pincers 411 and remove the processing in step, when rising to appointed place through unmanned aerial vehicle 1, position between control motor A3 adjustment wiring pincers 411 and the high altitude circuit, motor B405 controls again, drive wiring pincers 411 carries out the wiring processing to the high altitude circuit, the wiring in-process also can arrange motor A3 drive wiring pincers 411 and rotate, realize wiring pincers 411 wiring operation, its process is automatic operation simultaneously, the effectual realization is carried out automatic wiring processing to unmanned aerial vehicle to high altitude phenomenon.

The working principle is as follows: when the utility model is used, four groups of pillars 101 are uniformly distributed at the bottom of the unmanned aerial vehicle 1, the bottom ends of the pillars 101 are provided with the rubber seats 102, the rubber seats 102 have the effect of increasing friction and reducing abrasion, so that the unmanned aerial vehicle 1 is supported by the pillars 101 after descending, in the supporting process, the rubber seats 102 are used for anti-skidding and abrasion reduction treatment so as to avoid the occurrence of serious abrasion and damage of the pillars 101, the motor A3 is arranged in the installation box 2 at the bottom of the unmanned aerial vehicle 1 by the installation seat 301 matched with fastening bolts, the output shaft on the motor A3 is provided with the rotating shaft 302 by a shaft coupling, so that the motor A3 can drive the rotating shaft 302 to rotate forwards or reversely, the rotating disc 401 is fixedly arranged by fixing the rotating disc 401 on the wiring mechanism 4 in the bearing 201 on the installation box 2, the bearing 201 is fixedly arranged on the rotating disc 401, the rotation of the rotating disc 401 is not influenced, the bottom ends of the rotating shaft 302 are fixedly connected with the rotating disc 401, the rotating shaft 302 is rotated forward or backward to drive the rotating disc 401 to synchronously rotate, two sets of L-shaped brackets 402 are arranged at two sides of the bottom of the rotating disc 401, the left threaded rod 404 and the right threaded rod 404 are arranged between the two sets of L-shaped brackets 402 in a rotating mode, the L-shaped brackets 402 are fixedly arranged on the left threaded rod 404 and the right threaded rod 404 without influencing the rotation of the left threaded rod 404, the motor B405 is arranged on the outer wall at one side of the set of L-shaped brackets 402, the output shaft on the motor B405 is fixedly connected with one end of the left threaded rod 404 and the right threaded rod 404 through a coupler, the motor B405 can drive the left threaded rod 404 and the right threaded rod 404 to rotate forward or backward, two sets of moving blocks 406 are arranged at two sides of the outer wall of the left threaded rod 404 through threaded holes 407 in a threaded connection mode, and a limiting block 409 on the top of the moving blocks 406 is arranged on the outer wall of the supporting rod 403 in a sliding mode through holes 410 to drive the left threaded rod 404 to rotate forward or the backward, the two groups of moving blocks 406 can be driven to move outwards or inwards, the wiring clamp 411 is arranged at the bottom of the moving blocks 406, a rubber pad 412 is arranged on the outer wall of one side of the wiring clamp 411, the moving blocks 406 can move inwards or outwards, the wiring clamp 411 can be driven to synchronously move, when the unmanned aerial vehicle 1 ascends to a specified place, the motor A3 is controlled to adjust the position between the wiring clamp 411 and a high-altitude line, the motor B405 is controlled again, the wiring clamp 411 is driven to perform wiring processing on the high-altitude line, the wiring clamp 411 can also be driven to rotate by the motor A3 in a wiring process, wiring operation of the wiring clamp 411 is achieved, meanwhile, the process is automatic operation, automatic wiring processing of the unmanned aerial vehicle on the high-altitude phenomenon is effectively achieved, and wiring efficiency and effect are improved.

While the invention has been described above with reference to an embodiment, various modifications may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In particular, the various features of the disclosed embodiments can be used in any combination that is not specifically enumerated in this specification for the sake of brevity and resource savings, provided that no structural conflict exists. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.

Claims

1. Unmanned aerial vehicle high altitude automatic wiring pincers, including unmanned aerial vehicle (1), install bin (2) in the bottom of unmanned aerial vehicle (1), the lower surface central point of install bin (2) puts and is provided with bearing (201), the inside top central point of install bin (2) puts and installs motor A (3), its characterized in that: the bottom of the installation box (2) is provided with a wiring mechanism (4);

the wiring mechanism (4) comprises a driving part and a wiring part, the driving part is connected with the bearing (201), and the wiring part is connected with the driving part.

2. The unmanned aerial vehicle high altitude automatic wire holder of claim 1, characterized in that: pillar (101) are all installed to the front end and the rear end of unmanned aerial vehicle (1) bottom both sides, the bottom of pillar (101) is provided with rubber seat (102).

3. The unmanned aerial vehicle high altitude automatic wire connection clamp of claim 1, characterized in that: mount pad (301) are all installed to the both sides outer wall of motor A (3), through fastening bolt fixed connection between the top of mount pad (301) and the inside top of install bin (2), the one end fixed connection of shaft coupling and pivot (302) is passed through to the output shaft on motor A (3).

4. The unmanned aerial vehicle high altitude automatic wire holder of claim 1, characterized in that: the drive part comprises a rotary table (401), the outer wall of the rotary table (401) is fixedly connected with the inner wall of the bearing (201), L-shaped supports (402) are mounted on two sides of the bottom of the rotary table (401), and two sets of support rods (403) are arranged above the two opposite sides of the L-shaped supports (402).

5. The unmanned aerial vehicle high altitude automatic wire holder of claim 4, characterized in that: two sets of the below is rotated between the relative one side of L type support (402) and is connected with about threaded rod (404), and is a set of install motor B (405) on the outer wall of one side of L type support (402), the output shaft on motor B (405) passes through shaft coupling and controls the one end fixed connection of threaded rod (404).

6. The unmanned aerial vehicle high altitude automatic wire connection clamp of claim 1, characterized in that: the wiring component comprises a moving block (406), a threaded hole (407) is formed in the center of the surface of the moving block (406), connecting rods (408) are arranged on two sides of the top of the moving block (406), a limiting block (409) is arranged at the top end of each connecting rod (408), and a through hole (410) is formed in the center of the surface of each limiting block (409).

7. The unmanned aerial vehicle high altitude automatic wire holder of claim 6, characterized in that: the bottom of the moving block (406) is provided with a jointing clamp (411), and the outer wall of one side of the jointing clamp (411) is provided with a rubber pad (412).