CN220884848U - Unmanned aerial vehicle is patrolled and examined to electric power - Google Patents
Unmanned aerial vehicle is patrolled and examined to electric power Download PDFInfo
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- CN220884848U CN220884848U CN202322867873.XU CN202322867873U CN220884848U CN 220884848 U CN220884848 U CN 220884848U CN 202322867873 U CN202322867873 U CN 202322867873U CN 220884848 U CN220884848 U CN 220884848U
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- 238000007689 inspection Methods 0.000 claims abstract description 36
- 238000001931 thermography Methods 0.000 claims abstract description 28
- 230000003139 buffering effect Effects 0.000 claims description 5
- 238000004140 cleaning Methods 0.000 abstract description 6
- 239000012535 impurity Substances 0.000 abstract description 6
- 238000004804 winding Methods 0.000 abstract description 4
- 238000007664 blowing Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 4
- 206010020649 Hyperkeratosis Diseases 0.000 description 3
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
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Abstract
The utility model discloses an electric power inspection unmanned aerial vehicle, which comprises a machine body, a power mechanism and folding supporting legs, wherein a visible light camera and an infrared thermal imaging camera are arranged at the lower end of the machine body, the visible light camera and the infrared thermal imaging camera are connected with the machine body through an adjusting mechanism, an air pump assembly is arranged on the adjusting mechanism, an air ejector tube is arranged at one end of the air pump assembly, and two groups of air ejector nozzles are arranged on the air ejector tube; the folding support leg disclosed by the utility model is automatically folded after taking off, so that the unmanned aerial vehicle support leg is effectively prevented from winding a cable, the inspection stability is improved, the horizontal angle position and the axial angle position of the camera shooting mechanism can be adjusted by the adjusting mechanism, the flexibility of the camera shooting mechanism in inspection operation is improved, compressed gas is blown onto the lens of the camera shooting mechanism through the blowing mechanism, impurities adhered to the lens of the camera shooting mechanism are removed by means of the impact force of the gas, self-cleaning is realized, shutdown cleaning is not needed, the inspection progress is not influenced, and the inspection efficiency is improved.
Description
Technical Field
The utility model relates to the technical field of inspection unmanned aerial vehicles, in particular to an electric inspection unmanned aerial vehicle.
Background
The drone is an aircraft that is maneuvered using a radio remote control device and a self-contained programming device. The device has the characteristics of small volume and convenient operation. Unmanned aerial vehicles are widely applied in more and more industries, such as terrain exploration, high-altitude power inspection, outdoor high-altitude shooting and the like. When unmanned aerial vehicle is applied to electric power inspection, the electric power construction degree of difficulty has been reduced, has solved regional inspection problem, improves electric power inspection's efficiency and security through inspection unmanned aerial vehicle.
The current electric power inspection unmanned aerial vehicle's bottom landing leg is fixed structure, can not fold, and electric power inspection environment is comparatively complicated, and improper operation will lead to unmanned aerial vehicle landing leg winding cable, and the stability of flight in-process is to be improved, and unmanned aerial vehicle is equipped to patrol and examine and use camera mechanism equally for fixed structure, through unmanned aerial vehicle self position control to the regulation of shooting position, adjusts inconveniently, and it is lower to patrol and examine the flexibility, and unmanned aerial vehicle is at the in-process of patrolling and examining, and easy adhesion impurity on its camera only can carry out normal work of patrolling and examining after the clearance need shut down, influences the progress of patrolling and examining.
Disclosure of utility model
The utility model aims to provide an electric inspection unmanned aerial vehicle so as to solve the problems in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle is patrolled and examined to electric power, includes organism, power unit and folding landing leg, visible light camera and infrared thermal imaging camera are installed to the lower extreme of organism, be connected through adjustment mechanism between visible light camera and the infrared thermal imaging camera and the organism, install air pump assembly on the adjustment mechanism, the jet-propelled pipe is installed to air pump assembly's one end, be provided with two sets of air nozzles on the jet-propelled pipe.
The adjusting mechanism comprises a rotary driving base, a rotary disc is arranged at the lower end of the rotary driving base, a fixing frame is arranged at the lower end of the rotary disc, a first motor is arranged at the outer side of the fixing frame, a first driving shaft is arranged at one end of the first motor, a driving block is fixedly sleeved on the first driving shaft, and the driving block is fixedly connected with a visible light camera and an infrared thermal imaging camera.
The folding support legs are provided with two groups, and the two groups of folding support legs are respectively positioned at two sides of the lower end of the machine body.
The folding support leg comprises a mounting frame, a second motor is mounted on the outer side of the mounting frame, a second driving shaft is mounted at one end of the second motor, and a first support leg frame is fixedly sleeved on the second driving shaft.
The outer side of one end of the first support leg frame is provided with a third motor, one end of the third motor is provided with a third driving shaft, and a second support leg frame is fixedly sleeved on the third driving shaft.
Wherein, the bottom of second landing leg frame is provided with the buffering callus on the sole.
Wherein the power mechanism comprises a motor and a paddle.
Wherein, the top of organism is provided with the battery compartment.
Compared with the prior art, the utility model has the beneficial effects that:
The folding support legs are automatically folded after taking off, the folding support legs are folded at two sides of the lower end of the machine body, the support legs of the unmanned aerial vehicle are effectively prevented from winding cables, the stability of the unmanned aerial vehicle during flight inspection is improved, the folded support legs cannot shield a camera, and the visual field range of the camera is improved.
The adjusting mechanism is flexible and adjustable, the horizontal angle position and the axial angle position of the visible light camera and the infrared thermal imaging camera can be adjusted through the adjusting mechanism, the flexibility of the camera mechanism in inspection operation is improved, the camera mechanism can be flexibly adjusted through the adjusting mechanism under the condition that the flight angle of the unmanned aerial vehicle is not changed, the operation difficulty of the unmanned aerial vehicle is reduced, and the inspection flexibility is improved.
The air pump component, the air ejector pipe and the air nozzle jointly form the blowing mechanism, compressed air can be blown onto the lenses of the visible light camera and the infrared thermal imaging camera through the blowing mechanism, impurities adhered to the lenses of the visible light camera and the infrared thermal imaging camera are removed by means of the impact force of the air, self-cleaning in the flight inspection process is realized, shutdown cleaning is not needed, inspection progress is not influenced, and inspection efficiency is improved.
Drawings
FIG. 1 is a top plan perspective view of the present utility model;
FIG. 2 is a bottom perspective view of the present utility model;
FIG. 3 is a schematic view of the structure of the adjusting mechanism of the present utility model;
FIG. 4 is a schematic view of a folding leg of the present utility model;
fig. 5 is a folding schematic view of the folding leg of the present utility model.
In the figure: 1. a body; 2. a power mechanism; 3. folding the support legs; 4. a visible light camera; 5. an infrared thermal imaging camera; 6. an adjusting mechanism; 7. a rotation driving base; 8. a rotating disc; 9. a fixing frame; 10. a first motor; 11. a first drive shaft; 12. a driving block; 13. an air pump assembly; 14. a gas lance; 15. an air nozzle; 16. a mounting frame; 17. a second motor; 18. a second drive shaft; 19. a first leg rest; 20. a third motor; 21. a third drive shaft; 22. a second leg rest; 23. buffering foot pads; 24. a motor; 25. a paddle wing; 26. and a battery compartment.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, the present utility model provides a technical solution: the utility model provides an electric power inspection unmanned aerial vehicle, including organism 1, power unit 2 and folding landing leg 3, organism 1 includes laser range finder and gas image sensor, visible light camera 4 and infrared thermal imaging camera 5 are installed to the lower extreme of organism 1, be connected through adjustment mechanism 6 between visible light camera 4 and the infrared thermal imaging camera 5 and the organism 1, install air pump assembly 13 on the adjustment mechanism 6, air jet 14 is installed to air pump assembly 13's one end, be provided with two sets of air nozzles 15 on the air jet 14, visible light camera 4 and infrared thermal imaging camera 5 constitute camera mechanism jointly, through the detail and the thermal distribution on this camera mechanism capture equipment surface, detect potential problem, operating personnel carries out real-time control to unmanned aerial vehicle through remote control equipment, when unmanned aerial vehicle flies power plant equipment and facility, high resolution image is captured through camera mechanism, video and thermal image.
Wherein, folding landing leg 3 is automatic fold after taking off, as shown in fig. 5, folding landing leg 3 fold in the both sides of organism 1 lower extreme, effectively prevent unmanned aerial vehicle landing leg winding cable, improve the stability when the flight is patrolled and examined to the landing leg after folding can not cause the shelter from camera, improves camera's field of vision scope.
The adjusting mechanism 6 is flexible and adjustable, the horizontal angle position and the axial angle position of the visible light camera 4 and the infrared thermal imaging camera 5 can be adjusted through the adjusting mechanism 6, the flexibility of the camera shooting mechanism in inspection operation is improved, the camera shooting mechanism can be flexibly adjusted through the adjusting mechanism 6 under the condition that the flight angle of the unmanned aerial vehicle is not changed, the operation difficulty of the unmanned aerial vehicle is reduced, and the inspection flexibility is improved.
Wherein, air pump assembly 13, jet pipe 14 and air nozzle 15 constitute jetting mechanism jointly, can blow compressed gas to the camera lens of visible light camera 4 and infrared thermal imaging camera 5 through this jetting mechanism, rely on gaseous impact force, get rid of the impurity of adhesion on the camera lens of visible light camera 4 and infrared thermal imaging camera 5, realize the flight and patrol and examine the self-cleaning of in-process, need not to shut down the clearance, can not influence the progress of patrolling and examining, improved and patrolled and examined efficiency.
Wherein, adjustment mechanism 6 includes rotary drive base 7, rotary disk 8 is installed to rotary drive base 7's lower extreme, rotary motor is built-in to rotary drive base 7, fixed between rotary motor's the output shaft and rotary disk 8, mount 9 is installed to rotary disk 8's lower extreme, first motor 10 is installed in mount 9's the outside, first drive shaft 11 is installed to first motor 10's one end, fixed connection between first motor 10's output shaft and the first drive shaft 11, fixed cover is equipped with drive block 12 on the first drive shaft 11, fixed connection between drive block 12 and visible light camera 4 and the infrared thermal imaging camera 5.
Wherein, the rotating electrical machines inside the rotation driving base 7 drive the rotary disk 8 to rotate when working, drive the mount 9 to rotate through the rotary disk 8, drive the synchronous rotation of visible light camera 4 and infrared thermal imaging camera 5 through the mount 9, carry out nimble regulation to the horizontal angle position of visible light camera 4 and infrared thermal imaging camera 5.
The first motor 10 drives the first driving shaft 11 to rotate during operation, the driving block 12 is driven to rotate through the first driving shaft 11, the driving block 12 drives the visible light camera 4 and the infrared thermal imaging camera 5 to synchronously rotate, and the axial angle positions of the visible light camera 4 and the infrared thermal imaging camera 5 are flexibly adjusted.
Wherein, folding landing leg 3 is provided with two sets of, and two sets of folding landing legs 3 are located the both sides of organism 1 lower extreme respectively, and when folding landing leg 3 was in the state of expanding, support whole inspection unmanned aerial vehicle through two sets of folding landing legs 3.
The folding support leg 3 comprises a mounting frame 16, a second motor 17 is mounted on the outer side of the mounting frame 16, a second driving shaft 18 is mounted at one end of the second motor 17, an output shaft of the second motor 17 is fixedly connected with the second driving shaft 18, and a first support leg frame 19 is fixedly sleeved on the second driving shaft 18.
Wherein, the second motor 17 drives the second driving shaft 18 to rotate when working, and the first supporting leg frame 19 is driven to synchronously rotate through the second driving shaft 18.
Wherein, the outside of first landing leg frame 19 one end installs third motor 20, and third drive shaft 21 is installed to the one end of third motor 20, and fixed connection is between the output shaft of third motor 20 and the third drive shaft 21, and the fixed cover of third drive shaft 21 is equipped with second landing leg frame 22.
Wherein, the third motor 20 is operated to drive the third driving shaft 21 to rotate, and the second leg frame 22 is driven to synchronously rotate by the third driving shaft 21.
Wherein, through the first landing leg frame 19 of second motor 17 rotary drive, through the second landing leg frame 22 of third motor 20 rotary drive, realize folding and expansion of folding landing leg 3, when unmanned aerial vehicle flight patrols and examines, folding landing leg 3 is in folding state, and unmanned aerial vehicle descends, and folding landing leg 3 is in expansion state.
Wherein, the bottom of second landing leg frame 22 is provided with buffering callus on the sole 23, and buffering callus on the sole 23 plays the cushioning effect.
The power mechanism 2 comprises a motor 24 and a paddle 25, the motor 24 drives the paddle 25 to rotate at a high speed, and lift force is generated to fly by means of the lift force.
The top of the machine body 1 is provided with a battery compartment 26, and the battery compartment 26 is internally provided with a battery module, so that stable power support is provided for the whole unmanned aerial vehicle.
Working principle: when in use, the battery compartment 26 is internally provided with a battery module, provides stable electric power support for the whole unmanned aerial vehicle, an operator controls the unmanned aerial vehicle in real time through remote control equipment, the four sets of motors 24 of the power mechanism 2 drive the four sets of paddles 25 to rotate at high speed, lift force is generated, the unmanned aerial vehicle flies by relying on the lift force, after the unmanned aerial vehicle takes off, the folding support leg 3 is automatically folded under the drive of the second motor 17 and the third motor 20, so that the stability of the flight inspection is improved, the visible light camera 4 and the infrared thermal imaging camera 5 together form a camera mechanism, details and heat distribution of the surface of the equipment are captured through the camera mechanism, potential problems are detected, and when the unmanned aerial vehicle flies through power plant equipment and facilities, capturing high resolution images, videos and thermal images by a camera mechanism, collecting data, and when in inspection, the horizontal angle position and the axial angle position of the visible light camera 4 and the infrared thermal imaging camera 5 are adjusted by the adjusting mechanism 6, under the condition of not changing the flight angle of the unmanned aerial vehicle, the camera shooting mechanism is flexibly adjusted by the adjusting mechanism 6, when the impurities are adhered to the lenses of the visible light camera 4 and the infrared thermal imaging camera 5, the visible light camera 4 and the infrared thermal imaging camera 5 are driven to reset, the air pump component 13 works, two compressed air is sprayed out through the two groups of air nozzles 15, the air is sprayed onto the lenses of the camera mechanism, the impurities adhered to the lenses of the visible light camera 4 and the infrared thermal imaging camera 5 are removed by means of the impact force of the air, self-cleaning is achieved, when inspection is completed and landing is carried out, the folding supporting legs 3 are automatically unfolded under the driving of the second motor 17 and the third motor 20, and the whole inspection unmanned aerial vehicle is supported through the two groups of folding supporting legs 3.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides an unmanned aerial vehicle is patrolled and examined to electric power, includes organism (1), power unit (2) and folding landing leg (3), its characterized in that: the camera is characterized in that a visible light camera (4) and an infrared thermal imaging camera (5) are arranged at the lower end of the machine body (1), the visible light camera (4) and the infrared thermal imaging camera (5) are connected with the machine body (1) through an adjusting mechanism (6), an air pump component (13) is arranged on the adjusting mechanism (6), an air jet pipe (14) is arranged at one end of the air pump component (13), and two groups of air jet nozzles (15) are arranged on the air jet pipe (14).
2. The power inspection drone of claim 1, wherein: the adjusting mechanism (6) comprises a rotary driving base (7), a rotary disk (8) is installed at the lower end of the rotary driving base (7), a fixing frame (9) is installed at the lower end of the rotary disk (8), a first motor (10) is installed on the outer side of the fixing frame (9), a first driving shaft (11) is installed at one end of the first motor (10), a driving block (12) is fixedly sleeved on the first driving shaft (11), and the driving block (12) is fixedly connected with a visible light camera (4) and an infrared thermal imaging camera (5).
3. The power inspection drone of claim 1, wherein: the folding support legs (3) are provided with two groups, and the two groups of folding support legs (3) are respectively positioned at two sides of the lower end of the machine body (1).
4. The power inspection drone of claim 1, wherein: the folding support leg (3) comprises a mounting frame (16), a second motor (17) is mounted on the outer side of the mounting frame (16), a second driving shaft (18) is mounted at one end of the second motor (17), and a first support leg frame (19) is fixedly sleeved on the second driving shaft (18).
5. The power inspection drone of claim 4, wherein: a third motor (20) is arranged on the outer side of one end of the first support leg frame (19), a third driving shaft (21) is arranged at one end of the third motor (20), and a second support leg frame (22) is fixedly sleeved on the third driving shaft (21).
6. The power inspection drone of claim 5, wherein: the bottom end of the second leg frame (22) is provided with a buffering foot pad (23).
7. The power inspection drone of claim 1, wherein: the power mechanism (2) comprises a motor (24) and a paddle wing (25).
8. The power inspection drone of claim 1, wherein: the top of the machine body (1) is provided with a battery compartment (26).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322867873.XU CN220884848U (en) | 2023-10-25 | 2023-10-25 | Unmanned aerial vehicle is patrolled and examined to electric power |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322867873.XU CN220884848U (en) | 2023-10-25 | 2023-10-25 | Unmanned aerial vehicle is patrolled and examined to electric power |
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| CN220884848U true CN220884848U (en) | 2024-05-03 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118457965A (en) * | 2024-06-28 | 2024-08-09 | 陈志源 | Image acquisition system and method for electric power inspection unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118457965A (en) * | 2024-06-28 | 2024-08-09 | 陈志源 | Image acquisition system and method for electric power inspection unmanned aerial vehicle |
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