CN220349968U - Unmanned aerial vehicle recognition device - Google Patents
Unmanned aerial vehicle recognition device Download PDFInfo
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- CN220349968U CN220349968U CN202321588896.0U CN202321588896U CN220349968U CN 220349968 U CN220349968 U CN 220349968U CN 202321588896 U CN202321588896 U CN 202321588896U CN 220349968 U CN220349968 U CN 220349968U
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- 239000000428 dust Substances 0.000 claims abstract description 18
- 238000007789 sealing Methods 0.000 claims abstract description 14
- 238000007664 blowing Methods 0.000 claims abstract description 10
- 230000035939 shock Effects 0.000 claims description 10
- 238000010521 absorption reaction Methods 0.000 claims description 5
- 230000003139 buffering effect Effects 0.000 abstract description 3
- 238000004140 cleaning Methods 0.000 abstract description 3
- 238000007689 inspection Methods 0.000 description 10
- 238000013016 damping Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008094 contradictory effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000012423 maintenance 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
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Abstract
The utility model relates to the technical field of unmanned aerial vehicle equipment, and particularly discloses an unmanned aerial vehicle identification device, which comprises: unmanned aerial vehicle, shock-absorbing structure, backup pad, lug, slide bar, spacing frame, buffering gasbag, dust removal structure, sealed lantern ring, gas piping, blow the gaseous ring, venthole, regulation structure, mounting panel, bottom plate and camera; according to the utility model, when the unmanned aerial vehicle body drops, the bottom of the sliding rod is positioned below the convex blocks, the sliding rod can firstly contact the ground, so that the sliding rod can slide towards the top and extrude the buffer air bag, the unmanned aerial vehicle body is convenient to buffer and shock-absorb, the landing impact is reduced, the convex blocks at the bottom of the supporting plate facilitate the supporting plate to stably support on uneven ground, the stability is increased, the buffer air bag is extruded to extrude gas from the sealing lantern ring and enter the blowing ring through the gas pipeline, the gas is discharged from the gas outlet, and the discharged gas can clean dust on the surface of the camera, so that the dust adhesion is avoided, the camera is convenient to use, the cleaning is automatic, and the use is convenient.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle equipment, and particularly relates to an unmanned aerial vehicle identification device.
Background
The power inspection is to inspect the outdoor equipment in the power station, and the running state information of the power equipment is acquired, so that whether the power equipment has abnormal phenomena such as thermal defects and foreign matter hanging or not is detected, the safety of power production is ensured, the conventional inspection mode is manual inspection, and the manual inspection is low in efficiency and long in time consumption. Along with the technology constantly develops artifical inspection gradually by the elimination, unmanned aerial vehicle inspection has become mainstream gradually, and most use the camera to gather the image when unmanned aerial vehicle inspection, need descend after unmanned aerial vehicle inspection, because the position of power station construction is most comparatively remote areas, the environment in these areas is comparatively complicated, leads to the camera to receive ground extrusion easily when unmanned aerial vehicle descends to make the camera damage.
In the chinese patent with publication number CN212951171U, an unmanned aerial vehicle image acquisition and recognition device for electric power inspection is mentioned, which comprises a machine body, a fixed block is fixedly connected to the front side of the machine body, and a movable plate is movably connected to the inside of the fixed block. According to the image acquisition and recognition device of the electric power inspection unmanned aerial vehicle, the camera moves upwards when the machine body descends and is subjected to pressure through the pressure groove, the movable plate and the connecting column are driven to move upwards when the camera moves upwards, interaction force exists between the rotary plate and the fixed clamping groove when the movable plate moves upwards, the rotary plate rotates under the action of the interaction force, the rotary plate rotates and is separated from the fixed clamping groove, the movable plate drives the rotary plate to move upwards, the camera can move upwards when the camera is extruded through a series of mechanical structures, damage to the camera is avoided, the phenomenon that the camera moves when the camera is slightly extruded is avoided through the design of the rotary plate and the torsion spring, although the scheme has the advantages that the mechanical structure is complex, the manufacturing cost is high, the maintenance is troublesome, meanwhile, the unmanned aerial vehicle is easy to influence in flight when in actual use, the scheme does not have the effect of cleaning the surface of the camera, and certain limitation exists when the unmanned aerial vehicle is used;
in this regard, the inventor proposes an unmanned aerial vehicle recognition device for solving the above-mentioned problems.
Disclosure of Invention
The utility model aims to provide an unmanned aerial vehicle identification device for solving the problems in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
an unmanned aerial vehicle identification device, comprising:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a bottom plate is fixedly arranged at the bottom of the unmanned aerial vehicle body, and a camera is arranged in the middle of the bottom plate;
the damping structure is arranged at the bottom of the unmanned aerial vehicle body and is used for damping the unmanned aerial vehicle body;
the dust removing structure is positioned on the side face of the camera and connected with the damping structure, and is used for removing dust from the camera;
and the adjusting structure is arranged on the bottom plate and is used for adjusting the angle of the camera.
Preferably, the shock-absorbing structure comprises a supporting plate, the supporting plate is fixedly arranged at the bottom of the unmanned aerial vehicle body, two sliding rods are connected to the inner wall of the bottom plate in a sliding mode, the bottoms of the sliding rods penetrate through and are connected with the inner wall of the supporting plate in a sliding mode, two buffer air bags are arranged on the inner wall of the bottom plate, and the tops of the sliding rods are in contact with the buffer air bags.
Preferably, a plurality of protruding blocks are arranged at the bottom of the supporting plate, and the bottoms of the protruding blocks are higher than the bottoms of the sliding rods.
Preferably, a limiting frame is fixed on the side face of the sliding rod, and the limiting frame can be abutted against the supporting plate.
Preferably, the dust removing structure comprises two sealing lantern rings, the sealing lantern rings are connected with the buffer air bags, one sides of the sealing lantern rings away from the buffer air bags are rotatably sleeved with gas pipelines, one ends of the gas pipelines are connected with gas blowing rings, a plurality of gas outlet holes are formed in the gas blowing rings in a circumferential array, and the gas outlet holes are matched with the cameras.
Preferably, the adjusting structure comprises a mounting plate, the mounting plate is connected with the bottom plate in a rotating way, one section of the gas pipeline is fixed on the inner wall of the mounting plate, one side of the camera is fixed on the side surface of the mounting plate, a telescopic rod is connected to the bottom plate in a rotating way, and one end, away from the bottom plate, of the telescopic rod is connected with the side surface of the mounting plate in a rotating way.
Compared with the prior art, the utility model has the beneficial effects that:
(1) According to the utility model, the unmanned aerial vehicle, the adjusting structure, the mounting plate, the telescopic rod, the bottom plate and the camera are arranged, so that when the unmanned aerial vehicle body is used, the telescopic rod is controlled to work, the mounting plate and the gas pipeline are conveniently driven to rotate around the bottom plate, the angle of the camera on the mounting plate is driven to change, the picture is conveniently switched, and the unmanned aerial vehicle body can be comprehensively inspected.
(2) According to the utility model, through the arrangement, the shock absorption structure, the supporting plate, the convex blocks, the sliding rods, the limiting frame, the buffer air bags, the dust removal structure, the sealing lantern ring, the gas pipeline, the gas blowing ring and the gas outlet holes, when the unmanned aerial vehicle body descends, the bottoms of the sliding rods are positioned below the convex blocks, the sliding rods can contact the ground firstly, so that the buffer air bags can slide towards the top and are extruded, the buffering shock absorption of the unmanned aerial vehicle body is facilitated, the landing impact is reduced, the convex blocks at the bottoms of the supporting plates facilitate the supporting plates to stably support on uneven ground, the stability is increased, the buffer air bags are extruded to extrude gas from the sealing lantern ring, the gas is introduced into the gas blowing ring through the gas pipeline, and the discharged gas is discharged from the gas outlet holes, so that dust adhesion on the surface of the camera is avoided, the use of the camera is facilitated, the automatic cleaning is facilitated, and the use is convenient.
Drawings
FIG. 1 is one of the perspective views of the present utility model;
FIG. 2 is a second perspective view of the present utility model;
FIG. 3 is a schematic illustration of the connection of the slide bar, cushion bladder and gas lines of the present utility model;
FIG. 4 is a schematic diagram of the connection of the dust removal structure, mounting plate and camera of the present utility model;
FIG. 5 is a schematic illustration of the connection of the sealing collar and gas line of the present utility model;
FIG. 6 is a schematic view of the connection of the air ring and the air outlet holes of the present utility model;
in the figure: 1. unmanned plane; 2. a shock absorbing structure; 21. a support plate; 22. a bump; 23. a slide bar; 24. a limit frame; 25. a buffer air bag; 3. a dust removal structure; 31. a sealing collar; 32. a gas line; 33. a gas blowing ring; 34. an air outlet hole; 4. an adjustment structure; 41. a mounting plate; 42. a telescopic rod; 5. a bottom plate; 6. a camera is provided.
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.
Embodiment one:
referring to fig. 1 to 6, an unmanned aerial vehicle recognition device includes:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, wherein a bottom plate 5 is fixedly arranged at the bottom of the unmanned aerial vehicle body 1, and a camera 6 is arranged in the middle of the bottom plate 5;
the shock absorption structure 2 is arranged at the bottom of the unmanned aerial vehicle body 1 and is used for absorbing shock of the unmanned aerial vehicle body 1;
the dust removing structure 3 is positioned on the side surface of the camera 6 and connected with the damping structure 2, and is used for removing dust from the camera 6;
the adjusting structure 4 is arranged on the bottom plate 5 and is used for adjusting the angle of the camera 6.
The shock-absorbing structure 2 includes backup pad 21, backup pad 21 fixed mounting in the bottom of unmanned aerial vehicle organism 1, the bottom inner wall sliding connection of bottom plate 5 has two slide bars 23, the bottom of slide bar 23 run through and with the inner wall sliding connection of backup pad 21, two buffer airbag 25 are installed to the inner wall of bottom plate 5, the top of slide bar 23 with buffer airbag 25 is inconsistent.
A plurality of protruding blocks 22 are installed at the bottom of the supporting plate 21, and the bottom of the protruding blocks 22 is higher than the bottom of the sliding rod 23.
The side of slide bar 23 is fixed with spacing frame 24, spacing frame 24 can with backup pad 21 is contradicted, and spacing frame 24 avoids slide bar 23 to drop, guarantees simultaneously that slide bar 23 can keep on contradicting with buffer air bag 25, avoids slide bar 23 sliding distance longer to cause impact damage to buffer air bag 25.
The dust removing structure 3 comprises two sealing lantern rings 31, the sealing lantern rings 31 are connected with the buffer air bags 25, one side, far away from the buffer air bags 25, of each sealing lantern ring 31 is rotatably sleeved with a gas pipeline 32, one end of each gas pipeline 32 is connected with a gas blowing ring 33, a plurality of gas outlet holes 34 are formed in the gas blowing ring 33 in a circumferential array, and the gas outlet holes 34 are matched with the cameras 6.
The adjusting structure 4 comprises a mounting plate 41, the mounting plate 41 is rotationally connected with the bottom plate 5, one section of the gas pipeline 32 is fixed on the inner wall of the mounting plate 41, one side of the camera 6 is fixed on the side surface of the mounting plate 41, a telescopic rod 42 is rotationally connected on the bottom plate 5, and one end, far away from the bottom plate 5, of the telescopic rod 42 is rotationally connected with the side surface of the mounting plate 41.
From the above, when the unmanned aerial vehicle body 1 is used, an operator can conveniently drive the mounting plate 41 and the gas pipeline 32 to rotate around the bottom plate 5 by controlling the telescopic rod 42 to work, so that the angle of the camera 6 on the mounting plate 41 is driven to change, the picture is convenient to switch, and the unmanned aerial vehicle body 1 can conveniently and comprehensively patrol;
in addition, when unmanned aerial vehicle organism 1 descends, slide bar 23 bottom is located lug 22 below, slide bar 23 can contact ground earlier, thereby can slide and extrude buffer air bag 25 to the top, be convenient for carry out buffering shock attenuation to unmanned aerial vehicle organism 1, reduce the impact nature of falling to the ground, the lug 22 of backup pad 21 bottom is convenient for backup pad 21 at the steady support of uneven ground, increase stability, and buffer air bag 25 receives the extrusion and can extrude gas from sealed lantern ring 31, and enter into in the gas ring 33 through gas line 32, discharge from venthole 34, the exhaust gas can clear up camera 6 surface dust, thereby avoid the dust to adhere and influence camera 6 to use, be convenient for clear up automatically, facilitate the use.
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 (6)
1. An unmanned aerial vehicle recognition device, characterized by comprising:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein a bottom plate (5) is fixedly arranged at the bottom of the unmanned aerial vehicle body (1), and a camera (6) is arranged in the middle of the bottom plate (5);
the shock absorption structure (2), the shock absorption structure (2) is arranged at the bottom of the unmanned aerial vehicle body (1) and is used for absorbing shock of the unmanned aerial vehicle body (1);
the dust removing structure (3) is positioned on the side face of the camera (6) and connected with the shock absorbing structure (2) and is used for removing dust from the camera (6);
the adjusting structure (4) is arranged on the bottom plate (5) and used for adjusting the angle of the camera (6).
2. The unmanned aerial vehicle identification device of claim 1, wherein: the shock-absorbing structure (2) comprises a supporting plate (21), the supporting plate (21) is fixedly arranged at the bottom of the unmanned aerial vehicle body (1), two sliding rods (23) are connected to the inner wall of the bottom plate (5) in a sliding mode, the bottoms of the sliding rods (23) penetrate through and are connected with the inner wall of the supporting plate (21) in a sliding mode, two buffer air bags (25) are arranged on the inner wall of the bottom plate (5), and the tops of the sliding rods (23) are in contact with the buffer air bags (25).
3. The unmanned aerial vehicle identification device of claim 2, wherein: the bottom of the supporting plate (21) is provided with a plurality of protruding blocks (22), and the bottom of each protruding block (22) is higher than the bottom of the sliding rod (23).
4. The unmanned aerial vehicle identification device of claim 2, wherein: the side of the sliding rod (23) is fixedly provided with a limiting frame (24), and the limiting frame (24) can be abutted against the supporting plate (21).
5. The unmanned aerial vehicle identification device of claim 2, wherein: the dust removal structure (3) comprises two sealing lantern rings (31), the sealing lantern rings (31) are connected with the buffer air bags (25), one side, away from the buffer air bags (25), of each sealing lantern ring (31) is rotatably sleeved with a gas pipeline (32), one end of each gas pipeline (32) is connected with a blowing ring (33), a plurality of air outlet holes (34) are formed in the blowing rings (33) in a circumferential array, and the air outlet holes (34) are matched with the camera (6).
6. The unmanned aerial vehicle identification device of claim 5, wherein: the adjusting structure (4) comprises a mounting plate (41), the mounting plate (41) is rotationally connected with the bottom plate (5), one section of the gas pipeline (32) is fixed on the inner wall of the mounting plate (41), one side of the camera (6) is fixed on the side face of the mounting plate (41), a telescopic rod (42) is rotationally connected on the bottom plate (5), and one end, far away from the bottom plate (5), of the telescopic rod (42) is rotationally connected with the side face of the mounting plate (41).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321588896.0U CN220349968U (en) | 2023-06-21 | 2023-06-21 | Unmanned aerial vehicle recognition device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321588896.0U CN220349968U (en) | 2023-06-21 | 2023-06-21 | Unmanned aerial vehicle recognition device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220349968U true CN220349968U (en) | 2024-01-16 |
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ID=89478046
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321588896.0U Active CN220349968U (en) | 2023-06-21 | 2023-06-21 | Unmanned aerial vehicle recognition device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220349968U (en) |
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2023
- 2023-06-21 CN CN202321588896.0U patent/CN220349968U/en active Active
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