CN221024211U - Unmanned aerial vehicle security protection inspection equipment - Google Patents
Unmanned aerial vehicle security protection inspection equipment Download PDFInfo
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- CN221024211U CN221024211U CN202323154599.8U CN202323154599U CN221024211U CN 221024211 U CN221024211 U CN 221024211U CN 202323154599 U CN202323154599 U CN 202323154599U CN 221024211 U CN221024211 U CN 221024211U
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- 238000007689 inspection Methods 0.000 title claims abstract description 20
- 230000007246 mechanism Effects 0.000 claims abstract description 25
- 230000001681 protective effect Effects 0.000 claims abstract description 23
- 238000004140 cleaning Methods 0.000 claims abstract description 22
- 230000010405 clearance mechanism Effects 0.000 claims abstract description 11
- 230000000670 limiting effect Effects 0.000 claims description 8
- 238000000034 method Methods 0.000 abstract description 4
- 238000012544 monitoring process Methods 0.000 abstract description 4
- 239000007787 solid Substances 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 3
- 230000009471 action Effects 0.000 abstract description 2
- 239000000428 dust Substances 0.000 description 5
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram 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
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- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
The utility model discloses unmanned aerial vehicle security inspection equipment, and relates to the technical field of unmanned aerial vehicles. Including fixed wing unmanned aerial vehicle, fixed wing unmanned aerial vehicle bottom is fixed with clearance mechanism, clearance mechanism includes the shell, shell both ends inner wall both sides are fixed with tensile cylinder respectively, tensile cylinder output is fixed with the ejector pad, two the ejector pad opposite face is fixed with the solid piece respectively, two gu the joint has the elasticity strip jointly in solid piece top, two gu the joint has the rubber brush jointly in solid piece bottom, the opening has been seted up to the shell bottom, the contact of opening inner wall has two protective housing, two mutual joint of protective housing. According to the utility model, the rubber brush and the protective shell are added in the cleaning mechanism, so that the camera is prevented from being directly contacted with the outside in the use process, the safety of the camera is improved, and the quality of the monitoring image quality is improved under the action of the rubber brush.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to unmanned aerial vehicle security inspection equipment.
Background
In some special scenes, the unmanned aerial vehicle is required to carry out security inspection work, so that unmanned aerial vehicle security inspection equipment is required.
The police security unmanned aerial vehicle with the patent publication number of CN218929821U drives the screw rod to rotate through the motor, and under the limiting effect of the limiting rod, the cleaning plate can reciprocate up and down on the side surface of the camera assembly, so that the dust, the rainwater and the fog on the surface of the camera can be cleaned, and the quality of a monitoring picture can be ensured.
However, in the practical use process of the security inspection equipment, because the outdoor environment is uncontrollable, the cleaning plate of the device cannot well clean the surface of the camera in the environment full of dust, dust possibly adheres to the surface of the cleaning plate, the quality of the monitoring image quality is reduced, the applicability of the device is also reduced, and the applicant provides the unmanned aerial vehicle security inspection equipment for the purpose.
Disclosure of utility model
The utility model aims to provide unmanned aerial vehicle security inspection equipment 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: unmanned aerial vehicle security protection inspection equipment, including fixed wing unmanned aerial vehicle, fixed wing unmanned aerial vehicle bottom is fixed with clearance mechanism, clearance mechanism includes the shell, shell both ends inner wall both sides are fixed with tensile cylinder respectively, tensile cylinder output is fixed with the ejector pad, two the ejector pad opposite face is fixed with the fixed block respectively, two the joint has the elastic strip jointly at fixed block top, two the joint has the rubber brush jointly in fixed block bottom, the opening has been seted up to the shell bottom, opening inner wall contact has two protective housing, two protective housing joint each other, the bottom of rubber brush contacts with the outer wall of two protective housings, two protective housing outer wall both sides are fixed with the fixed block respectively, the draw-in groove has been seted up to fixed block one side, one of them the common rotation in protective housing inner wall both sides is connected with the dead lever, the dead lever bottom is fixed with the camera.
Preferably, the two sides of the bottom of the fixed wing unmanned aerial vehicle are respectively fixed with a supporting frame, and the two sides of the cleaning mechanism are jointly fixed with a control mechanism.
Preferably, the cleaning mechanism further comprises a chassis, two clamps are fixedly connected to the bottom of the chassis in a sliding mode, a plurality of pressure springs are fixed between the two clamps, one ends of the clamps are respectively clamped with two sides of the inner wall of the shell, a plurality of limiting rods are respectively fixed to two sides of the inner wall of two ends of the shell, two stretching cylinders are respectively located at the bottoms of the limiting rods, the top of the rubber brush is fixed to the bottom of the elastic strip, and first bolts are clamped among the elastic strip, the fixing blocks and the rubber brush through common threads.
Preferably, the control mechanism comprises two fixed frames, one end of each fixed frame is fixed with two sides of the cleaning mechanism, a fixed box is fixed on one side of the inner wall of each fixed frame, two fixed box openings correspond to each other, fixed plates are fixed on two sides of the outer wall of each fixed box, springs are fixed on one side of the inner wall of each fixed box, a retaining plate is fixed on one end of each spring, the outer wall of each retaining plate is connected with the inner wall of each fixed box in a sliding manner, a pushing block is fixed on the bottom of each retaining plate, a notch is formed in the bottom of each fixed box, one end of each pushing block penetrates through the notch of the bottom of each fixed box, two sides of each pushing block are connected with two sides of the inner wall of each notch in a sliding manner, a second bolt is clamped between each fixed plate and each pushing plate in a threaded manner, a motor is fixed on one side of each retaining plate, and a clamping block is clamped with one side of each set of the cleaning mechanism.
Preferably, the height of the pushing block cannot be larger than the distance from the bottom of the limiting rod to the bottom of the inner wall of the shell, and the limit distance of the rubber brush is larger than the maximum circumference of the protective shell.
Preferably, the fixed wing unmanned aerial vehicle, the stretching cylinder, the camera and the motor are electrically connected in sequence, and the fixed wing unmanned aerial vehicle, the stretching cylinder, the camera and the motor share one control terminal.
Compared with the prior art, the utility model has the beneficial effects that:
This unmanned aerial vehicle security protection equipment of patrolling and examining through the setting to clearance mechanism, has increased rubber brush and protective housing the inside, at the camera use, has not only avoided the direct contact of camera with external world, has improved the security of camera to under the effect through rubber brush, improve the quality of control image quality.
Meanwhile, in the cleaning mechanism, the stretching air cylinder and the pushing block are also arranged, and the cleaning work of the protective shell can be ensured to be carried out at intervals by pushing the rubber brush, so that the quality of the monitoring image quality is further improved.
Drawings
FIG. 1 is a schematic top view of the present utility model;
FIG. 2 is a schematic view of the bottom structure of the present utility model;
FIG. 3 is a schematic view of a cleaning mechanism according to the present utility model;
FIG. 4 is an enlarged view of a portion A of FIG. 3;
fig. 5 is a schematic structural diagram of a control mechanism according to the present utility model.
In the figure: 1. fixed wing unmanned aerial vehicle; 2. a cleaning mechanism; 201. a chassis; 202. a clip; 203. a pressure spring; 204. a housing; 205. a limit rod; 206. a stretching cylinder; 207. a pushing block; 208. fixing blocks; 209. an elastic strip; 210. a rubber brush; 211. a first bolt; 212. a protective shell; 213. fixing blocks; 214. a fixed rod; 215. a camera; 3. a control mechanism; 301. setting a frame; 302. fixing the box; 303. a fixed plate; 304. a spring; 305. a retaining plate; 306. a push plate; 307. a second bolt; 308. a motor; 309. a clamping block; 4. and (5) supporting a frame.
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.
When manual operation cannot be performed, an unmanned aerial vehicle is required to be used for working, so that unmanned aerial vehicle security inspection equipment is required, most of traditional security inspection equipment is in actual use, because of large external environment difference, a method for timely and effectively cleaning a camera is not available in many cases, the image quality of shooting is reduced, the user experience is reduced, and the unmanned aerial vehicle security inspection equipment is proposed by the applicant.
As shown in fig. 1 to 5, the present utility model provides a technical solution: the unmanned aerial vehicle security inspection equipment comprises a fixed wing unmanned aerial vehicle 1, a cleaning mechanism 2 is fixed at the bottom of the fixed wing unmanned aerial vehicle 1, the cleaning mechanism 2 comprises a shell 204, a stretching cylinder 206 is respectively fixed at two sides of the inner walls of two ends of the shell 204, a push block 207 is fixed at the output end of the stretching cylinder 206, two push blocks 207 are respectively fixed with a fixed block 208, elastic strips 209 are jointly clamped at the tops of the two fixed blocks 208, rubber brushes 210 are jointly clamped at the bottoms of the two fixed blocks 208, an opening is formed at the bottom of the shell 204, two protective shells 212 are contacted with the inner walls of the opening, the bottoms of the rubber brushes 210 are mutually clamped, the outer walls of the two protective shells 212 are contacted with each other, fixed blocks 213 are respectively fixed at two sides of the outer walls of the two protective shells 212, a clamping groove is formed at one side of the fixed block 213, a fixed rod 214 is jointly rotationally connected with two sides of the inner wall of one of the protective shells 212, a camera 215 is fixed at the bottom of the fixed rod 214, the fixed wing unmanned aerial vehicle 1 bottom both sides are fixed with strut 4 respectively, the clearance mechanism 2 both sides are fixed with control mechanism 3 jointly, clearance mechanism 2 still includes chassis 201, chassis 201 bottom sliding connection is fixed with two clips 202, be fixed with a plurality of pressure spring 203 between two clips 202, two clip 202 one end respectively with the mutual joint of the inner wall both sides of shell 204, shell 204 both ends inner wall both sides are fixed with a plurality of gag lever post 205 respectively, two tensile cylinder 206 are located every group gag lever post 205 bottom respectively, the top of rubber brush 210 is fixed with the bottom of elastic strip 209 mutually, the joint has first bolt 211 between elastic strip 209, the joint of common screw thread between solid piece 208 and the rubber brush 210, the height of ejector pad 207 can not be greater than the distance of gag lever post 205 bottom to shell 204 inner wall bottom, the limit distance of rubber brush 210 is greater than the maximum girth of protective housing 212, fixed wing unmanned aerial vehicle 1, the stretching cylinder 206, the camera 215 and the motor 308 are electrically connected in sequence, and the four share one control terminal.
It should be noted that: when the camera 215 is cleaned, the air cylinder 206 is stretched to drive the pushing blocks 207 to move, and the rubber brushes 210 are clamped between the pushing blocks 207, so that dust on the outer wall of the protective shell 212 can be cleaned effectively, stability in the cleaning process can be guaranteed due to the action of the limiting rod 205, and meanwhile, stability of the rubber brushes 210 can be guaranteed due to the clamping of the elastic strips 209.
As shown in fig. 5, the present utility model provides a technical solution: unmanned aerial vehicle security protection inspection equipment, including control mechanism 3, control mechanism 3 includes two fixed shelves 301, two fixed shelves 301 one end is fixed mutually with clearance mechanism 2 both sides jointly, fixed box 302 is fixed with to fixed shelf 301 inner wall one side, two fixed box 302 opening parts correspond each other, fixed box 302 outer wall both sides are fixed with fixed plate 303 respectively, fixed box 302 inner wall one side is fixed with spring 304, spring 304 one end is fixed with the butt plate 305, butt plate 305 outer wall and fixed box 302 inner wall sliding connection each other, butt plate 305 bottom is fixed with ejector pad 207, the breach has been seted up to fixed box 302 bottom, ejector pad 207 one end passes the breach of fixed box 302 bottom, and ejector pad 207 both sides and breach inner wall both sides sliding connection each other, common screw thread joint has second bolt 307 between two fixed plate 303 and the ejector pad 306, butt plate 305 one side is fixed with motor 308, the clamping block 309 is fixed with the clamping block 308 to the output, one side of clamping block 309 and the clamping groove mutual joint of seting up of each group 213 one side in clearance mechanism 2.
It should be noted that: when the camera is cleaned, the motor 308 will drive the clamping block 309 to rotate firstly, because the clamping block 309 is clamped on the two fixed blocks 213, the two protecting shells 212 will also rotate at intervals, the cleaning mechanism 2 will clean one of the protecting shells 212, because the camera inside the protecting shell 212 is rotationally connected with the inner wall of the protecting shell 212, and because of the weight of the camera, the camera will not rotate, so as to clean the dust on the outer wall of the protecting shell 212.
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 hereto without departing from the spirit and scope of the utility model as defined by the appended embodiments and equivalents thereof.
Claims (6)
1. Unmanned aerial vehicle security protection equipment of patrolling and examining, including fixed wing unmanned aerial vehicle (1), its characterized in that: fixed wing unmanned aerial vehicle (1) bottom is fixed with clearance mechanism (2), clearance mechanism (2) include shell (204), shell (204) both ends inner wall both sides are fixed with tensile cylinder (206) respectively, tensile cylinder (206) output is fixed with ejector pad (207), two ejector pad (207) opposite face is fixed with fixed block (208) respectively, two joint has elastic strip (209) at fixed block (208) top, two joint has rubber brush (210) jointly in fixed block (208) bottom, the opening has been seted up to shell (204) bottom, opening inner wall contact has two protective housing (212), two protective housing (212) each other joint, the bottom of rubber brush (210) contacts with the outer wall of two protective housing (212), two protective housing (212) outer wall both sides are fixed with fixed block (213) respectively, the draw-in groove has been seted up to fixed block (213) one of them both sides joint has dead lever (214) jointly, dead lever (215) bottom fixed lever (215).
2. The unmanned aerial vehicle security inspection device of claim 1, wherein: the two sides of the bottom of the fixed wing unmanned aerial vehicle (1) are respectively fixed with a supporting frame (4), and the two sides of the cleaning mechanism (2) are jointly fixed with a control mechanism (3).
3. The unmanned aerial vehicle security inspection device of claim 1, wherein: the cleaning mechanism (2) further comprises a chassis (201), two clamping clips (202) are fixedly connected to the bottom of the chassis (201) in a sliding mode, a plurality of pressure springs (203) are fixedly arranged between the clamping clips (202), one ends of the clamping clips (202) are respectively clamped with two sides of the inner wall of the shell (204) in a mutually clamping mode, a plurality of limiting rods (205) are respectively fixed to two sides of the inner wall of two ends of the shell (204), two stretching cylinders (206) are respectively located at the bottoms of each group of limiting rods (205), the tops of the rubber brushes (210) are fixed to the bottoms of the elastic strips (209), and first bolts (211) are clamped between the elastic strips (209), the fixing blocks (208) and the rubber brushes (210) in a common thread mode.
4. The unmanned aerial vehicle security inspection device of claim 2, wherein: the control mechanism (3) comprises two fixed frames (301), one end of each fixed frame (301) is fixed with two sides of the cleaning mechanism (2) together, one side of the inner wall of each fixed frame (301) is fixed with a fixed box (302), two openings of each fixed box (302) are mutually corresponding, two sides of the outer wall of each fixed box (302) are respectively fixed with a fixed plate (303), one side of the inner wall of each fixed box (302) is fixed with a spring (304), one end of each spring (304) is fixed with a retaining plate (305), the outer wall of each retaining plate (305) is connected with the inner wall of each fixed box (302) in a sliding mode, the bottom of each retaining plate (305) is fixed with a pushing block (207), one end of each fixed box (302) is provided with a notch, two sides of each pushing block (207) are mutually connected with two sides of the inner wall of the notch in a sliding mode, two sides of each retaining plates (303) are mutually clamped with a second bolt (307) in a threaded mode, one side of each retaining plate (305) is fixed with a motor (308), and one side of each retaining block (308) is clamped with one side of the cleaning mechanism (309), and one side of each retaining block (309) is fixed with one side of the cleaning mechanism (309).
5. The unmanned aerial vehicle security inspection device of claim 1, wherein: the height of the pushing block (207) cannot be larger than the distance from the bottom of the limit rod (205) to the bottom of the inner wall of the shell (204), and the limit distance of the rubber brush (210) is larger than the maximum circumference of the protective shell (212).
6. The unmanned aerial vehicle security inspection device of claim 1, wherein: the fixed wing unmanned aerial vehicle (1), the stretching cylinder (206), the camera (215) and the motor (308) are electrically connected in sequence, and the fixed wing unmanned aerial vehicle, the stretching cylinder, the camera and the motor share one control terminal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323154599.8U CN221024211U (en) | 2023-11-22 | 2023-11-22 | Unmanned aerial vehicle security protection inspection equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323154599.8U CN221024211U (en) | 2023-11-22 | 2023-11-22 | Unmanned aerial vehicle security protection inspection equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221024211U true CN221024211U (en) | 2024-05-28 |
Family
ID=91178999
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323154599.8U Active CN221024211U (en) | 2023-11-22 | 2023-11-22 | Unmanned aerial vehicle security protection inspection equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221024211U (en) |
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2023
- 2023-11-22 CN CN202323154599.8U patent/CN221024211U/en active Active
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