CN220595233U - Unmanned aerial vehicle patrols and examines - Google Patents
Unmanned aerial vehicle patrols and examines Download PDFInfo
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- CN220595233U CN220595233U CN202322256465.0U CN202322256465U CN220595233U CN 220595233 U CN220595233 U CN 220595233U CN 202322256465 U CN202322256465 U CN 202322256465U CN 220595233 U CN220595233 U CN 220595233U
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 30
- 230000007246 mechanism Effects 0.000 claims abstract description 19
- 238000007667 floating Methods 0.000 claims abstract description 13
- 238000007689 inspection Methods 0.000 claims description 18
- 238000007789 sealing Methods 0.000 claims description 18
- 238000007664 blowing Methods 0.000 claims description 5
- 230000009471 action Effects 0.000 abstract description 4
- 230000007547 defect Effects 0.000 abstract description 4
- 238000000034 method Methods 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 4
- 239000003086 colorant Substances 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 238000001228 spectrum Methods 0.000 description 3
- 239000000428 dust Substances 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000701 chemical imaging Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a patrol unmanned aerial vehicle, which comprises a patrol unmanned aerial vehicle main body, wherein a multispectral pan-tilt camera is arranged at the bottom end of the patrol unmanned aerial vehicle main body, two symmetrical supporting rods are fixedly arranged on the outer surface of the patrol unmanned aerial vehicle main body, supporting plates are fixedly arranged at the bottom ends of the two supporting rods, a floating mechanism is arranged on the lower surface of the supporting plate, and a walking assembly which is convenient for the patrol unmanned aerial vehicle main body falling on the water surface to walk on the water surface is arranged at the end part of the supporting plate. According to the utility model, the floating mechanism is arranged, so that the unmanned aerial vehicle can stably land on the water surface when the electric quantity is insufficient in the process of executing the water surface task, and can float on the water surface under the action of the two inflatable airbag cushions, so that the stable landing of the unmanned aerial vehicle is realized, and the defect that the unmanned aerial vehicle cannot land on the water surface in the prior art is effectively overcome.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a patrol unmanned aerial vehicle.
Background
Multispectral unmanned aerial vehicle is one kind can carry out multispectral imaging's unmanned aerial vehicle platform. The basic principle is that a plurality of hardware wave band sensors are used for capturing images with different wavelength spectrum resolutions, and related information of a target object is obtained through processing and analyzing a spectrum imaging image. The multispectral unmanned aerial vehicle has wide application range, and covers a plurality of fields such as agriculture, forestry, environment monitoring, urban planning and the like. But in terms of affinity, a wide range of applications are realized in agriculture in many cases.
Among the prior art, a patrol unmanned aerial vehicle of publication number CN218055641U has adopted including "organism, the equal swing joint in both sides of organism has the screw, the equal fixedly connected with landing leg in both sides of organism bottom, the buffer tank has been seted up to the bottom of landing leg, the inner chamber fixedly connected with spring of buffer tank, the bottom fixedly connected with buffer rod of spring, the scheme of the bottom fixedly connected with backing plate of buffer rod, this scheme passes through organism, screw, landing leg, buffer tank, spring, buffer rod, backing plate, casing, first riser, first spout, screw rod, motor, shaft coupling, thread bush, lifter, second riser, second spout, movable block, guide pulley, camera, dust absorption board, fan, dust collection box and filter, makes the patrol unmanned aerial vehicle that possesses long-distance photograph intelligent acquisition function protect the subassembly through protection machanism to this has improved the availability factor and the practicality that possess patrol unmanned aerial vehicle that examines of patrol intelligent acquisition function.
However, the above solution still has some drawbacks, for example, when the unmanned aerial vehicle is in the process of executing the task close to the water surface, and the unmanned aerial vehicle has low power and cannot fly on the land far away from the water surface, the unmanned aerial vehicle proposed by the above patent technology easily falls into the water, so that the unmanned aerial vehicle is damaged, i.e. the technical solution proposed by the above patent technology has the defect that the unmanned aerial vehicle cannot land on the water surface.
In view of the above, the utility model provides an inspection unmanned aerial vehicle.
Disclosure of Invention
The utility model aims to provide a patrol 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 patrols and examines, includes the unmanned aerial vehicle main part of patrolling and examining and sets up the actuating mechanism that is used for driving the unmanned aerial vehicle main part of patrolling and examining at the unmanned aerial vehicle main part surface of patrolling and examining, the bottom of the unmanned aerial vehicle main part of patrolling and examining is provided with multispectral cloud platform camera, the surface of the unmanned aerial vehicle main part of patrolling and examining has set firmly two symmetrical bracing pieces, and the bottom of two bracing pieces has all set firmly the backup pad, the lower surface of backup pad is provided with floating mechanism;
the floating mechanism comprises a rectangular storage groove formed in the lower surface of the supporting plate and a mounting groove formed in the inner top wall of the rectangular storage groove, an inflatable air bag column is fixedly arranged on the inner wall of the mounting groove, an inflatable air bag cushion is fixedly arranged at the bottom end of the inflatable air bag column, the inflatable air bag column and the inflatable air bag cushion are mutually communicated, and the floating mechanism further comprises a first air pump which is fixedly arranged on the surface of the supporting rod and used for inflating the inflatable air bag column.
As the preferable technical scheme, the bottom end inner wall of the inflatable airbag column is fixedly provided with two symmetrical flow limiting plates for limiting the air flow, and a narrow air flow channel is formed between the two flow limiting plates.
As the preferable technical scheme, the air inlet end of the first air pump is provided with a filter cover, the air outlet end of the first air pump is provided with an inflation tube extending to the inside of the inflatable air bag column, and the inflation tube penetrates through the inside of the supporting rod.
As the preferable technical scheme, the lower surface of backup pad articulates there are two be used for carrying out sealed closing plate to rectangular storage tank, and the opposite face when two closing plates are closed has all set firmly the elastic sealing strip.
As the preferable technical scheme, the inside of the two elastic sealing strips is provided with magnetic strips mutually attracted with each other.
As the preferable technical scheme, the tip of backup pad is provided with the walking subassembly that the unmanned aerial vehicle main part of patrolling and examining of being convenient for to descend at the surface of water carries out the surface of water walking.
As the preferable technical scheme, walking subassembly is including seting up at the inside cavity of backup pad tip plate body to and set firmly the second air pump at the cavity inner wall, the end of giving vent to anger of second air pump is provided with the gas blow pipe that extends to the backup pad outside, the inner wall of cavity still has set firmly the stand-by power supply who is used for carrying out the power supply to the second air pump.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the utility model, the floating mechanism is arranged, so that the unmanned aerial vehicle can stably land on the water surface when the electric quantity is insufficient in the process of executing the water surface task, and can float on the water surface under the action of the two inflatable airbag cushions, so that the stable landing of the unmanned aerial vehicle is realized, and the defect that the unmanned aerial vehicle cannot land on the water surface in the prior art is effectively overcome.
2. According to the utility model, by arranging the walking assembly, when the power of the unmanned aerial vehicle is insufficient, the unmanned aerial vehicle needs to temporarily land on the water surface, so that the unmanned aerial vehicle landing on the water surface can smoothly return to the shore, the practicability is high, and the unmanned aerial vehicle is worthy of popularization and use in special environments.
Drawings
In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic perspective 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 showing an expanded perspective structure of the floating mechanism of the present utility model;
FIG. 4 is a schematic view of the second view structure of FIG. 3 according to the present utility model;
FIG. 5 is a schematic side sectional view of a support plate according to the present utility model;
fig. 6 is a schematic diagram of the front cross-section of the support plate of the present utility model.
In the figure: 1. inspection of the unmanned aerial vehicle main body; 2. a driving mechanism; 3. multispectral pan-tilt camera; 4. a support rod; 5. a support plate; 6. a floating mechanism; 601. a rectangular storage groove; 602. a mounting groove; 603. an inflatable airbag column; 604. an inflatable airbag cushion; 605. a first air pump; 606. a flow-limiting plate; 607. a sealing plate; 608. an elastic sealing strip; 609. a magnetic stripe; 7. a walking assembly; 701. a second air pump; 702. an air blowing pipe; 703. and a standby power supply.
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.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this utility model belongs. The terminology used herein in the description of the utility model is for the purpose of describing particular embodiments only and is not intended to be limiting of the utility model. The term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.
In order to better understand the above technical solutions, the following detailed description will refer to the accompanying drawings and specific embodiments.
According to the drawings 1-6, the embodiment of the utility model provides an inspection unmanned aerial vehicle, which comprises an inspection unmanned aerial vehicle main body 1 and a driving mechanism 2 arranged on the outer surface of the inspection unmanned aerial vehicle main body 1 and used for driving the inspection unmanned aerial vehicle main body 1 to fly, wherein a multispectral cradle head camera 3 is arranged at the bottom end of the inspection unmanned aerial vehicle main body 1, the multispectral cradle head camera 3 mainly adopts a multispectral technology, and light rays with different wavelengths are converted into different colors by utilizing the wavelength difference of the light rays with different colors, so that the acquisition and the processing of the light rays with different colors are realized. The multispectral holder camera 3 is internally provided with a plurality of spectrum sensors, including red, green, blue and other light sensors, which can respectively collect signals of different colors of light and convert the signals into digital signals for processing; in the multispectral holder camera 3, the function of the holder is very important, and the holder can realize the up-down, left-right, rotation and other movements of the camera, so that the camera can cover a larger range, and the multispectral holder camera 3 can realize the multi-angle and all-directional monitoring of targets through the movement of the holder.
Two symmetrical support rods 4 are fixedly arranged on the outer surface of the inspection unmanned aerial vehicle main body 1, support plates 5 are fixedly arranged at the bottom ends of the two support rods 4, and a floating mechanism 6 is arranged on the lower surface of each support plate 5;
the floating mechanism 6 comprises a rectangular storage groove 601 formed in the lower surface of the supporting plate 5 and a mounting groove 602 formed in the inner top wall of the rectangular storage groove 601, two sealing plates 607 used for sealing the rectangular storage groove 601 are hinged to the lower surface of the supporting plate 5, and elastic sealing strips 608 are fixedly arranged on opposite surfaces of the two sealing plates 607 when the two sealing plates 607 are closed.
The inside of two elastic sealing strips 608 all is provided with the magnetic stripe 609 that mutually magnetism attracts mutually, after taking in the rectangle storage tank 601 with inflatable airbag pad 604, can close two closing plates 607 and make two elastic sealing strips 608 extrudeed each other and dock fixedly under the effect of magnetic stripe 609, realizes the closure to the rectangle storage tank 601.
The inner wall of the installation groove 602 is fixedly provided with an inflatable airbag column 603, the inner wall of the bottom end of the inflatable airbag column 603 is fixedly provided with two symmetrical flow limiting plates 606 for limiting the airflow, and a narrow airflow channel is formed between the two flow limiting plates 606.
The bottom end of the inflatable airbag column 603 is fixedly provided with an inflatable airbag cushion 604, the inflatable airbag column 603 and the inflatable airbag cushion 604 are mutually communicated, and the floating mechanism 6 further comprises a first air pump 605 which is fixedly arranged on the surface of the supporting rod 4 and is used for inflating the inflatable airbag column 603.
The air inlet end of the first air pump 605 is provided with a filter cover, and the air outlet end of the first air pump 605 is provided with an air inflation tube extending to the inside of the air inflation bag column 603, and the air inflation tube penetrates through the inside of the support rod 4.
According to the unmanned aerial vehicle, the floating mechanism 6 is arranged, when the electric quantity is insufficient in the process of executing a water surface task, the first air pump 605 can be started to inflate the inside of the inflatable air bag column 603 through the remote controller, so that the inflatable air bag column 603 is inflated, meanwhile, under the action of the two current limiting plates 606, air flows can firstly fill the inflatable air bag column 603 and then fill the inflatable air bag pad 604 with air, when the inflatable air bag column 603 is full, the inflatable air bag column 603 is inflated and stretched, the inflatable air bag pad 604 is pushed up to open the two sealing plates 607, the inflatable air bag pad 604 is inflated to be in a plate shape after the inflatable air bag pad 604 is continuously inflated, and therefore the unmanned aerial vehicle can stably land on the water surface and float on the water surface under the action of the two inflatable air bag pads 604, and the defect that the unmanned aerial vehicle cannot land on the water surface in the prior art is effectively solved.
The tip of backup pad 5 is provided with the walking subassembly 7 that the unmanned aerial vehicle main part 1 of patrolling and examining that is convenient for drop on the surface of water walks on the surface of water.
The walking assembly 7 comprises a cavity formed in the end plate body of the support plate 5 and a second air pump 701 fixedly arranged on the inner wall of the cavity, an air blowing pipe 702 extending to the outside of the support plate 5 is arranged at the air outlet end of the second air pump 701, and a standby power supply 703 for supplying power to the second air pump 701 is further fixedly arranged on the inner wall of the cavity.
According to the utility model, by arranging the walking assembly 7, after the unmanned aerial vehicle needs to temporarily land on the water surface when the unmanned aerial vehicle is insufficient, the second air pump 701 can be started through the remote controller, so that the second air pump 701 blows air to the end part of the supporting plate 5 through the air blowing pipe 702, the unmanned aerial vehicle can be driven to slide and walk on the water surface under the reaction force generated during blowing, and meanwhile, the direction of the unmanned aerial vehicle can be regulated during walking on the water surface by controlling the starting and stopping of the two second air pumps 701, so that the unmanned aerial vehicle landed on the water surface can smoothly return to the shore, and the unmanned aerial vehicle has high practicability and is worthy of popularization and use under special environments.
In particular, the first air pump 605 and the second air pump 701 are electric air pumps that can be inflated and deflated.
The foregoing has shown and described the basic principles, principal features and advantages of the utility model. It will be understood by those skilled in the art that the present utility model is not limited to the above-described embodiments, and that the above-described embodiments and descriptions are only preferred embodiments of the present utility model, and are not intended to limit the utility model, and that various changes and modifications may be made therein without departing from the spirit and scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (7)
1. The utility model provides an unmanned aerial vehicle patrols and examines, including patrolling and examining unmanned aerial vehicle main part (1) and setting up and be used for driving the actuating mechanism (2) that patrol and examine unmanned aerial vehicle main part (1) flight at the unmanned aerial vehicle main part (1) surface of patrolling and examining, its characterized in that: the intelligent inspection unmanned aerial vehicle comprises an inspection unmanned aerial vehicle main body (1), wherein a multispectral pan-tilt camera (3) is arranged at the bottom end of the inspection unmanned aerial vehicle main body (1), two symmetrical supporting rods (4) are fixedly arranged on the outer surface of the inspection unmanned aerial vehicle main body (1), supporting plates (5) are fixedly arranged at the bottom ends of the two supporting rods (4), and a floating mechanism (6) is arranged on the lower surface of each supporting plate (5);
the utility model provides a float mechanism (6) is including seting up rectangle storage tank (601) at backup pad (5) lower surface to and seting up mounting groove (602) at rectangle storage tank (601) inner roof, the inner wall of mounting groove (602) has set firmly inflatable bag post (603), inflatable bag pad (604) have set firmly to the bottom of inflatable bag post (603), and inflatable bag post (603) and inflatable bag pad (604) communicate each other, float mechanism (6) still including setting up first air pump (605) that are used for carrying out the inflatable to inflatable bag post (603) on bracing piece (4) surface.
2. The inspection drone of claim 1, wherein: two symmetrical flow limiting plates (606) for limiting the air flow are fixedly arranged on the inner wall of the bottom end of the inflatable air bag column (603), and a narrow air flow channel is formed between the two flow limiting plates (606).
3. The inspection drone of claim 1, wherein: the air inlet end of the first air pump (605) is provided with a filter cover, the air outlet end of the first air pump (605) is provided with an air inflation pipe extending to the inside of the air inflation bag column (603), and the air inflation pipe penetrates through the inside of the supporting rod (4).
4. The inspection drone of claim 1, wherein: the lower surface of the supporting plate (5) is hinged with two sealing plates (607) for sealing the rectangular storage groove (601), and elastic sealing strips (608) are fixedly arranged on opposite surfaces of the two sealing plates (607) when the two sealing plates are closed.
5. The inspection drone of claim 4, wherein: the inside of the two elastic sealing strips (608) is provided with magnetic strips (609) which are mutually magnetic and mutually attracted.
6. A drone as claimed in any one of claims 1 to 5, wherein: the end of backup pad (5) is provided with the walking subassembly (7) that inspection unmanned aerial vehicle main part (1) that are convenient for drop at the surface of water walks on the surface of water.
7. The inspection drone of claim 6, wherein: the walking assembly (7) comprises a cavity formed in the end plate body of the supporting plate (5) and a second air pump (701) fixedly arranged on the inner wall of the cavity, an air blowing pipe (702) extending to the outside of the supporting plate (5) is arranged at the air outlet end of the second air pump (701), and a standby power supply (703) for supplying power to the second air pump (701) is further fixedly arranged on the inner wall of the cavity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322256465.0U CN220595233U (en) | 2023-08-21 | 2023-08-21 | Unmanned aerial vehicle patrols and examines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322256465.0U CN220595233U (en) | 2023-08-21 | 2023-08-21 | Unmanned aerial vehicle patrols and examines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220595233U true CN220595233U (en) | 2024-03-15 |
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ID=90173396
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322256465.0U Active CN220595233U (en) | 2023-08-21 | 2023-08-21 | Unmanned aerial vehicle patrols and examines |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220595233U (en) |
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2023
- 2023-08-21 CN CN202322256465.0U patent/CN220595233U/en active Active
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