CN218055645U - Unmanned aerial vehicle for monitoring - Google Patents
Unmanned aerial vehicle for monitoring Download PDFInfo
- Publication number
- CN218055645U CN218055645U CN202221264494.0U CN202221264494U CN218055645U CN 218055645 U CN218055645 U CN 218055645U CN 202221264494 U CN202221264494 U CN 202221264494U CN 218055645 U CN218055645 U CN 218055645U
- Authority
- CN
- China
- Prior art keywords
- monitor
- unmanned aerial
- aerial vehicle
- plate
- cylinder
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Emergency Alarm Devices (AREA)
Abstract
The utility model provides an unmanned aerial vehicle for monitoring, including unmanned aerial vehicle body and monitor, the base plate is installed to unmanned aerial vehicle body bottom, and the loading ring is installed to the base plate bottom, installs two sector plates of mutual disposition in the loading ring, and two opposite side surfaces of sector plate are the arcwall face; two groups of clamping pieces are arranged at one end of the monitor, which is positioned in the loading ring, and are respectively arranged corresponding to the two fan-shaped plates, and each clamping piece comprises an upper clamping plate and a lower clamping plate which are positioned at the upper side and the lower side of each fan-shaped plate, and each fan-shaped plate is clamped between the upper clamping plate and the lower clamping plate. The monitor of the utility model can be detachably arranged in the loading ring, different monitoring tasks can be carried out by directly replacing the monitor when in use, and devices required to be carried outside are reduced; the monitor and the loading ring are connected in a rotary clamping manner, and the monitor and the controller are connected in a plug-in connection manner, so that the monitor is convenient to replace.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle is used in monitoring.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicle according to application, can be divided into for military use and civilian use: for military use, unmanned aerial vehicles are divided into reconnaissance aircraft and target drone; in the civil aspect, the unmanned aerial vehicle industry is applied, and the unmanned aerial vehicle is really just needed. At present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
In the aspect of unmanned aerial vehicles applied to environment monitoring, multiple unmanned aerial vehicles are required to work cooperatively when monitoring of environment pictures and air parameters is carried out, multiple devices are required to be carried when people go out, and monitoring cost is high.
SUMMERY OF THE UTILITY MODEL
Based on the technical problem who exists in the background art, the utility model provides an unmanned aerial vehicle is used in monitoring.
The utility model provides an unmanned aerial vehicle for monitoring, including unmanned aerial vehicle body and monitor, the base plate is installed to unmanned aerial vehicle body bottom, and the loading ring is installed to the base plate bottom, installs two fan-shaped plates of mutual disposition in the loading ring, and two fan-shaped plate relative side faces are the arcwall face; two groups of clamping pieces are arranged at one end of the monitor, which is positioned in the loading ring, and are respectively arranged corresponding to the two fan-shaped plates, and each clamping piece comprises an upper clamping plate and a lower clamping plate which are positioned at the upper side and the lower side of each fan-shaped plate, and each fan-shaped plate is clamped between the upper clamping plate and the lower clamping plate.
Preferably, the distance between the end parts of the two sector plates is not less than the width of the upper clamping plate and the lower clamping plate.
Preferably, the anti-skidding silica gel sheet is arranged on one side, close to the lower clamping plate, of the upper clamping plate.
Preferably, the distance between the lower clamping plate and the sector plate is 1-3mm.
Preferably, the position of the inner wall of the loading ring, which is located on one side, away from the sector plate, of the lower clamping plate is provided with an internal thread section and an internal thread section in threaded connection with an external thread sleeve, the external thread sleeve is in contact with the lower clamping plate, and one end, away from the lower clamping plate, of the external thread sleeve is connected with a fixing sleeve attached to the bottom end face of the loading ring.
Preferably, the unmanned aerial vehicle body includes the rectangle mounting bracket, and rectangle mounting bracket top four corners position all is provided with the connecting rod, and the supporting legs is installed to rotatory fan and its bottom on the connecting rod top, installs the controller of being connected with the monitor electricity in the rectangle mounting bracket, and the base plate is installed in rectangle mounting bracket bottom.
Preferably, the monitor is provided with a male plug connecting post, a through hole for the male plug connecting post to pass through is formed in the position, corresponding to the male plug connecting post, of the substrate, the male plug connecting post comprises a first cylinder, a second cylinder and a third cylinder which are sequentially connected, the diameters of the first cylinder, the second cylinder and the third cylinder are sequentially reduced from one end close to the monitor to one end far away from the monitor, insulating layers are arranged outside the first cylinder and the third cylinder, and an elastic sleeve is sleeved on the third cylinder; the controller is provided with a female plug stepped hole which is matched with the male plug connecting column and is used for inserting the male plug connecting column.
Preferably, the elastic sleeve is a spring.
Preferably, the monitor is an image acquisition camera, a gas sampler, a temperature monitor or a moisture detector.
The utility model provides an unmanned aerial vehicle for monitoring, the monitor can be dismantled and install in loading the ring, can carry out different monitoring tasks through directly changing the monitor when using, reduces the device that needs to carry out; the monitor and the loading ring are connected in a rotary clamping manner, and the monitor and the controller are connected in a plug-in connection manner, so that the monitor is convenient to replace.
Drawings
Fig. 1 is a schematic structural view of an unmanned aerial vehicle for monitoring provided by the present invention;
fig. 2 is an assembly view of a monitor and a loading ring in the unmanned aerial vehicle for monitoring according to the present invention;
FIG. 3 isbase:Sub>A sectional view taken along line A-A of FIG. 2;
fig. 4 is a schematic structural diagram of a loading ring in the unmanned aerial vehicle for monitoring according to the present invention;
fig. 5 is a schematic structural diagram of a monitor in the unmanned aerial vehicle for monitoring provided by the present invention;
fig. 6 is the utility model provides a structural schematic diagram of outer thread bush among unmanned aerial vehicle for monitoring.
Detailed Description
Referring to fig. 1-6, the utility model provides an unmanned aerial vehicle is used in monitoring, including unmanned aerial vehicle body and monitor 1, wherein:
the unmanned aerial vehicle body includes rectangle mounting bracket 9, and 9 top four corners positions of rectangle mounting bracket all are provided with connecting rod 10, and supporting legs 12 are installed to rotatory fan 11 and its bottom on connecting rod 10 top, install the controller 13 of being connected with monitor 1 electricity in the rectangle mounting bracket 9.
The base plate 2 is arranged at the bottom of the rectangular mounting frame 9, the loading ring 3 is arranged at the bottom of the base plate 2, and the monitor 1 is detachably arranged in the loading ring 3.
In this embodiment, monitor 1 demountable installation can carry out different monitoring tasks through direct change monitor 1 when using in loading ring 3, reduces the device that needs to carry out.
In this embodiment, for the dismouting of convenient monitor 1, install two fan-shaped plates 4 of mutual disposition in the loading ring 3, two fan-shaped plate 4 relative side are the arcwall face. Monitor 1 is located one end in loading ring 3 and installs two sets of folders, and two sets of folders correspond the setting with two sector plates 4 respectively, and the folder includes that the punch holder 5, the lower plate 6 that are located sector plate 4 upper and lower both sides and sector plate 4 joint are between punch holder 5 and lower plate 6, and the distance between two sector plate 4 tip is not less than the width of punch holder 5, lower plate 6. When the monitor 1 is installed, firstly, two upper clamping plates 5 are respectively inserted above the sector plates 4 from the position between the end parts of the two sector plates 4, then the monitor 1 is rotated, so that the upper clamping plates 5 are positioned above the sector plates 4 and the lower clamping plates 6 are positioned below the sector plates 4, and at the moment, the sector plates 4 are clamped between the upper clamping plates 5 and the lower clamping plates 6; when the monitor 1 is disassembled, the monitor 1 is rotated, the upper clamping plate 5 and the lower clamping plate 6 are moved to a position between the ends of the two sector plates 4, and then the monitor 1 is pulled outwards, so that the monitor 1 can be disassembled.
In a specific embodiment, in order to improve the assembling firmness of the monitor 1, an anti-slip silicone sheet is arranged on one side of the upper clamping plate 5, which is close to the lower clamping plate 6. After the anti-skid plastic sheet is arranged, the distance between the lower clamping plate 6 and the sector plate 4 is 1-3mm.
In a specific embodiment, an internal thread section is arranged on the inner wall of the loading ring 3 at a position of the lower clamping plate 6 far away from the fan-shaped plate 4, the internal thread section is in threaded connection with an external thread sleeve 7, the external thread sleeve 7 is in contact with the lower clamping plate 6, and one end of the external thread sleeve 7 far away from the lower clamping plate 6 is connected with a fixing sleeve 8 attached to the bottom end face of the loading ring 3. Support lower plate 6 through external screw thread cover 7 and fixed cover 8 to form to monitor 1 and block, monitor 1 takes place the obscission appearance because of unmanned aerial vehicle's vibrations when preventing to use unmanned aerial vehicle for a long time.
In a specific embodiment, as shown in the figure, the monitor 1 is provided with a male plug connection pole, a through hole for the male plug connection pole to pass through is opened at a position corresponding to the male plug connection pole on the substrate 2, the male plug connection pole includes a first cylinder 14, a second cylinder 15 and a third cylinder 16 which are connected in sequence, from one end close to the monitor 1 to one end far away from the monitor 1, the diameters of the first cylinder 14, the second cylinder 15 and the third cylinder 16 are reduced in sequence, the first cylinder 14 and the third cylinder 16 are both provided with insulating layers outside, the second cylinder 15 is used as a power supply connection part, an elastic sleeve 17 is sleeved on the third cylinder 16, and the elastic sleeve 17 is preferably a spring. The controller 13 is provided with a female pin stepped hole which is matched with the male pin connecting column and into which the male pin connecting column is inserted. After the male plug connecting column is matched and connected with the female plug stepped hole, the upper clamping plate 5 is pressed on the sector plate 4 when the spring abuts against the stepped surface, and the upper clamping plate 5 and the sector plate 4 are prevented from sliding relatively.
In a particular embodiment, the monitor 1 is an image acquisition camera, a gas sampler, a temperature monitor 1, or a moisture detector.
The above, only be the embodiment of the preferred of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, which are designed to be replaced or changed equally, all should be covered within the protection scope of the present invention.
Claims (9)
1. An unmanned aerial vehicle for monitoring is characterized by comprising an unmanned aerial vehicle body and a monitor (1), wherein a base plate (2) is installed at the bottom of the unmanned aerial vehicle body, a loading ring (3) is installed at the bottom of the base plate (2), two fan-shaped plates (4) which are oppositely arranged are installed in the loading ring (3), and one opposite side surfaces of the two fan-shaped plates (4) are arc-shaped surfaces; monitor (1) is located one end of loading ring (3) and installs two sets of folders, and two sets of folders correspond the setting with two sector plates (4) respectively, and the folder is including being located upper clamping plate (5), lower clamping plate (6) and sector plate (4) joint between upper clamping plate (5) and lower clamping plate (6) of sector plate (4) upper and lower both sides.
2. Unmanned aerial vehicle for monitoring according to claim 1, characterized in that, the distance between two sector plates (4) tip is no less than the width of punch holder (5), lower plate (6).
3. Unmanned aerial vehicle for monitoring according to claim 1, characterized in that, the upper splint (5) is provided with anti-skidding silica gel piece near the lower splint (6) side.
4. Unmanned aerial vehicle for monitoring according to claim 3, characterized in that the distance between lower splint (6) and sector plate (4) is 1-3mm.
5. An unmanned aerial vehicle for monitoring as claimed in any of claims 1-4, wherein the inner wall of the loading ring (3) is provided with an internal thread section at a position on one side of the lower clamping plate (6) far away from the sector plate (4), the internal thread section is in threaded connection with an external thread sleeve (7), the external thread sleeve (7) is in contact with the lower clamping plate (6), and one end of the external thread sleeve (7) far away from the lower clamping plate (6) is connected with a fixed sleeve (8) attached to the bottom end face of the loading ring (3).
6. The unmanned aerial vehicle for monitoring of any one of claims 1-4, wherein the unmanned aerial vehicle body comprises a rectangular mounting frame (9), four corners of the top end of the rectangular mounting frame (9) are provided with connecting rods (10), a rotating fan (11) is installed at the top end of each connecting rod (10), supporting legs (12) are installed at the bottom end of each connecting rod, a controller (13) electrically connected with the monitor (1) is installed in the rectangular mounting frame (9), and the base plate (2) is installed at the bottom of the rectangular mounting frame (9).
7. The unmanned aerial vehicle for monitoring according to claim 6, wherein the monitor (1) is provided with a male plug connecting post, a through hole for the male plug connecting post to pass through is formed in the position, corresponding to the male plug connecting post, of the substrate (2), the male plug connecting post comprises a first cylinder (14), a second cylinder (15) and a third cylinder (16) which are sequentially connected, the diameters of the first cylinder (14), the second cylinder (15) and the third cylinder (16) are sequentially reduced from one end close to the monitor (1) to the end far away from the monitor (1), insulating layers are respectively arranged outside the first cylinder (14) and the third cylinder (16), and an elastic sleeve (17) is sleeved on the third cylinder (16); the controller (13) is provided with a female plug stepped hole which is matched with the male plug connecting column and is used for the male plug connecting column to be inserted.
8. Unmanned aerial vehicle for monitoring according to claim 7, characterized in that elastic sleeve (17) is a spring.
9. A drone for monitoring according to any one of claims 1 to 4, characterised in that the monitor (1) is an image acquisition camera, a gas sampler, a temperature monitor or a moisture detector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221264494.0U CN218055645U (en) | 2022-05-24 | 2022-05-24 | Unmanned aerial vehicle for monitoring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221264494.0U CN218055645U (en) | 2022-05-24 | 2022-05-24 | Unmanned aerial vehicle for monitoring |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218055645U true CN218055645U (en) | 2022-12-16 |
Family
ID=84432715
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221264494.0U Active CN218055645U (en) | 2022-05-24 | 2022-05-24 | Unmanned aerial vehicle for monitoring |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218055645U (en) |
-
2022
- 2022-05-24 CN CN202221264494.0U patent/CN218055645U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN218055645U (en) | Unmanned aerial vehicle for monitoring | |
| CN213677162U (en) | Remotely-controlled unmanned aerial vehicle sampling device | |
| CN107416179B (en) | Four-axis plant protection unmanned aerial vehicle convenient to transportation and loading and unloading | |
| CN213229120U (en) | Remote sensing surveying and mapping unmanned aerial vehicle with accurate positioning | |
| CN207889980U (en) | A kind of novel photovoltaic unmanned plane O＆M inspection device | |
| CN207106849U (en) | A kind of more rotor unmanned aircrafts of agricultural plant protection | |
| CN105109679A (en) | Locking component and multi-rotor unmanned aerial vehicle | |
| CN211391730U (en) | Unmanned aerial vehicle with aerial survey camera quick detach mechanism | |
| CN208882124U (en) | A kind of camera system of unmanned plane | |
| CN209956233U (en) | Unmanned aerial vehicle quick assembly disassembly carry device | |
| CN211107953U (en) | Unmanned aerial vehicle lift cantilever crane connection structure | |
| CN218172576U (en) | Unmanned aerial vehicle landing leg | |
| CN107187585A (en) | A kind of unmanned plane | |
| CN211196607U (en) | Foldable multiaxis unmanned aerial vehicle | |
| CN214824108U (en) | Unmanned aerial vehicle with detachable wings | |
| CN215622756U (en) | Aviation survey and drawing unmanned aerial vehicle | |
| CN209037870U (en) | Loading device and multi-spectral camera equipment based on unmanned plane | |
| CN215043778U (en) | Unmanned aerial vehicle audible and visual alarm device | |
| CN213473520U (en) | Unmanned aerial vehicle aircraft with high altitude sprays function | |
| CN107284654B (en) | Four-axis plant protection unmanned aerial vehicle convenient to transport | |
| CN209834024U (en) | Generator fixing part universal for engine | |
| CN217893258U (en) | Dustproof protection device of bare soil flying dust aerial survey unmanned aerial vehicle | |
| CN215475701U (en) | Foldable unmanned wing | |
| CN111762331B (en) | Unmanned aerial vehicle protection is with split type shielding device | |
| CN209852598U (en) | Installation base of infrared camera on unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |