CN218142172U - Aviation electric board for fixed monitoring of unmanned aerial vehicle - Google Patents
Aviation electric board for fixed monitoring of unmanned aerial vehicle Download PDFInfo
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- CN218142172U CN218142172U CN202222724251.7U CN202222724251U CN218142172U CN 218142172 U CN218142172 U CN 218142172U CN 202222724251 U CN202222724251 U CN 202222724251U CN 218142172 U CN218142172 U CN 218142172U
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Abstract
The utility model relates to an unmanned air vehicle technique field just discloses an unmanned aerial vehicle fixed monitoring is with avionics board, including unmanned aerial vehicle body, avionics board, the inside dismouting mechanism that is provided with of unmanned aerial vehicle body, dismouting mechanism is including mounting panel, connecting rod, L type connecting rod one, mounting panel one side and avionics board one side fixed connection, mounting panel opposite side and connecting rod one end fixed connection, the connecting rod other end runs through the installation incasement side and extends to the installation incasement portion, connecting rod one side and a L type connecting rod top fixed connection, L type connecting rod one-side extrusion contact has L type connecting rod two, two one side fixed mounting of L type connecting rod have electric telescopic handle, electric telescopic handle one end and installation incasement wall fixed connection have realized can be fast convenient carrying out fixed mounting and dismantlement with the avionics board, have solved and have dismantled the avionics board and have dismantled the too loaded down with trivial details problem of change step, have improved unmanned aerial vehicle's work efficiency.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an avionics board for fixed monitoring of unmanned aerial vehicle.
Background
Unmanned aerial vehicle is called unmanned aerial vehicle for short, and is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, compared with the unmanned aerial vehicle, the unmanned aerial vehicle is more suitable for tasks too easy, dirty or dangerous, and can be divided into military use and civil use according to the application field, the unmanned aerial vehicle is divided into a reconnaissance plane and a target plane, and the civil use, unmanned aerial vehicle and industrial use are really just needed by the unmanned aerial vehicle; in the application in fields such as aerial photography, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey and drawing, news report, electric power is patrolled and examined, relief of disaster, movie & TV is shot, make romantic, great expansion unmanned aerial vehicle's use itself, developed country is also in the active extension industry application and development unmanned aerial vehicle technique, but current unmanned aerial vehicle can't be with the quick fixed mounting that carries on of avionics board to the step that needs dismantle the avionics board and change is too loaded down with trivial details, thereby lead to unmanned aerial vehicle's work efficiency to reduce.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle is avionics board for fixed monitoring has solved the problem among the above-mentioned background art.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle is avionics board for fixed monitoring, includes unmanned aerial vehicle body, avionics board, the inside dismouting mechanism that is provided with of unmanned aerial vehicle body, dismouting mechanism is including mounting panel, connecting rod, L type connecting rod one, mounting panel one side and avionics board one side fixed connection, mounting panel opposite side and connecting rod one end fixed connection, the connecting rod other end runs through the install bin outside and extends to inside the install bin, connecting rod one side and a top fixed connection of L type connecting rod, L type connecting rod one-to-one side extrusion contact has L type connecting rod two, two one side fixed mounting of L type connecting rod have electric telescopic handle, electric telescopic handle one end and install bin inner wall fixed connection.
Preferably, the inner wall of the L-shaped connecting rod II is slidably connected with a first sliding rod, one end of the first sliding rod is fixedly connected with the inner wall of the installation box, the other end of the first sliding rod is fixedly connected with one side of the bearing plate, the bottom of the bearing plate is fixedly connected with the inner wall of the installation box, and the L-shaped connecting rod II can be better and stably moved.
Preferably, connecting rod one end fixed mounting has the limiting plate, the spacing groove has been seted up to limiting plate one side, spacing inslot wall and gag lever post one end extrusion contact, the gag lever post other end runs through the baffle-box outside and extends to inside the baffle-box.
Preferably, the movable plate is fixedly mounted at one end of the limiting rod, two ends of the movable plate are connected with the inner wall of the buffer box in a sliding mode, one side of the buffer box is fixedly connected with the inner wall of the installation box, and a first spring is fixedly mounted between one side of the limiting plate and the inner wall of the installation box, so that the avionic board can be better and quickly fixedly mounted.
Preferably, the inside buffer gear that is provided with of unmanned aerial vehicle body, buffer gear is including carrier bar, buffer board, carrier bar one end and install bin outside fixed connection, the carrier bar other end and buffer board one side fixed connection.
Preferably, the inner wall of the buffer plate is connected with a second sliding rod in a sliding mode, a stabilizer bar is fixedly mounted at the bottom of the buffer plate, and a sliding block is fixedly mounted at one end of the stabilizer bar.
Preferably, slider inner wall and the two outer wall sliding connection of slide bar, slider one end and two one end fixed connection of spring, two other ends of spring and unmanned aerial vehicle body inner wall fixed connection, the shock attenuation buffering of carrying on that can be better protects the aviation electroplax.
Preferably, two one ends fixed mounting of slide bar have the stopper, two bottoms of slide bar and unmanned aerial vehicle body inner wall fixed connection, the dodge gate has openly been seted up to the unmanned aerial vehicle body
The utility model provides an unmanned aerial vehicle is avionics board for fixed monitoring. This unmanned aerial vehicle is avionics board for fixed monitoring possesses following beneficial effect:
(1) The utility model discloses in: according to the avionics board for fixed monitoring of the unmanned aerial vehicle, the avionics board can be quickly and conveniently fixed, mounted and dismounted through the dismounting mechanism mounted in the unmanned aerial vehicle body, the problem that the avionics board needs to be dismounted and replaced, and the steps are too complicated is solved, and the working efficiency of the unmanned aerial vehicle is improved;
(2) The utility model discloses in: this aviation electroplax for unmanned aerial vehicle fixed monitoring has realized through installing at the inside buffer gear of unmanned aerial vehicle body can carrying out the shock attenuation buffering when unmanned aerial vehicle work takes place to vibrate, has solved the unable problem with the effectual protection of aviation electroplax, has improved the live time of aviation electroplax, has avoided the frequent change aviation electroplax.
Drawings
FIG. 1 is a schematic view of the front view of the device of the present invention;
FIG. 2 is a schematic cross-sectional view of the apparatus of the present invention;
FIG. 3 is an enlarged schematic view of the detaching mechanism of the present invention;
fig. 4 is an enlarged schematic view of a portion a in fig. 3 according to the present invention.
In the figure: the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, an avionic board 2, a dismounting mechanism 3, a mounting plate 301, a connecting rod 302, a first L-shaped connecting rod 303, a second L-shaped connecting rod 304, an electric telescopic rod 305, a first sliding rod 306, a bearing plate 307, a limiting plate 308, a limiting rod 309, a moving plate 310, a buffer box 311, a mounting box 312, a buffer mechanism 4, a bearing rod 401, a buffer plate 402, a second sliding rod 403, a sliding block 404 and a stabilizing rod 405.
Detailed Description
As shown in fig. 1-4, the utility model provides a technical solution: an avionics board for fixing and monitoring an unmanned aerial vehicle comprises an unmanned aerial vehicle body 1 and an avionics board 2, wherein a dismounting mechanism 3 is arranged in the unmanned aerial vehicle body 1, the dismounting mechanism 3 comprises a mounting plate 301, a connecting rod 302 and an L-shaped connecting rod I303, one side of the mounting plate 301 is fixedly connected with one side of the avionics board 2, the other side of the mounting plate 301 is fixedly connected with one end of the connecting rod 302, the other end of the connecting rod 302 penetrates through the outer side of a mounting box 312 and extends into the mounting box 312, one side of the connecting rod 302 is fixedly connected with the top of the L-shaped connecting rod I303, one side of the L-shaped connecting rod I303 is in extrusion contact with an L-shaped connecting rod II 304, one side of the L-shaped connecting rod II 304 is fixedly provided with an electric telescopic rod 305, one end of the electric telescopic rod 305 is fixedly connected with the inner wall of the mounting box 312, the inner wall of the L-shaped connecting rod II 304 is slidably connected with a slide rod I306, one end of the slide rod I306 is fixedly connected with the inner wall of the mounting box 312, the other end of the slide rod I306 is fixedly connected with one side of the mounting plate 307, the bottom of a bearing plate 307 is fixedly connected with the inner wall of an installation box 312, one end of a connecting rod 302 is fixedly provided with a limiting plate 308, one side of the limiting plate 308 is provided with a limiting groove, the inner wall of the limiting groove is in extrusion contact with one end of a limiting rod 309, the other end of the limiting rod 309 penetrates through the outer side of the buffer box 311 and extends into the buffer box 311, one end of the limiting rod 309 is fixedly provided with a movable plate 310, the two ends of the movable plate 310 are in sliding connection with the inner wall of the buffer box 311, one side of the buffer box 311 is fixedly connected with the inner wall of the installation box 312, a first spring is fixedly arranged between one side of the limiting plate 308 and the inner wall of the installation box 312, a buffer mechanism 4 is arranged in an unmanned aerial vehicle body 1, the buffer mechanism 4 comprises a bearing rod 401 and a buffer plate 402, one end of the bearing rod 401 is fixedly connected with the outer side of the installation box 312, the other end of the bearing rod 401 is fixedly connected with one side of the buffer plate 402, and the inner wall of the buffer plate 402 is in sliding connection with a second sliding rod 403, buffer board 402 bottom fixed mounting has stabilizer bar 405, stabilizer bar 405 one end fixed mounting has slider 404, slider 404 inner wall and two 403 outer wall sliding connection of slide bar, slider 404 one end and two one end fixed connection of spring, two other ends of spring and 1 inner wall fixed connection of unmanned aerial vehicle body, two 403 one end fixed mounting of slide bar have the stopper, two 403 bottoms of slide bar and 1 inner wall fixed connection of unmanned aerial vehicle body, the dodge gate has openly been seted up to unmanned aerial vehicle body 1, realized that can be fast convenient carry out fixed mounting and dismantlement with the avionics board, the problem that it is too loaded down with trivial details to have solved the change step with the avionics board to dismantle is solved, unmanned aerial vehicle's work efficiency has been improved, realized can when unmanned aerial vehicle work takes place to vibrate, carry out the shock attenuation buffering, the problem of unable effectual protection with the avionics board has been solved, the live time of avionics board has been improved, the avionics board has been avoided regular change.
When the avionics board for fixed monitoring of the unmanned aerial vehicle is used, when the unmanned aerial vehicle is used, the avionics board 2 is placed inside the unmanned aerial vehicle body 1 through a movable door arranged on the front surface of the unmanned aerial vehicle body 1, the connecting rod 302 arranged on one side of the mounting plate 301 is inserted into the mounting box 312, the L-shaped connecting rod II 304 is driven to move on the sliding rod I306 by starting the electric telescopic rod 305 to work, the L-shaped connecting rod II 304 is driven to contact with the L-shaped connecting rod I303 arranged on one side of the connecting rod 302 and to be extruded and fixed, the connecting rod 302 is driven to move to drive the limiting plate 308, the limiting plate 308 is driven to move by the limiting plate 308, the limiting plate 308 extrudes the spring I at the moment, the moving plate 310 is driven to move by the limiting rod 309, and thus the avionics board 2 is fixedly mounted, when unmanned aerial vehicle flight produces the vibration, remove through extrusion carrier bar 401 and drive buffer board 402 and remove on two 403 slide bars, it removes to drive stabilizer bar 405 through buffer board 402 and removes, it moves on two 403 slide bars to drive slider 404 through stabilizer bar 405 removal, slider 404 can extrude spring two and carry out the shock attenuation buffering this moment, thereby can protect avionics board 2, finally realized can be fast convenient carry out fixed mounting and dismantlement with the avionics board, the problem that it is too loaded down with trivial details to have solved the need to dismantle the avionics board and change the step is improved, unmanned aerial vehicle's work efficiency is improved, when having realized can work at unmanned aerial vehicle and take place the vibration, shock attenuation buffering is carried out, the problem of unable effectual protection with the avionics board has been solved, the live time of avionics board has been improved, the frequent change avionics board has been avoided.
Claims (8)
1. The utility model provides an unmanned aerial vehicle is avionics board for fixed monitoring, includes unmanned aerial vehicle body (1), avionics board (2), its characterized in that: unmanned aerial vehicle body (1) is inside to be provided with dismouting mechanism (3), dismouting mechanism (3) are including mounting panel (301), connecting rod (302), L type connecting rod (303), mounting panel (301) one side and aviation electric board (2) one side fixed connection, mounting panel (301) opposite side and connecting rod (302) one end fixed connection, the connecting rod (302) other end runs through the install bin (312) outside and extends to inside install bin (312), connecting rod (302) one side and L type connecting rod (303) top fixed connection, L type connecting rod (303) one side extrusion contact has L type connecting rod two (304), L type connecting rod two (304) one side fixed mounting has electric telescopic handle (305), electric telescopic handle (305) one end and install bin (312) inner wall fixed connection.
2. The avionics board for fixed monitoring of unmanned aerial vehicles according to claim 1, characterized in that: the inner wall of the L-shaped connecting rod II (304) is connected with a sliding rod I (306) in a sliding mode, one end of the sliding rod I (306) is fixedly connected with the inner wall of the installation box (312), the other end of the sliding rod I (306) is fixedly connected with one side of a bearing plate (307), and the bottom of the bearing plate (307) is fixedly connected with the inner wall of the installation box (312).
3. The avionics board for unmanned aerial vehicle fixed monitoring according to claim 1, characterized in that: connecting rod (302) one end fixed mounting has limiting plate (308), the spacing groove has been seted up to limiting plate (308) one side, spacing inslot wall and gag lever post (309) one end extrusion contact, gag lever post (309) other end runs through the baffle-box (311) outside and extends to inside of baffle-box (311).
4. The avionics board for fixed monitoring of unmanned aerial vehicles according to claim 3, characterized in that: gag lever post (309) one end fixed mounting has movable plate (310), movable plate (310) both ends and baffle-box (311) inner wall sliding connection, baffle-box (311) one side and install bin (312) inner wall fixed connection, fixed mounting has spring one between limiting plate (308) one side and install bin (312) inner wall.
5. The avionics board for unmanned aerial vehicle fixed monitoring according to claim 1, characterized in that: the unmanned aerial vehicle body (1) is inside to be provided with buffer gear (4), buffer gear (4) are including carrier bar (401), buffer board (402), carrier bar (401) one end and install bin (312) outside fixed connection, the carrier bar (401) other end and buffer board (402) one side fixed connection.
6. The avionics board for fixed monitoring of unmanned aerial vehicles according to claim 5, characterized in that: the inner wall of the buffer plate (402) is connected with a second sliding rod (403) in a sliding mode, a stabilizer bar (405) is fixedly mounted at the bottom of the buffer plate (402), and a sliding block (404) is fixedly mounted at one end of the stabilizer bar (405).
7. The avionics board for unmanned aerial vehicle fixed monitoring according to claim 6, characterized in that: slider (404) inner wall and two (403) outer wall sliding connection of slide bar, slider (404) one end and two one end fixed connection of spring, two other ends of spring and unmanned aerial vehicle body (1) inner wall fixed connection.
8. The avionics board for fixed monitoring of unmanned aerial vehicles according to claim 7, characterized in that: slide bar two (403) one end fixed mounting has the stopper, slide bar two (403) bottom and unmanned aerial vehicle body (1) inner wall fixed connection, the dodge gate has openly been seted up in unmanned aerial vehicle body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222724251.7U CN218142172U (en) | 2022-10-17 | 2022-10-17 | Aviation electric board for fixed monitoring of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222724251.7U CN218142172U (en) | 2022-10-17 | 2022-10-17 | Aviation electric board for fixed monitoring of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218142172U true CN218142172U (en) | 2022-12-27 |
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ID=84570701
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222724251.7U Active CN218142172U (en) | 2022-10-17 | 2022-10-17 | Aviation electric board for fixed monitoring of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218142172U (en) |
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2022
- 2022-10-17 CN CN202222724251.7U patent/CN218142172U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230519 Address after: 526070, 1st floor, Building 11, Shuangchuangyuan, Guanyan Avenue, Dinghu District, Zhaoqing City, Guangdong Province. Northwest side of the intersection of Tongxing Road and Shunjing Road, Zone 31, Guicheng New City, Dinghu District, Zhaoqing City Patentee after: Guangdong century South Technology Co.,Ltd. Address before: 518000 604, block a, building 6, Shenzhen International Innovation Valley, Dashi 1st Road, Xili community, Xili street, Nanshan District, Shenzhen, Guangdong Patentee before: Shenzhen kebit Aviation Technology Co.,Ltd. |