CN214267949U - A remove unmanned aerial vehicle for outdoor monitoring - Google Patents
A remove unmanned aerial vehicle for outdoor monitoring Download PDFInfo
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- CN214267949U CN214267949U CN202022696203.2U CN202022696203U CN214267949U CN 214267949 U CN214267949 U CN 214267949U CN 202022696203 U CN202022696203 U CN 202022696203U CN 214267949 U CN214267949 U CN 214267949U
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Abstract
The utility model discloses a remove unmanned aerial vehicle for outdoor monitoring, including organism, link and camera, the symmetric shaping has two hypotenuses on the link, the bottom of link has the bottom plate through two elastic connection of spring, it has the connecting rod of flange to run through the top shaping on the link, the inner chamber of link is equipped with the guide arm on the horizontal direction, the outside of guide arm is equipped with two spring one and two movable blocks. The utility model discloses in, the outside at the connecting rod is established to the spring two, the both ends of spring two respectively with link and bottom plate butt, under the effect of spring one, two movable blocks are close to each other, the gyro wheel with the shaping at the inclined plane looks butt of movable block bottom, when unmanned aerial vehicle falls to the ground and strikes ground, spring one takes place deformation with spring two, played the shock attenuation effect of buffering, compare traditional unmanned aerial vehicle, the buffering effect is better, can effectually avoid unmanned aerial vehicle internals's damage.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a remove unmanned aerial vehicle for outdoor monitoring.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", 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.
Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; 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, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
The landing gear of the existing unmanned aerial vehicle is mostly spliced by carbon fiber composite material pipes or is provided with a special-shaped bent plate and a bent pipe, and is clamped by screw fastening or outer surface extrusion, the landing gear of the device is difficult to play a buffering role when landing, and the impact force of the unmanned aerial vehicle on the ground is large in the landing process, so that the internal parts of the unmanned aerial vehicle are easily damaged.
Disclosure of Invention
The utility model aims to provide a: in order to solve the problems, the mobile unmanned aerial vehicle for outdoor monitoring is provided.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a remove unmanned aerial vehicle for outdoor monitoring, includes organism, link and camera, the symmetric shaping has two hypotenuses on the link, the bottom of link has the bottom plate through two elastic connection of spring, it has the connecting rod of flange to run through the top shaping on the link, the inner chamber of link is equipped with the guide arm on the horizontal direction, the outside of guide arm is equipped with two spring one and two movable blocks, two the equal shaping in bottom of movable block has the inclined plane, install the gyro wheel with inclined plane looks butt on the bottom plate.
As a further description of the above technical solution:
the spring sleeve is arranged outside the connecting rod.
As a further description of the above technical solution:
the bottom plate is connected with a balancing weight through screw thread screwing.
As a further description of the above technical solution:
the lower surface wall of the bottom plate is bonded with a rubber pad.
As a further description of the above technical solution:
the connecting frame is fixedly connected with the machine body through a locking bolt.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:
1. the utility model discloses in, the outside at the connecting rod is established to the spring two, the both ends of spring two respectively with link and bottom plate butt, under the effect of spring one, two movable blocks are close to each other, the gyro wheel with the shaping at the inclined plane looks butt of movable block bottom, when unmanned aerial vehicle falls to the ground and strikes ground, spring one takes place deformation with spring two, played the shock attenuation effect of buffering, compare traditional unmanned aerial vehicle, the buffering effect is better, can effectually avoid unmanned aerial vehicle internals's damage.
2. The utility model discloses in, the upper surface wall of bottom plate has closed the balancing weight soon through the screw thread, and the balancing weight can effectually avoid unmanned aerial vehicle to take place to turn on one's side, has improved unmanned aerial vehicle's security, and the balancing weight is detachable with the bottom plate to be connected moreover, and the user can adjust the quantity of balancing weight as required, and adaptability is stronger.
Drawings
Fig. 1 shows a schematic structural diagram of an unmanned aerial vehicle provided according to an embodiment of the present invention;
fig. 2 shows a schematic structural diagram of a moving block provided according to an embodiment of the present invention;
fig. 3 shows according to the utility model discloses unmanned aerial vehicle looks sideways at the schematic diagram that provides.
Illustration of the drawings:
1. a body; 2. locking the bolt; 3. a guide bar; 4. a moving block; 5. a first spring; 6. a connecting frame; 7. a flange; 8. a connecting rod; 9. a base plate; 10. a balancing weight; 11. a roller; 12. a rubber pad; 13. a second spring; 14. a bevel; 15. a camera; 16. a beveled edge.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: a movable unmanned aerial vehicle for outdoor monitoring comprises a machine body 1, a connecting frame 6 and a camera 15, wherein the connecting frame 6 is fixedly connected with the machine body 1 through a locking bolt 2, a threaded hole screwed with the locking bolt 2 is formed in the side wall of the machine body 1, two inclined edges 16 are symmetrically formed on the connecting frame 6, a bottom plate 9 is elastically connected to the bottom of the connecting frame 6 through a second spring 13, a connecting rod 8 with a flange 7 formed at the top end penetrates through the connecting frame 6, the bottom end of the connecting rod 8 is fixedly connected with the bottom plate 9, the connecting rod 8 is in sliding fit with the connecting frame 6, a second spring 13 is sleeved outside the connecting rod 8, two ends of the second spring 13 are respectively abutted against the bottom plate 9 and the connecting frame 6, a guide rod 3 in the horizontal direction is arranged in an inner cavity of the connecting frame 6, the guide rod 3 is fixedly connected with the connecting frame 6, two first springs 5 and two movable blocks 4 are arranged outside the guide rod 3, under the action of the first spring 5, the two moving blocks 4 are close to each other, inclined planes 14 are formed at the bottoms of the two moving blocks 4, idler wheels 11 which are abutted to the inclined planes 14 are installed on the bottom plate 9, the idler wheels 11 extrude the inclined planes 14 in the process that the bottom plate 9 drives the idler wheels 11 to move upwards, and the first spring 5 deforms and can give a buffering force to the bottom plate 9.
Specifically, as shown in fig. 1, close soon through the screw thread on the bottom plate 9 and be connected with balancing weight 10, under the bad circumstances of weather, balancing weight 10 can effectually avoid unmanned aerial vehicle to take place to turn on one's side, has improved unmanned aerial vehicle's security, and the detachable connected mode that this kind of screw thread closed soon simultaneously, the user can adjust the quantity of balancing weight 10 as required, and adaptability is stronger.
Specifically, as shown in fig. 1, the lower surface wall of the bottom plate 9 is bonded with a rubber pad 12, the rubber pad 12 can play a certain buffering role, and meanwhile, the friction coefficient of the rubber pad 12 is large, so that the unmanned aerial vehicle can be effectively prevented from deviating, and the placing stability of the unmanned aerial vehicle is improved.
The working principle is as follows: when unmanned aerial vehicle falls to the ground and receives the impact, bottom plate 9 drives connecting rod 8 and takes place to remove, and spring two 13 takes place to deform, can give a cushion effect to unmanned aerial vehicle, and gyro wheel 11 extrudes inclined plane 14, and movable block 4 extrudees spring one 5, and spring one 5 takes place to deform, can give unmanned aerial vehicle a buffer effect again, under the effect of two buffers, has played absorbing effect, can effectually avoid the inside electronic components of unmanned aerial vehicle to take place to damage.
The above, only be the concrete implementation of the preferred embodiment 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, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (5)
1. The utility model provides a remove unmanned aerial vehicle for outdoor monitoring, includes organism (1), link (6) and camera (15), its characterized in that, the symmetric shaping has two hypotenuses (16) on link (6), the bottom of link (6) has bottom plate (9) through two (13) elastic connection of spring, it has connecting rod (8) of flange (7) to run through on link (6), the inner chamber of link (6) is equipped with guide arm (3) on the horizontal direction, the outside of guide arm (3) is equipped with two spring (5) and two movable block (4), two the bottom of movable block (4) all takes shape to have inclined plane (14), install gyro wheel (11) with inclined plane (14) looks butt on bottom plate (9).
2. A mobile drone for outdoor monitoring according to claim 1, characterised in that the second spring (13) is fitted on the outside of the connecting rod (8).
3. A mobile drone for outdoor monitoring according to claim 2, characterised in that the base plate (9) has a counterweight (10) screwed thereto.
4. A mobile drone for outdoor monitoring according to claim 3, characterised in that the lower surface wall of the floor (9) is glued with a rubber mat (12).
5. A mobile unmanned aerial vehicle for outdoor monitoring according to any of claims 1-4, wherein the link (6) is fixedly connected with the machine body (1) through a locking bolt (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022696203.2U CN214267949U (en) | 2020-11-20 | 2020-11-20 | A remove unmanned aerial vehicle for outdoor monitoring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022696203.2U CN214267949U (en) | 2020-11-20 | 2020-11-20 | A remove unmanned aerial vehicle for outdoor monitoring |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214267949U true CN214267949U (en) | 2021-09-24 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022696203.2U Active CN214267949U (en) | 2020-11-20 | 2020-11-20 | A remove unmanned aerial vehicle for outdoor monitoring |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214267949U (en) |
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2020
- 2020-11-20 CN CN202022696203.2U patent/CN214267949U/en active Active
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