CN221214660U - Unmanned aerial vehicle auxiliary take-off platform - Google Patents
Unmanned aerial vehicle auxiliary take-off platform Download PDFInfo
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- CN221214660U CN221214660U CN202323233510.7U CN202323233510U CN221214660U CN 221214660 U CN221214660 U CN 221214660U CN 202323233510 U CN202323233510 U CN 202323233510U CN 221214660 U CN221214660 U CN 221214660U
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- 230000007246 mechanism Effects 0.000 claims abstract description 12
- 238000005096 rolling process Methods 0.000 claims description 4
- 238000009434 installation Methods 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle auxiliary take-off platform, which comprises a base, universal wheels, a balance weight, a limiting block, a convex groove, a platform, a supporting rod, a connecting groove, a connecting rod, rollers and a windproof mechanism, wherein the base is provided with a plurality of guide rails; the utility model has reasonable and simple structure, low production cost, convenient installation and complete functions, and can effectively ensure the stability of the platform when the unmanned aerial vehicle takes off through the arranged balance weight, the limiting block, the convex groove, the platform, the supporting rod, the connecting groove, the connecting rod and the idler wheels; according to the utility model, the problem that wind affects the unmanned aerial vehicle greatly during take-off can be effectively guaranteed through the right baffle, the left baffle, the front baffle and the rear baffle.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle auxiliary take-off platform.
Background
The drone is a drone that is maneuvered with a radio remote control device and a self-contained programming device. Unmanned aerial vehicles are becoming more and more mature in development and wider in application field.
Now people can use unmanned aerial vehicle to shoot in order to shoot better scenery, and unmanned aerial vehicle is taking off, and ground unevenness leads to unmanned aerial vehicle unbalance, and then makes unmanned aerial vehicle can not fine take off, still easily by wind blow, and influence the effect of taking off, consequently research and development one kind can balance unmanned aerial vehicle and place, makes unmanned aerial vehicle fine take off, can also block wind simultaneously, makes the effect of taking off better, has consequently proposed an unmanned aerial vehicle auxiliary take off platform.
Disclosure of utility model
The utility model aims to solve the problems and provide an unmanned aerial vehicle auxiliary take-off platform, which solves the problems that in order to shoot better scenery, the unmanned aerial vehicle is used for shooting, and when the unmanned aerial vehicle takes off, the unmanned aerial vehicle is unbalanced due to uneven ground, so that the unmanned aerial vehicle cannot take off well, and is easy to be blown by wind to influence the take-off effect, so that the unmanned aerial vehicle can be placed in a balanced manner, the unmanned aerial vehicle can take off well, wind can be blocked, and the take-off effect is better.
In order to solve the problems, the utility model provides a technical scheme that: an unmanned aerial vehicle auxiliary take-off platform comprises a base, universal wheels, a balance block, a limiting block, a convex groove, a platform, a supporting rod, a connecting groove, a connecting rod, rollers and a windproof mechanism; universal wheels are fixedly connected to the periphery of the lower surface of the base; the upper end of the base is connected with a balance weight; limiting blocks are fixedly connected to two sides of the top end of the balance block; convex grooves are formed in the front side and the rear side of the top end of the balance block; the upper end of the balance block is provided with a platform; support rods are fixedly connected to the periphery of the bottom end of the platform; the bottom end of the supporting rod is provided with a connecting groove, two sides of the bottom end of the supporting rod are fixedly connected with connecting rods, and the idler wheels are connected to the connecting rods; the outer sides around the base are provided with windproof mechanisms.
Preferably, the convex groove is protruded by 1.2-1.3 cm.
Preferably, the roller is connected to the convex groove in a rolling way.
Preferably, the specific structure of the wind prevention mechanism is as follows: the device comprises a right baffle, a left baffle, a front baffle and a rear baffle; a right baffle is fixedly connected to the right side of the upper end of the base; a left baffle is fixedly connected to the left side of the upper end of the base; the front end of the base is connected with a front baffle, and the rear end of the base is connected with a rear baffle.
Preferably, the right baffle, the left baffle, the front baffle and the rear baffle are identical in height with each other.
Preferably, the front baffle and the rear baffle are detachable.
The utility model has the beneficial effects that:
(1) The utility model has reasonable and simple structure, low production cost, convenient installation and complete functions, and can effectively ensure the stability of the platform during the take-off of the unmanned aerial vehicle through the arranged balance weight, the limiting block, the convex groove, the platform, the supporting rod, the connecting groove, the connecting rod and the idler wheels.
(2) According to the utility model, the problem that wind affects the unmanned aerial vehicle greatly during take-off can be effectively guaranteed through the right baffle, the left baffle, the front baffle and the rear baffle.
Drawings
Fig. 1 is a schematic structural view of the present utility model.
Fig. 2 is a schematic view of a partial structure of the present utility model.
Fig. 3 is an overall schematic diagram of the balance weight of the present utility model.
FIG. 4 is an overall schematic view of the wind-break mechanism of the present utility model.
1-A base; 2-universal wheels; 3-balancing blocks; 4-limiting blocks; 5-convex grooves; 6-a platform; 7-supporting rods; 8-connecting grooves; 9-connecting rods; 10-rolling wheels; 11-a wind-prevention mechanism; 12-right baffle; 13-left baffle; 14-front baffle; 15-a tailgate.
Detailed Description
As shown in fig. 1 to 4, the present embodiment adopts the following technical scheme: an unmanned aerial vehicle auxiliary take-off platform comprises a base 1, universal wheels 2, a balance block 3, a limiting block 4, a convex groove 5, a platform 6, a supporting rod 7, a connecting groove 8, a connecting rod 9, a roller 10 and a windproof mechanism 11; universal wheels 2 are fixedly connected to the periphery of the lower surface of the base 1; the upper end of the base 1 is connected with a balance weight 3; limiting blocks 4 are fixedly connected to two sides of the top end of the balance weight 3; convex grooves 5 are formed in the front side and the rear side of the top end of the balance weight 3; the upper end of the balance weight 3 is provided with a platform 6; support rods 7 are fixedly connected to the periphery of the bottom end of the platform 6; the bottom end of the supporting rod 7 is provided with a connecting groove 8, two sides of the bottom end of the supporting rod 7 are fixedly connected with connecting rods 9, and the idler wheels 10 are connected to the connecting rods 9; the stability of the platform during the take-off of the unmanned aerial vehicle can be effectively ensured; the outer sides of the periphery of the base 1 are provided with windproof mechanisms 11.
Wherein the convex groove 5 is protruded by 1.2-1.3 cm; the roller 10 is connected to the convex groove 5 in a rolling way.
As shown in fig. 1 to 4, the specific structure of the wind prevention mechanism 11 is as follows: comprises a right baffle 12, a left baffle 13, a front baffle 14 and a rear baffle 15; the right side of the upper end of the base 1 is fixedly connected with a right baffle 12; the left side of the upper end of the base 1 is fixedly connected with a left baffle 13; the front end of the base 1 is connected with a front baffle 14, and the rear end of the base 1 is connected with a rear baffle 15, so that the problem that wind affects the unmanned aerial vehicle greatly during take-off can be effectively guaranteed.
Wherein the heights of the right baffle 12, the left baffle 13, the front baffle 14 and the rear baffle 15 are consistent with each other; the front baffle 14 and the rear baffle 15 are both detachable.
The use state of the utility model is as follows: the utility model has reasonable and simple structure, low production cost, convenient installation and complete functions, when in use, firstly, the take-off platform is pushed to be used, the unmanned aerial vehicle is placed on the platform 6, when the ground is uneven, the self-balancing treatment can be carried out through the balance weight 3, the limiting block 4, the convex groove 5, the platform 6, the supporting rod 7, the connecting groove 8, the connecting rod 9 and the roller 10 which are arranged below, and when the take-off wind speed is high, the wind shielding treatment can be carried out through the right baffle 12, the left baffle 13, the front baffle 14 and the rear baffle 15 which are arranged.
In the description of the present utility model, it should be understood that the terms "coaxial," "bottom," "one end," "top," "middle," "another end," "upper," "one side," "top," "inner," "front," "center," "two ends," etc. indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model.
In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "configured," "connected," "secured," "screwed," and the like are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intermediaries, or in communication with each other or in interaction with each other, unless explicitly defined otherwise, the meaning of the terms described above in this application will be understood by those of ordinary skill in the art in view of the specific circumstances.
While the basic principles and main features of the present utility model and advantages of the present utility model have been shown and described, it will be understood by those skilled in the art that the present utility model is not limited by the foregoing embodiments, which are described in the foregoing specification merely illustrate the principles of the present utility model, and various changes and modifications may be made therein without departing from the spirit and scope of the utility model, which is defined in the appended claims and their equivalents.
The control mode of the utility model is controlled by manually starting and closing the switch, the wiring diagram of the power element and the supply of the power supply are common knowledge in the field, and the utility model is mainly used for protecting the mechanical device, so the utility model does not explain the control mode and the wiring arrangement in detail.
Claims (6)
1. An unmanned aerial vehicle auxiliary take-off platform which is characterized in that: the anti-wind device comprises a base (1), universal wheels (2), a balance block (3), a limiting block (4), a convex groove (5), a platform (6), a supporting rod (7), a connecting groove (8), a connecting rod (9), a roller (10) and a wind-proof mechanism (11);
Universal wheels (2) are fixedly connected to the periphery of the lower surface of the base (1);
The upper end of the base (1) is fixedly connected with a balance weight (3);
limiting blocks (4) are fixedly connected to two sides of the top end of the balance block (3);
convex grooves (5) are formed in the front side and the rear side of the top end of the balance block (3);
the upper end of the balance block (3) is provided with a platform (6);
The periphery of the bottom end of the platform (6) is fixedly connected with a supporting rod (7);
The bottom end of the supporting rod (7) is provided with a connecting groove (8), two sides of the bottom end of the supporting rod (7) are fixedly connected with connecting rods (9), and the idler wheels (10) are connected to the connecting rods (9);
wind-proof mechanisms (11) are arranged on the outer sides of the periphery of the base (1).
2. The unmanned aerial vehicle assisted take-off platform of claim 1, wherein: the height of the convex groove (5) is 1.2-1.3 cm.
3. The unmanned aerial vehicle assisted take-off platform of claim 1, wherein: the roller (10) is connected to the convex groove (5) in a rolling way.
4. The unmanned aerial vehicle assisted take-off platform of claim 1, wherein: the specific structure of the windproof mechanism (11) is as follows: comprises a right baffle (12), a left baffle (13), a front baffle (14) and a rear baffle (15);
the right side of the upper end of the base (1) is fixedly connected with a right baffle (12);
A left baffle (13) is fixedly connected to the left side of the upper end of the base (1);
the front end of the base (1) is connected with a front baffle (14), and the rear end of the base (1) is connected with a rear baffle (15).
5. The unmanned aerial vehicle assisted take-off platform of claim 4, wherein: the heights of the right baffle (12), the left baffle (13), the front baffle (14) and the rear baffle (15) are consistent with each other.
6. The unmanned aerial vehicle assisted take-off platform of claim 4, wherein: the front baffle (14) and the rear baffle (15) are detachable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323233510.7U CN221214660U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle auxiliary take-off platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323233510.7U CN221214660U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle auxiliary take-off platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221214660U true CN221214660U (en) | 2024-06-25 |
Family
ID=91567786
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323233510.7U Active CN221214660U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle auxiliary take-off platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221214660U (en) |
-
2023
- 2023-11-29 CN CN202323233510.7U patent/CN221214660U/en active Active
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