CN215043800U - Unmanned aerial vehicle sliding landing platform with vibration alignment mechanism - Google Patents
Unmanned aerial vehicle sliding landing platform with vibration alignment mechanism Download PDFInfo
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- CN215043800U CN215043800U CN202121088586.3U CN202121088586U CN215043800U CN 215043800 U CN215043800 U CN 215043800U CN 202121088586 U CN202121088586 U CN 202121088586U CN 215043800 U CN215043800 U CN 215043800U
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Abstract
The utility model discloses an unmanned aerial vehicle smooth platform that falls with vibrations counterpoint mechanism, including the platform lower floor, the round hole has been seted up at platform lower floor's top, still including: the platform upper strata, platform upper strata swing joint is in platform lower floor top to carry out preliminary counterpoint to unmanned aerial vehicle. The utility model discloses in, during the use, because platform upper strata surface is smooth platform, and be narrow frustum type under wide, can counterpoint for the first time through the platform upper strata, platform lower floor's four corners is through installing spring mechanism additional, insert the spring through beating the round hole, put the platform on upper strata, insert small-size fixed column, through vibrating motor control vibration, through installing spring mechanism additional, make the vibration more smooth, unmanned aerial vehicle counterpoints more accurately, the follow-up use for unmanned aerial vehicle smooth landing platform provides convenience, and then the result of use of current unmanned aerial vehicle smooth landing platform has been improved.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle smooth platform that falls with vibrations counterpoint mechanism.
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.
At present, current unmanned aerial vehicle smooth landing platform still has the weak point, and when current unmanned aerial vehicle descended, the position of descending was not accurate, influences unmanned aerial vehicle's follow-up charging and originated slip, and then has reduced the result of use of current unmanned aerial vehicle smooth landing platform.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: in order to solve the problems, the unmanned aerial vehicle sliding landing platform with the vibration alignment mechanism is provided.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle smooth platform that falls with vibrations counterpoint mechanism, includes the platform lower floor, the round hole has been seted up at platform lower floor's top, still including:
the upper platform layer is movably connected above the lower platform layer so as to carry out preliminary alignment on the unmanned aerial vehicle;
vibrations portion, vibrations portion fixes on platform lower floor to make unmanned aerial vehicle counterpoint more accurate.
As a further description of the above technical solution:
the vibration part comprises a vibration motor and a spring, the top of the vibration motor is fixedly connected with the bottom of the lower layer of the platform, the spring is arranged between the upper layer of the platform and the lower layer of the platform, the bottom of the spring is inserted into the round hole, a fixing column is inserted into the spring, and the bottom of the fixing column is connected with the inside of the round hole in a screwing mode.
As a further description of the above technical solution:
the fixed column penetrates through the upper layer of the platform.
As a further description of the above technical solution:
the bottom of the fixed column is connected with the inside of the round hole in a screwing mode through a thread groove.
As a further description of the above technical solution:
the bottom surface of the upper layer of the platform is of a trapezoidal structure.
As a further description of the above technical solution:
and an anticorrosive coating is coated on the outer surface wall of the upper layer of the platform.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:
the utility model discloses in, during the use, because platform upper strata surface is smooth platform, and be narrow frustum type under wide, can counterpoint for the first time through the platform upper strata, platform lower floor's four corners is through installing spring mechanism additional, insert the spring through beating the round hole, put the platform on upper strata, insert small-size fixed column, through vibrating motor control vibration, through installing spring mechanism additional, make the vibration more smooth, unmanned aerial vehicle counterpoints more accurately, the follow-up use for unmanned aerial vehicle smooth landing platform provides convenience, and then the result of use of current unmanned aerial vehicle smooth landing platform has been improved.
Drawings
Fig. 1 shows a schematic cross-sectional structure provided according to an embodiment of the present invention;
fig. 2 shows a schematic top view structure provided according to an embodiment of the present invention;
fig. 3 shows a schematic diagram of a partially enlarged structure at a in fig. 1 according to an embodiment of the present invention.
Illustration of the drawings:
1. a platform lower layer; 2. a circular hole; 3. a vibration motor; 4. a platform upper layer; 5. fixing a column; 6. a spring.
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: the utility model provides an unmanned aerial vehicle smooth platform that falls with vibrations counterpoint mechanism, includes platform lower floor 1, and round hole 2 has been seted up at platform lower floor 1 top, still including:
the upper platform layer 4 is movably connected above the lower platform layer 1 so as to carry out preliminary alignment on the unmanned aerial vehicle;
vibrations portion, vibrations portion fix on platform lower floor 1 to make unmanned aerial vehicle counterpoint more accurate.
Specifically, as shown in fig. 1, vibrations portion is including vibrating motor 3 and spring 6, and vibrating motor 3 top and 1 bottom fixed connection of platform lower floor, and spring 6 locate between platform upper strata 4 and the 1 of platform lower floor, and pegs graft inside round hole 2 spring 6 bottom, and 6 inside pegs graft of spring have fixed column 5, and fixed column 5 bottom and 2 inside spiral closures of round hole are connected, further counterpoint unmanned aerial vehicle.
Specifically, as shown in fig. 3, the fixing column 5 penetrates through the upper platform layer 4, so that the spring 6 drives the upper platform layer 4 to vibrate.
Specifically, as shown in fig. 1, the bottom of the fixing column 5 is screwed with the inside of the circular hole 2 through a thread groove, and the upper layer 4 of the platform can be fixed when the fixing column is not used.
Specifically, as shown in fig. 2, 4 bottom surfaces on the platform upper strata are trapezium structure, and the length on two trapezoidal upper and lower bases is confirmed according to specific unmanned aerial vehicle model, and the position at four angles on air park has four sunkenly, just in time can block four angles of unmanned aerial vehicle, and this is that the unmanned aerial vehicle of special for having four feet sets up, if unmanned aerial vehicle's bottom is the crossbar type, just cancel four recesses, 4 surfaces on the platform upper strata are smooth planes, the unmanned aerial vehicle's of being convenient for preliminary counterpoint.
Specifically, as shown in fig. 2, an anticorrosive coating is coated on the outer surface wall of the platform upper layer 4 to protect the platform upper layer 4 and prolong the service life.
The working principle is as follows: during the use, because 4 surfaces on platform upper strata are smooth platform, and be the frustum type of narrow down about wide, can counterpoint through platform upper strata 4 for the first time, 1 four corners on platform lower floor is through installing spring mechanism additional, insert spring 6 through beating round hole 2, put the platform on upper strata, insert small-size fixed column 5, through vibrating motor 3 control vibration, through installing spring mechanism additional, make the vibration more smooth, unmanned aerial vehicle counterpoints more accurately, the follow-up use for unmanned aerial vehicle smooth landing platform provides convenience, and then the result of use of current unmanned aerial vehicle smooth landing platform has been improved.
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 (6)
1. The utility model provides an unmanned aerial vehicle smooth platform that falls with vibrations counterpoint mechanism, includes the platform lower floor, its characterized in that, the round hole has been seted up at platform lower floor's top, still including:
the upper platform layer is movably connected above the lower platform layer so as to carry out preliminary alignment on the unmanned aerial vehicle;
vibrations portion, vibrations portion fixes on platform lower floor to make unmanned aerial vehicle counterpoint more accurate.
2. The unmanned aerial vehicle sliding platform with the vibration aligning mechanism according to claim 1, wherein the vibration portion comprises a vibration motor and a spring, the top of the vibration motor is fixedly connected with the bottom of the lower layer of the platform, the spring is arranged between the upper layer of the platform and the lower layer of the platform, the bottom of the spring is inserted into the circular hole, a fixed column is inserted into the spring, and the bottom of the fixed column is screwed with the inside of the circular hole.
3. The unmanned aerial vehicle sliding platform with the vibration aligning mechanism according to claim 2, wherein the fixing column is arranged in the upper layer of the platform in a penetrating manner.
4. The unmanned aerial vehicle sliding platform with the vibration aligning mechanism according to claim 2, wherein the bottom of the fixed column is connected with the inside of the circular hole in a screwing manner through a thread groove.
5. The sliding landing platform with the vibration aligning mechanism for the unmanned aerial vehicle as claimed in claim 1, wherein the bottom surface of the upper layer of the platform is of a trapezoidal structure.
6. The unmanned aerial vehicle sliding platform with the vibration aligning mechanism according to claim 1, wherein an anti-corrosion coating is coated on the outer surface wall of the platform upper layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121088586.3U CN215043800U (en) | 2021-05-20 | 2021-05-20 | Unmanned aerial vehicle sliding landing platform with vibration alignment mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121088586.3U CN215043800U (en) | 2021-05-20 | 2021-05-20 | Unmanned aerial vehicle sliding landing platform with vibration alignment mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215043800U true CN215043800U (en) | 2021-12-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121088586.3U Active CN215043800U (en) | 2021-05-20 | 2021-05-20 | Unmanned aerial vehicle sliding landing platform with vibration alignment mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215043800U (en) |
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2021
- 2021-05-20 CN CN202121088586.3U patent/CN215043800U/en active Active
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