CN220562978U - Unmanned aerial vehicle landing platform for atmosphere detection - Google Patents
Unmanned aerial vehicle landing platform for atmosphere detection Download PDFInfo
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- CN220562978U CN220562978U CN202322149173.7U CN202322149173U CN220562978U CN 220562978 U CN220562978 U CN 220562978U CN 202322149173 U CN202322149173 U CN 202322149173U CN 220562978 U CN220562978 U CN 220562978U
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- 238000001514 detection method Methods 0.000 title claims abstract description 18
- 239000000872 buffer Substances 0.000 claims description 13
- 230000000694 effects Effects 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 claims description 2
- 230000000630 rising effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicle platforms, and provides an unmanned aerial vehicle landing platform for atmosphere detection, which comprises three bottom pipes, wherein the number of the bottom pipes is three; the lifting mechanism is arranged on the bottom pipe; the adjusting and supporting mechanism is arranged on the bottom pipe and comprises an adjusting and supporting component, a moving component and a limiting component; wherein, adjust the supporting component and including the stay tube. According to the utility model, the rotating block, the threaded rod and the pointed head are arranged, and the rotating block is sequentially rotated, so that the convex ring rotates along the inner wall of the bottom pipe, the rotating block drives the side block to move downwards along the inner wall of the side opening through the threaded rod, and the threaded rod drives the pointed head to move downwards to adjust the whole length of each bottom pipe until the whole lower platform is positioned horizontally, and the purpose of horizontally placing the landing unmanned aerial vehicle on different grounds is achieved; through above-mentioned technical scheme, solve the unable horizontal unmanned aerial vehicle problem of placing of different ground among the prior art.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle platforms, in particular to an unmanned aerial vehicle landing platform for atmosphere detection.
Background
At present, operating personnel often need use unmanned aerial vehicle auxiliary detection when detecting the atmosphere, because the detection area environment is comparatively abominable, and unmanned aerial vehicle is higher to the requirement of landing environment, thereby need be equipped with corresponding landing platform and accomplish unmanned aerial vehicle's lift, and current landing platform is mostly by landing plate and support frame constitution, when landing platform is on uneven subaerial use, be difficult to guarantee that the landing plate is in the horizontality, and then can lead to unmanned aerial vehicle landing unstable, thereby there is the risk of crash when probably making unmanned aerial vehicle land, consequently need improve it.
Disclosure of Invention
The utility model provides an unmanned aerial vehicle landing platform for atmosphere detection, which solves the problem that different floors in the related art cannot horizontally place a landing unmanned aerial vehicle.
The technical scheme of the utility model is as follows: an unmanned aerial vehicle landing platform for atmosphere detection comprises
The number of the bottom pipes is three;
the lifting mechanism is arranged on the bottom pipe;
the adjusting and supporting mechanism is arranged on the bottom pipe and comprises an adjusting and supporting component, a moving component and a limiting component;
the adjusting support assembly comprises a support tube, a pointed head is movably sleeved in the support tube, and the pointed head moves to the outside of the support tube through the moving assembly.
As a preferable technical scheme of the utility model, the moving assembly comprises a rotating block, a threaded rod and a convex ring;
the bottom of rotatory piece and the top fixed connection of stay tube, the surface of protruding type ring cup joints with the inner wall activity of end pipe, the lower extreme and the rotatory piece fixed connection of protruding type ring, the surface of threaded rod cup joints with the inner wall screw thread of rotatory piece, the upper end of threaded rod extends to the inside of end pipe, the lower extreme and the tip fixed connection of threaded rod.
As a preferable technical scheme of the utility model, the limiting component comprises a side opening and a side block;
the side port is arranged in the bottom tube, the inner wall of the side port is movably sleeved with the outer surface of the side block, and the side surface of the side block is fixedly connected with the outer surface of the threaded rod.
As a preferable technical scheme of the utility model, the lifting mechanism comprises a buffer component, a protection component and a placement component;
the placing component comprises a lower platform, a connecting rod and an upper platform;
the bottom of lower platform and the top fixed connection of bottom tube, the surface of connecting rod cup joints with the inner wall activity of lower platform, the upper end and the upper platform fixed connection of connecting rod, buffer unit passes through the connecting rod and buffers upper platform.
As a preferable technical scheme of the utility model, the buffer component comprises a stop block and a rigid spring;
the top of dog and the bottom fixed connection of connecting rod, the one end of stiff spring and the bottom fixed connection of lower platform, the other end of stiff spring and dog fixed connection.
As a preferable technical scheme of the utility model, the protection component comprises a first rubber block and a second rubber block;
the bottom of first rubber piece and the top fixed connection of upper table, the top of second rubber piece and the bottom fixed connection of first rubber piece, the internal surface of second rubber piece cup joints with the surface activity of lower table, the surface of second rubber piece and first rubber piece is soft.
As a preferable technical scheme of the utility model, the outer surface of the rotating block is fixedly provided with the convex blocks in annular equidistant mode, and the convex blocks have rough outer surfaces.
As a preferable technical scheme of the utility model, the first rubber block is fixedly sleeved with the marking block, and the marking block is made of reflective materials.
The working principle and the beneficial effects of the utility model are as follows:
1. according to the utility model, the rotating block, the threaded rod and the pointed head are arranged, and the rotating block is sequentially rotated, so that the convex ring rotates along the inner wall of the bottom pipe, the rotating block drives the side block to move downwards along the inner wall of the side opening through the threaded rod, and the threaded rod drives the pointed head to move downwards to adjust the whole length of each bottom pipe until the whole lower platform is positioned horizontally, and the purpose of horizontally placing the landing unmanned aerial vehicle on different grounds is achieved.
2. According to the utility model, the rigid springs, the first rubber blocks and the second rubber blocks are arranged, so that the first rubber blocks and the second rubber blocks can protect the top and the outer side of the platform due to the design of the first rubber blocks and the second rubber blocks, the second rubber blocks and the first rubber blocks can further protect against the unmanned aerial vehicle on the top or the outer side of the platform, and then the upper platform can buffer and protect the unmanned aerial vehicle falling on the first rubber blocks through the rigid springs, the connecting rods and the check blocks, so that the impact force generated when the unmanned aerial vehicle falls is reduced, and the purpose of protecting the unmanned aerial vehicle is achieved.
Drawings
The utility model will be described in further detail with reference to the drawings and the detailed description.
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic view of the bottom structure of the present utility model;
FIG. 3 is a schematic side cross-sectional view of the present utility model;
FIG. 4 is a schematic side cross-sectional view of a bottom tube of the present utility model;
fig. 5 is a schematic view of a partial enlarged structure at a in fig. 4.
In the figure: 1. a bottom tube; 2. a lower platform; 3. a male ring; 4. a rotating block; 5. a support tube; 6. a threaded rod; 7. a tip; 8. a side port; 9. a bump; 10. a side block; 11. a connecting rod; 12. a stop block; 13. a rigid spring; 14. a top platform; 15. a first rubber block; 16. marking the block; 17. and a second rubber block.
Detailed Description
The technical solutions of the embodiments of the present utility model will be clearly and completely described below in conjunction with the embodiments of the present utility model, and it is apparent that the described embodiments are only some embodiments of the present utility model, not all embodiments. All other embodiments, which can be made by one of ordinary skill in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Example 1
As shown in fig. 1-2, this embodiment provides an unmanned aerial vehicle landing platform for atmosphere detection, including
A bottom pipe 1, the number of which is three;
a lifting mechanism arranged on the bottom pipe 1;
the adjusting and supporting mechanism is arranged on the bottom tube 1 and comprises an adjusting and supporting component, a moving component and a limiting component;
wherein, adjust the supporting component and including stay tube 5, the inside activity of stay tube 5 cup joints tip 7, and tip 7 moves to the outside of stay tube 5 through the removal subassembly.
In this embodiment, through moving the subassembly to will make tip 7 take place to move down and insert in earth, and increase the holistic length of bottom tube 1, make the whole level that is located of lower platform 2 through adjusting the holistic length of bottom tube 1 in proper order afterwards, then alright place unmanned aerial vehicle on the mechanism of rising and falling rise and detect the atmosphere, thereby reached different ground levels and placed the purpose of rising and falling unmanned aerial vehicle.
Example 2
As shown in fig. 5, based on the same concept as the above embodiment 1, the present embodiment also proposes that the moving assembly includes a rotating block 4 and a threaded rod 6 and a male ring 3;
the bottom of rotatory piece 4 and the top fixed connection of stay tube 5, the surface of protruding type ring 3 cup joints with the inner wall activity of end pipe 1, the lower extreme and the rotatory piece 4 fixed connection of protruding type ring 3, the surface of threaded rod 6 cup joints with the inner wall screw thread of rotatory piece 4, the upper end of threaded rod 6 extends to the inside of end pipe 1, the lower extreme and the tip 7 fixed connection of threaded rod 6.
In this embodiment, the rotating block 4 is rotated, so that the convex ring 3 rotates along the inner wall of the bottom tube 1, and the rotating block 4 drives the pointed head 7 to move through the threaded rod 6.
Example 3
As shown in fig. 2, based on the same concept as that of the above embodiment 1, the present embodiment also proposes that the limiting assembly includes a side opening 8 and a side block 10;
the side port 8 is arranged in the bottom tube 1, the inner wall of the side port 8 is movably sleeved with the outer surface of the side block 10, and the side surface of the side block 10 is fixedly connected with the outer surface of the threaded rod 6.
In this embodiment, through the design of the side opening 8 and the side block 10, when the threaded rod 6 drives the tip 7 to move, the side block 10 will limit the threaded rod 6 through the side opening 8 at this time, so that the threaded rod 6 can only drive the tip 7 to move up and down.
Example 4
As shown in fig. 3, based on the same concept as that of the above embodiment 1, this embodiment also proposes that the landing gear includes a buffer assembly and a protection assembly and placement assembly;
the placing component comprises a lower platform 2, a connecting rod 11 and an upper platform 14;
the bottom of lower platform 2 and the top fixed connection of bottom tube 1, the surface of connecting rod 11 cup joints with the inner wall activity of lower platform 2, and the upper end and the upper platform 14 fixed connection of connecting rod 11, buffer assembly passes through connecting rod 11 and buffers upper platform 14.
In this embodiment, through the design of stiff spring 13 to make upper platform 14 through connecting rod 11 and buffer module to the unmanned aerial vehicle who falls at carry out buffer protection, and make the protection of protection subassembly collide the unmanned aerial vehicle in this platform top or the outside, thereby reduced the impact force that unmanned aerial vehicle produced when descending, and then reached the purpose of protection unmanned aerial vehicle.
Example 5
As shown in fig. 3, based on the same concept as embodiment 1 described above, this embodiment also proposes that the damper assembly includes a stopper 12 and a stiff spring 13;
the top of dog 12 and the bottom fixed connection of connecting rod 11, the one end of stiff spring 13 and the bottom fixed connection of lower platform 2, the other end of stiff spring 13 and dog 12 fixed connection.
In this embodiment, the rigid spring 13 and the stop 12 are designed, so that the rigid spring 13 elastically resets the connecting rod 11 through the stop 12.
Example 6
As shown in fig. 3, based on the same concept as embodiment 1 described above, this embodiment also proposes that the protective assembly comprises a first rubber block 15 and a second rubber block 17;
the bottom of the first rubber block 15 is fixedly connected with the top of the upper platform 14, the top of the second rubber block 17 is fixedly connected with the bottom of the first rubber block 15, the inner surface of the second rubber block 17 is movably sleeved with the outer surface of the lower platform 2, and the outer surfaces of the second rubber block 17 and the first rubber block 15 are soft.
In this embodiment, by designing the second rubber block 17 and the first rubber block 15, the first rubber block 15 and the second rubber block 17 will protect the top and the outer side of the platform, and the second rubber block 17 and the first rubber block 15 will protect the unmanned aerial vehicle colliding with the top or the outer side of the platform.
Example 7
As shown in fig. 1, based on the same concept as that of the above embodiment 1, this embodiment also proposes that the outer surface of the rotating block 4 is fixedly installed with the bumps 9 annularly equidistant, and the outer surface of the bumps 9 is rough.
In this embodiment, through the design of lug 9 to make the operating personnel be difficult to the hand when rotatory piece 4 skidded, and then make operating personnel at rotatory piece 4 more convenient.
Example 8
As shown in fig. 3, based on the same concept as that of the above embodiment 1, this embodiment also proposes that the first rubber block 15 is fixedly sleeved with the marking block 16, and the marking block 16 is made of a reflective material.
In this embodiment, the design of the marking block 16 makes it easier for the unmanned aerial vehicle to determine the position of the platform for falling through the reflection of light of the marking block 16.
The working principle and the using flow of the utility model are as follows:
when using on level ground, operating personnel can stay tube 5 place ground directly and wholly carry out the level to lower platform 2 and place, when using on uneven ground, operating personnel is through rotatory piece 4 this moment, thereby will make protruding ring 3 take place to rotate along the inner wall of bottom tube 1, and then make rotatory piece 4 drive side piece 10 through threaded rod 6 and take place to move down along the inner wall of side mouth 8, thereby will make threaded rod 6 drive tip 7 take place to move down and insert in earth, then operating personnel adjusts the whole length of bottom tube 1 through rotatory piece 4 in proper order, until stopping when making lower platform 2 wholly be located the level, then operating personnel alright place unmanned aerial vehicle and rise the detection atmosphere on first rubber piece 15, thereby the purpose of different ground level placements unmanned aerial vehicle has been reached.
Then when unmanned aerial vehicle descends, unmanned aerial vehicle can confirm the position of first rubber piece 15 through the reflection of light of mark piece 16 more easily and drop this moment, because the design of first rubber piece 15 and second rubber piece 17, thereby will make this platform top of first rubber piece 15 and second rubber piece 17 protection and outside, and then make the unmanned aerial vehicle of this platform top or outside of second rubber piece 17 and first rubber piece 15 protection bump, go up platform 14 and connecting rod 11 and dog 12 and carry out the buffering protection to the unmanned aerial vehicle who descends on first rubber piece 15 through stiff spring 13 afterwards, thereby the impact force that produces when having reduced unmanned aerial vehicle and having reached the purpose of protection unmanned aerial vehicle.
The foregoing description of the preferred embodiments of the utility model is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the utility model.
Claims (8)
1. The unmanned aerial vehicle landing platform for atmosphere detection is characterized by comprising
A bottom pipe (1) with three numbers;
the lifting mechanism is arranged on the bottom pipe (1);
the adjusting and supporting mechanism is arranged on the bottom pipe (1) and comprises an adjusting and supporting component, a moving component and a limiting component;
the adjusting support assembly comprises a support tube (5), a pointed end (7) is movably sleeved in the support tube (5), and the pointed end (7) moves to the outside of the support tube (5) through the moving assembly.
2. The unmanned aerial vehicle landing platform for atmosphere detection according to claim 1, wherein: the moving assembly comprises a rotating block (4), a threaded rod (6) and a convex ring (3);
the bottom of rotatory piece (4) and the top fixed connection of stay tube (5), the surface of protruding type ring (3) cup joints with the inner wall activity of end pipe (1), the lower extreme and the rotatory piece (4) fixed connection of protruding type ring (3), the surface of threaded rod (6) cup joints with the inner wall screw thread of rotatory piece (4), the inside of end pipe (1) is extended to the upper end of threaded rod (6), the lower extreme and the tip (7) fixed connection of threaded rod (6).
3. The unmanned aerial vehicle landing platform for atmosphere detection according to claim 1, wherein: the limiting assembly comprises a side opening (8) and a side block (10);
the side opening (8) is arranged in the bottom tube (1), the inner wall of the side opening (8) is movably sleeved with the outer surface of the side block (10), and the side surface of the side block (10) is fixedly connected with the outer surface of the threaded rod (6).
4. The unmanned aerial vehicle landing platform for atmosphere detection according to claim 1, wherein: the lifting mechanism comprises a buffer component, a protection component and a placement component;
the placing component comprises a lower platform (2), a connecting rod (11) and an upper platform (14);
the bottom of lower platform (2) is fixedly connected with the top of bottom tube (1), the surface of connecting rod (11) cup joints with the inner wall activity of lower platform (2), the upper end and the upper platform (14) fixed connection of connecting rod (11), and buffer assembly passes through connecting rod (11) to upper platform (14) buffering.
5. The unmanned aerial vehicle landing platform for atmosphere detection according to claim 4, wherein: the buffer assembly comprises a stop block (12) and a rigid spring (13);
the top of dog (12) and the bottom fixed connection of connecting rod (11), the one end of stiff spring (13) and the bottom fixed connection of lower platform (2), the other end of stiff spring (13) and dog (12) fixed connection.
6. The unmanned aerial vehicle landing platform for atmosphere detection according to claim 4, wherein: the protection assembly comprises a first rubber block (15) and a second rubber block (17);
the bottom of first rubber piece (15) and the top fixed connection of upper platform (14), the top of second rubber piece (17) and the bottom fixed connection of first rubber piece (15), the internal surface of second rubber piece (17) cup joints with the surface activity of lower platform (2), the surface of second rubber piece (17) and first rubber piece (15) is soft.
7. The unmanned aerial vehicle landing platform for atmosphere detection according to claim 2, wherein: the outer surface of the rotating block (4) is fixedly provided with protruding blocks (9) in annular equidistant mode, and the protruding blocks (9) are rough in appearance.
8. The unmanned aerial vehicle landing platform for atmosphere detection according to claim 6, wherein: the inside of first rubber piece (15) is fixed to be cup jointed mark piece (16), mark piece (16) adopt reflection of light material to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322149173.7U CN220562978U (en) | 2023-08-10 | 2023-08-10 | Unmanned aerial vehicle landing platform for atmosphere detection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322149173.7U CN220562978U (en) | 2023-08-10 | 2023-08-10 | Unmanned aerial vehicle landing platform for atmosphere detection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220562978U true CN220562978U (en) | 2024-03-08 |
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ID=90089791
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322149173.7U Active CN220562978U (en) | 2023-08-10 | 2023-08-10 | Unmanned aerial vehicle landing platform for atmosphere detection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220562978U (en) |
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2023
- 2023-08-10 CN CN202322149173.7U patent/CN220562978U/en active Active
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