CN220535989U - Unmanned aerial vehicle landing platform - Google Patents
Unmanned aerial vehicle landing platform Download PDFInfo
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- CN220535989U CN220535989U CN202322260019.7U CN202322260019U CN220535989U CN 220535989 U CN220535989 U CN 220535989U CN 202322260019 U CN202322260019 U CN 202322260019U CN 220535989 U CN220535989 U CN 220535989U
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- 239000011248 coating agent Substances 0.000 claims description 6
- 238000000576 coating method Methods 0.000 claims description 6
- 238000000034 method Methods 0.000 abstract description 5
- 238000012876 topography Methods 0.000 abstract description 3
- 238000003780 insertion Methods 0.000 description 6
- 230000037431 insertion Effects 0.000 description 6
- 238000013507 mapping Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
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- 230000004048 modification Effects 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The application discloses unmanned aerial vehicle landing platform, including the take-off and landing plate, take-off and landing plate side is provided with the pterygoid lamina, and the take-off and landing plate passes through coupling assembling and is connected with the telescopic link, and the take-off and landing plate upper surface is provided with the liquid pipe, and the liquid pipe includes transparent shell, and transparent shell side mark has horizontal scale mark, is equipped with liquid in the transparent shell; the pterygoid lamina that take off and land board side was connected can be used to extend the surface of taking off and land board and extend, have the telescopic link to be used for propping up the take off and land board, the telescopic link can be used to adjust take off and land board height and make the take off and land board be higher than ground for adapt to various topography of taking off and land, through the length of adjusting each telescopic link, can adjust the levelness of taking off and land board, further, the liquid pipe is used for the calibration to take off and land board planarization, and then guarantee the levelness of taking off and land board, guarantee unmanned aerial vehicle's take off and land gesture level, with guarantee unmanned aerial vehicle take off and land stability, reduce the risk that takes off and land in-process accident and accident take place.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle landing platform.
Background
Unmanned aerial vehicles are unmanned aerial vehicles that are operated by means of a radio remote control device and a self-contained program control device, or are operated by a computer either fully or intermittently autonomously.
A mapping drone is a type of drone used for mapping and geographic information system applications. It may be equipped with mapping equipment such as cameras, lidar etc. for collecting ground data. Mapping unmanned aerial vehicles typically have longer flight times, greater load capacities, and greater accuracy, and can quickly acquire large amounts of geographic data in a shorter time.
In actual unmanned aerial vehicle survey and drawing, rotor unmanned aerial vehicle and perpendicular take off and land unmanned aerial vehicle when field operation, the field bottom surface condition is complicated, takes off and land the stage, needs a horizontal platform that has certain area to be used for guaranteeing unmanned aerial vehicle's take off and land gesture level to guarantee unmanned aerial vehicle take off and land's stability, reduce the risk that takes off and land in-process accident and unexpected emergence, and then ensure that the accurate surveying and drawing instrument on the unmanned aerial vehicle is not impaired inefficacy.
Disclosure of Invention
The utility model provides an unmanned aerial vehicle landing platform which is used for guaranteeing the landing posture level of an unmanned aerial vehicle and improving the stability of taking off and landing of the unmanned aerial vehicle.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
the utility model provides an unmanned aerial vehicle landing platform, includes the take-off and landing plate, take-off and landing plate side is provided with the pterygoid lamina, the take-off and landing plate passes through coupling assembling and is connected with the telescopic link, take-off and landing plate upper surface is provided with the liquid pipe, the liquid pipe includes transparent shell, transparent shell side mark has the horizontal scale mark, the liquid is filled in the transparent shell.
In an embodiment of the application, coupling assembling includes the pivot, the pivot rotates with the take-off and landing board to be connected, the pivot is connected with the telescopic link, pivot one side is provided with the fixed block, be provided with the screw hole on the fixed block, the screw hole is provided with the screw, the draw-in groove has been seted up on the pivot surface.
In one embodiment of the application, the lifting plate side is provided with a first jack, the wing plate side is provided with a plug, and the first jack is plugged with the plug for detachable connection of the wing plate and the lifting plate.
In an embodiment of the present application, the lifting plate upper surface is provided with a second jack.
In an embodiment of the present application, a plurality of indicator lights are mounted on the wing plate.
In an embodiment of the application, the pterygoid lamina surface mounting has the photovoltaic board, take off and land the board bottom surface and be provided with the battery, photovoltaic board and battery electric connection.
In one embodiment of the present application, the landing plate surface is coated with a buffer coating.
The beneficial effects of this application lie in: the wing plates connected with the side edges of the lifting plates can be used for extending and expanding the surfaces of the lifting plates, can also be used for installing and placing functional components, and is beneficial to improving the comprehensive use function of the lifting plates. The telescopic link is used for propping up the take-off and landing plate, and the telescopic link can be used for adjusting the take-off and landing plate height and make the take-off and landing plate be higher than ground for adaptation, shallow water, muddy ground, soft grassland take-off topography, preferably, the telescopic link can be used for electric telescopic link, can adjust the levelness of take-off and landing plate through the length of adjusting each telescopic link, and further, the liquid pipe is used for the calibration to take-off and landing plate planarization, and then guarantees the levelness of take-off and landing plate, guarantees unmanned aerial vehicle's take-off and landing gesture level, in order to guarantee unmanned aerial vehicle take-off and landing stability, reduce the risk that takes-off and landing in-process accident and accident take-off and-landing.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, a brief description will be given below of the drawings that are needed in the embodiments or the prior art descriptions, and it is obvious that the drawings in the following description are some embodiments of the present application, and that other drawings can be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic perspective view of a landing platform of an unmanned aerial vehicle according to an embodiment of the present application;
fig. 2 is a schematic liquid pipe structure of a landing platform of an unmanned aerial vehicle according to an embodiment of the present disclosure;
fig. 3 is a schematic bottom perspective view of a landing platform of an unmanned aerial vehicle according to an embodiment of the present disclosure;
fig. 4 is a schematic structural diagram of a connection component of a landing platform of an unmanned aerial vehicle according to an embodiment of the present application;
fig. 5 is a schematic structural diagram of a landing platform of an unmanned aerial vehicle according to another embodiment of the present disclosure;
fig. 6 is a schematic structural diagram of a landing platform of an unmanned aerial vehicle according to another embodiment of the present disclosure;
in the figure: the lifting plate-1, the first jack-11, the second jack-12, the storage battery-13 and the buffer coating-14;
wing plate-2, plug-in block-21, indicator lamp-22, photovoltaic panel-23;
the device comprises a connecting component-3, a rotating shaft-31, a fixed block-32, a threaded hole-321, a screw-322 and a clamping groove-33;
a telescopic rod-4;
liquid tube-5, transparent shell-51.
Detailed Description
For the purposes of making the objects, technical solutions and advantages of the embodiments of the present application more clear, the technical solutions in the embodiments of the present application are clearly and completely described below, and it is obvious that the described embodiments are some embodiments of the present application, but not all embodiments. All other embodiments, which can be made by one of ordinary skill in the art without inventive effort, are also within the scope of the present application based on the embodiments herein.
It should be noted that in the description of the present application, the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate an azimuth or a positional relationship based on the drawings, and are merely for convenience of description of the present application and for simplification of the description, and do not indicate or imply that the apparatus or element to be referred to must have a specific azimuth, be configured and operated in a specific azimuth, and therefore should not be construed as limiting the present application.
The terms "mounted," "connected," "coupled," and "connected" are to be construed broadly in this application, and may be, for example, fixedly connected, detachably connected, or integrally connected; may be a mechanical connection; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the terms in this application can be understood by those of ordinary skill in the art in a specific context.
The embodiment provides an unmanned aerial vehicle landing platform, as shown in fig. 1-6, including take-off and landing plate 1, take-off and landing plate 1 side is provided with pterygoid lamina 2, take-off and landing plate 1 is connected with telescopic link 4 through coupling assembling 3, take-off and landing plate 1 upper surface is provided with liquid pipe 5, liquid pipe 5 includes transparent shell 51, transparent shell 51 side mark has horizontal scale mark 52, the liquid is filled in the transparent shell 51.
The wing plate 2 connected with the side edge of the lifting plate 1 can be used for extending and expanding the surface of the lifting plate 1, increasing the surface area of the lifting plate 1, and the wing plate 2 can be used for installing and placing other functional components, so that the comprehensive service performance of the lifting plate 1 is improved. The side of take-off and landing plate 1 is provided with four telescopic links 4, telescopic link 4 is connected with take-off and landing plate 1 through coupling assembling 3, telescopic link 4 is used for propping up take-off and landing plate 1 and is higher than ground, telescopic link 4 can be used for adjusting take-off and landing environment such as river course shallow water, muddy ground, complicated topography such as soft meadow, preferably, telescopic link 4 selects electric telescopic link, through the length of each telescopic link 4 of adjustment, and then the levelness of adjustment take-off and landing plate 1, take-off and landing plate 1 upper surface is provided with liquid pipe 5, liquid pipe 5 is supported by transparent shell 51, transparent shell 51 side mark has horizontal scale mark 52, liquid level in liquid pipe 5 coincides or is parallel with horizontal scale mark 52 when take-off and landing plate 1 is in the horizontality, liquid level in liquid pipe 5 and horizontal scale mark 52 can produce the contained angle when take-off and landing plate 1 inclines, the length of telescopic link 4 makes take-off and landing plate 1 keep the level because in the balanced condition of liquid, the horizontal surface position of liquid total surface is in the level and the level of adjustment 5 can take-off and landing plate 1 and landing plate and the level of the unmanned aerial vehicle can take-off and landing plate 1, the level can be kept the level with the level of the unmanned aerial vehicle, the level can be kept in the level and the level of the unmanned aerial vehicle is high, the level.
In one embodiment of the present application, as shown in fig. 4 and 5, the connection assembly 3 includes a rotating shaft 31, the rotating shaft 31 is rotationally connected with the lifting plate 1, the rotating shaft 31 is connected with the telescopic rod 4, a fixing block 32 is disposed on one side of the rotating shaft 31, a threaded hole 321 is disposed on the fixing block 32, a screw 322 is disposed in the threaded hole 321, and a clamping groove 33 is formed in the surface of the rotating shaft 31.
The pivot 31 rotates with take-off and landing plate 1 to be connected, pivot 31 is connected with telescopic link 4 can make telescopic link 4 follow pivot 31 direction of rotation activity, and then can adjust the angle that telescopic link 4 supported take-off and landing plate 1, improve the regulation flexibility ratio, be used for adapting to more complex environment, be provided with screw hole 321 on fixed block 32, screw hole 321 and screw 322 cooperate, when telescopic link 4 rotates suitable position, need fix a position pivot 31, otherwise telescopic link 4 can be in unstable state when supporting, so be provided with fixed block 32 on one side of pivot 31, screw hole 321 on the fixed block 32 sets up the orientation towards pivot 31, rotate screw 322 when needs fixed pivot 31, screw 322 self screw and screw hole 321 cooperate, the front end of screw 322 precesses to pivot 31 direction when rotating screw 322, the pivot 31 surface is provided with draw-in groove 33, can lock pivot 31 when screw 322's front end screw in draw-in groove 33, and then fix telescopic link 4, when screw 322 front end unscrews draw-in groove 33 of pivot 31, pivot 31 can resume the rotation.
In one embodiment of the present application, as shown in fig. 3, a first jack 11 is disposed on a side edge of the lifting board 1, a plug 21 is disposed on a side edge of the wing board 2, and the first jack 11 is plugged with the plug 21 for detachable connection of the wing board 2 and the lifting board 1.
When the lifting plate 1 is required to be used, the plug 21 arranged on the side edge of the wing plate 2 can be inserted into the first jack 11 arranged on the side edge of the lifting plate 1 to be fixed, the plug 21 is cuboid, the first jack 11 is matched with the plug 21, the plug contact surface of the plug 21 and the first jack 11 is a rectangular plane, and the rectangular contact plane can give vertical upward supporting force to the plug 21 so as to prevent the plug 21 from falling off from the first jack 11. Alternatively, the length of the insertion block 21 extending into the first insertion hole 11 is such that the first insertion hole 21 is sufficient to give the insertion block 21 a supporting force vertically upward. Further, an anti-slip adhesive tape may be wound on the insert block 21 to ensure the tightness of the insert block 21 and the first jack 11, so as to prevent the insert block 21 from falling off from the first jack 11 during use. When the lifting plate 1 is not needed, the plug block 21 can be pulled out from the first jack 11, so that the plane area of the lifting plate 1 is reduced, and the lifting plate 1 is convenient to transport.
In one embodiment of the present application, as shown in fig. 1, the upper surface of the lifting plate 1 is provided with a second insertion hole 12.
After the inserted block 21 that the wing plate 2 side set up is pulled out from first jack 11, can insert second jack 12 with inserted block 21, as shown in fig. 6, can be used to be convenient for transport the fixed pterygoid lamina 2 and the take-off and land board of dismantling on the one hand, on the other hand when rotor unmanned aerial vehicle takes off, initial blade rotational speed can not provide stable lift, and there is the stability that the air current disturbance can influence unmanned aerial vehicle initial take off like ground, can peg graft the inserted block 21 of wing plate in second jack 12 departments, reduce the influence of ground air current to unmanned aerial vehicle take off, stability when improving unmanned aerial vehicle and take off.
In one embodiment of the present application, as shown in fig. 5, a plurality of indicator lights 22 are mounted on the wing plate 2.
When unmanned aerial vehicle operates the landing, meet under the poor situation of visibility, turn on pilot lamp 22 on the pterygoid lamina 2, can carry out the landmark to unmanned aerial vehicle's return journey and guide, also be favorable to under darker flight environment, unmanned aerial vehicle positions the position of landing platform in the distance.
In one embodiment of the present application, as shown in fig. 3 and 5, the photovoltaic panel 23 is mounted on the surface of the wing plate 2, the storage battery 13 is disposed on the bottom surface of the lifting plate 1, and the photovoltaic panel 23 is electrically connected with the storage battery 13.
When unmanned aerial vehicle survey and drawing is carried out in the field, unmanned aerial vehicle lack of electricity's condition can appear, and accessible photovoltaic board 23 charges battery 13 under unmanned aerial vehicle power supply's condition, and rethread battery 13 is mended the electricity to unmanned aerial vehicle, has improved unmanned aerial vehicle's duration, improves unmanned aerial vehicle's survey and drawing efficiency.
In one embodiment of the present application, as shown in fig. 5, the surface of the landing plate 1 is coated with a buffer coating 14.
The buffer coating 14 is a coating coated on the surface of the take-off and landing plate 1, and the coating position is in the central area of the take-off and landing plate 1, so that an additional protective layer is provided for the take-off and landing plate 1, friction and abrasion between the unmanned aerial vehicle and the surface of the platform are reduced, the hardness of the surface of the platform is improved, and damage to unmanned aerial vehicle components and surveying and mapping instruments caused by impact vibration due to too high descending speed of the unmanned aerial vehicle is avoided.
In the actual use process of the application: the inserting blocks 21 on the side edges of the wing plates 2 are inserted into the first inserting holes 11, then the length of the telescopic rods 4 and the supporting angle of the telescopic rods 4 for supporting the lifting plate 1 are adjusted according to the actual bottom surface conditions, and the liquid level in the liquid pipe 5 is observed to be level with the horizontal scale marks 52 marked by the liquid pipe 5 during adjustment, so that the horizontal state of the lifting plate 1 is ensured.
As shown in fig. 6, the insert block 21 of the wing plate 2 can be inserted into the second insertion hole 12, the telescopic rod 4 is rotated to be flush with the wing plate 2 to store the device, and the surrounding central space can be used for placing the unmanned aerial vehicle, so that the unmanned aerial vehicle is prevented from being knocked and damaged in the transferring process.
Finally, it should be noted that the above embodiments are merely for illustrating the technical solution of the present application, and are not limiting; although the present application has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art will understand; the technical scheme described in the foregoing embodiments can be modified or some or all of the technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit of the corresponding technical solutions from the scope of the technical solutions of the embodiments of the present application.
Claims (6)
1. The utility model provides an unmanned aerial vehicle landing platform, includes take-off and landing plate (1), its characterized in that, take-off and landing plate (1) side is provided with pterygoid lamina (2), take-off and landing plate (1) are connected with telescopic link (4) through coupling assembling (3), take-off and landing plate (1) upper surface is provided with liquid pipe (5), take-off and landing plate (1) side is provided with first jack (11), pterygoid lamina (2) side is provided with inserted block (21), first jack (11) with inserted block (21) peg graft be used for pterygoid lamina (2) with take-off and landing plate (1) can dismantle and be connected, liquid pipe (5) are including transparent shell (51), transparent shell (51) side mark has horizontal scale mark (52), be equipped with liquid in transparent shell (51).
2. The unmanned aerial vehicle landing platform according to claim 1, wherein the connecting assembly (3) comprises a rotating shaft (31), the rotating shaft (31) is rotationally connected with the landing plate (1), the rotating shaft (31) is connected with the telescopic rod (4), a fixed block (32) is arranged on one side of the rotating shaft (31), a threaded hole (321) is formed in the fixed block (32), a screw (322) is arranged in the threaded hole (321), and a clamping groove (33) is formed in the surface of the rotating shaft (31).
3. The unmanned aerial vehicle landing platform according to claim 1, wherein the upper surface of the landing plate (1) is provided with a second receptacle (12).
4. The unmanned aerial vehicle landing platform according to claim 1, wherein a plurality of indicator lights (22) are mounted on the wing plate (2).
5. The unmanned aerial vehicle landing platform according to claim 1, wherein the wing plate (2) is provided with a photovoltaic plate (23) on the surface, a storage battery (13) is arranged on the bottom surface of the landing plate (1), and the photovoltaic plate (23) is electrically connected with the storage battery (13).
6. The unmanned aerial vehicle landing platform according to any of claims 1 to 5, wherein the surface of the landing plate (1) is coated with a buffer coating (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322260019.7U CN220535989U (en) | 2023-08-22 | 2023-08-22 | Unmanned aerial vehicle landing platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322260019.7U CN220535989U (en) | 2023-08-22 | 2023-08-22 | Unmanned aerial vehicle landing platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220535989U true CN220535989U (en) | 2024-02-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322260019.7U Active CN220535989U (en) | 2023-08-22 | 2023-08-22 | Unmanned aerial vehicle landing platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220535989U (en) |
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2023
- 2023-08-22 CN CN202322260019.7U patent/CN220535989U/en active Active
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