CN115743664B - Portable unmanned aerial vehicle air park - Google Patents
Portable unmanned aerial vehicle air park Download PDFInfo
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- CN115743664B CN115743664B CN202211482452.9A CN202211482452A CN115743664B CN 115743664 B CN115743664 B CN 115743664B CN 202211482452 A CN202211482452 A CN 202211482452A CN 115743664 B CN115743664 B CN 115743664B
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- 239000002184 metal Substances 0.000 claims abstract description 40
- 238000012544 monitoring process Methods 0.000 claims abstract description 9
- 230000005540 biological transmission Effects 0.000 claims description 51
- 239000004744 fabric Substances 0.000 claims description 8
- 238000003780 insertion Methods 0.000 claims description 5
- 230000037431 insertion Effects 0.000 claims description 5
- 230000000149 penetrating effect Effects 0.000 claims description 4
- 238000010009 beating Methods 0.000 claims 1
- 230000003993 interaction Effects 0.000 abstract description 2
- 230000001681 protective effect Effects 0.000 abstract description 2
- 230000007246 mechanism Effects 0.000 description 8
- 238000006073 displacement reaction Methods 0.000 description 5
- 238000009434 installation Methods 0.000 description 5
- 230000008859 change Effects 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
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- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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Abstract
The invention discloses a portable unmanned aerial vehicle parking apron which comprises an inserting rod and a device metal plate, wherein the bottom end of the device metal plate is fixedly arranged with the top end of the inserting rod, and a monitoring assembly is fixedly arranged at the top of one side of the device metal plate. According to the invention, after the unmanned aerial vehicle falls onto the landing platform, the distance between the two infrared distance measuring sensors on two feet of the unmanned aerial vehicle is detected, the unmanned aerial vehicle is pushed by the side clamping assembly, and the unmanned aerial vehicle is integrally rotated and adjusted on the top of the landing platform by the deflection assembly, so that the unmanned aerial vehicle can quickly reach a correct parking posture after falling, the problem that the unmanned aerial vehicle cannot be pushed and aligned due to the inclined posture is avoided, the unmanned aerial vehicle can be quickly aligned under any parking angle, and the top of the parked unmanned aerial vehicle is provided with the protective automatic folding shielding cover, so that the unmanned aerial vehicle can be normally parked in various weather and can perform data interaction and charging work.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a portable unmanned aerial vehicle parking apron.
Background
Unmanned aerial vehicle automatic airport, also known as unmanned aerial vehicle airport, unmanned aerial vehicle hangar or unmanned aerial vehicle nest refers to the special place of parking that designs for unmanned aerial vehicle specially. The unmanned aerial vehicle can be directly deployed to the operation site, the problem of manual carrying unmanned aerial vehicle commute is solved, the biggest advantage of site deployment is that the emergent operation capability of the unmanned aerial vehicle is enhanced, and the operation efficiency is also greatly improved. When the unmanned aerial vehicle does not work, the unmanned aerial vehicle is standby in an automatic airport, and when the unmanned aerial vehicle works, an airport cabin door is opened, and the unmanned aerial vehicle automatically flies out to work. Unmanned aerial vehicle automatic airport generally includes airport cabin body, lift platform, automatic system of coming into the middle, automatic charging system, weather station, UPS, industry air conditioner etc. and main functions generally include parking unmanned aerial vehicle, independently charge, independently patrol and examine, a key take off, accurate landing, flight condition monitoring, real-time transmission, flight route planning etc..
Among the prior art, like unmanned aerial vehicle positioner and apron of chinese patent publication No. CN109963786a, this unmanned aerial vehicle positioner includes: the device comprises a driving assembly, a first transmission mechanism matched with the driving assembly, and a second transmission mechanism arranged in linkage with the first transmission mechanism, wherein the first transmission mechanism comprises a first push rod, the second transmission mechanism comprises a second push rod, and the second push rod can move along the axial direction of the first push rod; under the drive of the drive assembly, the first transmission mechanism drives the first push rod to move, and the first transmission mechanism is linked with the second transmission mechanism to drive the second push rod to move, so that the first push rod and the second push rod are matched to push the unmanned aerial vehicle to a preset position.
However, in the prior art, the unmanned aerial vehicle automatic airport is large in size and heavy in mass because of more equipment and outdoor work, can only be used for fixed deployment, is difficult to install, deploy and carry, has long installation and deployment time, needs more personnel, cannot rapidly work, and when the unmanned aerial vehicle is recovered, the symmetrically arranged pushing pieces are utilized to synchronously push the unmanned aerial vehicle on the take-off and landing platform, and although most of parked unmanned aerial vehicles can rapidly swing and position to work, the unmanned aerial vehicle which is inclined at approximately forty-five degrees after stopping is stopped, four corners of the unmanned aerial vehicle are uniformly pushed when the pushing pieces shrink and squeeze, and cannot deflect on the take-off and landing platform, so that the unmanned aerial vehicle cannot be charged or connected with a data plug due to the error of stopping posture.
Disclosure of Invention
In order to overcome the defects of the prior art, the technical problem to be solved by the invention is to provide a portable unmanned aerial vehicle parking apron, so that the problems that an unmanned aerial vehicle automatic airport provided by the background art is large in size and heavy in mass, can only be used for fixed deployment, is difficult to install, deploy and transport, has long installation and deployment time, needs a lot of personnel, cannot be used for quick operation, and can synchronously push unmanned aerial vehicles on a take-off and landing platform by utilizing symmetrically arranged pushing pieces when the unmanned aerial vehicles are recovered, and can realize quick positioning work of most parked unmanned aerial vehicles, but for the unmanned aerial vehicles which are inclined at approximately forty-five degrees after stopping, four corners of the unmanned aerial vehicles are uniformly pushed when the pushing pieces shrink and squeeze, the unmanned aerial vehicles cannot deflect on the take-off and landing platform, and cannot charge or access data plugs due to the error of the parking posture are solved.
To achieve the purpose, the invention adopts the following technical scheme:
the invention provides a portable unmanned aerial vehicle parking apron, which comprises an inserted link and a device sheet metal, wherein the bottom end of the device sheet metal is fixedly arranged at the top end of the inserted link, a monitoring assembly is fixedly arranged at the top of one side of the device sheet metal, the monitoring assembly comprises a bracket, a monitor and two infrared ranging sensors, the two infrared ranging sensors are respectively and fixedly arranged at two sides of the bracket, the monitor is fixedly arranged on the bracket, a lifting platform is fixedly arranged at the top end of the device sheet metal, and a folding shielding cover, a lateral clamping assembly, a deflection assembly and an automatic inserting assembly are movably arranged on the lifting platform; when the device is stopped, after the unmanned aerial vehicle freely falls onto a landing platform, firstly, whether the distances between two feet of the unmanned aerial vehicle and the two infrared ranging sensors are the same or not is detected through the two infrared ranging sensors; if the two infrared distance measuring sensors are different, representing the correct parking posture of the unmanned aerial vehicle after falling and not being adjusted, then starting the lateral clamping assembly to push the unmanned aerial vehicle to the central position of the take-off and landing platform, and detecting the distance between the two infrared distance measuring sensors; if the distances are the same, starting a folding shielding cover and an automatic plugging assembly to shield and protect the outer side of the unmanned aerial vehicle, and inserting the shielding cover and the automatic plugging assembly into a charging interface and a data transmission interface respectively; if the distance is still not the same, represent unmanned aerial vehicle parking state and show for the picture, forty-five degrees are put to one side and are parked, will start deflection subassembly and rotate the adjustment with unmanned aerial vehicle wholly in the platform top of taking off and land, and two infrared ranging sensors detect unmanned aerial vehicle both feet interval in real time all the time during, when until the interval is the same, then represent unmanned aerial vehicle and fall the back and be the correct parking gesture of putting forward, stop deflection subassembly work immediately to start folding shielding cover and automatic grafting subassembly.
The side direction clamping assembly comprises a first motor, a first transmission belt, a first rotating shaft and two first lead screws, wherein the output end of the first motor is movably connected with the first rotating shaft through the first transmission belt, the two ends of the first rotating shaft are fixedly provided with first bevel gears, the two ends of the first lead screws are fixedly provided with second bevel gears, the two ends of the first lead screws are respectively meshed with the two second bevel gears, the two first push blocks are respectively connected with the two first lead screws in a threaded manner, the two push rods are movably arranged between the first lead screws, the two ends of the two push rods are respectively fixedly arranged at the tops of the four first push blocks, after the first motor is started, the first motor drives the first rotating shaft to rotate through the first transmission belt, the meshed first bevel gears and second bevel gears are utilized to enable the two first lead screws to rotate, the two push blocks on the same first lead screw are enabled to displace along the first lead screws, the displacement of the two push blocks is achieved, the distance between the two push rods is changed, the unmanned aerial vehicle is positioned in the middle of the unmanned aerial vehicle to be clamped, and the gesture of the unmanned aerial vehicle is changed.
The deflection assembly comprises a chassis, a plurality of connecting rods, an inner disc, a second transmission belt and a second motor, wherein the inner side of the chassis is welded with the outer side of the inner disc through the plurality of connecting rods, a first driven wheel is fixedly arranged at the bottom end of the inner disc, the first driven wheel is movably connected with the output end of the second motor through the second transmission belt, after the unmanned aerial vehicle falls on the chassis, when the unmanned aerial vehicle is detected to rotate, the second motor is started, the second transmission belt drives the first driven wheel and the inner disc fixed at the top of the first driven wheel to rotate, and accordingly the chassis drives the unmanned aerial vehicle parked at the top of the first driven wheel to rotate.
In the preferred technical scheme of the invention, a plurality of anti-skid grooves are uniformly formed in the upper surface of the chassis, a plurality of through holes are formed in the inner side of the chassis in a penetrating manner, the anti-skid grooves are used for increasing friction force between the unmanned aerial vehicle and the top of the chassis and preventing the unmanned aerial vehicle from sliding during rotation, and the through holes are used for avoiding shielding a heat dissipation channel.
In the preferred technical scheme of the invention, the bottom end of the support is fixedly arranged on the outer side of the equipment sheet metal, and the top end of the support is fixedly provided with a positioner which is used for determining the stop position of the unmanned aerial vehicle.
In the preferred technical scheme of the invention, the radiators are fixedly arranged at the bottoms of the two sides of the equipment sheet metal, the input ends of the radiators are inserted into the lifting table, the circuit insertion interfaces are fixedly arranged in the equipment sheet metal, the top channels of the radiators pass through the inside of the equipment sheet metal so as to facilitate the heat discharge in the equipment sheet metal, and the circuit insertion interfaces can be externally connected with different equipment so as to realize the installation of mutually stacked equipment layers in the device.
In a preferred technical scheme of the invention, the folding shielding cover comprises a second rotating shaft, a third driving belt, a third motor, a plurality of arc rods and U-shaped pipes, wherein the two ends of the second rotating shaft are respectively clamped with a first driving gear, the top of the first driving gear is meshed with a second driving gear, one end of the second driving gear is fixedly provided with a clamping block, the inner side of the clamping block is clamped with one end of one arc rod, each arc rod is movably inserted into the U-shaped pipe, the second rotating shaft is movably connected with the output end of the third motor through the third driving belt, and after the third motor is started, the third motor drives the second rotating shaft and the first driving gears at the two ends of the second rotating shaft through the third driving belt, so that the second driving gear meshed with the second rotating shaft can drive the arc rods at the top, and the axle center of the second driving gear is used as a rotating shaft to deflect.
In the preferred technical scheme of the invention, a placing plate is fixedly arranged on one side of each U-shaped pipe, a plurality of arc rods are connected in series through elastic ropes, folding waterproof cloth is clamped between every two adjacent arc rods, and when the arc rod at the top deflects, the arc rods connected in series with the folding waterproof cloth are pulled to follow the deflection through the elastic ropes, so that the folding waterproof cloth can be rapidly unfolded, and a shell cover is formed to protect the outer side of the unmanned aerial vehicle.
In the preferred technical scheme of the invention, the two sides of the second first rotating shaft end are respectively provided with the trigger, the top of each trigger is fixedly provided with the metal sheet, the outer side of the second rotating shaft is fixedly sleeved with the pressing block, the pressing block is driven to rotate when the second rotating shaft rotates, and the metal sheet on the other side is pressed down after the pressing block rotates, so that the third motor is powered off to stop the deflection work of the second rotating shaft.
In the preferred technical scheme of the invention, the automatic plugging assembly comprises a fourth motor, a third transmission gear, a fourth transmission gear, a second screw rod, two second push blocks and two plugs, wherein one side of each second push block is fixedly installed with the bottoms of the corresponding two plugs, the two second push blocks are respectively connected with two ends of the corresponding second screw rod in a threaded manner, the fourth motor is movably connected with the fourth transmission gear through the third transmission gear, the shaft center of the second screw rod and the shaft center of the fourth transmission gear are fixedly plugged, and after the fourth motor is started, the second screw rod is driven to rotate through the third transmission gear and the fourth transmission gear, so that the two second push blocks on the screw rod respectively carry the corresponding two plugs to displace along the screw rod, the distance between the two plugs is adjusted, and the interfaces of the unmanned aerial vehicle can be plugged into or pulled out respectively.
In the preferred technical scheme of the invention, a guide rod is movably inserted between the two plugs, the tops of the two plugs are movably inserted with the lifting platform, and the guide rod is used for preventing the two plugs from rolling when the two plugs are displaced and can be accurately inserted into the corresponding interfaces of the unmanned aerial vehicle.
In the preferred technical scheme of the invention, a plurality of movable grooves are uniformly formed in the bottom of the inserted link in a penetrating manner, and a deflection rod is rotatably arranged in each movable groove.
The beneficial effects of the invention are as follows:
according to the portable unmanned aerial vehicle parking apron, after the unmanned aerial vehicle lands on the take-off and landing platform, the distance between the two infrared distance measuring sensors and the distance between the two infrared distance measuring sensors are respectively measured by the two infrared distance measuring sensors, the unmanned aerial vehicle is pushed by the side clamping assembly, and the unmanned aerial vehicle is rotated and adjusted on the top of the take-off and landing platform by the deflection assembly, so that the unmanned aerial vehicle can quickly reach a correct parking posture after landing, the problem that the unmanned aerial vehicle cannot be pushed and adjusted due to the inclined posture is avoided, the unmanned aerial vehicle can be quickly adjusted at any parking angle, and the top of the parked unmanned aerial vehicle is provided with the protective automatic folding shielding cover, so that the unmanned aerial vehicle can be normally parked and conduct data interaction and charging work in various weather.
Divide into a plurality of equipment layers that pile up each other with unmanned aerial vehicle automatic airport, every layer is small, the quality is light, and single can easily carry, pile up, install and dismantle, makes unmanned aerial vehicle automatic airport's whole zero, realizes not having to use for the lifting means can install fast and deploy, dismantle the transportation.
When the device is used, the device can work by only stacking and inserting necessary device layers, the unnecessary device layers in the device metal plate can be used by fast stacking and inserting, the functions of the device are rapidly expanded, the performance of the device is improved, and the damaged layer can be repaired by replacing the new device layer when the device is damaged, so that the device can work again, and the maintenance efficiency is greatly improved.
Drawings
Fig. 1 is a schematic structural view of a portable unmanned aerial vehicle apron according to the present invention;
fig. 2 is a schematic top view of a metal plate of a portable unmanned aerial vehicle parking apron according to the present invention;
fig. 3 is a schematic bottom view of a metal plate of a portable unmanned aerial vehicle apron;
fig. 4 is a schematic diagram of an internal structure of a metal plate of a portable unmanned aerial vehicle parking apron;
fig. 5 is a schematic structural view of a folding shelter of a portable unmanned aerial vehicle tarmac according to the present invention;
FIG. 6 is a schematic view of a part of a folding shelter of a portable unmanned aerial vehicle parking apron according to the present invention;
FIG. 7 is a schematic view of a side clamping assembly of a portable unmanned aerial vehicle tarmac according to the present invention;
FIG. 8 is a schematic view of a deflection assembly of a portable unmanned aerial vehicle tarmac according to the present invention;
FIG. 9 is an enlarged schematic view of FIG. 5 at A;
FIG. 10 is a schematic view of an automatic docking assembly for a portable unmanned aerial vehicle tarmac according to the present invention;
FIG. 11 is a schematic view of the bottom structure of a plunger of a portable unmanned aerial vehicle tarmac according to the present invention;
fig. 12 is a schematic view of an internal structure of a portable unmanned aerial vehicle tarmac according to the present invention;
fig. 13 is a schematic view of a shutdown state.
In the figure:
1-inserting a rod; 10-a movable groove; 11-deflecting the rod; 2-equipment sheet metal; 20-a line plug interface; 21-a landing stage; 3-a heat sink; 4-folding the shielding cover; 40-a second rotating shaft; 41-a third belt; 410-briquetting; 412-a trigger; 413-sheet metal; 42-a third motor; 43-first transmission gear; 44-a second drive gear; 45-clamping blocks; 46-arc-shaped rod; 460-bungee cord; 461-folding waterproof cloth; 47-placing the plate; 48-U-shaped tube; a 5-lateral clamping assembly; 50-a first motor; 51-a first belt; 52-a first rotating shaft; 53-first bevel gear; 54-a second bevel gear; 55-a first screw rod; 56-a first push block; 57-push rod; a 6-deflection assembly; 60-chassis; 61-anti-skid grooves; 62-a through hole; 63-a connecting rod; 64-inner disc; 65-a first driven wheel; 66-a second belt; 67-a second motor; 7-an automatic plugging assembly; 70-fourth motor; 71-a third transmission gear; 72-fourth drive gear; 73-a second screw rod; 74-a second push block; 75-plug; 76-a guide bar; 8-monitoring the assembly; 80-a bracket; 81-positioners; 82-a monitor; 83-infrared ranging sensor.
Detailed Description
The technical scheme of the invention is further described below by the specific embodiments with reference to the accompanying drawings.
As shown in fig. 1-13, in the embodiment, a portable unmanned aerial vehicle parking apron is provided, which comprises an inserting rod 1 and a device metal plate 2, wherein the bottom end of the device metal plate 2 is fixedly installed with the top end of the inserting rod 1, a monitoring component 8 is fixedly installed at the top of one side of the device metal plate 2, the monitoring component 8 comprises a bracket 80, a monitor 82 and two infrared ranging sensors 83, the two infrared ranging sensors 83 are respectively and fixedly installed at two sides of the bracket 80, the monitor 82 is fixedly installed on the bracket 80, a lifting platform 21 is fixedly installed at the top end of the device metal plate 2, and a folding shielding cover 4, a lateral clamping component 5, a deflection component 6 and an automatic plugging component 7 are movably installed on the lifting platform 21; when the device is stopped, after the unmanned aerial vehicle freely falls onto the landing platform 21, firstly, whether the distances between two feet of the unmanned aerial vehicle and the two infrared ranging sensors 83 are the same or not is detected through the two infrared ranging sensors 83; if the two infrared distance measuring sensors 83 are different, the unmanned aerial vehicle represents a correct parking posture which is not aligned after falling, then the lateral clamping assembly 5 is started to push the unmanned aerial vehicle to the central position of the take-off and landing platform 21, and the two infrared distance measuring sensors 83 detect the distance; if the distances are the same, starting the folding shielding cover 4 and the automatic plugging assembly 7 to shield and protect the outer side of the unmanned aerial vehicle, and inserting the shielding cover into a charging interface and a data transmission interface; if the distances are still not the same, the unmanned aerial vehicle is represented to be parked in a state shown in fig. 13, the forty-five-degree inclined parking is performed, the deflection assembly 6 is started to rotate and adjust the unmanned aerial vehicle on the top of the lifting platform 21, the distance between two feet of the unmanned aerial vehicle is always detected in real time by the two infrared ranging sensors 83 until the distances are the same, the unmanned aerial vehicle is represented to be correctly parked in a correct posture after falling, the deflection assembly 6 is immediately stopped to work, and the folding shielding cover 4 and the automatic plugging assembly 7 are started.
According to the invention, the unmanned aerial vehicle automatic airport is divided into a plurality of mutually stacked equipment layers, each layer is small in size and light in weight, and a single person can easily carry, stack, install and detach, so that the unmanned aerial vehicle automatic airport is integrated into zero, and rapid installation, deployment, disassembly and transportation can be realized without using a lifting tool.
When in use, the necessary equipment layers are stacked and spliced for assembly, and the operation can be realized. The unnecessary equipment layers in the equipment sheet metal 2 can be used by fast stacking and plugging, so that the functions of the equipment are rapidly expanded and the performance is improved. When equipment is damaged, the damaged layer can be repaired by replacing the damaged layer with a new equipment layer, so that the equipment can work again, and the maintenance efficiency is greatly improved. The necessary equipment layers mainly comprise a lifting layer, a control layer and a supporting layer, and other equipment layers further comprise a power supply layer, a standby power supply layer, a temperature control layer, an edge computing layer, a data center layer, a power conversion layer, a standby layer, a network layer, a parking layer, an airport tower and the like, and the layers can be rapidly expanded by stacking the layers in the equipment sheet metal 2.
The lateral clamping assembly 5 comprises a first motor 50, a first transmission belt 51, a first rotating shaft 52 and two first screw rods 55, wherein the output end of the first motor 50 is movably connected with the first rotating shaft 52 through the first transmission belt 51, the two ends of the first rotating shaft 52 are fixedly provided with first bevel gears 53, one ends of the two first screw rods 55 are fixedly provided with second bevel gears 54, the two first bevel gears 53 are respectively meshed with the two second bevel gears 54, the two first screw rods 55 are respectively connected with two first push blocks 56 in a threaded manner, two push rods 57 are movably arranged between the two first screw rods 55, and the two ends of the two push rods 57 are respectively fixedly arranged at the tops of the four first push blocks 56; after the first motor 50 is started, the first rotating shaft 52 is driven to rotate through the first transmission belt 51, the two first screw rods 55 are rotated by utilizing the meshed first bevel gear 53 and second bevel gear 54, so that the two pushing blocks 56 on the same first screw rod 55 are displaced along the first screw rod 55, the displacement of the two pushing rods 57 is realized, the distance between the two pushing rods 57 is changed, the unmanned aerial vehicle in the middle is clamped and pushed, and the parking posture of the unmanned aerial vehicle is changed.
The deflection assembly 6 comprises a chassis 60, a plurality of connecting rods 63, an inner disc 64, a second transmission belt 66 and a second motor 67, wherein the inner side of the chassis 60 is welded with the outer side of the inner disc 64 through the plurality of connecting rods 63, a first driven wheel 65 is fixedly arranged at the bottom end of the inner disc 64, and the first driven wheel 65 is movably connected with the output end of the second motor 67 through the second transmission belt 66; after the unmanned aerial vehicle falls on the chassis 60, when detecting and needing to rotate, the second motor 67 is started, and the second transmission belt 66 drives the first driven wheel 65 and the inner disc 64 fixed at the top of the first driven wheel to rotate, so that the chassis 60 drives the unmanned aerial vehicle parked at the top of the first driven wheel to rotate.
As shown in fig. 8, a plurality of anti-skid grooves 61 are uniformly formed on the upper surface of the chassis 60, and a plurality of through holes 62 are formed inside the chassis 60; the anti-slip groove 61 is used for increasing the friction force between the unmanned aerial vehicle and the top of the chassis 60, preventing the unmanned aerial vehicle from sliding during rotation, and the through hole 62 is used for avoiding shielding the heat dissipation channel.
According to the illustration in fig. 2, the bottom of the support 80 is fixedly mounted to the outer side of the equipment sheet metal 2, and the top of the support 80 is fixedly mounted with a positioner 81, wherein the positioner 81 is used for determining the stop position of the unmanned aerial vehicle.
According to the figures 2, 3 and 4, the bottom of two sides of the metal plate 2 of the device is fixedly provided with the radiator 3, the input end of the radiator 3 is inserted on the lifting platform 21, the circuit insertion interface 20 is fixedly arranged inside the metal plate 2 of the device, the top channel of the radiator 3 passes through the inside of the metal plate 2 of the device so as to facilitate the heat discharge inside the metal plate 2 of the device, and the circuit insertion interface 20 can be externally connected with different devices so as to realize the installation of mutually stacked device layers in the device.
According to the embodiment shown in fig. 5, 6 and 9, the folding shielding cover 4 comprises a second rotating shaft 40, a third driving belt 41, a third motor 42, a plurality of arc-shaped rods 46 and a U-shaped pipe 48, wherein the two ends of the second rotating shaft 40 are respectively clamped with a first driving gear 43, the top of the first driving gear 43 is meshed with a second driving gear 44, one end of the second driving gear 44 is fixedly provided with a clamping block 45, the inner side of the clamping block 45 is clamped with one end of one arc-shaped rod 46, each arc-shaped rod 46 is movably inserted into the U-shaped pipe 48, and the second rotating shaft 40 is movably connected with the output end of the third motor 42 through the third driving belt 41; after the third motor 42 is started, the third driving belt 41 drives the second rotating shaft 40 and the first driving gears 43 at two ends of the second rotating shaft, so that the second driving gear 44 meshed with the second rotating shaft can drive the arc-shaped rod 46 at the top, and the axle center of the second driving gear 44 is taken as a rotating shaft to deflect.
According to fig. 5 and 6, a placement plate 47 is fixedly installed on one side of each of the plurality of U-shaped pipes 48, a plurality of arc rods 46 are connected in series through elastic ropes 460, and a folding waterproof cloth 461 is clamped between every two adjacent arc rods 46, when the topmost arc rod 46 deflects, the plurality of arc rods 46 connected in series with the topmost arc rod 46 are pulled to follow the deflection through the elastic ropes 460, so that the folding waterproof cloth 461 can be rapidly unfolded to form a shell cover for protection on the outer side of the unmanned aerial vehicle.
According to fig. 5 and 9, two sides of one end of the second rotating shaft 40 are respectively provided with a trigger 412, the top of each trigger 412 is fixedly provided with a metal sheet 413, the outer side of the second rotating shaft 40 is fixedly sleeved with a pressing block 410, the pressing block 410 is driven to rotate when the second rotating shaft 40 rotates, and when the pressing block 410 rotates 180 degrees, the other side of the metal sheet 413 is pressed down, so that the third motor 42 is powered off to stop the deflection work of the second rotating shaft 40.
According to the embodiment shown in fig. 10, the automatic plugging assembly 7 comprises a fourth motor 70, a third transmission gear 71, a fourth transmission gear 72, a second screw rod 73, two second push blocks 74 and two plugs 75, wherein one side of each second push block 74 is fixedly installed with the bottoms of the corresponding two plugs 75, the two second push blocks 74 are respectively connected with two ends of the corresponding second screw rod 73 in a threaded manner, the fourth motor 70 is movably connected with the fourth transmission gear 72 through the third transmission gear 71, and the second screw rod 73 is fixedly plugged with the axial center of the fourth transmission gear 72; after the fourth motor 70 is started, the second screw rod 73 is driven to rotate through the third transmission gear 71 and the fourth transmission gear 72, so that two second push blocks 74 on the screw rod 73 respectively carry two plugs 75, displacement is carried out along the screw rod, the distance between the two plugs 75 is adjusted, and the interfaces of the unmanned aerial vehicle can be plugged into or pulled out respectively.
According to the illustration in fig. 10, a guiding rod 76 is movably inserted between two plugs 75, the tops of the two plugs 75 are movably inserted with the landing platform 21, and the guiding rod 76 is used for preventing the two plugs 75 from rolling during displacement and can be accurately inserted into the corresponding interfaces of the unmanned plane.
According to the illustration shown in fig. 11, a plurality of movable slots 10 are uniformly formed in the bottom of the insert rod 1, and a deflection rod 11 is rotatably mounted in each movable slot 10, when the bottom end of the insert rod 1 is inserted into the ground, the bottom end of the deflection rod 11 is in contact with the ground to be extruded, and the top ends of the deflection rods 11 are close to each other, so as to avoid the insert rod 1 from toppling when receiving external force.
The application method and the working principle of the device are as follows: when the device is stopped, the unmanned aerial vehicle freely falls onto the landing platform 21. Firstly, detecting whether the distances between two feet of the unmanned aerial vehicle and the two infrared ranging sensors 83 are the same or not through the two infrared ranging sensors 83; if different, represent the unmanned aerial vehicle and fall behind the correct parking gesture of non-centering, then, start side direction clamping assembly 5 and push unmanned aerial vehicle to the central point of take off and land platform 21, during the period, after side direction clamping assembly 5's first motor 50 starts, will drive first pivot 52 rotatory through first drive belt 51, utilize the first bevel gear 53 of meshing and second bevel gear 54 for two first lead screws 55 rotate, thereby make two ejector pad 56 on same first lead screw 55 displace along first lead screw 55, and then realize the displacement of two push rods 57, change two push rod 57 interval, carry out the centre gripping promotion to the unmanned aerial vehicle that is located in the middle, change unmanned aerial vehicle's parking gesture.
Meanwhile, two infrared ranging sensors 83 perform distance detection; if the distance is the same, the folding shielding cover 4 and the automatic plugging component 7 are started to shield and protect the outer side of the unmanned aerial vehicle, and the charging interface and the data transmission interface are inserted.
If the distance is still not the same, the parking state of the unmanned aerial vehicle is shown in fig. 13, the unmanned aerial vehicle is parked in a forty-five degree oblique position, the deflection assembly 6 is started to rotate and adjust the unmanned aerial vehicle on the top of the landing platform 21, during the period, the second motor 67 of the deflection assembly 6 is started, the second driving belt 66 drives the first driven wheel 65 and the inner disc 64 fixed on the top of the first driven wheel to rotate, and therefore the chassis 60 drives the unmanned aerial vehicle parked on the top of the first driven wheel to rotate. Simultaneously, two infrared ranging sensors 83 detect unmanned aerial vehicle both feet interval in real time all the time, when the interval is the same, then represent unmanned aerial vehicle falls behind and be the correct parking gesture of straightening to stop deflection assembly 6 work immediately to start folding shielding cover 4 and automatic grafting subassembly 7.
When the folding shielding cover 4 is started, the third motor 42 is started, and the third driving belt 41 drives the second rotating shaft 40 and the first driving gears 43 at two ends of the second rotating shaft, so that the second driving gear 44 meshed with the second rotating shaft can drive the arc-shaped rod 46 at the top, and the axle center of the second driving gear 44 is taken as a rotating shaft to deflect. When the topmost arc-shaped rod 46 deflects, the plurality of arc-shaped rods 46 connected in series with the topmost arc-shaped rod 46 are pulled to follow the deflection through the elastic rope 460, so that the folding waterproof cloth 461 can be rapidly unfolded to form a shell cover for protecting the outer side of the unmanned aerial vehicle.
In addition, when the automatic plugging assembly 7 is started, the fourth motor 70 is started, and drives the second screw rod 73 to rotate through the third transmission gear 71 and the fourth transmission gear 72, so that two second push blocks 74 on the screw rod 73 respectively carry two plugs 75, displace along the screw rod, further adjust the distance between the two plugs 75, and respectively insert or extract the interface of the unmanned aerial vehicle.
Other techniques of this embodiment employ the prior art.
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the spirit and scope of the invention. The invention is not to be limited by the specific embodiments disclosed herein, and other embodiments are within the scope of the invention as defined by the claims of the present application.
Claims (8)
1. The utility model provides a portable unmanned aerial vehicle air park, includes inserted bar (1), equipment panel beating (2) bottom and inserted bar (1) top fixed mounting, its characterized in that: the device comprises a device sheet metal (2), wherein a monitoring assembly (8) is fixedly arranged at the top of one side of the device sheet metal (2), the monitoring assembly (8) comprises a support (80), a monitor (82) and two infrared ranging sensors (83), the two infrared ranging sensors (83) are respectively and fixedly arranged at two sides of the support (80), the monitor (82) is fixedly arranged on the support (80), a lifting platform (21) is fixedly arranged at the top end of the device sheet metal (2), and a folding shielding cover (4), a lateral clamping assembly (5), a deflection assembly (6) and an automatic plugging assembly (7) are movably arranged on the lifting platform (21);
the lateral clamping assembly (5) comprises a first motor (50), a first transmission belt (51), a first rotating shaft (52) and two first screw rods (55), wherein the output end of the first motor (50) is movably connected with the first rotating shaft (52) through the first transmission belt (51), the two ends of the first rotating shaft (52) are fixedly provided with first bevel gears (53), one end of each first screw rod (55) is fixedly provided with a second bevel gear (54), the two first bevel gears (53) are respectively meshed with the two second bevel gears (54), the two first push blocks (56) are connected with the two first screw rods (55) in a threaded manner, two push rods (57) are movably arranged between the two first screw rods (55), and the two ends of each push rod (57) are respectively fixedly arranged at the tops of the four first push blocks (56);
the deflection assembly (6) comprises a chassis (60), a plurality of connecting rods (63), an inner disc (64), a second transmission belt (66) and a second motor (67), wherein the inner side of the chassis (60) is welded with the outer side of the inner disc (64) through the plurality of connecting rods (63), a first driven wheel (65) is fixedly arranged at the bottom end of the inner disc (64), and the first driven wheel (65) is movably connected with the output end of the second motor (67) through the second transmission belt (66);
the folding shielding cover (4) comprises a second rotating shaft (40), a third driving belt (41), a third motor (42), a plurality of arc rods (46) and U-shaped pipes (48), wherein the first driving gears (43) are clamped at two ends of the second rotating shaft (40), the second driving gears (44) are meshed with the tops of the first driving gears (43), clamping blocks (45) are fixedly arranged at one ends of the second driving gears (44), the inner sides of the clamping blocks (45) are clamped with one end of one arc rod (46), each arc rod (46) is movably spliced with one U-shaped pipe (48), and the second rotating shaft (40) is movably connected with the output end of the third motor (42) through the third driving belt (41);
the automatic inserting assembly (7) comprises a fourth motor (70), a third transmission gear (71), a fourth transmission gear (72), a second screw rod (73), two second pushing blocks (74) and two plugs (75), wherein one side of each second pushing block (74) is fixedly installed at the bottoms of the corresponding two plugs (75), the two second pushing blocks (74) are respectively in threaded connection with two ends of the corresponding second screw rod (73), the fourth motor (70) is movably connected with the corresponding fourth transmission gear (72) through the third transmission gear (71), and the second screw rod (73) is fixedly inserted into the axial center of the corresponding fourth transmission gear (72).
2. The portable unmanned aerial vehicle tarmac of claim 1, wherein: a plurality of anti-skid grooves (61) are uniformly formed in the upper surface of the chassis (60), and a plurality of through holes (62) are formed in the inner side of the chassis (60) in a penetrating mode.
3. The portable unmanned aerial vehicle tarmac of claim 1, wherein: the bottom of the bracket (80) is fixedly arranged on the outer side of the equipment metal plate (2), and the top of the bracket (80) is fixedly provided with a locator (81).
4. The portable unmanned aerial vehicle tarmac of claim 1, wherein: the device is characterized in that radiators (3) are fixedly installed at the bottoms of two sides of the device metal plate (2), the input ends of the radiators (3) are inserted on the lifting platform (21), and a circuit insertion interface (20) is fixedly installed inside the device metal plate (2).
5. The portable unmanned aerial vehicle tarmac of claim 1, wherein: a placing plate (47) is fixedly arranged on one side of each U-shaped pipe (48), a plurality of arc-shaped rods (46) are connected in series through elastic ropes (460), and folding waterproof cloth (461) is clamped between every two adjacent arc-shaped rods (46).
6. The portable unmanned aerial vehicle tarmac of claim 1, wherein: the two sides of one end of the second rotating shaft (40) are respectively provided with a trigger (412), the tops of the triggers (412) are respectively fixedly provided with a metal sheet (413), and the outer side of the second rotating shaft (40) is fixedly sleeved with a pressing block (410).
7. The portable unmanned aerial vehicle tarmac of claim 1, wherein: a guide rod (76) is movably inserted between the two plugs (75), and the tops of the two plugs (75) are movably inserted with the lifting platform (21).
8. The portable unmanned aerial vehicle tarmac of claim 1, wherein: a plurality of movable grooves (10) are uniformly formed in the bottom of the inserted link (1) in a penetrating mode, and a deflection rod (11) is rotatably installed in each movable groove (10).
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| CN116151590B (en) * | 2023-04-07 | 2023-07-04 | 中国民用航空飞行学院 | Modularized unmanned aerial vehicle airport planning method for urban air traffic |
| CN117944919A (en) * | 2024-03-27 | 2024-04-30 | 山西中创天达科技有限公司 | Unmanned aerial vehicle autonomous take-off and landing system |
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| WO2019085151A1 (en) * | 2017-10-30 | 2019-05-09 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle positioning device and parking apron |
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| JP7083099B2 (en) * | 2017-05-11 | 2022-06-10 | 大平電子株式会社 | Drone landing gear |
| GB2583418B (en) * | 2017-05-27 | 2022-08-03 | Skysys Intelligent Tech Suzhou Co Ltd | Drone parking garage |
| CN207089676U (en) * | 2017-08-01 | 2018-03-13 | 杭州米希科技有限公司 | Unmanned plane touch down attitude adjusts fixed system and the airplane parking area using the system |
| CN110406689A (en) * | 2018-04-27 | 2019-11-05 | 北京三快在线科技有限公司 | Airplane parking area and UAV Landing system |
| CN110872003A (en) * | 2018-08-30 | 2020-03-10 | 一飞智控(天津)科技有限公司 | Logistics unmanned aerial vehicle airport and control method thereof |
| CN209956243U (en) * | 2019-05-29 | 2020-01-17 | 山东厚德测控技术股份有限公司 | Unmanned aerial vehicle parking apron capable of automatically adjusting parking position |
| CN110729778A (en) * | 2019-09-29 | 2020-01-24 | 沈阳航空航天大学 | Automatic charging device that returns to center of class umbrella-shaped unmanned aerial vehicle |
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| CN112977862B (en) * | 2021-03-30 | 2022-07-01 | 宁波道充科技有限公司 | Unmanned aerial vehicle wireless charging parking apron |
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| WO2019085151A1 (en) * | 2017-10-30 | 2019-05-09 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle positioning device and parking apron |
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