CN112249355A - Unmanned aerial vehicle take-off and landing device for water conservancy - Google Patents
Unmanned aerial vehicle take-off and landing device for water conservancy Download PDFInfo
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- CN112249355A CN112249355A CN202011095254.8A CN202011095254A CN112249355A CN 112249355 A CN112249355 A CN 112249355A CN 202011095254 A CN202011095254 A CN 202011095254A CN 112249355 A CN112249355 A CN 112249355A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
- B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
- B60L53/35—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
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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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
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- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The invention discloses a water-utilizing unmanned aerial vehicle take-off and landing device, which comprises: the device comprises a box body, a protection mechanism, an automatic butt joint mechanism, a rotating mechanism, a storage battery, a night indicator light, a tripod, a water conservancy aerial photography unmanned aerial vehicle and a controller; the protection mechanism is arranged at the top end of the inner cavity of the box body; the automatic butt-joint mechanism is arranged on the front side of the bottom end of the inner cavity of the box body; the rotating mechanism is arranged at the bottom end of the inner cavity of the box body and is positioned at the rear side of the automatic butt joint mechanism; the tripod is detachably arranged at the center of the bottom end of the box body; the water conservancy aerial photography unmanned aerial vehicle is placed at the top end of the rotating mechanism; the controller is arranged at the center of the front side of the box body. This unmanned aerial vehicle take off and land device is utilized to water can realize that the unmanned aerial vehicle interface docks with the outside charger is automatic when realizing that unmanned aerial vehicle charges, easy operation, labour saving and time saving to can prevent that unmanned aerial vehicle from damaging to the automatic waterproof and rainproof protection of unmanned aerial vehicle and can open automatically when unmanned aerial vehicle parks.
Description
Technical Field
The invention relates to the technical field of water conservancy, in particular to a water utilization unmanned aerial vehicle take-off and landing device.
Background
For a long time, people all over the world construct a great deal of various types of hydraulic engineering for different purposes in different historical periods and different natural conditions, particularly after world war II, the engineering constructed in short decades is more, the speed is high, the scale is large, the technical level is high, the engineering exceeds the prior historical stage, and great benefits are obtained, tens of thousands of reservoirs are constructed on a plurality of rivers, the total storage capacity reaches 6 billion cubic meters, the regulation capacity of the runoff is greatly increased, the flood resistance of the rivers is improved through comprehensive measures of reservoirs, dikes, river regulation, partial storage of flood and the like, the current water conservancy ecological problem is more and more severe, the flood resistance is improved, the water environment is improved, the water ecology is repaired, the nationwide river growth is comprehensively promoted, the healthy life of rivers and lakes is maintained, and remarkable effects are obtained so far, because the frequency of manual river patrol is limited, the visual field is narrow, and the evidence obtaining capability for illegal behaviors is insufficient, a remote monitoring unmanned aerial vehicle is adopted to patrol the river to shoot pictures at the present stage, daily automatic patrol is carried out on a patrol river section, a route is fixed along two sides of a river channel for aerial photography, data are transmitted back to a command center in real time, the unmanned aerial vehicle is remotely monitored to patrol the pictures, and when abnormality occurs, the pictures can be taken for pollution sources and suspected illegal persons to obtain evidence;
in the prior art, unmanned aerial vehicle needs the manual butt joint charger interface of staff when the charging process, and the operation is comparatively troublesome to unmanned aerial vehicle takes off and land mostly is open-air take off and land, and unmanned aerial vehicle lacks the waterproof rain-proof protection device when stopping, leads to unmanned aerial vehicle to damage easily.
Disclosure of Invention
The invention aims to provide a water-utilizing unmanned aerial vehicle take-off and landing device, which at least solves the problems that in the charging process of the unmanned aerial vehicle in the prior art, workers need to manually butt a charger interface, the operation is troublesome, the unmanned aerial vehicle takes off and lands in the open air, and the unmanned aerial vehicle is easy to damage due to the lack of a waterproof and rainproof protection device when the unmanned aerial vehicle is parked.
In order to achieve the purpose, the invention provides the following technical scheme: a water utility drone take-off and landing apparatus comprising:
a box body;
the protection mechanism is arranged at the top end of the inner cavity of the box body;
the automatic butt joint mechanism is arranged on the front side of the bottom end of the inner cavity of the box body;
the rotating mechanism is arranged at the bottom end of the inner cavity of the box body and is positioned at the rear side of the automatic butt joint mechanism;
the storage battery is embedded in the left lower corner of the inner cavity of the box body;
the night indicator lamp is arranged at the center of the top end of the rear side of the box body through a bracket;
the tripod is detachably arranged at the center of the bottom end of the box body;
the water conservancy aerial photography unmanned aerial vehicle is placed at the top end of the rotating mechanism;
the controller is arranged at the center of the front side of the box body and is electrically connected with the storage batteries respectively.
Preferably, the automatic docking mechanism includes: the device comprises a first mounting seat, a first motor, a screw rod, a screw rod nut, a first guide rail and a first sliding block; the first mounting seat is arranged in front of the left of the inner cavity of the box body along the front-back direction; the first motor is arranged on the front side of the top end of the first mounting seat along the front-back direction and is electrically connected with the controller; the screw rod screw is in threaded connection with the output end of the first motor along the front-back direction; the screw nut is in threaded connection with the outer wall of the screw rod; the number of the first guide rails is two, and the two first guide rails are arranged on the left side and the right side of the top end of the first mounting seat along the front-back direction respectively; the number of the first sliding blocks is two, the number of the first sliding blocks in each group is two, and the first sliding blocks in two groups are respectively sleeved on the front side and the rear side of the outer wall of the left first guide rail and the outer wall of the right first guide rail.
Preferably, the automatic docking mechanism further includes: the second mounting seat, the second guide rail, the second sliding block, the top plate and the second electric push rod; the second mounting seats are arranged at the top ends of the left group and the right group along the left-right direction, and the lower surfaces of the second mounting seats are fixedly connected with the top ends of the screw nuts; the number of the second guide rails is two, and the two second guide rails are respectively arranged on the front side and the rear side of the top end of the second mounting seat along the left-right direction; the number of the second sliding blocks is two, the number of the second sliding blocks in each group is two, and the two groups of the second sliding blocks are respectively sleeved on the left side and the right side of the outer wall of the front second guide rail and the outer wall of the rear second guide rail; the top plate screws are connected to the top ends of the front and rear groups of second sliding blocks; the second electric push rod is arranged on the left side of the top end of the second mounting seat in the left-right direction, the right end of the second electric push rod is connected with the bottom end of the top plate through screws, and the second electric push rod is electrically connected with the controller.
Preferably, the automatic docking mechanism further includes: the device comprises a mounting frame, a charging plug and an induction probe; the mounting frame is arranged at the center of the top end of the top plate along the vertical direction; the charging plug is mounted at the top end of the side wall of the mounting rack through a support and is electrically connected with the storage battery; inductive probe installs the lateral wall of mounting bracket, inductive probe and controller electric connection.
Preferably, the rotating mechanism further includes: the rotating mechanism comprises a rotating mechanism shell, a rotating plate, a worm wheel, a second motor and a multi-thread worm; the rotating mechanism shell is arranged at the central position of the rear side of the bottom end of the inner cavity of the box body; the rotating plate is rotatably connected to the center of the top end of the inner cavity of the rotating mechanism shell through a bearing, an inner ring of the bearing is in interference fit with the outer wall of the rotating plate, and an outer ring of the bearing is fixedly connected with the inner wall of the rotating mechanism shell; the worm wheel screw is connected to the bottom end of the rotating plate; the second motor is arranged in the inner cavity of the rotating mechanism shell along the front-back direction and is electrically connected with the controller; the multi-thread worm is connected to the output end of the second motor along the front and back direction through screws, and the multi-thread worm is meshed with the worm wheel.
Compared with the prior art, the invention has the beneficial effects that: this water utilizes unmanned aerial vehicle take off and land device:
1. the left and right first electric push rods are shortened to pull the connecting seats at the corresponding positions to move outwards, so that the first electric push rods take the rotating connection positions with the pin shafts of the fixing frames as vertexes, the inner ends of the first electric push rods drive the connecting seats to rotate upwards, and the sealing cover plates at the corresponding positions are driven to rotate outwards by the cooperation of the connecting seats, so that the sealing cover plates can relieve the sealing of the top ends of the inner cavities of the box bodies, and the sealing of the sealing cover plates on the box bodies can be realized;
2. the multi-thread worm is driven by the second motor to rotate clockwise or anticlockwise, so that the worm wheel is driven to rotate clockwise or anticlockwise under the action of the rotating force of the multi-thread worm, and the worm wheel drives the outer charging port of the water conservancy aerial photography unmanned aerial vehicle to align to the direction of the front charging plug under the cooperation of the rotating plate;
3. the induction probe monitors the position of a charging port on the outer side of the water conservancy aerial photography unmanned aerial vehicle in the inner cavity of the box body and sends an azimuth signal to the inside of the controller, the second electric push rod shortens or extends by itself to push the top plate to drive the mounting frame to drive the charging plug to horizontally move to the right side or the left side to a designated position, the first motor drives the screw rod to rotate clockwise or anticlockwise, so that the screw nut drives the second mounting seat to be in a limiting effect of the second mounting seat under the action of the rotation force of the screw rod, and the second mounting seat drives the charging plug to be in butt joint with the charging port on the outer side of the water conservancy aerial photography unmanned aerial vehicle under the coordination of the second mounting seat, the second sliding block, the top plate;
thereby can realize when unmanned aerial vehicle charges, realize that the unmanned aerial vehicle interface docks with the outside charger is automatic, easy operation, labour saving and time saving to can prevent that unmanned aerial vehicle from damaging to the automatic waterproof rain-proof protection of unmanned aerial vehicle and can open automatically when unmanned aerial vehicle parks.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is an exploded view of the tank of FIG. 1;
FIG. 3 is an exploded view of the protection mechanism of FIG. 1;
FIG. 4 is an exploded view of the automatic docking mechanism of FIG. 1;
fig. 5 is an exploded view of the rotating mechanism of fig. 1.
In the figure: 1. the box, 2, protection mechanism, 21, the seat rotates, 22, sealed apron, 23, the mount, 24, first electric push rod, 25, the connecting seat, 4, automatic docking mechanism, 41, first mount pad, 42, first motor, 43, lead screw, 44, screw nut, 45, first guide rail, 46, first slider, 47, the second mount pad, 48, the second guide rail, 49, the second slider, 410, the roof, 411, the second electric push rod, 412, the mounting bracket, 413, charging plug, 414, inductive probe, 5, slewing mechanism, 51, slewing mechanism casing, 52, the rotor plate, 53, the worm wheel, 54, the second motor, 55, the multi-thread worm, 6, the battery, 7, the night pilot lamp, 8, the tripod, 9, the water conservancy is taken photo by plane unmanned aerial vehicle, 10, the controller.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: a water utility drone take-off and landing apparatus comprising: the water conservancy aerial photography system comprises a box body 1, a protection mechanism 2, an automatic butt joint mechanism 4, a rotating mechanism 5, a storage battery 6, a night indicator light 7, a tripod 8, a water conservancy aerial photography unmanned aerial vehicle 9 and a controller 10; the protection mechanism 2 is arranged at the top end of the inner cavity of the box body 1, and the sealing property of the interior of the box body 1 is good; the automatic butt-joint mechanism 4 is arranged on the front side of the bottom end of the inner cavity of the box body 1; the rotating mechanism 5 is arranged at the bottom end of the inner cavity of the box body 1 and is positioned at the rear side of the automatic butt joint mechanism 4; the storage battery 6 is embedded in the lower left corner of the inner cavity of the box body 1, the storage battery 6 is directly purchased, installed and used from the market according to actual use requirements, and the storage battery 6 can be connected with an external charger to supply power and charge electric devices inside the device and the water conservancy aerial photography unmanned aerial vehicle 9; the night indicating lamp 7 is installed at the center of the top end of the rear side of the box body 1 through a support, the night indicating lamp 7 is directly purchased from the market and installed and used according to actual use requirements in a specific use model, and the night indicating lamp 7 can conduct illumination guiding when the water conservancy aerial photography unmanned aerial vehicle 9 lands; the tripod 8 is detachably arranged at the center of the bottom end of the box body 1, so that the tripod 8 can be folded for storage; the water conservancy aerial photography unmanned aerial vehicle 9 is placed at the top end of the rotating mechanism 5, and the water conservancy aerial photography unmanned aerial vehicle 9 is directly purchased, installed and used from the market according to the actual use requirement; the controller 10 is arranged at the center of the front side of the box body 1, the controller 10 is electrically connected with the storage battery 6, and the specific use model of the controller 10 is directly purchased, installed and used from the market according to the actual use requirement.
Preferably, the automatic docking mechanism 4 further includes: a first mounting base 41, a first motor 42, a screw rod 43, a screw nut 44, a first guide rail 45 and a first sliding block 46; the first mounting seat 41 is arranged in front of the left of the inner cavity of the box body 1 along the front-back direction; the first motor 42 is arranged on the front side of the top end of the first mounting seat 41 along the front-back direction, the first motor 42 is electrically connected with the controller 10, the specific usage model of the first motor 42 is directly purchased from the market and installed and used according to the actual usage requirement, and the controller 10 can control the first motor 42 to drive the screw rod 43 to rotate clockwise or anticlockwise; the lead screw 43 is screwed to the output end of the first motor 42 in the front-rear direction; the screw nut 44 is screwed on the outer wall of the screw rod 43, and the screw nut 44 can drive the second mounting seat 47 to move towards the front side or towards the back side under the rotating force of the screw rod 43; the number of the first guide rails 45 is two, and the two first guide rails 45 are respectively arranged on the left side and the right side of the top end of the first mounting seat 41 along the front-back direction; the number of first slider 46 is two sets of, and the number of every first slider 46 of group is two, and two sets of first sliders 46 cup joint respectively in the outer wall front and back both sides of two first guide rails 45 about, and first slider 46 can slide around the outer wall of first guide rail 45.
Preferably, the automatic docking mechanism 4 further includes: a second mounting seat 47, a second guide rail 48, a second sliding block 49, a top plate 410 and a second electric push rod 411; the second mounting seats 47 are arranged at the top ends of the left and right groups 16 along the left-right direction, and the lower surfaces of the second mounting seats 47 are fixedly connected with the top ends of the screw nuts 44; the number of the second guide rails 48 is two, and the two second guide rails 48 are respectively arranged on the front side and the rear side of the top end of the second mounting seat 47 along the left-right direction; the number of the second sliding blocks 49 is two, the number of each group of the second sliding blocks 49 is two, the two groups of the second sliding blocks 49 are respectively sleeved on the left and right sides of the outer walls of the front and rear second guide rails 48, and the second sliding blocks 49 can slide left and right on the outer walls of the second guide rails 48; the top plate 410 is in screw connection with the top ends of the front and rear groups of second sliding blocks 49; the second electric push rod 411 is arranged on the left side of the top end of the second mounting seat 47 in the left-right direction, the right end of the second electric push rod 411 is in screw connection with the bottom end of the top plate 410, the second electric push rod 411 is electrically connected with the controller 10, the specific use model of the second electric push rod 411 is directly purchased, installed and used from the market according to actual use requirements, and the second electric push rod 411 can be controlled by the controller 10 to be shortened or extended through the second electric push rod 411 so as to push the top plate 410 to move towards the right side or towards the left side.
Preferably, the automatic docking mechanism 4 further includes: mounting block 412, charging plug 413, and inductive probe 414; the mounting frame 412 is arranged at the top center of the top plate 410 along the up-down direction; the charging plug 413 is installed at the top end of the side wall of the installation frame 412 through a support, the charging plug 413 is electrically connected with the storage battery 6, the charging plug 413 is specifically purchased and installed from the market and used according to actual use requirements, and the charging plug 413 is a magnetic connector so as to be connected and charged conveniently; inductive probe 414 installs the lateral wall at mounting bracket 412, inductive probe 414 and controller 10 electric connection, and inductive probe 414 specifically uses the model to require directly to purchase the installation and use from the market according to actual use, and inductive probe 414 can be controlled by controller 10 and monitor the box 1 inner chamber water conservancy unmanned aerial vehicle 9 outside position of charging, and inductive probe 414 is to the inside position signal that sends of controller 10.
Preferably, the rotating mechanism 5 further includes: a rotation mechanism housing 51, a rotation plate 52, a worm wheel 53, a second motor 54, and a multi-wire worm 55; the rotating mechanism shell 51 is arranged at the central position of the rear side of the bottom end of the inner cavity of the box body 1; the rotating plate 52 is rotatably connected to the center of the top end of the inner cavity of the rotating mechanism shell 51 through a bearing, an inner ring of the bearing is in interference fit with the outer wall of the rotating plate 52, and an outer ring of the bearing is fixedly connected with the inner wall of the rotating mechanism shell 51; the worm wheel 53 is screwed at the bottom end of the rotating plate 52; the second motor 54 is arranged in the inner cavity of the rotating mechanism shell 51 along the front-back direction, the second motor 54 is electrically connected with the controller 10, the specific usage model of the second motor 54 is directly purchased, installed and used from the market according to the actual usage requirement, and the controller 10 can control the second motor 54 to drive the multi-wire worm 55 to rotate clockwise or anticlockwise; the multi-wire worm 55 is screwed to an output terminal of the second motor 54 in the front-rear direction, the multi-wire worm 55 is engaged with the worm wheel 53, and the worm wheel 53 can be rotated clockwise or counterclockwise by the rotation force of the multi-wire worm 55.
Preferably, the protection mechanism 2 further includes: the sealing device comprises a rotating seat 21, a sealing cover plate 22, a fixing frame 23, a first electric push rod 24 and a connecting seat 25; the number of the rotating seats 21 is two, the number of each group of rotating seats 21 is several, and the two groups of rotating seats 21 are respectively arranged on the left side and the right side of the top end of the box body 1 from front to back in a clearance manner; the number of the sealing cover plates 22 is two, the two sealing cover plates 22 are respectively and rotatably connected to the inner sides of the left and right groups of rotating seats 21 through pin shafts, and the sealing cover plates 22 rotate outwards or inwards by taking the rotating connection positions of the pin shafts with the rotating seats 21 as vertexes; the number of the fixing frames 23 is two, the two fixing frames 23 are respectively installed at the top ends of the left side and the right side of the box body 1, the rotating connection position of the first electric push rod 24 and the fixing frame 23 is used as a vertex in the extending and shortening processes, and the inner end of the first electric push rod 24 drives the connecting seat 25 to slightly rotate upwards or downwards; the number of the first electric push rods 24 is two, one ends of the two first electric push rods 24 are respectively rotatably connected with the outer sides of the top ends of the left and right fixing frames 23 through pin shafts, the first electric push rods 24 are electrically connected with the controller 10, the specific use model of the first electric push rods 24 is directly purchased, installed and used from the market according to the actual use requirement, and the first electric push rods 24 can be controlled by the controller 10 to be stretched and shortened by themselves so as to pull the connecting seats 25 at the corresponding positions to move inwards or outwards; the number of the connecting seats 25 is two, the two connecting seats 25 are respectively installed at the center position of the outer side of the top ends of the left and right sealing cover plates 22, and the other ends of the left and right first electric push rods 24 are respectively connected with the left and right connecting seats 25 in a rotating manner through a pin shaft.
All the electrical components in the present application can be connected with an external adaptive power supply through a wire, and an adaptive external controller should be selected to connect according to specific actual use conditions to meet the control requirements of all the electrical components, and the specific connection mode and the control sequence thereof should be referred to in the following working principle that the electrical components are electrically connected in sequence, the detailed connection means thereof is a known technology in the art and is not described, and the following main description of the working principle and the process specifically works as follows.
Step 1: during takeoff, a worker fixes the tripod 8 at a designated take-off and landing position, and controls the controller 10 to start the left and right first electric push rods 24, so that the left and right first electric push rods 24 are shortened by the worker to pull the connecting seat 25 at the corresponding position to move outwards, because the inner side and the outer side of the first electric push rod 24 are respectively and rotatably connected with the connecting seat 25 and the fixing frame 23 through pin shafts, and the fixing frame 22 is rotatably connected with the fixing frame 21 through the pin shafts, so that the rotating connection position of the first electric push rod 24 and the fixing frame 23 is taken as a vertex in the shortening process, the inner end of the first electric push rod 24 drives the connecting seat 25 to slightly rotate upwards, and the sealing cover plate 22 at the corresponding position is driven to rotate outwards by taking the rotating connection position of the pin shaft of the rotating seat 21 as the vertex under the cooperation of the connecting seat 25;
step 2: after aerial photography, the water conservancy aerial photography unmanned aerial vehicle 9 descends in the inner cavity of the box body 1 under the guidance of the night indicator lamp 7, the staff control controller 10 starts the second motor 54, so that the second motor 54 drives the multi-thread worm 55 to rotate clockwise or anticlockwise, and as the worm wheel 53 is meshed with the multi-thread worm 55, the worm wheel 53 is driven to rotate clockwise or anticlockwise under the action of the rotating force of the multi-thread worm 55, and further the worm wheel 53 drives the outer side charging port of the water conservancy aerial photography unmanned aerial vehicle 9 to align to the direction of the front side charging plug 413 under the coordination of the rotating plate 52;
and step 3: when the water conservancy aerial photography unmanned aerial vehicle 9 is charged, a worker controls the controller 10 to start the induction probe 414, the induction probe 414 monitors the position of a charging port on the outer side of the water conservancy aerial photography unmanned aerial vehicle 9 in the inner cavity of the box body 1, the induction probe 414 sends an orientation signal to the inside of the controller 10 to enable the controller 10 to start the second electric push rod 411 and the first motor 42 in sequence, the second electric push rod 411 shortens or extends through itself to push the top plate 410 to move towards the right side or the left side, further the top plate 410 drives the mounting frame 412 to drive the charging plug 413 to horizontally move towards the right side or the left side to a specified position under the limiting action of the second sliding block 49, the first motor 42 drives the lead screw 43 to rotate clockwise or anticlockwise, and due to the threaded connection between the lead screw nut 44 and the lead screw 43, the lead screw nut 44 drives the second mounting seat 47 to move towards the front side or the back side under the, further, the second mounting seat 47 is under the limiting effect of the second mounting seat 46, so that the second mounting seat 47 drives the charging plug 413 to be in butt joint with the outer charging port of the water conservancy aerial photography unmanned aerial vehicle 9 under the matching of the second mounting seat 48, the second sliding block 49, the top plate 410 and the mounting frame 412 for charging;
thereby can realize when unmanned aerial vehicle charges, realize that the unmanned aerial vehicle interface docks with the outside charger is automatic, easy operation, labour saving and time saving to can prevent that unmanned aerial vehicle from damaging to the automatic waterproof rain-proof protection of unmanned aerial vehicle and can open automatically when unmanned aerial vehicle parks.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides a water utilizes unmanned aerial vehicle take off and land device which characterized in that includes:
a box body (1);
the protection mechanism (2) is arranged at the top end of the inner cavity of the box body (1);
the automatic butt joint mechanism (4) is arranged on the front side of the bottom end of the inner cavity of the box body (1);
the rotating mechanism (5) is arranged at the bottom end of the inner cavity of the box body (1) and is positioned at the rear side of the automatic butt joint mechanism (4);
the storage battery (6) is embedded in the left lower corner of the inner cavity of the box body (1);
the night indicator lamp (7) is arranged at the center of the top end of the rear side of the box body (1) through a bracket;
the tripod (8) is detachably arranged at the center of the bottom end of the box body (1);
the water conservancy aerial photography unmanned aerial vehicle (9) is placed at the top end of the rotating mechanism (5);
the controller (10) is arranged at the center of the front side of the box body (1), and the controller (10) is electrically connected with the storage battery (6) respectively.
2. The unmanned aerial vehicle take-off and landing device for water conservancy of claim 1, wherein: the automatic docking mechanism (4) comprises:
the first mounting seat (41) is arranged in the front left of the inner cavity of the box body (1) along the front-back direction;
the first motor (42) is arranged on the front side of the top end of the first mounting seat (41) along the front-back direction, and the first motor (42) is electrically connected with the controller (10);
a screw rod (43) screwed to the output end of the first motor (42) in the front-rear direction;
a screw nut (44) screwed to the outer wall of the screw rod (43);
the number of the first guide rails (45) is two, and the two first guide rails (45) are respectively arranged on the left side and the right side of the top end of the first mounting seat (41) along the front-back direction;
the number of the first sliding blocks (46) is two, the number of the first sliding blocks (46) in each group is two, and the first sliding blocks (46) in each group are respectively sleeved on the front side and the rear side of the outer wall of the left first guide rail and the outer wall of the right first guide rail (45).
3. The unmanned aerial vehicle take-off and landing device for water conservancy of claim 1, wherein: the automatic docking mechanism (4) further comprises:
the second mounting seats (47) are arranged at the top ends of the left group (16) and the right group (16) along the left-right direction, and the lower surfaces of the second mounting seats (47) are fixedly connected with the top ends of the screw nuts (44);
the number of the second guide rails (48) is two, and the two second guide rails (48) are respectively arranged on the front side and the rear side of the top end of the second mounting seat (47) along the left-right direction;
the number of the second sliding blocks (49) is two, the number of the second sliding blocks (49) in each group is two, and the two groups of the second sliding blocks (49) are respectively sleeved on the left side and the right side of the outer wall of the front second guide rail (48) and the right side of the outer wall of the rear second guide rail (48);
the top plate (410) is connected to the top ends of the front and rear groups of second sliding blocks (49) through screws;
second electric putter (411), set up along left right direction the top left side of second mount pad (47), the right-hand member of second electric putter (411) and the bottom screwed connection of roof (410), second electric putter (411) and controller (10) electric connection.
4. The unmanned aerial vehicle take-off and landing device for water conservancy of claim 1, wherein: the automatic docking mechanism (4) further comprises:
a mounting frame (412) which is arranged at the center position of the top end of the top plate (410) along the vertical direction;
the charging plug (413) is installed at the top end of the side wall of the mounting frame (412) through a support, and the charging plug (413) is electrically connected with the storage battery (6);
the induction probe (414) is arranged on the side wall of the mounting rack (412), and the induction probe (414) is electrically connected with the controller (10).
5. The unmanned aerial vehicle take-off and landing device for water conservancy of claim 1, wherein: the rotating mechanism (5) further comprises:
the rotating mechanism shell (51) is arranged at the central position of the rear side of the bottom end of the inner cavity of the box body (1);
the rotating plate (52) is rotatably connected to the center of the top end of the inner cavity of the rotating mechanism shell (51) through a bearing, an inner ring of the bearing is in interference fit with the outer wall of the rotating plate (52), and an outer ring of the bearing is fixedly connected with the inner wall of the rotating mechanism shell (51);
a worm wheel (53) screwed to the bottom end of the rotating plate (52);
the second motor (54) is arranged in the inner cavity of the rotating mechanism shell (51) along the front-back direction, and the second motor (54) is electrically connected with the controller (10);
and the multi-wire worm (55) is connected to the output end of the second motor (54) in a screw mode in the front-back direction, and the multi-wire worm (55) is meshed with the worm wheel (53).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011095254.8A CN112249355A (en) | 2020-10-14 | 2020-10-14 | Unmanned aerial vehicle take-off and landing device for water conservancy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011095254.8A CN112249355A (en) | 2020-10-14 | 2020-10-14 | Unmanned aerial vehicle take-off and landing device for water conservancy |
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| Publication Number | Publication Date |
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| CN112249355A true CN112249355A (en) | 2021-01-22 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202011095254.8A Withdrawn CN112249355A (en) | 2020-10-14 | 2020-10-14 | Unmanned aerial vehicle take-off and landing device for water conservancy |
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| CN (1) | CN112249355A (en) |
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| CN115743660A (en) * | 2022-12-05 | 2023-03-07 | 无锡格物智能科技有限公司 | Double-cabin unmanned aerial vehicle hangar |
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Application publication date: 20210122 |