CN113799995A - Intelligent iron tower service station for midway transduction of rotary wing type unmanned aerial vehicle - Google Patents
Intelligent iron tower service station for midway transduction of rotary wing type unmanned aerial vehicle Download PDFInfo
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- CN113799995A CN113799995A CN202110923406.7A CN202110923406A CN113799995A CN 113799995 A CN113799995 A CN 113799995A CN 202110923406 A CN202110923406 A CN 202110923406A CN 113799995 A CN113799995 A CN 113799995A
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 title claims abstract description 86
- 229910052742 iron Inorganic materials 0.000 title claims abstract description 43
- 230000026683 transduction Effects 0.000 title claims abstract description 20
- 238000010361 transduction Methods 0.000 title claims abstract description 20
- 230000003139 buffering effect Effects 0.000 claims abstract description 8
- 238000009434 installation Methods 0.000 claims abstract description 3
- 230000005611 electricity Effects 0.000 claims description 22
- 239000000428 dust Substances 0.000 claims description 21
- 230000005540 biological transmission Effects 0.000 claims description 12
- 230000008901 benefit Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 230000005484 gravity Effects 0.000 description 3
- 238000013459 approach Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 210000001503 joint Anatomy 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000008054 signal transmission Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002457 bidirectional effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
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Classifications
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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
-
- 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
- B60L53/12—Inductive energy transfer
-
- 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
- B60L53/60—Monitoring or controlling charging stations
- B60L53/66—Data transfer between charging stations and vehicles
-
- 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
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
-
- 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/05—Programmable logic controllers, e.g. simulating logic interconnections of signals according to ladder diagrams or function charts
- G05B19/054—Input/output
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
- H02J7/0045—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction concerning the insertion or the connection of the batteries
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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
- Y02T90/16—Information or communication technologies improving the operation of electric vehicles
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Manufacturing & Machinery (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention relates to the technical field of service stations for transduction of unmanned aerial vehicles, in particular to an intelligent iron tower service station for midway transduction of a rotary wing type unmanned aerial vehicle, which comprises a base (1), a positioning assembly (4), a quick charging assembly (5) and a buffer assembly (9); an iron tower (2) is arranged on the upper surface of the base (1), a top plate (3) is arranged on the upper surface of the iron tower (2), and symmetrically arranged sliding grooves are formed in the middle of the top plate (3); the positioning component (4) is connected to the inside of the sliding groove in a sliding manner; the quick charging assembly (5) is fixedly connected to the inner wall of a through hole formed in the center of the top plate (3), and the upper end of the quick charging assembly (5) is located above the upper surface of the top plate (3); buffering subassembly (9) set up in the upper surface of roof (3), buffering subassembly (9) respectively with locating component (4) and quick charge subassembly (5) cooperation installation. The invention has the advantages of high reliability, wide application range, long service life and the like.
Description
Technical Field
The invention relates to the technical field of service stations for transduction of unmanned aerial vehicles, in particular to an intelligent iron tower service station for the medium transduction of a rotary wing type unmanned aerial vehicle.
Background
Along with the development of science and technology, in the life production process, rotor unmanned aerial vehicle's application range is more and more extensive. For example, the electric power department uses rotor unmanned aerial vehicle to patrol and inspect the overhead cable, or uses rotor unmanned aerial vehicle to explore road conditions and so on, rotor unmanned aerial vehicle can exert self advantage in many cases and help people to accomplish specific tasks, current rotor unmanned aerial vehicle who uses battery powered is because the electric quantity restriction, flight time is shorter, it is difficult to accomplish the task under long distance and the long-time condition, even increase battery capacity, but also can not bring the extension of flight time because of the increase of loading capacity, if need can charge the transduction in-process of flying, then can increase rotor unmanned aerial vehicle's working range and efficiency by a wide margin, for this reason, we provide a rotor unmanned aerial vehicle intelligent iron tower service station for midway transduction.
Disclosure of Invention
The invention aims to overcome the existing defects and provides an intelligent iron tower service station for energy conversion in a rotary wing type unmanned aerial vehicle, which is simple and convenient to operate, high in reliability and wide in application range, avoids misoperation, prolongs the service life and can effectively solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: an intelligent iron tower service station for midway energy conversion of a rotary wing type unmanned aerial vehicle comprises a base, a positioning assembly, a quick charging assembly and a buffering assembly;
an iron tower is arranged on the upper surface of the base, a top plate is arranged on the upper surface of the iron tower, and symmetrically arranged sliding grooves are formed in the middle of the top plate;
the positioning assembly is connected to the inside of the sliding groove in a sliding manner;
the quick charging assembly is fixedly connected to the inner wall of the through hole formed in the center of the top plate, and the upper end of the quick charging assembly is located above the upper surface of the top plate;
buffering subassembly sets up in the upper surface of roof, and buffering subassembly cooperates the installation with locating component and quick charging subassembly respectively, prevents that the surface of wireless charger from gathering the dust and influencing the charging effect, increase of service life can detect rotor unmanned aerial vehicle's the state of rising and falling, and easy operation is convenient, avoids appearing the maloperation, carries out accurate location with rotor unmanned aerial vehicle, avoids because the inaccurate phenomenon that leads to can't charging in location, and the reliability is high, and application scope is wide.
Further, still include solar photovoltaic board and electric cabinet, the solar photovoltaic board passes through the support and sets up in the upper end right flank of iron tower, the electric cabinet sets up in the upper surface of base, and the inside of electric cabinet is equipped with battery and PLC controller respectively, the input of battery is connected to the output electricity of solar photovoltaic board, and the input of PLC controller is connected to the output electricity of battery, generates electricity through solar energy, energy saving, green.
Furthermore, the positioning assembly comprises a T-shaped sliding plate, a supporting block and a first electric push rod, wherein a vertical plate body of the T-shaped sliding plate is respectively in sliding connection with the inner wall of the sliding groove corresponding to the top plate, connecting balls are respectively arranged at the lower end of the T-shaped sliding plate, the supporting block is arranged at the center of the lower surface of the top plate, return springs are respectively arranged on the side surfaces of the supporting block, the outer side ends of the return springs are respectively and fixedly connected with the outer arc surfaces of the adjacent connecting balls, the first electric push rod is fixedly connected with a fixing plate arranged on the left side of the front end of the lower surface of the top plate, a tightening belt is fixedly connected with the end of the first electric push rod far away from the lower surface of the top plate, guide rollers are symmetrically arranged on the left side of the front end of the lower surface of the top plate, the end of the tightening belt far away from the first electric push rod is fixedly connected with the outer arc surfaces of the guide rollers on the rear side, and the outer arc surfaces of the tightening belt are in sliding connection with the guide rollers on the front side, the surface in tightening band in proper order with the through-hole inner wall sliding connection that four connection ball insides set up, the output of PLC controller is connected to first electric putter's input electricity, carries out accurate location to rotor unmanned aerial vehicle after falling, is convenient for charge smoothly.
Further, the buffering subassembly includes pressure sensor and platen, pressure sensor fixed connection is respectively in the mounting hole bottom surface of roof upper surface four corners setting, pressure sensor's upper surface all is equipped with buffer spring, buffer spring's top all is connected with the lower fixed surface of platen, the input of PLC controller is connected to the equal electricity of pressure sensor's output, the inside of platen is equipped with the logical groove that corresponds with T type slide position, reduce the impact force of rotor unmanned aerial vehicle descending in-process, and stability is improved, detects rotor unmanned aerial vehicle simultaneously.
Further, the quick charge subassembly includes second electric putter and wireless charger, second electric putter fixed connection is in the through-hole inner wall that roof center set up, the outside cambered surface of second electric putter and the inside round hole inner wall fixed connection that sets up of supporting shoe, wireless charger sets up in second electric putter's push rod top, wireless charger is located the upper surface top of roof, and the hole position of dodging that wireless charger and platen center set up corresponds, and the output of PLC controller is connected to the equal electricity of input of second electric putter and wireless charger, adopts liftable structure to be convenient for dock with unmanned aerial vehicle's the head that charges fast, and operation is simple and convenient, avoids appearing the phenomenon that the butt joint is not in place.
Further, still include GPRS data transmission ware, GPRS data transmission ware sets up in the inside bottom surface of automatically controlled case, and GPRS data transmission ware is connected with the two-way electricity of PLC controller, makes things convenient for long-range manual control, is convenient for maintain.
Further, still include slide rail, dust cover and third electric putter, the dust cover hinges in the front and back side of roof through the hinge respectively, the slide rail sets up respectively in the lower surface of dust cover, third electric putter has two, and two third electric putter's lower extreme passes through U type connector rotation with the backup pad that iron tower upper end front and back side set up respectively and is connected, and two third electric putter's upper end passes through U type connector rotation with slide rail lower surface sliding connection's slider respectively and is connected, and the input electricity of third electric putter links the output of PLC controller, prevents that the surface of wireless charger from gathering the dust and influencing the effect of charging, prolongs life.
Further, the telescopic rod is arranged on the outer side face of the supporting block, the outer end of the telescopic rod is fixedly connected with the outer arc face of the connecting ball on the same side, and the telescopic rod is located inside the adjacent reset springs respectively, so that the stability of the T-shaped sliding plate during sliding is improved.
Furthermore, the bird repeller is arranged at the upper end of the left side face of the iron tower and is a wind-driven bird repeller, so that birds are prevented from nesting in the iron tower.
Compared with the prior art, the invention has the beneficial effects that: this intelligent iron tower service station is used in midway transduction of rotor type unmanned aerial vehicle has following benefit:
1. when rotor unmanned aerial vehicle need charge, send a signal to outside terminal equipment, outside terminal equipment gives the PLC controller with signal transmission through GPRS data transmission ware, two third electric putter of PLC controller control are opened, third electric putter's push rod shrink drives the dust cover rotatory along the hinge, the top that makes the platen is not sheltered from, charge the completion back, third electric putter starts to promote the dust cover rotatory, two dust cover closures seal the platen, prevent that the surface of wireless charger from gathering the dust and influencing the effect of charging, increase of service life.
2. Rotor unmanned aerial vehicle descends the upper surface at the platen, the platen is because rotor unmanned aerial vehicle's gravity extrudees buffer spring downwards, buffer spring has reduced the impact force when rotor unmanned aerial vehicle descends, the pressure value increase that pressure sensor detected, pressure sensor transmits pressure signal for the PLC controller, when PLC controller detects pressure sensor's pressure stability, judge that rotor unmanned aerial vehicle steadily descends, rotor unmanned aerial vehicle plays the back of flying, the pressure on pressure sensor surface reduces this moment, the PLC controller judges that rotor unmanned aerial vehicle leaves, detect rotor unmanned aerial vehicle, the operation is thus simple and convenient, avoid appearing the maloperation.
3. The first electric putter of PLC controller control starts, and first electric putter's push rod drives the one end removal in tightening belt, and tightening belt drives four and connects the ball and draw close to the supporting shoe, connects the ball simultaneously and drives the T type slide rather than fixed connection and draw close to the supporting shoe, carries out accurate location with rotor unmanned aerial vehicle, avoids because the inaccurate phenomenon that leads to can' T charging in location, and the reliability is high.
4. PLC controller starts second electric putter, and second electric putter's push rod drives wireless charger and shifts up, and wireless charger charges to it with rotor unmanned aerial vehicle's the end contact that charges, but the rotor unmanned aerial vehicle of different heights of practicality charges and uses, has improved application scope.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of a positioning assembly according to the present invention;
FIG. 3 is a schematic view of a buffer assembly according to the present invention;
FIG. 4 is a schematic plan view of the present invention in partial section;
FIG. 5 is an enlarged view of the structure of the present invention at A.
In the figure: the device comprises a base 1, an iron tower 2, a top plate 3, a positioning assembly 4, a sliding plate 41T, a connecting ball 42, a supporting block 43, a return spring 44, a tightening belt 45, a first electric push rod 46, a quick charging assembly 5, a second electric push rod 51, a wireless charger 52, a sliding rail 6, a PLC (programmable logic controller) 7, a GPRS (general packet radio service) data transmitter 8, a buffer assembly 9, a pressure sensor 91, a buffer spring 92, a bedplate 93, a dust cover 10, a third electric push rod 11, a bird repeller 12, a solar photovoltaic panel 13, an electric control box 14, a storage battery 15, a telescopic rod 16 and a guide roller 17.
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 embodiment provides a technical solution: an intelligent iron tower service station for midway transduction of a rotary wing type unmanned aerial vehicle comprises a base 1, a positioning assembly 4, a quick charging assembly 5 and a buffer assembly 9;
referring to fig. 1, an iron tower 2 and an electric cabinet 14 are arranged on the upper surface of a base 1, a top plate 3 is arranged on the upper surface of the iron tower 2, and two sets of symmetrically arranged sliding chutes are arranged in the middle of the top plate 3; iron tower 2's upper end right flank is equipped with the support, be equipped with solar photovoltaic board 13 on the support, electric cabinet 14's inside is equipped with battery 15 and PLC controller 7 respectively, battery 15's input is connected to solar photovoltaic board 13's output electricity, battery 15's input is connected through a solar controller electricity to solar photovoltaic board 13's output when concrete implementation, PLC controller 7's input is connected to battery 15's output electricity, generate electricity through solar energy, energy saving, green.
Referring to fig. 1-2, the positioning assembly 4 is slidably connected in the sliding slot of the top plate 3, the positioning assembly 4 includes four T-shaped sliding plates 41, a supporting block 43 and a first electric push rod 46, the vertical plates of the T-shaped sliding plates 41 are respectively slidably connected with the inner walls of the sliding slots corresponding to the top plate 3, the lower ends of the T-shaped sliding plates 41 are respectively provided with a connecting ball 42, the supporting block 43 is disposed at the center of the lower surface of the top plate 3, the side surfaces of the supporting block 43 are respectively provided with four return springs 44, the outer ends of the return springs 44 are respectively fixedly connected with the outer arc surfaces of the adjacent connecting balls 42, the first electric push rod 46 is fixedly connected with a fixing plate (not shown) disposed at the left side of the front end of the lower surface of the top plate 3, the end of the push rod of the first electric push rod 46 is fixedly connected with a tightening belt 45, the tightening belt 45 is made of a metal alloy thin plate with elastic deformation, the left side of the front end of the lower surface of the top plate 3 is symmetrically provided with the guide rollers 17, end that first electric putter 46 was kept away from to take 45 and the guide roll 17 extrados fixed connection of rear side tighten up, the lateral surface of taking 45 and the guide roll 17 extrados sliding connection of front side, the one end that first electric putter 46 was kept away from to take 45 is in proper order with the inside through-hole inner wall sliding connection who sets up of four connecting balls 42, PLC controller 7's output is connected to first electric putter 46's input electricity, PLC controller 7 controls first electric putter 46 and starts, the push rod of first electric putter 46 drives the one end removal of taking 45 of tightening up, take 45 to drive four connecting balls 42 and draw close to supporting shoe 43, connecting ball 42 simultaneously drives and draws close to supporting shoe 43 rather than fixed connection's T type slide 41, thereby carry out accurate location with rotor unmanned aerial vehicle, it charges to advance smoothly.
Referring to fig. 2, the telescopic rod 16 is disposed in the return spring 44, and two ends of the telescopic rod 16 are respectively and fixedly connected with the support block 43 and the connecting ball 42, so that the structural design can prevent the problem of deflection in the process of compressing the return spring 44, and improve the stability of the T-shaped sliding plate 41 during sliding.
Referring to fig. 3-5, the fast charging assembly 5 is fixedly connected to an inner wall of a through hole formed in the center of the top plate 3, the upper end of the fast charging assembly 5 is located above the upper surface of the top plate 3, the fast charging assembly 5 includes a second electric push rod 51 and a wireless charger 52, the second electric push rod 51 is fixedly connected to the inner wall of the through hole formed in the center of the top plate 3, an outer arc surface of the second electric push rod 51 is fixedly connected to an inner wall of a circular hole formed in the supporting block 43, the wireless charger 52 is arranged at the top end of the push rod of the second electric push rod 51, the wireless charger 52 is located above the upper surface of the top plate 3, the PLC controller 7 starts the second electric push rod 51, the push rod of the second electric push rod 51 drives the wireless charger 52 to move upwards, the wireless charger 52 contacts with the charging end of the rotor unmanned aerial vehicle to charge the rotor vehicle, and a liftable structure is adopted to facilitate rapid docking with the charging head of the unmanned aerial vehicle, the operation is simple and convenient, and the phenomenon of improper butt joint is avoided.
Referring to fig. 3-5, a buffer assembly 9 is disposed on the upper surface of the top plate 3, the buffer assembly 9 is respectively installed in cooperation with the positioning assembly 4 and the fast charging assembly 5, the buffer assembly 9 includes a pressure sensor 91 and a platen 93, the pressure sensor 91 is respectively and fixedly connected to the bottom surfaces of mounting holes disposed at four corners of the upper surface of the top plate 3, buffer springs 92 are disposed on the upper surface of the pressure sensor 91, the top ends of the buffer springs 92 are respectively and fixedly connected to the lower surface of the platen 93, the output end of the pressure sensor 91 is electrically connected to the input end of the PLC controller 7, a through groove corresponding to the T-shaped sliding plate 41 is disposed inside the platen 93, the wireless charger 52 corresponds to an avoidance hole disposed in the center of the platen 93, the input ends of the second electric push rod 51 and the wireless charger 52 are electrically connected to the output end of the PLC controller 7, and the unmanned rotorcraft lands on the upper surface of the platen 93, platen 93 is because rotor unmanned aerial vehicle's gravity extrudees buffer spring 92 downwards, the pressure value increase that pressure sensor 91 detected, pressure sensor 91 gives PLC controller 7 with pressure signal transmission, when PLC controller 7 detected pressure sensor 91's pressure stability, judge that rotor unmanned aerial vehicle steadily descends, reduce the impact force of rotor unmanned aerial vehicle descending in-process, improve stability, detect rotor unmanned aerial vehicle simultaneously.
Please refer to fig. 4, further including a slide rail 6, a dust cover 10 and two third electric push rods 11, the dust cover 10 is hinged to the front and rear side surfaces of the top plate 3 through hinges, the slide rail 6 is disposed on the lower surface of the dust cover 10, the number of the third electric push rods 11 is two, the lower ends of the two third electric push rods 11 are rotatably connected with the supporting plate disposed on the front and rear side surfaces of the upper end of the iron tower 2 through U-shaped connectors, the upper ends of the two third electric push rods 11 are rotatably connected with the sliding blocks slidably connected to the lower surface of the slide rail 6 through U-shaped connectors, the input end of the third electric push rod 11 is electrically connected with the output end of the PLC controller 7, thereby preventing the surface of the wireless charger 52 from collecting dust to affect the charging effect and prolonging the service life.
Referring to fig. 1, the electronic control box further includes a GPRS data transmitter 8, the GPRS data transmitter 8 is disposed on the bottom surface of the interior of the electronic control box 14, and the GPRS data transmitter 8 is electrically connected to the PLC controller 7 in a bidirectional manner, so that remote manual control and maintenance are facilitated.
Referring to fig. 1, the bird repeller 12 is further included, the bird repeller 12 is arranged at the upper end of the left side face of the iron tower 2, the bird repeller 12 is a wind-driven bird repeller, birds are repelled under the action of wind, nesting of the birds on the iron tower is avoided, and the service life of the iron tower service station is prolonged.
The working principle of the intelligent iron tower service station for midway transduction of the rotor type unmanned aerial vehicle provided by the invention is as follows:
when the unmanned gyroplane needs to be charged, a signal is sent to an external terminal device, the external terminal device sends the signal to the PLC controller 7 through the GPRS data transmitter 8, the PLC controller 7 controls the two third electric push rods 11 to be opened, the push rods of the third electric push rods 11 contract to drive the dust cover 10 to rotate along the hinge, so that the upper part of the bedplate 93 is not shielded, the unmanned gyroplane lands on the upper surface of the bedplate 93, the bedplate 93 downwards extrudes the buffer spring 92 due to the gravity of the unmanned gyroplane, the pressure value detected by the pressure sensor 91 is increased, the pressure sensor 91 transmits the pressure signal to the PLC controller 7, when the PLC controller 7 detects that the pressure of the pressure sensor 91 is stable, the unmanned gyroplane is judged to land stably, at the moment, the PLC controller 7 controls the first electric push rod 46 to be started, the push rod of the first electric push rod 46 drives one end of the tightening belt 45 to move, the tightening belt 45 drives the four connecting balls 42 to approach the supporting block 43, the connecting balls 42 drive the T-shaped sliding plate 41 fixedly connected with the connecting balls to approach the supporting block 43, so that the rotor unmanned aerial vehicle is accurately positioned, then the PLC controller 7 starts the second electric push rod 51, the push rod of the second electric push rod 51 drives the wireless charger 52 to move upwards, the wireless charger 52 is contacted with the charging end of the rotor unmanned aerial vehicle to charge the rotor unmanned aerial vehicle, after the charging is completed, the PLC controller 7 controls the first electric push rod 46 to move reversely, the tightening belt 45 is released, the reset spring 44 drives the connecting balls 42 to reset at the moment, so that the T-shaped sliding plate 41 relieves the limitation on the rotor unmanned aerial vehicle, the rotor unmanned aerial vehicle takes off, the pressure on the surface of the pressure sensor 91 is reduced at the moment, and the PLC controller 7 controls the second electric push rod 51 and the wireless charger 52 to reset after judging that the rotor unmanned aerial vehicle leaves, meanwhile, the third electric push rod 11 is started to push the dust covers 10 to rotate, the two dust covers 10 are closed to seal the bedplate 93, dust is prevented from being accumulated on the surface of the wireless charger 52 to affect the charging effect, and the service life is prolonged.
It should be noted that the first electric putter 46, the second electric putter 51, the wireless charger 52, the GPRS data transmitter 8 and the third electric putter 11 disclosed in the above embodiments may be freely configured according to practical application scenarios, the first electric putter 46 is suggested to be a WDTW type micro electric putter, the GPRS data transmitter 8 is suggested to be an MGTC-30214G all-network data transmission module, and the PLC controller 7 controls the first electric putter 46, the second electric putter 51, the wireless charger 52, the GPRS data transmitter 8 and the third electric putter 11 to operate by a method commonly used in the prior art.
Example two
The structure of the first embodiment is basically the same, except that: the rear side of the solar photovoltaic panel 13 is provided with a spherical shell 18, the outer side of the spherical shell 18 is provided with an arc-shaped rack 19 and a plurality of groups of pulleys 20, the support comprises a front support 21 and a rear support 22 which are hinged with each other, a first motor 23 is fixedly assembled on the front support 21, an output shaft of the first motor 23 is provided with a first main transmission gear 24, the end part of the rear support 22 close to the front support 21 is provided with a first driven gear 25, the first main transmission gear 24 is in meshing transmission with the first driven gear 25, and the first motor 23 is driven by the first main transmission gear 24 and the first driven gear 25
The upper surface of the base 1 is provided with an iron tower 2 and an electric cabinet 14, the upper surface of the iron tower 2 is provided with a top plate 3, and the middle part of the top plate 3 is provided with two groups of symmetrically arranged sliding chutes; iron tower 2's upper end right flank is equipped with the support, be equipped with solar photovoltaic board 13 on the support, electric cabinet 14's inside is equipped with battery 15 and PLC controller 7 respectively, battery 15's input is connected to solar photovoltaic board 13's output electricity, battery 15's input is connected through a solar controller electricity to solar photovoltaic board 13's output during concrete implementation, PLC controller 7's input is connected to battery 15's output electricity, generate electricity through solar energy, the energy can be saved, green
The above description is only an embodiment of the present invention, and not intended to limit the scope of the present invention, and all modifications of equivalent structures and equivalent processes, which are made by using the contents of the present specification and the accompanying drawings, or directly or indirectly applied to other related technical fields, are included in the scope of the present invention.
Claims (9)
1. The utility model provides a midway transduction of rotor type unmanned aerial vehicle is with intelligent iron tower service station which characterized in that: comprises a base (1), a positioning component (4), a quick charging component (5) and a buffer component (9);
an iron tower (2) is arranged on the upper surface of the base (1), a top plate (3) is arranged on the upper surface of the iron tower (2), and symmetrically arranged sliding grooves are formed in the middle of the top plate (3);
the positioning component (4) is connected to the inside of the sliding groove in a sliding manner;
the quick charging assembly (5) is fixedly connected to the inner wall of a through hole formed in the center of the top plate (3), and the upper end of the quick charging assembly (5) is located above the upper surface of the top plate (3);
buffering subassembly (9) set up in the upper surface of roof (3), buffering subassembly (9) respectively with locating component (4) and quick charge subassembly (5) cooperation installation.
2. The intelligent iron tower service station for midway transduction of rotor type unmanned aerial vehicle of claim 1, which is characterized in that: still include solar photovoltaic board (13) and electric cabinet (14), solar photovoltaic board (13) set up in the upper end right flank of iron tower (2) through the support, electric cabinet (14) set up in the upper surface of base (1), and the inside of electric cabinet (14) is equipped with battery (15) and PLC controller (7) respectively, the input of battery (15) is connected to the output electricity of solar photovoltaic board (13), and the input of PLC controller (7) is connected to the output electricity of battery (15).
3. The intelligent iron tower service station for midway transduction of rotor type unmanned aerial vehicle of claim 2, wherein: the positioning assembly (4) comprises a T-shaped sliding plate (41), a supporting block (43) and a first electric push rod (46), wherein a vertical plate body of the T-shaped sliding plate (41) is in sliding connection with the inner wall of a sliding groove corresponding to the top plate (3) respectively, a connecting ball (42) is arranged at the lower end of the T-shaped sliding plate (41), the supporting block (43) is arranged at the center of the lower surface of the top plate (3), a reset spring (44) is arranged on the side surface of the supporting block (43), the outer end of the reset spring (44) is fixedly connected with the outer arc surface of the adjacent connecting ball (42), the first electric push rod (46) is fixedly connected with a fixing plate arranged on the left side of the front end of the lower surface of the top plate (3), a tightening belt (45) is fixedly connected with the end of the first electric push rod (46), guide rollers (17) are symmetrically arranged on the left side of the front end of the lower surface of the top plate (3), and the end, far away from the first electric push rod (46) of the tightening belt (45) is fixedly connected with the outer arc surface of the guide rollers (17) on the rear side The outer side face of the tightening belt (45) is connected with the outer arc face of the guide roller (17) on the front side in a sliding mode, the outer surface of the tightening belt (45) is sequentially connected with the inner wall of the through hole formed in the four connecting balls (42) in a sliding mode, and the input end of the first electric push rod (46) is electrically connected with the output end of the PLC controller (7).
4. The intelligent iron tower service station for midway transduction of rotor type unmanned aerial vehicle of claim 3, wherein: buffer unit (9) include pressure sensor (91) and platen (93), pressure sensor (91) fixed connection respectively is in the mounting hole bottom surface of roof (3) upper surface four corners setting, and the upper surface of pressure sensor (91) all is equipped with buffer spring (92), and the top of buffer spring (92) all is connected with the lower fixed surface of platen (93), and the input of PLC controller (7) is all connected to the output of pressure sensor (91) electricity, and the inside of platen (93) is equipped with the logical groove that corresponds with T type slide (41) position.
5. The intelligent iron tower service station for midway transduction of rotor type unmanned aerial vehicle of claim 4, wherein: the quick charging assembly (5) comprises a second electric push rod (51) and a wireless charger (52), the second electric push rod (51) is fixedly connected to the inner wall of a through hole formed in the center of the top plate (3), the outer arc surface of the second electric push rod (51) is fixedly connected with the inner wall of a round hole formed in the supporting block (43), the wireless charger (52) is arranged at the top end of the push rod of the second electric push rod (51), the wireless charger (52) is located above the upper surface of the top plate (3), the wireless charger (52) corresponds to the avoidance hole formed in the center of the table plate (93), and the input ends of the second electric push rod (51) and the wireless charger (52) are electrically connected with the output end of the PLC controller (7).
6. The intelligent iron tower service station for midway transduction of rotor type unmanned aerial vehicle of claim 2, wherein: still include GPRS data transmission ware (8), GPRS data transmission ware (8) set up in the inside bottom surface of electric cabinet (14), and GPRS data transmission ware (8) are connected with PLC controller (7) two-way electricity.
7. The intelligent iron tower service station for midway transduction of rotor type unmanned aerial vehicle of claim 2, wherein: still include slide rail (6), dust cover (10) and third electric putter (11), dust cover (10) are respectively through hinge joint in the front and back side of roof (3), slide rail (6) set up respectively in the lower surface of dust cover (10), third electric putter (11) have two, and the lower extreme of two third electric putter (11) passes through U type connector rotation with the backup pad that iron tower (2) upper end front and back side set up respectively and is connected, and the upper end of two third electric putter (11) passes through U type connector rotation with slide rail (6) lower surface sliding connection's slider respectively and is connected, and the output of PLC controller (7) is connected to the input electricity of third electric putter (11).
8. The intelligent iron tower service station for midway transduction of rotor type unmanned aerial vehicle of claim 3, wherein: the telescopic rod is characterized by further comprising telescopic rods (16), wherein the telescopic rods (16) are arranged on the outer side surfaces of the supporting blocks (43), the outer end heads of the telescopic rods (16) are fixedly connected with the outer arc surfaces of the connecting balls (42) on the same side, and the telescopic rods (16) are located inside the adjacent return springs (44).
9. The intelligent iron tower service station for midway transduction of rotor type unmanned aerial vehicle of claim 1, which is characterized in that: the bird repeller is characterized by further comprising a bird repeller (12), wherein the bird repeller (12) is arranged at the upper end of the left side face of the iron tower (2), and the bird repeller (12) is a wind-driven bird repeller.
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| CN202110923406.7A CN113799995A (en) | 2021-08-12 | 2021-08-12 | Intelligent iron tower service station for midway transduction of rotary wing type unmanned aerial vehicle |
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