CN108674685A - A kind of shaft tower apron - Google Patents
A kind of shaft tower apron Download PDFInfo
- Publication number
- CN108674685A CN108674685A CN201810482181.4A CN201810482181A CN108674685A CN 108674685 A CN108674685 A CN 108674685A CN 201810482181 A CN201810482181 A CN 201810482181A CN 108674685 A CN108674685 A CN 108674685A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- cabin
- parking area
- controller
- airplane parking
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000034 method Methods 0.000 claims description 24
- 230000006698 induction Effects 0.000 claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 9
- 238000004891 communication Methods 0.000 claims description 7
- 230000006378 damage Effects 0.000 abstract description 8
- 230000002411 adverse Effects 0.000 abstract description 4
- 108010066057 cabin-1 Proteins 0.000 description 40
- 230000008569 process Effects 0.000 description 16
- 230000001276 controlling effect Effects 0.000 description 11
- 230000005611 electricity Effects 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 238000007689 inspection Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000002452 interceptive effect Effects 0.000 description 3
- 241001465754 Metazoa Species 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 208000014674 injury Diseases 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000005674 electromagnetic induction Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 238000010408 sweeping Methods 0.000 description 1
- 238000002834 transmittance Methods 0.000 description 1
Classifications
-
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
-
- 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
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electromagnetism (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Power Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
This application discloses a kind of shaft tower apron, including cabin, cabin is connect with shaft tower by holder, and one end is provided with antenna and radar outside cabin, and side is provided with photovoltaic panel, and cabin is internally provided with airplane parking area and master controller；Master controller is provided with power supervisor, accumulator group, air pump assembly and controller, and power supervisor is electrically connected with photovoltaic panel, accumulator group, radar, air pump assembly, controller respectively；Sliding slot is provided in cabin, airplane parking area is slidably connected by push rod and sliding slot, and controller is connected with air pump assembly, and air pump assembly is connected with push rod；Charger is provided on airplane parking area, charger is electrically connected with accumulator group；Antenna and radar are communicated to connect with controller respectively.Berth unmanned plane for airplane parking area inside cabin, and is charged to unmanned plane by photovoltaic panel, effectively avoids unmanned plane from being influenced by extraneous adverse circumstances, reduces the damage of unmanned plane, improves the service efficiency of unmanned plane, and then improve the working efficiency of unmanned plane.
Description
Technical field
This application involves unmanned plane applied technical field more particularly to a kind of shaft tower aprons.
Background technology
Multi-rotor unmanned aerial vehicle have the advantages that it is easy to operate, be swift in response, load is abundant, task is widely used, use extensively
In the inspection and maintenance of transmission line of electricity.At this stage, the unmanned plane for being applied to polling transmission line uses lithium battery as dynamic substantially
Power power supply, is limited by battery capacity so that multi-rotor unmanned aerial vehicle inspection is short there are single task time, inspection distance is close asks
Topic.
To alleviate the above problems, shaft tower or ground are provided with unmanned plane airport.Current existing unmanned plane airport is
Open horizontal layout.The unmanned plane airport of open horizontal layout in use, needs to rest in unmanned plane outdoor
Environment in stop or charging.
In existing unmanned plane airport, unmanned plane berths after stopping for a long time in charging process, easily by fitful wind, sleet,
The influence of thunder and lightning so that unmanned plane is easy to be damaged, and weakens the service efficiency of unmanned plane, and then reduces the work effect of unmanned plane
Rate.In order to solve this problem, a kind of shaft tower apron is proposed.
Invention content
This application provides a kind of shaft tower aprons, to solve the problems, such as that existing unmanned plane is ineffective.
To solve the above-mentioned problems, the application provides technical solution below:
A kind of shaft tower apron, including cabin, cabin are connect with shaft tower by holder, the one of corresponding ground outside cabin
End is provided with antenna and radar, and the side outside cabin is provided with photovoltaic panel, is set gradually close to one end of radar inside cabin
There are airplane parking area and master controller；Master controller is provided with power supervisor, accumulator group, air pump assembly and controller, electricity
Source manager is electrically connected with photovoltaic panel, accumulator group, radar, air pump assembly, controller respectively, battery component not with radar,
Air pump assembly, controller electrical connection；Sliding slot is provided in cabin, airplane parking area is slidably connected by push rod and sliding slot, controller with
Air pump assembly is connected by conducting wire, and air pump assembly is connected with push rod by conduit, and charger is provided on airplane parking area, charging
Device is electrically connected with accumulator group；Antenna and radar are communicated to connect with controller respectively.
Optionally, airplane parking area is provided with multiple, and each airplane parking area successively and is not set to inside cabin from top to bottom.
Optionally, antenna is connect with controller by shielded wire, and radar is connect with controller by serial communication.
Optionally, push rod pushes airplane parking area to move along sliding slot, and the side of airplane parking area is provided with baffle, the size of baffle with
Cabin size matches.
Optionally, photovoltaic panel is provided with two pieces, and two pieces of photovoltaic panels are symmetrical with two sides of cabin.
Optionally, charger is radio induction charging device.
A kind of shaft tower apron charging method, method include：
The position of unmanned plane is determined by radar, and by location transmission to controller；
Controller controls push rod by controlling air pump assembly, and cabin is released in airplane parking area by push rod by sliding slot；
It is dropped on the airplane parking area by day line traffic control unmanned plane, and airplane parking area is placed back in cabin；
It is charged to unmanned plane by controlling battery pack.
As shown from the above technical solution, the application provides a kind of shaft tower apron, including cabin.Cabin passes through with shaft tower
Holder connects, and effectively reduces the occupancy of ground space, has saved resource.In order to can with the position of accurate judgement unmanned plane,
The one end on corresponding opposite is provided with radar outside cabin.During use, controller is by radar emission signal to unmanned plane, nothing
Man-machine to transmit signals to radar, received signal is transmitted to controllers for radar, so that it is determined that the position of unmanned plane.In order to
Unmanned plane landing can be automatically controlled, one end of cabin outside corresponding ground is provided with antenna.Antenna not only can be by controller
Information be transferred to collection control terminal, controller and unmanned plane interactive information can also be made.In order to make unmanned plane in the process of shutdown
In continue to charge, the side outside cabin is provided with photovoltaic panel.Photovoltaic panel converts the solar energy received to electric energy, and will
Electric energy is transferred to unmanned plane.In order to make in the stopping process of unmanned plane, the influence that unmanned plane receives bad border is reduced, inside cabin
It is disposed with airplane parking area close to one end of radar, unmanned plane can be parked in airplane parking area.In order to which make can accurately unmanned plane
Stop, be disposed with master controller close to one end of radar inside cabin.Master controller is provided with power management
Device, accumulator group, air pump assembly and controller, power supervisor respectively with photovoltaic panel, accumulator group, radar, air pump assembly, control
Device electrical connection processed, battery component are not electrically connected with radar, air pump assembly and controller.Power supervisor generates photovoltaic panel
Electric energy is transferred to the storage of accumulator group, and the electric energy of storage is transferred to radar, air pump assembly and controller by accumulator respectively.Control
Device is connect with antenna, radar, and controller controls antenna and radar emission, receives signal, so that it is determined that the position of unmanned plane, and make
Unmanned plane drops on airplane parking area.In order to make unmanned plane avoid the interference of external environment, airplane parking area during shutdown is charged
When not in use, it is positioned in cabin, cabin is released in airplane parking area by when use again.Cabin is passed in and out in order to facilitate airplane parking area, is shut down
Sliding slot is provided in level ground, airplane parking area is slidably connected by push rod and sliding slot, and controller is connected with air pump assembly by conducting wire, gas
Pump group part 1 is connected with push rod by conduit.During use, controller controls push rod, push rod by controlling air pump assembly
Airplane parking area disengaging cabin is controlled again.It charges in order to facilitate unmanned plane, charger, charger and accumulator is provided on airplane parking area
Electric energy is transferred to charger by group electrical connection, accumulator group, and charger charges to unmanned plane.In the application, by cabin and stop
The parked unmanned plane in machine level ground, and give unmanned plane to charge by photovoltaic panel, be effectively prevented from unmanned plane shut down charging process be subject to it is outer
Boundary's adverse circumstances influence, and reduce the damage of unmanned plane, improve the service efficiency of unmanned plane, and then improve the work effect of unmanned plane
Rate.
Description of the drawings
In order to illustrate more clearly of the technical solution of the application, letter will be made to attached drawing needed in the embodiment below
Singly introduce, it should be apparent that, for those of ordinary skills, without having to pay creative labor,
Other drawings may also be obtained based on these drawings.
Fig. 1 is a kind of structural schematic diagram for shaft tower apron that application provides；
Fig. 2 is a kind of structural schematic diagram for cabin that application provides；
Fig. 3 is a kind of flow diagram for shaft tower apron charging method that application provides；
Description of the drawings：1- cabins, 2- shaft towers, 3- holders, 4- antennas, 5- radars, 6- photovoltaic panels, the airplane parking areas 11-, in 12-
Heart controller, 111- push rods, 112- sliding slots, 113- chargers, 121- power supervisors, 122- accumulator groups, 123- air pump groups
Part, 124- controllers.
Specific implementation mode
It is a kind of structural schematic diagram of shaft tower apron provided by the embodiments of the present application referring to Fig. 1.The apron includes
Cabin 1, cabin 1 are connect with shaft tower 2 by holder 3.Since shaft tower 2 is shared shaft tower so that shaft tower 2 can be not only that cabin 1 carries
For support, other functions of shared shaft tower are also can ensure that.Since cabin 1 is mounted on the side of shared shaft tower, and the structure of cabin 1
It is compact so that unmanned airport not additional floor not by the interference of ground animals and plants, does not influence shared shaft tower other functions, is convenient for nothing
Man-machine landing.In order to can be with the position of accurate judgement unmanned plane, one end that opposite is corresponded to outside cabin 1 be provided with radar 5.Make
With in the process, controller 124 transmits signals to unmanned plane by radar 5, and unmanned plane transmits signals to radar 5, and radar 5 will connect
The signal transmission received is to controller 124, so that it is determined that the position of unmanned plane.In order to which unmanned plane landing, machine can be automatically controlled
One end of 1 outside corresponding ground of storehouse is provided with antenna 4.The information of controller 124 can be not only transferred to collection control eventually by antenna 4
End, can also make controller 124 and unmanned plane interactive information.In order to make unmanned plane that can continue to charge during shutdown,
Side outside cabin 1 is provided with photovoltaic panel 6.Photovoltaic panel 6 converts the solar energy received to electric energy, and electric energy is transmitted
To unmanned plane.In order to make in the stopping process of unmanned plane, the influence that unmanned plane receives bad border is reduced, is leaned on inside 1 storehouse of sealer
One end of nearly radar 5 is disposed with airplane parking area 11, and unmanned plane can be parked in airplane parking area 11.In order to make can accurately nobody
The stop of machine is disposed with master controller 12 in 1 inside of cabin close to one end of radar 5.Master controller 12 is provided with
Power supervisor 121, accumulator group 122, air pump assembly 123 and controller 124, power supervisor 121 respectively with photovoltaic panel 6,
Accumulator group 122, radar 5, air pump assembly 123, controller 124 be electrically connected, accumulator group 122 respectively with radar 5, air pump assembly
123 and controller 124 be electrically connected.Required voltage is different when being worked due to each equipment, and power supervisor 121 need to produce photovoltaic
Raw electric energy is converted into the voltage needed for equipment, and required voltage is transferred to each equipment successively.Great abundance of sunshine when, photovoltaic
The electric energy that plate 6 generates after sunlight supplies after 121 voltage stabilizing of power supervisor to the charging of accumulator group 122 and each equipment
Electricity.Under unglazed or low light condition, the electric energy stored in accumulator group 122 is powered to power supervisor 121, power supervisor 121
It is respectively radar 5, charger 113, air pump assembly 123, controller 124 after the incoming call of accumulator group 122 is converted to different voltages
Power supply.Controller 124 is using intelligent embedded system to power management module 121, radar 5, charger 113 and air pump assembly
123 are uniformly automatically controlled.Autonomous operation situation is occurred to collection control terminal, when the airport by GSM network for controller 124
, it can be achieved that data sharing between each airport, group net operation when a wide range of arrangement.By information sharing, stopping for unmanned plane is flexibly grasped
Pool, effectively improves the utilization rate of cabin 1, facilitates the stop and charging of unmanned plane so that unmanned plane can be carried out promptly can work
Make state, and then improves the working efficiency of unmanned plane.Controller 124 is also connect with antenna 4, controller in addition to being connect with radar 5
124 emit by controlling antenna 4 and radar 5, receive signal, so that it is determined that the position of unmanned plane, and make unmanned plane accurately
It drops on airplane parking area 11.In order to make unmanned plane avoid the interference of external environment during shutdown is charged, airplane parking area 11 exists
When not in use, it is positioned in cabin 1, cabin 1 is released into airplane parking area 11 again when use.Cabin 1 is passed in and out in order to facilitate airplane parking area 11,
Sliding slot 112 is provided in airplane parking area 11, airplane parking area 11 is slidably connected by push rod 111 and sliding slot 112, controller 124 and air pump
Component 123 is connected by conducting wire, and air pump assembly 123 is connected with push rod 111 by conduit.During use, controller 124
Push rod 111 is controlled by controlling air pump assembly 123, push rod 111 controls airplane parking area 11 and passes in and out cabin 1 again.In order to facilitate nobody
Machine charges, and charger 113 is provided on airplane parking area 11, and charger 113 is electrically connected with accumulator group 122, and accumulator group 122 will
Electric energy is transferred to charger 113, and charger 113 charges to unmanned plane.In the application, pass through 11 parked nothing of cabin 1 and airplane parking area
It is man-machine, and charged to unmanned plane by photovoltaic panel 6, it is effectively prevented from unmanned plane and shuts down the extraneous adverse circumstances that charging process is subject to
It influences, reduces the damage of unmanned plane, improve the service efficiency of unmanned plane, and then improve the working efficiency of unmanned plane.
In order to further save space, in the present embodiment, airplane parking area 11 is provided with multiple, and each airplane parking area 11 is from upper
It is not set to successively and inside cabin 1 under.In the present embodiment, cabin 1 is provided with airplane parking area 11 using three-dimensional so that can be same
When stop multiple UAVs, the unmanned plane that charging terminates in cabin 1 can also be used as guest machine use, when low battery unmanned plane berths
When charging, guest machine, which can take off rapidly to take over to work on, realizes unmanned plane relay-type high density inspection.This guest machine substitutes
The mode of low battery unmanned plane work, effectively increases the service efficiency of unmanned plane, improves the working efficiency of unmanned plane.
In order to reduce the loss of signal in signals transmission, in the present embodiment, antenna 4 passes through shielding with controller 124
Conducting wire connects, and radar 5 is connect with controller 124 by serial communication.Control 124 connects antenna 4 by shielded wire, reduces
Interference of the loss and external signal of cable inner signal to cable inner signal, improves effectiveness, further
Landing time and the landing place for accurately controlling unmanned plane, reduce the breakage of unmanned plane so that the service life of unmanned plane extends
It is improved with working efficiency.The effect of radar 5 is to judge the position of unmanned plane.During use, unmanned plane is sent to controller 124
After docked request, radar 5 can capture the spatial position of unmanned plane automatically, and data are sent to controller by serial communication
124, controller 124 links with unmanned plane through wireless telecommunications and unmanned plane is guided accurately to berth on retractable airplane parking area 11.
Controller 124 links antenna 4 by shielded antenna, and connects radar 5 by serial communication, can not only reduce information and be transmitted across
Information loss in journey, can also be efficiently received and transmitting information, and the information by receiving accurately controls unmanned plane
Landing reduces the landing damage of unmanned plane, extends the service life of unmanned plane, improve the working efficiency of unmanned plane.
In order to allow airplane parking area 11 according to circumstances optionally to pass in and out in cabin 1, it is provided with sliding slot 112 in cabin 1, pushes away
Bar 111 pushes airplane parking area 11 to move along sliding slot 112.After the landing request that unmanned plane is sent is confirmed, controller 124 is logical
Crossing air pump assembly 123 pushes push rod 111 to release airplane parking area 11 outside cabin 1 along sliding slot 112；After unmanned plane landing, according to outer
Boundary's environment chooses whether airplane parking area 11 being retracted into cabin 1.In order to make unmanned plane berth in charging process, from environmental injury,
In the present embodiment, the side of airplane parking area 11 is provided with baffle, and size and 1 size of cabin of baffle match.Baffle and cabin 1
The other three side makes cabin 1 become a closed space so that unmanned plane is during stopping charging not by extraneous meteorological item
Part influences, and when unmanned plane encounters burst meteorological condition in task, unmanned plane, which can stop airport rapidly, to be evaded, and evil is reduced
Erosion of the bad environment to unmanned plane, extends the service life of unmanned plane, improves the ability of unmanned plane continuous work, further
Improve working efficiency.
In order to make unmanned plane during berthing, without external power supply power supply can normal operation, in the present embodiment, light
Volt plate 6 is provided with two pieces, and two pieces of photovoltaic panels 6 are symmetrical with two sides of cabin 1.It is one kind provided by the present application referring to Fig. 2
The structural schematic diagram of cabin.On two adjacent sides of baffle that two pieces of photovoltaic panels 6 are set to airplane parking area 11, can not only it reduce
Damage of the photovoltaic panel 6 when being installed on shared shaft tower to photovoltaic panel 6, can also make photovoltaic panel 6 fully receive sunlight, and connect
The solar energy received is converted into electric energy.Electric energy is by wire transmission to the power supervisor 121 in cabin 1, power supervisor
121 adjust the voltage of electric energy according to the required voltage of each device, and the voltage regulated is conveyed to each device, for nothing
Man-machine charging.The setting of photovoltaic panel 6 not only can provide electric energy when berthing for unmanned plane, reduce the setting of external power supply；
It can also be that unmanned plane provides charging at any time, when preventing existing power supply without electricity, can not power to unmanned plane, improve nobody
The charge efficiency of machine, and then improve unmanned plane and wait for engine efficiency so that when next unmanned plane charging, spare unmanned plane can rapidly into
Enter working condition, improves the working efficiency of unmanned plane.
In order to make the stop charging process of unmanned plane more automate, in the present embodiment, charger 113 is set as wirelessly feeling
Inductive charging device.Radio induction charging device can transmit electrical power to unmanned plane by the form of wireless induction.In order to make charger 113
Electric energy is passed into unmanned plane in a wireless form, the first induction coil is internally provided in radio induction charging device, unmanned plane
Bottom is provided with the second induction coil.According to electromagnetic induction principle, charger 113 passes through the first induction coil and second line of induction
Electric energy is transferred to unmanned plane by circle.In order to reduce the energy loss of electric energy transmittance process, the upper plane and unmanned plane of charger 113
Ground want parallel, i.e., charger 113 is vertical with the uniform baffle of unmanned plane.Charger 113 fills unmanned plane by wireless induction
Electricity so that the charging process of unmanned plane more automates, and improves the charge efficiency of unmanned plane so that unmanned plane can quickly fill with
Electricity simultaneously enters standby host state, working condition is quickly entered when other unmanned planes need charging, and then improve the work of unmanned plane
Efficiency.
From above-described embodiment as can be seen that this application provides a kind of shaft tower apron, which includes cabin 1, machine
Storehouse 1 is connect with shaft tower 2 by holder 3.Since shaft tower 2 is shared shaft tower so that shaft tower 2 can be not only that cabin 1 provides support, also
It can ensure that other functions of shared shaft tower.Since cabin 1 is mounted on the side of shared shaft tower, and cabin 1 is compact-sized so that
Unmanned airport not additional floor not by the interference of ground animals and plants, does not influence shared shaft tower other functions, is convenient for unmanned plane landing.
In order to can be with the position of accurate judgement unmanned plane, one end that opposite is corresponded to outside cabin 1 be provided with radar 5.During use,
Controller 124 transmits signals to unmanned plane by radar 5, and unmanned plane transmits signals to radar 5, the letter that radar 5 will receive
Number it is transferred to controller 124, so that it is determined that the position of unmanned plane.In order to automatically control unmanned plane landing, 1 outside of cabin is right
The one end on ground is answered to be provided with antenna 4.The information of controller 124 can be not only transferred to collection control terminal by antenna 4, can also be made
Controller 124 and unmanned plane interactive information.In order to make unmanned plane that can continue to charge during shutdown, outside cabin 1
Side be provided with photovoltaic panel 6.Photovoltaic panel 6 converts the solar energy received to electric energy, and electric energy is transferred to unmanned plane.For
Make in the stopping process of unmanned plane, the influence that unmanned plane receives bad border is reduced, close to the one of radar 5 inside 1 storehouse of sealer
End is disposed with airplane parking area 11, and unmanned plane can be parked in airplane parking area 11.In order to make can accurately unmanned plane stop,
1 inside of cabin is disposed with master controller 12 close to one end of radar 5.Master controller 12 is provided with power supervisor
121, accumulator group 122, air pump assembly 123 and controller 124, power supervisor 121 are electric with photovoltaic panel 6, accumulator group respectively
122, radar 5, air pump assembly 123, controller 124 be electrically connected, accumulator group 122 respectively with radar 5, air pump assembly 123 and control
Device 124 processed is electrically connected.Required voltage is different when being worked due to each equipment, the electricity that power supervisor 121 need to generate photovoltaic
It can be converted into the voltage needed for equipment, and required voltage is transferred to each equipment successively.Great abundance of sunshine when, photovoltaic panel 6 pass through
The electric energy generated after sunlight is after 121 voltage stabilizing of power supervisor to the charging of accumulator group 122 and the power supply of each equipment.It is unglazed
Or under low light condition, the electric energy that is stored in accumulator group 122 is powered to power supervisor 121, and power supervisor 121 is by accumulator
122 incoming call of group is respectively radar 5, charger 113, air pump assembly 123, the power supply of controller 124 after being converted to different voltages.Control
Device 124 carries out unification using intelligent embedded system to power management module 121, radar 5, charger 113 and air pump assembly 123
It automatically controls.Autonomous operation situation is occurred to collection control terminal, when the airport is arranged on a large scale by GSM network for controller 124
When, it can be achieved that data sharing between each airport, group net operation.By information sharing, berthing for unmanned plane is flexibly grasped, is effectively improved
The utilization rate of cabin 1, and then improve the working efficiency of unmanned plane.Controller 124 also connects with antenna 4 in addition to being connect with radar 5
It connecing, controller 124 emits by controlling antenna 4 and radar 5, receives signal, so that it is determined that the position of unmanned plane, and make nobody
Machine accurately drops on airplane parking area 11.In order to make unmanned plane avoid the interference of external environment during shutdown is charged, stop
Machine level ground 11 when not in use, is positioned in cabin 1, and cabin 1 is released in airplane parking area 11 again when use.In order to facilitate airplane parking area 11 into
Go out cabin 1, sliding slot 112 is provided in airplane parking area 11, airplane parking area 11 is slidably connected by push rod 111 and sliding slot 112, controller
124 are connected with air pump assembly 123 by conducting wire, and air pump assembly 123 is connected with push rod 111 by conduit.During use,
Controller 124 controls push rod 111 by controlling air pump assembly 123, and push rod 111 controls airplane parking area 11 and passes in and out cabin 1 again.In order to
Facilitate unmanned plane to charge, charger 113 is provided on airplane parking area 11, charger 113 is electrically connected with accumulator group 122, electric power storage
Electric energy is transferred to charger 113 by pond group 122, and charger 113 charges to unmanned plane.In the application, pass through cabin 1 and airplane parking area
11 parked unmanned planes, and charged to unmanned plane by photovoltaic panel 6, it is effectively prevented from unmanned plane and shuts down the external world that charging process is subject to
Adverse circumstances influence, and reduce the damage of unmanned plane, improve the service efficiency of unmanned plane, and then improve the working efficiency of unmanned plane.
In order to further save space, in the present embodiment, airplane parking area 11 is provided with multiple, and each airplane parking area 11 is from top to bottom successively
And it is not set to inside cabin 1.In order to reduce the loss of signal in signals transmission, in the present embodiment, antenna 4 and controller
124 are connected by shielded wire, and radar 5 is connect with controller 124 by serial communication.In order to allow airplane parking area 11 according to feelings
Condition optionally passes in and out in cabin 1, and sliding slot 112 is provided in cabin 1, and push rod 111 pushes airplane parking area 11 to transport along sliding slot 112
It is dynamic.In order to make unmanned plane berth in charging process, environmental injury is exempted from, in the present embodiment, the side of airplane parking area 11 is provided with gear
Plate, size and 1 size of cabin of baffle match.In order to make unmanned plane during berthing, it is without external power supply power supply
Can normal operation, in the present embodiment, photovoltaic panel 6 is provided with two pieces, and two pieces of photovoltaic panels 6 are symmetrical with two sides of cabin 1.For
The stop charging process of unmanned plane is set more to automate, in the present embodiment, charger 113 is set as radio induction charging device.
Corresponding with a kind of shaft tower apron of the application, present invention also provides a kind of shaft towers to be charged with apron
Method.It is a kind of flow diagram of shaft tower apron charging method provided by the present application referring to Fig. 3.This method includes：
S01：The position of unmanned plane is determined by radar, and by location transmission to controller；
When unmanned plane is supported into apron, unmanned plane sends request of berthing, machine by built-in wireless communication module to airport
Antenna was listened to receive signal response and take over unmanned aerial vehicle (UAV) control power in field.
Radar on cabin determines the position of unmanned plane, and by the location transmission of unmanned plane to control by surface sweeping unmanned plane
Device processed.
S02：Controller controls push rod by controlling air pump assembly, and cabin is released in airplane parking area by push rod by sliding slot；
Controller pushes away the airplane parking area put according to the unmanned plane position selection received, and selected airplane parking area is passed through air pump
Component controls push rod, makes push rod that airplane parking area be exited cabin along sliding slot.
S03：It is dropped on airplane parking area by day line traffic control unmanned plane, and airplane parking area is placed back in cabin；
Location information is transferred to controller by the relative position between radar scanning unmanned plane and selected airplane parking area；Controller
It guides unmanned plane to drop on selected airplane parking area by antenna, and airplane parking area is placed back in into cabin by controlling air pump assembly
It is interior.
S04：It is charged to unmanned plane by controlling battery pack.
Power supervisor converts voltage according to the charge request that controller is sent out, and the voltage converted is transferred to charging
Electric energy is being transferred to unmanned plane, to realize unmanned plane charging process by device by the induction of charger.
Those skilled in the art will readily occur to its of the application after considering the embodiment of specification and practice here
Its embodiment.This application is intended to cover any variations, uses, or adaptations of the application, these modifications, purposes or
Person's adaptive change follows the general principle of the application and includes the not used common knowledge in the art of the application
Or conventional techniques.The description and examples are only to be considered as illustrative, and the true scope and spirit of the application are by following
Claim is pointed out.
It should be understood that the application is not limited to the precision architecture for being described above and being shown in the accompanying drawings, and
And various modifications and changes may be made without departing from the scope thereof.Scope of the present application is only limited by the accompanying claims.
Claims (7)
1. a kind of shaft tower apron, which is characterized in that including cabin (1), wherein
The cabin (1) is connect with shaft tower (2) by holder (3), and one end of the external corresponding ground of the cabin (1) is provided with day
Line (4) and radar (5), the external side of the cabin (1) are provided with photovoltaic panel (6), and the cabin (1) is internal close to the thunder
It is disposed with airplane parking area (11) and master controller (12) up to the one end of (5)；
The master controller (12) is provided with power supervisor (121), accumulator group (122), air pump assembly (123) and control
Device (124), the power supervisor (121) respectively with the photovoltaic panel (6), the accumulator group (122), the radar (5),
The air pump assembly (123), the controller (124) electrical connection, the accumulator group (122) respectively with the radar (5), institute
State air pump assembly (123), the controller (124) electrical connection；
Sliding slot (112) is provided in the cabin (1), the airplane parking area (11) is sliding by push rod (111) and the sliding slot (112)
Dynamic connection, the controller (124) are connected with the air pump assembly (123) by conducting wire, the air pump assembly (123) and institute
State push rod (111) by conduit to be connected, be provided with charger (113) on the airplane parking area (11), the charger (113) with
Accumulator group (122) electrical connection；
The antenna (4) and the radar (5) are communicated to connect with the controller (124) respectively.
2. apron according to claim 1, which is characterized in that the airplane parking area (11) is provided with multiple, and each institute
State airplane parking area (11) from top to bottom successively and not to be set to the cabin (1) internal.
3. apron according to claim 1, which is characterized in that the antenna (4) passes through screen with the controller (124)
Conducting wire connection is covered, the radar (5) is connect with the controller (124) by serial communication.
4. apron according to claim 1, which is characterized in that the push rod (111) pushes along the sliding slot (112)
The side of airplane parking area (11) movement, the airplane parking area (11) is provided with baffle, the size of the baffle and the cabin (1)
Size matches.
5. apron according to claim 1, which is characterized in that the photovoltaic panel (6) is provided with two pieces, and described in two pieces
Photovoltaic panel (6) is symmetrical with two sides of the cabin (1).
6. apron according to claim 1, which is characterized in that the charger (113) is radio induction charging device.
7. a kind of shaft tower apron charging method, which is characterized in that the method includes：
The position of unmanned plane is determined by radar, and by location transmission to controller；
The controller controls push rod by controlling air pump assembly, and cabin is released in airplane parking area by the push rod by sliding slot；
It is dropped on the airplane parking area by day line traffic control unmanned plane, and the airplane parking area is placed back in the cabin；
It is charged to unmanned plane by controlling battery pack.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810482181.4A CN108674685A (en) | 2018-05-18 | 2018-05-18 | A kind of shaft tower apron |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810482181.4A CN108674685A (en) | 2018-05-18 | 2018-05-18 | A kind of shaft tower apron |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108674685A true CN108674685A (en) | 2018-10-19 |
Family
ID=63806782
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810482181.4A Pending CN108674685A (en) | 2018-05-18 | 2018-05-18 | A kind of shaft tower apron |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108674685A (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109533330A (en) * | 2018-10-24 | 2019-03-29 | 珠海模范智能科技有限公司 | A kind of unmanned plane recyclable device and recovery method |
| CN109972889A (en) * | 2019-04-02 | 2019-07-05 | 国网山东省电力公司经济技术研究院 | Power communication lightning protection signal tower with hangar |
| CN110293858A (en) * | 2019-06-24 | 2019-10-01 | 大连理工大学 | A kind of continuous self monitor method and device based on unmanned plane and intelligent airplane parking area |
| CN110601366A (en) * | 2019-09-23 | 2019-12-20 | 国网江西省电力有限公司宜春供电分公司 | Electric power monitored control system based on thing networking |
| CN110901939A (en) * | 2019-12-20 | 2020-03-24 | 国网山西省电力公司电力科学研究院 | Unmanned aerial vehicle parking device |
| CN111467711A (en) * | 2020-04-15 | 2020-07-31 | 东北电力大学 | Power transmission line cluster type mountain fire monitoring and extinguishing device and control method thereof |
| CN112346476A (en) * | 2020-11-06 | 2021-02-09 | 广东电科院能源技术有限责任公司 | Automatic unmanned aerial vehicle inspection system and method |
| CN112639526A (en) * | 2019-12-20 | 2021-04-09 | 深圳市大疆创新科技有限公司 | Parking apron detection device and control method |
| CN112693334A (en) * | 2021-01-13 | 2021-04-23 | 重庆华创智能科技研究院有限公司 | Wireless charging control method and system based on unmanned aerial vehicle airport |
| CN112706940A (en) * | 2020-12-25 | 2021-04-27 | 芜湖翼讯飞行智能装备有限公司 | Small-size shutdown system for logistics unmanned aerial vehicle and control method thereof |
| CN112900946A (en) * | 2021-01-13 | 2021-06-04 | 重庆华创智能科技研究院有限公司 | Many storehouses unmanned aerial vehicle airport with wireless function of charging |
| WO2021189518A1 (en) * | 2020-03-25 | 2021-09-30 | 南京达索航空科技有限公司 | Automatic charging device for unmanned aerial vehicle |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204679793U (en) * | 2015-05-26 | 2015-09-30 | 河海大学 | A kind of full-automatic remote distance power circuit unmanned plane inspection tour system |
| CN106025930A (en) * | 2016-07-30 | 2016-10-12 | 福州大学 | Unmanned aerial vehicle autonomous grid line patrol system |
| CN205676786U (en) * | 2016-05-31 | 2016-11-09 | 王秋丽 | Full aluminum multilamellar helistop system |
| CN106149577A (en) * | 2016-07-30 | 2016-11-23 | 福州大学 | A kind of wedge shape chargeable electrical network shaft tower unmanned plane airplane parking area and control method thereof |
| CN106284110A (en) * | 2016-09-30 | 2017-01-04 | 深圳市天域智能有限公司 | Airplane parking area and control system thereof |
| CN206367620U (en) * | 2016-12-28 | 2017-08-01 | 芜湖元一航空科技有限公司 | A kind of device stored for unmanned plane |
| CN107199912A (en) * | 2017-07-17 | 2017-09-26 | 国家电网公司 | A kind of rechargeable type moves unmanned hangar |
| CN207218351U (en) * | 2017-08-18 | 2018-04-10 | 华南理工大学 | A kind of round-the-clock wireless charging platform of power patrol unmanned machine |
-
2018
- 2018-05-18 CN CN201810482181.4A patent/CN108674685A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204679793U (en) * | 2015-05-26 | 2015-09-30 | 河海大学 | A kind of full-automatic remote distance power circuit unmanned plane inspection tour system |
| CN205676786U (en) * | 2016-05-31 | 2016-11-09 | 王秋丽 | Full aluminum multilamellar helistop system |
| CN106025930A (en) * | 2016-07-30 | 2016-10-12 | 福州大学 | Unmanned aerial vehicle autonomous grid line patrol system |
| CN106149577A (en) * | 2016-07-30 | 2016-11-23 | 福州大学 | A kind of wedge shape chargeable electrical network shaft tower unmanned plane airplane parking area and control method thereof |
| CN106284110A (en) * | 2016-09-30 | 2017-01-04 | 深圳市天域智能有限公司 | Airplane parking area and control system thereof |
| CN206367620U (en) * | 2016-12-28 | 2017-08-01 | 芜湖元一航空科技有限公司 | A kind of device stored for unmanned plane |
| CN107199912A (en) * | 2017-07-17 | 2017-09-26 | 国家电网公司 | A kind of rechargeable type moves unmanned hangar |
| CN207218351U (en) * | 2017-08-18 | 2018-04-10 | 华南理工大学 | A kind of round-the-clock wireless charging platform of power patrol unmanned machine |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109533330A (en) * | 2018-10-24 | 2019-03-29 | 珠海模范智能科技有限公司 | A kind of unmanned plane recyclable device and recovery method |
| CN109972889B (en) * | 2019-04-02 | 2020-08-28 | 国网山东省电力公司经济技术研究院 | Power communication lightning protection signal tower with hangar |
| CN109972889A (en) * | 2019-04-02 | 2019-07-05 | 国网山东省电力公司经济技术研究院 | Power communication lightning protection signal tower with hangar |
| CN110293858A (en) * | 2019-06-24 | 2019-10-01 | 大连理工大学 | A kind of continuous self monitor method and device based on unmanned plane and intelligent airplane parking area |
| CN110601366A (en) * | 2019-09-23 | 2019-12-20 | 国网江西省电力有限公司宜春供电分公司 | Electric power monitored control system based on thing networking |
| CN110901939A (en) * | 2019-12-20 | 2020-03-24 | 国网山西省电力公司电力科学研究院 | Unmanned aerial vehicle parking device |
| CN112639526A (en) * | 2019-12-20 | 2021-04-09 | 深圳市大疆创新科技有限公司 | Parking apron detection device and control method |
| CN110901939B (en) * | 2019-12-20 | 2023-01-03 | 国网山西省电力公司电力科学研究院 | Unmanned aerial vehicle parking device |
| WO2021189518A1 (en) * | 2020-03-25 | 2021-09-30 | 南京达索航空科技有限公司 | Automatic charging device for unmanned aerial vehicle |
| CN111467711A (en) * | 2020-04-15 | 2020-07-31 | 东北电力大学 | Power transmission line cluster type mountain fire monitoring and extinguishing device and control method thereof |
| CN112346476A (en) * | 2020-11-06 | 2021-02-09 | 广东电科院能源技术有限责任公司 | Automatic unmanned aerial vehicle inspection system and method |
| CN112706940A (en) * | 2020-12-25 | 2021-04-27 | 芜湖翼讯飞行智能装备有限公司 | Small-size shutdown system for logistics unmanned aerial vehicle and control method thereof |
| CN112693334A (en) * | 2021-01-13 | 2021-04-23 | 重庆华创智能科技研究院有限公司 | Wireless charging control method and system based on unmanned aerial vehicle airport |
| CN112900946A (en) * | 2021-01-13 | 2021-06-04 | 重庆华创智能科技研究院有限公司 | Many storehouses unmanned aerial vehicle airport with wireless function of charging |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108674685A (en) | A kind of shaft tower apron | |
| CN110103800B (en) | Unmanned aerial vehicle intelligent inspection operation vehicle suitable for power transmission line and inspection method | |
| CN107394873B (en) | Full-automatic environment-friendly wireless charging system of electric power inspection unmanned aerial vehicle | |
| CN108357689B (en) | Unmanned aerial vehicle port capable of being automatically charged | |
| CN108438245B (en) | Drawer type unmanned aerial vehicle nest | |
| CN110794873A (en) | Automatic inspection system and method for power transmission line | |
| CN108995823A (en) | Unmanned plane wireless sharing charging airplane parking area and the wireless charging method with priority | |
| CN109018413A (en) | A kind of vehicle-mounted unmanned aerial vehicle machine nest and its application method | |
| CN205986293U (en) | A solar energy wireless charging device for unmanned aerial vehicle | |
| CN106774427A (en) | Waters automatic tour inspection system and method based on unmanned plane | |
| CN106532897A (en) | Power supply management system for solar energy unmanned aerial vehicle | |
| CN107046437A (en) | A kind of vehicle-mounted unmanned aerial vehicle is tethered at signal reconnaissance system | |
| CN106368478A (en) | Distributed unmanned aerial vehicle charging machine hangar | |
| CN108909514A (en) | More AGV power management systems and method based on automatic battery replacement | |
| CN106394929A (en) | Photovoltaic charging device of rotary-wing unmanned aerial vehicle | |
| CN205489663U (en) | Energy depot | |
| CN112140914B (en) | Unmanned aerial vehicle power supply system | |
| CN109050868B (en) | Intelligent tethered unmanned aerial vehicle system | |
| CN108422884A (en) | Electric car electric energy replenishment system based on unmanned plane | |
| CN111610802A (en) | Relay control method and system for unmanned aerial vehicle flight | |
| CN103754373A (en) | Wired power multiple rotor wing unmanned aerial vehicle | |
| CN110641298A (en) | Unmanned aerial vehicle landing and landing charging device and unmanned aerial vehicle task handover method | |
| CN109709972A (en) | A kind of Internet of Things network communication system and method based on unmanned plane | |
| CN204998782U (en) | There is rope direct current multiaxis aircraft | |
| CN112937858A (en) | Novel inspection method for vertical take-off and landing fixed wing unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20181019 |
|
| RJ01 | Rejection of invention patent application after publication |