CN107176047A - A kind of unmanned plane shuts down storehouse - Google Patents
A kind of unmanned plane shuts down storehouse Download PDFInfo
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- CN107176047A CN107176047A CN201710391868.2A CN201710391868A CN107176047A CN 107176047 A CN107176047 A CN 107176047A CN 201710391868 A CN201710391868 A CN 201710391868A CN 107176047 A CN107176047 A CN 107176047A
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- Prior art keywords
- unmanned plane
- claw
- storehouse
- temperature
- parking area
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
- B60L53/35—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
- B60L53/37—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles using optical position determination, e.g. using cameras
-
- 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
- B64F1/007—Helicopter portable landing pads
-
- 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
- B60L53/11—DC charging controlled by the charging station, e.g. mode 4
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
- B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
- B60L53/35—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
- B60L53/36—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles by positioning the vehicle
-
- 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
- B60L53/50—Charging stations characterised by energy-storage or power-generation means
- B60L53/51—Photovoltaic means
-
- 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
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
- B64F1/125—Mooring or ground handling devices for helicopters
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
- E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft
-
- 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
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Architecture (AREA)
- Aviation & Aerospace Engineering (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
Storehouse is shut down the present invention relates to a kind of unmanned plane, belongs to unmanned plane landing ancillary technique field.Unmanned plane, which shuts down storehouse, includes controller, airplane parking area and the automatic charge device being controlled by the controller, and controller includes memory and processor；Automatic charge device includes a pair of card pressure components, and card pressure component includes claw, actuator and the charging electrode of card pressure unmanned plane undercarriage transverse bar, and actuator drives claw to be pressed in card and moved between charge position and off-position, and charging electrode is installed on claw.By setting claw and charging electrode being installed on claw, so that the unmanned plane in charged state is retained on airplane parking area, with ensure the continuous of charging process with stably.
Description
Technical field
Land servicing unit the present invention relates to unmanned plane, specifically, be related to a kind of nobody with automatic charge device
Machine shuts down storehouse.
Background technology
UAV, i.e. unmanned plane, are operated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, because having the advantages that cost is low, efficiency-cost ratio is good, risk is low, survival ability is strong, mobility is good, and extensively should
Shot for high-altitude, and in express delivery delivery field with very strong application prospect.
Unmanned plane is generally powered by being mounted in battery thereon, and being limited to can battery-mounted limited mass, and power consumption
Constantly increase with the increase of auxiliary equipment, cause its single voyage partially short, limit its application prospect and development.
A kind of nothing is disclosed in order to extend in the endurance of unmanned plane, Publication No. CN106368478A patent document
People it is on duty distributed unmanned plane charging hangar, it include hangar protect casing, airplane parking area, can slip lid solar panel,
Battery pack, GPS/ Big Dipper positioning and communicatings unit, control unit and wireless charging unit, battery pack are electrically connected with solar panel
To be charged to it, wireless charging unit is electrically connected with battery pack and controlled unit control ground is to resting on airplane parking area
Unmanned plane is charged.
Unmanned plane charging hangar is set by distribution, can effectively extend the endurance of unmanned plane, but it is nothing
Line charges, and compared with wired charging, not only charge efficiency is relatively low, and charging equipment high expensive.
The content of the invention
It is an object of the invention to provide a kind of unmanned plane shut down storehouse, with for unmanned plane provides landing aid in while, energy
For the automatic wired charging of its progress.
To achieve these goals, the unmanned plane that the present invention is provided, which shuts down storehouse, includes controller, airplane parking area and controlled device
The automatic charge device of control, controller includes memory and processor；Automatic charge device includes a pair of card pressure components, card pressure
Component includes card pressure unmanned plane undercarriage transverse bar or claw, actuator and the charging electrode of support feet, actuator driving claw
Press and moved between charge position and off-position in card, charging electrode is installed on claw.
In the course of the work, as actuator driving claw is moved at card pressure charge position, claw card is pressed in unmanned plane
On undercarriage transverse bar or support feet, and by charging electrode and the open electrode contact being located on undercarriage to unmanned plane
Charged, while blocking pressure both sides undercarriage upwards from contra by a pair of claws, unmanned plane is consolidated in charging process
Hold on airplane parking area, effectively ensure continuity, the stability of charging process, and can effectively prevent from causing nobody because of exterior vibration
Machine is slided on airplane parking area, it is ensured that the safety after its landing；After charging is completed, actuator driving claw moves to off-position,
Unmanned plane can continue to fly and extend its endurance.
Specific scheme is that the temperature detection sensor that oriented controller output temperature detects data is installed on claw, storage
Device is stored with computer program, and following steps can be realized when computer program is executed by processor：In charging process, if detection
When being higher than the first temperature threshold to the temperature of claw, control actuator driving claw release undercarriage, and move to card pressure again and fill
Electric position is charged, and repeats release steps with card pressure charge step again until the temperature of claw is less than the first temperature threshold；
If the temperature that the charging process more than double all detects claw exceedes second temperature threshold value, send and change carrying for electrode
Wake up；First temperature threshold is higher than second temperature threshold value；Wherein, temperature detection sensor may be selected from thermocouple, NTC etc..To pass through
Temperature variations of the claw in charging process are monitored, whether whether good or electrode is old for judging the contact situation of two electrodes
Change to threshold value is changed, not only can ensure that and effectively, efficiently charge, and be easy to supervise whole equipment progress running status
Control.
Another specific scheme is that the charging electrode on claw is detected using the more than four lines feedbacks with voltage compensation
Charging structure.
Another specific scheme is that airplane parking area is provided with the notch slid through for claw, and notch is installed with cunning between both sides
The resealable zipper that moving part is pulled or promoted by claw, so that when claw moves to off-position, notch will be by slide fastener on airplane parking area
Closure, to prevent unmanned plane in descent, does not stop to predeterminated position undercarriage occur and be embedded in the notch, effectively ensures that
Claw mobile route will not be blocked during subsequent charge, can normally be taken off after also ensure that unmanned plane landing.
Another specific scheme is that charging electrode is the conductive fibre fabric or net metal being attached on claw card pressure surface
Structure.Using conductive fibre fabric or reticulated metal structures as charging electrode, be easy to its with undercarriage on transverse bar
Electrode card press contacts, it is ensured that the contact effect in charging process；In addition, using conductive fibre fabric as charging electrode, can be abundant
There is certain flexibility using it, make it more abundant with electrode card press contacts on undercarriage, charging is further improved
The contact effect of process.
Another specific scheme includes walking mechanism and aligning mechanism for card pressure component, and walking mechanism includes longitudinal direction
Guide rail and the longitudinal sliding block that can be slided along longitudinal rail, claw are fixedly connected with longitudinal sliding block；Aligning mechanism is included laterally
Guide rail, two longitudinally arranged push rods, transverse sliders and the driving transverse slider actuator that transversely guide rail is slided, two push away
Bar is distributed in the aircraft gate both sides of airplane parking area and is fixedly connected with transverse slider.When unmanned plane is drop on airplane parking area, control
Unmanned plane is pushed into center of the airplane parking area on lateral attitude by the actuator of device aligning mechanism by push rod, is then controlled
Undercarriage transverse bar or support bar are pushed down in the center and card that unmanned plane is pushed into lengthwise position by walking mechanism claw, so that right
The fault-tolerance increase of unmanned plane landing place deviation, further ensures that charging process can be normally carried out.
More specifically scheme be unmanned plane shut down be provided with the outer wall in storehouse communication module and wind sensor, optical sensor and
Rain sensor, unmanned plane is shut down in storehouse and is provided with temperature sensor and register；Airplane parking area is provided with NFC/ at its aircraft gate
RFID card reader and guide device is aligned for being guided to unmanned plane landing place, direction, card is installed on claw
It is pressed onto a detection switch；Memory storage has computer program, and following steps can be realized when computer program is executed by processor：
The condition information for shutting down storehouse surrounding environment is detected based on wind sensor, optical sensor and rain sensor, current environment shape is judged
Whether state, which is suitable to unmanned plane, is stopped；The docked request of unmanned plane is received by communication module, and based on to current ambient conditions
Judge, send and stop feedback information；Control NFC/RFID card reader reads the authentication letter for resting in unmanned plane on airplane parking area
Breath, and its identity is verified；If the unmanned plane drives two push rods to be pushed into unmanned plane by checking, control actuator
Center in the transverse direction of aircraft gate, then controls driver driving claw that unmanned plane is pushed into the centre bit on the longitudinal direction of aircraft gate
Put；Redirected if detecting card and being pressed onto the state of a detection switch, control automatic charge device charges to unmanned plane；
If the unmanned plane detects whether storehouse temperature is located at outside preset temperature interval by authentication by temperature sensor,
If so, then storehouse temperature is adjusted within preset temperature interval by control register.Wherein, card is pressed onto a detection switch and may be selected from
Microswitch, photoelectric detection switch etc., with ensure card be pressed onto position so that charging electrode and the electrode contact on undercarriage it is same
When, it is to avoid damage undercarriage by pressure；Align guide device and may be selected from two-dimension code label, optics target, U-shaped indicator lamp etc., by setting up
Guide device is aligned, can effectively ensure that unmanned plane is stopped to desired locations, is easy to card to press component to carry out card pressure charging to it.It is many
Individual sensor, which detects night-environment offer illumination available for hangar or detects bad weather condition, interrupts unmanned plane trip
Task.
Another specific scheme is that unmanned hangar airplane parking area uses engraved structure, and air-flow is anti-during reducing unmanned plane landing
Bullet takes off or landed caused influence to unmanned plane, so as to land exactly in predeterminable area, so that filling on claw
Electrode can be more accurate and preferably card is depressed on the charging electrode on undercarriage, effectively ensures that the progress of charging process.
Another specific scheme is that the top plate that unmanned plane shuts down storehouse is plug-type cover plate, and unmanned plane shuts down storehouse and is provided with and will stop
Release the elevating mechanism of hangar shell in machine level ground.To reduce shadow of the air-flow to unmanned plane stability that rebounded when unmanned plane takes off or landed
Ring, so as to land exactly in predeterminable area, so that the charging electrode on claw can be more accurate and preferably card has been depressed into
Fall on the charging electrode on frame, effectively ensure that the progress of charging process.
It is preferred that scheme shut down storehouse for unmanned plane and include more than two layers of library unit, library unit is including containment vessel and is arranged on
Airplane parking area and automatic charge device in containment vessel；Library unit below the library unit of top includes being arranged in containment vessel
Plug-type drawer structure, plug-type drawer structure includes draw back plate and the driving draw back plate actuator that transversely guide rail is slided, and stops
Machine level ground is arranged on draw back plate with card pressure component；The front panel of plug-type drawer structure is hinged with draw back plate, plug-type drawer knot
Structure is provided with the actuator for promoting front panel to be rotated around hinge between closing position and tiling position.
By setting library unit structure, it is easy to set the library unit number of plies according to need to actually stop unmanned plane quantity, and improves soil
Ground service efficiency.By the way that the airplane parking area of library unit is arranged into drawer-type structure, it is easy to time lower floor's library unit to store or release nothing
It is man-machine, and press component to coordinate with draw back plate by card, it is ensured that library unit containment vessel is being released or drawn in unmanned plane by draw back plate
During stability and security.The front panel of drawer-type structure is arranged to structure able to turn on or off, to be taken off in unmanned plane
Or landing when, tile front panel and reduce air-flow bounce-back to unmanned plane land caused by influence.
Preferred scheme is mutually orthogonal or opposite for the draw back plate push-and-pull direction of adjacent two layers library unit.With avoid two framves without
It is man-machine the problem of interfere when resting on the airplane parking area of adjacent two layers, improve and shut down the unmanned plane that storehouse can land simultaneously
Quantity.
Brief description of the drawings
Fig. 1 is the stereogram of the embodiment of the present invention 1；
Fig. 2 be the embodiment of the present invention 1 in stereogram of the library unit of unmanned plane after coverboard is omitted is parked；
Fig. 3 is the stereogram of plug-type drawer structure in the embodiment of the present invention 1；
Fig. 4 is pressed with the stereogram of the plug-type drawer mechanism of unmanned plane for card in the embodiment of the present invention 1；
Fig. 5 is the structural representation of bottom library unit in the embodiment of the present invention 2；
Fig. 6 is the backside configuration schematic diagram of bottom library unit in the embodiment of the present invention 2；
Fig. 7 is the structural representation of drawer structure in the embodiment of the present invention 2；
Fig. 8 is the structural representation of card pressure component in the embodiment of the present invention 2；
Fig. 9 is the structural representation of top library unit in the embodiment of the present invention 3.
Embodiment
With reference to embodiments and its accompanying drawing the invention will be further described.
Embodiment 1
Referring to Fig. 1, from bottom to top, unmanned plane, which shuts down storehouse, includes controller, library unit 1, library unit 21, library unit 22, storehouse
Connection is removably secured by fixture between unit 23 and top library unit 24, adjacent two layers library unit, in actual use
Can be according to the library unit of the different number of plies of unmanned plane quantity configuration need to be stopped.
Referring to Fig. 1 to Fig. 4, the structure to library unit by taking the library unit 1 of bottom as an example is illustrated, and it includes support frame
11st, containment vessel and the plug-type drawer structure in containment vessel, plug-type drawer structure include draw back plate 3, airplane parking area 4,
The push-and-pull actuator 63 that a pair of card pressure components 5 and driving draw back plate 3 are slided along guide rod 61,62.
Airplane parking area 4 is installed on draw back plate 3 with card pressure component 5, to be pushed out or draw in containment vessel with draw back plate 3.
It is installed with airplane parking area 4 and aligns guide device 7, aligns guide device 7 including U-shaped indicator lamp 71 and positioned at the U-shaped institute of indicator lamp 71
Enclose square indicator lamp 72, circular indicator lamp 73 and the triangle indicator lamp 74 in region.
Card pressure component 5 includes detent mechanism and walking mechanism, claw 51 and actuator 8.
Der Laengslenker 53 and can be slided along Der Laengslenker 53 that walking mechanism is parallel to each other including transverse support bar 52, two
Sliding block 54, the end of transverse support bar 52 is fixedly connected with sliding block 54, so as to be slided along Der Laengslenker 53.
The cross section of transverse support bar 52 is semi-circular structure, and claw 51 is provided with the semicircle being engaged with transverse support bar 52
Three claws 51 are fixed with fixed via, every transverse support bar 52, claw 51 is wedge-shaped claw, in the wedge shape of wedge-shaped claw
Conductive fibre fabric and microswitch are attached with face, conductive fibre fabric is used as charging electrode.Der Laengslenker 53 constitutes the present embodiment
In longitudinal rail, claw 51 is fixedly connected by transverse support bar 52 with sliding block 54.It is also possible to use being attached on card pressure surface
Net metal electrode substitute conductive fibre fabric be used as charging electrode.
It is fixed on the claw 51 in same transverse support bar 52 and constitutes fixed positive pole charging electrode on one group of claw, it is another
Fixed negative pole charging electrode in group.
Actuator 8 includes the screw rod transmission company of leading screw and nut mechanism and motor, motor and leading screw and nut mechanism
Connect, the nut in leading screw and nut mechanism is fixedly connected with the claw 51 in centre position, so as to promote middle claw 51 and pass through
Transverse support bar 52 drives claw 51 by two sides to move or be moved away to the guide device 7 that aligns on airplane parking area 4 together, i.e., to stopping
The aircraft gate movement on machine level ground 4 is moved away from.
Draw back plate 3 is slidably connected by sliding block 53 with guide rod 51,52.Push-and-pull actuator 6 includes leading screw and nut mechanism with driving
The screw rod transmission of dynamic motor, motor and leading screw and nut mechanism is connected, the bottom of the nut in leading screw and nut mechanism and draw back plate 3
Face is fixedly connected, and releases or promote together library unit to protect draw back plate 3 and the airplane parking area being installed on it 4, card pressure component 5
Shell.
Containment vessel includes bottom plate, top plate and two side plates not shown in side plate 12, side plate 13 and figure, one of side plate
It is fixedly connected with the fix bar 31 on draw back plate 3, so as to be moved with draw back plate 3, other plates are to be fixed on support frame
On 11.
In the course of the work, storehouse is shut down based on UAV Intelligent management and running platform, unmanned plane and this unmanned plane, passes through nothing
Human-machine intelligence's management and running platform Collaborative Control each unmanned plane, to control the fixed point cruise of unmanned plane, tasks carrying and make a return voyage
Function.
In the present embodiment, unmanned plane 01 is a rotary wind type unmanned plane, and it is manipulated by matching remote control.Unmanned plane bag
Flight control system, communication system, alignment system, dynamical system and battery composition are included, its alignment system includes GPS or similar satellites
Positioning unit and vision positioning system, by GPS by within the scope of unmanned plane Automatic dispatching to vision positioning, then pass through vision
Alignment system is realized and drop on airplane parking area to be charged.It can receive the instruction of ground control system and be cruised with the instruction
To certain particular range (unmanned plane cruising range) interior any point.
Open electrode is installed with the transverse bar 012 of the undercarriage 011 of unmanned plane 01.The open electrode is to be embedded in
Conductive fibre fabric on transverse bar 012, it coordinates with the conductive fibre fabric being installed on wedge-shaped claw.The open electrode passes through
Voltage detecting is to prevent from being likely to occur reverse current under operating mode that unmanned plane does not land correctly, while there is cable overcurrent protection to melt
Disconnected function, to prevent accidental short circuit from causing to damage to unmanned plane and automatic charging platform.
Unmanned plane is shut down and is additionally provided with the thermostat module being electrically connected with the controller, power module, communication module and positioning on storehouse
Module.
Power module includes service cable, power supply, relay, indicator lamp and power supply interface.Service cable is along aluminium alloy branch
Frame structure arrangement is supportted, to avoid causing movable device interference.Cable connection power supply output stage, passes through flexure spring formula cable
By in electrical energy transportation to each unmanned plane aircraft gate.Relay directly controls the output of power supply interface voltage, and indicator lamp is used to detect
Power supply interface working condition.Power supply is dc source, AC power or the body solar energy accessed by charging platform interface
Power supply is powered, the power supply standard needed for being charged by internal power supply change-over device there is provided unmanned plane.
Guide device is aligned on the aircraft gate centre position of airplane parking area, is adopted by the airborne camera of unmanned plane 01
After collection, recognized by unmanned plane image identification function, the location data produced with reference to unmanned plane gyroscope, for determining for unmanned plane
Position, align.The embedded low diverging LED light pearl of guiding mark is aligned, so that camera gathers image under low-light (level) environment.
The top plate of top library unit 24 is along slide rail driving solar panel, to realize to top storehouse list by linear electric motors
While the keying in member protection storehouse, electric energy is produced, when unmanned plane needs release, top plate is released and received after unmanned plane takes off
Return, when unmanned plane needs landing, top plate is released and withdrawn after unmanned plane landing.
For remaining every layer can unit, when unmanned plane needs release, plug-type drawer structure is released simultaneously to be risen in unmanned plane
Withdrawn after flying, when unmanned plane needs landing, plug-type drawer structure is released and withdrawn after unmanned plane landing.Below airplane parking area
Space connects the positive and negative polarities of power supply by flexure spring cable respectively, by power supply lead on unmanned plane aircraft gate and with located at card
Charging electrode electrical connection on pawl 51.
Controller is controlled to all library units simultaneously.And by every layer can unit pull direction be arranged to different directions,
In the present embodiment, the Way out of the draw back plate of four library units in bottom is different, can allow unmanned planes more than four framves
Landing simultaneously.
When shutdown storehouse is connected to unmanned plane landing instruction, a vacant library unit release airplane parking area will be specified by shutting down storehouse.
After unmanned plane landing, card is pressed on the transverse bar 012 of unmanned plane both sides undercarriage by wedge-shaped claw, so that unmanned plane is fixed,
And start to perform charging by charging electrode contact with open electrode.After unmanned plane charging complete, shut down storehouse and receive
The instruction of unmanned plane standby for takeoff, airplane parking area is released, while wedge-shaped claw is moved to both sides, is discharged unmanned plane undercarriage, that is, is caused
Dynamic device 8 promotes claw 51 to be pressed in card and moved between charge position and off-position.After unmanned plane leaves, airplane parking area is withdrawn.
Optional built-in/external mini air conditioner in storehouse is shut down as thermostat module, suitable temperature, humidity ring are provided for unmanned plane
Border.For example, being less than in environment temperatureShi Qidong air-conditionings preheat for unmanned plane, are higher than in environment temperatureShi Qidong is empty
It is adjusted to unmanned plane cooling.
Communication module be used for management and running Platform communication, with pass through communication module send charging reservation information, the opposing party
The working status parameter of face unmanned plane automatic charging hangar device, including power supply supply parameter, charging electrode whether normally contact,
Whether protection device normally waits key parameter to be also to be uploaded in real time on management and running platform by communication module.
Label recognizer is set on unmanned plane aircraft gate, is in the present embodiment NFC/RFID card reader, for reading
Unmanned plane electronic labeling information is taken, to unmanned plane authentication, after being proved to be successful, unmanned plane can be charged.
Locating module is used for the positional information for obtaining hangar, and is managed this information access unmanned plane by communication module
Platform, reference is provided for unmanned plane.
Controller is the control axis of unmanned plane hangar, and it gathers each component working state by internal electronic circuit
Information, produces control instruction, controls each executing agency's co-operating, realizes the function of unmanned plane hangar.
The course of work is as follows, and unmanned plane sends charge request in good time according to airborne BMS parameter；Management and running platform is obtained
Take the unmanned plane in administrative area and shut down position, aircraft gate seizure condition and other work state informations in storehouse, be it
Storehouse is shut down with a rational charging, and guides its cruise to relevant position；When unmanned plane cruises to when shutting down near storehouse, pass through
The guide device that aligns being arranged on aircraft gate aligns landing, passes through authentication, you can start automatic charging.Work as charging complete
Afterwards, unmanned plane, which takes off, leaves aircraft gate.Specially：
(1) management and running platform sends charging reservation letter according to the charge request of unmanned plane to the communication module for shutting down storehouse
Breath, unmanned plane automatic charge device is responded.Controller control top library unit opens top plate 241 or other library units are released
Airplane parking area 4.
(2) unmanned plane cruises to above unmanned plane automatic charge device according to Position Fixing Navigation System, starts slow whereabouts, and
In descent, constantly basis aligns guide device 7 and carries out pose adjustment.
(3) after unmanned plane stabilization is accommodated on airplane parking area 4, the label recognizer being now connected with controller communication
Start to scan the label of unmanned motor spindle, carry out authentication, after recognizing successfully, top plate 241 or airplane parking area 4 are withdrawn, together
When, controller sends instruction control actuator 8 and promotes clamping jaw 51 mobile to centre, until card pushes down the transverse bar 012 of undercarriage,
And by being arranged in whether the microswitch on claw 51 fastens in place to feed back, while avoiding damage to undercarriage 011.
(4) after unmanned plane is held, the relay closure of power module, the indicator lamp of power module is lighted, and conveys electric current
The charging of unmanned machine battery is given, meanwhile, management and running platform is informed by communication module, the corresponding of unmanned plane automatic charging hangar is stopped
Seat in the plane is in charged state；After unmanned machine battery is full of, the relay of power module disconnects, and its indicator lamp extinguishes, and leads to
Cross communication module and inform that the corresponding unmanned machine battery of management and running platform is filled with, while ejector plate 241 or exiting airplane parking area
4, two groups of claws are moved to both sides, unclamp unmanned plane, and unmanned plane is in state to be flown.
(5) after unmanned plane flies away from the continuation continuation of the journey of shutdown storehouse, top plate 241 or airplane parking area 4 are closed, and the library unit is in
Holding state, meanwhile, local unmanned plane aircraft gate occupied information is updated to management and running platform by communication module.
The working region of whole system can be divided into movement area, three intervals in hangar workspace and service area.
Movement area is the workplace of unmanned plane, and unmanned plane flies and the device measuring by carrying with workplace
The target information collected and is sent to high in the clouds at corresponding data by target environment, collection, or can also be by the state of itself
Information is sent to high in the clouds or system controller, completes the interaction of information.
Hangar workspace is the location of hangar, and it is usually mounted with the equipment such as hangar, controller, remote control, can basis
This three is integrated or separated by demand, can realize the friendship of information between this three by wired or wireless mode
Stream.Wherein system controller is the core of system, and system controller such as obtains people when obtaining the outside instruction to hangar
The instructions such as instruction, the high in the clouds control temperature of machine takeoff and landing, are instructed by parsing these, send corresponding from control to respective layer
Instruction, from control by obtaining analysis instruction after, control actuator, the executing agency such as temperature control module and charging equipment holds
Take action and make, the status information of the hangar of collection can also be sent to system controller from controlling, such as hangar closure or unlatching,
Whether charge, a series of status informations such as unmanned plane state, state of temperature, system controller can send these information
To high in the clouds, data can also be parsed, unmanned plane and user are fed back to according to the result of parsing afterwards, such as, control nothing
Man-machine some other states of flight and execution.
Service area is the region of analyzing and processing data in data set, while being also the region of man-machine interaction.System controller
Substantial amounts of data are obtained, after the analysis of these data in detail, by final structural feedback to user, user obtains these letters
After breath, instructions can be assigned, and unmanned plane or system controller are sent to by high in the clouds, the work(of remote monitoring is realized
Energy.
It is as follows for the partial duty flow of hangar in systems：
Its controller by receive unmanned plane take off landing instruction or server end control unmanned plane landing of taking off
The opening or closure of instruction control distribution library unit, while controller can also be by detecting whether unmanned plane reaches, to control
Make the opening or closure of the charging hangar of distribution.After unmanned plane arrival is detected, controller control claw fixes nobody
Whether machine simultaneously closes equipment compartment, need charging to perform corresponding charge function according to unmanned plane after closure.If temperature detection is passed
The temperature that sensor is detected in library unit is too low or too high, and controller can open temperature control module, and temperature is changed to suitable temperature
Degree, while the temperature that controller can also receive the temperature adjusting instruction control hangar in high in the clouds is reached in the scope specified, all the time
Unmanned plane is set to be in suitable temperature range.In addition, system controller can also be by the temperature information of collection, unmanned plane
Whether the temperature information of the status informations such as charge condition, location status and hangar, hangar correspondence unmanned plane the shape such as can run
State information, and transmit these information to server and preserved and fed back to user.
Whether hangar can be received the status information such as unmanned plane and hangar temperature and be sent to unmanned plane by controller,
It is performed emergency function, such as, drop to emergency point.This part specific workflow mainly plays illustration, high in the clouds
Action with controller, controller and unmanned plane, controller and hangar is in addition to above-mentioned, in addition to other functions,
It is numerous to list herein.
Embodiment 2
As the explanation to the embodiment of the present invention 2, the difference only pair with above-described embodiment 1 is illustrated below.
Referring to Fig. 5 to Fig. 8, airplane parking area 4 is a hollowed-out board structure, and it is supported between draw back plate 32 by polylith supporting plate,
Constitute the ventilative built on stilts Rotating fields in both sides；Through hole is equipped with the biside plate 33 of drawer structure and for illuminating under night environment
LED 35, is hinged between front panel 34 and draw back plate 32 by hinge, promotes the around hinge of front panel 34 to cut with scissors by actuator 36
Axle is rotated, to control front panel 34 to switch between tiling position and erection position, by setting logical on airplane parking area 4 and side plate 33
Hole, and front panel 34 is in its flat presentation during unmanned plane rises and falls, it can efficiently reduce to rotor downwash
Bounce-back, improves the stability of unmanned plane during flying.
In the present embodiment, using the Quick Response Code on airplane parking area 4 as guide device is aligned, in addition, being additionally provided with
NFC/RFID card reader, for reading the authentication information that the electronic tag on unmanned plane is included.
Running status warning lamp 91, waterproof plug for industrial use 95, power output socket and sky are installed on the wall of library unit side
Air cock 94, retreat 2 buttons and tight guard's valve 97.
The notch 41 slid through for claw 51 is provided with airplane parking area 4, unmanned plane was landed in order to reduce notch 41
The influence of journey, is provided for the resealable zipper (not shown) opened and closed to it, the two of resealable zipper on the notch 41
Cloth is fixed on the two side of notch 41 by modes such as bondings, and makes the upper surface horizontal alignment on its side and airplane parking area 4, is sealed
The mouth sliding part of slide fastener is fixedly connected with the fixed part 86 on claw 51 and is pulled or promoted by it, to be filled in claw 51 from card pressure
When electric position retreats to off-position, notch 41 is closed, and opened when card is pressed.
Process is being used, claw 51 can be adjusted to the position for droping to unmanned plane on airplane parking area 4, but it is along vertical
To adjustment, in order that unmanned plane can be located at predeterminated position and be charged, it is respectively provided with aircraft gate both sides longitudinally arranged
Push rod 92,93, the two two ends can be slided by sliding block along the cross slide way not shown in figure, so as to be promoted by actuator
Transversely guide rail is slided push rod 92,93, you can the displacement of unmanned plane in the horizontal is adjusted.Push rod 92,93, cross slide way
And matched sliding block constitutes the aligning mechanism in the present embodiment together.
Voltage detection pin 82 is fixed with claw 51, it is reversed to prevent charging electrode for detecting battery polar on unmanned plane
And there is reverse current, mainly occur in the case where unmanned plane does not land correctly.Two voltage detection pins 82 are with being located at
Fall the conductive electrode electrical connection on frame, and the conductive electrode is electrically connected with the voltage detecting pin of unmanned machine battery, i.e., it feeds back
Situation of change of the cell voltage in charging process on unmanned plane, so that distal end voltage compensation can be carried out to unmanned machine battery, with two
Root charging electrode constitutes four tapes in the present embodiment together the feedback detection charging structure of voltage compensation, of courses, can be by
They are arranged to more than five lines the feedback detection charging structure with voltage compensation.
Offered on the matrix of claw 51 and thermocouple is installed on the mounting groove for installing Kato 87, Kato 87, should
The temperature variations that thermocouple is used for claw 51 in charging process are monitored.
The installation unit of claw 51 includes slide 84, optical axis 85, the straight line flange bearing that can be slided along longitudinal rail 81
88th, preload adjustable spring mechanism 83, back seat 89 and fixed seat 98.
Back seat 89 is fixed on slide 84, and two optical axises 85 are arranged along longitudinal rail 81 and one end is fixed on back seat 89,
I.e. the length direction of optical axis 85 is installed on back seat 89 while the direction arrangement of off-position is pointed to along card pressure charge position, straight-line method
Blue bearing 88 can be slidably sleeved on optical axis 85 along optical axis 85, and fixed seat 98 is fixedly connected with two straight line flange bearings 88,
I.e. fixed seat 98 can be slidably mounted on optical axis 85 along optical axis 85, and claw 51 is to be removably mounted in fixed seat 98
Fast disassembly type falcon connects charging head, is changed when there is aging in order to charging electrode.
Preload adjustable spring mechanism 83 is provided between fixed seat 98 and back seat 89, you can bullet between the two is pressed on by adjustment
The decrement of spring, to change pretightning force of the claw 51 along longitudinal direction, is easy to it to form compensator or trimmer pressure when card presses unmanned plane undercarriage
With buffer displacement, effectively ensure card pressure compactness and avoid the occurrence of hard extruding and squeeze bad unmanned plane undercarriage or claw 51.The bullet
Spring mechanism 83 includes being pressed on stage clip between back seat 89 and fixed seat 98, and for adjust between fixed seat 98 and back seat 89 it is compressible between
Pull bar away from threshold value.
In the course of the work, temperature detection data of the controller processor based on thermocouple, execution is stored in controller and deposited
Computer program in reservoir is to realize following steps：
(1) in charging process, if the temperature for detecting claw 51 is higher than the first temperature threshold, control actuator driving
Claw 51 discharge unmanned plane undercarriage, and move to again card pressure charge position charged, repeat release steps with again block pressure
Charge step is until the temperature of claw 51 is less than the first temperature threshold.By the change to the temperature in charging process of claw 51,
Whether well judged with the charge contact to claw, to ensure the safety of charging process.
(2) if the temperature that the charging process more than double all detects claw exceedes second temperature threshold value, send
Change the prompting of electrode.The continuous aging with the use of electrode, causes its resistance to become big, i.e. its heating in charging process
Amount can be higher than new electrode, so as to be monitored by monitoring temperature to its aging conditions, with prompting changing charging electrode.
Wherein, the first temperature threshold is higher than second temperature threshold value, and concrete numerical value need to carry out detection determination according to actual conditions.
Embodiment 3
As the explanation to the embodiment of the present invention 3, the difference only pair with above-described embodiment 1 is illustrated below.
Referring to Fig. 9, sensor 96 is installed with the lateral wall of library unit, sensor 96 is integrated with wind sensor, light and passed
Sensor and rain sensor, to be detected to the environmental aspect around hangar, and will detect that data are sent to the place in controller
Device is managed, processor judges whether current ambient conditions are suitable to unmanned plane and stop according to coherent detection data, and will determine that result is led to
Cross communication module and feed back to unmanned plane or regulation platform.In the present embodiment, sensor 96 is arranged on plug-type cover plate 241.
The lower section of airplane parking area 4 is provided with for it vertically to be released to the elevating mechanism outside containment vessel, in the present embodiment, is risen
Descending mechanism elects jack as.
In the present embodiment, communication module can be 3G, 4G, wifi or other similar wireless communication modules, for connecing
Receive the scheduling control commands of server master station or PC ends and upload unmanned hangar state.
This example only technical concepts and features to illustrate the invention, its object is to allow person skilled in the art's energy
Solution present disclosure much of that is simultaneously implemented according to this, and it is not intended to limit the scope of the present invention.It is all spiritual according to the present invention
The equivalent change or modification that essence is made, should all be included within the scope of the present invention.
Claims (10)
1. a kind of unmanned plane shuts down storehouse, including controller, airplane parking area and the automatic charge device controlled by the controller, described
Controller includes memory and processor；
It is characterized in that：
The automatic charge device includes a pair of card pressure components, and the card pressure component includes the transverse bar of card pressure unmanned plane undercarriage
Or claw, the driving claw of support feet are pressed the actuator moved between charge position and off-position in card and are installed in described
Charging electrode on claw.
2. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that the oriented controller is installed on the claw
Output temperature detects the temperature detection sensor of data, and the memory storage has computer program, the computer program quilt
Following steps can be realized during the computing device：
In charging process, if the temperature for detecting the claw is higher than the first temperature threshold, the actuator driving is controlled
The claw discharges the undercarriage, and moves to the card pressure charge position again and charged, and repeats release steps and again
Card pressure charge step is until the temperature of the claw is less than first temperature threshold；
If the temperature that the charging process more than double all detects the claw exceedes second temperature threshold value, send and change
The prompting of electrode；
First temperature threshold is higher than the second temperature threshold value.
3. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
The airplane parking area is provided between the notch slid through for the claw, the notch both sides and is installed with sliding part by described
The resealable zipper that claw is pulled or promoted.
4. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
The charging electrode is the conductive fibre fabric or net metal electrode being attached on the card pressure surface of the claw.
5. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
The card pressure component includes walking mechanism and aligning mechanism；
The walking mechanism includes longitudinal rail and the longitudinal sliding block that can be slided along the longitudinal rail, and the claw is indulged with described
It is fixedly connected to sliding block；
The aligning mechanism includes cross slide way, two longitudinally arranged push rods, transverse sliders and drives the transverse direction
The actuator that sliding block is slided along the cross slide way, two push rods be distributed in the aircraft gate both sides of the airplane parking area and with institute
Transverse slider is stated to be fixedly connected.
6. unmanned plane according to claim 5 shuts down storehouse, it is characterised in that the unmanned plane is shut down and installed on the outer wall in storehouse
There are communication module, wind sensor, optical sensor and rain sensor, the unmanned plane, which is shut down, is provided with temperature sensor and tune in storehouse
Warm device；The airplane parking area is provided with to align at its aircraft gate and installed on guide device and NFC/RFID card reader, the claw
There is card to be pressed onto a detection switch；
The memory storage has computer program, and the computer program can be realized following step during the computing device
Suddenly：
The situation letter for shutting down storehouse surrounding environment is detected based on the wind sensor, the optical sensor and the rain sensor
Breath, judges whether current ambient conditions are suitable to unmanned plane and stop；
The docked request of unmanned plane is received by the communication module, and based on the judgement to current ambient conditions, sends and stops
Feedback information；
Control NFC/RFID card reader reads the authentication information for resting in unmanned plane on the airplane parking area, and its identity is entered
Row checking；
If the unmanned plane drives two push rods that unmanned plane is pushed into the transverse direction of aircraft gate by checking, control actuator
Center, then controls driver to drive the claw that unmanned plane is pushed into the center on the longitudinal direction of aircraft gate；
If detect it is described block be pressed onto the state of a detection switch and redirect, control automatic charge device is to unmanned plane progress
Charging；
If the unmanned plane detects whether storehouse temperature is located at preset temperature area by authentication by the temperature sensor
Between outside, if so, then controlling the register that storehouse temperature is adjusted within preset temperature interval.
7. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
The airplane parking area is engraved structure.
8. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
The top plate that the unmanned plane shuts down storehouse is plug-type cover plate, and the unmanned plane shutdown storehouse is provided with releases its shell by airplane parking area
Elevating mechanism.
9. the unmanned plane according to any one of claim 1 to 8 claim shuts down storehouse, it is characterised in that：
The unmanned plane, which shuts down storehouse, includes more than two layers of library unit, and the library unit includes containment vessel and installed in the protection
The airplane parking area and the automatic charge device in shell；
Library unit below the library unit of top includes the plug-type drawer structure being arranged in the containment vessel, the push-and-pull
Formula drawer structure includes draw back plate and the driving draw back plate actuator that transversely guide rail is slided, the airplane parking area and the card
Component is pressed to be arranged on the draw back plate；
The front panel of the plug-type drawer structure is hinged with the draw back plate, and the plug-type drawer structure is provided with promotion institute
State the actuator that front panel is rotated around hinge between closing position and tiling position.
10. unmanned plane according to claim 9 shuts down storehouse, it is characterised in that：
The push-and-pull direction of the draw back plate of adjacent two layers library unit is opposite or mutually orthogonal.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710391868.2A CN107176047A (en) | 2017-05-27 | 2017-05-27 | A kind of unmanned plane shuts down storehouse |
| GB2009295.3A GB2583418B (en) | 2017-05-27 | 2018-05-25 | Drone parking garage |
| PCT/CN2018/088435 WO2018219226A1 (en) | 2017-05-27 | 2018-05-25 | Unmanned-aerial-vehicle hangar |
| CN201810517922.8A CN108502201B (en) | 2017-05-27 | 2018-05-25 | Unmanned aerial vehicle parking garage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710391868.2A CN107176047A (en) | 2017-05-27 | 2017-05-27 | A kind of unmanned plane shuts down storehouse |
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| Publication Number | Publication Date |
|---|---|
| CN107176047A true CN107176047A (en) | 2017-09-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710391868.2A Pending CN107176047A (en) | 2017-05-27 | 2017-05-27 | A kind of unmanned plane shuts down storehouse |
| CN201810517922.8A Active CN108502201B (en) | 2017-05-27 | 2018-05-25 | Unmanned aerial vehicle parking garage |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810517922.8A Active CN108502201B (en) | 2017-05-27 | 2018-05-25 | Unmanned aerial vehicle parking garage |
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| CN108657456A (en) * | 2018-06-27 | 2018-10-16 | 深圳市多翼创新科技有限公司 | Rackwork |
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| WO2018219226A1 (en) * | 2017-05-27 | 2018-12-06 | 星逻智能科技(苏州)有限公司 | Unmanned-aerial-vehicle hangar |
| CN109018413A (en) * | 2018-09-13 | 2018-12-18 | 张欣 | A kind of vehicle-mounted unmanned aerial vehicle machine nest and its application method |
| CN109062261A (en) * | 2018-08-14 | 2018-12-21 | 深圳市烽焌信息科技有限公司 | A method of guidance unmanned plane enters charging platform |
| CN109455308A (en) * | 2018-12-27 | 2019-03-12 | 祺步智能科技（上海）有限公司 | A kind of unmanned plane shuts down library and means of transport |
| CN109502039A (en) * | 2018-11-30 | 2019-03-22 | 山东大学 | A kind of vehicle-mounted unmanned aerial vehicle stops cabinet equipment, automatic replacement battery methods and system |
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