CN207028881U - A kind of unmanned plane shuts down storehouse - Google Patents
A kind of unmanned plane shuts down storehouse Download PDFInfo
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- CN207028881U CN207028881U CN201720614879.8U CN201720614879U CN207028881U CN 207028881 U CN207028881 U CN 207028881U CN 201720614879 U CN201720614879 U CN 201720614879U CN 207028881 U CN207028881 U CN 207028881U
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- unmanned plane
- claw
- shuts down
- parking area
- storehouse
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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Abstract
It the utility model is related to a kind of unmanned plane and shut down storehouse, belong 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；Automatic charge device includes a pair of cards and presses component, 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
It the utility model is related to unmanned plane landing servicing unit, specifically, be related to a kind of with automatic charge device
Unmanned plane shuts down storehouse.
Background technology
UAV, i.e. unmanned plane, 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 there is very strong application prospect in express delivery delivery field.
Unmanned plane is generally powered by being mounted in battery thereon, be 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.
In order to extend the endurance of unmanned plane, a kind of nothing is disclosed in 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 electrically connect with solar panel
To be charged to it, wireless charging unit electrically connects 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
Micro USB electricity, compared with wired charging, not only charge efficiency is relatively low, and charging equipment high expensive.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane and shuts down storehouse, to provide the same of landing auxiliary for unmanned plane
When, can be the automatic wired charging of its progress.
To achieve these goals, unmanned plane provided by the utility model, which shuts down storehouse, includes controller, airplane parking area and controlled
The automatic charge device of device control processed；Automatic charge device includes a pair of cards and presses component, and card pressure component, which includes card pressure unmanned plane, to be risen
Fall the claw, actuator and charging electrode of frame transverse bar or support feet, actuator drives claw in card pressure charge position and release
Moved between position, 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 contacted by charging electrode with the open electrode on undercarriage and to unmanned plane
Charged, while block 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 slides on airplane parking area, it is ensured that its safety after landing；After completing to charge, actuator driving claw moves to off-position,
Unmanned plane can continue to fly and extend its endurance.
Specific scheme is to be provided with card on claw to be pressed onto a detection switch, and card, which is pressed onto a detection switch and may be selected from fine motion, to be opened
Pass, photoelectric detection switch etc..While ensuring that card is pressed onto position so that charging electrode contacts with the electrode on undercarriage, avoid pressing
Bad undercarriage.
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 to be provided with temperature detection sensor on claw, and temperature detection sensor may be selected from thermoelectricity
Idol, NTC etc..With by monitoring temperature variations of the claw in charging process, it is available for the contact situation for judging two electrodes
Whether aging to threshold value is changed, for example, when detecting that claw temperature is too high in charging process, is judged as electrode to no good or electrode
It is too small that card does not press tightly close or contact surface, solves the problem control claw to unclamp and to attempt card piezoelectricity pole again；If repeatedly
Claw temperature is too high when detecting charging after card pressure, can determine whether for ageing of electrode, to carry out repair and maintenance with prompting and change.
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 occur undercarriage to predeterminated position 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 the electrode card press contacts on undercarriage, further improve charging
The contact effect of process.
Another specific scheme is that airplane parking area is provided with its aircraft gate for being carried out to unmanned plane landing place, direction
Guide what is aligned to align guide device, align guide device and may be selected from two-dimension code label, optics target, U-shaped indicator lamp etc..Pass through
Set up and align guide device, can effectively ensure that unmanned plane is stopped to desired locations, be easy to card pressure component to carry out card pressure to it and fill
Electricity.
Another specific scheme is that airplane parking area is provided with NFC/RF I D card reader at its aircraft gate.Existed with reading configuration
NFC label/electronic tag on unmanned plane, is verified with the identity to unmanned plane.
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 slider and the driving transverse slider actuator that transversely guide rail slides, 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 airplane parking area at the center on lateral attitude by the actuator of device aligning mechanism by push rod, is then controlled
At the center that unmanned plane is pushed into lengthwise position by walking mechanism claw and card pushes down undercarriage transverse bar or support bar, so as to right
The fault-tolerance increase of unmanned plane landing place deviation, further ensures that charging process can be normally carried out.
Another specific scheme is that hangar carries wind sensor, optical sensor and rain sensor, is detected for hangar
Night-environment provides illumination or detects that bad weather condition interrupts unmanned plane trip task.
Another specific scheme is that unmanned hangar airplane parking area uses engraved structure, anti-to reduce air-flow when unmanned plane lands
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 its containment vessel 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.
Preferable scheme is the library unit that unmanned plane shutdown storehouse includes more than two layers, and library unit includes containment vessel and is arranged on
Airplane parking area and automatic charge device in containment vessel.It is easy to set the library unit number of plies according to need to actually stop unmanned plane quantity, and carries
High USE RIGHT OF LAND FLOWING.
The push-and-pull that one preferred scheme includes being arranged in containment vessel for the library unit below the library unit of top
Formula drawer structure, plug-type drawer structure include draw back plate and drive the draw back plate actuator that transversely guide rail slides, airplane parking area
It is arranged on card pressure component on draw back plate.It is easy to time lower floor's library unit storage or release unmanned plane, and component is pressed with pushing away by card
Arm-tie coordinates, it is ensured that stability and security of the draw back plate during releasing by unmanned plane or drawing in library unit containment vessel.
Scheme further preferably is mutually orthogonal or opposite for the push-and-pull direction of adjacent two layers library unit draw back plate.With avoid two framves without
Man-machine the problem of interfering when resting on the airplane parking area of adjacent two layers, improve and shut down the unmanned plane that storehouse can land simultaneously
Quantity.
Another preferred scheme is hinged for the front panel of plug-type drawer structure with draw back plate, plug-type drawer structure
It is provided with the actuator for promoting front panel to be rotated around hinge between closing position and tiling position.Unmanned plane takes off or put down when landing
Paving front panel is rebounded to the influence caused by unmanned plane landing with reducing air-flow.
Brief description of the drawings
Fig. 1 is the stereogram of the utility model embodiment 1；
Fig. 2 is that stereogram of the library unit of unmanned plane after coverboard is omitted is parked in the utility model embodiment 1；
Fig. 3 is the stereogram of plug-type drawer structure in the utility model embodiment 1；
Fig. 4 is the stereogram of the plug-type drawer mechanism that card is pressed with unmanned plane in the utility model embodiment 1；
Fig. 5 is the structural representation of bottom library unit in the utility model embodiment 2；
Fig. 6 is the backside configuration schematic diagram of bottom library unit in the utility model embodiment 2；
Fig. 7 is the structural representation of drawer structure in the utility model embodiment 2；
Fig. 8 is the structural representation of card pressure component in the utility model embodiment 2；
Fig. 9 is the structural representation of top library unit in the utility model embodiment 3.
Embodiment
With reference to embodiments and its accompanying drawing the utility model is described in further detail.
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
Unit 23 and top library unit 24, connection is removably secured by fixture between adjacent two layers library unit, in actual use
Can be according to the library unit that need to stop the unmanned plane quantity configuration difference number of plies.
Referring to Fig. 1 to Fig. 4, the structure of library unit is illustrated by taking the library unit 1 of bottom as an example, 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,
A pair of card pressure components 5 and the push-and-pull actuator 63 for driving draw back plate 3 to be 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, aligning guide device 7 includes 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.
Walking mechanism includes 52, two Der Laengslenkers being parallel to each other 53 of transverse support bar and can slided along Der Laengslenker 53
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
Fixed via, three claws 51 is fixed with 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 as charging electrode.Der Laengslenker 53 forms 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 it is attached on card pressure surface
Net metal electrode substitute conductive fibre fabric as charging electrode.
It is fixed on the claw 51 in same root transverse support bar 52 and forms 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 on machine level ground 4 is mobile or is moved away from.
Draw back plate 3 is slidably connected by sliding block 53 and 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 connects, 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 that movable device is caused to interfere.Cable connection power supply output stage, pass 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, and passes through the power supply change-over device of inside, there is provided the power supply standard needed for unmanned plane charging.
Guide device is aligned on the aircraft gate centre position of airplane parking area, is gathered by the airborne camera of unmanned plane 01
Afterwards, identified by unmanned plane image identification function, the location data with reference to caused by 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 to drive solar panel along slide rail by linear electric motors, single to top storehouse to realize
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 export direction 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 as to which unmanned plane be 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 are released, while wedge-shaped claw moves to both sides, are discharged unmanned plane undercarriage, that is, are 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.Preheated for example, starting air-conditioning when environment temperature is less than 10 DEG C for unmanned plane, start air-conditioning when environment temperature is higher than 30 DEG C
Cool for unmanned plane.
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,
It is also to be uploaded in real time on management and running platform by communication module that whether protection device, which normally waits key parameter,.
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 to obtaining the positional information of hangar, and by communication module by this information access unmanned plane management
Platform, reference is provided for unmanned plane.
Controller is the control axis of unmanned plane hangar, and it gathers each component working state by the electronic circuit of inside
Information, control instruction is produced, each executing agency's co-operating is controlled, 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 obtains
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 shutdown storehouse, pass through
The guide device that aligns being arranged on aircraft gate aligns landing, passes through authentication, you can starts 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 are 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 slowly to fall, and
In descent, constantly basis aligns guide device 7 and carries out pose adjustment.
(3) after unmanned plane is stably accommodated on airplane parking area 4, the label recognizer that is now connected with controller communication
Start the label of scanning uav bottom, carry out authentication, after identifying 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 avoid 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
Charged to unmanned machine battery, 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 accordingly unmanned machine battery fills with management and running platform, while ejector plate 241 or exit airplane parking area
4, two groups of claws move to both sides, unclamp unmanned plane, and unmanned plane is in state to be flown.
(5) fly away from and shut down after storehouse continues continuation of the journey after unmanned plane, top plate 241 or airplane parking area 4 are closed, and the library unit is in and treated
Machine 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 three movement area, hangar workspace and service area sections.
Movement area is the workplace of unmanned plane, and unmanned plane is flown in workplace and the device measuring by carrying with
Target environment, gather corresponding data and the target information collected is sent to high in the clouds, 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 is when the outside instruction to hangar of acquisition, for example obtains people
The instruction of machine takeoff and landing, high in the clouds control the instruction such as temperature, by parsing these instructions, are sent accordingly 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
Action is made, and the status information of the hangar of collection can also be sent to system controller from control, for example, hangar closure or open,
Whether charging, a series of status informations, the system controller such as unmanned plane state, state of temperature 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 is also the region of man-machine interaction.System controller
Substantial amounts of data are obtained, after the detailed analysis of these data, 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, realize the work(of remote monitoring
Energy.
It is as follows for the partial duty flow of hangar in systems：
Take off landing of its controller by receiving unmanned plane instructs or the landing of taking off of the control unmanned plane of server end
The open or close of instruction control distribution library unit, while controller can also be by detecting whether unmanned plane reaches, to control
Make the open or close of the charging hangar of distribution.After detecting that unmanned plane reaches, controller control claw fixes nobody
Machine simultaneously closes equipment compartment, whether needs the charge function corresponding to execution that charges according to unmanned plane after closure.If temperature detection passes
Sensor detects that the temperature 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 controller can also receive the temperature of the temperature adjusting instruction control hangar in high in the clouds and reach 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
The temperature information of the status informations such as charge condition, location status and hangar, hangar correspond to whether 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 set to perform 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 utility model embodiment 2, the difference only pair with above-described embodiment 1 is said below
It is bright.
Referring to Fig. 5 to Fig. 8, airplane parking area 4 is a hollow out harden structure, and it is supported between draw back plate 32 by polylith supporting plate,
Form the ventilative aerial 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, it is hinged between front panel 34 and draw back plate 32 by hinge, the around hinge hinge of front panel 34 is promoted by actuator 36
Rotate, it is logical by being set on airplane parking area 4 and side plate 33 to control front panel 34 to switch between tiling position and erection position
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, improve 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, the authentication information included for reading the electronic tag on unmanned plane.
Running status warning lamp 91, waterproof plug for industrial use 95, power output socket and sky are installed in library unit side wall
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 on the notch 41, and the two of resealable zipper
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.
The position for droping to unmanned plane on airplane parking area 4 can be adjusted using process, claw 51, 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 both 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 forms 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 electrically connects 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 forms four tapes in the present embodiment together the feedback detection charging structure of voltage compensation, of courses, can incite somebody to action
They are arranged to more than five lines the feedback detection charging structure with voltage compensation.
The mounting groove for installing Kato 87 is offered on the matrix of claw 51, thermocouple is installed on Kato 87, should
Thermocouple is used to be monitored the temperature variations of claw 51 in charging process.
The installation unit of claw 51 include can along longitudinal rail 81 slide slide 84, optical axis 85, straight line flange bearing 88,
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 fast in fixed seat 98 to be removably mounted on
The formula falcon of tearing open 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, it 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 are stored in controller and deposited
Computer program in reservoir is to realize following steps：
(1) in charging process, if detect that the temperature of claw 51 is higher than the first temperature threshold, control actuator driving
Claw 51 discharges unmanned plane undercarriage, and moves to card pressure charge position again and charged, and repeats release steps and is pressed with card again
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 charging process more than twice in succession all detects that the temperature of claw exceedes second temperature threshold value, send
Change the prompting of electrode.The continuous aging with the use of electrode, its resistance is caused 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 utility model embodiment 3, the difference only pair with above-described embodiment 1 is said below
It is bright.
Referring to Fig. 9, sensor 96 is installed with the lateral wall of library unit, sensor 96 is integrated with wind sensor, light passes
Sensor and rain sensor, to be detected to the environmental aspect around hangar, and place in controller is sent to by data are detected
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.
For this example only to illustrate technical concepts and features of the present utility model, its object is to allow person skilled in the art
Scholar can understand content of the present utility model and implement according to this, can not limit the scope of protection of the utility model with this.All
The equivalent change or modification made according to the utility model Spirit Essence, it should all cover within the scope of protection of the utility model.
Claims (13)
1. a kind of unmanned plane shuts down storehouse, including controller, airplane parking area and the automatic charge device controlled by the controller；
It is characterized in that：
The automatic charge device includes a pair of cards and presses component, 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：
Card is installed on the claw and is pressed onto a detection switch.
3. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
Charging electrode on the claw detects charging structure for the more than four lines feedbacks with voltage compensation.
4. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
Temperature detection sensor is installed on the claw.
5. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
The airplane parking area is provided with the notch slid through for the claw, and sliding part is installed with by described between the notch both sides
The resealable zipper that claw is pulled or promoted.
6. 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.
7. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
The airplane parking area is provided with NFC/RFID card reader at its aircraft gate and aligns guide device；
The unmanned plane is shut down and is provided with wind sensor, optical sensor and rain sensor on the outer wall in storehouse.
8. 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 slider and the driving transverse direction
The actuator that sliding block slides 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.
9. unmanned plane according to claim 1 shuts down storehouse, it is characterised in that：
The airplane parking area is engraved structure.
10. 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.
11. the unmanned plane according to any one of claim 1 to 10 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 slides, the airplane parking area and the card
Component is pressed to be arranged on the draw back plate.
12. unmanned plane according to claim 11 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.
13. unmanned plane according to claim 11 shuts down storehouse, it is characterised in that：
The front panel of the plug-type drawer structure is hinged with the draw back plate, and the plug-type drawer structure, which is provided with, promotes institute
State the actuator that front panel rotates around hinge between closing position and tiling position.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720614879.8U CN207028881U (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 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720614879.8U CN207028881U (en) | 2017-05-27 | 2017-05-27 | A kind of unmanned plane shuts down storehouse |
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| Publication Number | Publication Date |
|---|---|
| CN207028881U true CN207028881U (en) | 2018-02-23 |
Family
ID=61469999
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| Application Number | Title | Priority Date | Filing Date |
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| CN201720614879.8U Active CN207028881U (en) | 2017-05-27 | 2017-05-27 | A kind of unmanned plane shuts down storehouse |
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| Country | Link |
|---|---|
| CN (1) | CN207028881U (en) |
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| CN108454859A (en) * | 2018-05-16 | 2018-08-28 | 星际控股集团有限公司 | A kind of fixed mechanism of unmanned plane on intelligent warning lamp |
| CN108490971A (en) * | 2018-03-21 | 2018-09-04 | 深圳臻迪信息技术有限公司 | Unmanned plane job platform |
| WO2018219226A1 (en) * | 2017-05-27 | 2018-12-06 | 星逻智能科技(苏州)有限公司 | Unmanned-aerial-vehicle hangar |
| WO2019127225A1 (en) * | 2017-12-28 | 2019-07-04 | 深圳市大疆创新科技有限公司 | Positioning device for unmanned aerial vehicle |
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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 |
| GB2583418B (en) * | 2017-05-27 | 2022-08-03 | Skysys Intelligent Tech Suzhou Co Ltd | Drone parking garage |
| GB2583418A (en) * | 2017-05-27 | 2020-10-28 | Skysys Intelligent Tech Suzhou Co Ltd | Unmanned-aerial-vehicle hangar |
| WO2019127225A1 (en) * | 2017-12-28 | 2019-07-04 | 深圳市大疆创新科技有限公司 | Positioning device for unmanned aerial vehicle |
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| CN108490971A (en) * | 2018-03-21 | 2018-09-04 | 深圳臻迪信息技术有限公司 | Unmanned plane job platform |
| CN108454859A (en) * | 2018-05-16 | 2018-08-28 | 星际控股集团有限公司 | A kind of fixed mechanism of unmanned plane on intelligent warning lamp |
| CN111055751A (en) * | 2018-05-31 | 2020-04-24 | 南京涵曦月自动化科技有限公司 | On-vehicle unmanned aerial vehicle storage device that uses |
| CN110871905A (en) * | 2018-08-30 | 2020-03-10 | 一飞智控(天津)科技有限公司 | Lifting parking lot for logistics unmanned aerial vehicle and control method thereof |
| CN110173144A (en) * | 2019-04-16 | 2019-08-27 | 同济大学 | A kind of centering rechargeable unmanned plane shutdown library |
| CN110173144B (en) * | 2019-04-16 | 2020-07-28 | 同济大学 | Centering charging type unmanned aerial vehicle parking garage |
| CN110043094B (en) * | 2019-04-16 | 2020-04-07 | 同济大学 | On-vehicle unmanned aerial vehicle parking garage |
| CN110043094A (en) * | 2019-04-16 | 2019-07-23 | 同济大学 | A kind of vehicle-mounted unmanned aerial vehicle shutdown library |
| CN113060042A (en) * | 2019-12-31 | 2021-07-02 | 天津大学 | Unmanned aerial vehicle battery reloading platform and unmanned aerial vehicle battery reloading method based on manipulator |
| CN111056032A (en) * | 2020-01-20 | 2020-04-24 | 上海交通大学 | Unmanned ship-borne unmanned aerial vehicle charging lifting system and implementation method |
| CN111056032B (en) * | 2020-01-20 | 2021-07-20 | 上海交通大学 | Unmanned ship-borne unmanned aerial vehicle charging lifting system and implementation method |
| CN112061412A (en) * | 2020-08-11 | 2020-12-11 | 上海瀚沧科技有限公司 | Unmanned aerial vehicle intelligence hangar suitable for multiple installation demand |
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| CN113428027A (en) * | 2021-07-02 | 2021-09-24 | 星逻智能科技(苏州)有限公司 | Centralized unmanned aerial vehicle rapid refrigeration constant temperature system |
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