CN110053503A - A kind of solar energy unmanned plane automatic charging room - Google Patents
A kind of solar energy unmanned plane automatic charging room Download PDFInfo
- Publication number
- CN110053503A CN110053503A CN201910440488.2A CN201910440488A CN110053503A CN 110053503 A CN110053503 A CN 110053503A CN 201910440488 A CN201910440488 A CN 201910440488A CN 110053503 A CN110053503 A CN 110053503A
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- China
- Prior art keywords
- unmanned plane
- block
- cover
- charging
- spring
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- Granted
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- 238000007600 charging Methods 0.000 title claims abstract description 96
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 36
- 238000007789 sealing Methods 0.000 claims abstract description 23
- 229910052802 copper Inorganic materials 0.000 claims description 34
- 239000010949 copper Substances 0.000 claims description 34
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 33
- 210000002683 foot Anatomy 0.000 claims description 8
- 238000009434 installation Methods 0.000 claims 1
- 230000001681 protective effect Effects 0.000 abstract description 4
- 230000003628 erosive effect Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 5
- 230000002411 adverse Effects 0.000 description 2
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
Classifications
-
- 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
- B60L53/30—Constructional details of charging stations
-
- 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
-
- 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
-
- 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
Abstract
The embodiment of the invention discloses a kind of solar energy unmanned plane automatic charging rooms, including main body frame, in the upper surface of the main body frame, there are four sealing covers for rotation connection, and the adjusting component for driving sealing cover rotation is equipped in the upper end of the main body frame, the upper surface of the main body frame is equipped with placing modules, charging assembly is installed above the placing modules, the equipment is provided with charging assembly, its erosion that can sufficiently completely cut off extraneous rainwater by water retaining cover when in use, so that situations such as unmanned plane is not in short circuit when charging, simultaneously when unmanned plane charging, the charging end of unmanned plane can be clamped and be limited under the action of charging holddown spring by gripping block, even if there is strong wind atmosphere in the external world, unmanned plane will not move easily, the case where cannot proceed normally so as to avoid charging, its protective is higher.
Description
Technical field
The present embodiments relate to unmanned plane fields, and in particular to a kind of solar energy unmanned plane automatic charging room.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer.Compared with manned aircraft, nobody
Machine is often more suitable for the task of those too " slow-witted, dirty or dangerous ", and unmanned plane can consume great electricity when in use, therefore make
User will use various equipment and charge, and traditional unmanned plane is all that then battery charges again by changing battery, operation compared with
Be it is cumbersome and need to frequently replace battery, and New-type charge equipment now can by the modes such as solar panel electric power storage into
Row plugs in, so that operation is simpler laborsaving.
But the unmanned plane charging equipment common currently on the market is generally faced with, and charged area is all direct and extraneous ring
Border contact, once phenomena such as extraneous rain is dropped in charged area, will result in short circuit when being charged later generation, together
When most of charging platforms safeguard procedures it is smaller, if encountering adverse circumstances such as strong wind atmosphere, just easily blown unmanned plane
Charging is caused to cannot proceed normally.
Summary of the invention
For this purpose, the embodiment of the present invention provides a kind of solar energy unmanned plane automatic charging room, with solve in the prior art due to
Charged area be all directly contacted with external environment, once extraneous rain is dropped in charged area, when being charged later
Phenomena such as will result in short circuit generation, while the safeguard procedures of most of charging platforms are smaller, if encountering adverse circumstances such as strong wind
Environment just easily makes unmanned plane be blown the problem of causing charging cannot proceed normally.
To achieve the goals above, embodiments of the present invention provide the following technical solutions:
A kind of solar energy unmanned plane automatic charging room, including main body frame rotate in the upper surface of the main body frame and connect
Sealing cover there are four connecing, and the adjusting component for driving sealing cover rotation, the body frame are equipped in the upper end of the main body frame
The upper surface of frame is equipped with placing modules, is equipped with charging assembly above the placing modules；
The charging assembly includes the water retaining cover being slidably connected on placing modules, is symmetrically arranged with two in the water retaining cover
One side surface of a gripping block, the gripping block is connect by the holddown spring that charges with water retaining cover, and the gripping block is another
Side surface is equipped with copper sheet erecting bed, and the copper sheet erecting bed is equipped with charging copper sheet in the side close to water retaining cover, and in institute
It states and main charge sheet and secondary charge sheet is installed on copper sheet erecting bed, slidably connect anti-skidding copper sheet on the pair charge sheet, and
It is equipped with fixed insulating boot in the pair charge sheet, sliding insulating boot is slidably connected in the fixed insulating boot, the sliding is exhausted
Charging pushing top spring is fixedly installed between edge cover and fixed insulating boot.
As a preferred solution of the present invention, the placing modules include placing outer cover, place the upper of outer cover described
Side slidably connects placement block, and conductive platform is provided in the placement outer cover, and the top of the conduction platform connects equipped with several
Haptic element is equipped with sliding copper sheet above the contact feet, and the upper surface slide of the sliding copper sheet is connected with connected unit, described
The upper surface of connected unit is equipped with the connection component connecting with water retaining cover, and the block of placing is arranged in the side surface close to connected unit
There is ladder slide unit, and the center position for placing block lower surface is equipped with jack-up component, offers on the ladder slide unit
The component slippage slot of connection component is accommodated, the component slippage slot is provided with slip draw-in groove in the side close to connected unit, described
The pulley table being slidably connected with ladder slide unit is equipped in slip draw-in groove.
As a preferred solution of the present invention, the component that jacks up includes being fixedly installed in the adjusting for placing block lower surface
Spring is jacked up, the adjusting jacks up spring and is equipped with jack-up fixed block in the one end for being located remote from block, and the jack-up fixed block is left
The outer wall of right two sides offers adjusting block sliding slot, and the center position at left and right sides of the jack-up fixed block is provided with bullet
Spring fixed block, the adjusting block sliding slot is interior to be equipped with the adjusting slider being slidably connected with jack-up fixed block, the adjusting slider and bullet
It is fixedly installed with adjusting between spring fixed block and jacks up spring, the adjusting slider jacks up bar by connection and connect with connected unit.
As a preferred solution of the present invention, the connection component include the connection insulating boot being connect with connected unit and
The connection conductive shield connecting with water retaining cover is equipped in the connection insulating boot and connect the connection conduction that conductive shield is slidably connected
Piece, the connection conductive sheet is interior to be equipped with spring insulating boot, is equipped with and connect the connection of conductive shield connection in the spring insulating boot
Sliding spring.
As a preferred solution of the present invention, the upper surface for placing outer cover, which is equipped with, blocks component slippage slot
Sliding slot block cover.
As a preferred solution of the present invention, the sealing cover includes that several being rotatablely connected with main body frame block
Lid, the upper end of the shielding cover is equipped with rain-proof cover, and the shielding cover is being equipped with the sun close to the side surface for placing outer cover
It can solar panel and connecting column.
As a preferred solution of the present invention, the adjusting component includes the rotate gear being arranged in main body frame,
The side wall of the rotate gear is equidistantly equipped with several rack slides, is connected with above the rack slide through main body
The pulling platform of frame, the pulling platform are connect by adjusting yoke with connecting column.
As a preferred solution of the present invention, the cross section of the water retaining cover is U-shaped structure, and the water retaining cover
Height number is less than the height number of sliding slot block cover.
As a preferred solution of the present invention, the cross section of the ladder slide unit is ladder structure of right angle.
As a preferred solution of the present invention, the length value of the rack slide is greater than the diameter number of rotate gear
Value.
Embodiments of the present invention have the advantages that
(1) equipment is provided with charging assembly, can sufficiently completely cut off invading for extraneous rainwater by water retaining cover when in use
Erosion, so that situations such as unmanned plane is not in short circuit when charging, while when unmanned plane charging, gripping block can compress bullet in charging
The charging end of unmanned plane is clamped and limited under the action of spring, even if strong wind atmosphere occurs in the external world, unmanned plane will not be light
Easily mobile, the case where cannot proceed normally so as to avoid charging, protective is higher；
(2) equipment is provided with jack-up component, when unmanned plane be pressed in place block on when, place block can under the effect of gravity under
Drop, the ladder slide unit declined later can be such that the connection component for jacking up component two sides is pushed to close to each other, then mutually lean on
Close connection component can be slided with charging assembly, and unmanned plane is fixed, and carry out charging operations, easy to operate, and can be fitted
For various sizes of unmanned plane, the scope of application is wider；
(3) equipment be provided with drive sealing cover rotation adjusting component, when equipment when not in use, adjusting can be passed through
Component rotates sealing cover, and when four sealing covers are each perpendicular to main body frame, entire placing modules can be blocked, thus
The case where part of appliance is smashed by external impurities is avoided, protective is higher, and equipment volume can be with free extension, side
Equipment transport.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of invention without any creative labor, may be used also for those of ordinary skill in the art
To obtain other attached drawings according to these attached drawings.
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is enlarged drawing at A in Fig. 1；
Fig. 3 is anti-skidding copper sheet main view partial sectional view of the invention；
Fig. 4 is placing modules overhead, partial cut-away view of the present invention；
Fig. 5 is ladder slide unit side view partial sectional view of the present invention；
Fig. 6 is overhead, partial cut-away view of the present invention；
Fig. 7 is placing modules main view sectional view of the present invention.
In figure:
1- main body frame；2- battery；3- adjusts component；4- sealing cover；5- placing modules；6- charging assembly；7- is jacked up
Component；8- charging column；
301- rotate gear；302- rack slide；303- pulls platform；304- adjusting yoke；
401- shielding cover；402- rain-proof cover；403- solar panel；404- connecting column；
501- places outer cover；502- conduction platform；503- contact feet；504- slides copper sheet；505- connected unit；506- ladder is sliding
Platform；507- connection component；508- pulley table；509- places block；510- connection conductive shield；511- connection insulating boot；512- connection
Conductive sheet；513- spring insulating boot；514- connection sliding spring；515- sliding slot block cover；516- slip draw-in groove；517- component slippage
Slot；
601- water retaining cover；602- gripping block；603- charging copper sheet；604- charging holddown spring；605- copper sheet erecting bed；
The main charge sheet of 606-；607- pair charge sheet；The anti-skidding copper sheet of 608-；609- fixes insulating boot；610- slides insulating boot；611- charging
Pushing top spring；
701-, which is adjusted, jacks up spring；702- jacks up fixed block；703- adjusting block sliding slot；704- adjusting slider；705- connection
Jack up bar；706- spring anchor block；707-, which is adjusted, jacks up spring.
Specific embodiment
In order to make the invention's purpose, features and advantages of the invention more obvious and easy to understand, below in conjunction with the present invention
Attached drawing in embodiment, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that disclosed below
Embodiment be only a part of the embodiment of the present invention, and not all embodiment.Based on the embodiments of the present invention, this field
Those of ordinary skill's all other embodiment obtained without making creative work, belongs to protection of the present invention
Range.
As shown in Figure 1, the present invention provides a kind of solar energy unmanned plane automatic charging room, main purpose is to pass through charging
Component 6 completely cuts off the erosion of extraneous rainwater, so that situations such as unmanned plane is not in short circuit when charging, while can also pass through charging group
The charging end of unmanned plane is clamped and is limited by the gripping block 602 on part 6, and avoiding unmanned plane movement causes charging cannot be just
The case where often carrying out can allow equipment to not by jacking up component to carry out position adjusting to charging assembly 6 later
With size unmanned plane carry out charging operations, and can also by adjust component 3 come to sealing cover 4 carry out rotation process, make its
Entire placing modules 5 can be blocked when not in use to exist as shield, while the sealing cover 4 closed up can also reduce equipment
Volume keeps its transport more convenient.
Including main body frame 1, in the upper surface of the main body frame 1, there are four sealing cover 4, the sealing covers 4 for rotation connection
It is provided with the identical sealing cover 4 of four structures altogether, and is equipped with the tune for driving sealing cover 4 to rotate in the upper end of the main body frame 1
Component 3 is saved, is equipped with battery 2 in the lower section of the adjusting component 3, so that the electricity that solar panel 403 is converted is stored,
The upper surface of the main body frame 1 is equipped with placing modules 5, and the top of the placing modules 5 is equipped with charging assembly 6.
In present embodiment, in order to allow charging assembly 6 normally to realize charging, therefore in the upper table for placing block 509
Face is provided with charging column 8, and the both ends of the charging column 8 are provided with mounting rack, and the mounting rack is equipped with engaging set, the engaging
Set can be fixed on unmanned plane, so that charging column 8 and unmanned plane are fixed together, and charging column 8 can also pass through power supply
Line is connect with the battery on unmanned plane, so that the received electric current of charging column 8 can be transmitted to unmanned plane.
When in use, user can be opened four sealing covers 4 by adjusting component 3 equipment, to start conversion simultaneously
Stored current can make it drop to the top of placing modules 5, so that charging assembly 6 blocks once unmanned plane needs to charge later
Firmly the charging column 8 on unmanned plane carries out charging operations, and when in use, waterproofness is higher for more traditional equipment, and will not be easily
It is influenced by strong wind, while its scope of application is wider.
As shown in Figure 1, Figure 2 and Figure 3, one of the main feature in the charging room is, the charging assembly 6 includes that sliding connects
The water retaining cover 601 on placing modules 5 is connect, the water retaining cover 601 is altogether there are two settings, and two water retaining covers 601 are respectively about putting
It sets component 5 to be symmetrical arranged, arranged symmetrically in the water retaining cover 601 there are two gripping block 602, the side tables of the gripping block 602
Face is connect by the holddown spring 604 that charges with water retaining cover 601, and another side surface of the gripping block 602 is equipped with copper sheet peace
Platform 605 is filled, the copper sheet erecting bed 605 is equipped with charging copper sheet 603, the charging copper sheet 603 in the side close to water retaining cover 601
It is electrically connected with conductive shield 510 is connect, the mode of connection can be through power supply line, conductive copper sheet etc., and in the copper sheet
Main charge sheet 606 and secondary charge sheet 607 are installed on erecting bed 605, slidably connect anti-skidding copper sheet on the pair charge sheet 607
608, and it is equipped with fixed insulating boot 609 in the secondary charge sheet 607, sliding is slidably connected in the fixed insulating boot 609
Insulating boot 610 is fixedly installed with charging pushing top spring 611 between the sliding insulating boot 610 and fixed insulating boot 609.
The charging assembly 6 when in use, drives once water retaining cover 601 is connected conductive shield 510 towards the sliding of charging column 8,
Two gripping blocks 602 can be pushed when contacting charging column 8 opens, while the holddown spring 604 that charges can be also extruded, so that its
Elastic force increase tentatively limits the position of charging column 8, and charging column 8 can enter between two gripping blocks 602 later, at this time anti-skidding copper
The charging column 8 that piece 608 can be snapped into pushes to slide along secondary charge sheet 607, and with sliding insulating boot 610 along fixation
Insulating boot 609 slides, to squeeze charging pushing top spring 611, column 8 to be charged touches main charge sheet 606 later, ejection of charging
Spring 611 can reset, so that sliding insulating boot 610 resets, while the reset of anti-skidding copper sheet 608 skids off and by the position of charging column 8
It limits, it will not be movable easily the external world has strong wind to blow unmanned plane under the gripping of two charging assemblies 6.
As shown in Figure 1, Figure 2, shown in Fig. 4, Fig. 5 and Fig. 7, the two of the main feature in the charging room are, the placing modules 5 wrap
It includes and places outer cover 501, slidably connected in the top for placing outer cover 501 and place block 509, and in the placement outer cover 501
It is provided with conductive platform 502, the conduction platform 502, contact feet 503, sliding copper sheet 504 and connected unit 505 are conductive copper sheet system
At if can be by conductive platform 502, contact feet 503, sliding copper sheet 504 and connected unit 505 with power supply line generation in order to save cost
It replaces, the top of the conduction platform 502 is equipped with several contact feets 503, and the top of the contact feet 503 is equipped with sliding copper sheet
504, the upper surface slide of the sliding copper sheet 504 is connected with connected unit 505, and the upper surface of the connected unit 505 is equipped with and gear
The connection component 507 that water cover 601 connects, which can make 6 use of charging assembly close to placement block 509, described to put
It sets block 509 and the side surface close to connected unit 505 is provided with ladder slide unit 506, and the center for placing 509 lower surface of block
It is equipped at position and jacks up component 7, which is used to adjust the spacing between two charging assemblies 6, so that two chargings
Component 6 can freely reset, and the component slippage slot 517 for accommodating connection component 507 is offered on the ladder slide unit 506, described
Component slippage slot 517 is provided with slip draw-in groove 516 in the side close to connected unit 505, and the slip draw-in groove 516 is along ladder slide unit
506 settings, the slip draw-in groove 516 is interior to be equipped with the pulley table 508 being slidably connected with ladder slide unit 506.
The placing modules 5 when in use, once having unmanned plane to be placed on places 509 upper surface of block, place 509 meeting of block at this time
Since gravity pushes, later, ladder slide unit 506 can also glide with block 509 is placed, because of the cross of the ladder slide unit 506
Section is ladder structure of right angle, therefore ladder slide unit 506 can press against pulley table 508, makes it along component slippage slot 517 and towards close
The direction sliding of component 7 is jacked up, pulley table 508 can be moved with connected unit 505 and connection component 507 later, then charging group
Part 6 can also move closer to charging column 8, and be blocked carry out charging operations, after the completion of to be charged, unmanned plane can be made suitably to fly
It rises, is resetted so that jacking up component 7, charging assembly 6 is moved to initial position, unmanned plane can fly out the room that charges later.
As shown in Figure 1 and Figure 7, the component 7 that jacks up includes being fixedly installed in the adjusting jack-up bullet for placing 509 lower surface of block
Spring 701, the adjusting jack up spring 701 and are equipped with jack-up fixed block 702 in the one end for being located remote from block 509, which fixes
Block 702 is directly connected to main body frame 1, and the outer wall for jacking up 702 left and right sides of fixed block offers adjusting block sliding slot
703, and the center position in 702 left and right sides of jack-up fixed block is provided with spring anchor block 706, the adjusting block is sliding
The adjusting slider 704 being slidably connected with jack-up fixed block 702, the adjusting slider 704 and spring anchor block are equipped in slot 703
It is fixedly installed with adjusting between 706 and jacks up spring 707, the adjusting slider 704 jacks up bar 705 and connected unit 505 by connection
Connection.
When in use, unmanned plane is pressed at this time places on block 509 the jack-up component 7, later, adjusts and jacks up 701 meeting of spring
It is compressed, is gradually slided along main body frame 1 so that placing block 509, then, the placement block 509 of downslide can make 505 court of connected unit
The sliding of 702 direction of jack-up fixed block, the connected unit 505 slided later, which can push connection and jack up bar 705, to be rotated, while adjusting cunning
Block 704 can slide under the action of thrust along adjusting block sliding slot 703, and squeeze adjustments jack up spring 707, that is, increase adjusting
The elastic force of spring 707 is jacked up, later, when connected unit 505 is moved to the position that can not continue sliding, then represents charging assembly 6
Charging column 8 is sufficiently limited, if increasing the position of unmanned plane later, adjusts and jacks up the reset of spring 707, slided so that adjusting
The reset of block 704 resets connected unit 505, and charging assembly 6 can also be resetted with connected unit 505 later.
As shown in Figure 1, Figure 2 and Figure 7, the connection component 507 includes the connection insulating boot 511 connecting with connected unit 505
And the connection conductive shield 510 being connect with water retaining cover 601, the connection insulating boot 511 is interior to be equipped with and connect the sliding of conductive shield 510
The connection conductive sheet 512 of connection, the connection conductive sheet 512 is interior to be equipped with spring insulating boot 513, which deposits
It is being to make to connect sliding spring 514 phenomena such as stretching in reseting procedure offset will not be generated, avoiding the occurrence of will connect
The case where conductive sheet 512 blocks, interior be equipped with of the spring insulating boot 513 are slided with the connection for connecting the connection of conductive shield 510
Spring 514.
When in use, if connected unit 505 is slided towards 702 direction of fixed block is jacked up, two are charged the connection component 507
Component 6 can be close to each other, and placing block 509 at this time can gradually glide, therefore between being generated between water retaining cover 601 and placement block 509
Gap, connecting sliding spring 514 later can gradually reset, so that connection conductive shield 510 is with water retaining cover 601 along connection conductive sheet
512 declines, later, when water retaining cover 601 is contacted again and places block 509, connection sliding spring 514 stops resetting, and works as nothing
It is man-machine leave place block 509 when, adjust jack up spring 701 can push place block 509 and connection conductive shield 510 is increased to initial bit
It sets, connecting sliding spring 514 at this time can be stretched.
The upper surface for placing outer cover 501 is equipped with the sliding slot block cover 518 blocked to component slippage slot 517, the cunning
Slot block cover 518 is in order to withstand component slippage slot 517 and instill extraneous rainwater will not, to further increase the waterproof effect of equipment
Fruit, because the cross section of the water retaining cover 601 is U-shaped structure, therefore water retaining cover 601 can sufficiently block rainwater that so that it will not connect easily
Anti-skidding copper sheet 608 and main charge sheet 606 are touched, and the height number of the water retaining cover 601 is less than the high degree of sliding slot block cover 518
Value, so that water retaining cover 601 will not be influenced by sliding slot block cover 518, is unable to fully be caught in water retaining cover 601 so as to avoid charging column 8
Interior situation occurs.
As shown in Figure 1, the sealing cover 4 includes several shielding covers 401 being rotatablely connected with main body frame 1, this is several
A shielding cover 401 can form sealing space after closing up makes simultaneously so that placing modules 5 will not contact rainwater easily
The protective for obtaining equipment is higher, and the upper end of the shielding cover 401 is equipped with rain-proof cover 402, and the shielding cover 401 is close to placement
One side surface of outer cover 501 is equipped with solar panel 403 and connecting column 404, which is normal in the market
The solar panel seen.
The sealing cover 4, which needs to cooperate when in use, adjusts the use of component 3, if sealing cover 4 rotates 90 degree, shielding cover 401
It can lie low with rain-proof cover 402 in the upper surface of main body frame 1, so that shielding cover 401 is parallel to main body frame 1, it is extraneous later
Sunlight is contacted with solar panel 403, so that solar energy is converted into electric energy, and is stored in battery 2.
As shown in figures 1 to 6, the component 3 that adjusts includes the rotate gear 301 being arranged in main body frame 1, the rotation
Gear 301 can be controlled by modes such as photo resistance or remote controls, and the side wall of the rotate gear 301 is equidistantly pacified
Equipped with several rack slides 302, the top of the rack slide 302 is connected with the pulling platform 303 through main body frame 1, should
Platform 303 is pulled to be equipped with several altogether, and several pull platform 303 corresponding with corresponding shielding cover 401 respectively, the pulling platform
303 are connect by adjusting yoke 304 with connecting column 404.
When in use, user can open rotate gear 301 to the adjusting component 3, later, control it and be rotated by 90 °, so
Rack slide 302, which will slide, afterwards slides so that platform 303 is pulled to be pulled towards corresponding shielding cover 401 so that shielding cover 401 is put
Flat, because the length value of the rack slide 302 is greater than the diameters of rotate gear 301, therefore rotate gear 301 is rotated by 90 °
Afterwards, rack slide 302 is still engaged with rotate gear 301, so that subsequent overturning resets operation and can still carry out again.
The above, the above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations；Although referring to before
Stating embodiment, invention is explained in detail, those skilled in the art should understand that: it still can be to preceding
Technical solution documented by each embodiment is stated to modify or equivalent replacement of some of the technical features；And these
It modifies or replaces, the spirit and scope for technical solution of various embodiments of the present invention that it does not separate the essence of the corresponding technical solution.
Claims (10)
1. a kind of solar energy unmanned plane automatic charging room, which is characterized in that including main body frame (1), in the main body frame (1)
Upper surface rotation connection there are four sealing cover (4), and be equipped in the upper end of the main body frame (1) and sealing cover (4) driven to revolve
The upper surface of the adjusting component (3) turned, the main body frame (1) is equipped with placing modules (5), the top of the placing modules (5)
Charging assembly (6) are installed；
The charging assembly (6) includes the water retaining cover (601) being slidably connected on placing modules (5), and the water retaining cover (601) is interior
It is symmetrical arranged there are two gripping block (602), a side surface of the gripping block (602) passes through charging holddown spring (604) and gear
Water cover (601) connection, and another side surface of the gripping block (602) is equipped with copper sheet erecting bed (605), the copper sheet installation
Platform (605) is equipped with charging copper sheet (603) in the side close to water retaining cover (601), and pacifies on the copper sheet erecting bed (605)
Equipped with main charge sheet (606) and secondary charge sheet (607), anti-skidding copper sheet (608) are slidably connected on the pair charge sheet (607),
And be equipped with fixed insulating boot (609) in the secondary charge sheet (607), cunning is slidably connected in the fixed insulating boot (609)
Dynamic insulating boot (610) are fixedly installed with charging pushing top spring between the sliding insulating boot (610) and fixed insulating boot (609)
(611)。
2. a kind of solar energy unmanned plane automatic charging room according to claim 1, which is characterized in that the placing modules
(5) include placing outer cover (501), placement block (509) is slidably connected above the placements outer cover (501), and described put
It sets in outer cover (501) and is provided with conductive platform (502), the top of the conduction platform (502) is equipped with several contact feets (503), institute
It states and sliding copper sheet (504) is installed above contact feet (503), the upper surface slide of sliding copper sheet (504) is connected with
Consecutive (505), the upper surface of the connected unit (505) is equipped with the connection component (507) connecting with water retaining cover (601), described to put
It sets block (509) to be provided with ladder slide unit (506) in the side surface close to connected unit (505), and placement block (509) following table
The center position in face, which is equipped with, jacks up component (7), offers on the ladder slide unit (506) and accommodates connection component (507)
Component slippage slot (517), the component slippage slot (517) are provided with slip draw-in groove in the side close to connected unit (505)
(516), the pulley table (508) being slidably connected with ladder slide unit (506) is equipped in the slip draw-in groove (516).
3. a kind of solar energy unmanned plane automatic charging room according to claim 2, which is characterized in that the jack-up component
It (7) include being fixedly installed in adjusting jack-up spring (701) for placing block (509) lower surface, the adjusting jacks up spring (701) and exists
The one end for being located remote from block (509), which is equipped with, jacks up fixed block (702), the outer wall jacked up at left and right sides of fixed block (702)
It offers adjusting block sliding slot (703), and the center position at left and right sides of jack-up fixed block (702) is provided with spring
Fixed block (706), the adjusting block sliding slot (703) is interior to be equipped with the adjusting slider being slidably connected with jack-up fixed block (702)
(704), it is fixedly installed with adjusting between the adjusting slider (704) and spring anchor block (706) and jacks up spring (707), it is described
Adjusting slider (704) jacks up bar (705) by connection and connect with connected unit (505).
4. a kind of solar energy unmanned plane automatic charging room according to claim 2, which is characterized in that the connection component
It (507) include the connection insulating boot (511) being connect with connected unit (505) and the connection conductive shield being connect with water retaining cover (601)
(510), the connection conductive sheet (512) for being equipped in connection insulating boot (511) and connecting conductive shield (510) and being slidably connected, institute
It states in connection conductive sheet (512) and is equipped with spring insulating boot (513), be equipped in the spring insulating boot (513) and connect conductive shield
(510) the connection sliding spring (514) connected.
5. a kind of solar energy unmanned plane automatic charging room according to claim 2, which is characterized in that the placement outer cover
(501) upper surface is equipped with the sliding slot block cover (515) blocked to component slippage slot (517).
6. a kind of solar energy unmanned plane automatic charging room according to claim 1, which is characterized in that the sealing cover (4)
Including several shielding covers (401) being rotatablely connected with main body frame (1), the upper end of the shielding cover (401) is equipped with rain-proof cover
(402), and the shielding cover (401) close to place outer cover (501) a side surface be equipped with solar panel (403) and
Connecting column (404).
7. a kind of solar energy unmanned plane automatic charging room according to claim 6, which is characterized in that the adjusting component
It (3) include the rotate gear (301) being arranged in main body frame (1), the side wall of the rotate gear (301) is equidistantly equipped with
Several rack slides (302) are connected with the pulling platform through main body frame (1) above the rack slide (302)
(303), the pulling platform (303) is connect by adjusting yoke (304) with connecting column (404).
8. a kind of solar energy unmanned plane automatic charging room according to claim 5, which is characterized in that the water retaining cover
(601) cross section is U-shaped structure, and the height number of the water retaining cover (601) is less than the high degree of sliding slot block cover (515)
Value.
9. a kind of solar energy unmanned plane automatic charging room according to claim 2, which is characterized in that the ladder slide unit
(506) cross section is ladder structure of right angle.
10. a kind of solar energy unmanned plane automatic charging room according to claim 7, which is characterized in that the rack slide
(302) length value is greater than the diameters of rotate gear (301).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910440488.2A CN110053503B (en) | 2019-05-24 | 2019-05-24 | Solar unmanned aerial vehicle automatic charging room |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910440488.2A CN110053503B (en) | 2019-05-24 | 2019-05-24 | Solar unmanned aerial vehicle automatic charging room |
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| Publication Number | Publication Date |
|---|---|
| CN110053503A true CN110053503A (en) | 2019-07-26 |
| CN110053503B CN110053503B (en) | 2024-02-09 |
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| CN201910440488.2A Active CN110053503B (en) | 2019-05-24 | 2019-05-24 | Solar unmanned aerial vehicle automatic charging room |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111071084A (en) * | 2019-12-18 | 2020-04-28 | 安徽原上草节能环保科技有限公司 | New forms of energy fill electric pile with anticollision function |
| CN114180089A (en) * | 2021-12-11 | 2022-03-15 | 浙江极客桥智能装备股份有限公司 | Unmanned aerial vehicle air park system |
| CN114633645A (en) * | 2022-03-28 | 2022-06-17 | 山东智航智能装备有限公司 | Unmanned aerial vehicle contact clamping device and contact charging device that charge |
| CN117799889A (en) * | 2024-02-29 | 2024-04-02 | 苏州物图科技有限公司 | Charging equipment for unmanned aerial vehicle and charging method thereof |
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| KR20190012021A (en) * | 2017-07-26 | 2019-02-08 | 한국전력공사 | Pole type drone charging station and method for charging and replacing battery of drone |
| CN210174651U (en) * | 2019-05-24 | 2020-03-24 | 广东电网有限责任公司 | Automatic room that charges of solar energy unmanned aerial vehicle |
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| CN206685921U (en) * | 2017-03-28 | 2017-11-28 | 东莞市北钺模型科技有限公司 | A kind of unmanned plane charging device |
| KR20190012021A (en) * | 2017-07-26 | 2019-02-08 | 한국전력공사 | Pole type drone charging station and method for charging and replacing battery of drone |
| CN107650717A (en) * | 2017-10-10 | 2018-02-02 | 江苏信扬智能设备有限公司 | A kind of unmanned plane charging platform |
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| CN114180089B (en) * | 2021-12-11 | 2024-02-02 | 浙江极客桥智能装备股份有限公司 | Unmanned aerial vehicle air park system |
| CN114633645A (en) * | 2022-03-28 | 2022-06-17 | 山东智航智能装备有限公司 | Unmanned aerial vehicle contact clamping device and contact charging device that charge |
| CN114633645B (en) * | 2022-03-28 | 2023-09-26 | 山东智航智能装备有限公司 | Unmanned aerial vehicle contact clamping device that charges and contact charging device |
| CN117799889A (en) * | 2024-02-29 | 2024-04-02 | 苏州物图科技有限公司 | Charging equipment for unmanned aerial vehicle and charging method thereof |
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| Publication number | Publication date |
|---|---|
| CN110053503B (en) | 2024-02-09 |
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